Concorde Takeoff & Landing Manual
Concorde Takeoff & Landing Manual
,1
T/OfI& Landing Notes. .
~-
AIRWAYS'
. ,1.2]
Concorde
~ 13]
Performance
Take-Oft Data
Major~rfields 1.4
Manual
LancfI1l9 Data
MajorAirfields 15
Part 1
Take-Oft Data
MalnAltemates 1.6
Landing Data
MalnAltemates 1.7
Despatch Deviationsl
-STATEMENT OF INITIAL CERTIFICATION Special Operalklns 1.
This Manual. complies with the current ANO
(Air Navigation Order), AL·15-05 and FTS-Ol·01. Icy I Slippery &
The inclusion of an uncertlfied revision will
invalidate this Certification.
Contaminated Data
AndNotes
1.9
/1
~dJ.#t4k kl6y~ '.( . Generalised
Clpt A•.Robtnson , '.. :'
Gene~1 Manager Flight·T~hnlC8I&,;~gy
landing Data 1.11
and ~i& applicable, on~~IfOf ~~.'• .-EngIneer, ~:-::~~
British A!rways r ech Se~. OAA,APPfcIvaJ
Nr.DAI/8566178
serial No
'"
.
,
Take-Ofl Data
=,:
Charter
.:..
~2
1.1
Thi$~~blic~tion forms part of the'BrltlshAlrways'
~:~~dhamtr"1..'"3'
DeStinations
,;app;oved Operatlons.Manual.- .... i
, I·;
c')" ::
•
.
., ......---N·IETIER OF TRANSNllrrAI
. REVISION 05D'" .".
This petnnlnent leviSlon isin compliance with the'stlItemenfbf approval at thefront ofthismanual. .
CONTENTS
1.0.1. OCT 9211)3 MAR 96/04 LONDON STANSTED
1.0.2. FEB 92/02 MAR 96/03 STN/01 & 8TN/02 OCT92/02 MAR 96/03
LETTER OF TRANSMITTAL
REVISION 050
Thispermanent revision is in compliance with the statement of approval at the front of this manual. ~
GlASGOW ST.LUClA
GLAIOI MAR 96/01 lNF/OI APR 93/04 MAR 96/05
LETTER OF TRANSMITTAL
REVISION 05D
This permanent revision is in compliance with thestatement of approval at thefrontof this manual.
BANGOR GANDER
BGRIOI & BGRI02 MAR 96/01 YllX/Ol &YllX/02 MAR 96/01
YQ)(.m3 &YQX,1l4 MAR 96/01
BOSTON
8OSIOl &BOSI02 MAR 96/01 GOOSE
BOS/03 & BOS/04 MAR 96/01 YYRlDI &YYRlD2 MAR 96101
BOSIOS &BOSI06 MAR 96/01
8OSI07 &BOSI08 MAR 96/01 HALIFAX
BOSI09 & 8OSIl0 MAR 96/01 YHZIOI &YIW02 MAR 96/01
80S/I1& 8OSI12 MAR 96/01 YHZI03 &YIW04 MAR 9&101
BOS/13 MAR 96/01
HUMBERSIDE
BRIZE NORTON HUY/OI &HUY/02 MAR 96101
BZ1I01 & BZ1I02 MAR 96/01
JEDDAH
CAIRO JEDIOl & J£O/02 MAR 96/01
CAVIll & CAf/02 MAR 96/01 J£OI03 & J£O/04 MAR 96/01
CAf/03 & CAV04 MAR 96/01 JEDI05 &J£O/06 MAR 96/01
CAVIlS & CAV06 MAR 9&101
LAJES
DUBUN lERIOl &lER/02 MAR 96/01
DUB/Ol &DUB/02 MAR 96/01
USBON
EAST MIDLANDS L1S/01 & L1S/02 MAR 95/01
EMAIlIl & EMAI02 MAR 96101 L1S103 &US/04 MAR 95/01
The Listof Effective Pages Issue 05is amended bythis lener of Transmittal,
Issue 06 will beissued in due course.
lOT/3
Revision: 050
Ref: sscpartl.1ot 14 MAY 96
BRmsH
AIRWAYS CONCORDE PERFORMANCE MANUAL Part 1
LETTER OF TRANSMITTAL
REVISION 05D
Thispermanent revision is in comp6ance with the statement of approval at the front of this manual.
LIVERPOOL PRESTWICX
LPIJ01 &LPIJ02 MAR 96,/01 PIIiI1l1 &PIK/02 MAR 96,/01
LUXOR RIVADH
LXR/01 &LXR/02 MAR 96,/01 R!JWOl &RUH/02 MAR 96,/01
RUH/03 &RUH/04 MAR 96101
MANSTON
MSflD1 &MSflD2 MAR 96,/01 ROVANIEMJ
RVWDl &RVNI1l2 MAR 96,/01
MARS8LLE
MRSIOl & MRS/02 MAR 96/01 SANTAMARIA
MRSI03&MRSI04 MAR 96101 SMA/II1 &SMA/02 MAR 96,/01
OPORTO TAlF
OPO/ll1 & OP0/lI2 MAR 96101 TlFllll &T1F102 MAR 96101
T1F/03 &T1F104 MAR 96,/01
OTIAWA
YOWJ01 &YOWJ02 MAR 96,/01 TEES-SIDE
YOWJ03 &YOW/04 MAR 96/01 MMfJ01 &MMf1D2 MAR 96,/01
PARISC.D.G VALO'OR
CDG/01 &CDG/02 MAR 96,/01 YVOIDl &YV0/lI2 MAR 96,/01
CDG/03 &CDG,IIl4 MAR 96/01
SECTION 1.13.
PARISORLY 1.13.1. MAR 96,/01
ORYI01 & ORYJ02 MAR 96,/01
ORYJ03 & ORYJ04 MAR 96,/01 BANGOR
ORYIOS & ORYI06 MAR 96,/01 BGlVOl MAR 96,/01
LETTER OF TRANSMITTAL
REVISION 050
~ This permanent revision is in compliance with the statement of approval at the frontof this manual.
BOSTON HUMBERSIDE
~1&B0S/02 MAR 9&101 HUYlOl MAR 96/01
8OS/03 & BOSJ04 MAR 96/01
JEDDAH
BRIZE NORTON JEDIO1& J£OI02 MAR 96/01
BZ1JOl MAR 9&101 JEDI03 MAR 96/01
CAIRO lAJES
CAVOl &CAV02 MAR 9&101 TERlDI MAR 96/01
CAV03 MAR 96/01
USBON
DUBUN LISi1>I &USI02 MAR 96/01
DUBIO 1 MAR 96/01
UVERPOOL
EAST MIDLANDS LPlIOl MAR 96/01
EMMl1 MAR 96/01
LUXOR
EDINBURGH LXRIOI MAR 96/01
£OVOl MAR 96/01
MANSTON
FARO MSfJOI MAR 96101
FAOlO1 MAR 96101
MARSEILLE
GANDER MRSIOl & MRSI02 MAR 96/01
YQXI01 & YQXI02 MAR 96/01
NIAGARA FALLS
GOOSE IAG/Ol MAR 96/01
YVRI01 MAR 9&101
OPORTO
HAUFAX OPO/OI MAR 96101
YH1/01 &YHl/02 MAR 96/01
LETTER OF TRANSMITTAL
REVISION 05D
This permanent revision is in compliance with thestatement ofapproval at thefrontof thismanual. ~
OTTAWA VAlUOR
YOW/OI & YOW/02 MAR 96/01 YVOIOl MAR 96,101
PARISc.D.G
COGIO1 & COGlO2 MAR 96101
PARISORlY
ORYI01 & ORYI02 MAR 96/01
ORY/03 MAR 95101
PRES1WICK
PIK/Ol MAR 96/01
RIVADH
RUIfJOl & RUH/lI2 MAR 96/01
ROVANIEMI
RVN/Ol MAR 96/01
SANTAMARIA
SMAJIll MAR 96101
SHANNON
SN1'Wl MAR 96/01
TAlF
T1FlOl &T1F102 MAR 96/01
TEES-SIDE
MMf,IOl MAR 95101
~
LEP,v3&LEP,v4 JUH~ 1.4.1. OCT91,v1 Jl'IV44 JUNW03
LEP/OS JUN9W5 Jl'1V45 MAY95A!4
BARBADllS JF1V4& MAY92,v4
CONTIHTS ElGWl &BGlIDZ MAY9MlZ JflV47 OCT91,vl
1.0.1. MAR9Ml4
1.0.Z. MARBfm LONDON HEATHROW TOlIOXTO
U/R,Vl MAY9Ml2 YYlIOl &YYlIOZ MAR9ftm
SECTION 1.1. U/R,VZ DEC !lCW1 Yn'll3 &YYlIll4 MAR9Ml2
1.1. OCT97,G3 LHMl3 & LHIWol DEC9lWl ~&YYlIO& MAR9Ml2
1.1.1. F£BBV03 LHRI05 MAY9MlZ :
1.1.2. AUGB1,v2 LHRIO& DECBlWl WASHINGTON DUWS
1.1.3. SEP !lCW1 LHRI07 DEC9lWl 1AlWl DEC !lCW1
1.1.4. F£BBV03 LHRI08 OCTBtm 1AlWZ DCTMZ
1.1.5. NOV9QI1l2 l.AAfi MAY9MlZ 1AlW3 DEC !lCW1
1.1.&. OCT91,v2 LHIV10 DEC 9Q,1l1 1AlW4 OCT92m
1.1.7. NOVB7,02 LHIV11 &LHIVlZ DEC9lWl 1AlW5 DEC !lCW1
1.1.8. SEP!lCWI LHIVl3 &LHIVl4 DEC !lCW1 1AlW6 OCT97,02
1.1.9. SEP9OJ01 LHIVlS AUG 9l1ll3 1AlW7 DEC 90101
1.1.10. AU091,v2 LHIVl& AUG 95102 1AlW8 OCT9tm
1.1.11. & 1.1.12. AUG91,v2 LHIVl7 DEC 9Q,1l1 1AlW9 DEC 90101
\.-, 1.1.13.
1.1.14-
AUG91,v2
SEP!lCWI
LHIV18
LHIVl9
AUG91,v2
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IAO/lI
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DEC 90101
1.1.15. FEB92.v4 IAIl(lZ OCT9tm
1.1.1&. AlIli91,v2 NEW YORICJ.f.ll 1AIl(l3 DEC !lCW1
1.1.17. SEP 9OJl)1 J~1 MAY9MlZ :
1.1.18. JULmS JFlIOZ DEC9lWl S£CTIONU
1.1.19, JUlm3 JFlI03&JFIVll4 DEC 90101
\ 1.1.20. DEC9OID3 JFlIOS MAY9MlZ INDEX
~ 1.1.21. &1.1.22- JUNW04 FlI06 F£B92m 1.5.1. OCT91,vl
1.1.23- JUNW04 7 &JflI08 DIe 9Q,1l1
1.I.Z4. MAY9Ml3 JflV09 AlIli9Ml3 BARBADOS
1.1.25. FEBB2IOZ JFlVIO FmBV03 BGlIDI APR 93Ill3
1.1.26, MAR8M1S JFICIII DECM' :
1.1.21, &1.1.28, MAR8Ml4 JFIV12 OCT91,vZ LONDON HEATHROW
1.1.29. MAR8M1Z JFIV13 MAY8S104 LHRIOI &LHR.vZ MAR8M16
"- - I.UG.
1.1.31.
MARBMlI
MARBMlI
JFIV14
JFIC/1S
JFlVI6
F£B9V03
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MAY8S104
LHMl3
:
NEW YORK JfIC
MAR9M1S
LEP/l
Issue: OS
Rct. S$cpartl.lep 20SEP 94
8ItmSH
AIRWAYS CONCORDE PERFORMANCE MANUAl Part 1
lEPI2
Issue: OS
20SEP 94 Rei: sscpart 1.lep
B_
ADlWA"" CONCORDE PERFORMANCE MANUAL Part 1
lEP/3
Issue: 05
ReI: SSCpart1.l8p 20SEP 94
IllmsIt
Al!WAVS CONCORDE PERFORMANCE MANUAL Part 1
IWlSTON
MSfJlll MARMl
:
MARS£lUE
MRSJDl &MlI$1l2 MARIMlI
:
NJAGAIlA fAllS
1A~1 MARMl
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OPOIlll MARIMll
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VOW,1l1 &VOW,1l2 MARMl
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CDG/tll & CD~2 MARIMlI
:
PARlSORl.Y
DRY,1l1 & DRY,1l2 MARMl
ORY,1)3 MARMl
:
PRESTWICK
PlX,1l1 MAR9M11
:
RlYADII
RUlWl &RUlW2 MAR9M11
:
RDVANIEMI
RVlWI MAR9M11
:
SANTAMARIA
SMMII MAR9M11
:
S1IANNDN
SN!'Wl MAR9M11
:
TAIf
1lf,1l1 & 1lf,1l2 MAR9Mll
:
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MMEIOl MARIMlI
:
VAlD'DR
MWl MARIMll
LEP/4
Issue: 05
20SEP 94 ReI: sscpart I.Iep
=ys CONCORDE PERFORMANCE MANUAL CONTENTS
Part 1
SECTION 1.1 •• INTRO. NOTES/ ALTERNATE MINIMA
Explanatory Notes to Take-Off Data 1.1.1. - 1.1.13.
Explanatory Notes to landing Data 1.1.14. -1.1.19.
Explanatory Notes to ADM 1.1.20. - 1.1.24.
Right Planning Minima forAlternate Airfields 1.1.25. - 1.1.31.
SECTION 1.2.- CONVERSION TABLES / fACTORS
Weights / Temperatures 1.2.1.
Pressure / Speeds 1.2.2.
Distances 1.2.3. - 1.2.6.
OFE v P.A. (ft) 1.2.1.
Standard Pressure Altitude 1.2.8.
Conversion Factors 1.2.9.
SECTION 1.3.- CORRECTIONS
Wind Vector Diagram 1.3.1.
Pressure Altitude Corrections 1.3.3.
Maximum Take-Off Weight Corrections 1.3.4.
ATOW less PLTOW 1.3.5. - 1.3.6.
Reheat Failure Stop / Go Chart 1.3.7.
2 Engine Zero Rate of Climb Speed 1.3.8.
Pitch Attitude in Climb 1.3.9.
Take-Off P1 Bug Settings 1.3.10.
Take-Off Total Fuel Row Bug Settings 1.3.11.
SECTION 1.4.
Take-Off Data / Minima MajorAirfields
SECTION 1.5.
Landing Data / AOM MajorAirfields
SECTION 1.6.
Take-Off Data / Minima MainAlternates
SECTION 1.7.
landing Data / AOM MainAlternates
SECTION 1.8.
Combinations of Dispatch Dev. / Special Ops. 1.8.1.
Dispatch With Certain Items of Equipment U/S 1.8.2. • 1.8.14.
Dispatch With Certain Items ofEquipment Missing 1.8.15.
Fuel Saving Landings 1.8.16.
Carriage ofWide Cut (JP4) Type Fuel 1.8.11. - 1.8.18.
Take-Off Without Reheat 1.8.19. - 1.8.20.
Dispatch With Gear locked Down 1.8.21. - 1.8.26.
I ,)
i ",J
~
BRITI8K
AmwAYS CONCORDE PERFORMANCE MANUAL INTRO NOTES
TAKE-OFF
Take-off Minima are published. for all approved runways, on the Take-Off Data Pages for the
relevant runways, or, for those airfields where only Landing Data pages are provided. on
separate Take-off Minima Pages in Section 1.6.
N.B. If Take-off Minima is not published the runway is NOT APPROVED for take-off.
Where these values are subject to certain conditions. the published figures will be annotated '••
and an explanatory note will appear in the Notes section at the bottom of the page Ier on the
Take-off Minima Page where applicable).
This Notewill contain a statement of RVR requirement for take-off guidance, the position
(relative to the Airfield) of anyobstacles which arerequired to beidentified visually after
take-off, and theMet.Visibility and cloud-base required to achieve this -
ego "RVR for take-off guidance is ......rn. Obstacle(s) in initial climb path at (positions relative to
Airfield) must beidentified visually during initial climb:'
Normally RVR values are established in accordance with thefollowing table which should be
used if certain runway guidance aids leg.centre-line lights) arenot available at thetimeof
take-off:-
B. Visible painted Rwy ell plus edge guidance DAY and NIGHT - 20lJm
TDZ RVR & MID POINT (if reported). must beat or above minima. STOP END RVR is advisory only.
If actual TOW is close to RTOW, it is recommended thatthe STOP END RVR should be at or
above minima. These values will apply except where State Minima areover-riding.
If a Captain needs to determine minima for anAirfield I Runway for whichthereis none
published, either contactAerodromes & Performance (asperpara 1.1.1.) or,if this is not
possible, use ClG 100llft, VIS 5km. ~
The standard Take-off Minima is CLG NIL. VIS O.5sm forfourengined aircraft. The standard figure
is approved at all airfields unless a higher value is specified. On runways where standard
Take-off Minima are approved. the following minima are also approved:-
A. CLG NIL. VIS O.25sm (or RVR 16OOft). providing the runway is equipped with serviceable:-
4. In unusual circumstances. where none of the above are available. the runway is marked
in such a manner that the pilothas. at all times. visual reference sufficient for directional
guidance throughout the take-off run.
B.Touchdown RVR 1200ft with RVR 10001t on rollout end. providing the runway is equipped with
serviceable:-
2. Two operative transmissometers, either of which is not capable of reading lower than
RVR 1000ft.
C. Touchdown RVR 600ft with Mid-point RVR 600ft lif operative) and RVR 600ft on rollout end
provided the runway is equipped with serviceable:-
N.B. Where only two transmissometers are installed. the touchdown and rollout RVRs are
required. 11 three transmissameters are installed. the failure of anyone will nat affect
operations provided the two remaining RVRs are at or above the appropriate minimums
slated above.
A. CLG NIL. VIS O.25sm lor RVR 14OOft), providing the runway is equipped with serviceable:-
B. CLG NIL. RVR 6OlJft, providing the runway is equipped with serviceable:-
N.B. Touchdown and Mid-point trall$missometers must also be available, and neither to be
reading less than RVR 600ft.
N.B. In practicethe reheated climb may be required during the acceleration to en-route
climb speed.
No correction is necessary for the use of engine anti-icing during Take-Off at 3"C or below nor
for the use of air conditioning.
Operation of the fuel heater and airframe anti-icing systems have no effect on RTOW and
Take-Off speeds.
ALTERNATIVE 1
1st Segment - starts at the 35' point and ends when the undercarriage is retracted; it is
flown at Vz. The slope of the net flight path is never less than 1% in this
segment.
2nd Segment· is flown at Vz with the undercarriage retracted and ends at a net height of
600 feet above the runway.
ALTERNATIVE 2
1st Segment - starts at the 35ft point and ends when the undercarriage is retracted; it is
flown at Vz. The slope of the net flight path is never less than 1% in this
segment.
2nd Segment - is flown at Vzwith theundercarriage retracted and ends at such a height that
contingency rating is available until the end of the 3rd Segment.
3n1 Segment - is flownlevel at thepredetermined height (between 600 and 1500 ft) whilstthe
aircraft accelerates to Vz + 4D knots.
N.B. The 4d1 Segment will not be required if die 3rd Segment is flown at 15OOft.
It is permissible to extrapolate for a maximum of :re beyond the range of temperatures given on
the Take-Off data pages as follows:-
- For temperatures LOWER than the lowest tabulated temperature, use the MTOW and
associated Take-Off speeds at the lowest tabulated temperature.
- For temperatures HIGHER than the highest chart temperature, reduce the MTOW at this ~
temperature by 1.000kgJOe up to a maximum of :re. Use the Take-Off speeds at the
highest tabulated temperature.
Do not attempt to extrapolate for a particular temperature and wind component where no data
has been given.
The following Take-Off speeds are given for each temperature and wind combination:- ~
V, - The DRY runway decision speed. V,WET is obtained by subtracting 15kt from V,DRY.
The minimum allowable V,. V,MIN. is 132kt.
VR - The Rotation Speed is the target speed at which the pilot initiates action to change
pitch attitude with the intention of leaving the ground. The minimum allowable VR,
VRMIN, is 139kt.
Vz - The initial climb out speed. one engine inoperative, is the target speed at the screen
height (35h) aher an engine failure on a continued Take-Off. Vz is found by adding the
increment to VR given at the bottom of each wind column. I
~
62 - Screen attitude.
The weight extracted from the Take-Off data page for the actual outside air temperature ~
(OAT) and forcast wind component, corrected for pressure altitude. centre of gravity and
DDM items is the Performance Limited TOW.
Maximum Authorised TOW is 185070kg. Notional weights in excess of this figure are
tabulated when available to enable thehighest possible weights to beused priorto applying
significant negative corrections such as some DDM items.
N.B. The FAA Environmental Impact Statement and Noise Rule requires all Concorde
operations from any U.S airfield to be restricted to a MATOW of 182250kg.
B. Determine the least favourable wind component. No special allowance is required for light
and variable winds. Observe maximum tail and cross wind limitations. Caution should be
exercised should any variation in wind condition be expected et or around the time of
departure.
C. Enter the Take-Off data page with the least favourable wind component and actual OAT and
extract theMTOW. Vt , V",Vzand a 2. interpolating asnecessary. Apply corrections asfollows
to obtain the PLTOW.
1.1.13. CORRECTIONS
Any corrections to the tabulated MTOW value must be made in the following manner -,
A. Pressure Altitude
The tabulated MTOW and Take-off speeds are corrected for Pressure Altitude using the
information given on page 1.3.1.
B. Centre of Gravity
1. 54% Co • RTOW Improvement With Take·off CG Position of 54% Co
b.lncreasethe PLTOW by the increment shown on page 1.1.8. Limit actual TOW to this
For Take-Off at weights below14OllOOkg the aft C.G. limit is 53% Co to avoid spurious M/CG ~
warnings.
c. If the actual TOW is lessthan the value obtained in b. the difference between the
PLTOW before the reduction was applied and the actual TOW must be used to
delermine the "actualTOW lessthanPLTOW' Take-Off speed and 92 corrections.
,,"
'1&8'
140
130
:3.2
':::'3.0·
2.8
2.6
3.2
3.0
2.8
2.6
3.3"·:
3.1·
2..9
2.1
3.3
3.1
2.9
2.1
3.4
3.2
3.0
2.8
:
:
Corrections are made for any allowable Dispatch Deviations using the information given in
Section 1.8.
D. Take·Off Speeds
If the actual Take-Off weight is less than PLTOW, extract from the appropriate tables the
correction for V, dry and VI wet, VR and Vz. Deduct these values from those given for
PlTOW to obtain the actual values. From the same correction table extract the correction
for 92' Add thisvalue to thatgiven for PLTOW corrected for pressure altitude to obtain the
actual value. Check that V, dryand V, wet arenotless than 132 knots, VR is notlessthan 139
knots and 9 2 is not more than 111".
In order to reduce the number of occasions of Take-Offs being abandoned at lookt because
of a failure of one reheat. the procedure below should be followed when the PlTOW and
Actual TOW corrections have been calculated.
Enter the reheat failure STOP/GO chart in this section with PlTOW and Actual Take-Off
Weight and determine the point of intersection.
If thepointliesin the GO area of thechart. thisindicates thatif one reheat is failed at 100kt,
theTake-Off may be continued and normal procedures followed. In this case, V, calculated
for Actual Take-Off Weight must beincreased by 10kt. Noother adjustments to VIlo Vz or 9 2
are required.
If the point of intersection onthe STOP/GO chartliesin the STOP area, theTake-Off will be
abandoned if, at lookt. all four reheats are not operative.
Normal noise abatement procedures should continue to be followed in the GO case and no
significant increase in noise levels is expected.
This procedure must not be used on a slippery runway.
B. At some airports (for example Miami) immediately before the individual runway RTOW charts
a table is provided which gives the noise levels at the most critical noise measuring post
associated with a Take-Off at 181.000kg in the specified temperature conditions for each
runway and SID at that airport. This information is provided to indicate which runways and
Standard Instrument Departures are the least noise sensitive and hence enables the best
choice of runway and route to be made. to reduce noise to the minimum possible, ATC and
other requirements permitting.
C. At New York as an alternative to B. above Noise Advisory Charts are provided for the two
preferred runways 31L and 22ft.
In addition to 31L and 22R, 22L and 13R may also be used for Concorde 'Transatlantic'
departures.
13R should never be used if it is possible to use 31L, 22R or 22L within the Performance
Umitations of the aircraft, using a re-clearance technique where necessary. Should use of
the're-clearance planning' fail to reduce the actual TOW sufficiently to allow,in Performance
terms, the use of 31L, 22R or 22L and/or these runways are unacceptable for ATC reasons,
then 13R may be used.
Todecide between 31L, 22ft and 22L (the RTOW chartfor 22L may be used as a noise advisory
chartl»
1. Determine the noise advisory Take-Off weight for each runway from the charts.
2. If 31L, 22R or 22L is the ATC runway and the actual TOW is below the noise advisory
Take-Off weight then use that runway.
3. If only one runway shows the actual TOW is below the noise advisory Take-Off weight
and it is not the ATC runway, then request that runway and adjust taxi fuel.
4. If the actual TOW exceeds the noise advisory Take-Off weights on 311.. 22R or 22L .....#
runways, then 22R becomes the preferential runway in all instances provided that the
233"R is available. It is recommended that "Reclearance Planning" should be considered
atthe Captain's discretion in orderto keep actual TOW belowthenoise advisory Take-Off
weight limit.
5. Should none of the above runways be available, Rwy 31R or 13L may be used. These two
runways are the last choice because both are very noise sensitive. ~
The Noise Advisory Charts are based on a Polar presentation in order to take into account
theaffects of crosswind. The charts areentered using thereported surface windspeed and
direction. Weight are obtained bylinear interpolation. The charts are produced in bands of
temperatures as follows:-
Up to re
re to Irc
~c to 27"C
2rC 10 3rC
EXAMPLE:
WN 2&O"15kt
TEMP 2O"C.
ACTUAL TOW 171l1OOkg.
ATC RUNWAY 31L
D.At main and alternate airports where nospecific noise abatement procedures areprovided. a
requirement for minimising noise may still exist the following technique should be used at
such airports. The method consists of following the standard noise abatement procedues. as
described in the FCOM, and throttling back at 1l1OOft. above the airfield rather than time.
The required !throttle angles are given in the appropriate table in this section. The power
available after throttling is sufficient to maintain a minimum gradient of 30/0 with a 20" bank
angle. If bank angles between 20" and 250 are required the Nz values should be increased by
1.5%. The normal SIDS and/or ATC instructions should be followed. After throttling 250kt
should be maintained until any crossing height requirements are assured. Acceleration may
then be carried out ATC permitting. Normal incremental power settings should be used until
clear of noise sensitive areas.
lIE 180
-\glf >jI11: :j1.32 :ju' l5.f·l(i)
~i 93.·:.&•·.c·.·.·.:94.8· .•.......•
20.6 19.4 18.3 17.3 16.3
92.0 93.0 93.9 94.8 95.7
55. : .~j 9~;~.... .
1!.I.l.·.··•.':.•: .' :.•·..•.
.»0
.••.
··•
9.'·
.••·.·.... 11;9> >}g.l
0ll.3 101.2
::::.:;.-
]j:/:
_
lour.
.. ,
lIf~~~: :.~:.:
.:>::..;;....
•. ~•••. -:.td :itl
'fur 9411
1$.2 ita. 13.1 iJij lEt:
I- 9U 51.!)": .4 100.1': ~~ ..
170 22.3 21 1 201 19.1 18.1 17.1 16.1 15.1 14.2 13.2 12.2
90.5 91.4 92.3 93.2 94.1 95.0 95.8 95.7 97.5 98.4 992
~
~ .~ f.
.,..•. . •. :.••.•! !.·'
.'
•••. 3,•..,.··............tii;:21;1:20.2:lsjjil]1H 1'7.2 :.::·~
9l(tf· 9U\92.393;2 94~1 9U ._·.•.6.·.·.Wo.•:·.:•·• '.•~
• . •~
.• •. •~•.•. . :.•:.'';.1!.•'•.~•:. ·•·.:•·. .:li2}
-.v iI'~ •. guy,
1&0 23.9 23.1 22.1 2U 20.2 19.1 18.1 17.1 16.1 15.1 14.4
88.9 89.9 90.7 91.5 92.3 93.2 94.1 95.0 95.8 96.7 97.3
150 24.8 24.8 24.8 22.9 21.8 20.8 19.8 18.9 18.1 11.2 16.4
81.5 88.4 89.2 90.0 90.9 91.8 92.6 93.4 94.1 94.9 95.6
11
······:·:·:·:·:··;·;··' ·· ·· · · :··· :·:·:· · · · · · ···_-··.-_. ,.<':::~;::~:: ;.:.':.,., -- - ....•... ..•.....................-;'.'" >:.
130 26.3 25.7 25.1 24.6 24.1 23.6 22.1 21.1 20.9 20.0 19.0
85.3 86.2 81.0 87.8 88.6 89.4 90.2 91.0 91.7 92.5 93.3
Nz ('le)
100Dkg fiOIIlI
Nz (%1
········.ANI)8ElOW .. 150
'. ··)·.9ir\·} i·" ···•·.. .·152
100 153
102 155 165
104 157 167
158 168
160 170
161 ·171
182 172'
N.B. VRf F is the target speed for final approach and crossing the threshold with all engines
operating. light wind. Iow turbulence and auto throttle engaged. For other conditions ~
refer to (he Flying Manual.
1.1.16. LANDING
Landing Data Pages are provided for all Normal Destination (Part 1) and Alternate (Part 2)
Airfields.
~ Yellow pages will be provided, where possible, for Temporary situations and will be included
either facing the relevant permanent page, or loose leaf on handout
Each page allows for upto two runways, published in ascending numeric order (and alphabetical
where applicable).
N.B. Absence of landing data for a particular runway at an airfield where other runways are
covered. implies it is NOT APPROVED for landing.
If data is required for an airfield for which a Landing Data page is not available, or when a
change to the published data arises at short notice, either:-
A. Max wt Permitted
The Maximum Landing Weight permitted for an Airfield is normally Max Stuctural Weight,
but may be governed by airfield elevation (WAT limit).
The Maximum Permitted Landing Weight published for each Runway for Manual ~
Dry/Slippery and Autoland Dry/Slippery, is useable up to the number of knots of tailwind .. .
component listed. The maximum tailwind component for all these catagories is 10kt. For
Manual approaches weights are published based on both VREF + 7 and VREF, for Manual
Slippery, Autoland and Autoland Slippery published weights are based on VREF.
The Maximum Landing Weight for Fuel Saving Landings of 130000kg is usuable up to the ~
number of knots of tailwind component listed, based ona manual approach at VREF in dryor
wet (up to 3mm water) runway conditions. Refer to Special Operations 1.8.16.
N.B. Autoland is NOT APPROVED if the GS angle exceeds 3.1 0 or is less than 2.5".
If the maximum tailwind listed is less than 10kt (Manual Dry/Slippery, Autoland
Dry/Slippery), the Maximum Landing Weight should be reduced by the tabulated value of
"Red'n per extra Jet 1W kg", for tailwinds greater than the figure listed, but not exceeding
10kt maximum.
E. Ine per kt HW kg
If the Maximum Landing Weight in Zero Wind is lessthan the Maximum Structural Landing ~
Weight, an "Inc per kt HWkg" is given, to be added to the weight, up to Maximum Landing
Weight of 111130kg.
A. 1.25 VM1N 1g (3") (themin. speed in the finalsteady approach configuration with thrustfor
a 3 degree angle of descent).
B. 1.20 VMIN 19 (MT) (the min. speed in the same configuration with minimum authorised
thrust for final approach).
Before using the tables, ensure that the Landing Distances published are valid, e.g.
threshold not inset due WIP. If a restriction is in force, and no Yellow Page has been
provided, refer to Generalised landing Charts.
B. Procedure
1. Ensure Arrival OAT is less than WAT limited Temperature VREF or Vm + 7kt as
applicable.
Z. Extract Maximum Tailwind Component or Still Air Maximum landing Weight for
appropriate landing conditions. Restart using landing Weight as necessary.
The ICAO Airfield Category requirement is produced by considering the length, maximum width
of the fuselage and frequency of movements of the largest aircraft normally using that airfield.
Airfields promulgated Category B may be used when movement rate is sufficiently low.
Temporary airfield depletions to Category 7 are permitted.
The slippery runway data. when used, may well produce very limiting landing weights so it is
essential that careful thought is given before use.
A slippery runway caused by ice is usually of short duration, but a slippery runway can be
caused by water on rubber deposits and on smooth surfaces. If a runway is promulgated as
liable to be slippery when wet, it means that a certain portion of the runway (in UK more than
100 metres) has a Mu meter reading of .39 (.49 JBllor below. This could mean that the whole
runway has a braking action ofmedium/good - very farremoved from theassumed co-efficient of
0.05 Mu (0.05 JBllfor a slippery runway.
As well asrubber deposits and smooth sufaces. local pools of water can also give a liable to be
slippery when wet state. In the Performance Manual whenever such a statement is made, an
indication ofwhere and whywill beincluded to enable pilots to make a better assessment of the
particular situation. Whilst one cannot and should not interpolate between normal wet runway
data and slippery runway data, the two sets of data for a particular runway give an indication of
possible margins and may assist the Captain to choose the most appropriate level of
performance for the conditions.
A wet runway is defined as having up to 3mm of water onthe surface and a friction co-efficient
of ~PhProximatbelY Odne half of that of a dry runway butwith "braking action good". The landing ~
welg 15 are ase on a wet runway.
Aooded runways must be considered as slippery.
Either
A. Enquiries of pilots of suitable transport aircrafton recent operations from a runway find
the runway is reasonably smooth in comparison with other runways reguarly used by
Concorde and the runway must be known to have no undue tendency to deteriorate.
or
B. The runway has been recently laid to ICAD standards by reputable contractors and
operations on it with heavy aircraft are producing no adverse comment.
For one of the early take-offs from such a runway it is necessary to obtain a record of C of G
accelerations using the AIDS recorder. The record should be passed to the CM for analysis.
For runways where clearance cannot be obtained by the procedure given above, the maximum
weight for take-off is limited by runway roughness considerations to 135000kg (with or without
passengers).
For take-off at weights of 135000kg or less no limitations related to runway roughness are
applicable and no authorisation is required.
N.B. The minimum height for disengagement of the autopilot when operating to the above
minima depends on the runway status lsee para 1.1.30.1.
This presentation is replacing an earlier standard quoting both 'Circling' and 'Visual' heights,
respectively accounting for all obstacles within thestated radius. or only those withina specified
sector. These minima are intended for use on a Circling approach following break-off from an
instrument approach to another runway.
RVR or Visibility limits quoted aretheState minima or where nosuch minima exists the minimum
RVR for Visual landing with approach lighting available.
The minimum IN FUGHT VISIBIUTY required for Circling is defined as 120 x circling speed in
knots = ..... metresl, using the speed for Category 0 aircraft 1205kt) as defined in ICAO PANS OPS
lfor Concorde this equates to 4100ml..
1.1.34. ICAO PANS OPS (Doe 8168) SPEED RELATED AlC CATEGORY
Aircraft are divided into five speed categories. These are based on a nominal threshold speed
defined as 1.3 times the stalling speed in the landing configuration at Maximum Certificated ~
Landing Weight. The ICAO Category for the CONCORDE is O.
Cat 2 - Three consecutive Approach or Runway C/l Lights and then the Runway ~
must be continuously in view, and the aircraft must be seen to be tracking
satisfactorily.
Cat 3A - Three consecutive Runway C/l Lights. If after decision to land has been
announced the visual segment is reduced, the Captain may complete the landing
provided the Autopilot remains engaged.
Cat 2 - Three consecutive Approach orRunway Cll lights and then theRunway must be
continuously inview,and theaircraft seen to be tracking satisfactorily.
Cat 3A- Three consecutive Runway Clllights. If after decision to land has been
announced the visual segment is reduced, the Captain may complete thelanding
provided the Autopilot remains engaged.
A.An approach may be commenced down to 1000ft above DA as normal, provided both
ILS and PAR are operative and used. It is essential to check that PAR monitoring will be
available, and to advise ATC it will beused.
B. An approach may be continued if thereported VIS falls below minima only after the
aircraft:-
If minima of 300ft/ 0.75sm orless are quoted, these shall be increased byl OOft and0.25sm if
anyofthefollowing are notavailable:-
GS, OM and outer l.BCN. Approach Lights. unless the landing Data Page says otherwise..
Rev: paras re-numbered due inclusion ofnewpara 1.1.36. 1.1.23 JUN 94/04
8llITlSH
AIRWAYS CONCORDE PERFORMANCE MANUAL INTRO NOTES
AOM
C. DME at theGfide Slope site may be substituted fortheILS OM when published onthe
procedure.
D. Unless thelanding Data page says otherwise, standard increments are to be applied to the
minima where ILS components are inoperative:-
OM, MMorAlS
OM, MMorAlS
HIRl, TOll,
RCLS orRVR 50ft O.25sm
Transmissometer
Approaches are banned in Canada when Touchdown RVR I'A1 is less than 1200ft,
and/or theMidPoint RVR ('81 is less then 700ft. The Rollout RVR, if available, is advisory only.
Both Touchdown and Mid-Point RVRs must be at orabove thepublished minima. The Rol/out
RVR, if available, isadvisory only.
~ A.When flight planning or replanning in flight, to areas or aerodromes otherthan those listed
below, normal destination minima will apply. except:-
a.The forcasts for both destination and alternate must ~~~ 100ft and 0.5 mile
above Cat 1minima. AND Unless both areforcast to . , 20O!!jhd 1mileabove Cat 1
minima. anadditional en-route alternate within1000n - estination and 500nm of
trackmust beforecast to beat least200ft and t mile above Cat 1 minima.
c. Prolonged landing delays must not beforecast. When replanning in flight, the
reported andforecast weather at thenominated alternate must beequal to, or
better than 800ft I 2sm.
B. When flightplanning or replanning in flightto any of the following areas or aerodromes the
weather at the nominated alternate must beforecast to beequal to or better than the
appropriate alternate minima. If anin flightdiversion is made thealternate becomes the
destination and normal destination minima apply.
C.ln Canada and the Philippines where minima arelisted as800ft I 2sm theuseof900ft 11Y2sm
or 1000ft /1 smis permitted; where minima arelisted as600ft I 2sm theuseof 700ft I Phsm or
800ft I lsm is permitted.
~ D.The alternate minima for aerodrome in Taiwan onlyapply if thedestination is forecast below
5000ft I 5sm otherwise normal landing minima apply.
E. In Australia nomination of analternate requires thatthe forecast for thealternate must not
include:
3. Possibility of fog.
AIRFIELD NOMINATED AS
~ DESTINATION ALTERNATE RUNWAY FACIUTY ALTERNATE MINIMA
(HAA) (Vis)
AIRAELD NOMINATED AS
DESTINATION ALTERNATE RUNWAY FACILITY ALTERNATE MINIMA
(HM) (Vis)
PHILADELPHIA All ILS 700 2sm
27L NOB 800 2.5sm
All Others 800 2sm
09R Conv.llS NotApproved
~
STEPHENVILLE 28 IlS 1100 2sm
All Others 1400 3sm
WEIGHTS
KG LB KG l8 KG LB KG LBLB KG LB KG L8 KG La KG
300 661-4 &DO 1322-8 900 1984·2 300 136-1 600 212-1 900 408-2
10 22.Q 10 683-4 10 1344·8 10 2006-2 10 4-6 10 1~ 10 216-1 10 412·8
~ 20 44·1 20 705-5 20 1366·9 20 202802 20 9·1 20 14501 20 281·2 20 411·3
30 66·1 30 727·5 30 1388·9 30 2050-3 30 13·7 30 14901 30 285-8 30 42'·8
40 88·2 40 749-6 40 1411-0 40 2012·3 40 lB·l 40 154-2 40 290-3 40 42&4
so 110-2 50 71106 50 1433-0 50 2094-4 50 22·7 50 158·8 50 294-8 50 430-9
60 132·3 60 793-7 60 1455-0 60 2116-4 60 27·2 60 163·3 60 299-4 60 435-4
10 154-3 70 815-1 10 147101 70 2138-5 70 3108 10 161·8 70 303-9 10 440-0
BO 116-4 80 83108 so 1499·1 BD 21&0-5 BD 36·3 80 172-4 BD 30H 80 444·5
90 198-4 90 859-8 90 1521·2 iD 2182-6 90 40-890 176·9 90 313-0 9D 449-0
100 220-5 400 881·8 700 1543·2 1000 2204-6 100 45-4 400 181-4 100 311·5 1000 453·6
~ 10 242·5 10 903-9 10 1565·3 10 49-9 10 186.Q 10 32200
20 264-6 20 925-9 20 1587·3 20 54-4 20 190·5 20 326-6
30 28&6 30 948-0 3D 1609-4 30 59-030 195-0 30 331·1
40 3UB-& 40
910-0 40 163104 40 63-S 40 199-6 40 335-6
50 33()07 50
992-1 50 1653·5 50 6&0 50 204-1 50 340-2
60 352·1 60
1014-1 60 1675·5 60 72-6 60 208-6 60 344·7
70 374·8 10
1036·2 70 1697·6 10 7701 70 213·2 70 349·3
80 396-8 80
1058-2 so 1719-6 80 81-6 BD 217·7 80 353·8
90 41&9 11J8Oo3
90 90 1741·6 go 86-2 90 222·3 90 358·3
l....
~ 200 440-9 1102·3
500 800 1163-1 200 90-1 500 226-8 BOO 362·9
10 4&3-0 10
1124-4 10 1785-1 10 95-3 10 231-3 10 3&1-4
20 485-0 20
1146-4 20 1801-8 20 99-820 235-9 20 371·9
30 501·1 30 1168-4 30 1829-8 30 104-3 30 24004 30 376-5
40 40
529·1 40 1190-5 1851·9 40 108·9 40 24409 40 381-0
50 so
551·2 50
1212·5 1873·9 50 11304 50 249·5 50 38&-5
60 573-2 60 1234-6 60 1896.Q 60 117-9 60 2540Q 60 390-1
~ 10 59502 10 1256-6 10 191800 70 122-5 70 25&5 70 394-6
80 617-2 80 1218·7 80 1940-1 so 12100 IQ 283-1 BO 399-2
90 639-3 90 1300·1 90 1962·1 90 131·5 90 26106 90 403·7
~I ili!'iIII11i
1000 55 13 21000 -17 -21 +31
2000 52 11 22000 -20 -29 +32
3000
4lXXJ
48
45
9
7
23000
24000
-24
-27
-31
-33 =U.::::tJ§::(.i :~~ +33
+34
~
5000
6000
41
37
5
3
2!iOOO
26000
-31
-33
-35
-36 +g.::.. i>f~·:::.J :~ +35
+36
1000
8000
34
30 -I
1 27000
28000
-36
-40
-38
-40 :r.4:::;:,.~:.:¥~·;::·:i :~ :~ j:.:. • . :;::.;.:~~~~~~~+~: +31
+38
il
'jllt_i ~5
9DOO 21 -3 29000 -44 -42 -1 ::::t:~·::::::·::1S~~[j:r+ 102 +39
10000 23 -5 30000 -44 -41 o :\+t8::::)fir': +104 +40
11000
12000
19
16
-1
-9
31000
32000
-51
-54
-46
-48 :~ l)~I>···::~g·:1~:~: +41
+42
~illll~~IHl~
-58
l:iiliill~1~~
13000 12-11 33000 -50 +43
14000 9-13 34000 -62 -52 +44
~ 15000 5-15 3500D -65 -54 +45
16000 1-11 36000 -69 -56 +46
17000
18000
-2 -19
-6 -21
31000
38000
-69
-69
-56
-56 ~,g?::":;'~:.:·1 :: +8 ;<+.82.~ . . +2I=:: +118
+47
+48
19000 -9 -23 39CXJO -69 -56 .+12::&ll. +48 +9 :··.f. .::~:+~t
-. ..
+ 119
::;:;:~:::~:;:;;:::' -.: . -.-
- - -,
+49
ATMOSPHERIC PRESSURES
Mbs Ins Hg mm Hg Mbs Ins Hg mm Hg
948·1 28-00 711·2 1000·6 29·55 750·6
949·8 28·05 712·5 1002·3 29·60 751·8
951-5 28·10 713·7 1003·9 29·65 753·1
953·2 28·15 715·0 1005·6 29·70 754-4
954·9 28·20 716·3 100J.3 29·75 755·6
956·5 28·25 71J.5 1009·0 29·80 756·9
958·2 28·30 718·8 1010·7 29·85 758·2
959·9 28·35 72D-l 1012·4 29·90 759·5
961-6 28·4ij 721-4 *1013-2 *29·92 *760-0
963·3 28·45 722·6 1014·1 29·95 760·7
965·0 28·50 723·9 1015·8 30·00 762·0
966·7 28·55 725·2 1017·5 30·05 763·3
968-4 28·60 726-4 1019·2 30·10 764·5
970·1 28·65 72H 1020·9 30·15 765·8
971·8 28·70 729·0 1022·6 30·20 767·1
973·5 28·75 730·2 1024·3 30·25 768·3
975·2 28·80 731·5 1026·0 30·30 769·6
976·9 28·85 732·8 102H 30·35 770·9
978·6 28·90 734·1 1029·3 30·4ij 772·2
98D-2 28·95 735-3 1031·0 30·45 773·4
981·9 29-00 736·6 103H 30·50 774·7
983·6 29·05 737·9 1034·4 30·55 776·0
985·3 29·10 739·1 1036·1 30·60 777·2
987·0 29·15 74ij·4 1037·8 30·65 778·5
988·7 29·20 741·7 1039·5 30·70 779·8
990-4 29·25 742·9 1041·2 3D-75 781·0 ~
992·1 29·30 744·2 1042·9 3D-80 782·3
993-8 29·35 745·5 1044·6 30·85 783·6
995-5 29·4ij 746·8 1046·2 30·90 784·9
997-2 29·45 748·0 1048·0 30·95 786·1
998·9 29·50 749·3 1049·7 31·00 781-4
1000-6 29·55 750·6 *ISA ~
SPEEDS
DISTANCES
mtrs yards feet mtrs yards feat Il11JS yards feet
5 5 16 205 224 672 405 443 1328
10 11 33 210 230 689 410 448 1345
15 16 49 215 235 105 415 454 1361
20 22 66 220 241 722 420 459 1318
25 21 82 225 246 138 425 465 1394
30 33 98 230 251 154 430 410 1410
35 38 115 23S 251 110 435 415 1426
40 44 131 240 262 181 440 481 1443
45 49 141 245 268 803 445 486 1459
50 55 164 250 213 820 450 492 1416
DISTANCES
mtrs yards feet mtrs yards feet mtrs yards feet
605
610
662
667
1985
2002
805
810
880
886
2641
2658
1010
1020
1105
1116
3314
3347
~
615 673 2018 815 891 2674 1030 1126 3379
620 678 2035 820 897 2691 1040 1137 3412
625 684 2051 825 902 2707 1050 1148 3445
630 689 2067 830 908 2723 1060 1159 3478
635 694 2083 835 913 2739 1070 1170 3511
640 700 2100 840 919 2756 1080 1181 3544
645 705 2116 845 924 2772 1090 1192 3576
650 711 2133 850 930 2789 1100 1203 3609
-..J
655 716 2149 855 935 2805 1110 1214 3642
660 722 2166 860 941 2822 1120 1225 3675
665 727 2182 865 946 2838 1130 1236 3707
670 733 2199 870 952 2855 1140 1247 3740
675 738 2215 875 957 2871 1150 1258 3773
680 744 2232 880 963 2888 1160 1269 3806
685 749 2248 885 968 2904 1170 1280 3839
690 755 2264 890 973 2920 1180 1291 3872 ~
695 760 2280 895 979 2936 1190 1301 3904
700 766 2297 900 984 2953 1200 1312 3937
DISTANCES
DISTANCES
mtrs yards feet mtrs yards feet mtrs yards feet
2610 2855 8564 2910 3183 9548 3210 3510 10531
2620 2865 8597 2920 3294 9581 3220 3521 10564 ~
2630 2876 8629 2930 3204 9613 3230 3532 10596
264ll 2887 8652 2940 3215 9646 3240 3543 10629
2650 2898 8695 2950 3226 9679 3250 3554 10662
2660 291l!l 8728 2960 3237 9712 3260 3565 10695
2670 2920 8761 2970 3248 9745 3270 3576 10728
2680 2931 8794 2980 3259 9778 3280 3587 10761
2690 2942 8826 2990 3270 9810 3290 3598 10793
2700 2953 8859 3000 3281 9842 3300 3609 10826
..... ·--t····
. .. .....
1 ' : :. : :-:-:.- ~ • • :
'
•
•••• 1 , ••
i
I
;
~j --_._~.
I
I
!
····i
.. . ~ -
.. ~ --
.
t
..
.. , .
'
I .: .
~ _1. __. __ .
,
I 1"
l
j
... l'
1
'" . -,"-.."P",.,..
" ,.
• . . • • . • , I.
" . '
, -...
;,
····1··.·
930 2350 2320 2300 2270 22<W 2210 2180 2150 2120 2090
940 2060 2030 2000 1980 1950 1920 1890 1860 1840 1810
950 1780 1750 1720 1690 1660 1630 1600 1570 1550 1520
960 1490 1460 1430 1<WO 1380 1350 1320 1290 1260 1230
970 1210 1180 1150 1120 1100 1070 104n 1010 980 960
980 930 900 870 840 810 780 750 720 700 670
990 640 610 580 560 530 500 480 450 420 400
1000 370 34n 310 290 260 230 200 170 150 120
1010 90 60 40 10 -20 -50 -70 -100 -130 -150
1020 -180 -210 -240 -260 -290 -320 -350 -380 -<WO -430
1030 -460 -480 -510 -54n -560 -590 -620 -650 -670 -700
1040 -720 -750 -780 -800 -830 -860 ·880 -910 -94ij -960
1050 -990 -1020
NOTE: For take-off calculations:- Entry with n.N.H. gives Height above or below Airport elevation.
RAnOS
The following ratios provide accurate enough answers for most practical purposes:-
41 n.mls 76 km
66 n.mls 76 st.mls
41 st.mls 66 km
1 kt 0.5 mtrs/sec
mtr/sec 2 kt
I.........
I ;
,~~-~ ~-:-~_A._. t---- ~~~+-~~
I . I
I I . r•
... i, .: .~
,
, ~
! ~--'1--
l .
~ iI
>
.
~
... - ~
z
::»
Cl:
C»
Z
9~
I-
Z
III
Z
o
Go
~
o 0
u
o
! 0
~ z
i
..I 10
et
I- 16
0 10 20 30 40 60
CROSSWIND COMPONENT lkt)
1020 2.3
1010 0.9
1030 2 ADD
1020
1010 O-----t-
1000 -0
990 -1 SUBTRACT
980 -2
910 -3
MTOW
(1000kgl 0 2 4 6 8
INCREMENT - TONNES
180 .90 .91 .92 .93 .94
(J1o.: • •.: " .);85.••..••. :. .88· .87. .,~B .•.• llQ . ..
MTOW
11000kgl 0 2 4 6 8
DECREMENT - TONNES
44
46
.: . ·so
48
"':.'.
'···'a.:.':,
'5&"','.'
58'"
60
62
. . ,.>; .:.
64
61
• ~~> .• '"
N.B. Minimum Allow": V, = 132kt. V. = 139kt.
Mul.1IftI Allowed: 8 2 = 18".
V2 Screen Speed corrections for Ictuel Take-off weights lesl Ihlln PLTOW •
N.B. Deduct I further 1 Kt for tv.ry 1000 Ft. P,....re Altftlde lbo" S.L for YIII. . . to 11ft of
fower 1111••
PRESSURE
ALTITUDE
FEET TEMPERATURE • DEGREES C
WEIGHT
,.
TONNES
185
175
170
VZRC • KNOTS
165
160
1SS
,.
150
1
140
130
120
115
110
N,B, Th' da.. aboya la for 'GEAR UP', for 'GEAR DOWN' IIPPIy the comcdon IIttlow.
GEAR UP ~ 1~ 1~ ~ 1W 1~ 100
GEAR DOWN ~ +7 +9 +11 +14 +17 +20
AJRRELD
PRESSURE
AlntUDE
FEET TEMPERATURE· DEGREES C
WBG",
,.
TONNES
'85
175
170
PITCH AntUDE • DEGREES
185~-lo;!~i,It.
160
155
150
145
140
135
130
125
120
115
110
42
41
40
P7 39
38
37
36
I
.10 o
I
N.B. If taking off at Pressure Altitudes above 2000ft or at Ambient Temperatures in excess of
+35°C. see Cruise Control Manuel.
o + 10 +20
·10
Ambienl temperalure °c I +30
I
I I I f I
. ,~ ~
; i·
21
FT
(1000 kg/hr)
19
N.B. If taking off at Pressure Altitudas abova 2000ft or at Ambient Temperatures in excess of
+35°C, see Cruise Control Manual.
AIRFIELD CODE
BARBADOS BGI
TORONTO YYZ
\J
( )
~
::::vs CONCORDE TAKE-OFF DATA BARBADOS
AID Elev 169ft GRANTLEY ADAMS
FULL LENGTH RWY 09
CLG NIL RVRNIS 200m SLOPE O.08%DN
TOR 3353m (11001ft) ED 3353m (11001ft) TOD(U) 3338m (10961ft)
\. OAT 10kt Ine 5kt Ine snu, Inc 101et Ine 201et Ine 30kt
~ "C TAIL Ikt TAIL Ikt AIR Ikt HEAD Ikt HEAD IIet HEAD
39 162.3 0.8 166.3 0.8 170.3 0.3 173.1 0.3 175.8 0.3 178.6
151/176 156/182 161/188 165/191 168/195 171/199
36 164.2 0.8 168.3 0.8 172.4 0.3 175.2 0.3 178.0 0.3 180.8
152/177 157/183 162/188 165/192 168/196 172/200
33 166.1 0.8 170.2 0.8 174.4 0.3 177.2 0.3 180.1 0.3 182.9
152/178 157/184 162/189 165/193 169/197 172/201
30 168.0 0.8 172.1 0.8 176.3 0.3 179.2 0.3 182.1 0.3 185.0
153/179 157/184 162/190 166/194 169/198 172/202
27 169.8 0.8 174.0 0.9 178.3 0.3 181.2 0.3 184.1 0.3 187.0
153/179 158/185 163/191 166/195 169/199 173/203
24 171.6 0.8 175.8 0.9 180.2 0.3 183.1 0.3 186.0 0.3 189.0
153/180 158/186 163/192 167/196 170/200 173/204
21 173.3 0.9 177.6 0.9 182.0 0.3 184.9 0.3 187.9 0.3 190.9
154/181 159/187 164/193 167/197 170/201 174/205
18 174.9 0.9 179.3 0.9 183.7 0.3 186.7 0.3 189.7 0.3 192.8
154/181 159/187 164/193 167/197 171/201 174/205
15 176.5 0.9 180.9 0.9 185.4 0.3 188.4 0.3 191.4 0.3 194.5
154/182 159/188 164/194 168/198 171/202 175/206
12 177.8 0.9 182.2 0.9 186.8 0.3 189.8 0.3 192.9 0.2 195.0
154/183 159/188 165/195 168/199 172/203 175/206
9 178.5 0.9 183.0 0.9 187.5 0.3 190.6 0.3 193.6 0.1 195.0
154/184 160/190 166/196 169/200 173/204 175/207
6 179.2 0.9 183.7 0.9 188.2 0.3 191.3 0.3 194.4 0.1 195.0
155/185 161/191 166/197 170/201 173/205 176/208
3 179.8 0.9 184.3 0.9 188.9 0.3 192.0 0.3 195.0 0.0 195.0
156/186 161/192 167/198 171/202 174/206 176/208
0 180.4 0.9 184.9 0.9 189.5 0.3 192.6 0.2 195.0 0.0 195.0
156/187 162/193 168/199 172/203 175/206 177/209
-3 181.0 0.9 185.5 0.9 190.1 0.3 193.2 0.2 195.0 0.0 195.0
157/188 163/194 169/200 172/204 175/207 177/209
V2= VR+ 21 VR+ 21 VR+ 21 VR+ 21 VR+ 21 VR+ 21
92= 13.5 13.5 13.0 13.0 12.5 12.5
1.Vl WET SPEED: V1 WET IS V1 DRY minus lSkt.
1. MIDHURST 1K
On crossing theLON 119R11.3d turn RIGHT to intercept LON 129R to LON 3.5d then RIGHT onto
Track 211°M lMIO D31R) to Midhurst and continue with SIO.
2. SOUTHAMPTON 2J(
On crossing the LON 119R11.3d turn RIGHT to intercept LON 129R to LON 3.5d then RIGHT onto
Track 226"M lOCK 046R).
At OCK 2d turn RIGHT to intercept 2S8R to OCK 19d then LEFT to Track 232"M ISAM 052RI to
Southampton.
3. COMPTON 2K
On crossing the LON 119R11.3d turn RIGHT using 25° bank applied expeditiously.
4. DOVER 2K
On crossing the LON 119R11.3d turn RIGHT using 25" bank applied expeditiously to achieve a
heading of 125°M.
NOTE - Rwy 091 must only be used when tflere is no other Rwy available.
1. MIDHURST 1J
Ahead to imercept LON 129R to LON 3.5d dlen RIGHT to imercept Track 2110fd (MID lJ31RI to
Midhurst and continue with SID.
2. SOUTHAMPTON 2J
Ahead to intercept LON 129R to LON 3.5d dlen RIGHT onto Track 226"M (OCK D46RI.
At OCK 2d mm RIGHT to intercept 258R to OCK 19d dlen LEFT to Track 23rM (SAM 052RI to
Southampton.
I
3. COMPTON 2J ~
Continue blm onto 285"M QDM to Woodley and continue with SIO.
4. OOVER 2J
At LON 144R blrn RIGHT using 15° bank applied expeditiously to achieve a heading of 125"M.
OAT 10kt Inc 5kt Inc STILL Inc 10kt Inc 20kt Inc 30kt
C TAIL Ikt TAIL Ikt. AIR Ikt HEAD Ikt HEAD Ikt HEAD
39 133.5 1.1 139.1 1.2 144.9 0.4 148.9 0.4 153.0 0.4 157.2
___ 4~~L451___ 131L151___ 1~,L161___ 1~5L16~___ 1~1L166___ 150L162
36 135.0 1.1 140.6 1.2 146.5 0.4 150.6 0.4 154.7 0.4 159.0
___ 133L153___ 13SL15S___ 1~,L16,___ li5Ll65___ 1~161___ 1~L110
33 136.4 1.1 142.1 1.2 148.1 0.4 152.2 0.4 156.4 0.4 160.7
___ 13~L15~___ 13SL1SS___ 1~,L163___ 1i5L165___ 1~SL16S___ 151L111
30 137.8 1.2 143.6 1.2 149.6 0.4 153.8 0.4 158.0 0.4 162.4
___ 11~L155___ 112L152___ 1~JL161___ li5L155___ liSL162___ lS1L11,
27 139.2 1.2 145.0 1.2 151.1 0.4 155.3 0.4 159.6 0.4 164.0
___ lJiL155___ 112L150___ 1i1L16i___ 1~5L151___ li2L110___ lS,L11J
24 140.5 1.2 146.4 1.2 152.5 0.4 156.8 0.4 161.1 0.4 165.5
___ 115L151___ 1J2L151___ li~L16S___ li6L16S___ li2L111___ 15,L11i
21 141.8 1.2 147.7 1.2 153.9 0.4 158.2 0.4 162.6 0.4 167.0
___ 11SL151___ liOL161___ 1i~L165___ 1~IL15~___ 150L11,___ 15~L11i
18 143.0 1.2 149.0 1.3 155.3 0.4 159.6 0.4 164.0 0.4 168.5
___ lJ6L15S___ liOL16,___ 1i~L166___ 1~IL16~___ 150L11~___ 15JL11S
15 144.2 1.2 150.2 1.3 156.5 0.4 160.9 0.4 165.3 0.5 169.9
___ 1J5L1SS___ 1iCL15J___ 1~sL15Z___ 1~SL11Q___ 151L113___ lS1L11~
12 145.3 1.2 151.4 1.3 157.7 0.4 162.1 0.4 166.6 0.5 171.2
___ 136L152___ 1i1L16J___ 1~SL16S___ liSL111___ 151L11~___ 15~L111
9 146.4 1.2 152.5 1.3 158.9 0.4 163.3 0.4 167.8 0.5 172.4
___ 131L160___ 1~lL16~___ 1~6L16S___ 1~2L111___ lSlL11~___ lSiL111
6 147.4 1.2 153.6 1.3 160.0 0.4 164.4 0.5 169.0 0.5 173.6
___ 131L160___ liZL165___ li6L162___ li2L11,___ 15,L115___ lS5L1ZS
3 148.4 1.2 154.6 1.3 161.1 0.4 165.5 0.4 170.0 0.5 174.7
___ 13aL161___ 1iZL165___ 1ilL162___ 150L11,___ 15,L115___ 155L11a
o 149.3 1.2 155.5 1.3 162.1 0.4 166.5 0.5 171.1 0.4 175.3
___ 13SL161___ 1iJL166___ lilL110___ 150L113___ 153L116___ lS6L112
-3 150.2 1.3 156.5 1.3 163.0 0.4 167.5 0.5 172.1 0.4 175.8
__ 112L16,___ 1~JL166___ 1iaL12l-__ 151L113___ 15iL116___ lS1L1S0
V2= VR+ 28 VR+ 26 VR+ 25 VR+ 23 VR+ 22 VR+ 22
82= 15.5 15.5 15.0 14.5 14.0 14.0
1. M.DHURST 2G
Turn LEFT using 15" bank to intercept LON 244R.
At LON 5.5d increase Nz by 2% and conlinue lEFT tum with maximum 25" bank on BUR 166R to
intercept DUN 158R.
At LON 12d turn RIGHT onto Track 202"M (MID 022R) to Midhurst
2. DOVER 3G
At LON 5d increase Nz by 2% and bank angle to 25" to intercept Track 12&"R to Epsom and ,.,)
continue with 810. ~
NOTE - Initial tum should not be lalde udl LON 219R (Ead 01 Runway).
1. SOUTHAMPTON 2G
Ahead to intercept LON 260R.
At LON 7d turn RIGHT onto Track 273°M (WOO 273MI to Woodley and increase N2 by 2%.
At lON 13d turn LEFT onto Track 22O"M (SAM O4ORI to Southampton.
2. COMPTON 2G
Ahead to intercept LON 260R.
At LON 7d turn RIGHT onto Track 273"M (WOO 273MI to Woodley and increase N2 by 2% and
continue with SIO.
~ 2.Noise Abatement Procedures: See pages LHR/16. LHR/17. LHR/18 and LHR/19.
1. MIDHURST 2f
Turn LEFT using lSO bank to intercept LON 244R.
At LON 5.5d increase ~ by 2% andcontinue LEFT turn with maximum 25" bank to intercept BUR
166R.
At lON 12d him RIGHT onto Track 202"M IMID 022R1 to Midhurst.
2. DOVER 2f
At 3IIOft QNH turn LEFT using lSO bank applied expeditiously.
At lON 5d increase N2 by 2% and bank angle to 25" to intercept EPM 131M and continue with ~
SIO.
NOTE - In!tilll IUm "ollld not be made until LON 244R lEnd of RUI1WllYI.
1. SOUTHAMPTON 2F
Ahead to intercept lON 260R.
At lON 7d turn RIGHT onto Track 273"M (WOO 273MI to Woodley and increase N2 by 2%.
At LON l3d turn LEFT onto Track 220 M (SAM 040RI to Southampton.
0
2. COMPTON 2F
Ahead to intercept LON 260R (take care not to turn before intercepting the radial).
At lON 7d turn RIGHT onto Track 273"M (WOO 273M) to Woodley and increase N2 by 2% and
continue with SID.
'.
~.
;, ,'.
.
r~,\
"JI
v
W
\ .
=ys CONCORDE
AID 8ev 13ft
TAKE-OFF DATA NEW YORK
J FKENNEDY
FULL LENGTH RWY 04L
CLG NIL RVR/VIS 600ft* SLOPENIL
TOR 3460m (11352ft) ED 3460m (11352ft) TOD(U) 2912m (9554ft)
OAT 101et Ine 51et Ine STILL Ine 101et Ine 201et Ine 301et
"C TAIL !Iet TAIL !Iet AIR !Iet HEAD Ikt HEAD Ikt HEAD
39 156.3 0.8 160.2 0.8 164.1 0.3 166.8 0.2 169.3 0.2 171.8
158/170 163/176 168/183 171/185 175/187 178/189
36 158.2 0.8 162.1 0.8 166.1 0.3 168.8 0.3 171.4 0.2 173.9
158/172 163/177 168/184 172/186 175/188 178/190
33 160.0 0.8 164.0 0.8 168.0 0.3 170.7 0.3 173.4 0.3 176.0
158/173 164/178 169/185 172/187 175/189 179/191
30 161.8 0.8 165.8 0.8 169.9 0.3 172.7 0.3 175.4 0.3 178.0
158/173 164/180 169/186 172/187 176/190 179/192
27 163.5 0.8 167.6 0.8 171.8 0.3 174.6 0.3 177.3 0.3 180.0
158/174 163/181 169/187 173/188 176/192 180/193
24 165.2 0.8 169.3 0.9 173.6 0.3 176.4 0.3 179.2 0.3 181.9
158/175 163/181 169/187 173/189 177/193 180/194
21 166.9 0.8 171.0 0.9 175.3 0.3 178.2 0.3 181.1 0.3 183.8
158/175 163/181 169/188 173/190 177/194 180/195
18 168.5 0.8 172.7 0.9 177.0 0.3 179.9 0.3 182.8 0.3 185.6
158/175 163/181 169/189 173/192 177/194 180/196
15 170.0 0.9 174.3 0.9 178.6 0.3 181.5 0.3 184.5 0.3 187.4
158/176 163/181 169/188 173/192 177/194 181/197
12 171.3 0.9 175.6 0.9 179.9 0.3 182.9 0.3 185.8 0.3 188.7
158/177 164/182 169/189 173/193 177/195 181/198
9 171.8 0.9 176.1 0.9 180.5 0.3 183.5 0.3 186.4 0.3 189.2
159/179 164/184 170/190 174/193 178/196 182/198
6 172.3 0.9 176.6 0.9 181.0 0.3 183.9 0.3 186.8 0.3 189.6
159/179 165/185 171/191 175/194 179/196 183/198
3 172.8 0.9 177.1 0.9 181.5 0.3 184.5 0.3 187.2 0.3 190.0
160/179 166/186 172/192 176/195 180/196 183/198
0 173.2 0.9 177.5 0.9 182.0 0.3 184.8 0.3 187.6 0.3 190.4
161/180 167/187 172/192 176/194 180/197 184/199
·3 173.7 0.8 177.9 0.9 182.4 0.3 185.2 0.3 187.9 0.3 190.6
161/180 167/187 173/192 177/195 181/197 185/199
V2= VR+ 22 VR+ 22 VR+ 22 VR+ 22 VR+ 21 VR+ 21
82= 14.0 14.0 13.5 13.5 13.0 13.0
1.Vl WET SPEED: Vl WET IS Vt DRY minus 15kt.
2.-Talte-Off Minima: Where RVRNIS is shown as O.5sm (240001 orless. higher minima may apply if
any radio orvisual aids are unserviceable. See para l. t.5 on Page t.1.3.
,.
T.O.W.
1l1DOkg -10
4&
23.5
89.6
-5
4&
23.5
89.6
0
46
AMBIENT TEMPERATURE - DEGREES C
23.5
89.6
5 10 15 2D 2S 30 35
44 44 44 45 4&
1. 24.0 24.5 24.5 23.5 22.5
88.7 88.7 88.7 89.7 90.6
NOTE CHANGE Of WEIGHT SCALE BElOW ~
40 40 -40 41 42 44 46 49 52
13D 24.5 25.0 25.5 24.5 23.5 22.5 21.5 20.5 19.5
87.8 87.8 87.8 BB.5 89.4 90.1 91.1 92.D 92.8
36 36 36 '11 39 41 43 4& 49 51
128 25.5 26.0 26.5 25.5 2S.O 24.0 23.0 22.D 21.D 20.0 ~
8&.6 8&.6 8&.6 87.4 88.2 89.0 89.8 90.8 91.6 92.4
32 32 32 33 35 37 40 43 46 49
110 26.D 26.5 27.0 27.0 26.0 25.5 24.5 23.5 22.5 21.5
85.7 85.7 85.7 86.5 87.2 BB.O 88.8 89.& 90.4 91.3
THROm£nME
THROTlU LEVER ANGLE
Nz ,.
SECONDS
OEGREES
\-,. t !
. ..,
~-:H~ ... f
.,......
r.:
t·
r-:::: -
:-1-:-: ~--
.,., i ••
,
.
.......• ,
:1:
1:::-;:-
.. t +
'1";:':":
-, t-·
r:;: ~j ::i j l:::
--~ ...-.---+--+-- .... ----
. ..:'
:: .,..
~~1' - t ..... 0-_." I
. .. ~
t t-.
r:-:-:[ '-
.
t
.. :1-
.. ,
t
.,.
_ .. • 0-_ • • •
., .
---+-.....-
•• j I , , . ,
rr:
-.
~
~':1
!" .- .. 1 ~
2. *Take-Off Minima: Where RVR/VIS is shown as0.5sm (24000) orless, higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
l. Turn RIGHT once stabilised at 92 and a rate of climb of 500 f.p.m. has been achieved, using 250
bank (achieved in 6 secs) maintaining 9 2,
3. At Noise Abatement Time the Engineer cancels reheat and throttles to Noise Power. If the
Captain is notsatisfied that 235kt will beachieved, hecallsNegatiwe to stop the ElO cancelling .
reheat and throttling back. Once theCaptain is satisfied thattheaircrafthas achieved 235kt he \~
calls Noise Now and the Engineer cancels the reheat and throttles back.
5kt to 8kt increase in IAS may be expected between initiation of noise countdown and
stabilised speed afterthrottling for noise. (Thus 230kt becomes minimum speed at initiation of
noise countdown). At throttle time the acbiewed .peed b8IWean 23S-25OId is to be
maintained.
Should the speed have increased above 250kt prior to Noise Abatement Time whilst
maintaining 9 z (due to low temperatures and/or low heights). no adjustment to pitch attitude
should be made until afterthe power cutback when 250kt should be sought and maintained.
4. After throttling maintain achieved speed t235-250ktI and turn onto assigned heading
(preferably 17l1"MI using no more than 100 bank. If assigned heading has been achieved prior
to throttle, maintain heading and throttle at given time.
At JFK 5d increase Nzto give Maximum Climb Power (over 10 secs) to accelerate or climb as
cleared by ATC.
2. Turn RIGHT once stabilised at 92 and arate of climb of 500 f.p.m. hasbeen achieved, using 250
bank lachieved in 6 secs) maintaining 92'
3. At Noise Abatement Time the Engineer cancels reheat and throttles to Noise Power. If the
Captain is notsatisfied that235kt will be achieved, hecalls Negative to stop the ElO cancelling
reheat and throttling back. Once theCaptain is satisfied thattheaircrafthas achieved 235kt he . .,)
calls Noise Now and the Engineer cancels the reheat and throttles back. .......,
5kt to Skt increase in IAS may be expected between initiation of noise countdown and
stabilised speed after throttling for noise. (Thus 230kt becomes minimum speed at initiation of
noise countdownl. At throttle time the achieved speed between m-25G1d is to be
maintained.
Co After throttling maintain achieved speed (235-250kt) and turn onto assigned heading ~
(preferably 18O"M) using nomore than IIr bank. If assigned heading has been achieved prior
to throttle, maintain heading and throttle at given time.
At JFK 5d increase N2 to give Maximum Climb Power (over 10 secslto accelerate or climb as
~~~ ~
NOTE:
s) For Take-off Weights below 140,oookg turn Right at 300ft QNH onto a heading of 18O"M
using 25" bank applied expeditiously.
b) If not given a heading of 18O"M prior to departure, request it and be prepared to delay
until request is granted - tIIis is Important for this highly sensitive Runway.
2.*Take-Off Minima: Where RVRIVIS is shown as0.5sm (240001 orless, higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
2. Turn RIGHT once stab~ised at82 and a rate of climb of500 f.pm.has been achieved. Using 25"
bank lachieved in 6 secs) maintaining 82'
3. At Noise Abatement Time the Engineer cancels reheat and throttles to Noise Power. If the
captain is notsatisfied that2351ct will beachieved. hecallsNegative to stop theEIO cancelling
reheat and throttling back. Once theCaptain is satisfied thattheaircrafthas achieved 2351ct he v . ).
calls Noise Now and the Engineer cancels the reheat and throttles back. ~
Slct to Ski increase in IAS may be expected between initiation of noise countdown and
stabilised speed afterthrottling for noise. (Thus 2301ct becomes minimum speed at initiation of
noise countdown). At throttle time the acbleYed spaed between Z3S-2SDld is to be
maintained.
4. After throttling maintain achieved speed (23S-2501ct) and tum onto assigned heading
(preferably Il1O"M) using nomore than Ill" bank. If assigned heading has been achieved prior
to throttle. maintain heading and throttle at given time.
At JRC 5dincrease N2 to give Maximum Climb Power (oyer 10 secslto accelerate or climb as
cleared by ATe.
NOTE:
a) For Tak~ff Weights below 140.DOllkg tum Right at 300ft QNH onto a heading of 18U"M
using ZSO bank applied expeditiously.
bl If not given a heading of 18O"M prior to departure. request it and be prepared to delay
until request is granted - this Is bDponaDl for this highly sensitive Runway.
'-' 115
5&
22.0
90.8
5&
22.0
90.8
57
22.0
911.8
57
21.D
91.&
58
20JI
92.4
58
19.0
93.2
1U
59
94.0
60
17.5
94.7
61
16.5
95.4
62
15.5
96.2
54 54 55 55 5& 5& 57 57 58 59
1111 23.0 23.D 23.0 22.0 21.0 20.0 19.5 18.5 17.5 16.5
90.0 9lI.D 90.0 90.8 91.6 92.4 93.1 93.8 94.5 95.3
52 52 53 53 54 54 55 5& 57 58
155 23.5 23.5 23.5 22.5 22.0 21.0 2D.O 19.0 18.5 17.5
89.5 89.5 89.5 90.2 9O.!l 91.1 92.4 93.2 93.9 94.7
50 50 51 51 52 52 53 54 55 5&
150 24.0 24.D 24.0 23.5 22.5 21.5 21.0 20JI 19.0 IB.o
88.9 88.9 B8.9 89.5 90.2 91.0 91.1 92.5 93.2 94.0
~ NOTE CHANGE Of WEl8HT SCALE BBOW
47 47 48 48 49 49 50 51 52 53
1. 24.5 25.0 25.0 24.5 24.0 23.0 22.0 21.5 20.5 20.0
87.7 87.7 87.7 88.6 89.2 89.8 90.5 91.2 91.9 92.6
43 43 44 44 45 45 46 47 48 49
1311 25.5 26.0 26.5 2&.0 25.0 24.5 23.5 22.5 21.5 21.0
86.8 86.8 86.8 87.5 88.2 88.9 89.6 90.3 91.0 91.1
«J 40 41 41 42 42 43 44 45 46
1211 26.0 26.5 27.0 27.0 26.0 25.0 24.5 23.5 23.D 22.0
85.8 85.8 B5.8 86.5 87.2 87.9 88.6 B9.3 9O.D 90.7
:J1 :J1 38 38 39 39 40 41 42 43
110 26.5 27.0 27.5 27.5 27.0 26.0 25.5 24.5 24.D 23.0
85.0 85.0 85.0 85.7 86.4 87.1 87.8 88.5 89.2 89.9
lHRDnU lIME SECONDS
1HHOITLE LEVER ANGlE DEBJIEES
~ Nz 'lit
......,
. .J
This chart is only to be used after the calculation of the Corrected Performance RTOW.
This chart is only to be used after the calculation of the Corrected Performance RTOW.
, ,)
~
This chart is only to be used after the calculation of the Corrected Performance RTOW.
RWY 22
(223OM)
This chart is only to be used aftet the calculation of the Corrected Performance RTOW.
This chart is only to be used after the calculation of the Corrected Performance RTOW.
RWY R
(223ClM)
2.*Talce-Off Minima: Where RVR/VIS is shown asO.5sm 1240Oft) orless, higher minima may apply if ~
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
2. -Take-Off Minima: Where RVRJV\S is shown as O.5sm 1240001 orless, higher minima may apply if ~
any radio orvisual aids are unserviceable. See para 1.1.5 onPage 1.1.3.
.......,"j
,
2.Tum LEFT once stabilised at92 and a rate of climb of SIlO f.pm. hasbeen achieved, using 2S"
bank (achieved in & secs) maintaining 9 2'
3. At Noise Abatement Tune Itle Engineer cancels reheat and Itlrottles to Noise Power. If the
Captain is not satisfied that 235fcl will be achieved, he calls Neptin to stDp the EJO cancelling
rehllseatNoan1d thMrottlin g bdaCthk. Once theCaptain issatisfied thatthe aircrafthas achieved 2351ct he , " .l
ca .. ow an e Engineer cancels tile reheat and throttles back. .....,
5lct to 81ct increase in JAS may be expected between i11i1iatioa of noise countdown and
stabilised speed afterthrottling fornoise. (Thus 230kt becomes minimum speed at initiation of
noise countdown). At throttle time Itle achieved speed Inltweeft Z35-25lItt is to be
maintained.
4. At heading of 235"M increae N2 rapidly to give Maximum Climb Power and decrease bank
angle to 75' to enable 250lIft crossing altitude to be achieved. Maintain 250tt On achieving
JRC 253ft apia throttle to Bug Power. AtCRI 5d linty increase ~ to Qimb Power (over 10
secs).
MOlE:
a) After passing 25DOft QNH bank angle may be increased to optimise tracking.
It) In the unlikely event of II1lt achieving 2SOOft QNH by JFX 253R leave Maximum Climb
Power until passing 2500ft QNH.
Continue with alternate one vertical profile, maintaining a LEFT turn with 15" bank until
established on the assigned departure routing.
This chart is only to be used after the calculation of the Corrected Performance RTOW.
\.. .
~
This chart is only to be used alter the calculation of the Corrected Performance RTOW.
This chart is onlv to be used after the calculation of the Corrected Performance RTOW.
~I
This chart is only to be used after the calculation of the Corrected Performance RTOW.
This chart is only to be used after the calculation of the Corrected Performance RTOW.
This chart is onlv to be used after the calculation of the Corrected Performance RTOW.
.. ,J
~
l. Turn LEFT once stabilised at 82 and a rate of climb of SlIJ f.p.m. has been achieved. using 25"
bank (achieved in 6 secs) maintaining 82'
3. At Noise Abatement Time the Engineer cancels reheat and thro1lles to Noise Power. If the
Captain isnotsatisfied that235kt will be achieved, hacalls Nltlativeto stop the EIO cancelling
reheat and throtlling back. Once theCaptain is satisfied thattheaircraft has achieved 235kt h e . .." J
calls NDise Now and the Engineer cancels the reheat and throttles back. ~
5lc1 to 8tt increase in IAS may be expected between initiatioa of noise countdown and
stabilised speed afterthrottling for noise. (Thus 230kt becomes minimum speed at initiation of
noise countdown). At throtlle time the aclliend speed betweea ZIS-2SDkt is to be
maintained. .
4. At heading of 235°M increase N2 rapidly to give Maximum Climb Power and decrease b a n k . .".l
angle to 7.5" to enable 2500ft crossing altitude to be achieved. Maintain 25OIct. On achieving ~
JAC 2S3R agaio throtlle to Bug Power. At CRI 5d s10wty increase N2 to Climb Power lover 10
secsl.
NOlI:
at After passing 2500ft ONH bank angle may be increased to optimise tracking.
11) In the unlikely event of aot achieving 2500ft QNH by JAC 2S3R leave Maximum Cftmb
Power until passing 2500ft ONH.
Continue with alternate one vertical profile. maintaining a LEFT turn wil!l 15" bank ulltJl
established on the assigned departure routing.
,. 57
16.5
95.3
57
16.5
95.3
58
16.5
95.3
58
15.5
96.4
59
14.5
97.4
60
110
98.6
62
12.0
99.6
63
10.5
100.5
&4
9.5
101.6
65
8.D
102.7
55 55 5& 5& 57 58 60 61 &2 63
115 17.5 17.5 17.5 1&.5 15.5 14.0 13.0 12.0 10.5 9.5
94.3 94.3 94.3 95.5 96.5 91.& 98.6 99.5 100.& 101.6
53 53 54 54 55 5& 58 59 60 &1
no 19.0 19.0 19.0 17.5 16.5 15.0 14.0 13.0 12.0 10.5
93.4 93.4 93.4 94.5 95.5 96.6 97.6 98.6 99.6 100.6
51 51 52 52 53 54 5& 57 58 59
1&5 2D.D 20.0 20.0 18.5 17.5 16.5 15.0 14.0 13.0 11.5
92.5 92.5 92.5 93.6 94.6 95.6 96.7 97.7 98.6 99.7
49 49 50 50 51 52 54 55 5& 57
160 21.D 21.D 21.D 19.5 ll5 17.5 16.5 15.0 14.0 110
91.8 91.8 91.8 92.7 93.7 94.7 95.7 96.7 91.6 98.7
47 47 48 48 49 50 52 53 54 55
155 21.5 21.5 21.5 21.D 19.5 18.5 17.5 16.5 15.0 14.0
~ 91.D 91.D 91.D 91.8 92.7 93.8 94.7 95.6 96.6 91.7
45 45 4& 46 47 48 50 51 52 53
150 22.5 22.5 22.5 21.5 20.5 19.5 18.5 17.5 16.0 15.0
90.3 90.3 90.3 91.2 92.0 92.9 93.8 94.8 95.& 96.7
OAT 10kt lne SJct Ine STILL Ine 10kt Ine 20kt Ine 301et
"C TAIL /Iet TAlL /kt AIR !let HEAD !let HEAD !let HEAD
39 151.5 0.8 155.5 0.8 159.4 0.3 162.0 0.3 164.7 0.3 167.5
148/165 153/169 158/174 162/177 165/181 168/185
36 153.3 0.8 157.4 0.8 161.3 0.3 164.0 0.3 166.7 0.3 169.5
148/166 153/170 159/175 162/178 165/182 169/186
33 155.1 0.8 159.2 0.8 163.2 0.3 165.9 0.3 168.6 0.3 171.5
149/167 154/170 159/175 162/179 166/183 169/187
30 156.8 0.8 161.0 0.8 165.1 0.3 167.8 0.3 170.6 0.3 173.4
149/168 154/171 159/176 163/180 166/184 169/188
27 158.5 0.9 162.8 0.8 166.9 0.3 169.6 0.3 172.4 0.3 175.3
149/169 154/172 160/177 163/181 166/185 170/189
24 160.2 0.9 164.5 0.8 168.7 0.3 171.4 0.3 174.3 0.3 177.2
150/170 155/173 160/178 163/182 167/186 170/190
21 161.8 0.9 166.1 0.9 170.4 0.3 173.2 0.3 176.0 0.3 179.0
150/171 155/174 160/179 164/182 167/186 171/190
18 163.3 0.9 167.8 0.9 172.1 0.3 174.9 0.3 177.8 0.3 180.8
151/172 156/175 161/180 164/183 168/187 171/191
15 164.8 0.9 169.3 0.9 173.7 0.3 176.5 0.3 179.4 0.3 182.4
151/173 156/175 161/180 165/184 168/188 171/192
12 166.1 0.9 170.6 0.9 175.0 0.3 177.8 0.3 180.8 0.3 183.8
151/173 156/176 162/181 165/184 169/188 172/192
9 166.7 0.9 171.2 0.9 175.5 0.3 178.4 0.3 181.3 0.3 184.4
152/173 157/176 162/182 166/185 169/189 173/193
6 167.3 0.9 171.7 0.9 176.0 0.3 178.9 0.3 181.9 0.3 184.9
153/174 158/177 163/183 167/186 170/190 174/194
3 167.8 0.9 172.2 0.9 176.5 0.3 179.4 0.3 182.4 0.3 185.4
154/174 159/178 164/184 168/187 171/191 174/195
0 168.3 0.9 172.7 0.9 177.0 0.3 179.9 0.3 182.9 0.3 185.9
154/174 160/178 165/184 168/188 172/192 175/194
·3 168.8 0.9 173.1 0.9 177.5 0.3 180.3 0.3 183.3 0.3 186.3
155/174 160/179 166/185 169/188 173/192 176/195
V2= VR+ 23 VR+22 VR+22 VR+ 22 VR+ 21 VR+ 21
92= 14.5 14.0 14.0 13.5 13.5 13.5
1.V1 WET SPEED: VI WET is VI DRY minus 15kt.
2.-T-.off Minima: Where RVR/VIS is shown as0.5sm 124000) orless, higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
2. Tum LEFT once S1abiflSed at 92 and a rate of climb of 500 f.p.m. has been achieved, using 25"
bant (achieved in 6 secs) maintaining 92.
3. At Noise Abatement Tune the Engineer cancels reheat and throttles to Noise Power. If the
Captain isnotsatisfied that 235kt will beachieved, hecalls NegBtile to stopthe EIO canceUing
reheat and throttling baet. Once the Captain is satisfied thatthe aircraft hasachieved 235tt he , J
calls Noise Now and the Engineer cancels the reheat and throttles baet. ~
5tt to 8b increase in IAS may be expected between initiation of noise countdown and
stabilised speed after throtlling for noise. (Thus 230tt becomes minimum speed at initiation of
noise coumdown). At throttle time the addeved speed between 235-2!iGkt is to be
main1ained.
NOTE:
_I After passing 2500ft ONH bank angle may be increased to optimise tracking.
•1In the unlikely event of DOt achieving 2SOOft ONH by JFK253R leave Maximum Climb
Power until passing 25DOft ONH. ~
Continue with alternate one vertical profile. maintaining a lEFT tum with ISO bant until
es1abli$hed on the assigned departure routing. ~
39 151.6 0.8 155.6 0.8 159.5 0.3 162.1 0.3 164.8 0.3 167.5
___ 1iBLlQ5___ 153L1~~_ 15SL125_ 1~aL12S_ 65LlS~ ~SL1SS
36 153.4 0.8 157.4 0.8 161.4 0.3 164.1 0.3 166.8 0.3 169.6
___ 1~eLl66__ 15JL110_ 59l115__ 16~L12~_ 5l1SJ___ 69L1Sl
33 155.1 0.8 159.3 0.8 163.3 0.3 166.0 0.3 168.7 0.3 171.6
___ l~iLlQ1___ 15~L110___ 15iL12~___ 16~L1S0___ 166L1S~___ 16iL1SS
30 156.9 0.8 161.1 0.8 165.2 0.3 167.9 0.3 170.7 0.3 173.5
___ 1~6S__ 1~11 159L121___ 16JL1S 66L185_ 16~L1Si
27 158.6 0.9 162.9 0.8 167.0 0.3 169.7 0.3 172.5 0.3 175.4
___ ~L16i___ 15~~_ 160L11S__ 16JL1S1_ 66Ll86__ 20L19D
24 160.2 0.9 164.6 0.8 168.8 0.3 171.5 0.3 174.4 0.3 177.2
___ 150L110___ 155L11J___ 160L129___ 16JL18~__ 1~1l186___ 120L191
21 161.8 0.9 166.2 0.9 170.5 0.3 173.3 0.3 176.1 0.3 179.0
___ 15QL11l___ 155Lllt___ 16DL12i__ 16iLl8J___ ~1L181_ 2lL1iQ
18 163.3 0.9 167.9 0.9 172.2 0.3 175.0 0.3 177.9 0.3 180.8
l5lL11~___ ~5_ 161L1S0___ 16iLl~ 8L18S 1L191
15 164.8 0.9 169.4 0.9 173.8 0.3 176.6 0.3 179.5 0.3 182.5
___ 151L11J___ 156Ll26___ 161L181___ 165L1~__ 16Sl188___ 111L19J
12 166.0 0.9 170.7 0.9 175.1 0.3 177.9 0.3 180.9 0.3 183.9
___ 51LlIJ___ 1561116___ 16~L181___ 165L185__ 168L189___ 11~L19J
9 166.8 0.9 171.3 0.9 175.6 0.3 178.5 0.3 181.4 0.3 184.4
5aL1li_ 157Ll16..__ 16~L1ez__ 66L186 6iLliO__ 111L19J
6 167.4 0.9 171.8 0.9 176.1 0.3 179.0 0.3 182.0 0.3 185.0
___ 15JLllt___ 15eLl22___ 16JL181-__ 162L18 120L191_ iL19S
3 167.9" 0.9 172.3 0.9 176.7 0.3 179.6 0.3 182.5 0.3 185.5
___ 15~L12~___ 159L128___ 16~l18~___ 162L188___ 111L19Z___ 12~LliS
o 168.4 0.9 172.8 0.9 177.1 0.3 180.0 0.3 183.0 0.3 185.9
__ 1~L1li___ 15iLl29 165l185___ 168L189___ 12~L19J___ 115L195
-3 168.9 0.9 173.2 0.9 177.6 0.3 180.5 0.3 183.4 0.3 186.3
___ 155Ll2~___ 16DL18D___ 1~6L185__ 169L189_ 111L19J___ 126L195
V2= VR+ 23 VR+ 22 VR+ 22 VR+ 22 VR+ 21 VR+ 22
82= 14.5 14.0 14.0 13.5 13.5 13.5
2. Turn LEFT once stabilised at 02 and a rate of climb of 500 f.p.m. has been achieved, using 25°
bank (achieved in 6 secsl maintaining O2,
3. At Noise Abatement Time the Engineer cancels reheat and throttles to Noise Power. If the
Captain is notsatisfied that235kt will be achieved, hecalls Negative to stop the E10 cancelling
reheat and throttling back. Once the Captain is satisfied thattheaircrafthas achieved 235kt h e )
calls Noise Now and the Engineer cancels the reheat and throttles back. \.J
5kt to Skt increase in IAS may be expected between initiation of noise countdown and
stabilised speed afterthrottling for noise. (Thus 230kt becomes minimum speed at initiation of
noise countdown). At throttle time the achieved speed between 235-250kt is to be
maintained.
NOTE:
81 After passing 25000 ONH bank angle may be increased to eptirnise tracking.
bl In the unlikely event of not achieving 2500ft ONH by JFK 253R leave Maximum Climb
Power until passing 2500ft ONH.
Continue with ahernate one vertical profile. maintaining a LEFT turn with 15° bank until
established on the CRI 176R.
"
v -..
I.)
-
~
",--
~
i .)
I .)
\J/
. _. .
=vs
AID Elev
CONCORDE
569ft
TAKE-OFF DATA TORONTO
FULL LENGTH RWY 06L
CLG NIL RVR/VIS 12000 SLOPE 0.07% ON
TOR 3200m (105000) EO 3200m (10500ft) TOO(U) 3085m (10121ft)
OAT 10kt Inc 5k~ Inc STILL Inc 10~ Inc 20k~ Inc 30kt
C TAIL Ikt TAIL Ik~ AIR Ikl HEAD Ik~ HEAD Ik~ HEAD
39 154.2 0.8 158.2 0.8 162.2 0.3 164.8 0.3 167.5 0.3 170.1
___ l~~Ll§S___ 15~Ll21___ 15~L11S___ 1§,L1S,___ 1§§L1S§__ 1§~L1S~
36 156.0 0.8 160.1 0.8 164.2 0.3 166.8 0.3 169.5 0.3 172.2
___ l~~Ll§~___ 15~Lll~___ 15~Ll1~___ 1§~L18~___ 1§§L1Sl___ 1§2l12Q
33 157.8 0.8 162.0 0.8 166.1 0.3 168.8 0.3 171.5 0.3 174.2
___ 15QL12Q___ 155L12~___ 19QL18Q___ 191L18~___ lQQL1SS___ 11QL121
30 159.5 0.9 163.9 0.8 168.0 0.3 170.7 0.3 173.4 0.3 176.2
___ 15QL11Q___ 155L115___ 19OL181___ 161L185___ 191L1SS___ 110L12,
27 161.2 0.9 165.7 0.8 169.8 0.3 172.6 0.3 175.4 0.3 178.2
___ 151L121___ 155L12g___ 19OL1S6___ 16i[lS5___ 1§1[18~___ 110l1~1
24 162.9 0.9 167.4 0.9 171.7 0.3 174.4 0.3 177.2 0.3 180.1
___ 151L12~___ 15g[111___ 19lL186___ 16i[18g___ 192[1~0___ 111L12i
21 164.5 0.9 169.1 0.9 173.4 0.3 176.2 0.3 179.1 0.3 181.9
___ 151L12J___ 15gL111___ 191[181___ 165[181___ 198L121___ 111L125
18 166.1 0.9 170.8 0.9 175.1 0.3 178.0 0.3 180.8 0.3 183.7
___ 156L!2i___ 151L118___ 166L1Si___ 165[18S___ 16SL12~___ 11~[126
15 167.6 1.0 172.4 0.9 176.7 0.3 179.6 0.3 182.5 0.3 185.5
___ 156L115___ 152L122___ 16~[lSi___ 165L188___ 19~[l~~___ 11~Ll~g
12 168.8 1.0 173.7 0.9 178.1 0.3 180.9 0.3 183.9 0.3 186.8
___ 151L115___ 152L12~~__ 161[lS5___ 16g[18~___ 16~[121___ 11~L1~2
9 169.7 0.9 174.3 0.9 178.7 0.3 181.6 0.3 184.6 0.3 187.5
___ 15~L11Q___ 158L180___ 19~[lSg___ 19lL1~0___ 11QL12i___ 12iL1~S
6 170.5 0.9 175.0 0.9 179.4 0.3 182.3 0.3 185.2 0.3 188.1
___ 15iL11g___ 15~L1S1___ 19iL181___ 168L121___ 111L125___ 12iL1~~
3 171.3 0.9 175.6 0.9 180.0 0.3 182.9 0.3 185.8 0.3 188.7
___ 155L11§___ 190L18,___ 195L18S___ 168[12,___ 112L1~g___ 115L,00
o 171.8 0.9 176.1 0.9 180.6 0.3 183.5 0.3 186.4 0.3 189.3
___ 155L112___ 191L181___ 199[1S~___ 192Ll~l-__ 111L121___ 126L'01
-3 172.3 0.9 176.6 0.9 181.1 0.3 184.0 0.3 186.9 0.3 189.8
___ 15gL118___ 19lL18i___ 191L120___ 11QL12i__ 11iL128___ 111L'01
V2= VR+ 21 VR+ 21 VR+ 21 VR+ 20 VR+ 20 VR+ 21
82= 14.0 13.5 13.5 13.0 13.0 13.0
OAT 10kt Inc 5kt Inc STILL Inc 10kt Inc 20k\ Inc 30kt
• C TAIL /kt TAIL Ik~ AIR /k~ HEAD /kt HEAD /kt HEAD
39 150.9 0.9 155.2 0.8 159.1 0.3 161.7 0.3 164.3 0.3 167.0
--- l!~llg~___ l~gllIQ___ lSlLllg___ lSSL16Q___ lS6L16i___ 161L166
36 152.6 0.9 157.1 0.8 161.0 0.3 163.7 0.3 166.3 0.3 169.0
___ li,L166___ li2L121___ ls~L122___ lSSL1Sl___ lsaL1ai___ 16,L1aa
33 154.3 0.9 158.9 0.8 162.9 0.3 165.6 0.3 168.3 0.3 171.0
--_ li~L162___ liILl1Z___ lS~Ll11___ lSSL1Sl___ ls~LlaS___ 16~L16~
30 156.0 1.0 160.8 0.8 164.8 0.3 167.5 0.3 170.2 0.3 173.0
--- 1i~L16S___ li2Lll~___ lS~L12a___ lS6L1S6___ lS~L1S6___ 16~Ll~Q
27 156.8 1.1 162.5 0.8 166.6 0.3 169.3 0.3 172.1 0.3 174.9
--- 1~3L12Q___ liSL11~___ lSJL12~___ lS6L1S~___ ls~Lle2___ 161Ll~1
24 158.5 1.2 164.3 0.8 168.4 0.3 171.2 0.3 174.0 0.3 176.8
___ liiL121___ liSL12~___ lSJL1SQ___ lS2L1Si___ 160LleS___ 16JL1~~
21 160.2 1.2 166.0 0.8 170.1 0.3 172.9 0.3 175.8 0.3 178.7
___ 1iiL121___ 1~SL12~___ lSiL1SO___ lS2Lle~___ 160L166___ 19iLl~J
18 161.8 1.2 167.6 0.8 171.8 0.3 174.6 0.3 177.5 0.3 180.5
___ !~iL126___ li~L12S___ lSiLlel___ lS2LleS___ 161L162___ 16iLl~~
I
15 163.3 1.2 169.1 0.9 173.4 0.3 176.3 0.3 179.2 0.3 182.1 ......"
___ 1~SL12~___ 1i~L126___ lSiL1S6___ lSSL1Sg___ 161L1~0___ 16iL12~
12 164.5 1.2 170.4 0.9 174.7 0.3 177.6 0.3 180.5 0.3 183.5
___ 1iSL12J___ lSQL126___ lSSL1S6___ lSSL1S6___ 16~Ll~1___ 16SL12S
9 165.0 1.2 171.1 0.9 175.4 0.3 178.2 0.3 181.1 0.3 194.1
___ li6L12i___ lSQL12S___ lS6L1Si___ lS2L1SS___ 16~Ll~,___ 166L126
6 166.9 0.9 171.6 0.9 175.9 0.3 178.8 0.3 181.8 0.3 184.7
___ 1~6L12i___ lSlL112___ lS6L1SS___ 160L1S~___ 16JL12J___ 162L122
3 167.8 0.9 172.2 0.9 176.5 0.3 179.4 0.3 182.3 0.3 195.2
___ 1i1L12i___ lS~L1SQ___ 1S1L1S6___ 161L120___ 16iL12i___ 16eL12e
o 169.5 0.8 172.7 0.9 177.1 0.3 179.9 0.3 182.9 0.3 185.7
___ li1L12S___ lSJL1S1___ lSSL1S2___ 161L121___ 16SL1~~___ 168L122
. -3 169.0 0.8 173.2 0.9 177.5 0.3 190.4 0.3 183.2 0.3 186.1
. 1ieLJ.26___ lSJL1SL__ lS~LleS___ J.fiU12L__ 166Ll~6___ 16S!L~00 .
V2= VR+ 22 VR+ 21 VR+ 21 VR+ 21 VR+ 21 VR+ 21
82= 14.0 14.0 13.5 13.5 13.5 13.0
OAT 10kt Inc 5kt Inc STILL Inc 10kt Inc 20kt Inc 30kt
C TAIL /kt TAIL /ltt AIR /kt: HEAD /kt. HEAD /kf;. HEAD
39 162.0 0.8 166.0 0.8 169.8 0.2 172.2 0.2 174.6 0.2 177.0
___ 15QL126___ 155L16~___ 1~QL1a2___ l~~Ll~~___ 1~2Ll~~___ 12QL1~~
36 164.0 0.8 168.0 0.8 171.9 0.2 174.3 0.2 176.8 0.2 179.2
'",-" ___ 151L12~___ 155L165___ 1~QL1~0___ 1~~L1~J___ 1~1L121___ lllL~QQ
33 165.9 0.8 170.0 0.8 173.9 0.2 176.4 0.2 178.9 0.2 181.4
___ 151L16Q___ 15~L16~___ 161L191___ 1~~L1~~___ 1~6L126___ 111L~01
30 167.8 0.8 171.9 0.8 176.0 0.2 178.4 0.2 180.9 0.3 183.5
___ 151L161___ 156Lla~___ 1~lL1~~___ 165L125___ 166L122___ 111L~Q£
27 169.7 0.8 173.8 0.8 177.9 0.2 180.4 0.3 183.0 0.3 185.6
___ 15~L16~__ 151L161___ 16~L121___ 165L126___ 16aL~OQ___ 11~L~OJ
24 171.5 0.8 175.7 0.8 179.9 0.2 182.4 0.3 185.0 0.3 187.6
___ 15~L16~___ 151L166___ 16~L1~~___ 165L121___ 16~L~Q1___ 12~L~0~
21 173.3 0.8 177.5 0.9 181.8 0.2 184.3 0.3 186.9 0.3 189.6
___ 15~L1aJ___ 151Lla~___ 16~L1~5___ 166L126___ l~~L~Q~___ 12JLZ05
18 175.0 0.9 179.3 0.9 183.6 0.3 186.2 0.3 188.8 0.3 191.5
___ 156L1a~___ 158L190___ 1~JL125___ 166L122___ 11QL&0~___ 12JL&0~
15 176.5 0.9 180.9 0.9 185.3 0.3 188.0 0.3 190.6 0.3 193.3
___ 156L16~___ 156L12Q___ 1~JL12~___ 1~1L~QO___ 12gL~QJ___ 12~LZQ1
12 177.8 0.9 182.2 0.9 186.7 0.3 189.3 0.3 192.0 0.3 194.7
___ 15~L165___ 156L121__~ 16~L122___ l~lL~QQ___ 111L~Q~___ 11~L~Ql
9 178.5 0.9 182.9 0.9 187.3 0.3 189.9 0.3 192.6 0.2 195.0
___ 15JL166___ 152L12~___ 16~L126___ 166L~Q1__ 116L~Q5___ 115L~Q6
6 179.1 0.9 183.5 0.9 187.8 0.3 190.5 0.3 193.1 0.2 195.0
___ 15~L161___ 152L12J___ 1~5L122___ 162L6Q6___ 11JL606___ 116LZQ2
3 179.7 0.9 184.1 0.8 188.3 0.3 191.0 0.3 193.7 0.1 195.0
___ 15~L166___ 1~QL12~___ 166L122___ 11QL~QJ___ 11JLaQ~_~_ 116L,Q2
o 180.2 0.9 184.7 0.8 188.8 0.3 191.5 0.3 194.2 0.1 195.0
_ 155L162___ 161L125___ 19lL6QQ___ 111L6Q~___ 11~L~Q2-_ 111L~lQ
-3 180.7 0.9 185.1 0.8 189.2 0.3 191.9 0.3 194.6 0.0 195.0
___ 15gL162 19lL125 192L~Ql 111L,Q~ 125LaQ6 126L~lQ.
OAT 10k~ Inc 5k~ Inc STILL Inc 10kt Inc 20k~ Inc 30k~
C TAIL /k~ TAIL /kt AIR /kt HEAD /kt HEAD Itt HEAD
39 154.6 0.8 158.8 0.8 162.8 0.2 164.9 0.2 167.2 0.2 169.6
___ ~OLlGe 1~5L113 15QLll~ lS3L1S~ 151L1S5 lSQL1S~
36 156.3 0.9 160.7 0.8 164.7 0.2 166.9 0.2 169.3 0.2 171.7
___ 1~oL16~___ 1~5L11~___ 150L1eO___ 153L1B3___ 151L1BG___ lSQL1~0
33 158.1 0.9 162.5 0.8 166.7 0.2 168.8 0.2 171.2 0.2 173.7
___ 1~lL110___ 1~5L11S___ 15QLle1___ ls~L1B~___ 151L1B2___ 19lLl~l
30 159.7 0.9 164.4 0.8 168.6 0.2 170.7 0.2 173.2 0.2 175.7
___ 1~lL111___ 1~gL!2S___ lSlL1e~___ 15~L1BS___ lSBL1BB___ lSlL12~
27 161.4 1.0 166.2 0.8 170.4 0.2 172.6 0.2 175.1 0.2 177.6
___ 1~!Lll1___ 1~gL11S___ 151L!B~___ 15SL1BS___ lSBL1B2___ 16~L12~
24 162.9 1.0 167.9 0.9 172.2 0.2 174.4 0.2 176.9 0.3 179.5 , ..J
~
___ 1~,L11~___ 1~SL122___ lSlL!B~___ 155L1B6___ lSBL12Q___ lS,L12J
21 164.4 1.0 169.6 0.9 173.9 0.2 176.2 0.2 178.7 0.3 181.3
___ 1~~L11J___ 1~2L!2S___ lS6L!B1___ 15SL1B2___ lS2L1~Q___ ls,L12~
18 165.9 1.1 171.3 0.9 175.6 0.2 177.9 0.3 180.5 0.3 183.1
___ 1~JL12~___ 112L122___ 156L!Bi___ lS6L!BB___ 152L121___ !gJL125
15 167.3 1.1 172.9 0.9 177.3 0.2 179.5 0.3 182.1 0.3 184.7
___ 1~JL125___ 1~BL122___ lSJL1BS___ 156L!SB___ lSoL126___ lSJL12S
12 168.6 1.1 174.2 0.8 178.3 0.3 180.9 0.3 183.5 0.3 186.1
___ 1~1L12S___ 1~BL1SQ___ lSJL1BS___ 152L1B2___ lSQL12~___ lS~Ll~6
9 169.9 1.0 174.9 0.8 179.0 0.3 181.6 0.3 184.2 0.3 186.9
___ 1~~L126___ 1~2L1Sl___ lS~L1B2___ 152L12Q___ lSlL12~___ lSSL121
6 171.1 0.9 175.6 0.8 179.7 0.3 182.3 0.3 184.9 0.3 187.6
___ !~~L11S___ 1~2L1B,___ lsSL1BB___ 15BL121___ lS~L125___ lSSL12S
3 172.0 0.9 176.3 0.8 180.3 0.3 183.0 0.3 185.6 0.3 188.3
___ 1~sL121___ lSQL1BJ___ 15SL1B2___ lS2L12,___ !SJL12g___ 16SL122
o 172.6 0.9 177.0 0.8 181.0 0.3 183.6 0.3 186.2 0.3 189.0
___ 1~6L11B__ lS1L1B~___ 15SL12Q___ 16QL123___ 163L121___ lS1L,00
-3 173.2 0.9 177.5 0.8 181.5 0.3 184.1' 0.3 186.8 0.3 189.5
___ 1~sL12~___ lS1LleS___ 152L120___ 16QL1~~___ lS~L1ge___ lSBL~Ql .
V2= VR+ 21 VR+ 21 VR+ 21 VR+ 21 VR+ 20 VR+ 21
82= 14.0 13.5 13.5 13.0 13.0 13.0
OAT 10kt Ine 5k~ Ine STILL Ine 10kt: Ine 20k~ Ine 30k~
. C TAIL Ik~ TAIL /kC AIR Ikt HEAD Ikt: HEAD Ikt HEAD
39 155.2 O.B 159.0 O.B 162.9 0.3 165.5 0.2 167.9 0.2 170.2
___ ~~L16~___ lS~L12S___ 4S~L1e1___ 16~Lle~___ 16SLle~___ 162L12Q
36 157.1 O.B 160.9 O.B 164.9 0.3 167.6 0.2 170.0 0.2 172.3
___ 1~~LI1Q___ 15~L11g___ 15~Lle~___ 16~le5___ 199L4~Q___ 19~1lil
33 158.9 O.B 162.B O.B 166.9 0.3 169.5 0.2 172.0 0.2 174.4
___ 1~~L111___ 15~L111___ 15~Lle~___ 16JLle6___ 166Ll~4___ 41QL1~~
30 160.7 O.B 164.7 O.B 16B.8 0.3 171.5 0.2 174.0 0.2 176.4
___ 15QL11~___ lSSL111___ 16QL1e~___ 16JLle1___ 166L12~___ 11QL12J
27 162.5 O.B 166.5 O.B 170.6 0.3 173.4 0.3 176.0 0.2 17B.4
___ 15QL11~___ 155L11e___ 16QL1e~___ 16JL1ee___ 161L122___ 11QL12~
24 164.3 O.B 16B.3 O.B 172.5 0.3 175.3 0.3 177.9 0.2 IBO.4
___ 15QL11~___ 1S5L112___ 16QLle5___ 16~Lla2___ 161L12J___ 111l1~~
21 165.9 O.B 170.0 O.B 174.2 0.3 177.1 0.3 179.8 0.2 182.3
___ 15!L11~___ 156LlaQ___ 161LlaQ___ 16~L1~Q___ 16aL!2!___ 111L125
1B 167.4 0.9 171.7 0.9 176.0 0.3 178.B 0.3 181.7 0.2 184.2
___ 151L115___ 156L1aQ___ 161Lla6___ 165L12Q___ 16aL12!___ 112L122
15 168.9 0.9 173.3 0.9 177.6 0.3 IBO.5 0.3 183.4 0.3 IB6.0
___ 15~L116___ lS1L1e1___ 16~L1e1___ 165L121___ 16eL125___ 112L1~2
12 170.2 0.9 174.6 0.9 178.9 0.3 181.8 0.3 184.8 0.2 187.3
___ 156L116___ 151L1a~~__ 162Llae___ 166L1~~___ 162L126___ 111L~QQ
9 171.0 0.8 175.2 0.9 179.6 0.3 182.5 0.3 185.2 0.3 187.8
___ lS~L111__ 15eL1e~___ 16JL1e2___ 166L12~___ 110L121___ 11~L12a
6 171.6 0.8 175.8 0.9 180.2 0.3 183.0 0.3 185.6 0.3 188.2
___ 1S~L11a___ 152L1a~___ 16~L12Q___ 1Q1L12~___ 111L1~2___ 11~L2Q1
3 172.2 0.8 176.4 0.9 180.8 0.3 183.6 0.2 186.1 0.2 188.6
___ lS~L112___ lS2L1eS___ 165L121__ 16eL125___ 11~L~QO___ 115L~Q~
o 172.7 0.9 177.0 0.9 181.3 0.3 184.0 0.2 186.5 0.2 189.0
___ 155L1aQ___ 16QL1a6___ 165L12~___ 162L126___ 12~L~Q1___ 116L~Q5
-3 173.2 0.8 177.4 0.9 181.8 0.2 184.3 0.2 186.7 0.3 189.3
___ 156L1a1___ 161L1aZ___ 166L19J____ 1zoLl~1___ 11~L~Q~___ 111l~Q6
OAT 10kt Inc 5kt Inc STILL Inc 10k~ Inc 20kt Inc 30kt
. C TAIL /kt TAIL /kt AIR /kt HEAD /k~ HEAD /kt HEAD
39 159.4 0.8 163.3 0.8 167.3 0.2 169.6 0.2 171.9 0.3 175.1
--- l5~lll~___ 15~LleO___ 16ll1e5___ 16SL1~O___ 166L1~!___ 121Ll~1
36 161.3 0.8 165.3 0.8 169.3 0.2 171.7 0.2 174.0 0.3 177.2
___ 15~L125___ 152Lle1___ 16~Lle6___ 16SL1~1___ 16~Ll~S___ 12~ll~e
33 163.2 0.8 167.2 0.8 171.3 0.2 173.8 0.2 176.1 0.3 179.3
___ 15,L126___ lS1Llel___ 16~L1e2___ 16SL1~1___ 16~Ll~~___ 126Ll~2
30 165.0 0.8 169.1 0.8 173.3 0.2 175.8 0.2 178.1 0.2 180.6
___ 15JL112___ lS6L166___ 16~L1ee___ 166L126___ 16~Ll~2___ 11JL601
27 166.8 0.8 171.0 0.8 175.2 0.3 177.8 0.2 180.2 0.2 182.6
___ ls~L122___ lS6L1e~___ 16JL16~___ 166Ll~~___ 120L12e___ !2JL6Q6
24 168.6 0.8 172.8 0.8 177.0 0.3 179.8 0.2 182.2 0.2 184.6
___ lSJL12e___ lS6L1e~___ 16JL1~O___ 1~2L12~___ 12QL12e___ 12~L6Q~
21 170.3 0.8 174.5 0.9 178.8 0.3 181.7 0.2 184.1 0.2 186.6
___ lS~L122___ lS2LleS___ 16~L121___ 162L12~___ 121L122___ 12~L6Q~
18 172.0 0.8 176.2 0.9 180.6 0.3 183.5 0.2 186.0 0.2 188.5
___ lS1L122___ !52L1eS___ 16~L!21 162L125___ 12!L6QQ___ !2~L6Q!
15 173.6 0.9 177.9 0.9 182.2 0.3 185.2 0.3 187.8 0.2 190.3
___ lSSL1eO___ 160L1e6___ 16SL126___ 16eL!26___ 111L6QQ___ !2SL6QS
12 174.8 0.9 179.2 0.9 183.6 0.3 186.6 0.3 189.2 0.2 191.7
___ 15SL1e1___ 16QL162___ 16SL12J___ 166L122___ 12~L601___ 12~L605
9 175.5 0.9 179.9 0.9 184.4 0.3 187.1 0.2 189.6 0.3 192.2
___ lSsL1e6___ 161L1ee___ 166L12!___ 16~L12e___ 11JL,06___ 12~L602
6 176.2 0.9 180.6 0.9 185.0 0.3 187.6 0.2 190.1 0.4 193.7
___ lS6L1e1___ 166L1e2___ 161L12S___ 110L122___ 111L60~___ 121L6Q6
3 176.7 0.9 181.1 0.9 185.5 0.2 188.0 0.2 190.5 0.4 194.4
___ lSlL1ei___ 1~~L12Q___ 16eL126___ 121L6Q1___ 115L605___ 116L6Q1
o 177.3 0.9 181.6 0.9 185.9 0.2 188.4 0.4 192.0 0.3 194.9
___ 152L1eS___ 16JL121___ 16eL122___ 116L6Q6___ 12SLZOi___ 122L6Qe
-3 177.7 0.9 182.1 0.8 186.2 0.3 189.7 0.3 192.5 0.2 195.0
___ 15aLle~___ 1~~L12~___ 162L12e___ 123L601___ 11~LZQS___ 11~L602
OAT 10kt Inc 5kt Inc STILL Inc 10kt Inc 20kt Inc 30kt
C TAIL /kt TAIL /kt AIR /kt HEAD /kt HEAD /kt HEAD
39 166.0 0.8 170.1 0.8 174.2 0.3 177.0 0.3 179.7 0.3 182.3
___ lS~lle~___ 151Llee___ l~~Ll~~___ 1~~L1ge___ 11QL~Q~___ 12JL~05
36 168.0 0.8 172.1 0.8 176.3 0.3 179.1 0.3 181.8 0.3 184.5
___ 151L1eJ___ 151L1e~___ 1~JL1~5___ 1~~L122___ 11QL~QJ___ 11JL6Q1
33 169.9 0.8 174.1 0.8 178.3 0.3 181.1 0.3 183.9 0.3 186.7
___ 151L1e~___ 151L120___ 1~~L12~___ l~~L'QO___ 11QL604___ 11~L,oe
30 171.8 0.8 176.0 0.9 180.3 0.3 183.1 0.3 186.0 0.3 188.8
___ 151LleS___ 151L1~1 1§6Ll~1___ 1~6L6QO___ 162L604___ 12JL6Qe
27 173.6 0.9 177.9 0.9 182.2 0.3 185.1 0.3 188.0 0.3 190.8
___ 151Ll65___ 156L121___ 166L121___ 1~6L~01___ 162L6Q~___ 12JL6Q~
~4 ~7S.4 0.9 179.7 0.9 184.1 0.3 187.0 0.3 189.9 0.3 192.8
___ 151L1e~___ 156L126___ 1~2L1~e___ 166L6Q2___ 162L606___ 11JL61Q
21 177.1 0.9 181.5 0.9 185.9 0.3 188.9 0.3 191.8 0.3 194.5
___ 151LleZ___ 156Ll~J___ 166L12~___ lSSL6QJ___ 1~~L6Q2___ 12JL610
18 178.8 0.9 183.2 0.9 187.7 0.3 190.7 0.3 193.6 0.1 195.0
___ 151L1el___
15 180.4
156Ll~1___
0.9 194.8
16,L19~___
0.9 189.4
1~~L60J___
0.3 192.4
1~2L6Q2___
0.3 195.0
126L210
0.0 195.0
\..,;
__ lSlL1ee___ 156L1~~___ 16,L,~0___ 16§L6Q~___ lS~L60e___ 126L61Q
12 181.7 0.9 196.2 0.9 190.8 0.3 193.7 0.1 195.0 0.0 195.0
___ lSlL1e2___ 152L195___ 62L201___ 166L605___ 162L601___ 126L609
9 182.5 0.9 187.0 0.9 191.4 0.3 194.3 0.1 195.0 0.0 195.0
___ 152119Q__ 152L196___ 16lL2Q,___ 162L2Q5___ 11QL,oe___ 12,L,lQ
6 193.2 0.9 197.7 0.9 192.0 0.3 194.9 0.0 195.0 0.0 195.0
___ 152Ll~1___ 15eL191___ 16!L2QJ___ 161L~QS___ l1QL~09___ 11JL211
3 183.9 0.9 199.4 0.8 192.6 0.2 195.0 0.0 195.0 0.0 195.0
___ 153L192___ 159L12e___ 16!L20~___ lSeL6Q1___ 11QL602___ 11JL211
o 184.5 0.9 189.0 0.9 193.3 0.2 195.0 0.0 195.0 0.0 195.0
5~L121___ 159L122___ 16SL205___ 16eL,oe___ 111L210___ 12!L616
-3 185.1 0.9 189.6 0.9 193.9 0.1 195.0 0.0 195.0 0.0 195.0
___ 15~L1~~___ 16QLZQO___ 166L2Q6___ 16~LZQa-__ l11L~lQ___ 12~LZ1a
OAT 10kt Inc 5kt Inc STILL Inc 10kt Inc 20kt Inc 30kt
C TAIL /kt TAIL /kt AIR /kt HEAD /kt HEAD /kt HEAD
39 162.4 0.8 166.4 0.8 170.5 0.3 173.1 0.3 175.7 0.3 178.3
___ l~!llll___ 15~Lla~___ 165L1a~___ 168Ll~~___ 111Ll~6___ 115LZQQ
36 164.3 0.8 168.4 0.8 172.5 0.3 175.2 0.3 177.9 0.3 180.5
___ 1~~L128___ 152L18~___ 165L1~Q___ 168L12~___ 12~L122___ b25L~Ql ~
33 166.2 0.8 170.3 0.8 174.5 0.3 177.2 0.3 179.9 0.3 182.7
___ 15~L122___ 152Lle~___ lS~L12Q___ 168L12~___ 11~L128___ 175L~0~
30 168.0 0.8 172.2 0.8 176.4 0.3 179.2 0.3 181.9 0.3 184.7
___ 15~L112___ 152L165___ lS~L!21___ 168L125___ 11~L122___ 11SLZOJ
27 169.8 0.8 174.0 0.9 178.3 0.3 181.1 0.3 183.9 0.3 186.7
___ lSJL18Q___ 158L186___ 16~L1~~___ 168L126___ 111L~OQ___ 125L~0~
24 171.6 0.8 175.8 0.9 180.2 0.3 183.0 0.3 185.8 0.3 188.7
___ 15~L181___ 158L181___ 16~L12J___ 168L122___ 111L~OQ___ 11SLzo~
21 173.2 0.9 177.6 0.9 182.0 0.3 184.8 0.3 187.7 0.3 190.6
___ 15JL181___ 158L181___ 16~L12J___ 168L121___ 111L~01___ 11SLZQ5
18 174.9 0.9 179.3 0.9 183.7 0.3 186.6 0.3 189.5 0.3 192.4
___ 153L18Z___ 158L188___ 16~L12~___ 168L128___ 111L606___ 115LZQ6
15 176.5 0.9 180.9 0.9 185.4 0.3 188.3 0.3 191.2 0.3 194.2
___ 153L183___ 158L182___ 16~L125___ 168L122-__ 111L~Q~___ 115L~06
12 177.8 0.9 182.2 0.9 186.7 0.3 189.7 0.3 192.6 0.2 195.0
___ 153L18J___ 152L162___ 16~L125___ 168L122___ 11~L~OJ___ 115LZQl
9 178.5 0.9 182.9 0.9 187.4 0.3 190.4 0.3 193.3 0.2 195.0
___ 15~L1e~___ 152L12Q___ 165L126___ 162LZQQ___ 11ZL~Oi___ 116LZQ1
6 179.1 0.9 183.5 0.9 188.1 0.3 191.0 0.3 193.9 0.1 195.0
___ 15~L18S___ 16QL121___ 166L121___ 162LZQ1___ 12JLZQ5___ 116Lz08
3 179.7 0.9 184.2 0.9 188.7 0.3 191.6 0.3 194.5 0.0 195.0
___ 155L186___ 161L12~___ 166L128___ 12QL~Q~___ 11~L~Q6___ 116L~Q2
o 180.3 0.9 184.8 0.9 189.3 0.3 192.2 0.3 195.0 0.0 195.0
___ 156L181___ 161L123___ 161L122___ 111L'Q3___ 115LZQ1___ 111L,Q2
-3 180.8 0.9 185.3 0.9 189.8 0.3 192.7 0.2 195.0 0.0 195.0
___ 156L188___ 16ZL12i___ 168LZQQ___ 11ZL~Q~___ 115L~Q1___ 128L~lQ
"-' 1811
69
17.5
69
17.5
69
17.5
70
16.5
70
15.5
96.2
70
15.0
71
14.0
97.8
72
13.0
98.5
73
12.0
99.3
74
11.0
100.2
94.5 94.5 94.5 95.3 95.9
67 67 67 68 6B 68 69 70 71 72
175 18.5 18.5 18.5 17.5 16.5 15.5 14.5 14.0 13.0 12.0
93.8 93.8 93.8 94.6 95.4 96.2 97.0 97.8 98.6 99.3
65 65 65 66 66 66 67 68 69 70
170 19.5 19.5 19.5 18.5 17.5 16.5 15.0 14.5 14.0 13.0
93.0 93.0 93.0 93.8 94.6 95.4 96.2 97.0 97.8 98.6
63 63 63 64 64 64 65 66 67 6B
165 20.0 20.0 20.0 19.5 18.0 17.5 16.5 15.5 14.5 14.0
92.3 92.3 92.3 93.1 94.0 94.1 95.4 96.2 97.0 97.1
61 61 61 62 62 62 63 64 65 66
~ 160 21.0 21.0 21.0 20.0 19.0 18.0 17.5 16.5 15.5 14.5
91.6 91.6 91.6 92.5 93.2 94.0 94.8 95.5 96.3 97.0
59 59 59 60 60 60 61 62 63 64
155 22.0 22.0 22.0 21.0 20.0 19.0 18.0 17.5 16.5 15.5
90.8 90.8 90.8 91.6 92.4 93.2 94.0 94.7 95.5 96.2
5& 56 56 57 57 57 58 59 60 61
~ 150 23.0 23.0 23.0 22.0 21.0 20.0 19.0 18.0 17.0 16.5
90.1 90.1 90.1 90.9 91.7 92.5 93.2 94.0 94.9 95.5
NOTE CHANGE OF WEIGHT SCALE BELOW
51 51 51 52 52 52 53 53 54 55
14U 23.5 24.0 24.0 23.5 22.5 21.5 20.5 19.5 19.0 18.0
89.0 89.0 89.0 89.1 90.5 91.3 92.0 92.8 93.5 94.2
46 46 46 47 47 47 48 48 49 50
~ 130 24.0 25.0 25.0 24.5 23.5 22.5 22.0 21.0 20.0 19.0
87.9 87.9 87.9 88.7 89.5 90.2 90.9 91.5 92.4 93.1
41 41 41 42 42 42 43 43 44 45
120 24.5 25.5 26.0 25.5 24.5 24.0 23.0 22.0 21.0 20.0
87.1 87.1 B7.1 87.8 BB.6 89.3 90.0 90.1 91.4 92.2
36 36 36 37 37 37 38 38 38 39
110 25.5 26.0 26.5 26.5 26.0 24.5 24.5 23.5 22.0 21.0
86.3 86.3 B6.3 87.0 87.7 88.5 89.2 89.9 90.7 91.4
THROmE TIME SECONDS
THRonLE LEVER ANGLE DEGREES
Nz %
OAT 10kt Inc 5kt Inc STILL Inc 10kt Inc 20kt Inc 30kt
C TAIL /kt TAIL /kt AIR /kt HEAD /kt HEAD /kt HEAD
39 156.3 0.8 160.4 0.8 164.4 0.3 167.1 0.3 169.9 0.3 172.7
___ 1~5l1§2___ 1~QL11~___ 1~5l1SQ___ 15SL1S~___ 1§lL1SS___ 1§~Ll~2
36 158.0 0.9 162.3 0.8 166.4 0.3 169.2 0.3 171.9 0.3 174.8
___ li5L12Q___ 15QL12~___ 155L161___ 15SL1S5___ 161L16~___ 165L12J
33 159.8 0.9 164.2 0.8 168.3 0.3 171.1 0.3 173.9 0.3 176.8
___ li5L121___ 15QLllQ___ 155L16~___ 15~L1SQ___ lQ~L12Q___ 16~Ll~i
30 161.5 0.9 166.1 0.8 170.3 0.3 173.1 0.3 175.9 0.3 178.8
___ liQLll~___ 151Llll___ 156L1SJ___ 15~L16§___ 16~L12Q___ 16QL1~~
27 163.2 0.9 167.9 0.8 172.1 0.3 175.0 0.3 177.8 0.3 180.8
___ ligLll~___ l~lLlll___ 156L1SJ___ 15~L1Sl___ 16JL1~1___ 1§QL125
24 164.8 1.0 169.6 0.9 173.9 0.3 176.8 0.3 179.7 0.3 182.7
___ li2L121___ 151LllS___ 15QL1Si___ lQQL1SS___ 161L12~___ 19QL12Q
21 166.3 1.0 171.3 0.9 175.7 0.3 178.6 0.3 181.5 0.3 184.5
___ li2L12i___ 1~~L122___ 1~2L1S5___ 16QL1S2___ 1§3L123___ 161L121
18 167.8 1.0 173.0 0.9 177.4 0.3 180.3 0.3 183.3 0.3 186.4
___ lilLl15___ 15~L1SQ___ 152L1S5___ lQQL162___ 16iL123___ 161L12S
15 169.2 1.1 174.6 0.9" 179.0 0.3 182.0 0.3 185.0 0.3 188.1
___ li6LllQ___ 15~L16Q___ lsSL1S6___ lQlL12Q___ 16iL12i___ 166L12S
12 170.5 1.1 175.9 0.9 180.3 0.3 183.3 0.3 186.4 0.3 189.5
___ li6Ll16___ 15JL161___ lssL1S2___ 151L121___ 155L125___ 16SL122
9 171.7 1.0 176.6 0.9 181.1 0.3 184.1 0.3 187.1 0.3 190.2
___ li2Llll___ 15iL16Z___ 152L1S6___ 15~L122___ 166L126___ 152{2QQ
6 172.8 0.9 177.3 0.9 181.8 0.3 184.8 0.3 187.8 0.3 190.9
___ li2Llll___ 15iL18J___ 16QL1S2___ 153L123___ 1§6L122___ 11QL~Ql
3 173.6 0.9 178.0 0.9 182.4 0.3 185.4 0.3 188.5 0.3 191.6
___ 15QLl16___ 15SL18i___ 16QL12Q___ 16~L12i___ 1§2L126___ 111L~Q~
o 174.2 0.9 178.6 0.9 183.1 0.3 186.1 0.3 189.1 0.3 192.2
___ 151L122___ 15§L185___ 161Ll~1___ 15iL125___ 168L122___ 111L~Q3
-3 174.7 0.9 179.1 0.9 183.6 0.3 186.6 0.3 189.7 0.3 192.8
___ 151L16Q___ 152L186___ 16,L12Z___ 165L126___ 162L~gg___ 11~L2Qi
OAT 10kt Inc 5kt Inc STILL Inc 10kt Inc 20kt Inc 30kt
C TAIL /kt TAIL /kt AIR /kt HEAD /kt HEAD /kt HEAD
39 161.0 0.8 165.0 0.8 169.0 0.3 171.7 0.3 174.3 0.3 177.0
___ 15§Ll15___ 16~L181___ 165L.86___ 16~Ll~Q___ 11~Ll~~___ 115L1~S
36 162.9 0.8 167.0 0.8 171.1 0.3 173.7 0.3 176.4 0.3 179.1
___ 1~SL!2§___ 161L162___ 166L162___ !Q~L121___ 12~L!2S___ 126L122
33 164.8 0.8 168.9 0.8 173.1 0.3 175.8 0.3 l78.5 0.3 181.2
___ ~SSL~22___ 161L162___ 166L166___ 110Ll~~___ 11JL1~6___ 116L~QQ
30 166.6 0.8 170.7 0.9 175.0 0.3 177.8 0.3 180.5 0.3 183.3
___ lS5L111___ 161L18~___ 166L162___ 110L12J___ 11JL121___ 111L~01
27 168.4 0.8 172.6 0.9 176.9 0.3 179.7 0.3 182.5 0.3 185.3
___ 155L118___ 161L18~___ 166Ll~0___ 120L12~___ 12~L~~6___ l11L~0~
24 170.1 0.9 174.4 0.9 178.7 0.3 181.6 0.3 184.4 0.3 187.3
___ 15SL11~___ 160L185___ 166L121___ 110L12S___ 11JL1~6___ 121L~Q~
21 171.8 0.9 176.1 0.9 180.5 0.3 183.4 0.3 186.2 0.3 189.1
___ 155L11~___ 160L185___ 166Ll~1___ 110L125___ 11~L!~~___ l11L~OJ
18 173.4 0.9 177.8
0.9 182.2 0.3 185.2 0.3 188.0 0.3 191.0
___ lSSL180___ 16QL186___ 166Ll~Z___ 110L126___ 11JL~QQ___ l11L~Q! ~
15 175.0 0.9 179.4 0.9 183.9 0.3 186.8 0.3 189.7 0.3 192.7
___ lS5L181___ 161L181___ 166Ll~J___ 11QL1~1___ 11~L~QQ___ l11L~Q~
12 176.3 0.9 180.7 0.9 185.2 0.3 188.2 0.3 191.1 0.3 194.1
~__ lS5L161___ 161L181___ ~66L12J___ 11QL1~1___ 12jL~Q1___ 116L~QS
9 176.9 0.9 181.4 0.9 185.9 0.3 188.9 0.3 191.8 0.3 194.8
___ lS6L16Z___ 161L16S___ 161L12j___ 111L1~8___ 125L~Q~___ lZ8LZQ6
6 177.6 0.9 IB2.0 0.9 186.5 0.3 189.5 0.3 192.4 0.3 195.0
___ 156L16J___ 16~L18~___ 166L1~S___ 11~L1~~___ 12SL~QJ___ 11~L~QZ
3 17B.2 0.9 IB2.6 0.9 187.2 0.3 190.1 0.3 193.1 0.2 195.0
___ 152L16j___ 161L1~0___ 166L126___ 11~L~QQ___ 116L~Q~___ 11~LZ02
o 17B.8 0.9 183.2 0.9 IB7.7 0.3 190.7 0.3 193.6 0.1 195.0
___ lS8L18S___ 161Ll~1___ 16~L1~1___ 11JL~Ql___ 112L~QS___ 16Q~Q6
-3 179.3 0.9 183.7 0.9 IBB.3 0.3 191.2 0.3 194.2 0.1 195.0
___ 158Lle6___ 16~L192___ !10Ll~8___ !1jL~Q~___ 11eL~Q6___ le1~g~
OAT 10kt Inc 5kt Inc STILL Inc 10kt Inc 20kt Inc 30kt
. C TAIL /kt TAIL /kt AIR /kt HEAD /kt HEAD /kt HEAD
39 162.5 0.8 166.5 0.8 170.5 0.2 172.9 0.2 175.4 0.2 177.9
___ 155l111___ 160L161___ 165L16~___ 168Ll~~___ 12aLl~S___ 12SL1~~
36 164.5 0.8 168.5 0.8 172.6 0.2 175.0 0.2 177.5 0.3 180.1
___ 155L128___ 16QL1S~ 16SL1~Q___ 162L!2j___ 12~Ll~2 !l~L~QQ ....,.
,.,j
33 166.3 0.8 170.5 0.8 174.6 0.2 177.1 0.2 179.6 0.3 182.2
___ 15~Lll~___ 160L1S5___ 166Ll~1___ ~6~L12~___ 11~Ll~8___ 116L~01
30 168.2 0.8 172.4 0.8 176.6 0.2 179.1 0.3 181.7 0.3 184.3
___ lS~L180___ 16QL186___ 165L1~1___ 16~L1~S___ 11JL1~9___ 116L~Q~
27 170.0 0.8 174.2 0.9 178.5 0.3 181.1 0.3 183.7 0.3 186.4
___ 15~L180___ 16QL186___ 165L1~2___ 16~L126___ 12JL1~~___ 111L~QJ
24 171.8 0.8 176.0 0.9 180.4 0.3 183.0 0.3 185.7 0.3 188.4
___ 15~L181___ 160L181___ 165L1~J___ 16~L121___ 113L2QO___ 122L~Oi
21 173.5 0.9 177.8 0.9 182.2 0.3 184.9 0.3 187.6 0.3 190.3
___ 15iL182___ 16QL1S8___ 16SL12~___ 16~L1~1___ 11JL~Ql___ 122L~QS
18 175.1 0.9 179.5 0.9 184.0 0.3 186.7 0.3 189.4 0.3 192.2
___ 15iL1a~___ 16QL188___ 165Ll~i___ 16~L1~8-__ 11JL20~___ 112L~QS
15 176.7 0.9 181.2 0.9 185.6 0.3 188.5 0.3 191.2 0.3 194.0
___ 15iL18J___ 160L189___ 165L195___ 169L1~2___ 11JL~0~___ 121L~06
12 178.0 0.9 182.5 0.9 187.0 0.3 189.8 0.3 192.6 0.2 195.0
___ 15iL18~___ 16QL1~Q___ 165L126___ 16~Ll~2___ 121L~0~___ 121L~Ql
9 178.7 0.9 183.1 0.9 187.6 0.3 190.4 0.3 193.1 0.2 195.0
___ 155L18S___ 161Ll~1___ 166L1~2___ 12QLaOO___ 11iL20i___ 111L~01
6 179.2 0.9 183.7 0.9 188.2 0.3 190.9 0.3 193.7 0.1 195.0
___ lS6L186___ 161L1~~___ 161L198___ 111L201-__ 115L205___ 12aL~08
3 179.8 0.9 184.3 0.9 188.7 0.3 191.4 0.3 194.2 0.1 195.0
___ 156L186___ 16~L19~___ 168L19S___ 122L~Q~___ 116L~06___ 118L2Q8
o 180.4 0.9 184.8 0.9 189.2 0.3 191.9 0.3 194.6 0.0 195.0
___ 152L181___ 161L1~3___ 168L192___ 122L~03-__ 116L206___ 129L~09
-3 180.8 0.9 185.3 0.9 189.6 0.3 192.3 0.3 195.0 0.0 195.0
___ 158L188___ 16JL1~i___ 16~L~QQ___ 12JL201___ 121L202___ 180L209
V2= VR+ 21 VR+ 21 VR+ 21 VR+ 21 VR+ 21 VR+ 21
92= 13.5 13.0 13.0 13.0 12.5 12.5
OAT 10kt Inc 5kt Inc STILL Inc 10kt Inc 20kt Inc 30kt
C TAIL /kt TAIL /~t AIR /kt HEAD /kt HBAD /kt HEAD
39 151.3 1.2 157.1 0.8 161.1 0.3 163.8 0.3 166.5 0.3 169.4
___ 1~ll1§§___ ~ll16~___ 15§L12~___ 16QL11~___ 16~LIDJ___ 166L1Dl
36 153.0 1.2 158.9 0.8 163.0 0.3 165.8 0.3 168.5 0.3 171.4
___ 1ilL166___ 1~2L61Q___ 151L116___ 1p.QL16Q___ 16JL1Si___ 1~6L!~e
33 154.7 1.2 160.6 0.9 164.9 0.3 167.7 0.3 170.5 0.3 173.4
___ li6L161___ lS~L!1!___ 151L112___ 160L161___ 16iLle5___ 161L162
30 156.3 1.2 162.3 0.9 166.7 0.3 169.6 0.3 172.4 0.3 175.4
___ l~eL16e___ 15~L12~___ !SIL!Z6___ 161L16~___ 16iL166___ 161L1~Q
27 157.9 1.2 163.9 0.9 168.5 0.3 171.4 0.3 174.3 0.3 177.3
___ 1~2L162___ 15JL11J___ lSeL!1e___ 161L16~___ 16iL166___ 16eL121
24 159.4 1.2 165.5 1.0 170.3 0.3 173.2 0.3 176.1 0.3 179.1
___ 1~2L1IQ___ 153L12~___ 156L112___ 161L161___ 165L161___ 16eL!~1
21 160.8 1.2 167.0 1.0 172.0 0.3 174.9 0.3 177.9 0.3 180.9
___ 150L111___ lSiL115___ 1~2L1eQ___ 16~Lle!___ 165L166___ 16~L!26
18 162.2 1.3 168.5 1.0 173.7 0.3 176.6 0.3 179.6 0.3 182.7
___ 150L121___ 15iL125___ 152L160___ 16~L16i___ 166L186___ 162L121
IS 163.6 1.3 169.9 1.1 175.3 0.3 178.2 0.3 181.3 0.3 184.4
___ 15QL11~___ 155L126___ 15~L161___ 161L165___ 166L162___ 162L121
12 164.9 1.3 171.2 1.1 176.6 0.3 179.6 0.3 182.6 0.3 185.7
___ lS1L11J___ 155L111___ 16QL16~___ 163L166___ 161Ll~Q___ 120L12i
9 166.1 1.3 172.5 1.0 177.3 0.3 180.3 0.3 183.4 0.3 186.5
___ 151L121___ 1~6L121___ 161L181___ 16~L162___ 161L1~1___ 121L125
6 167.2 1.3 173.6 0.9 178.0 0.3 181.0 0.3 184.1 0.3 187.2
___ 15~L12~___ 156L116___ 161L16i___ 16SL168___ 166L12~___ 11~L126
3 168.3 1.2 174.2 0.9 178.7 0.3 181.7 0.3 184.8 0.3 187.9
___ !5,L11~___ 151L112___ 16,L1SS___ 166L182___ 162L121___ 11~L1~1
o 169.4 1.1 174.9 0.9 179.3 0.3 182.3 0.3 185.4 0.3 188.6
___ 15~L12S___ 1S6L1SQ___ 16~L1S6___ 166L12Q___ 11QL12i___ 121L126
-3 170.4 1.0 175.4 0.9 179.9 0.3 182.9 0.3 186.0 0.3 189.1
___ lS~L11S___ lseL1Sl___ 16~L161___ 161L1~1___ 111L125___ 11~L12~
AIRRELD CODE
BARBADOS BGI
TORONTO yyz
WASHINGTON DULLES lAD
\J
U
=Yfl CONCORDE
AID Elev 169ft
LANDING DATA QNH BARBADOS
Maxwt Permitted (For pre flight planning) 111130kg
RUNWAY 09 21
STATUS (E)
WAT Limit: VREF 1VREf + 7kt 49°/4go
I'
~
=5
AID Elev
CONCORDE
80ft
LANDING DATA QNH LONDON
HEATHROW
Max wt Permitted (For pre flight planning) 111130kg
RUNWAY 05 09L
STATUS (L)
~ WAT Umit: VREF 1 VREF + 7kt 49°/49°
\eiJ
V
-
1,,1
~
i::'vs CONCORDE LANDING DATA QNH NEW YORK
AID Elev 13ft J.F.K.
Maxwt Permitted (For pre flightplanning) 111130kg
RUNWAY 04L 04R
STATUS (A) (l)
WAT Umit: VREF / VREF + 7kt 49°/49°
~
Landing Distance Available 3460m/11352ft 2560m/8399ft
Slope NIL NIL
Notes
Manual VREF + 7kt lOkt 6kt
Manual VREF 10kt 9kt
Autoland VREF 2kt
Manual Slippery VREF 10kt 99.1 .
Autoland Slippery VREF N/A
Fuel Saving ldg Weight VREF 10kt 2kt
Red'n perextra kt1W 3500kg
Incperkt HW 600kg
TDZElev 12ft 12ft
.~ ---------_---:...:.~-------.,;.---
GS/HtatTHR 2.86"160ft W/53ft
~.. TDZElev
GS/HtatTHR
12ft
JOI5Oft
12ft
JO/42ft
~
=ys
AID Elev 313ft
CONCORDE LANDING DATA QNH WASHINGTON
DULLES
Max wt Permitted (For pre flight planning) 111130kg
RUNWAY 01L 01R
STATUS (E) (l)
WAT limit: VREF 1 VREF + 7kt 49"/48" 49"/48"
~
landing Distance Available 3505m/1150ntt 3505m/115OlJft
Slope .16 DN .16 ON
Notes Note 1 Notes 2,3
Manual VREF + 7kt 10kt 10kt
Manual ...........•..........................................VREF 10kt 10kt
~ Autoland VREF 10kt 10kt
Manual Slippery VREF 10kt 10kt
Autoland Slippery VREF 4kt 4kt
Fuel Saving Ldg Weight VREF 10kt 10kt
Red'n per extra kt TW 35D0kg
Inc per kt HW
TDZElev 287ft 313ft
~ GS/Ht at THR ~l54ft ~155ft
IAD/02 FEB 92/03 Rev: Sim Con ILS VIS & Note(SIAPs 91-22 &23)
=s CONCORDE
AID Elev 313ft
LANDING DATA
RUNWAY 19R 30
STATUS (L)
WAT Limit: VREF 1 VREF + 7kt 49°/48° 49"/48°
Rev: Sim Con ILS VIS & Note(SIAPs 91-22 & 231 IAD/03 FEB 92103
i,;1
\wJl
~
BRITISH
CONCORDE PERFORMANCE MANUAL TAKE-oFF DATA
AlIrNAYS
MAIN ALTERNATES
'",-,
-
I..
"",~ .J
INTENTIONALLV
LEFT
BLANK
1.6.2 MAR 96/03 Section 1.6. Rev: General Revision I Page now I.l.B
=vs CONCORDE
AID 8ev 62ft
TAKE-OFF DATA ANTIGUA
FULL LENGTH RWY 07
CLG NIL RVRNIS O.25nm SLOPE O.38%DN
TOR 2743m (8999ft) EO 2743m (8999ft) TOD 2770m (9088ft)
OAT 101tt Ine 51ct lne STILL Ine 101d Ine 201d lne 301d
"C TAIL Ikt TAIL Ikt AIR Ikt HEAD lid HEAD Ikt HEAD
39 145.7 1.1 151.2 1.1 156.7 0.3 159.9 0.3 162.6 0.3 165.5
141/161 145/165 150/169 153/172 156/176 159/180
36 147.4 1.1 152.9 1.1 158.5 0.3 161.8 0.3 164.6 0.3 167.5
141/162 146/166 150/170 163/173 156/177 160/181
33 149.0 1.1 154.6 1.1 160.3 0.3 163.7 0.3 166.5 0.3 169.4
141/163 146/167 150/171 153/174 157/178 160/182
30 150.5 1.1 156.2 1.2 162.0 0.3 165.5 0.3 168.4 0.3 171.3
142/164 146/168 151/172 154/175 157/179 160/183
27 152.0 1.2 157.8 1.2 163.6 0.4 167.3 0.3 170.2 0.3 173.2
142/165 147/169 151/173 154/175 157/179 161/183
24 153.5 1.2 159.3 1.2 165.2 0.4 169.1 0.3 172.0 0.3 175.0
143/166 147/170 151/173 154/176 158/180 161/184
21 154.9 1.2 160.8 1.2 166.8 0.4 170.7 0.3 173.7 0.3 176.7
143/166 147/170 152/174 155/177 158/181 162/185
18 156.3 1.2 162.2 1.2 168.3 0.4 172.3 0.3 175.4 0.3 178.4
143/167 148/171 152/175 155/178 159/181 162/186
15 157.6 1.2 163.6 1.2 169.7 0.4 173.7 0.3 177.0 0.3 180.1
144/168 148/172 153/176 156/178 159/182 162/186
12 158.8 1.2 164.8 1.2 171.0 0.4 175.0 0.3 178.3 0.3 181.4
144/168 149/172 153/176 156/179 159/183 163/187
9 159.9 1.2 165.9 1.2 172.1 0.4 175.9 0.3 179.0 0.3 182.1
145/169 149/173 154/177 157/180 160/184 164/188
6 160.9 1.2 166.9 1.2 173.1 0.3 176.6 0.3 179.6 0.3 182.8
145/170 150/174 154/177 157/181 161/185 164/189
3 161.9 1.2 167.9 1.2 174.1 0.3 177.2 0.3 180.3 0.3 183.4
146/170 150/174 155/178 158/182 162/186 165/190
0 162.8 1.2 168.8 1.2 174.8 0.3 177.8 0.3 180.9 0.3 184.0
146/170 151/174 155/179 159/183 162/187 166/191
-3 163.6 1.2 169.7 1.1 175.3 0.3 178.3 0.3 181.4 0.3 184.5
147/171 151/175 156/179 160/183 163/187 167/192
V2= VR+ 24 VR+ 23 VR+ 22 VR+ 21 VR+ 21 VR+ 21
92= 15.0 14.5 14.0 14.0 13.5 13.5
1.V1 WET SPEED: V1 WET IS V1 DRY minus 15kt.
,-01
~
2.*TaJce.Off Minima: Where RVR/VIS is shown as0.5sm (24000) orless, higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
2.-Take-Off Minima: Where RVR/VIS is shown as O.5sm 1240001 orless, higher minima may apply if ~
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
2.*TalaHJff Minima: Where RVR/VIS is shown as0.5sm (24000) orless, higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
2.*Take-Off Minima: Where RVR/VIS is shown as 0.5sm (240Oft) orless, higher minima may apply if ~
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
I
~
2.·TaJte.Off Minima: Where RVR/VIS is shown as 0.5sm (24000) orless, higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
2.-TaJce.Off Minima: Where RVR/VIS is shown asO.5sm 12400ftl orless, higher minima may apply if ~
any radio orvisual aids are unselViceable. See para 1.1.5 on Page 1.1.3.
'Xc•.... ' 2.*Tate-OffMinima: Where RVR/VIS is shown as0.5sm 1240001 orless, higher minima may apply if
-- any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
2.·Take-Off Minima: Where RVRMS is shown as 0.5sm (240001 orless, higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
2. eTu.otf Minima: Where RVR,IVIS is shown asO.5sm (240OftI orless, higher minima may apply if ~
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
2.*TakHlff Minima: Where RVR/VIS is shown as 0.5sm (240001 orless, higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
21 167.2 0.8 171.2 0.8 175.4 0.3 178.2 0.3 180.8 0.3 183.4 ~
152/176 157/182 163/189 166/193 169/197 173/202
18 168.8 0.8 172.9 0.9 177.2 0.3 180.0 0.3 182.7 0.3 185.3
153/177 158/183 163/189 166/193 170/198 173/202
15 170.4 0.8 174.5 0.9 178.8 0.3 181.7 0.3 184.4 0.3 187.1
153/178 158/184 163/190 167/194 170/198 174/203
12 171.7 0.8 175.8 0.9 180.1 0.3 183.0 0.3 185.8 0.3 188.5
154/178 159/184 164/190 167/195 171/199 174/203
9 172.2 0.8 176.4 0.9 180.7 0.3 183.5 0.3 186.2 0.3 188.8
154/179 159/185 165/192 168/196 172/200 175/205
6 172.7 0.8 176.9 0.9 181.2 0.3 183.9 0.3 186.5 0.3 189.3
155/181 160/187 165/193 169/197 173/202 176/204
3 173.2 0.8 177.4 0.8 181.6 0.3 184.2 0.3 186.8 0.3 189.6
156/182 161/188 166/194 170/198 174/203 177/205
0 173.7 0.8 177.9 0.8 182.0 0.2 184.5 0.3 187.2 0.3 189.9
157/183 162/189 167/195 1711199 174/202 178/205
·3 174.1 0.8 178.3 0.8 182.3 0.2 184.8 0.3 187.5 0.3 190.2
157/184 163/190 168/196 1721200 175/203 179/206
V2= VR+ 22 VR+ 22 VR+ 22 VR+ 22 VR+ 22 VR+ 22
82= 14.0 14.0 13.5 13.5 13.5 13.0
1.VI WET SPEED: VI WET IS Vl ORY rnmus 15kt.
2. *Tu.Gff Minima: Where RVR/VIS is shown asO.5sm 1240(0) orless, higher minima may apply if ~
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
2.-Take-Off Minima: Where RVR/VIS is shown as0.5sm (24000) orless, higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
2. ·TaJce.Off Minima: Where RVRMS is shown asO.5sm (240Oftl orless, higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
2.·TaktHJffMinima: Where RVR/VIS is shown as0.5sm (24000) orless, higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5. on page 1.1.3.
2.·Tak~ Minima: Where RVR/VIS is shown as0.5sm (240Oft) orless, higher minima may apply if ~
any radio orvisual aids are unserviceable. See para 1.1.5. onpage 1.1.3.
2.-Take-Off Minima: Where IMWIS isshown as O.Ssm (24000) orless, higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5. on page 1.1.3.
2.*Tafr8.Off Minima: Where RVRMS is shown asO.5sm 1240Oft) orless, higher minima may apply jf ~
any radio orvisual aids are unserviceable. See para 1.1.5. on page 1.1.3.
INTENTIONALLY
LEFT
BLANK
1.7.2 MAR 96/03 Sec:tion 1.7. Rev: General Revision I Page now 11.8
=vs CONCORDE
AID Elev 62ft
LANDING DATA QNH ANTIGUA
Max wt Permitted (For pre flight planningl 111130kg
RUNWAY 07 25
STATUS
WAT Umit: VREF 1VREF + 7kt 49"/49° 49"/49"
Landing Distance Available 2543m 18344ft 2743m 19000ft
Slope .38 ON .38 UP
Notes Notes 1,2 Note 2
Manual VREF + 7kt 5kt 6kt
Manual VREF Bkt 10kt
Autoland VREF
Manual S6ppery VREF 96.2 100.2
Autoland S6ppery VREF
Fuel Saving Ldg Weight VREF
Red'n per extra kt TW 3500kg 3500kg
Incperkt HW 600kg 600kg
TOZSev 62ft 20ft
GS/HtatTHR
APPROACH DA DH/(HAT) RYR DA DH/(HAT) RYR
(ftl (It) (ft) (ft)
VOROME . 730 (66BI 2nm 710 (6901 2nm
VOR .. 1050 (98BI 2.75nm 750 (7301 2nm
NOBOME .. 590 (570) 1.5nm
NOB .. 590 (570) 1.75nm
NOB(BCP) .. 1050 (988) 2.75nm 1050 (988) 2.75nm
Circling 1Visual (radius 5.3nm) .. 1050 (988) 2.75nm 1050 (988) 2.75nm
RM DIRECTION
APPROACH WAY PT (15nm) NI6"59~ N17'1~1
W 062° 01.0 W 061" 33.8
TOUCHDOWN WAY PT N17°07.9 N17°0B.7
W 061 °48.0 W 061" 46.B
1. Landing Rwy07: DD NOT make 1BO° tum at Rwy intersection, proceed to 1lJming circle at Rwy end.
2. Circling 1VISUal & BCP: All circuits SOUTH of Rwy 07/25 only.
(~
LEFT
BLANK
I
~
BRmSH
AIrNIAYS CONCORDE LANDING DATA QNH BALTIMORE
AID Elev 146ft
Max wt Permitted IFor pre flight planning) 111130kg
RUNWAY 10 15R
STATUS (L) (A)
"- WAT Limit: VREF / VREF + 7kt
Landing Distance Available
49"/49· 49°/49°
3033m / 9951ft 2901m/9519ft
Slope .12 ON .110N
Notes Note 1 Note 2
ManuaL................................ VREF + 7kt 10kt 10kt
Manual.............................................VREF 10kt 10kt
Autoland ..........................................VREF 10kt
Manual Stippery...............................VREF lkt Okt
Autoland S6ppery ............................VREF 101.0
Fuel Saving Ldg Weight...................VREF
Red'n per extra ktTW 3500kg 3500kg
Incper kt HW 600](g
TOZElev 144ft 140ft
GS/HtatTHR 3·/56ft 3°/59ft
APPROACH DA DHIlHAT) RVR DA DH/(HAT) RYR
(ft) 1ft) (ft) (ft)
ILS C2 ........................................Autoland 115R 12000
ILS ClR....................................... Coupled 200R 18000 200R 2400ft
ILSC1 ...................................................... 350 (206) 18000 340 (200) 2400ft
ILSH No Flt/Dir......................................... 450 (306) 22000 440 (300) 2400ft
lLZ ........................................................... 550 (406) 50000 USE CIRCUNG MINIMA
VOROME ................................................. 670 (526) 5000ft
VOR.......................................................... 1270 (1126) 2.5sm
VOR DME-A(BCP) .................................... 1250 (1104) 3sm 1250 (1104) 3sm
Circling / Visuallradius 5.3nm)................ 1250 (1104) 3sm 1250 (1104) 3sm
RWY DIRECTION 094°T 144·T
APPROACH WAY PT(15nm) N39·' 1.5 N39°23.2
wOn·00.5 W 076·52.3
TOUCHDOWN WAY PT N39° 10.5 N39°11.1
~ W076°41.2 W076°40.9
t. lLZ 10: lLZ unusable above 360Oft. If MMinop increase Vis by0.25sm.
BWI/02 MAR 96/06 Section 1.7. Rev: Rwy 33L ILS/ILSH/LLZ RVRs Revised
EIRmSH
AlFtNAYS CONCORDE LANDING DATA QNH BIRMINGHAM
AID Elev 325ft
Max wt Permitted (For pre flight planning) tt1130kg
RUNWAY 15 33
STATUS (A) (A)
WAT LimitVREF / VREF + 7kt 48"/48" 48"/48"
landing Distance Available 2279m /7477ft 23D4m /7559ft
Slope .25 UP .25 ON
Notes Notes 1,2 Notes 1,3
Manual..................................VREF + 7kt 105.0 107.0
Manual.............................................VREF lkt tkt
Autoland ..........................................VREF
"'-' Manual Sfippery...............................VREF NlA N/A
Autoland Slippery ............................VREF
Fuel Saving ldg Weight...................VREF
Red'n per extra kt TW 3500kg 3500kg
IncperktHW 600kg 600kg
TDZElev 303ft 325ft
GS/HtatTHR 3j55ft 3j54ft
APPROACH DA DH/(HAT} RVR DA DH/(HAT} RVR
(ft) (ft) (ft) (ft)
ILS ClR....................................... Coupled
210R 550m 200R 550m
ILSC1 ......................................................
(207) 550m 510 530 12051 550m
ILSH NoFlt/Dir .........................................
(307) 700m 610 630 13051 700m
LU...........................................................
(467) tOOOm no anD 14751 1DOOm
NDBoME.................................................
830 (527) 1100m 850 15251 1100m
SRAlterm 2nm).......................................
870 (5671 t200m 850 (525) 1100m
I
Circling/Visuallradius 5.3nm)................
1350 110251 BOOm 1350 (1025) 800m
~
RWY DIRECTION 146"T 326"T
APPROACH WAY PT1'5nm) N52"40.2 N52"14.5
WOOt"59.3 W 001 "30.7
TOUCHDOWN WAY PT N52"27.8 N52"26.9
W001"45.5 W 001 "44.4
l 1. ILSCl & C1R Rwys 15/33: IfTOZ orRCL inop RVR becomes 600m.
~
2. NOB DME Rwy15:Final approach track offset by 5' and intercepts RCl0.5nm before THR.
3.NOB DME Rwy 33: Final approach track offset by6"and intercepts RCL 0.5nm before THR.
LEFT
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~
BIlmSH
AIIWAYS CONCORDE LANDING DATA QNH FORT DE FRANCE
AID Elev 16ft
Max wt Permitted (For pre flight planning) 111130kg
RUNWAY 09 27
STATUS (B)
WAT limit: VREF 1VREF + 7kt 49"/49° 49"/49 °
landing Distance Available 3300m /1 0827ft 3000m /9842ft
Slope .05 UP .06DN
Notes Note 1 Note 1
ManuaL•..........•............•.....•.VREF + 7kt 10kt 10kt
Manual.............................................VREF 10kt 10kt
Autoland ..........................................VREF
Manual Slippery...............................VREF 9kt 2kt
Autoland Slippery ............................VREF
Fuel Saving ldg Weight...................VREF
Red'n per extra ktTW 3500kg 3500kg
Ine perkt HW
TDZElev 10ft 13ft
GS/Htat THR 3°/52ft
APPROACH DA DH/(HAT) RVR DA DH/(HAT) RVR
(ft) 1ft) (ft) (ft)
IlS C1 ...................................................... 380 (370) 1350m
IlSHNo FItIDir ......................................... 380 (370) 1350m
~ lLZ........................................................... 740 (730) 3.3km
VOR DME ................................................. 470 (460) 2.2km 1420 (14071 3.5km
VOR.......................................................... 680 (670) 3.1km
NOB ......................................................... 940 19301 3.5km
Circling 1Visuallradius 5.3nml................ 1700 (1684) 3.5km 1700 116841 3.5km
0T 0T
RWY DIRECTION 080 260
APPROACH WAY PT(15nm) N14°32.6 N14°38.1
W 061°16.6 W060044.3
TOUCHDOWN WAY PT N14°35.2 N 14·35.5
W061°01.3 W060059.6
1. CirclinlVV"lSuBI: Approved Day only.
~..
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:::s CONCORDE LANDING DATA QNH GLASGOW
AID Elev 26ft
Max wt Permitted 1For pre flight planning) 111130kg
RUNWAY 05 23
STATUS (E) (E)
WAT Umit: VREF /VREF + 7kt 49,49° 49°/49°
Landing Distance Available 2658m /872Oft 2353m /772Oft
Slope .09 ON .09 UP
Notes Note 1,2 Note 1,2
Manual. VREF + 7kt 8kt Okt
Manual VREF 10kt 4kt
Autoland VREF 5kt 108.8
Manual Sfippery VREF 102.7 N/A
Autoland Slippery VREF N/A N/A
Fuel Saving Ldg Weight. VREF
Red'n per extrakt TW 3S00kg 3500kg
IncperktHW 600kg 600kg
TDZElev 26ft 20ft
GS/Htat THR 3/52ft 3°/SOft
APPROACH DA DH/(HAT) RYR DA DH/(HAT) RYR
1ft) 1ft) (ft) 1ft)
ILS ClR Coupled 210R S50m 210R 5S0m
ILS Cl . 230 1204) S50m 220 (200) 5S0m
ILSH No At/Dir .. 330 1304) 650m 320 (300) 650m
llZoME .. 480 1454) 900m S10 14901 l000m
VOR OME . 530 IS04) 1000m S10 14901 1000m
NOB OME . 7S0 (730) 1500m
NOB . 980 (954) lS00m
SRA (term 2nm) . 1120 11094) lSCOm 720 (700) 1400m
Circling / Visual (radius S.3nm) .. 17S0 11724) 800m 17S0 11724) 800m
RWY DIRECTION 046°T 226°T
APPROACH WAY PT (15nm) N5S041.4 N56°03.1
W 004° 46.0 W 004° 05.9
TOUCHDOWN WAY PT N5SoS1.8 N 55°52.7
W 004° 26.9 W 004° 25.2
1. Noise Restrictions: Oue to noise restrictions, theminimum Altitude forjoining Visual Final Approach
should be1530ft QNH to intercept a 3degree glideslope.
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=~ CONCORDE LANDING DATA QNH LONDON
AID Elev 202ft GAlWlCK
Max wt Permitted IFor pre flight planning) 111130kg
RUNWAY 08l 08R
STATUS (L)
WAT Umit: VREF /VREF + 7kt 49°/49° 49°/49°
Landing Distance Available 2243m /73600 2766m /9075ft
Slope .05DN .07 ON
Notes Note 2 Note 1,3
Manual VREF + 7kt 103.9 10kt
Manual VREF Okt 10kt
Autoland VREF 7kt
Manual Slippery VREF N/A 106.4
Autoland Slippery VREF N/A
Fuel Saving Ldg Weight... VREF
Red'n per extra Id1W 3500kg 3500kg
Incper kt HW 600kg 600kg
TDZElev 195ft 195ft
GS/HtatTHR 3°/53ft
APPROACH DA DH/IHAl) RYR DA DH/(HAl) RVR
Iftl (ft) (ftl (ftl
ILS C3A Autoland 15R 200m
ILS C2 Autoland 100R 400m
ILS C1R Coupled 200R 550m
ILSC1 .. 400 (205) 550m
ILSH No FlVDir .. 500 (305) 650m
LLZ .. SOD (605) 1200m
SRA (term 2nm) .. 900 (705) 1500m no (575) 1200m
Circling / Visual (radius 5.3nm) .. 1150 (94S) 1500m 1150 (94S) BOOm
RWY DIRECTION 078°T 07SoT
APPROACH WAY PT (15nm) N51·05.6 N51°05.5
WOOO·35.S WOOO·35.7
TOUCHDOWN WAY PT N51·0S.S N 51·08.7
W 000°12.4 W 000°12.3
1. ILS C3A Rwy OBR: Minimum Mid-point .. RVR 150m, Stop-end RVR .. Advisory only.
2. Rwy 08lJ26R: Is promulgated asanemergency runway and willonly be used when the main runway
is closed.
2. RwyOBL/2&R: Ispromulgated asanemergency runway and willonly beused when themain runway
is closed.
LEFT
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=~ CONCORDE lANDING DATA QNH MANCHESTER
AID Elev 256ft
Max wt Permitted (For pre flight planning) 111130kg
RUNWAY 06 24
STATUS (E) (L)
WAT Umit VREF 1VREF + 7kt 49;49· 49·/49·
Landing Distance Available 2621 mIS599ft 2865m 194000
Slope .49 UP .49 DN
Notes Note 2 Note 1,2
ManuaL VREF + 7kt 9kt 101ct
Manual VREF 10kt 101ct
Autoland VREF 3kt 7kt
Manual Slippery VREF 104.0 107.7
Autoland Slippery VREF N/A N/A
Fuel SaVing Ldg Weight.. VREF
Red'n per extra let TW 3500kg 3500kg
Incper kt HW 600kg 600kg
TDZ Bev 211ft 250ft
GSlHt at THR 3·/57ft 3·/55ft
APPROACH DA DH/(HAT) RVR DA DH/(HAT) RVR
(ft) (ft) (ft) (ft)
ILS C3A Autoland 15R 200m
ILS C2 Autoland 100R 400m
ILS C1R Coupled 200R 550m
ILS Cl......................................................
420 (209) 550m 450 (201) 550m
ILSH No FtVDir 520 (309) 650m 550 (301) 650m
LLZ OME...................................................
620 (409) 900m 620 (371) SOOm
VOR OME.................................................
680 1469) 1000m 680 14311 900m
NOB OME.................................................
680 1469) 1DOOm 680 (4311 900m
Circling/Visuallradius 5.3nm)................
1300 (1044) 800m 1300 (1044) 800m
RWY DIRECTION 051°T 231·T
APPROACH WAY PT115nm) N53·11.3 N53·31.0
W 002·36.7 WOOl·56.0
TOUCHDOWN WAY PT N53·20.8 N53·21.6
W 002·17.2 W 002·15.6
1. ILS C3A Rwy24: Minimum Mid·point.· RVR 150m, Stop·end RVR·· Advisory only.
2. ILSCl & ClR Rwy06/24: If TOZ orRCL inop RVR becomes 600m.
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BRmSH
AJlfWAYS CONCORDE LANDING DATA QNH MONTREAL
AID Elev 270ft MIRABEL
Max wt Permitted (For pre flight planning) 11113Dkg
RUNWAY 06 11
STATUS (E) (L)
"-' WAT Umit VREF / VREF + 71et
landing Distance Available
49°/48"
3658m / 120000
49°/48°
3658m / 12DDOft
Slope .14 ON .18 UP
Notes
ManuaL............................... VREF + 71et 1Diet 1Diet
Manual.............................................VREF 1Diet lDkt
Autoland ..........................................VREF 1Diet 1Diet
Manual Slippery...............................VREF 1Diet 1Diet
Autoland Stippery ............................VREF 71et lOIet
Fuel8aving Ldg Weight...................VREF
Red'n per extra let TW 3500kg
IncperletHW
TDZ8ev 256ft 247ft
~ GS/HtatTHR 3"/52ft 3"l56ft
APPROACH DA DH/(HA1) RVR DA DH/(HA1) RVR
(ft) (ft) (ft) (ft)
ILSCl ...................................................... 460 (204) 26000 450 1203) 26000
I ILSH No FlVDir ......................................... 560 (304) 26000 550 (3031 26000
""'-" LU........................................................... 690 1434) SOOllft 730 (483) 1.25sm
NOB ......................................................... 890 1634) 1.25sm 930 1683) 1.5sm
Circling / Visuallradius 5.3nm)................ 1100 (830) 2sm 1100 (830) 2sm
RWY DIRECTION 045°T 09SoT
APPROACH WAY PT115nml N4S029.6 N45°42.3
W 074° 16.4 W074"26.6
TOUCHDOWN WAY PT N45°40.2 N4S040.2
W 074°01.3 W 074° 05.3
~
"
2. ILSaid"tep to Rwy04R: Based on anILS Rwy O4L approach with a side-step manoeuvre to land on
Rwy04R.
RUNWAY 09 27
STATUS (E)
WAT limit VHEF / VHEF + 7rr 48°/48° 48°/48°
Landing Distance Available 2995m /9826ft 2995m /9826ft
Slope .20 ON .20 UP
Notes
ManuaL VHEF + 7kt 10kt 10kt
ManuaL VHEF 10kt 10kt
~ Autoland VHEF 10kt
Manual Slippery VHEF lkt 2kt
Autoland Slippery VHEF 96.0
Fuel Saving ldg Weight VREF
Red'n per extra kt TW 3500kg 3500kg
IncperktHW 600kg
TDZElev 482ft 468ft
GS/HtatTHR 3i62ft
APPROACH DA DH(HAll RVR DA DHIHAll RVR
(ft) (ft) (ft) (ft)
ILSC1 . 690 12081 18000
ILSH NoRt/Dir .. 790 13081 22000
lLZ . 970 14881 50000
VOR OME . 990 15221 1.5sm
VOR .. 1270 18021 2.5sm
NOB .. 1150 16681 1.75sm
Circling / Visuallradius 5.3nm) . 1300 1809) 2.5sm 1300 (809) 2.5sm
RWY DIRECTION 079"r 259"
APPROACH WAYPT(15nm) N41 "27.2 N41 "33.2
W074"27.0 W073°46.1
TOUCHDOWN WAY PT N41 "30.1 N41 "30.4
W074"07.4 W074"05.8
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:vs CONCORDE LANDING DATA QNH PHILADELPHIA
AID Elev 21ft
Max wt Permitted (For pre flight planningl 111130kg
RUNWAY 09L 09R
STATUS (A) (l)
WAT Umit VREF /VREF + 7kt 49·/49· 49·/49·
Landing Distance Available 2896m /95000 3200m /1 05000
Slope .03 ON .11 ON
Notes Note 1
Manua!. VREF + 7kt 10kt 10kt
Manual VREF 10kt 10kt
Autoland VREF 10kt
Manual Snppery VREF Okt 6kt
Autoland Slippery VREF 110.1
Fuel Saving Ldg Weight VREF
Red'n per extraktTW 3500ltg 3500kg
Incper kt HW 600kg
TOZElev 14ft 21ft
GS/HtatTHR 3·/57ft 3°/56ft
APPROACH OA OH/(HAT) RVR DA OH/(HAT) RVR
1ft) 1ft) 1ft) 1ft)
Its C2 Autoland 110R 12000
Its Cl .. 220 (2061 2400ft 230 (209) 18000
ItsH NoFlVDir .. 320 13061 28000 330 13091 22000
Converging Its .. 730 (7091 2.5sm
Its Side-step .. 730 (716) 2sm
lLZILandi Fix) . 490 (4761 O.75sm
lLZIBaldn Fix) . 570 (549) 50000
LLZ .. 730 (716) 1.5sm 730 (709) 1.5sm
SRA. . 530 15161 1.5sm 570 (549) 50000
Circting / Visual (radius 5.3nm) .. 850 (829) 2.Ssm 850 (829) 2.5sm
RWY DlRECnON 075°T 075·T
APPROACH WAY PT 115nm) N39·48.2 N39·47.8
W 075·34.2 W 075·35.3
TOUCHDOWN WAY PT N39· 52.1 N39· 51.7
W.075°1S.3 W 07S· 16.4
1. Sidestep to 09L: Based on an Its Rwy 09R approach with a side-step manoeuvre to land onRwy 09L.
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=ys CONCORDE
AID Elev 57ft
LANDING DATA QNH PORT OF SPAIN
Max wt Permitted (For pre flight planning) 111130kg
RUNWAY 10 28
STATUS (B)
WAT Limit: VREF IVREF + 7kt 49°/49" 49°/49°
Landing Distance Available 3200m / 105000 3200m /1 05000
Slope .24 UP .24 ON
Notes
ManuaL VREF + 7kt 10kt 10kt
Manual VREF 10kt 10kt
~ Autoland VREF
Manual Stippery VREF 8kt 5kt
Autoland Slippery VREF
Fuel Saving Ldg Weight... VREF
Red'n per extra kt TW 3500kg 3500kg
Incper kt HW
, TOZSev 32ft 57ft
~ GS/Ht at THR 3j49ft
APPROACH OA OH/(HAT) RVR OA OH/(HAT) RVR
fit) (ft) (ft) (ft)
ILS Cl . 290 (258) lnm
ILSH No FWDir . 390 (358) lnm
LLZ . 610 (578) 1.5nm
NDB .. 610 (578) 1.5nm
Circfing / Visual (radius 5nm) . 1050 (993) 3nm 1050 (993) 3nm
0T 0T
RWY DIRECTION 090 270
APPROACH WAY PT (t5nm) N10'35.6 N10°35.6
W061°36.5 W061·04.2
TOUCHDOWN WAY PT N10°35.6 N10°35.6
W061°21.2 W06t·19.5
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BIlIT1liH
AIRWAYS CONCORDE LANDING DATA ONH ST. LUCIA
AID Elev 11ft
Max wt Permitted (For pre flight planning) 111130kg
RUNWAY 10 28
STATUS
WAT Umit: VREF / VREF + 7kt 49°/49° 49"/49°
Landing Distance Available 2743m /90000 2743m /90000
Slope NIL NIL
Notes Note 1 Note 1
Manual..................................VREF + 7kt 10kt 10kt
Manual.............................................VREF 10kt 10kt
"'-' Autoland ..........................................VREF
Manual S6ppery...............................VREF 106.6 106.6
Autoland Sfippery ............................VREF
Fuel saving Ldg Weight...................VREF
Red'n per extra kt1W 3500kg 3500kg
Incper kt HW 600kg 600kg
TDZSev 9ft 9ft
~ GS/Htat1HR
APPROACH DA DH/IHAT) RVR DA DH/(HAT) RYR
(ft) 1ft) (ft) (ft)
VOR DME................................................. 780 (771) 3.6km 820 (811) 4km
VOR .......................................................... 830 (821) 4km 820 (811) 4km
NOB ......................................................... 840 (831) 4km 940 (931) 4.8km
Circling / Visual (radius 5.3nml................ 1200 (1189) 4.8km 1200 (1198) 4.8km
RWY DIRECTION 089°T 269"1
APPROACH WAY PT115nm) N 13°43.6 N13°44.2
W 061"13.3 W 060" 41.0
TOUCHDOWN WAY PT N13°43.9 N13°43.9
W 060·57.9 W060056.4
1. Circling and visual minima: SOUTH of Rwy 10/28 only.
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J
~
:=~ CONCORDE LANDING DATA QNH WINDSOR LOCKS
AID Elev 174ft
Max wt Permitted IFor pre flight planning) 111130kg
RUNWAY 06 15
STATUS (E)
WAT Limit: VREF / VREF + 7kt 49°/49° 49°/49°
Landing Distance Available 2896m /95000 2087m /6847ft
Slope .12 ON .02 UP
Notes
ManuaL VREF + 7kt 10kt 92.0
Manual VREF 1Dirt 102.8
Autoland VREF 10kt
Manual Slippery VREF Okt N/A
Autoland Slippery VREF 99.0
Fuel saving Ldg Weigl1t VREF
Red'n per extra kt TW 3500kg 3500kg
IncperktHW 600kg 600kg
TOZElev 174ft 172ft
GS/HtatTHR 3"1500
APPROACH DA DH/IHAT) RYR DA DH/(HAT) RVR
1ft) (ft) 1ft) (ft)
ILS Cl . 380 (206) 1800ft
ILSH No Flt/Dir .. 480 (306) 2200ft
LLl .. 870 1696) 1.5sm
VORDME . 910 1736) 1.75sm
VOR . 1130 (958) 3sm
NOB . 950 17761 2sm
Circling/Visuallradius 5.3nm) .. 1100 (926) 3sm 1100 1926) 3sm
RWlDIRECTION 044°T 134"1"
APPROACH WAY PT115nm) N41°45.1 N42"06.9
W072·55.8 W 072"56.1
TOUCHDOWN WAY PT N41°55.9 N41 "56.5
041.8
W 072 W 072°41.6
Rev: ILS Rwy 06RVR reduced Section 1.7. BOl/Ot MAR 96/07
::':s CONCORDE lANDING DATA QNH WINDSOR LOCKS
AID Elev 174ft
Maxwt Permitted (For pre flight planning) 111130kg
RUNWAY 24 33
STATUS (A) (8)
WAr Limit: VREF/VREF + 7kt 49;49" 49;49" -1
~
Landing Distance Available 2896m /950Oft 2087m /6847ft
Slope .12 UP .02DN
Notes Notes 1,2
Manual VREF + 7kt 10kt 91.8
Manual VREF 10kt 102.6
Autoland VREF
Manual Slippery VREF Okt N/A
Autoland Slippery VREF
Fuel Saving Ldg Weight.. VREF
Red'n per extra kt TW 3500kg 3500kg
IncperktHW 600kg
TDZElev 170ft 172ft
GS/HtatTHR 3;59ft 3°/59ft
APPROACH DA DH/IHAT) RYR DA DH/(HAT) RYR
1ft) 1ft) Iftl 1ft)
ILS Cl . 370 1200) 2400ft 380 (208) 0.75sm
ILSH No FltlDir . 470 1300) 2400ft 480 (308) 0.75sm
LLZ .. 570 1400) 5000ft 550 (378) lsm
VOR . 610 14401 5000ft 550 (3781 lsm
Circling/Visual (radius 5.3nm) .. 1100 1926) 3sm 1100 (926) 3sm
RWY DIRECTION 224"r 314 "T
APPROACH WAY PT 115nm) N42°07.8 N41°45.4
W072"26.3 W 072°26.1
TOUCHDOWN WAY PT N41"57.0 N41°55.8
W072°40.3 WOn040.6
1. LLZ 24: If ALS inop increase VIS by 0.25sm.
-
:)
~
CONCORDE PERFORMANCE MANUAL DISPATCH DEVIATIONS
SPECIAL OPERATIONS
The table below lists the combinations of dispatch deviations/special operations which are NOT
PERMITIEO. Where certain combinations arepermitted the penalties for each case must beadded
together to calculate the overall penalty.
12. Carriage of wide cut IJP4) type fuel 1.5, ID, 11, 13,14,16,11
13. Take-off from contaminated runways 7, 12,15,16
Due to the increased landing speeds. it is recommended that where a slippery runway
condition could occur on landing use 01 this procedure is restricted to cases where the
stopping distances are clearly non-critical.
B. RIGHT PLANNING
1. No penalties required.
C. TAKE-Off
1. No penalties required.
D. lANDING
1. Use VREf+ 7 landing data only. Reduced Noise Approach is NOT approved.
2. Tha landing distance required is increased by 4%. Reduce the actual landing distance
available by 4% using the table below. Use this Effective landing Distance to enter the " ,.J
appropriate Generalised Landing Distance chart to obtain a runway limited landing ~
weight.
1.In the event of the landing gearfailing to retractthe aircraftshould return to the departure
airfield. The reduction in climb gradient dueto dragandlow airspeed in combination with
an engine failure will reduce net level off altitude to low levels. Refer to the net ceiling
chart for this configuration in this section.
B. TAKE-OFF
(1000kg)
Rev:
CONCORDE PERFORMANCE MANUAL DISPATCH
DEVIATIONS
29-1 DISPATCH WITH ONE GREEN SYSTEM HYDRAUUC PUMP INOPERATIVE (cont)
C. LANDING
1.For Y. landings the landing WAT limited weight must be reduced by 2% using the lable
below.
2. For VIlEf + 7 lendings the lending WAT limited weight must be reduced by 3% using the
table below.
32-6 DISPATCH WITH ONE WHEEL BRAKE (OR ANTI·SKID CHANNEL) INOPERATIVE
~, A. UMlTATlONS
1. Dispatch with one wheel brake (or anti-skid channel) inoperative in combination with a
secondary noule locked withintherange 10" to 21° is aUlhorised provided theinoperative
brake lor anti-skid unit) and nozzle are not on the same side of the aircraft.
B. RIGHT PlANNING
1. No penallies required.
C. TAKE·OFF
1. The PLTOW must be raduced by 1.75% using the table below.
32-6 DISPATCH WITH ONE WHEEL BRAKE (OR ANTI-SKID CHANNEl) INOPERAnVE
(cont)
D. The landing distance required is increased by 5%. Reduce the actual landing distance
available by 5% using the table below. Use this Eftective Landing Distence to enter the
eppropriete Generalised landing Distance chart to obtain a runway limited landing weight.
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11-4 DISPATCH WITH ONE OR MORE SECONDARY AIR DOOR SVmMS FAILED SHUT
A. UMITAnONS
B. FLIGHT PLANNING
1. No penalties required.
C. TAKE·OFf
1. The PLTOW must be reduced by 0.330/0 for each system selected shutlup to a maximum
reduction of 0.99%) using the table below.
1. No penalties required.
1. Only one flight with system failed on is permitted before the fault is rectified.
B. RIGHT PLANNING
1. The flight plan fuel must be increased by the amount given in the table below.
EXTRA FUel(kgl
C. TAKE·OFF
1. At ambient temperatures of +3"C and above the PLTOW must be reduced by 0.5% for
each engine anti-icing systems continuously operating (up to a maximum penalty of
1.5%1. At temperatures below 3"C no penalties are required.
PLTDW 140 150 \60 170 180 \90
(1000kgl
PENAlTY 0.7 0.8 0.8 0.9 0.9 1.0
(1000kgl
D. lANDING
1. At ambient temperatures of +3"C and above the landing WAT limited weight must be
reduced by 1% for each engine anti·icing system continuously operating (up to a
maximum of 2%1 using the table below.
A. UMITAnONS
B. TAKE-OFF
1. The PLTOW must be reduced by 5% for ona or more engines without contingency power
using the table below. ~
C. LANDING
1. The landing WAT limited weight must be reduced by 6% for oneor more engines without
contingency power using the table below.
~ A. UMITAnONS
1.Clearance for dispatch in this condition is limited to those ceses where only one engine is
affected. For that engine the TIO monitor caption, fuel f1owrate. P7 and Nz instruments
must be serviceable.
B. FUGHT PLANNING
1. No penalties required.
C. TAKE·OFF
1. The PLTOW must be reduced by 0.5% using the table below.
2.The P7 and Frtake-off bug settings must bereduced bytheamount shown onpage 1.5.10.
D. lANDING
1. The landing WAT limited weight must be reduced by 1% using the table below.
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78·1 DISPATCH WITH ONE SECONDARY NOULE LOCKED WITHIN RANGE 10" to 27°
A. UMITAnONS
1. Dispatch with one wheel breke (or enti-skid channel) inoperative in combination with a
secondary noule locked withinthe range 10"to 27' is authorised provided theinoperative
brake (or anti-skid unitI end noule are not on the same side of the aircraft.
B. FUGHT PlANNING
1. The flight plan fuel must be increased by the amount given in the "ONE SECONDARY
NOZZLE LOCKED BETWEEN 10" AND 2.".' chart in this section.
Z. The value of the supersonic portion of the trip for some current sectors is given in the
table below.
SECTOR SUPERSONIC
PORTION OF TRIP
LHR-JFK 85%
JFK-LHR 85%
"
, ,,·tHFHAll ." •.• ,<~ •.•.•.
, IAO-lHR ...'»88%
IAo-MiA
MIA-IAD
C. TAKE-Off
• ".4.5'." .4.8'
D. LANDING
1. The lending WAT limiled weight musl be reduced by 4% using the table below.
18-1 DISPATCH WITH ONE SECONOARY NOZZLE LOCKED WITHIN RANGE 10" to 21°
(contt
D. LANDING (contl
Z. The lending distance required is increased bV 1.5%. Reduce the acluallanding distance
available by 7.5% using the table below. Use this Effective Landing Distence to enterthe
appropriate Generalised landing Distance chart to obtain a runway limited landing
weight.
._. I
1,
, . ... "'1".-, •. ~.
t l::rt!-
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+ -.- .. . :1 .. .:
Rev. 1.8.13. DEC 90102
8RmaH
AIRWAYS CONCORDE PERFORMANCE MANUAL DISPATCH
DEVIATIONS
A. UMrTATlONS
1. If the take-off is to be carried out from a slippery runway the inoperative reheat must be
on engine 1 or 2 (due to the reduced thrust from engine 4 during the early part of the
take-off roll.
B. FUGHT PLANNING
1. For supersonic sectors the flight planfuel must be increased by the amount given in the V
table below.
+20
+10
C. TAKE·OFF
D. LANDING
1. The landing WAT limited weight must be reduced by 14% using the table below.
A. UMITATIONS
1. If two reheats are inoperative theymust notbe on the same side of the
aircraft.
B. FUGHT PLANNING
1. For supersonic sectors the flightplanfuel must be Increased by the amount
given in the tablebelow.
C. TAKE-OFF
~ 1. The PLTOW mustbe reduced by 14% using the tablebelow.
D. LANDING
SPECIAL OPERATIONS
A. INTRODUCTION
Landings at weights above the maximum structural weight of t11,130kg are pennitted for
fuel saving reasons provided thatthe limitations and procedures given in the Flying Manual
Vol 2 Section 4 are followed and the performance effects given below are applied.
B. UMITAnONS
Observe the following:
C. LANDING
Or
1. Enter the appropriate Generalised Landing Distance Chart with Landing Distance
Available. Correct for wind, slope and airfield pressure altitude to obtain a Runway ~
Umited Landing Weight
2. Enter the appropriate Maximum Landing Weight (WAT Umitl Chart withthe landing
ambient temperature and correct for airfield pressure altitude to obtain a WAT
Umited Landing Weight
3. The Perfonnance Umited Landing Weight is the lower of the Runway Umited and ..)
the WAT Limited Landing Weight. ~
~ INTRODUCTION
Flight with wide cut (JP4) typefuelis onlypermitted if the limitations and procedures given in the
Flying Manual Vol. 2Section 4 arefollowed and theperformance effects given below areapplied.
B. fliGHT PlANNING
The density of wide cut (JP4) type fuel may be significantly lower than that of normal fuel i.e.
densities below 0.76 are relatively common with JP4 type fuel. As a result the likelihood of
reaching limiting values of take-off CG limited fuels and tankvolumetric capacities areincreased.
Sufficient data is published in the Refuelling Book and load and Balance Manual to coverthe
majority of fuel densities likely to be experienced.
Observe the maximum altitude of 36,OOOft and the maximum TAT of + 15°C using the graph on
page 1.8.18. overleaf as a guide.
C. TAKE-OFF
D. lANDING
The landing WAT limited weight must be reduced by 6% using the table below.
,
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A. UMITAnONS
2. All the performance effects for an unreheated take-off are included in this procedure.
Therefore, the performance effects for Dispatch With One Reheat Inoperative and Dispatch
With One or more Secondary Air Door Systems Failed Shut do NOT need to beapplied to the
unreheated take-off case but the landing penalties still apply.
B. RIGHT PLANNING
1. Take-off is not permitted if the airfield pressure altitude is above 4.0D0ft.
~ C. TAKE-OFF
1. The PlTOW must be reduced by 25% using the table below.
D. LANDING
1. No penalties required.
E. NOISE ABATEMENT
1. GENERAL
~ The standard noise abatement instructions asgiven in theFlying Manual should befollowed
except that noise abatement speed is 225kt in place of 250kt.
2. SPECIRC PROCEDURES
Where specific noise abatement instructions are provided e.g. London Heathrow.
Washington. New York etc., the following corrections to these instructions should be
applied:
1 GENERAUSED PROCEDURE
a.Afterthrottling maintain 225kt until any crossing height requirements are assured.
N.B. Take-off witllout reheat may not necessarily be tile optimum for overall noise
abatement whentIIis procedure is used since tile noise under tile flight patll will be
greater aftertllrottling due to lower height gain. Mostnoisereduction will bein tile
immediate airportsurroundings to tile side of tile runway and to tile side of tile flight
patll. However, take-off wltllout reheat should be used where possible at weights
below 140000kg. in tile Interest of aircraft handling and passenger comfort. since
noise levels botll witll and witllout reheat at tIIese weights are considerably below ... )
tIIose produced by heavy weight take-oils. ~
Secondary Air Doors must beclosed during take-off and must notbeopened untila speed of
250kt has been achieved whatever procedure has been utilised.
A. UMITAnONS
1. Gear must be established locked down and landing gear doors locked shut before flight.
3. Areas ofknown turbulence should beavoided. If rough air is encountered, flightis permitted at
the maximum speed limit but in order to avoid frequent overspeed excursions it may be
necessary to select a speed below the maximum. For performance reasons speed reductions
below the maximum permitted speed should be kept to a minimum.
B. FLIGHT PLANNING
1. DESTINAnON AIEL AND nME
Destination Fuel and TIme should be obtained from the "GEAR DOWN OPERATION -
DESTINATION FUEL AND TIME" chart in thissection. The chart values include allowances
for take-off and approach and landing. In addition, the chart also gives maximum cruise
height available as a function of Take-Off weight.
f Alternate fuel and time can also be obtained from the "GEAR DOWN OPERATION -
DESTINATION FUEL AND TIME" chart in this section. Tothis should be added an alternate
reserve allowance of 8500kg, representing 30 mins hold at 60000 and 250kt at a mean weight
of 10SOOOkg.
3. TERRAIN CLEARANCE
With gear down and speed limited to 270kt the net ceiling obtainable in the event of engine
failure canbevery restrictive. The "GEAR DOWN OPERATION - NET CE/UNGS" chart in this
section should be used to establish en-route terrain clearance.
C. TAKE·OFf
1. The PLTOW must be reduced by 7% using the table below.
D. LANDING
1. For VUF landings the landing WAT limited weight must be reduced by 0.5% using the table
below.
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QC 762
Rev:
8Rrnmt
'-wAYS CONCORDE PERFORMANCE MANUAL SPECIAL
OPERATIONS
GEAR DOWN OPERATION CHART 2
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CONCORDE PERFORMANCE MANUAL ICY/SUPPERY
A. INTRODUCTION
This is the most difficult situation to deal with simply because there is no reliable way of
measuring braking co-efficient which is representative of a stopping aircraft. A slippery runway
is defined as one with a uniform theoretical braking co-efficient of 0.05 Mu (0.05 JBII. it is
important to note thatthis condition is assumed to beuniform over thefull length and breadth of
the appropriate runway surface - a most unlikely situation. In slippery runway conditions
stopping the aircraft presents the greatest problem.
The slippery runway data, when used, may well produce very limiting Take-off weights so it is
essential that careful thought is given before use.
A slippery runway caused byice is usually of short duration buta slippery runway can becaused
bywateronrubber deposits and onsmooth surfaces. If a runway is promulgated as"liable to be
slippery when wet", it means thata certain portion of the runway (in UK more than lOOml hsa a
Mu-meter reading of 0.39 10.49 JBII or below. This could mean that the whole runway has a
braking action of medium/good - veryfar removed from theassumed co-efficient of0.05 Mu10.05
JBllfor a slippery runway.
As well as rubber deposits and smooth surfaces, local pools of water can also give a "liable to
beslippery when wet" state. InthePerformance Manual whenever such a statementis made, an
indication of where and why will be included to enable pilots to make better assessment of the
particular situation. Whilst one cannot and should not interpolate between normal wet runway
data and slippery runway data thetwo sets of data for a particular runway give anindication of
possible margins and may assist the Captain to choose the most appropriate level of
performance for the conditions.
B. UMITATlONS
If more than one abnormal operation applies check thatthecombination is permitted by refering
to the "COMBINATIONS OF OISPATCH DEVIATIONS/SPECIAl OPERATIONS in Section 1.8.
The procedure in Section 1.1. "CONTINUED TAKE-OFF WITH ONE REHEAT FAILED -
UNPREMEDlATED" must NOT be used on an icy/slippery runway.
3.
Either:-
OR:-
Obtain the difference between actualONH and1013.2 mb, then use one of themethods to correct
thePLTOW. associated speeds and 9 2• depending onthevalue of V, found above:
USE V, = 132kt
Obtain the difference between theActual Take-off Weight andthePLTOW then use one of the
following methods to furthercorrectthetake-off speeds and 82. depending onthevalue of V1
(corrected for pressure height) found in 1.9.2. E.
IFV1 (corrected for pressure height) > 132kt apply normal corrections.
USE V1 = 132kt
'~
6 136.4 6.6 169.2 3.5 186.8 0.3 189.8 0.3 192.7 19.3
___ ~~~Ll~~___ lJ6L12~__ ~J~L~2~___ 1~QLl2a__ ~~~L6Q6___ _ _
4 138.9 6.7 172.2 3.0 16i.2 0.3 190.2 0.3 193.1 19.3
___ lJ6L~~~___ !J6L!22___ !JQL12~ ~QL!~~___ li~L6QJ___ __ _
2 141.4 6.8 175.2 2.5 187.6 0.3 190.5 0.3 193.4 19.3
___ J6L!~~___ lJ6L1Z~___ !J1L!2~__ lilL6QQ___ SL6QJ-- _
o 143.9 6.9 178.2 2.0 188.0 0.3 190.9 0.3 193.8 19.4
--- lJ6Ll~2___ lJ6LleL__ !JZL!22___ ' ~6L6QQ___ H~L6Q~__ __ _
-2 146.6 6.9 181.3 1.4 186.3 0.3 191.2 0.3 194.1 19.4
__ !J6L!~2-- lJ6L1SZ___ !Jall21--_ i6L~Ql___ 1~lL6Qi__ _ _
-4 149.2 '7.0 184.0 0.9 186.6 0.3 191.5 0.3 194.4 19.4
,
___ lJ~!§l___ lJ6L~21___ !J~L!~2-- liJL6Q!__ !~lL6Q~___ __ _
"-' -6 152.0 6.5 184.3
__ lJ6Ll§J___ !JJL!26___
0.9 188.9 0.3 191.7
lJ~Ll~a___ !i~L6Ql___
0.3 194.6 19.5
~eL6Q~___ _ _
-8 154.8 6.0 184.6 0.9 189.1 0.3 192.0 0.3 194.9 19.5
___ ~J6Ll§~___ lJJL!~6___ 1~QL!2e___ ~~L6Q,-__ 1~2L6Q§___ _ _
-10 157.6 5.4 184.8 0.9 189.4 0.3 192.2 0.3 195.0 19.5
___ lJ6L!§1___ !J~L12J___ !!QL!2~___ !i~L6Q6___ 1!2L6Q§___ _ _
-12 157.6 5.4 184.7 0.9 189.3 0.3 192.1 0.3 195.0 19.5
___ lJ6Ll§2___ lJ!L12J___ !!QL!22___ !i~L6Q6___ 1~2L6QQ___ _ _
-14 157.6 5.4 184.6 0.9 189.1 0.3 192.0 0.3 194.9 19.5
___ lJ6Ll§1___ lJiLl~J___ iQL122__ ~i5L6Q6__ 1!2L6QQ___ _ _
-16 157.6 5.4 184.5 0.9 189.0 0.3 191.9 0.3 194.8 19.5
___ !J6L!61___ J~L12J___ !i!L!2~_ li5L6Q6___ li2L6Q§___ _ _
-18 157.6 5.4 184.4 0.9 188.9 0.3 191.8 0.3 194.7 19.5
___ lJ6Ll§1___ iL!2J___ !ilL!22--- aQJ_ !i2L6Q§_ __ _
-20 157.6 5.3 184.3 0.9 188.8 0.3 191.7 0.3 194.6 19.5
___ !J6L!§1___ JiL!2J___ !i~L~2 !i5L6QJ__ 1~2L6Q§___ _ _
-22 157.6 5.3 184.2 0.9 188.7 0.3 191.6 0.3 194.4 0.1 195.0
___ !J6L!§1___ JiL121-__ ~!L~2__ li5L6QJ !i2L6Q§___ 15JL6Q~
OAT 10kt Inc 5kt Inc STILL Inc 10kt Inc 20kt Inc 30kt ~
C TAIL /kt TAIL /kt AIR /kt HEAD /kt HEAD /kt HEAD
6 135.7 6.5 168.3 3.6 166.5 0.3 169.5 0.3 192.4 19.2
___ !l~L!~~___ !1~L~Z~___ !1~L!~~___ !~QL!~e___ !iiL~Q~___ _ _
4 138.1 6.6 171.3 3.1 186.9 0.3 189.9 0.3 192.8 19.3
___ !~~L!~~___ 11~L!ZQ___ !1gL!~2___ !~QL~~___ 1~~L~Q6___ _ _
2 140.6 6.B 174.4 2.5 187.3 0.3 190.2 0.3 193.1 19.3
__ !1~L!~~___ !1~L1Z§___ !aZL1~2___ !~lL!~~___ !~~L~Q1___ _ _
o 143.1 6.8 177.3 2.1 187.7 0.3 190.6 0.3 193.5 19.3
___ 1~6Ll~2___ 11~Lle6___ !a2L!~~___ !i~L6QQ___ 1~~L6Qa___ _ _
-2 145.7 6.9 180.3 1.5 188.0 0.3 190.9 0.3 193.8 19.4
___ !16L!~2___ !a~L!e2___ laeL12Q___ !i~L6QQ___ l~~L~Q~___ __ _
-4 14B.4 7.0 183.5 1.0 168.3 0.3 191.2 0.3 194.1 19.4
___ !16LlgQ___ 11~L12Q___ laeL!~2__ ~L6Q!___ ~ZL~Q~___ _
-6 151.1 6.6 184.0 0.9 188.6 0.3 191.4 0.3 194.3 19.4
___ 1~~L!g6___ 111Ll~1___ la~L12Z__ !~~L6Ql___ 1~eL~Q2___ _ _
-8 153.9 6.1 164.3 0.9 166.6 0.3 191.7 0.3 194.6 19.5
___ l~~L!§~___ 11~L12~__ !~QL12e___ !~~L~Q~___ 1~aL'Q5___ __ _
-10 156.7 5.6 164.5 0.9 169.1 0.3 191.9 0.3 194.8 19.5
___ 11~Ll~g___ 11%l126___ 1~QL12e___ !~5L6Q~___ 1~2L~Q§___ __
-12 156.7 5.5 184.4 0.9 189.0 0.3 191.8 0.3 194.7 19.5
l~aLl§g___ 1~~L1~6__ ~Q~e___ li5L6Q6__ !~2L~Q~__ __
-14 156.7 S.5 1B4.3 0.9 16B.B 0.3 191.7 0.3 194.6 19.5
1~Llgg__ !a~Ll~6--_ ~QLl~e___ !~5L6Q~__ li~~§___ __ _
-16 156.7 S.S 184.2 0.9 1BB.7 0.3 191.6 0.3 194.5 19.4
11~Llg§__ la~Ll~~_ QLl2~ !~~L6Q6___ l~~L6Q~__ _
-18 156.7 5.5 164.1 0.9 1B6.6 0.3 191.5 0.3 194.4 19.4
___ 116Llgg__ !1~L12~__ 1~QLl2a___ 1~5L6Q6___ l~~§ _
-20 156.7 5.5 164.0 0.9 1BB.S 0.3 191.4 0.3 194.2 19.4
__ !1~Llgg__ la~L12~_ 1~QLl2~~ !~5L6Q6___ !~~L~Q§___ __ _
-22 156.7 5.4 183.9 0.9 16B.4 0.3 191.2 0.3 194.1 0.1 195.0
___ !1~Llgg !a~L12~__ QLl28-__ !~5L~Q~___ l~~LaQ~___ !S~L~2
~ JAT 10kt Inc 5kt Inc STILL Inc 10kt Inc 20kt Inc 30kt
C TAIL /kt TAIL /kt AIR /kt HEAD /kt HEAD /kt HEAD
6 160.5 4.2 181.7 0.9 186.1 0.3 188.8 0.3 191.4 0.3 194.2
___ l~~Ll§~___ b~~L!~l___ !~!L!~§___ b!gL~~___ l~gL~Q~___ !~!L~Q2
4 163.3 3.7 182.0 0.9 186.4 0.3 189.0 0.3 191.7 0.3 194.5
___ !~~Ll11___ !~~L!~~__ !~~L!~~__ 1JQL~Q___ ~!L~~___ !~~L~Q~
2 166.3 3.2 182.4 0.9 186.7 0.3 189.3 0.3 192.0 0.3 194.8
___ 1~~L111____ 1~QL1~~___ !~~!~2-- !~~Q2-- l~!L~Qi-__ !~5L~Q~
o 169.3 2.7 182.8 0.8 187.0 ~.3 189.6 0.3 192.3 0.3 194.9
___ 1~~L!1~___ !~1L!~1___ !~JL1i1--_ !!1L~g!___ l~~L~Q~___ !~L~Q§
-2 172.3 2.2 183.1 0.8 187.2 0.3 189.8 0.3 192.5 0.2 195.0
___ !~~Ll11___ !12Ll~1___ !~iL!~1-__ ~eL~Q!__ !~~L~Q~__ !~!L~Q~
-4 175.3 1.6 183.4 0.8 187.4 0.3 190.0 0.3 192.7 0.2 195.0
__ !J~L12i-__ !~aL!~~___ !~!L!~~__ !!2L~Q ~~L~QQ_ l[!L~Q2
-6 179.2 0.9 183.6 0.8 187.6 0.3 190.2 0.3 192.9 0.2 195.0
___ !J~Llaa___ !~eL12~___ !~~Ll~a___ !~~L~Q~_ !~~L~Q2___ 1~~L~Q2
-8 179.4 0.9 183.8 0.8 187.8 0.3 190.4 0.3 193.0 0.2 195.0
___ lJ~L!aa___ !~2L12i___ 1~QL!2~___ !~QL~QJ___ l~~L~Q§___ l~~L~Q~
-10 179.7 0.9 184.0 0.8 188.0 0.3 190.6 0.3 193.2 0.2 195.0
___ 111Llai-__ 1~QL1~!___ !~~L12~__ !~lL~Qi-__ l~~L~QQ__ ~~L~Q~
-12 179.6 0.9 183.9 0.8 187.8 0.3 190.5 0.3 193.1 0.2 195.0
___ !JJLla~___ !iQL1~~___ liQL122___ l~!L~Q~___ l~~L~Q!___ lQQL~Q2
-14 179.5 0.9 183.8 0.8 187.7 0.3 190.4 0.2 192.9 6.2 195.0
___ !JJLla~___ biQL1~~__ !iQL!~~___ l~L~Qi___ 1~~L~Q1___ !QQL~Q2
-16 179.4 0.9 183.7 0.8 187.6 0.3 190.2 0.3 192.8 0.2 195.0
___ 11JL~ai-__ iQL!~~___ liQL!~~ !~L~Q~___ l~~L~Q1--_ lQQL~Q2
-18 179.2 0.9 183.5 0.8 187.4 0.3 190.1 0.2 192.6 0.2 195.0
___ lJJLla2--_ iQL!2!__ !!L~QQ !~lL~Qi__ b5~Q1--_ lQQL~Q2
-20 179.1 0.9 183.4 0.8 187.3 0.3 189.9 0.3 192.5 0.2 195.0
___ lJJLla2--_ liQL!2i-__ !i!L~2-__ 15lL~Q~__ 15~Q!___ lQQL~Q~
-22 179.0 0.8 183.2 0.8 187.2 0.2 189.7 0.3 192.3 0.3 194.9
___ !1~Lla2___ liQL!2i___ !~L~QQ___ !~~QJ__ l~QL~Q QQL~Q2
OAT 10kt Inc 5kt Inc STILL Inc 10kt Inc 20kt Inc 30kt
C TAIL /kt TAIL /kt AIR /kt HEAD /kt HEAD /kt HEAD
---6 ---------- ----------
120.1 5.7 148.5 ----------
6.0 178.7 ----------
0.3 181.6 184.5 0.3 -------
0.3 ---------- 187.3
~J~L~12___ ~~~L~gb___ !JJLl~Q___ b12L!~1___ !ilL!~~__ ~gL12e
4 122.1 5.8 151.1 5.6 179.0 0.3 182.0 0.3 184.9 0.3 187.6
___ J~Ll~l__ 11~~gJ___ lJJL122-- l~L!~J___ ~~Ll25- l~§Ll~
2 ~24.2 5.9 153.9 5.1 179.4 0.3 182.3 0.3 185.2 0.3 187.8 ~
___ lJ~Ll~~ lJ~Llg~ ~J~Ll~~_ lJeL~J..__ ~l~_ ~2L~~~
o 126.3 6.1 156.7 4.6 179.8 0.3 182.6 0.3 185.4 0.3 188.1
lJ~L~~~___ lJ~L~gg___ !J~Ll~~__ lJ2L12 ~1L12~_ ~eL~2~
-2 128.5 6.2 159.5 4.1 180.0 0.3 182.9 0.3 185.6 0.3 188.3
'~~~~Q ~J~L~Qe- __ !J~L~~ 112L!21- ~Ll~_ ~eL~QQ
-4 130.8 6.3 162.4 3.6 180.3 0.3 183.1 0.3 185.8 0.3 188.4
J~Ll~2___ !J~L1IQ___ J§L~~___ 1~QL1~i-__ i2Ll~__ ~2L~QQ ~
-6 133.1 6.5 165.4 3.0 180.5 0.3 183.3 0.3 186.0 0.3 188.6
l~~Ll~~___ !J~Ll1~___ lJQL!~~___ li!L!~___ li~L122___ b5QL~Q!
-8 135.5 6.6 168.4 2.5 180.7 0.3 183.5 0.3 186.2 0.2 188.7
___ lJ~Ll~l___ !1~Llli___ 111Ll~~___ lilL12i___ ~§L122___ 15QL~Q~
-10 138.0 6.7 171.5 1.9 180.9 0.3 183.7 0.3 186.3 0.3 188.9 ~
___ . JU!5iL_ ~L.u§___ lJflL!2&_ H&L!2!___ i2Ll~iL__ 151L~Q;I. . .'
-12 138.0 6.7 171.5 1.9 180.8 0.3 183.6 0.3 186.2 0.3 188.8
___ lJ~L15~___ lJ~Lll§___ !JflL!~&___ ;l.i~Ll~!__ lilL12fl___ ;I.~lL~Q;I.
-14 138.0 6.7 171.5 1.8 180.7 0.3 183.5 0.3 186.1 0.3 188.7
___ ;l.J~L!~~ lJ~L!l§___ lJeLl2! 1!6L12i-_ lilL!2e 151L~Q1J
-16 138.0 6.7 171.5 1.8 180.6 0.3 183.3 0.3 185.9 0.3 188.6 ~
~Ll~~ J~Lll§___ JflLl21___ !6Ll~___ ilLl~e__ 51L2Ql
-18 138.6 6.7 171.5 1.8 180.5 0.3 183.2 0.3 185.8 0.3 188.4
___ lJ~L!~~___ 11~l1Q___ lJflLl~~__ li~L194___ 1!~2fl-__ ~lL2Ql
-20 138.0 6.7 171.5 1.8 180.4 0.3 183.1 0.2 185.6 0.3 188.3
11~L!5~___ lJ~Ll1Q___ !JflL!2!_ li6L~_ !!2L!2e___ !~lL~Q;I.
-22 138.0 6.7 171.5 1.8 180.3 0.3 182.9 0.3 185.5 0.3 188.1
1~Ll~~___ lJ~Ll2§___ 1flL121_ li~Ll~i 2L12a___ S!~Q;I. ~
V2= VEl'" 35 VR+ 24 VR+ 23 VR+ 23 VR+ 22 VR+ 23
82= 16.5 14.5 13.5. 13.5 13.0 13.0
1.*TaJce.Off Minima: Where RVR/VIS is shown as0.5sm 1240Oft) orless, higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5 onPage 1.1.3.
OAT 10kt Inc 5kt Inc STILL Inc 10kt Inc 20kt Inc 30kt
C TAIL /kt TAIL /kt AIR /kt HEAD /kt HEAD /kt HEAD
1.-Take-Off Minima: Where RVR/VlS is shown as0.5sm 124000) orless, higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
OAT 10kt Inc 5kt Inc STILL Inc 10kt Inc 20kt Inc 30kt
C TAIL /kt TAIL /kt AIR /kt HEAD /kt HEAD /kt HEAD
--- ---- ------ ----- ----- -------1---
6 120.1 5.7 148.5 6.9 183.2 0.5 188.3 0.3 191.5 0.3 194.7
___ lJ~L~__ lJ~L1Ql___ 1~2Ll89__ lJQLl~Q___ liQL~Q~__ liiL~Qi
4 122.1 5.8 151.1 6.9 165.6 0.3 166.8 0.3 191.9 0.3 195.0
__ IJ~Ll~l_ l~~LIQ~___ l~Ll~__ l~~Ll~l___ lilL~Ql__ i~~Q~
2 124.2 5.9 153.9 6.4 166.1 0.3 189.2 0.3 192.4 0.3 195.0
___ 132L1i2_ lJ2L1Q5__ ~l l12Ll~1-_ lil~ l~~Q~
o 126.3 6.1 156.7 6.0 166.5 0.3 189.6 0.3 192.8 0.2 195.0
___ l~lii_ lJaLl~ ~ ~2Ll~e_ ZL~QZ_ ~QQ
-2 128.5 6.2 159.5 5.5 186.9 0.3 190.0 0.3 193.2 0.2 195.0
___ l1~~Q_ lJ2LlQS___ l~lai l~Ll~~_ li~L~J__ QL~
-4 130.8 6.3 162.4 5.0 167.3 0.3 190.4 0.3 193.6 0.1 195.0
___ 1~~Lli2__ lJ~Ll1Q___ lJJLl~__ IJ~Ll~~__ liJL~QJ__ li~L2Ql I
-6 133.1 6.5 165.4 4.4 187.6 0.3 190.8 0.3 194.0 0.1 195.0 ~
__ l1~Lli~__ 112Ll14__ ~l~ lJ~~Qa- liiL2Qi_ li1L~Ql
-8 135.5 6.6 166.4 3.9 187.9 0.3 191.1 0.3 194.3 0.1 195.0
__ 112L151_ l~Ll1i ll5Ll~_ QL2QQ ~_ li~l
-10 136.0 6.7 171.5 3.4 188.3 0.3 191.4 0.3 194.6 0.0 195.0
___ UZill&_ ~Ll1Q l~ lliL~_ iaL~QS
-12 138.0 6.7 171.5 3.3 188.2 0.3 191.3 0.3 194.5 0.0 195.0
-__ lJ4Ll5&_ l~~LIIQ__ QL1~___ liQ~Ql-- i~L6Q~_ liaL~QS
-14 138.0 6.7 171.5 3.3 188.1 0.3 191.3 0.3 194.4 0.1 195.0
__ lJZL~ IJ2Lll~__ l~l~_ liQ~Q i5L2Q L~Qa
-16 138.0 6.7 171.5 3.3 188.0 0.3 191.2 0.3 194.3 0.1 195.0
_ llU~_ ~Ll~ asz QQQl-- ~~_ UaL4QS
-18 138.0 6.7 171.5 3.3 187.9 0.3 191.1 0.3 194.2 0.1 195.0
_ ~ill&- ~Ll1Q_ 141L2Ql__ 2Q~_ liaL~
-20 138.0 6.7 171.5 3.3 187.8 0.3 191.0 0.3 194.2 0.1 195.0
__ lJ2L~__ 1~2LIIQ_ IJ6Ll~ lil~Ql--_ ~2Q5__ liSL6QS
-22 138.0 6.7 171.5 3.2 187.7 0.3 190.9 0.3 194.1 0.1 195.0
___ IJaLl~~__ 1~6Ll1~___ IJ~Ll~l___ UIQQl-__ i5L~Q~___ liaL~Qa
1.-Tu.off Minima: Where RVR/VIS is shown as0.5sm (240OftI orless, higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5 onPage 1.1.3.
3.Noise Abatement Procedures: See Pages JF1q19, 20, 21, 22, 23, 24and 25.
OAT 10kt Inc 5kt Inc STILL Inc 10kt Inc 20kt Inc 30kt
C TAIL /kt TAIL /kt AIR /kt HEAD /kt HEAD /kt HEAD
--- 0.8 ----------
----------
6 183.0 187.1 0.8 ---------- ----------
191.0 0.3 193.6 19.4 ---------- -------
~~L1~___ l~SL~~l___ l~L~QJ___ 1~5L6QQ___ _ _
4 183.3 0.8 187.4 0.8 191.3 0.3 193.9 19.4
___ ~~L1~6___ l~5Ll~8___ ~~L6Q~__ 1~1L6Q1-__ _ _
2 183.6 0.8 187.7 0.8 191.5 0.3 194.1 19.4
___ l~QL1~~___ l~lLl~~___ l~~L~~___ lS2L~QZ___ _ _
o 184.0 0.8 187.9 0.8 191.8 0.3 194.4 19.4
_-_ l~lLl~~___ l~ZL1~~___ 1~~L6Q~___ 1SSL6Qe___ _ _
-2 184.3 0.8 1BB.1 0.8 192.0 0.3 194.6 19.5
___ ~lLl~~___ 1~8L6QQ___ l~L~Q5___ lS~L6Qa___ __ _
-4 IB4.5 0.8 188.3 0.8 192.2 0.2 194.7 19.5
~6~S___ ~~L6QQ_~' lSSL6~_ 15QL6QS-__ _
-6 184.7 0.8 188.5 0.8 192.4 0.2 194.9 19.5
___ i~Ll~~___ 1~~L6QQ___ l~L~~ R~QS___ _ _
-B 1B4.B 0.8 188.6 0.8 192.5 0.2 195.0 19.5
___ li~L12R___ 1~QL6Ql___ 1~L6Q~__ lL~Qa___ _ _
-10 184.9 0.8 188.B O.B 192.7 0.2 195.0 19.5
___ iiLl2l__ 1~lL6Ql___ 1~L6QR___ 15~L6Q~___ _ _
-12 184.9 0.8 188.7 O.B 192.5 0.2 195.0 19.5
___ ~iLl~R___ lS1L6Ql___ lS1L~Q§_ lR6L6Q2__ __ _
-14 1B4.8 0.7 ~88.5 0.8 192.4 0.3 195.0 19.5
___ liiL!25___ l51L6Q1___ 1~L6Q~__ lR6L6Q2-__ _ _
-16 184.6 0.8 188.4 0.8 192.3 0.2 194.8 19.5
liiL19 151L6Q1__ 1~L6~ 156l6Q2-__ _
-18 184.5 0.8 188.3 0.8' 192.1 0.3 194.7 19.5
iL la!6Ql_ 7 ~Q2-
-20 184.4 0.7 188.1 0.8 192.0 0.2 194.5 19.4
__ WLl2R 151L1Q1 illa~ 6L6QL -+-__
-22 IB4.2 0.8 188.0 0.8 191.8 0.2 194.3 0.1 195.0 0.0 195.0
__ l~Ll~_ lS1L~Ql___ 158L6 ~l6Q2- lR§L61Q__ lR2L61Q
V2= VR+ 23 VR+ 23 VR+ 23 VR+ 23 VR+ 23 VR+ 23
82= 13.5 13.0 13.0 12.5 12.5 12.5
1.-Take-Off Minima: Where RVR/VIS is shown as 0.5sm (240001 orless, higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
3.Noise Abatement Procedures: See Pages JF(q32. 33, 34, 35. 36. 37. 38and 39.
2
-----'--l~---_ ....
-o
-2
--
-4
------+..-----+
---l~-
-6
....
--l~----~~~Y2-
-8
....
--l~----_I_.!..:i~~~
-10
-
-16
-----
-
-18
-20
.-22
1.ARRESTER GEAR: This data isvalid only with Arrester Net in DOWN position.
I ROVAN! EM! I
1./0 E1ev 645ft
Rl,.'Y G
CLG RVR/VIS SLOPE O.23%UP
TOR 3000m (9843!t) ED 3000m (9843f~) TOO 3300m (10627ft)
OAT 10kt Inc 5kt Inc STILL Inc lOk~ Inc 20kt :nc 30~t
C TAIL /kt TAIL /kt AIR Ikt HEAD /kt HEAD /kt HEAD
-18 120.3 5.6 148.4 2.2 170.8 1.2 182.7 0.3 185.6
.--- !~6L1J2___ l~~L1~l___ ~J6Ll22___ 1JiLl2~___ l12L12e
-20 120.3 5.6 148.4 2.2 170.; 1.2 162.6 0.3 185.7
.--_. 1~6Ll~2___ l~6L1~l___ 116L122___ lJ~L12~ lJ2L!2e
-22 120.3 5.6 148.4 2.2 170. 7 1.2 162.5 0.3 185.5
__________ 1~6L1J~___ lJ6Ll~l___ lJ6!l22___ 1~~L121___ lJ~L12e
V2=
82=
VR+
0.0
0 VR+ 42
17.5
VR+ 29
16.0
VR·' 24
14.0
I vs- 22
13.0
VR+ 22
0.0
I .
1. Arrester Gear: This data is valid only with Arrester Net in DOWN position.
RWY ~
CLG RVR/VIS SLOPE 0.16'DN
TOR 3505m (11499ft) ED 3505m (11499ft) TOO 3828m (12559ft)
OAT 10kt Inc 5kt Inc STILL Inc 10kt Inc 20kt Inc 30kt
C TAIL Ikt TAIL Ikt AIR Ikt HEAD Ikt HEAD Ikt HEAD
RWY~
CLG RVR/VIS SLOPE 0.16'DN
TOR 3505m (11499ft) ED 3505m (11499ft) TOD 3855m (12648ft)
OAT 10kt Inc 5kt Inc STILL Inc 10kt Inc 20kt Inc 30kt
C TAIL /kt TAIL Ikt AIR /kt HEAD Ikt HEAD Ikt HEAD
6 117.0 5.6 145.0 6.8 179.0 0.9 188.4 0.3 191.4 0.3 194.4
___ lJ~L112-__ 132L159___ 13~LleS___ 135L198___ 139L~Q2 Q~
4 119.5 5.6 147.7 6.9 182.1 0.7 188.9 0.3 191.9 0.3 194.9
___ lJ~L13 lJ2L1~Q___ 1J2L19Q_ 5L199.... 1jQL2QJ- 1iiL2Q~
2 121.5 5.8 150.3 7.0 185.4 0.4 189.3 0.3 192.3 0.3 195.0
___ 1J4L1j1___ 1J2L1~2___ 1J2L19j__ 6Ll99_.... ljQL~Q1 liiL2Q1
o 123.6 5.9 153.1 b.7 186.7 0.3 189.7 0.3 192.6 0.2 195.0
___ 1J2L1~~___ 32L1~j__ 1J2L19~__ L~QQ___ lJ1L2Q~ ~2Q2
-2 125.7 6.0 155.9 6.2 187.1 0.3 190.0 0.3 193.0 0.2 195.0
___ 112LUj U2L1g~_. __ UJL12Q..__ IJWQQ___ lJ1L~Qj ~Qe
-4 127.9 6.2 159.7 5.7 187.4 0.3 190.3 0.3 193.3 0.2 195.0
___ 13~L1j5__ 1~2Ll~e___ 1JJL192__ 38L~Q1___ 1j2L2Q5___ li6L2Qe
-6 130.2 6.3 161.6 5.2 187.7 0.3 190.7 0.3 193.6 0.1 195.0
___ IJ~LU2_.... J2L11~___ 11jLl91___ JaL2Q1_.... 1jJL2Q5_ li5L2Qe
-8 132.5 6.4 164.5 4.7 188.0 0.3 190.9
0.1 195.0 0.3 193.9
__ 11~LU9___ 1J2L111___ 1J5Ll9a___ 12L~Qi-__ 1~Jl2~ 7 Q2
-10 134.9 6.5 167.5 4.2 198.3 0.3 191.2 0.3 194.2 0.1 195.0
___ 11~Ll5Q ...._ 1J2L11 51198___ jQL2Q2___ lJjL2Q 7 Q2
-12 134.9 6.5 167.5 4.1 188.2 0.3 191.1 0.3 194.1 0.1 195.0
___~~~Q___ 2L111___ 115L128___ lJQL~Q2___ 12Q Q2
-14 134.9 6.5 167.5 4.1 188.1 0.3 191.0 0.3 194.0 0.1 195.0
___ 112Ll~g___ 1J2111J___ 115L199__ 1jQL2Q2___ jiL2 li1L2Q9
-16 134.9 6.5 167.5 4.1 188.0 0.3 190.9 0.3 193.9 0.1 195.0
___ 1J2L15~_ IJ2L11J___ 1J51192___ jQL2Q2___ 1iiL~QQ..__ 1jeL2Q9
-18 134.9 6.5 167.5 4.1 187.9 0.3 190.8 0.3 193.8 0.1 195.0
___ 112L150___ 1J2L11J___ 115L122___ iQLaQ1___ 1iiL2Q1-__ IjaL2g9
-20 134.9 6.5 167.5 4.1 187.8 0.3 190.7 0.3 193.7 0.1 195.0
_ 112L150___ 112L11J___ 115L199 1jQ12Q1...._ 1ijLaQ2...._ 8L21Q
-22 134.9 6.5 167.5 4.0 187.6 0.3 190.6 0.3 193.6 0.1 195.0
112LlSQ__ 14L12J___ IJ5L129__ 01--- lijLaQl--- 121Q
V2= VR+ 35 ~R+ 25 I vn+ 22 VR+ 22 VR+ 22 VR+ 22
82= 17.0 14.5 I 13.0 13.0 12.5 12.5
RWY ~
CLG RVR/vIS SLOPE 0.16%UP
TOR 3505m (11499ft) ED 3505m (11499ft) TOO 3761m (12339ft)
:::--::::--:::--::~-::~-:::::-:::--::::-":::l-:::t
C TAIL /kt TAIL /kt AIR Ikt HEAD Ikt
--:::--::::--
HEAD Ikt HEAD
6 123.2 5.9 152.5 6.2 183.7 0.3 186.7 0.3 189.8 0.3 192.8
___ 1J2L1~2___ lJ2L1~~___ 1J~L1~i___ 1~lL12~___ l~lLiQQ___ l!SL~Qi
4 i25.3 6.0 155.3 5.8 184.1 0.3 187.2 0.3 190.2 0.3 193.3
___ 1~2L1~~___ 1JiL166___ lJJL192___ lJ1L19§___ 1!2L2QQ___ l!§LZQi
2 127.5 6.1 158.1 5.3 184.6 0.3 187.6 0.3 190.6 0.3 193.7
___ lJ2L1iS___ 132L1~S___ 13iL193___ 1~BL121___ 1~2Ligl___ li~L2Q5
o 129.7 6.2 160.9 4.8 185.0 0.3 188.0 0.3 191.0 0.3 194.1
___ 1~iL1il 1JiL169 1JiL12i 1~9L1ge. __ 1iJl~Q2 1ilLiQ§
-2 132.0 6.4 163.9 4.3 185.4 0.3 188.4 0.3 191.4 0.3 194.4
___ 1~2L1~2___ 1J2Ll21___ 1J5L19~___ 1~2L19B___ 1~JL2Q2___ 1!BL2Q~
-4 134.4 6.5 166.8 3.8 185.7 0.3 188.7 0.3 191.7 0.3 194.8
___ 13al1SQ___ 132L123___ 13~L125___ liQL129___ 1~~L2QJ___ liBLiQ2
-6 136.8 6.6 169.8 3.2 186.0 0.3 189.0 0.3 192.0 0.3 195.0
___ 132L152___ 132L115__ 13§L195___ liQL199___ 1!5L2QJ___ l~LaQl I
~
-8 139.3 6.7 172.8 2.7 186.3 0.3 189.3 0.3 192.3 0.3 195.0
IJ2L1S~__ 132L111___ 32L19~___ l~lL~QQ___ 1!SL2Qi__ li2l2QB
-10 141.8 6.8 175.7 2.2 186.6 0.3 189.6 0.3 192.6 0.2 195.0
12L155___ 132LlS2___ 132Ll26___ 1i2L2QQ___ 1i6L2Qi___ 15QL2QB
-12 141.8 6.8 175.7 2.2 186.5 0.3 189.5 0.3 192.5 0.2 195.0
___ 132L155___ 132L1S2___ 13lL196___ 1i2L2QQ___ 1i6L2Qi__ 15QL20B
-14 141.8 6.8 175.7 2.1 186.4 0.3 189.4 0.3 192.4 0.3 195.0
__ lJ2L155___ 132L1S2__ 13lL196___ i2L2QQ___ 1~6L2Q~_ L20B
-16 141.8 6.8 175.7 2.1 186.3 0.3 189.3 0.3 192.3 0.3 195.0
lJal155___ 132L1S2___ 13lL196___ 1ialaQQ_ ~6L~__ 15QL2QB
-18 141.8 6.8 175.7 2.1 186.2 0.3 189.2 0.3 192.2 0.3 195.0
_ 132L155__ 132L182___ 13lL126___ 1i2L2QQ__ 1~6LaQ~___ 15QL2QB
-20 141.8 6.8 175.7 2.1 186.1 0.3 189.1 0.3 192.1 0.3 195.0 .
___ 132L155___ 132L1S2 13lL192___ 1i2L~QQ__ t5L2Qi__ 15QL2Q8
-22 141.8 6.8 175.6 2.1 186.0 0.3 109.0 0.3 192.0 0.3 195.0
32L155___ 32L1S2 132L122__.. •i2L2Q1__ 1i6laQS__ SQL2Q9
V2=
92..
YR+ 33
16.5
YR+ 23
14.0
VR+ 22
13.0
I VR+ 22 VR+ 22
12.5
VR+ 22
12.5
I 13.0
RWY~
CLG RVR/VIS SLOPE 0.16\UP
TOR 3s0sm (11499ft) ED 350sm (11499ft) TOD 3669m (12037ft)
~ OAT 10kt Inc 5kt Inc STILL Inc 10kt Inc 20kt Inc 30kt
C TAIL Ikt TAIL /kt AIR Ikt HEAD /kt HEAD /kt HEAD
6 123.2 5.9 152.5 6.6 185.7 0.3 188.6 0.3 191.4 0.3 194.2
___ l~~L~___ !~~L16~___ 1~~Ll~5__ 1~2L!~___ !i!~Q~___ !~~Q6
4 125.3 6.0 155.3 6.2 186.1 0.3 189.0 0.3 191.7 0.3 194.6
J~Ll~___ 1~L!66__ 1~~L!~5___ lJ2Ll~2--_ !i!~~___ !~6~Q6
2 127.5 6.1 158.1 5.7 186.5 0.3 189.3 0.3 192.1 0.3 194.9
___ !~~L~__ !1~L!68-__ l~~Lli5__ !~L!~___ li~~Ql-__ !i6~Q1
o 129.7 6.2 160.9 5.2 186.9 0.3 189.6 0.3 192.4 0.3 195.0
___ !~~L!i2___ !1~L!6~___ !~iL!~6- !~L~Q~___ ~1L~__ 2la22
-2 132.0 6.4 163.9 4.7 187.2 0.3 189.9 0.3 192.7 0.2 195.0
___ ~~L!~~__ !~~L!2!_ L!~2_ ~~QQ___ !~~L~Q~___ li2L6Q2
'-4 134.4 6.5 166.8 4.1 187.4 0.3 190.2 0.3 192.9 0.2 195.0
__ !~~!5Q___ 11~L!~___ 1~5L!~1___ !iQL~Q!___ i~L~___ QS
-6 136.8 6.6 169.8 3.6 187.7 0.3 190.4 0.3 193.2 0.2 195.0
___ !1~L!56___ !1~L1Z5___ 1~6Ll~2___ iQL~Q!--_ !~L~Q5___ !iBL~a
-8 139.3 6.7 172.8 3.0 187.9 0.3 190.6 0.3 193.4 0.2 195.0
_ la~L!5i___ 1~___ !16Ll~_ !!!L~Q!__ i5L~Q5-__ !i~QS
-10 141.8 6.8 175.7 2.5 188.1 0.3 190.8 0.3 193.6 0.1 195.0
__ !~~L!55___ !~6L!a~___ 2L!~__ li!L~Q~_ 1i~Q6___ 5Q~Qa
-12 141.8 6.8 175.7 2.5 188.0 0.3 190.7 0.3 193.5 0.1 195.0
___ !1~L!55___ !1~L!a~___ ~2L!~B-_ !~L~Q~___ ligL~Q6___ 15Q~Q~
-14 141.8 6.8 175.7 2.4 187.9 0.3 190.6 0.3 193.4 0.2 195.0
__ !~~L!55___ !~~Lla~___ !a2L!~a__ !ilL~~_ li~Q6___ !5Q~Q~
-16 141.8 6.8 175.7 2.4 187.8 0.3 190.5 0.3 193.3 0.2 195.0
___ l~~Ll55___ !~~L!e~___ ~2Ll~__ !~L~~___ i~Q6___ 15QL~Q~
-18 141.8 6.8 175.7 2.4 187.6 0.3 190.4 0.3 193.1 0.2 195.0
_ l~~Ll55__ 11~L!e~___ 112L!~B-_ lilL~~___ igL~6- 15QL~Q~
-20 141.8 6.8 175.7 2.4 187.5 0.3 190.2 0.3 193.0 0.2 195.0
___ lllL! l~L!SL.... 132L!~iL_ HU~~ l~~Q6-_ 15Qa~
-22 141.8 6.8 175.6 2.4 187.4 0.3 190.1 0.3 192.9 0.2 195.0
__ U~L!55_ n~Lle~ lllL!~B-_ !~L~L_ ~~Q6.. 22
V2= VR+ 33 VR+ 22 VR+ 22 VR+ 22 VR+ 22
82= 15.5 13.0 13.0 12.5 12.5
j
~
--
..,,4
J
A.. INTRODUCTION
The following table provides guidance for determining whether contaminated runwa y
performance is applicable. 11 is recommended that fur further information reference be made to
the introductory notes to both the "Iake-uf from Icy/Slippery but not Contaminated Runways"
data in this Section and the normal Performance Data in Section 1.1.
N.B. If the ambient temperature is above + S<Callow the runway to drain or clear sufficiently to
allow Normal Performance to be used.
B. UMITATlONS
If more than oneabnormal operation applies check that the combination is permitted by refering
to the"COMBINATIONS OF DISPATCH DEVIATIONS/SPECIAL OPERATIONS" tablein Section 1.8.
The procedure in Section 1.1 . "CONTINUED TAKE-OFF WITH ONE REHEAT FAILED
UNPREMEOIATEO" must NOT be used on a contaminated runway.
Individual runway tables are provided for the main departure airfields. They are produced for
suitable ranges of winds and temperatures and extrapolation outside these ranges is NOT
permitted. The low values of VI required to meet the accelerate stop requirements on an
icy/slippery runway may result in the PLTOW becoming additionally limited by V'M IN (= 132I:t).
1. Ensure that the TOR and EO quoted agree with the officially published figures.
3.
Either:-
Enter the RTOW table with the ambient conditions found in 2. and extract the PLTOW.
associated speeds and 9 2• interpolating as necessary.
OR:-
Refer to the generalis ed charts in this section lor 'Ta ke-off from icyfs lippery or
contaminated runways" 10 obtain the PlTOW. associated speeds and 9 2,
5.0
'"
AOD 0.2
USE VI = 132kt
N.B. No correction 10 S 2 is required ifV,lcorncled forpressure height) is less than 132kt. Use
V, = 132kt.
Obtain the difference between the Actual Take-off Weightand the PLTOW then use one of
the following methods to further correct the take-off speedsand O%' depending onthe value
01V, Iccrected for pressureheight) flJlllld ahave:
USE V, = 132kt
G. DISPATCHDEVIATIONS! SPECIALOPERATIO NS
11 any abnormal operations lifebeing considered the relevant penalty should be applied to the
PlTOWand associated speeds found above (corrected forpressure height) before COl'Tecting
the take-off speeds and Oz forthe Actual Take-off Weight.
OAT lOkt rnc Sltt I nc STILL rnc roxe I nc 2Qkt Inc JOltt
C TAI L /kt TAIL / ltt AIR / kt HEAD /kt HEAD /lt t HEAD
1. Noise Abatement Proceduree: See Pages l HR/1 D, 11, .12 and 13.
OAT l Okt Inc 5kt I nc STILL I nc lakt Inc ~ Okt Inc J Okt
C TAIL / kt TAIL Ikt AI R /k.t HEAD / kt HEAD ! kt HEAD
OAT lOkt Ine 5kt Ine STILL Ine lOkt rnc 20k t Ine 30kt
C TAIL Ikt TAIL Ikt AIR lu HEAD I kt HEAD Ikt HEAD
--- -------- - --------- ---------- 172 .6 0.3 ----------
6 120 .1 5 .7 146 .5 4 .3 169 .9 0 .3 ----------
---- --
1 7 5. 8 0.3 178.6
--- UU1'L_ l J.U151 ___ l .J:.:iLllIL _:- l ' ~Lle. ___ liJ.L1SQ.___ HaL1~Q
,
- - - l.J.UHL__ UU1.L__ U.Lne__ = U QLlf!:.L __ lHL1Sl__ 179
124 .2 5 .9 153.9 3.3 170.6 0.3 173 .5 0 .3 176 .5 0.3
UflLl!i!Q
.5
--- UUH.__ l J U l l:i5___ l.J.!2L11S!___ HoaeL.- H5LlElL__ 1 1~L;!, ~ 1
0 1 26 . 3 6 .1 156 .7 2.8 170 .9 0.3 173 .8 0 .3 176 . 8 0 .3 179 .8
U.LHL__ ...Ll••___ = HUleL__ H.aeL _
-,--- U.LH._ _ u Ul. e___ l.J.UlflQ___
128 .5 6 .2 159 .5
l ' .L12 ~ __
2 .3 171.2 0 .3 174. 1 0 .3 177.1
H~Ll~l
0.3 180 .1
-.
-- 130 . 8 6.3 162 .4 1.8 171.4
HUleL _ H.aee___
0.3 174 .3
--- l J.U H L __ nU11Q___ ueLleo ___ HUlei-__ l~ . Ll ee ___
- 6 133.1 6 .5 165 .4 1.3 171.7 0 .3 17 4 .6 0.3 177 . 6 0 .3 1 80 . 6
0.3 177 .3
1.OL 1~'
0 .3 180 . 4
1. lL l~.
• 179.4
HQLle~ __
0 .9 1 64 . 0
0 .9 168 .6 0 .3 191 .5 0 .3 1 94 . 7 19. 5
H2L12Q___ 1.:iJL1~1 ___ lS:U~Ql __ 1.lL'Q;___
---
2 179 .8 0 .9 184 . 4 0 .9 189.0 0 .3 192 .1 0 .3 1 9 5 . 0 1 9 . 5
- ----
- - - HlL1e; ___ H 2L1SlL__ lSM12L__ l ssa OL _ 152L2QS___ -- -----
a 180.2 0 .9 184 .8 0 .9 189. 4 0 .3 19 2. 5 0 .2 1 9 5 .0 1 9. 5
-- lHLlelL __ 1~e L1~' ___ l S1Ll.2fL __ l;U,Q,-__ 1••aQ; ___ -------
-2 18 0. 6 0 . 9 185 . 2 0 .9 189 .a 0 . 3 192 .8 0 .2 1 9 5 . 0 19 . 5
-.
--- HU1.6l2___
180 . 9
181 .3
H~Ll~'
0 .9 185 . 5
0 .9 1 85 .8
___ 155Ll~HL_ l ;~ aQ ,-
0 .9 19 0 . 1
190 . 4
0 .3 193 .2
--- H UleZ___ H2L1S!.L__ l.5fUl5!5!___ I flOLzO:L __ 1fl1:a.012___ - -----
-5 o.e 0 .3 193 .5
__ 1.U'Q.__~ -------
0 .2 195. 0 1 9. 5
0 . 1 195.0 1 9. 5
l1:JL1Sl-__ ___ ___ ___
---
-8 1 81 .6
1.QL1~'
0 .9 186 .1
l;.L l ~ ~
0 .9 19 0 . 8
Iflla.O~
0 .3 193 . 8
__ 1.~aQ.
0 .1 195 .0 19 .5
- -----
- -- 1H Ll.ee-__ 1.lLl~~ ___ 1.51L2..Q0___ 1.1L'O~ __ Ifl .5a.OL __ ------
l a 1 81. 9 0 .9 1 86.4 o.e 191. 1 0 .3 194 . 1 0.1 1 95 .0 19 .5
l; lLl ~~ ___ l.eLoQQ__
--- H;Llee-_
12 181 . 8 0.9 1 66.4 0 . 9 191 .0
l.U'Q~
0 .3 194.0
__ Ifl~a.OL __
0 . 1 19 5 . 0 1 9 .5
- -----
--- H.5LIE!fL__ 1.51L121:___ 1.513L~00 ___ l 12 U~ 0 1: __ I flflLzoL __ -- - - - --
I ' 1 61 . 7 0 .9 1 66. 3 0 .9 190 .9 0 .3 19 3. 9 0 . 1 19 5 . 0 19 .5
--- H.Llee___ l .5 lLJ.S!~ ___ 1.56aOL__ 1.U'Q.___ l • • aQL_~ - - ---
I. 1 61. 6 0 .9 1 86 .2 0.9 190 .8 0 .3 19 3 . 8 0 . 1 1 9 5 . 0 19 . 5
--- H . L1ee-__ ___ l;eLoQL_ 1.U.Q.__ l • • aQe__~ ------
l.lLl.~.
18 1 61 .5 0 . 9 186 . 1 0.9 19 0. 7
0 .3 19 3 . 7 0 .1 1 9 5 . 0 19 . 5
--- H .aee___ l.5!Ll5!L_ l;eLoQL__ 1.U'Q.__ 1.• • aQe___ - - ---
20 1 61 .4 0 . 9 1 86 .0 0.9 190 .6 0.3 19 3 . 6 0 . 1 1 95. 0 19 .5
-- H .aee___ 1.lLl~ . ___ l~ E!L~QL __ l.flU~Q.5.___ l ••aQe___
22 18 1 . 3 0 .9 1 85.9 0.9 190 .5 0 .3 193 .5 0 . 1 1 9 5. 0 0 .0
- ---
195 . 0
--- H .5L1E!S!___ 1.lLl~. ___ l.5E!L2QL__ 1. U ' Q. ___ 1. oaoe___ 1.~a1Q
OAT l Okt Ine 5kt Ine STILL Inc IOkt Ine 20kt Ine 30ll:t
C Ikt TAIL Ikt AIR Ikt IlEAO I k t
TAIL HEAD 1>< HEAD
6 1 20. 1 5 . '
--------- ---------- ----- ----
--- ---------- 148.5 5 .5 1 7 5 .9 0 . 3 179 . 0 0 .3 ---------
182 .2
-------
0 .3 185 .5
___ ___ UU160 ___ __ H ZLla.e-__
--- U, Ln~ l~ Ul51 Ufl LIE! ~ H,L 1~,
• 12 2 .1
l~UHL_
5.8 151.1
IJUJ.6J _
5 .0 176 .3 0.3 1 7 9 .5
1liL1eQ__ ueL11M_
0.3 182 .6
H,L1e~
0 . 3 185.9
H1L1~~
2 124 ,2 5 . 9 15 3.9 4 . 6 176 .8 0 .3 179 . 9
0.3 193 .1 0 . 3 186 . 4
---
0
n,LH,_ UZLlfiL_ illLlflL_ U2Llfl:.s-.- HU1 ~_~
1 26. 3 6.1 156 . 7 4. 1 177 .2 0 . 3 180.3 0. 3 183 . 5 0 . 3
il2Ll2§
l 86 .S
--- U U H L __ U,L1EfL__ U;L1e1_ U2l16, __ H4 L1~L." U eL1i!>
-2 1 2 8 . 5 6 .2 159 .5 3 .6 177. 6 0 . 3 180 .7 0 .3 183 .9 0 . 3 1 87 .2
-.
---
--
-6
-
U,L14,_ _
130 .a
l ~ , L 14L
133. 1
1~,L1Ee
6 . 3 162.4
6 .5 16 5 .4
__ l ..L16' __ 14oL16,_
3 .1 178 .0
__ IJU 12Q___ U,L1eL __ 141L1eL__
2.6 178 . 3
0. 3 1 8 1. 1
0.3 181.4
H4L1~'L __ 146L1~;
0.3 184.3
14 ;L1 ~ L
0.3 184 .6
0 . 3 1 87 .S
__ 142l1~;
0.3 1 87 . 9
__~ I J.ii:L12Z__ _ _ H ILl fl_'_ ___
--
-8
l~, LH ~
135 .5 6 . 6 168.4
1~1L1e~
2. 0 17 8 . 6 0 . 3 181.8
H5L1~,
0 . 3 185.0
lSQL1~5
0 . 3 IBB.2
--- llli1;L_ n,L12L-_ UUlf!5:___ 14U16e_ il5L1~L.- 1;Q[121
- 10 136 . 0 6.' 171.5 1. 5 1 79 .0 0.3 182 . 1 0 . 3 185.3 0 . 3 IBB .S
-12- ~~,m?
JZ~_ ueL1e4__ H<[lee_ H1L1~,-- 1;lLl21
138 . 0 6.7 171.5 1. 5 178.9 0. 3 1 8 2.0 0. 3 1 85 . 2 0 .3 188.4
--- U<[l;<-_ .n'L1ZfL__ 1~eL1e4 __ H,L1e~_ H1L1~_ 1 ;lL1~1
0 . 3 188 .3
- I ' 13S.0 6.7 171.5 1. 5 17 8 .8 0 .3 181.9 0. 3 185.1
-,,- 1 38 .0
-16
n ,L1;,__ IJ. U116:_ _ 1~eL1 e 4- __
6 .7 171.5 1.4 178. 7
1 4, L1e~_ H1L 1~
0 .3 161.6 0 .3 185. 0
1; 1l121
0.3 186 .3
___ U,L115__ __ ___
--- 1~, L1 S,
- 18 136 .0 6 . ' 1 7 1. 5
1~ eL1 e4- 1 4 U1e~
0 .3 1 81 .8 0.3 18 4.9 0 . 3 188 . 2
1.. 17 8.6
H1L 1~L_ 1;1L121
n U1112___ 1~eL1e ; __c 1 4~L1e~_ 141L1~,-- 1;1L121
---
- 20
l.J.;Ul~Z __
1 38 . 0 6. 7 1 71.5 1.4 17 8 .5 0 . 3 181. 7 0. 3 184 .8 0 .3 188. 1
1~<[1;'_= I J.zL126:__ l~eL1e ;..__ ~4~L1eL=- lSlLl:ll ~~mL"
- 22 138.0 6. 7 171 .5 1. 4 1 78. 5 0 .3 161.6 0.3 18 4 . 7 0.3 188 .0
--- U U 1; L.- U,L11fL- 1~eL1e; ___ H ~L1e2..- 141L1 ~ ~ _ _ .LS1l121
v2= VR+ 35 YR. 24 VR+ 2 2 VR. 22 VR. 22 VR+ 22
82:: 16.5 14 . 5 13 . 5 13.5 13.0 13. 0
. .
1. •Take-OffMmlma. Where AVR,NIS ISshownas O.Ssm (24DOftI or less, higher minimamayapply If
Bny radio orvisual aids areunserviceable. See para 1.1 .5 on Page 1.1.3.
3. Noise Abatement Procedures: See PagesJ FKl1 9, 20, 21, 22,23, 24and 25.
1. - Take-On Minima: WhereRVFWIS is shown as O.5sm l2400ft} or less, higher minima may apply if
anyradio orvisual aidsare unserviceable. See para 1.1.5 on Page 1.1 .3.
3. Noise Abatement Prcceeures: See Pages JFIq32, 33, 34, 35, 36, 37, 38 and 39.
ROVANI EMI
-22
___
__________ UZLU2
1 10 . 0 5 .7 1 38.3 t
lJZL1:iL__ UZLJ.66 . .1J.i<L•• o
2 . 1 159 .5 1 .7T1?G.6
l JZL1J2___ lJZL1:iJ---tJ.JZL1•• ---tl J. ; ~leo--- l 1. Ll.Q
neL12Q
0 . 3179 .6
1. Arreste r Gear: This data is valid only with Arrester Net in DOWN position.
ROVANIEMI
-4
110. 0
lJZL 1J~
112 . 5
r
5 .6 138 .0
lJ2Ll~J_ __
5. 6 140. 5
2.1 1 5 ~ .1
lJ2L l ~e
2 . : . 152 . 0
1 .61:7= .~
+1JiLl e2___
1.3 1175 .3
C. 3 177 .7
lJeL le~
:. 3 176.1
-6
~"Ll'~___
L15 . 0
•••Ll,.___
5. 6 14 3 .0 2. 2
~" L;lQ---I~ ~'Ll6' ~- - ~.a Lla.
~ 64 ._ 1.1 _1 5 . 7 ~. 3 ~7 8 . 4
lJ~ L l~~___ lJ~ L1 S 2 _ _ _ l J Z L i l ~_ _ _ ~~SL ~6J _ _ _ l J~ Lla 2
-8 117.6 5 .6 14 5 .6 2 . 2 167 . 8 0. 8 176 .0 0 .3 176 . 8
I J ~L I J ~ __ _ lJ2L1SS___ l JZ Ll l~ __ _ ~~ 5 Lle i_ __ ~4Q Lle 2
- 10 12 0 .2 5 .6 14 8 .3 2 .2 17 0 .8 O .5 1:7 6 . ~ 0 . 3 1 79 .1
-:2
l" Ll ' ~_ _ _
120 .2
1••Ll.C___ "••L.:l t ",.L". ; ___
5 .6 148 . 3 2 .2 17 0 .7 0 . 5 1 76 .2 0 . 3 1 75 .0
l ;~ /l aa
- 22
1 20 .2 5 .6 1 4 8 . 3 2. 2 A7 0 .
l J 2 L1J~ _ __ IJ~L15Q_ __
120 . 2 5 . 6 146 . 3
1
0' ~ll, ~ .9
2. 2 11 7 0 . 7
O .~ 17 8 .7
l J2Ll : 1 tlJ5Ll64___ 140L16e
0 . 5 17 = . 6 0 . 3 178 . 6
lJ 2 Ll J~ 1 J ~ L 1 64- l§:OLJ.ee
lJZL15Q__.- 1 -n2 L l1L _- fl
·: 2=
: 2=
VR.
0.0
0 VR· 42
17.5
VR+ 30
16. 0
VF-. 24
14 . 0
I V~ ~
~3 . 5
22 VR+ 22
13 . 5
1. Attester Gear: This d ata is valid only with Arrester Net in DOWN posit ion.
II OAT
C
lOkt
TA.IL
Inc
I kt
sxe
TAIL
I nc
/kt
STILL rnc
AI R / kt
IOM
HEAD
Inc
/ kt
2 0k t
HEAD
lnc
I ltt
JOk t
HEAD
6 123.7 5.9 153 .2 4.8 177 .1 0.3 18 0.2 0 . 3 18 3.4 0.3 186.6
__ 1JZL1~l- _ 1JZL10~___ 1J4L1BJ___ 1J6L162 1~JL1B1 142L1BO
4 125 .9 6 .0 156 .0 4 .3 177. 6 0 . 3 180 . 7 0 .3 183 . 9 0.3 187.1
___ 1JZL1~~ 1JZL1BO___ 1J.L16J 1JBL166__ 1~JL1BZ 142L1BO
2 128 .0 6 .2 158.8 3.9 178 .1 0.3 181.2 0.3 184 .3 0 .3 187.6
. 1JZL140 1JZL106 1J.L1B4 14QL166 1~~L1BJ 1~BL1B2
o 130 .3 6 .3 161.7 3 .4 178.5 0 . 3 IB1 .6 0.3 184 .8 0.3 188.0
___ 1JZL1~ 1JZL12Q__ 1JOL16. l~QLl6B 144l1BJ 1~BL1B6
-2 1 32.6 6.4 164 .6 2.9 178.9 0 . 3 182 . 0 0.3 185 .2 0 .3 188 .4
___ 1JZl14B-__ 1JZl12Z___ 1JOL16.___ 141l 1BQ___ 14'L1B~___ 1~BL1B6
-4 1 35.0 6.5 167 .6 2. 3 17 9. 3 0 .3 182 . 4 0 . 3 18 5. 5 0 . 3 188 . 8
___ 1JZl1'l-- 1JZl124___ 1J2l160___ 1~lL1BQ_ __ 140l1B4__ 1.Ql1BB
-6 1 37 .4 6 .6 17 0 .6 1 .8 179 . 6 0 . 3 182.7 0.3 185 . 9 0 . 3 189.2
___ 1JZL1.Z 1JZL12' 1J6l1Bl-__ 14ZL1B1___ l~OllB ' 1.QL1BB
-8 139 .9 6.7 173.6 1.3 180.0 0 . 3 183 .1 0. 3 186.3 0 .3 189 .5
. 1JZL1'~ 1JZL126 1J6l162__ 14JL1B1 142l1Bo 1. 1l ZQQ
-10 142.5 6 .6 175 . 7 0.9180 .3 0 .3 1 8 3 . 4 0.3 186.6 0. 3 189 .9
___ 1JZL1.O___ 1JZL161___ 1JBL16e 1~Jl1BZ___ 1~2L1BO___ 1.ZlZQ1
~12 142 .5 6 .6 175 .6 0 . 9 180 .2 0. 3 18 3. 3 0 .3 186.5 0 .3 189.8
__ 1JZL1. 0- 1JZL16Z___ 1JBLlBB___ 14JL1BZ___ 142l1Bo_ 1.ZLZQ1
-14 142.5 6 .6 175.5 0 .9 1 80 .1 0 .3 183 . 2 0 .3 186.4 0. 3 189 . 7
___ 1JZL1.O___ 1JZl1BZ___ 1JBL166___ 1~JL1BZ_ 142L1BO_ l'ZL~Q1
-16 142 .5 6. 6 175 .4 0. 9 180 .0 0 .3 183. 2 0 .3 186. 3 0.3 189.6
___ 1JZL1.0_ 1JZL16Z__ 1JBL16B 14JL1BZ___ 1~el1BO 15ZLZQ1
48 142 .5 6.6 175.4 0 .9 180 . 0 0.3 183. 1 0 .3 186 .2 0 .3 189 . 5
___ 1JZL1.0_ 1JZL16Z_ 1JBL1B6___ 14JL1BZ___ 146L1Bo__ 1. ZLZQ1
~O 142 .5 6.6 175.3 0 .9 119 .9 0 .3 183 . 0 0.3 186 . 2 0 .3 189.4
___ 1JZL1.5___ 1JZL16Z___ 1JBl166___ 14Jl1BZ__ 14eL1B2_ 1.ZlZQ1
~2 142 . 5 6 .5 175.2 0 .9 179 .8 0. 3 182. 9 0 .3 186 .1 0 .3 189 .3
___ 1JZL1.5___ 1JZL16Z 1JBL1e6___ 1~'L1eZ 1 ~6L 1B2__ 5ZLZQ1
in- VR+ 32 VR+ 23 VR+ 22 VR+ 22 VR+ 22 VR+ 22
e2 ~ 16 . 5 14 . 0 13 .5 13.0 13 .0 13 .0
I
A. INmDOUCTIO N
lnihal reference MUST be made to tile introductory notes and limitations for the icyfslipperyor
conteminated take-of data In th.s sub-sectam, as appropriate.
1. Determine the runway state fo r tho planned depanure t.e. icy/slippery but nol contaminated,
standing water/slush or dry snow.
Z. Obtain the approprieto fi eld length, no rmally ur e lesser of the Take-all Run Available,
Emergen cy Distance or the Take-olf Dislence tusebrel quoted on me specilic icy/slippery or
contaminated RTOW table provided. Whore no specific table is provided use the lesser ofthe
Iake-olt Run Available, Emergency Oistence or the Take-off Oislance!Useble) quoted on the
normal performance ATOW toble in Section 1 or as detmed in Section 1.10.1. (G. 2 - 41.
3. Obta in the least favourable wind component and embienl lemporaturc. Take-offs in tailwinds
greater then !ikt are NOT permitted when using these generalised charts.
4. Enter with the appropriate lenglll into Sheet 1 ot me ·'TAKE·OH FROM ICY/SLI PPERY OR
CONTAMINATED RUNWAYS" charts in this section. Correct 'or runway slope and wind
component beforelransfering to Sheet 2 and 3 to extractthe PlTOW, associated speeds and
8 2 fo r the airfield pressure ellitud u, Note that the correction lor runway slope is always
unfavourable i.e. has the seme cttect whether uphill or downhill.
5. Correct the take-oft speeds and 8 2 for Actual Take-all Weight tess than PlTOW using the
normal procedures in Sections 1.1 . or 1.3. of this manual including correcting for Actual TOW
below 140,OOIlkg.
6. If any abnormal operations are being considered tha PLTOW and associated speeds found in
3. above should be ccnecred lot this before correcting lhe take-off speeds and 8 2 fot the
Actual TOW.
I.. . .:' , , nr
I' t ..
c...·1: n: j ~ '~f'
,:H, I, "
"i1i" , ""i"';·
. 'x' 'I t I
I " i; I"" ~ It, 1'1
" I t lit .. I
ii!j! I), ' :' ,
~
I:: L 1[ / I~} W" Y lid: ~. i I' mr:i
;: . 'it- I,"'j-; ..t, · .;" ,Wi i . , ' i'= . .lifl·
o·
::r "; o.
.",iH : ...
I : ~ 00' ill~tWI,J j , in:l tlI '..Wl ;fflt~' '~' F':'
f f .:
:"
.. ru r',
':"
, +41
'i i ~l
: :J1Hi
'1 , .. . i·'
,.": " _.,It .,,1:.tt:;.
,.:• +-..: it: . ' :: "11.' • ,.
. i.:
;..
t.,
i:# '1~'I'l
..i . ,IT:
~ti l
.. 1.
~ r;-";.1. .' •
:, :I' " L'P~'~r'Rjbw lraOb'b) Hi • 'If! ::if . it'iR,1
!H,li ,- fll'
8 r : - : - : - ' : --
i: ,:: :
11:,::, "... i'i I
~
" " ,.. " r
:.
ii ~. ~-<1'
::': 'C6
__ ':
, •••
.. 11'1"11
. ""I
'I., ~, .i:
."
'I' l:l Hi
_,11 . -'--1.
, ·F' ,I
.~. ',:,
*
1 1'i! i:~ ,.
.,Ui. ",' ' ji:,Ii:' , 'ii
':;1 if'!'! ill! :; HI [i1' '~if!f1 ' ,I; 'iP lit{ ,I, i' 1111
I·,
" ::",, !:
' ISI!
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AERODROME A
DATElTIME OF OBSERVATION
(Time of completion of measurement in UTCI B B B
RUNWAY DESIGNATOR C C C
CLEAREDRUNWAY LENGTH, IF LESS THAN PUBLISHEDLENGTH [m] D D D
CLEAREDRUNWAY WIDTH, IF LESSTHAN PUBLISHEDWIDTH (ml
If offset LEFTor RIGHT of centreline add 'L' or 'R' E E E
DEPOSITSOVERTOTAL RUNWAY LENGTH
(Observed on each third of the runway, starting from threshold having the lower
dosignation numbor)
NIL- ClEAR AND DRY
1- DAMP
2 - WET OR WATER PATCHES
3 - RIME OR FROSTCOVERED(depth normally loss than 1 mm)
4- DRY SNOW F F ·F
5-WETSNOW
6 - SLUSH
7-ICE
8 - COMPACTEDOR ROLLEDSNOW
9 - FROZENRUTS OR RIDGES
See Note 5 overleaf
MEAN DEPTHImm)FOR EACH THIRD OF TOTAL RUNWAY LENGTH G G G
BRAKING ACTION ON EACH THIRD OF RUNWAY AND MEASURING
EQUIPMENT
Measured or Calculated Coefficient or Estimated Braking Action
0·40 and above GOOD -5
0·39 to 0·36 MEDIUM/GOOD -4
0·35toO·30 MEDIUM -3
0·29 to 0·26 MEDIUM/POOR -2 H H H
0·25 and below POOR -1
9 - unreliable UNRELIABLE -9
IWhen quoting a measured coefficient use the observed two fi\luros, followod by
the abbreviation of the measured equipment used. When quotmg an estimate use
single digits).
CRITICALSNOWBANKS EXIST: IIf prosent, insert height (cml/distance from the
odge of runway Im) followed by 'L', 'R' or 'LR' if applicable J J J
RUNWAY LIGHTS, IIf obscured, insert 'YES' followod by 'L',
'R' or both 'LR' if applicable) K K K
FURTHERCLEARANCEIIf planned insert length Imllwidth (m) to be cleared
or if to full dimension, insort 'TOTAl') L L L
FURTHERClEARANCE EXPECTEDTO BE COMPLffiD BY ....IUTCI M M M
TAXIWAY.lif no appropriate taxiway is available, insert)'NO' N N N
TAXIWAY SNOWBANKS mmore than 6OCm, high distance apart in M P P P
APRON IIf unusable, indicated by 'NO' R
NEXT PLANNED OBSERVATION/MEASUREMENT IS FOR.....(day/
monthlhour in GMT) S
PlAIN LANGUAGE REMARKS. mrequired lo.g. sandingigrining carried out)T
SIGNATURE OF ORIGINATOR
(not for transmissionl
Notes
11I When reporting on two or three runways transmit Column 1 down to and including item P
then Column 2, then Column 3lif appropriate) and finish with items Rand Sand T
(2) Items together with their indicator must be dropped completely, where no information is to
be included.
(3) Metric units must be used and the unit of measurement not reported.
(4) The maximum validity of SNOTAM is 24 hours. New SNOTAM must be issued whenever
there is a significant change in conditions. The following changes relating to runway
conditions are considered as significant:
la) a change in the coefficient of friction of about .05
Ib) changes in depth of deposit greater than the following: 20 mm for dry snow, 10 mm for
wet snow; 3mm for slush;
Ic) a change in the available length or width of a runway of 10 per cent or more;
Id) any change in the type of deposit or extent of coverage which requires reclassification
in Items F or T of the SNOTAM;
le) When critical snow banks exist on one or both sides of the runway, any change in the
height or distance from centre line;
If) any change in the conspicuity of runway lighting caused by obscuring of the lights; and
Ig) any other conditions known to be significant according to experience or local
circumstances.
IS) Suitable combinations of these numbers may be used to indicate varying conditions over
runway segments. If more than one deposit is present on the same portion of the runway,
they shou/a be reported in sequence from the top to the bottom. Drifts, depths of deposits
appreciably greater than the average values, or other significant characteristics of the
deposits may be reported under item "T" in plain language.
(6) In the U.K. in conditions of slush or thin deposits of wet snow, the words 'Not Measured' will
be used in item 'H' at certain Aerodromes. The Mu-Metar will normally be used at
ABERDEEN, BELFAST,BENBECULA, BRISTOL,EAST MIDLANDS, EDINBURGH, GLASGOW,
INVERNESS, JERSEY,KIRKWALL, LEEDS,L1VERPOOL, LONDON IGATWICK & HEATHROW
& STANSTED), LUTON, MANCHESTER, NEWCASTLE, PRESTWICK, STORNOWAY,
SUMBURGH, TEES-SIDE & WICK for assessment of runway braking action, with the
decelerometer method as a back-up.IS
Use the following abbreviations to indicate the type of measuring equipment used:
DBV Diagonal Braked Vehicle SKH Skiddometer Ihigh pressure tire)
JBI James Brake Index SKL Skiddometer (Iow pressure tirel
MUM Mu-meter TAP Tapley-meter
SFT Friction Tester
PART 2
DECODE OF EIGHTFIGURE GROUP APPENDED TO ROUTINE MOTNElOPMET
The first two digits indicate the Runwav Designator.
The third digit indicates the Runwav Deposits.
The founh digit indicates the extent of runway contamination. .
The fifth and sixth digits indicate the depth 0 deposit.
The seventh and eighth (jigits indicate the friction co-efficient or Braking Action.
A RUNWAY DESIGNATOR
The two digits correspond to the Runwav Designator, e.l1. 09, 27, etc. In the case of parallel
runways the "left" runway is shown minus the l and the Right" runway has 50 added so that
OSR becomes 59 and 27R becomes 77. Whenever All runways are affected the figure group 88
will be used. (Note: 99 may sometimes appear as the first two digits. This does not purport to be
a runway indicator but means that the information is a repetition of the last message because
no new message has been received in time for transmission.)
B RUNWAY DEPOSITS
Expressed as single digits from 0 to 9, having the following meanings:
o . Clear and dry
1 • Damp
2 • Wet or water patches
3 - Rime or frost covered (Depth normallv less than 1 mm)
4· Dry snow
5· Wet snow
6· Slush
7 - Ice
8 • Compacted or rolled snow
9 - Frozen ruts or ridges
I - Tvpe of deposit not reponed (eg due to runway clearance in progress).
C EXTENT OF RUNWAY CONTAMINATION
The extent of runway contamination is expressed as a single digit in accordance with the
following scale:
1 - less than 10% of runway contaminated (covered)
2 - 11% to 25% of runway contaminated (covered)
5 - 26% to 50% of runway contaminated (covered)
9 - 51% to 100% of runway contaminated (covered)
I - not reported (eg due to runway clearance in progress).
D DEPTH OF DEPOSIT
Expressed as two digits thereafter the following
on the following scale. code should be used:
00 less than lmm 92 10cm
01 lmm 93 15cm
02 2mm 94 20cm
etc up to 95 25cm
10 lcm 96 30cm
15 1.5cm 97 35cm
20 2cm 98 40cm or more
etc upto 99 RIW or RlWs non-operational due to snow,
90 9cm slush. ice or large drifts, depth not measured.
(NOTE: Code figure 91 " • Depth of deposit operationally not significant
is NOT used) or not measureable.
Between code figures 92 and 98 the depth of
deposit can easily be determined by multiplying
the last digit by 5 e.g. 94 = 4 x 5 = 20
NOTE: The quoted depth is the mean of a number of readings or, if operationally significant, the
greatest depth measured.
UST OF AERODROMES FOR WHICH IT MAY BE EXPECTED THAT RUNWAY CONDmON REPORTS WIll BE
ADDED TO THE MOTNE/OPMET BROADCAST.
AALBORG BRUSSELS HAMBURG LYON/SAT OSTEND STUTIGART
AMSTERDAM BUCHAREST/O HANNOVER MADRID PARIs/COG TAMPERE
ANKARA BUDAPEST HELSINKI MALMO PARIs/ORLY TURIN
BASLE COLOGNE ISTANBUL MILANlL POZNAN TURKU
BELGRADE COPENHAGEN JONKOPING MILANlM PRAGUE VIENNA
BERGEN DRESDEN KLAGENFURT MOSCOWfS ROTIERDAM WARSAW
BERLlNfSCH'LD DUBLIN KRISTIANSAND MOSCOWN SAARBRUCKEN ZAGREB
BERLINITEMP'F DUSSELDORF LENINGRAD MUNICH SALZBURG ZURICH
BERLlNITEGEL FRANKFURT L1LLE NORKOPING SHANNON
BILLUND GENEVA LINZ NURNBERG SOFIA
BRATISLAVA GOTHENBURG WUBWANA OSLOfF STAVANGER
BREMEN GRAZ LUXEMBOURG OSLOIG STOCKHOLMlA
The following UK Airports may include runway condition reports in OPMET Broadcast bulletins
(also available in Continental Europe on MOTNE).
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8RmsH
AIRwAYS CONCORDE PERFORMANCE MANUAL GENERALISED
TAKE-OFF'
1.10. GENERALISED TAKE-OFF DATA
1.10.1 PROCEDURE FOR THE USE OF GENERALISED TAKE-OFF WEIGHT CHARTS
B. Employ the Generalised Take-Off Weight Charts to obtain the RTOW, Vt , VR, Vz speeds and
screen altitude 92 for runways where no Take-off Data Page has been provided, or where
restrictions in length of runway have occured for which a revised Take-off Data Page is not
available.
C. Determine the least favourable wind component employing the range of forecast wind
condi1ions expected at time of take-off. Take-off in tailwind conditions exceeding 101d. is not
permitted.
D. Enter the WAT curve with ambient temperature and pressure altitude and read off the
maximum weight to meet the Second Segment Climb Gradient Limit
N.B. This weight. even if not limiting, is required to derive 9 2 and also to check obstacle
clearance by use of WAT weight ratio (see below).
E. Enter the Generalised Tyre Speed Limited weight chart with the ambient temperature and
pressure altitude, correct for least favourable wind component and read off the maximum
weight to meet the tyre rolling speed limit.
F. Enter the Generalised Brake Energy Limited Take-off weight chart Sheet 1 with ambient
temperature and pressure altitude, and correct for the leastfavourable wind component to
read off a point onthetransfer scale. Transfer thisto sheet 2, correctfor overall runway slope
and read offthe maximum weight to meet themaximum Brake Energy capacity of the brakes.
G.
t, Enter the appropriate length into Sheet 1 of the Generalised Runway Take-off Weight
chart, for overall runway slope and least favourable wind component to read off a point
on the transfer scale. Transfer this to sheet 2. Enter Sheet 2 with ambient temperature
and pressure altitude and proceed vertically to the intersection with a horizontal drawn
from thevalue on the transfer scale. Interpolate to read the weight to meet the runway
requirement.
1.10.1 PROCEDURE FOR THE USE OF GENERALISED TAKE-OFF WEIGHT CHARTS (cont)
G. (cant)
2.Where noTake-off Data Page is available, or where a chartis available butthe runway is
restricted at the lift off end, the appropriate length is the available Take-off Run. A check
should then be made for obstacle clearance, in particular allowing for obstacles on any
unusable portion of the runway, by making use of the Generalised Obstacle Clearance
Chart in this Section.
3.Where aTake-off Data Page hasbeen provided and thetemperature range is inadequate,
the appropriate length is the lesser of the Take-off Distance Usable and the Emergency
Distance quoted atthetop of thepage. This will automatically ensure obstacle clearance.
4. Where a Take-off Data Page is provided and the runway is restricted at the start of the
take-off, deduct the restriction from the lesser of the Take-off Distance Usable and the
Emergency Distance quoted at the top of the page and enter with this value. This will
automatically ensure obstacle clearance.
H.The minimum value of the take-off weight determined in D., E., F. and G. above becomes the
PLTOW for take-off. No correction should be made for the difference between pressure
altitude and the geographical elevation of the airfield as pressure altitude will have been
employed for chart entry. Correct PLTOW as necessary for the effects of Dispatch
Oeviations/Special Operations as specified in Section 1.8.
N.B. The actual take-off weight must not exceed any of the following:
1. Corrected PLTOW.
I. Take-Off Speeds
Enter the V2 chartwith ambient temperature and pressure altitude and read off the
Engine Failed Screen Speed V2 appropriate to the PLTOW.
Enter the V1 DRY chart, Sheet 1 with Ambient temperature and Pressure Altitude.
Proceed vertically to the PLTOW and read off avalue ontheTransfer Scale. Transfer
this value to Sheet 2 and correct for least favourable wind component and runway
slope and read off V1 DRY.
1. Enter the Generalised WAT weight ratio graph with WAT weight obtained in D.
above and proceed horizontally to intersect a line corresponding to PLTOW. Drop
a vertical from this intersection to read the WAT weight ratio.
2. Enter the 3 engine screen attitude graph with WAT weight ratio and read off 82'
1. Establish distance and height of the obstacle relative to the lift-off end of the usable
Take-off run.
2. The obstacles that may require checking are those within an area. commencing at the
lift-off end of the usable Take-off run. initially 200m wide about the extended runway
centreline (i.e. lOOm each side) and increasing in width on each side byoneeighth of the
distance out from the lift-off end. ~
B. Enter the Generalised Runway Take-off weight chart with ambient temperature. pressure
altitude, PlTOW. wind component and runway slope to determine the required length.
C. If the required length obtained is lessthan Usable Take-off Run. increase the distance to the
obstacle by the distance between theses two distances. ~
D.
1. Enter the Generalised WAT curve with pressure altitude and ambient temperature and
extract the WAT weight.
2. With thisweight and PLTOW enter theWATweight ratiograph and obtain a value of WAT
weight ratio.
E. Enter the Generalised Obstacle Clearance chartwith the distance of the obstacle fromthe end
of the required length {from B.). Correct for wind component, WAT weight ratio (found in 0.1
and runway gradient and obtain the maximum permitted height of an obstacle that will be
cleared by 35ft. at that distance.
F.1f the maximum permitted height is less thanthe actual obstacle height then the PLTOW must
be reduced until clearance is assured.
Actual Take-off weight must never exceed the Maximum Structural TOW.
VR 185kt.
.~
Vz 207kt.
V, DRY 165kt.
V, WET = 159kt.
From Table 1, Vz correction is zero. Now Actual TOW is 155.000kg giving a difference from
PlTOW of 12.50Dkg.
From Table 2.
VR difference -3kt
V, difference = -9kt
9 2 difference + 1.0"
Vz 207-0 207kt
~
VR = 185-3 182kt
92 13.8+1.0 14.8°
Obstacle at height 120ft at 140Dm from end of runway. Entering with PLTOW in the Generalised
Runway Take-off Weight chartextract the appropriate lengths. In this example the PLTOW was
limited by runway length and the appropriate length is 3100m. Distance of obstacle from end of
required length is given by (Runway length - appropriate length + obstacle distance from
runway endl,
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Rev: 1.10.7. DEC 90/01
8RmsH
AIRwAYS CONCORDE PERFORMANCE MANUAL GENERALISED
TAKE-OFF
GENERALISED TYRE SPEED LIMITED WEIGHT
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Rev: 1.10.11. DEC 90/01
CONCORDE PERFORMANCE MANUAL GENERALISED
TAKE-OFF
GENERALISED RUNWAY TAKE-OFF CHART 1
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CONCORDE PERFORMANCE MANUAL GENERALISED
LANDING
1.11. GENERALISED LANDING DATA
1.11.1 INTRODUCTION
~ This section provides generalised landing data required to schedule landings at the flight
planning stage or in flight. The data may be used when no runway specific landing data is
available, where a restriction in length has occurred or when a dispatch deviation applies.
Advisory information is provided for landing onslippery runways. It is based onapproach at VREF
and assumes the use of maximum reverse thrust. It should be used when intending to land on
runways considered icy/slippery or contaminated.
N.B. With any unserviceability affecting the stopping performance of the aircraft landing on
icylslippery or contaminated runways should be avoided asthe landing distance is likely
to exceed any runway length available.
Observe the following:
E. Runway clearance, The minimum acceptable cleared width for landing is 30m (100ft).
A. Enter the appropriate Generalised landingDistance Chart with landingDistance Available (or
effective LOA if a DDM item applies]. Correct for wind,slope and airfield pressure altitude to
obtain a Runway limited landing landing Weight.
B. Enter the appropriate Maximum Landing Weight (WAT Limit) Chart with landing ambient
temperature and correct for airfield pressure altitude to obtain a WAT Limited Landing . j
Weight ""'"
C. The Performance Limited Landing Weight is the lower or the Runwav Limited and the WAT
Limited Landing Weight.
D. Regulated landing Weight is the lower of the Performance limited Landing Weight and the
Maximum Authorised Landing Weight
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.. ..
'. -- .
... . ....-....----.... -. ......-.
~
: ~::: ::.: : ' , ' ,
. -.
,.
·• ---+-- .. . . .. ... - -
..~ l,
--.... ......, ......... .......... _ •• , ._ • . •
.:-:: ..,:.:.
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, .: -+ :... .
-~..
~...
...
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i.)
.. ~------~
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"v
BRITISH
CONCORDE PERFORMANCE MANUAl TAKE.QFF DATA
AulwAYS
ALTERNATES AND CHARTERS
LEFT
BLANK
:vs CONCORDE TAKE-OFF DATA BANGOR
AID Elev 192ft
FULL LENGTH RWY 15
CLG Nil RVR/VIS 60Oft* SLOPE 0.25%DN
TOR 3486m (11437ft) ED 3760m (12336ft) TOO 3760m (12336ft)
\.. OAT 1Gkt lne 5kt Inc snu, Inc 10kt Inc 20kt Inc 3Gkt
~ "C TAIL Ikt TAIL lid AIR lid HEAD lid HEAD lid HEAD
39 161.9 0.8 165.9 0.8 169.8 0.2 172.2 0.2 174.6 0.2 1n.0
154/179 160/184 165/187 169/190 173/194 177/197
36 163.9 0.8 167.9 0.8 171.8 0.2 174.3 0.2 176.7 0.2 179.2
154/180 159/186 165/188 169/191 173/195 177/198
33 165.7 0.8 169.8 0.8 173.8 0.2 176.3 0.2 178.8 0.2 181.3
153/180 159/186 165/189 169/192 172/196 176/199
30 167.6 0.8 171.7 0.8 175.7 0.3 178.3 0.2 180.8 0.2 183.3
153/181 159/187 165/191 168/193 172/197 176/200
27 169.4 0.8 173.6 0.8 177.6 0.3 180.3 0.2 182.8 0.2 185.3
153/182 159/188 164/192 168/194 172/197 176/201
24 171.2 0.8 175.4 0.8 179.5 0.3 182.2 0.2 184.7 0.3 187.3
153/182 159/189 164/192 168/195 172/198 176/202
\.
"'"-" 21 172.9 0.8 177.1 0.8 181.3 0.3 184.1 0.2 186.6 0.3 189.3
153/183 159/189 164/193 168/196 172/199 176/203
18 174.5 0.9 178.8 0.9 183.1 0.3 185.9 0.3 188.5 0.3 191.2
153/184 159/190 164/194 168/196 172/200 176/203
15 176.1 0.9 180.5 0.9 184.8 0.3 187.6 0.3 190.3 0.3 193.0
153/184 159/190 164/196 168/197 172/200 176/204
12 1n.4 0.9 181.8 0.9 186.2 0.3 189.0 0.3 191.7 0.3 194.4
153/185 159/191 165/196 168/198 172/201 176/205
9 178.0 0.9 182.4 0.9 186.7 0.3 189.5 0.3 192.1 0.3 194.8
154/186 159/192 165/196 169/199 173/202 1n/205
6 178.6 0.9 183.0 0.8 187.2 0.3 189.9 0.3 192.6 0.2 195.0
154/187 1601193 166/196 170/199 174/203 178/206
3 179.1 0.9 183.4 0.9 187.7 0.3 190.4 0.3 193.0 0.2 195.0
155/188 1611193 167/196 1711200 1751203 178/206
0 179.6 0.9 183.9 0.9 188.2 0.2 190.7 0.3 193.4 0.2 195.0
156/189 162/194 168/197 172/200 176/204 179/207
-3 180.1 0.8 184.3 0.8 188.5 0.3 191.1 0.3 193.7 0.1 195.0
157/190 162/194 168/198 1731201 177/205 180/207
V2= VR+ 21 VR+ 21 VR+ 21 VR+ 21 VR+ 21 VR+21
82= 13.5 13.5 13.0 13.0 13.0 12.5
1.Vl WET SPEED: Vl WET IS Vl DRY minus 15kt.
2.*Tak&-Off Minima: Where RVR/VIS is shown as 0.5sm 1240001 orless,higher minima may apply if
anyradio orvisual aids areunserviceable. See para 1.1.5 onPage 1.1.3.
2. *Tu.off Minima: Where RVRIVIS is shown asO.5sm 1240Oft) orless. higher minima may apply if ~
any radio orvisual aids are unserviceable. See para 1.1.5 onPage 1.1.3.
2.-Take-Off Minima: Where RVR/VIS is shown as 0.5sm (24000) orless, higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5 onPage 1.1.3.
2.*TaJce.Off Minima: Where RVRIVIS is shown as 0.5sm (24000) orless, higher minima may apply if ~
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
2.-Take-Off Minima: Where RVR/VIS is shown as 0.5sm (240Oft) orless, higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5 onPage 1.1.3.
4. Shipping: This data covers masts upto 60ftAMSL inthe shipping channel 679ft from theend ofTOR.
2.·TaJce.Off Minima: Where RVR/VIS is shown asO.5sm (240Oft) orless, higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
4. Shipping: This data covers masts upto 60ftAMSL inthe shipping channel 600ft from the end ofTOR.
2. ·Take-Off Minima: Where RVR/VIS is shown as0.5sm (240001 orless, higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
4. Shipping: This data assumes no shipping ispresent inthe shipping channel 561ft from the end ofTOR.
If shipping is present use data on page 80S/04.
Rev:(20/03/96) Section 1.12. 80S/03 MAR 96/01
=ys CONCORDE
AID Bev 20ft
TAKE·OFFDATA BOSTON
SHIPPING - 60ft
FULL LENGTH RWY 09
CLG Nil RVR/VIS 600ft· SLOPE O.04%DN
TOR 2134m (7001ft) EO 2134m (7001ft) TOO 2134m (7001ft)
OAT 101ct lne 5kt Ine STILL Ine 101ct Ine 201et Ine 301et
"C TAIL Ikt TAIL IIet AIR Ikt HEAD IIet HEAD Ikt HEAD
39 117.8 2.0 127.9 1.2 134.1 0.3 137.6 0.3 141.0 0.3 144.3
132/140 134/148 138/153 141/156 145/158 148/160
36 119.7 1.9 129.3 1.3 135.6 0.4 139.2 0.3 142.6 0.3 146.0
132/142 135/149 139/154 142/157 145/159 148/161
33 121.6 1.8 130.7 1.3 137.0 0.4 140.7 0.3 144.2 0.3 147.7
132/143 135/150 139/155 142/157 145/160 148/162
30 123.5 1.7 132.1 1.3 138.4 0.4 142.2 0.3 145.7 0.4 149.3
132/144 135/151 139/155 142/158 146/161 149/163
27 125.5 1.6 133.4 1.3 139.8 0.4 143.7 0.4 147.3 0.3 150.8
132/145 136/151 140/156 143/159 146/162 149/164
24 127.4 1.4 134.6 1.3 141.1 0.4 145.1 0.4 148.7 0.4 152.4
132/147 136/152 140/157 143/160 146/162 149/165
21 129.4 1.3 135.8 1.3 142.4 0.4 146.5 0.4 150.1 0.4 153.8
132/148 136/153 141/158 143/161 147/163 150/166
18 130.6 1.3 137.0 1.3 143.6 0.4 147.9 0.4 151.5 0.4 155.3
132/149 137/153 141/158 144/161 147/164 150/166
15 131.7 1.3 138.1 1.3 144.8 0.4 149.1 0.4 152.8 0.4 156.6
133/149 137/154 141/159 144/162 147/165 151/167
12 132.7 1.3 139.2 1.3 145.9 0.4 150.3 0.4 154.0 0.4 157.8
133/150 137/155 142/160 145/163 148/165 151/168
9 133.7 1.3 140.2 1.4 147.0 0.4 151.1 0.4 154.8 0.4 158.6
133/150 138/155 142/160 145/163 148/166 152/168
6 134.6 1.3 141.2 1.4 148.0 0.4 151.9 0.4 155.6 0.4 159.3
134/151 138/156 143/161 146/163 149/166 152/168
3 135.5 1.3 142.1 1.4 149.0 0.4 152.6 0.4 156.4 0.4 160.0
134/151 139/156 143/161 146/164 150/166 153/169
0 136.4 1.3 143.0 1.3 149.6 0.4 153.3 0.4 157.1 0.4 160.7
135/152 139/157 144/161 147/164 150/167 154/169
-3 137.2 1.3 143.9 1.3 150.3 0.4 154.0 0.4 157.7 0.4 161.3
135/152 140/157 144/162 148/164 151/167 154/169
V2= VR+ 33 VR+30 VR+ 28 VR+ 27 VR+ 26 VR+ 25
82= 16.5 16.0 15.5 15.5 15.0 15.0
1. VI WET SPEED: VI WET isVI DRY minus 15kt.
2. -Take-Off Minima: Where RVR/VIS is shown as0.5sm (240Oft) orless, higher minima may apply if ~
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
4.Shipping: This data covers masts upto 60ft AMSlinthe shipping channel 561ft from theend ofTOR.
If noshipping is present in channel use data on page BOS/03.
2.·Taku-Off Minima: Where RVR/VIS is shown as0.5sm 12400ftl orless. higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5 onPage 1.1.3.
4. Shipping: This data covers masts upto 60ft AMSlintheshipping channel 5118ft from theend ofTOR.
For masts upto 176ft use data onpage BOS/06.
2.·Take-Off Minima: Where RVR/VIS is shown as0.5sm 12400ftl orless, higher minima may apply if ~
any radio orvisual aids are unserviceable. See para 1.1.5 onPage 1.1.3.
4. Shipping: This data covers masts upto 176ft AMSlinthe shipping channel 5118ft from theend of
TOR. For masts upto 60ftuse data onpage BOS/05.
2.*TaJce.Off Minima: Where RVR/VIS is shown as 0.5sm (240OftI orless, higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
4. Shipping: This data covers masts upto 60ft AMSL inthe shipping channel 1529ft from theend ofTOR.
For masts upto 176ft use data onpage BOS/08.
2.-Tak.cJff Minima: Where RVR/VIS is shown as 0.5sm (240Oft) orless, higher minima may apply if ~
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
4. Sbipping: This data covers masts upto 176ft AMSl inthe shipping channel 1529ft from the end of
TOR. For masts up to 60ftuse data on page BOS/07.
BOS/08 MAR 96/01 Section 1.12. Rev:(20103/96)
:vs CONCORDE TAKE-OFF DATA BOSTON
AID 8ev 20ft SHIPPING - 60ft
FULL LENGTH RWY 22R
CLG NIL RVR/VIS O.25sm* SLOPE O.01%DN
TOR 2396m (7861ft) EO 2971m (9747ft) TOO 2396m (7861ftl
OAT 1Gb Ine 5kt lne STILL Ine 10kt lne 2Gkt Ine 30kt
t TAIL /kt TAIL Jkt AIR Jkt HEAD Jkt HEAD /Iet HEAD
39 137.1 1.1 142.7 1.2 148.6 0.4 152.6 0.4 156.8 0.3 160.1
153/155 157/159 161/163 164/166 166/169 169/172
36 138.6 1.1 144.3 1.2 150.3 0.4 154.4 0.4 158.6 0.3 162.1
153/156 157/160 161/164 164/167 167/170 170/173
33 140.2 1.2 146.0 1.2 152.0 0.4 156.1 0.4 160.4 0.4 164.0
153/157 158/161 162/165 164/168 167/171 170/174
30 141.7 1.2 147.5 1.2 153.6 0.4 157.8 0.4 162.1 0.4 165.9
154/158 158/162 162/166 165/169 168/172 171/175
27 143.2 1.2 149.1 1.2 155.2 0.4 159.4 0.4 163.8 0.4 167.7
154/159 158/163 163/167 165/170 168/173 171/176
24 144.6 1.2 150.5 1.2 156.7 0.4 161.0 0.4 165.4 0.4 169.6
154/159 159/164 163/168 166/171 168/174 171/177
21 146.0 1.2 152.0 1.2 158.2 0.4 162.6 0.4 167.0 0.4 171.3
155/160 159/164 163/169 166/171 169/174 172/177
18 147.3 1.2 153.3 1.3 159.7 0.4 164.0 0.4 168.5 0.5 173.1
155/161 160/165 164/169 167/172 169/175 172/178
15 148.6 1.2 154.7 1.3 161.0 0.4 165.5 0.4 170.0 0.5 174.6
156/162 160/166 164/170 167/173 170/176 172/179
12 149.8 1.2 155.9 1.3 162.4 0.4 166.8 0.5 171.4 0.5 176.1
156/162 160/167 165/171 167/174 170/177 173/180
9 151.0 1.2 157.2 1.3 163.7 0.4 168.2 0.5 172.8 0.4 176.8
157/163 161/167 165/171 168/174 171/177 174/181
6 152.1 1.2 158.3 1.3 164.9 0.4 169.4 0.5 174.0 0.3 177.4
157/163 161/168 166/172 168/175 171/178 175/182
3 153.2 1.3 159.5 1.3 166.1 0.4 170.6 0.4 175.1 0.3 178.1
157/164 162/168 166/173 169/176 172/179 175/183
0 154.1 1.3 160.5 1.3 167.1 0.4 171.6 0.4 175.7 0.3 178.7
158/165 162/169 167/173 170/176 173/179 176/184
·3 155.1 1.3 161.5 1.3 168.1 0.4 172.6 0.4 176.2 0.3 179.3
159/165 163/169 167/174 170/177 173/180 177/184
V2= VR+ 27 VR+ 25 VR+ 24 VR+ 22 VR+22 VR+ 21
92= 15.5 15.0 14.5 14.5 14.0 13.5
1.V1 WET SPEED: Vl WET IS Vl DRY minus 15kt
2.*Take-Off Minima: Where RVRIVIS is shown as 0.5sm (240Oftj orless. higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5 on Page 1.1.3.
4.Shipping: This data covers masts upto 60ft AMSL intheshipping channel 3219ft from theend ofTOR.
For masts upto 176ft use data on page BOSll0.
2. -Take-Off Minima: Where RVRMS is shown as0.5sm (24000) orless, higher minima may apply if ~
any radio orvisual aids are unserviceable. See para 1.1.5 onPage 1.1.3.
4. Shipping: This data covers masts upto 176ft AMSlin theshipping channel 3219ft from the end of
TOR. For masts up to 60ft use data onpage BOS/09.
BOS/l0 MAR 96/01 Section 1.12. Rev:120/03/961
=:8 CONCORDE
AID Bev 20ft
TAKE-OFF DATA BOSTON
SHIPPING - 60ft
FULL LENGTH RWY 27
CLG 900ft RVR/VIS lsm SLOPE O.04%UP
TOR 2134m (700lft) EO 2674m (8773ft) TOO 2134m (700lft)
OAT 101et lne 5kt Ine STILL Ine 101et Ine 201et lne 301et
-c TAIL /Iet TAIL /Iet AIR Ikt HEAD /Iet HEAD /Iet HEAD
39 127.5 1.1 133.0 1.1 138.7 0.4 142.7 0.4 146.7 0.4 150.9
148/148 152/152 156/157 159/159 162/162 164/165
36 129.0 1.1 134.6 1.2 140.4 0.4 144.3 0.4 148.4 0.4 152.6
148/149 152/153 157/157 159/160 162/163 165/166
33 130.5 1.1 136.1 1.2 141.9 0.4 146.0 0.4 150.1 0.4 154.3
148/150 153/154 157/158 160/161 162/164 165/167
30 131.9 1.1 137.6 1.2 143.5 0.4 147.5 0.4 151.7 0.4 156.0
149/151 153/155 157/159 160/162 163/165 166/168
27 133.2 1.2 139.0 1.2 144.9 0.4 149.1 0.4 153.3 0.4 157.6
149/151 153/156 158/160 160/163 163/166 166/169
24 134.6 1.2 140.4 1.2 146.4 0.4 150.5 0.4 154.8 0.4 159.2
149/152 154/156 158/161 161/164 164/167 166/169
21 135.8 1.2 141.7 1.2 147.8 0.4 152.0 0.4 156.3 0.4 160.7
150/153 154/157 158/161 161/164 164/167 167/170
18 137.1 1.2 143.0 1.2 149.1 0.4 153.3 0.4 157.7 0.4 162.2
150/153 155/158 159/162 162/165 165/168 167/171
15 138.3 1.2 144.2 1.2 150.4 0.4 154.7 0.4 159.1 0.4 163.6
150/154 155/158 159/163 162/166 165/169 168/172
12 139.4 1.2 145.4 1.2 151.6 0.4 156.0 0.4 160.4 0.4 164.9
151/155 155/159 160/164 163/167 165/169 168/172
9 140.5 1.2 146.5 1.3 152.8 0.4 157.2 0.4 161.7 0.4 166.2
151/155 156/160 160/164 163/167 166/170 169/173
6 141.5 1.2 147.6 1.3 154.0 0.4 158.4 0.4 162.9 0.5 167.5
152/156 156/160 161/165 164/168 166/171 169/174
3 142.5 1.2 148.7 1.3 155.1 0.4 159.5 0.4 164.0 0.5 168.7
152/156 157/161 161/165 164/168 167/171 170/174
0 143.5 1.2 149.7 1.3 156.1 0.4 160.6 0.4 165.1 0.5 169.8
153/157 157/161 162/166 165/169 167/172 170/175
-3 144.4 1.2 150.6 1.3 157.1 0.4 161.6 0.5 166.2 0.5 170.9
153/158 158/162 162/166 165/170 168/173 171/176
V2= VR+30 VR+ 28 VR+ 26 VR+ 25 VR+ 24 VR+23
02= 16.0 16.0 15.5 15.0 14.5 14.5
1.V1 WET SPEED: V1 WET IS Vl DRY minus 15kt.
3.Shipping: This data covers masts upto 60ft AMSL in theshipping channel 2021 ft from theend ofTOR.
For masts upto 116ft use data on page BOS/12.
3.Shipping: This data covers masts upto 176ft AM8L intheshipping channel2021ft from the end of
TOR. For masts upto 60ft use data on page B08/11.
OAT 10kt Ine 5kt Ine STILL Ine 10kt Ine 20kt Ine 30kt
"C TAIL /Iet TAIL !Iet AIR /Iet HEAD !Iet HEAD !Iet HEAD
39 150.8 0.8 154.6 0.8 158.5 0.3 161.1 0.3 163.7 0.3 166.5
149/165 154/170 159/175 163/178 166/182 170/185
36 152.6 0.8 156.5 0.8 160.4 0.3 163.0 0.3 165.7 0.3 168.5
150/166 155/171 160/176 163/179 167/183 170/185
33 154.4 0.8 158.3 0.8 162.3 0.3 164.9 0.3 167.6 0.3 170.5
150/167 155/172 160/177 163/180 167/184 170/186
30 156.1 0.8 160.1 0.8 164.1 0.3 166.8 0.3 169.6 0.3 172.4
150/168 155/173 160/178 164/181 167/185 171/187
27 157.8 0.8 161.8 0.8 165.9 0.3 168.6 0.3 171.4 0.3 174.3
151/169 156/173 161/179 164/182 168/185 171/188
24 159.5 0.8 163.6 0.8 167.7 0.3 170.4 0.3 173.2 0.3 176.2
151/170 156/174 161/180 165/183 168/186 171/189
21 161.1 0.8 165.2 0.8 169.4 0.3 172.2 0.3 175.0 0.3 178.0
151/171 156/174 161/181 165/183 168/187 172/190
18 162.6 0.9 166.9 0.8 171.1 0.3 173.9 0.3 176.8 0.3 179.7
152/171 157/175 162/180 165/184 169/188 172/192
15 164.1 0.9 168.4 0.9 172.7 0.3 175.5 0.3 178.4 0.3 181.4
152/172 157/176 162/181 166/185 169/188 173/193
12 165.4 0.9 169.7 0.8 173.9 0.3 176.8 0.3 179.7 0.3 182.8
152/173 158/177 163/182 166/185 170/189 173/194
9 166.0 0.8 170.2 0.9 174.5 0.3 177.4 0.3 180.3 0.3 183.3
153/173 158/178 164/184 167/187 171/190 174/193
6 166.5 0.8 170.7 0.9 175.0 0.3 177.9 0.3 180.8 0.3 183.8
154/173 159/178 164/184 168/187 171/191 175/194
3 167.0 0.8 171.2 0.9 175.5 0.3 178.4 0.3 181.3 0.3 184.4
155/173 160/179 165/185 169/188 172/192 176/195
0 167.5 0.8 171.6 0.9 176.0 0.3 178.8 0.3 181.8 0.3 184.8
155/174 161/179 166/185 170/189 173/192 177/195
-3 167.9 0.8 172.0 0.9 176.4 0.3 179.2 0.3 182.2 0.3 185.1
156/175 162/180 167/186 170/190 174/192 178/195
V2= VR+ 23 VR+ 23 VR+ 22 VR+ 22 VR+22 VR+ 22
92= 14.5 14.0 14.0 13.5 13.5 13.5
t. V1 WET SPEED: Vl WET IS Vl DRY mmus 15kt.
2.*Take-Off Minima: Where RVR/VIS is shown as 0.5sm (24000) orless, higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5 onPage 1.1.3.
4.Shipping: This data covers masts upto 60ftAMSL inthe shipping channel 1388ft from theend of TOR.
LEFT
BLANK
~=s CONCORDE TAKE-OFF DATA BRIZE NORTON
AID Elev 288ft
FULL LENGTH RWY 08
CLG Nil RVR/VIS 200m SLOPE O.36%DN
TOR 3050m (10007ft) ED 3248m (10656ft) TOD 3068m (10066ft)
OAT 10kt Ine Skt lne STILL Ine 10kt Ine ZOkt Ine 30kt
-C TAIL Ikt TAIL Ikt AIR Ikt HEAD IIet HEAD Ikt HEAD
39 153.5 0.9 158.0 0.8 161.9 0.3 164.5 0.3 167.1 0.3 169.8
152/167 156/171 162/177 165/181 168/185 172/189
36 155.4 0.9 159.9 0.8 163.9 0.3 166.5 169.2 0.3
0.3 171.9
152/168 157/172 162/178 165/182 169/186 172/190
33 157.1 0.9 161.8 0.8 165.8 0.3 168.4 0.3 171.2 0.3 173.9
152/169 157/173 162/179 166/183 169/187 172/191
30 158.8 1.0 163.7 0.8 167.7 0.3 170.4 0.3 173.1 0.3 175.9
153/170 158/173 1631179 166/183 169/187 173/192
27 160.5 1.0 165.5 0.8 169.5 0.3 172.3 0.3 175.0 0.3 177.9
153/171 158/174 1631180 166/184 170/188 173/192
24 162.1 1.0 167.2 0.8 171.4 0.3 174.1 0.3 176.9 0.3 179.8
154/172 158/175 163/181 167/185 170/189 173/193
21 163.6 1.0 168.8 0.9 173.1 0.3 175.9 0.3 178.7 0.3 181.7
154/172 159/176 164/182 167/186 171/190 174/194
18 165.1 1.1 170.4 0.9 174.8 0.3 177.7 0.3 180.5 0.3 183.5
154/173 159/177 164/182 168/186 171/190 174/194
15 166.6 1.1 171.9 0.9 176.5 0.3 179.3 0.3 182.2 0.3 185.2
155/174 160/177 165/183 168/187 171/191 175/195
12 167.8 1.1 173.2 0.9 177.8 0.3 180.6 0.3 183.6 0.3 186.6
155/175 160/178 165/183 169/187 172/192 1751196
9 168.8 1.1 174.1 0.9 178.4 0.3 181.2 0.3 184.2 0.3 187.2
I
156/175 161/178 166/185 169/189 173/193 176/197
~ 6 169.7 1.0 174.6 0.9 178.9 0.3 181.8 0.3 184.7 0.3 187.7
157/175 162/180 167/186 170/190 174/194 177/198
3 170.5 0.9 175.1 0.9 179.4 0.3 182.3 0.3 185.2 0.3 188.1
157/176 162/181 168/187 171/191 175/195 178/199
0 171.2 0.9 175.6 0.9 179.9 0.3 182.8 0.3 185.7 0.3 188.6
158/176 163/182 168/188 172/192 1751196 179/200
-3 171.9 0.8 176.0 0.9 180.3 0.3 183.2 0.3 186.1 0.3 188.9
159/177 164/183 169/189 173/193 176/197 180/201
V2= VR+ 22 VR+ 21 VR+ 21 VR+ 21 VR+ 21 VR+ 21
92= 14.0 14.0 13.5 13.5 13.0 13.0
1.Vt WET SPEED: Vl WET IS VI DRY mmus 15kt.
2.·Runway Availability: Rwy 16/34 authorised for use in DAY UGHT and VMC only.
2. *Runwil'fAvailability: Rwy16/34 authorised for use in DAY LIGHT and VMC only.
12 151.0 1.7 159.6 1.1 165.3 0.4 169.2 0.4 173.2 0.3 175.9
132/163 135/169 140/173 143/176 146/178 150/182
9 153.2 1.5 160.8 1.1 166.5 0.4 170.5 0.3 173.9 0.3 176.6
132/165 136/170 140/174 144/176 147/179 150/183
6 155.4 1.3 161.9 1.2 167.7 0.4 171.7 0.3 174.6 0.3 177.3
132/166 136/170 141/174 144/177 148/180 151/184
3 157.2 1.1 162.9 1.2 168.8 0.4 172.5 0.3 175.2 0.3 178.0
132/167 137/171 141/175 145/178 148/181 152/185
0 158.2 1.1 163.9 1.2 169.8 0.3 173.2 0.3 175.8 0.3 178.6
133/168 137/172 142/175 145/178 149/182 152/186
-3 159.1 1.2 164.9 1.2 170.8 0.3 173.7 0.3 176.4 0.3 179.1
133/168 138/172 142/176 146/179 150/183 153/187
V2= VR+ 26 VR+23 VR+22 VR+ 21 VR+ 21 VR+ 21
82= 15.5 14.5 14.0 14.0 13.5 13.5
1.V1 WET SPEED: Vl WET IS V1 DRY minus 15kt.
21 136.0 1.5 143.3 1.2 149.1 0.4 153.0 0.4 156.9 0.4 160.7 ~
132/153 136/158 140/162 143/165 146/168 150/170
18 138.1 1.3 144.5 1.2 150.4 0.4 154.4 0.4 158.3 0.4 162.1
132/154 136/159 141/163 144/166 147/169 150/171
15 139.5 1.2 145.7 1.2 151.7 0.4 155.7 0.4 159.6 0.4 163.6
132/155 137/160 141/164 144/167 147/169 150/172
12 140.6 1.2 146.8 1.2 152.9 0.4 156.9 0.4 160.9 0.4 164.8
133/156 137/160 142/164 145/167 148/170 151/172
9 141.6 1.3 147.9 1.2 153.8 0.4 157.9 0.4 161.8 0.4 165.7
133/156 138/161 142/165 145/168 148/170 151/173
6 142.6 1.3 148.9 1.2 154.8 0.4 158.8 0.4 162.7 0.4 166.6
133/157 138/161 143/165 146/168 149/171 152/173
3 143.6 1.2 149.7 1.2 155.7 0.4 159.7 0.4 163.5 0.4 167.3
134/157 138/162 143/166 146/169 149/171 153/174
0 144.5 1.2 150.5 1.2 156.5 0.4 160.5 0.4 164.3 0.4 168.1
134/158 139/162 144/166 147/169 150/172 153/174
-3 145.4 1.2 151.3 1.2 157.3 0.4 161.2 0.4 165.0 0.4 168.7
135/158 140/163 144/167 147/169 151/172 154/174
V2= VR+ 30 VR+ 27 VR+26 VR+ 25 VR+ 24 VR+23
820: 15.0 15.5 15.0 15.0 14.5 14.5
1.VI WET SPEED: Vl WET IS VI DRY minus 15kt.
l
'-'
'-' 2.Runway Surface: Rwy 141/32R liable to be slippery when wet only on rubber deposits.
2.Runway Surface: Rwy 141J32R liable to be slippery when wetonly onrubber deposits. ~
""" V2=
92=
156/171
VR+ 23
14.5
161/175
VR+ 22
14.0
166/180
VR+ 21
14.0
170/184
VR+ 21
13.5
173/188
VR+ 21
13.5
177/192
VR+20
13.5
1.V1 WET SPEED: V1 WET IS Vl DRY minus 15kt.
2.-Take-Off Minima: Where RVRNIS isshown as 0.5sm (24000) orless, higher minima may apply if
any radio orvisual aids areunserviceable. Seepara 1.1.5. on Page 1.1.3.
2.·Take-Off Minima: Where RVR/VIS is shown as0.5sm 1240001 orless, higher minima may apply if
any radio orvisual aids are unserviceable. See para 1.1.5. onPage 1.1.3.
, 21 161.1 1.1 166.6 0.9 171.3 0.3 174.2 0.3 177.1 0.3 180.1
146/171 150/174 155/179 158/183 162/187 165/191
18 162.6 1.1 168.1 1.0 173.0 0.3 175.9 0.3 178.8 0.3 181.8
146/172 151/175 155/180 159/184 162/188 166/192
15 164.0 1.1 169.6 1.0 174.6 0.3 177.5 0.3 180.5 0.3 183.5
146/172 151/176 156/180 159/184 163/188 166/192
12 165.3 1 .1 170.9 1.0 175.9 0.3 178.8 0.3 181.8 0.3 184.9
147/173 152/177 156/181 160/185 163/189 167/193
9 166.3 1.1 171.8 1.0 176.6 0.3 179.5 0.3 182.5 0.3 185.6
148/173 152/177 157/182 161/186 164/190 167/194
6 167.2 1.1 172.8 0.9 177.2 0.3 180.2 0.3 183.2 0.3 186.3
148/174 153/177 158/183 161/187 165/191 168/195
3 168.1 1.1 173.4 0.9 177.9 0.3 180.8 0.3 183.8 0.3 186.9
149/174 153/178 159/184 162/188 166/192 169/196
0 169.0 1.0 174.0 0.9 178.5 0.3 181.4 0.3 184.4 0.3 187.5
149/175 154/179 159/185 163/189 166/193 170/197
·3 169.7 1.0 174.5 0.9 179.0 0.3 181.9 0.3 184.9 0.3 188.0
150/175 155/180 160/186 164/190 167/194 171/198
V2= VR+ 22 VR+ 21 VR+ 21 VR+ 21 VR+ 21 VR+ 21
92= 14.0 14.0 13.5 13.5 13.5 13.0
1. V1 WETSPEED: V1 WET IS VI DRY minus 15kt.
"'-'
42 157.7 0.8 161.5 0.7 165.2 0.2 167.6 0.2 170.0 0.2 172.3
150/182 156/187 161/193 165/197 169/200 173/204
39 159.6 0.7 163.3 0.7 166.9 0.2 169.3 0.2 171.7 0.2 174.1
150/183 155/188 161/193 165/197 169/201 172/204
36 161.2 0.7 164.9 0.7 168.6 0.2 171.1 0.2 173.5 0.2 175.8
150/183 155/188 161/194 165/197 168/201 172/205
33 162.8 0.7 166.5 0.7 170.2 0.2 172.7 0.2 175.2 0.2 177.5
150/183 155/189 161/194 165/198 168/202 172/205
30 164.4 0.7 168.1 0.7 171.8 0.3 174.4 0.2 176.9 0.2 179.3
149/184 155/189 161/195 165/198 168/202 172/206
27 165.9 0.8 169.7 0.8 173.5 0.3 176.1 0.2 178.6 0.2 181.0
1491184 155/190 161/195 1651199 168/202 172/206
24 167.5 0.8 171.3 0.8 175.1 0.3 177.7 0.3 180.3 0.2 182.8
149/185 155/190 1611196 165/199 168/203 172/207
21 169.0 0.8 172.9 0.8 176.7 0.3 179.4 0.3 182.0 0.2 184.5
150/185 155/191 161/196 165/200 168/204 172/207
18 170.6 0.8 174.4 0.8 178.4 0.3 181.0 0.3 183.7 0.2 186.2
150/186 155/191 161/197 165/200 168/204 172/208
15 172.0 0.8 175.9 0.8 179.9 0.3 182.5 0.3 185.2 0.2 187.7
150/186 1551192 161/197 165/201 1681205 172/208
12 173.1 0.8 177.0 0.8 181.0 0.3 183.6 0.3 186.3 0.3 188.9
1501187 156/192 161/198 165/202 169/205 1731209
9 173.6 0.8 177.5 0.8 181.5 0.3 184.2 0.3 186.8 0.2 189.3
151/188 156/193 162/199 166/203 170/206 173/210
6 174.1 0.8 178.1 0.8 182.1 0.3 184.8 0.3 187.4 0.2 189.9
151/189 157/194 163/200 1671203 170/207 174/211
3 174.7 0.8 178.7 0.8 182.6 0.3 185.3 0.3 188.0 0.2 190.5
152/189 158/195 163/200 167/204 171/208 175/212
0 175.2 0.8 179.2 0.8 183.2 0.3 185.9 0.3 188.6 0.2 191.1
153/190 158/196 164/201 168/205 1721209 176/212
V2= VR+ 20 VR+ 19 VR+ 20 VR+ 20 VR+ 20 VR+ 20
92= 13.0 13.0 12.5 12.5 12.5 12.0
1.V1 WET SPEED: V1 WET IS VI DRY minus 15kt.
2.Arrester Gear: Above data is valid with Arrester Net in either UP orDOWN position.
2.Arrester Gear: Above data isva6d with Arrester Net in either UP orDOWN position. ~
39 153.8 1.0 158.7 0.8 162.8 0.3 165.5 0.3 168.2 0.3 171.0
155/167 159/172 164/177 167/181 171/185 174/189
36 155.5 1.0 160.6 0.8 184.7 0.3 167.4 0.3 170.2 0.3 173.1
155/168 159/173 164/178 168/182 171/186 174/190
33 157.2 1.1 162.5 0.8 166.6 0.3 169.4 0.3 172.2 0.3 175.1
155/169 160/173 165/179 168/183 171/187 175/191
30 158.8 1.1 164.3 0.8 168.5 0.3 171.3 0.3 174.1 0.3 177.1
156/170 160/174 165/180 169/184 172/188 175/192
27 160.4 1.1 166.1 0.8 170.3 0.3 173.1 0.3 176.0 0.3 179.0
156/171 161/175 166/181 169/185 172/189 175/193
24 162.0 1.2 167.8 0.9 172.1 0.3 175.0 0.3 177.9 0.3 180.9
157/171 161/176 166/182 169/185 173/190 176/194
21 163.5 1.2 169.5 0.9 173.8 0.3 176.7 0.3 179.7 0.3 182.7
157/172 161/176 166/182 170/186 173/190 176/194
18 164.9 1.2 171.1 0.9 175.5 0.3 178.4 0.3 181.4 0.3 184.5
158/173 162/177 167/183 170/187 174/191 177/195
15 166.2 1.3 172.6 0.9 177.1 0.3 180.1 0.3 183.1 0.3 186.2
158/174 162/178 167/183 171/187 174/191 177/196
12 167.5 1.3 173.9 0.9 178.4 0.3 181.4 0.3 184.4 0.3 187.5
159/174 163/178 168/184 171/188 175/192 178/196
9 168.8 1.2 174.7 0.9 179.2 0.3 182.1 0.3 185.2 0.3 188.3
159/175 163/179 169/185 172/189 175/193 179/198
6 169.9 1.1 175.4 0.9 179.9 0.3 182.8 0.3 185.9 0.3 189.0
160/176 164/180 169/186 173/190 176/195 180/199
3 171.0 1.0 176.1 0.9 180.5 0.3 183.5 0.3 186.6 0.3 189.7
160/176 165/181 170/187 174/191 177/196 180/200
0 172.1 0.9 176.7 0.9 181.1 0.3 184.2 0.3 187.2 0.3 190.4
160/177 166/182 171/188 174/192 178/196 181/201
·3 172.9 0.9 177.3 0.9 181.7 0.3 184.7 0.3 187.8 0.3 191.0
161/177 167/183 172/189 175/193 179/197 182/202
V2= VR+22 VR+ 21 VR+ 21 VR+ 21 VR+ 21 VR+ 21
02= 14.0 13.5 13.5 13.5 13.0 13.0
1.VI WET SPEED: VI WET IS VI DRY minus 15kt.
OA: lOk~ Inc Skt Inc STILL Inc 10kt Inc 20kt lnc 30kt
C ~AIL /kt ~AlL /k~ Ala Ik~ BEAD /kt HEAD /kt ~
1.0 153.1
I,
"'-
OAT 10kt Inc 5kt Inc STILL Inc 10kt Inc 20kt Inc 30ke
c TAIL Ikt TAIL /kt AIR !kt BEAD /kt HEAD /kt HEAD
39 148.3
l
.....1
~
I
~
I
V2= VR+ 22 VR+ 21 VR+ 20 VR+ 20 VR+ 20 VR+ 20 ~
82c 14.0 14.0 13.5 . 13.5 13.0 13.0
1.Vl WET SPEED: Vl WET is Vl DRY minus 15kt.
LEFT
BLANK
=vs CONCORDE
AID Elev 192ft
LANDING DATA QNH BANGOR
Max wt Permitted (For pre flight planningl 111130kg
RUNWAY 15 33
STATUS (L) (A)
WAT Limit: VREF / VREF + 7kt 49"/49° 49°/49.
Landing Distance Available 3486m /11437ft 3486m /11437ft
Slope .25 ON .25 UP
Notes Notes 1,2 Notes 1,2,3
Manual VREF + 7kt 10kt 10kt
Manual VREF 10kt 10kt
Autoland VREF 10kt
Manual Slippery VREF 10kt 10kt
Autoland Slippery VREF 3kt
Fuel Saving ldg Weight VREF
Red'n per extra kt TW 3500kg
Incperkt HW
TOZElev 192ft 163ft
GS/HtatTHR 3 "/55ft 3"157ft
APPRDACH DA DHIlHA1) RYR DA DH/(HA1) RYR
(ftl (ftl (ft) 1ft)
ILS C2 Autoland 160R 1600ft
ILS Cl .. 400 12081 1800ft 370 12071 2400ft
ILSH No At/Dir . 500 13081 2200ft 470 (3071 28000
lLZ . 750 15581 5000ft 610 14471 40000
VOR oME .. 610 14181 5000ft 630 (4671 50000
NOB . 770 (607) 1.5sm
SRA......................................................... 750 155S) 50000 630 1467) 50000
VOR.A1BCP!............................................. 1000 lSOS/ 2sm 1000 lSOS) 2sm
Circling/Visuallradius S.3nml............... 1000 ISOSI 2sm 1000 (80S) 2sm
RWY DIRECTION 134°T 314°T
APPROACH WAY PT1'5nm) N44°59.5 N44·37.4
W 069°06.0 W 06S· 33.6
TOUCHDOWN WAYPT N44°49.1 N44·47.S
W06S·S0.7 W06S·4S.S
1. YOR DME 15 & 33: If ALS inop RVR becomes 60000.
2. Circling and Visual & YOR.A(BCP): NOT AUTHORISED NORTH EAST of Rwy 15/33.
LEFT
BLANK
:':=s CONCORDE LANDING DATA QNH BERMUDA
AID Elev 12ft
Max wt Pennitted (For preflight planning) 111130kg
RUNWAY 12 30
STATUS (B)
WAT Limit: VRFf/ VRFf + 7KT 49°/49° 49"/49"
Landing Distance Available 2944m / 9659ft 2944m / 9659ft
Slope NIL NIL
Notes Notes 1,2 Notes 1,3
Manual VRFf + 7kt 10kt 10kt
I
Manual VREF 10kt 10kt
Autoland
'-" Manual Slippery
VREF
VREF lkt lkt
Autoland Slippery VREF
Fuel Saving Ldg Weight... VREF
Red'n per extra ktTW 3500kg 3500kg
Incperkt HW
l
."'-' TDZElev 11ft 12ft
GS/HtatTHR 3"/52ft
APPROACH DA DH(HAT) RVR DA DH(HAT) RVR
(ft) (ft) (ft) (ft)
Its Cl . 270 (258) 0.75sm
ItsH No FIVDir . 320 (308) 0.75sm
LLZ . 450 (438) lsm
VOR DME . 450 (439) 1.25sm 530 (518) 1.25sm
VOR . 650 (639) 1.5sm 650 (638) 1.5sm
Circling / Visual (radius 5.3nm) .. 850 1838) 2sm 850 (838) 2sm
RWY DIRECTION 1010r 281 "T
APPROACH WAY PT(15nm) N32"24.7 N32"18.7
W064"58.9 W064"22.4
TOUCHDOWN WAY PT N32"21.9 N32"21.6
W 064°41.5 W 064"39.8
1.Circling / V'ISUa!: All circuits NORTH of Rwy 12/30 only.
LEFT
BLANK
=ys CONCORDE
AID Elev 20ft
LANDING DATA QNH BOSTON
Max wt Permitted IFor pre flight planning) 111130kg
RUNWAY 04L 04R
STATUS (L)
WAT Limit: VREF / VREF + 7kt 49"149· 49°/49.
Landing Distance Available 2396m /7858ft 2698m /8852ft
Slope .01 UP .04 ON
Notes Note 2 Notes 1;2
Manual ................................. VREF + 7kt lkt 9kt
Manual ............................................VREF 5kt 10kt
Autoland ..........................................VREF 6kt
Manual Slippery...............................VREF N/A 104.5
Autoland S6ppery ............................VREF 90.7
Fuel Saving ldg Weight ..................VREF
Red'n per extra kt TW 3500kg 3500kg
Incperkt HW 600kg
TDZElev 15ft 18ft
\..-, GS/HtatTHR 3·/47ft
APPROACH DA DH/(HAT) RYR DA DH/(HAT) RVR
(ft) 1ft) (ft) (ft)
ILS C2 Autoland 100R 1200ft
ILS CIR Coupled 220R 1800ft
ILS Cl .. 220 (202) 1800ft
ILSH No Flt/Oif .. 320 (302) 2200ft
lLZ . 490 (472) 4000ft
NOB . 930 (912) 2.5sm
IlSITall Ships) . 360 (342) 6000ft
lLZ(Tall Ships) . 490 (472) 6000ft
Circ6ng / Visuallradius 5.3nm) . 900 (880) 2.75sm 900 (880) 2.75sm
0T
RWY DIRECTION 020 020·T
APPROACH WAY PT(15nm) N42°07.4 N42°07.2
W 071°07.8 W 071°07.5
TOUCHDOWN WAY PT N42°21.5 N42°21.3
W071°00.9 W071°00.6
t. LLZ 04R: If MM inop RVR becomes 5000ft.
2. Circling and \rlSual: NOT AUTHORISED Rwy 04l clockwise to Rwy 15R.
RUNWAY 09 15R
STATUS (A)
WAT Umit: VREF/VREF + 7kt 49"/49° 49°/49°
Landing Distance Available 2133m /70000 2805m /9203ft
Slope .04ON .04DN
Notes Note 2 Notes 1;2
Manual VREF + 7kt 97.8 101«
Manual VREF 105.4 101«
Autoland VREF
Manual Stippery VREF N/A 108.8
Autoland Slippery VREF
Fuel Saving Ldg Weight VREF
Red'n per extra kt TW 3500kg 3500kg
Incperkt HW 600kg 600kg
TOZSev 18ft 18ft
GS/HtatTHR 3°/59ft
APPROACH DA DH/IHAT) RVR DA DH/IHAT) RVR
(ft) (ft) 1ft) 1ft)
IlS Cl .. 270 (2521 40000
ILSH No FlVDir . 370 (3521 40000
lU . 630 (6121 1.75sm
VOR OME . 830 (812) 2.5sm
Circling I Visuallradius S.3nm) .. 900 1880) 2.75sm 900 (8801 2.75sm
RWY DIREcnON 076°T 13SoT
APPROACH WAYPT(15nm) N42°17.6 N42°32.9
W 071 °20.5 W 071 ° lS.3
TOUCHDOWN WAYPT N42°21.3 N42°22.3
W 071°00.8 W071°00.9
t, ILS15R: LLZ offset.
.......
,cl
LEFT
BLANK
~s CONCORDE LANDING DATA QNH CAIRO
AID Elev 382ft
Max wt Permitted (For pre flight planning) 111130kg
RUNWAY 05L 05R
STATUS (A) (A)
WAT Limit VREF I VREF + 71d 48°/48° 48°/48°
Landing Distance Available 3300m 11OB27ft 4000m/13123ft
Slope .09 UP .05 ON
Notes Note 1;2 Note 1;2
Manual VREF + 71d 1Old 1Old
Manual VREF 1Old 1Old
Autoland VREF
Manual Slippery VREF Bkt 1Old
Autoland Sfippery VREF
Fuel Saving ldg Weight VREF
Red'n per extra IdTW 3500kg
IncperktHW
TDZ8ev 190ft 382ft
GS/HtatTHR 3°/52ft 3/49ft
APPROACIt DA DH/fHAT) RVR OA DH/(HA1) RVR
1ft) 1ft) 1ft) 1ft)
ILSC1 . 480 (290) 650m 650 126B) 650m
ILSH No Flt/Dir . 580 (390) 800m 750 136B) 750m
LLZ . 810 1620) 1300m 760 1378) 800m
VOROME . 6BO (490) 1000m 930 1548) 1100m
VOR/NOB .. 970 (588) 1200m
LBCNOME .. 810
1620) 1300m
LBCN . 810
(620) 1300m 1090 170B) 1500m
Circling I Visual (radius 5nm) .. 1550
(1168) 800m 1550 11168) BOOm
0T 0T
RWY DIRECnON 050 050
APPROACH WAY PT It 5nm) N29°57.5 N29°56.3
E031 °09.6 E031 ° 10.7
TOUCHDOWN WAY PT N30°07.2 N30006.0
E031 °22.9 E031°24.0
1. RVRs: RVR measurements are only available forRwy 23R.
LEFT
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BRmSH
AJJMAYS CONCORDE LANDING DATA QNH DUBLIN
AID Elev 242ft
Max wt Pennitted (For pre flight planning) III t30kg
RUNWAY 10 28
STATUS (E) (E)
'-' WAT Umit: VREF 1VREF
Landing Distance Available
+ 7kt 49°/49"
2637m 18652ft
49i49"
2637m 18652ft
Slope .46 ON .46 UP
Notes Note 1 Note 1
Manual ................................. VREF + 7kt 7kt 8kt
Manual ............................................VREF 10kt 10kt
Autoland ..........................................VREF 2kt 4kt
Manual Slippery...............................VREF 99.2 103.7
Autoland S6ppery ............................VREF N/A N/A
Fuel Saving Ldg Weight ..................VREF
Red'n per extra kt 1W 3500kg 3500kg
Incperkt HW 600kg 600kg
TOZSev 242ft 202ft
~ GS/HtatTHR 3°/54ft 3153ft
APPROACH DA DH/(HA1) RYR DA DH/(HA1) RYR
(ft) (ft) (ft) (ft)
ILSel ......................................................
(2081 550m 450 410 (208) 550m
ILSH No F1VOir.........................................
(3081 700m 550 510 (308) 700m
SRA .........................................................
(6681 1400m 910 760 (558) 1200m
Circling 1Visual (radius 5.3nml ............... (8581 800m 1100 1100 (858) 800m
RWY DIRECTION 095°T 275°T
l
APPROACH WAY PT(15nm) N 53°26.6 N53°23.8
~ WOD6°42.5 W005·49.9
TOUCHDOWN WAY PT N 53·25.3 N53·25.2
W006°17.4 W 006"15.0
1. ILSe1 Rwy 10/28: If TOZ orRCL inop RVR becomes 6DOm.
INTENTIONALLY
LEFT
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BRmStI
AIJNIAYS CONCORDE LANDING DATA QNH EAST MIDLANDS
AID Elev 310ft
Max wt Permitted (For pre flight planning) 111130kg
RUNWAY 09 27
STATUS (A) (E)
WAT limit: VREF / VREF + 7kt 49"/48° 49°/48°
landing Distance Available 2280m / 74800 2280m / 7480ft
Slope .33 ON .33 UP
Notes
Manual ................................. VREF + 7kt 104.9 107.1
Manual ............................................VREF Okt lkt
\-- Autoland ..........................................VREF
Manual Slippery...............................VREF N/A
96.8
N/A
Autoland Slippery ............................VREF N/A
Fuel Saving Ldg Weight ..................VREF
Red'n per extra kt TW 3500kg 3500kg
Incper kt HW 600kg 600kg
TDZElev 305ft 280ft
GS/HtatTHR 3"/5Oft 3°/57ft
APPROACH DA DH/(HAl) RVR DA DH/(HAl) RVR
(ft) (ft) (ft) (ft)
ILS C1R........................................Coupled 210R 600m
ILSC1 ...................................................... 510 (205) 600m 480 (200) 600m
ILSH No Flt/Dir......................................... 610 (305) 650m 580 (300) 650m
LLlDME .................................................. 710 (405) 800m 680 (400) 800m
LLl........................................................... 710 (405) 800m 680 (400) 800m
NDBDME ................................................ 790 (485) 1DOOm 680 (400) 900m
NDB ......................................................... 790 1485) 1000m 680 (400) 900m
~ SRA (term 2nm) ...................................... 840 1535) 1100m 690 (410) 900m
Circling / Visual (radius 5.3nm) ............... 1200 (890) 800m 1200 (890) aOOm
RWY DIRECTION 088°T 268°T
APPROACH WAY PT(15nm) N 52°49.2 N52°50.3
W001°45.5 WOOO·53.9
TOUCHDOWN WAY PT N 52°49.8 N52°49.8
WOOl °21.7 W 001°18.7
LEFT
BLANK
BAmSH
AIRWAYS CONCORDE LANDING DATA QNH EDINBURGH
AID Elev 135ft
Max wt Permitted (For pre flight planning) 111130kg
RUNWAY 07 25
STATUS (E) (E)
~ WAT Umit: VREF /VREF + 7kt 49°/49° 49°/49°
Landing Distance Available 2347m /770Oft 2347m/770Oft
Slope 0.16 ON 0.16 UP
Notes Note 1;2 Note 1;2
Manual ................................. VREF + 7kt 110.0 Okt
Manual ............................................VREF 3kt 4kt
~ Autoland ..........................................VREF 101.3 104.3
Manual Slippery...............................VREF NlA NlA
Autoland Slippery ............................VREF NlA NlA
Fuel Saving ldg Weight ..................VREF
Red'n per extra kt TW 3S00kg 3S00kg
Incperkt HW 600kg 600kg
TDZElev 110ft 100ft
~ GS/HtatTHR 3°/55ft 3°/52ft
APPROACH DA DH/(HAl) RVR DA DH/(HAT) RVR
Iftl Iftl (ftl Iftl
Its C1R........................................Coupled 200R 550m 220R SSOm
Its Cl ...................................................... 310 1200) SSOm 300 (200) SSOm
'-' ILSH No FltlDir.........................................
lLZOME ..................................................
410
710
(300)
(600)
6S0m
1200m
400 (300) 6S0m
Circling/Visual (radius S.3nm) ............... 2050 (191S) SOOm 20S0 (1915) 800m
RM D1REcnON OS9°T 239°T
APPROACH WAY PT(15nml NSSo 48.9
NSSoOS.O
W003°4S.0
W002°5S.4
TOUCHDOWN WAY PT N5SoS6.7NSSoS7.3
W003°23.1
W003°21.4
1. Circling,lV'l$ual: IFcircfing restricted to NORTH ofRWY 07/2S minima may be reduced to
OA 12S0 / HAT (1115), however circting is notapproved following an SRA approach to RWY 07.
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I
~
::1$ CONCORDE LANDING DATA QNH FARO
NO Elev 24ft
Max wt Permitted (For pre flight planning) 111130kg
RUNWAY 11 29
STATUS
WAT Limit: VREF /VREF + 7kt 49"149° 49°/49°
Landing Distance Available 2445m /S022ft 2445m /S022ft
Slope .09 ON .09 UP
Notes Note 1 Note 1
Manual VREF + 7kt lkt lkt
Manual VREF 5kt 5kt
Autoland VREF
Manual Slippery VREF N/A N/A
Autoland Sfippery VREF
Fuel Saving Ldg Weight VREF
Red'n perextra ktTW 3500kg 3500kg
IncperktHW
TOZElev 24ft 18ft
GS/HtatTHR
APPROACH DA DH/(HAt) RVR DA DH/fHAt) RVR
(ft) (ft) (ft) (ft)
VOR OME . 460 (436) 1300m 510 (492) 1400m
VOR . 4S0 (456) 1300m 510 (492) 1400m
NOB . 570 (552) 1500m
Circling / Visual (radius 5.3nm) . S50 (S26) 800m S50 (826) SOOm
RWY DIRECTION 100 0T 2S00T
APPROACH WAY PT (1Snm) N37°03.6 N36°5S.1
WOOSo17.6 W007°39.0
TOUCHDOWN WAY PT N37°01.0 N37°00.7
W007°S9.1 W007°57.5
1.Circling / Visual Minima: Allcircuits SOUTH oftherunway due terrain. Visual approaches from the
NORTH are permitted, butdescent below 3000ft is notto be commenced before VFA 6d. Avoid an
excessive descent rate to prevent GPWS.
Avoid overflying builtupareas 3nm EAST and 6nm WEST ofairfield.
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:::aft CONCORDE lANDING DATA ONH GANDER
AID Elev 496ft
Max wt Permitted IFor pre flight planning) 111130kg
RUNWAY 04 13
STATUS (A) (A)
WAT Limit: VREF 1VREF + 71et 48°/48° 48°/48°
Landing Distance Available 3200ml t0500ft 27t3m/890Oft
Slope .26 UP .34DN
Notes
Manual VREF + 7kt 10kt 8kt
Manual VREF 10kt 10kt
Autoland VREF
Manual Slippery VREF 6kt 101.8
Autoland Slippery VREF
Fuel saving Ldg Weight VREF
Red'n per extra let TW 3500kg 3500kg
Incperkt HW 600kg
TDZElev 428ft 488ft
GS/Ht at THR 3°/59ft 3°/63ft
APPRDACH DA DH/(HAl) RVR DA DH/IHAT) RYR
(ft) (ft) (ft) (ftt
ILS Cl . 630 (202) 26000 690 (202) 2600ft
ILSH No FJ!/Dir .. 730 (302) 26000 790 (302) 2600ft
LLZ .. 810 (3821 SOOOft 930 (442) SOOOft
NOB .. 990 (S02) 50000
Circling I Visuallradius S.3nml ...·..·........ 1300 (8041 2sm 1300 (804) 2sm
[
RWY DIRECTION 011°T 107°T
~ APPROACH WAY PT (15nmt N48°40.S N49°01.5
W054°38.4 W OS4° 57.1
TOUCHDOWN WAY PT N4SoSS.2 N4SoS7.t
W054°34.1 W054°35.2
WOS4°29.2 W054°1t.3
TOUCHDOWN WAY PT N48°S6.8 N48°S6.7
WOS4"33.6 W054°33.1
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BAmsH
ADMAYS CONCORDE LANDING DATA QNH HALIFAX
AID Elev 471ft
Max wt Permitted IFor pre flight planningl 111130kg
RUNWAY 06 15
STATUS (A)
WAT Umit VREF /VREF + 7kt 4S,4S0 4So/4So
Landing Distance Available 2682m /88000 2347m /77000
Slope .06 ON .55 UP
Notes
Manual..................................VREF + 7kt Skt Okt
Manual.............................................VREF 10kt 3kt
Autoland ..........................................VREF
~ Manual Slippery...............................VREF 101.9 N/A
Autoland Slippery ............................VREF
Fuel Saving Ldg Weight...................VREF
Red'n per extra kt 1W 3S00kg 3S00kg
IncperktHW 600kg
TDZElev 462ft 441ft
\-, GS/Htat THR 3/500
APPROACH DA DH/IHAT) RVft DA DH/(HAT) RVR
(ft) (ft) (ft) (ft)
ILSC1 ...................................................... 650 1209) 26000
ILSH No Flt/Dir ......................................... 750 1309) 26000
LlZ........................................................... SOD 1359) 50000
LLZ Back Beam ........................................ 820 (3SS) lsm
NOB ......................................................... 1010 (548) lsm 850 1409) 1.2Ssm
Circling/ Visuallradius S.3nml................ 1300 1823) 2sm 1300 (823) 2sm
, 03SoT 12SoT
RWY DIRECnON
~
APPROACH WAY PT(1 5nm) N44°39.8 N4S002.2
W063°43.6 W063°48.S
TOUCHDOWN WAY PT N44°S2.1 N44°S3.6
W063°31.S W063°31.1
2. Rwy 21: The landing weights pUblished assume a landing distance of 2200m commencing from a
temporary threshold 250m before theinset landing threshold. Circling / Visual minima ONLY may be
used. allother minima is shown only for reference.
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=vs
AID Elev
CONCORDE
48ft
LANDING DATA QNH JEDDAH
KING ABDUL AZIZ
Max wt Permitted (For pre flight planning I 111130kg
RUNWAY 16L 16C
STATUS (E) (E)
WAT Limit: VREF / VREF + 7kt 49"/49"
Landing Distance Available 3690m /12106ft 3300m /1 0827ft
Slope .14 UP Nil
Notes Note 1 Notes 2;3
ManuaL VREF + 7kt 10kt 10kt
ManuaL VREF 10kt 10kt
Autoland VREF 10kt 10kt
Manual Slippery VREF 10kt Skt
Autoland Slippery VREF 9kt 2kt
Fuel Saving Ldg Weight.. VREF
Red'n per extra kt TW 3500kg 3500kg
Incper kt HW
TDZ Elev 30ft 26ft
GS/Ht at THR 3"/57ft 3"/52ft
APPROACH OA OH/IHAT) RYR OA OH/IHAT) RYR
(ftl (ft) 1ft) (ft)
ILS Cl...................................................... 230 12001 SOOm 230 1204) 550m
ILSH No Flt/Dir 330 13001 SOOm 330 13041 700m
LlZ........................................................... 470 14401 1200m 470 1444) 1200m
VOR DME................................................. 490 14601 1600m 470 1444) 1500m
Circling/Visual (radius 5.3nm)................ NOT AUTH NOT AUTH
RWl DIRECnON 159"T 159"T
APPROACH WAY PT115nm) N21"55.S N21"55.3
E039" 04.3 E039" 03.4
TOUCHDOWN WAY PT N21"41.S N21"41.3
E039"10.1 E039" 09.2
1.Approach Lights Rwy 1&L: If ALS inop the following RVR/VIS applies:-ILS 1200m, LLZ 2km,
VOR DME2km.
2. Approach Lights Rwy16R & 34L: If AlS inop the following RVR's apply:·llS1200m, LLZ lS00m.
3. Approach Lights Rwy 34R: If ALS inop the following RVR/VlS applies:·ILS 1200m, LLZ2km,
VOR DME 2.4km.
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:='8 CONCORDE LANDING DATA ONH LAJES
AID Elev 180ft
Max wt Permitted (For pre flightplanning) 111130kg
RUNWAY 15 33
STATUS (A)
WAT Umit: VREF / VREF + 7kt 49°/49° 49°/49.
Landing Distance Available 3312m/l0865ft 33t2m /1 0865ft
Slope .20 UP .20 ON
Notes Notes 1,2 Notes 1.2
Manual VREF + 7kt 10kt 10kt
Manual VREF 10kt 10kt
Autoland VR EF
Manual Slippery VREF 9kt Skt
Autoland Slippery VREF
Fuel Saving Ldg Weight VREF
Red'n perextra kt TW 3500kg 3500kg
IncperktHW
TDZElev 158ft 1SOft
GS/HtatTHR a·/54ft
APPROACH DA DH/(HAT) RYR DA DH/lHAT) RYR
(ft) (ft) (ft) (ft)
ILSC1 . 360 (202) 1520m
ILSH No Flt/Dir . 460 (302) 1520m
LLZ . 510 (352) 1520m
VOR (BCPI . 1000 (S20) 4km 1000 (S201 4km
NOB . 710 (552) 2.4km
PAR . 460 (302) 1520m 4S0 (3001 1520m
SRA . 610 (452) 2km 790 (6101 2.Skm
Circling 1Visual (radius 5.3nm) . 1000 (S20) 4km 1000 (S201 4km
RWY DIRECTION 141·T 321°T
APPROACH WAY PT(15nm) N3S058.1 N3S033.5
W 027°18.4 W 026° 52.9
TOUCHDOWN WAY PT N3So 46.5 N3S·45.2
W 027·06.3 W 027·05.0
1. Circling / Visual: Allcircuits EAST of runway due high ground WEST and SOUTH of NO.
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,
\J
:ys CONCORDE LANDING DATA QNH LISBON
AID Bev 314ft
Max wt Permitted IFor pre flight planning) 111130kg
RUNWAY 03 17
STATUS (E)
WAT Umit: VREF /VREF + 7kt 48°/48° 48"148°
Landing Distance Available 3715m /12188ft 2400m /7874ft
Slope .10 UP .55 ON
Notes Notes 1,2 Note I
Manual VREF + 7kt 10kt Okt
Manual VREF 10kt 3kt
Autoland VREF 10kt
Manual Slippery VREF lOkt N/A
Autoland Slippery VREF 9kt
Fuel Saving ldg Weight VREF
Red'n per extIa kt TW 3500kg 3500kg
Incperkt HW
TOZElev 331ft 374ft
GS/HtatTHR 3°/54ft
APPROACH DA DH/IHAT) RYR DA DH/IHAT) RVR
1ft) 1ft) 1ft) 1ft)
ILSC1 . 540 1209) 800m
ILSH NoFlt/Dir . 640 1309) 1000m
lLZ . 880 1549) 1400m
SRA [term 3nm) . 1270 1939) 1500m
Circling / Visuallradius 5.3nm) .. 1600 112261 800m 1600 (1226) 800m
RWY DIRECTION 023°T 168°T
APPROACH WAY PT 115nm) N38°32.1 N39°01.7
W 009° 16.1 W OOgO 12.1
TOUCHDOWN WAY PT N38°45.9 N3S047.0
W 01)9°08.6 W009°0S.1
t. Rwy Availability: Use Rwys 17 or 21 whenever possible.
2.GPWS Rwy03:Caution, a high probability exists foragenuine GPWS warning during circuits flown to
the West of theairfield when descending ondownwind leg orpositioning fora short final. Toalleviate
thisproblem:-
Aim to fly downwind (US 21 OR orascleared) descending to NOT BELOW 2500ft QNH and maintain
until commencing base tumat USlId orlater.
Adjust rate of descent during base tum to cross the OM at 1700ft QNH.
3.GPWS Rwy21:Due to anisolated outcrop of high terrain to the West of centreline a high probability of
a genuine GPWS exists, to avoid thisproblem endeavour to stabilise onthecentreline and glide path by
Snm from touchdown.
RUNWAY 09 27
STATUS (A)
WAT Limit: VREF /VREF + 7kt 49"149° 49°/49°
Landing Distance Available 2225m /73000 2286m /75000
Slope .25 UP .25 ON
Notes Note 1 Note 1,2
ManuaL VREF + 7kt 104.4 105.4
Manual. VREF Dkt Okt
Autoland VREF
Manual Slippery VREF N/A N/A
Autoland Slippery VREF
Fuel Saving Ldg Weight VREF
Red'n per extra kt TW 35DOkg 3500kg
Incperkt HW 600kg 60Dkg
TOZElev 58ft 77ft
GS/HtatTHR 3°/54ft
APPROACH DA DH/(HAT) RYR DA OH/IHAT) RYR
1ft) (ft) (ft) (ft)
ILS C1R Coupled 210R 550m
ILS Cl . 280 1203) 550m
ILSH No At/Dir . 380 13031 650m
lLZDME .. 430 (372) 800m 450 (373) 800m
NOB OME .. 630 (5531 1100m
SRA (Term 2nml .. 560 (5021 1DOOm 550 (4731 1000m
Circling I Visual (radius 5.3nml .. 950 (869) 800m 950 18691 800m
RM DIRECTION 086°T 266°T
APPROACH WAY PT (15nml N53°18.9 N53°21.1
W 003°16.8 W002"24.8
TOUCHDOWN WAY PT N53°20.0 N53°20.1
W002"51.8 W002"49.9
1. Runway Surface: Liable to be slippery when wetwhen Muis less than .39.
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:ys CONCORDE LANDING DATA QNH LUXOR
AID Bev 294ft
Max wt Permitted (For pre flightplenning) 111130kg
RUNWAY 02 20
STATUS (B)
WAT Umit: VREF / VREF + 7kt 49°/48° 49°/48°
Landing Distance Availeble 3000m /9843ft 3000m /9843ft
Slope .22ON .22 UP
Notes Note 1 Note 1
Manual VREF + 7kt 10kt 10kt
Manual VREF 10kt 10kt
Autolend VREF
Manual Slippery VREF lkt lkt
Autoland Slippery VREF
Fuel Saving ldg Weight VREF
Red'n perextra kt TW 3500kg 3500kg
IncperktHW
le.. TDZElev 294ft 272ft
"'-' GS/HtatTHR 3/500
APPROACH DA DH/(HA1) RVR DA DH/(HAT) RVR
(It) (It) (ft) (It)
ILS Cl . 510 (238) 800rn
ILSH No Flt/Dir .. 610 (338) 1000rn
VORoME .. 900 (606) 1500m 810 (538) 1400m
l.BCN .. 940 (646) 1500m 770 (498) 1300m
Circling / Visual (radius 5.3nm) .. 1500 (1206) 800m 1500 (1206) 800m
KWY DIRECTION 021°T 201°T
APPROACH WAY PT(15nm) N 25°25.3 N 25°54.7
E032°35.6 E032°48.2
TOUCHDOWN WAY PT N 25°39.3 N 25°40.7
E032° 41.6 E032° 42.2
1. Circfing and VISual: Allcircuits NORTH WEST of AID.
I
"'-'
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~
BIIfISll
AJlWAYS CONCORDE LANDING DATA QNH MANSTON
AID Elev 178ft
Max wt Permitted (For pre flight planning) 111130kg
RUNWAY 10 28
STATUS
WAT Umit: VREF / VREF + 7kt 49°/49° 49/49°
Landing Distance Available 2752m /9029ft 2752m /9D29ft
Slope NlL NlL
Notes
Manual .•......•..•.....•...........•... VREF + 7kt 101rt 10kt
Manual ............................................VREF 1Dirt 10kt
Autoland ..........................................VREF
Manual Slippery...............................VREF 106.4 106.4
Autoland Slippery ............................VREF
Fuel Saving Ldg Weight ..................VREF
Red'n per extra ktTW 3500kg 3500kg
Incper ktHW 600kg 600kg
TDlSev 178ft 178ft
GS/HtatTHR
APPROACH OA OH/tHAT) AYR OA OH/IHAT) AYR
(ft) (ft) (ft) (ft)
PAR ......................................................... 480 1302) 900m 480 (302) 900m
I SRA ......................................................... 580 1402) 1200m 590 (412) 1200m
~
Circling/ Visual (radius 5.3nm) ............... 1000 (822) 800m 1000 (8221 BOOm
RWY DIRECTION 101°T 281°T
APPROACH WAY PT(1Snm) N51°23.4 N51 ° 17.5
EOOO° 56.1 E001° 45.4
TOUCHDOWN WAY PT N51°20.6 N51°20.4
EOO1°19.7 E001°21.9
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:ys CONCORDE lANDING DATA QNH MARSEILLE
AID Elev 69ft
Max wt Permitted (For preflight planning) 111130kg
RUNWAY 14L 14R
STATUS (E)
WAT UmitVREF /VREF + 7kt 49·/49· 49·/49·
Landing Distance Available 316Om/10367ft 237Om/m6ft
Slope .51 UP .67UP
Notes Notes 1,2,3,5,6 Notes 1,3,4,6
Manual VREF + 7kt 10kt 1kt
Manual VREF 10kt 5kt
Autoland VREF 10kt
Manual Slippery VREF 7kt 91.7
Autoland Slippery VREF 108.6
Fuel Saving ldg Weight VREF
Red'n perextra ktTW 3500kg 3500kg
Inc perkt HW 600kg 600kg
TDZ Bev 8ft 7ft
GS/Ht at THR 3·155ft
APPROACH DA DH/(HAT) RYR DA DH/(HAT) RVR
(ft) (ft) (ft) 1ft)
ILS Cl......................................................
(262) 270
850m
ILSH No F1t/Dir......................................... (362) 370
1000m
lLZ...........................................................
(422) 430
1800m
l.BCNs 'MAR' & 'MS'............................... (572) 580
2450m
l.BCN'MAR'............................................ (832) 840
3.5km
Circling/Visuallradius 5.3nm) (1481) 1550
3.5km 1550 (1481) 3.5krn
RWYDIRECTlON 134·T 135·T
APPROACH WAY PT(15nm) N43· 37.3 N43·37.1
E004·57.2 E004" 57.6
TOUCHDOWN WAY PT N43"26.9 N43"26.5
E005"12.1 E005"12.3
1.088: Approach banexists for all procedures listed below wflen reported cloud ceiling orvertical
visibUity is lessthanfollowing:- Circlinw'Visual OBB 1440ft AAL
4. Runway Availabilty: Rwy 14R/32l for use in emergency only dueto low bearing strength.
3. Availability: Rwy 14R/32L far use in emergency only due to lowbearing strength.
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AID Elev
CONCORDE
590ft
LANDING DATA QNH NIAGARA FALLS
Max wt Permitted IFor pre flight planning) 111130kg
RUNWAY 10L 28R
STATUS (A)
WAT Umit VREF I VREF + 7kt 48748° 48·/48·
Landing Distance Available 2781m/9124ft 2781 mI 9124ft
Slope .01 DN .01 UP
Notes
Manua!.. VREF + 7kt 10kt 10kt
Manual VREF 10kt 10kt
Autoland VREF
Manual Slippery VREF 105.7 105.8
Autoland Sfippery VREF
Fuel Saving Ldg Weight VREF
Red'n per extra ktTW 3500kg 3500kg
IncperktHW 600kg 600kg
I TDZElev 589ft 588ft
"-' GS/HtatTHR 2.S·/66ft
APPROACH DA DH/(HAT} RYR DA DH/(HAT) RVR
lftl 1ft) 1ft) 1ft)
ILSel .. 790 (202) 24000
ILSH No Flt/Dir .. 890 (302) 24000
Ul .. 950 (362) 40000
NDB .. 1050 (462) 50000
Circling I Visual (radius S.3nm) . 1400 (810) 2sm 1400 (810) 2sm
RWY DIRECnON 090·T 270·T
APPROACH WAY PT115nm) N43°06.6 N43°06.6
W 079° 18.5 W078°35.5
TOUCHDOWN WAY PT N43°06.6 N43°06.6
W078°58.0 W078°S6.0
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:vs CONCORDE LANDING DATA QNH OPORTO
AID Elev 228ft
Max wt Pennitted (For preflight planning) 111130kg
RUNWAY 17 35
STATUS (A)
~ WAT Umit: VREF / VREF + 71CT 49·/49· 49,49·
Landing Distance Available 31S01Tl/l0433ft 3330lTl/l0925ft
Slope 0.71 UP 0.71 ON
Notes Note 1 Note 1
Manual.. VREF + 7kt 10kt 10kt
Manual VREF 10kt 10kt
Autoland VREl'
Manual S6ppery VREF 5kt 6kt
Autoland Slippery VREF
Fuel saving Ldg Weight.. VREF
Red'n perextra kt TW 3500kg 3500kg
Inc perktHW
TDZElev 151ft 227ft
GS/HtatTHR 2.7·/52ft
APPROACH DA DH(HAT) RVR DA DH(HAT) RVR
1ft) (ft) (ft) (ft)
ILSC1 .. 390 12391 600m
ILSH NoFItIOir .. 490 13391 700m
LLZ . 600 14491 900m
VOR OME . 600 14491 900m 660 (4331 900m
NOB .. 760 16091 1200m 1010 17S31 1500m
Circling / Visual (radius 5.3nml .. 1300 1'072) SOOm 1300 110721 SOOm
RWY DIRECnON 169'" 349'"
APPROACH WAY PT 115nml N 41 "30.3 N 40"59.3
W OOS·44.S W 00S"36.8
TOUCHDOWN WAY PT N41 °15.6 N 41 °14.0
WOOS °41.0 W 00S·40.6
1.Circling / VISUal: If circuits restricted to WEST ofrunway minima may bereduced to
OA 1050ft (HAA S22ft).
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BRmSH
AIRWAYS CONCORDE LANDING DATA QNH OTTAWA
AID Elev 374ft
Max wt Permitted (For pre flight planning) 111130kg
RUNWAY 07 14
STATUS (A)
WAT Limit: VREF 1VREF + 7kt 48,4So 4So/4S·
landing Distance Available 2438m 1 SOOOft 2941 m19649ft
Slope .09 ON .16UP
Notes
Manual ................................. VREF + 7kt 1kt 10kt
Manual ............................................VREF 5kt 10kt
~ Autoland ..........................................VREF
Manual Stippery...............................VREF N/A Okt
Autoland Slippery ............................VREF
Fuel Saving Ldg Weight ..................VREF
Red'n per extra kt1W 3500kg 3500kg
Incper kt HW
TOZElev 373ft 367ft
'-' GS/Htat THR 3°/55ft
APPROACH OA DH/(HAT) RVR DA DH/(HAT) RVR
(ft) (ft) (ftl (ft)
I
ILS C1 ...................................................... 580 (207) 26000
ILSH No FtVDir......................................... 680 (307) 26000
""-'..
lLZ........................................................... 830 (457) 50000
LLZ (BB) OME .......................................... 890 (523) 1.5sm
LLZ (BB) NOB........................................... 890 (523) l.5sm
VOR OME................................................. 890 (523) 1.5sm
VOR NOB ................................................. 890 (523) 1.5sm
~ NOB ......................................................... 890 (517) 1.25sm
Circling 1Visual (radius 5.3nm) ............... 1200 (8261 2sm 1200 (826) 2sm
RWY DIRECTION 057°T 126°T
APPROACH WAY PT(15nm) N45°10.6 N45°28.3
W 075°38.1 W075°58.4
TOUCHDOWN WAY PT N45°18.8 N45°19.5
W075·40.3 W075°41.1
\-" 3. ILSe1 & C1R Rwys 09 & 10: IfTDZ orRClinop RVR becomes 600m.
3. ILSC1 & C1R Rwys 27 & 28: If TOZ orRClinop RVR becomes 600m.
3. ILSCl & C1R Rwy 26: IfTDZ orRCLinop RVR becomes 6DOm.
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:vs CONCORDE LANDING DATA ONH PRESTWICK
AID Elev 66ft
Malt wt Permitted (For pre flight planning) 111130kg
RUNWAY 13 31
STATUS (B) (A)
WAT Umit: VREF IVREF + 7kt 49749° 49°/49°
Landing Distance Available 2743m 1 8999ft 2987m 198000
Slope .27 UP .27 ON
Notes Notes 1,2 Notes 1,2
Manual VREF + 7kt 10kt 10kt
Manual VREF 10kt 10kt
Autoland VREF
Manual Slippery VREF 105.2 Okt
Autoland Slippery VREF
Fuel Saving Ldg Weight VREF
Red'n per extra ktTW 3500kg 3S00kg
Incperkt HW 600kg 600kg
TOZElev 38ft 66ft
GS/HtatTHR 3°/53ft 3.So/56ft
APPROACH DA DH/(HAT) RVR DA DH/(HAT) RVR
(ft) (ft) (ft) (ft)
ILS Cl . 250 (212) 600m 280 (214) aDOrn
ILSH No FItIOir . 340 (302) 650m 370 (304) 6S0m
LLZ . 420 (382) 800m NOT AUTH
NOB .. 490 (452) 900m NOT AUTH
SRA (term 2nm) . 570 (S32) 1100m BOO (734) 1S00m
Circling 1Visual (radius 5.3nm) . 11 SO (10~) BOOm 1150 (1084) 800m
RWY DIRECnON 121°T 301°T
APPROACH WAY PT(1Snm) N55°38.6 N5S022.4
W 004°59.4 W 004° 11.9
TOUCHDOWN WAY PT N55° 30.9 N5So 30.2
W 004°36.6 W 004° 34.5
1. fire Cover: Normal fire cover at PIK is ICAD Cat 6 with upgrades to Cat 7,8 and 9 on request at 60
mins notice. A minimum ofICAO Cat8 is required bV Concorde and thisshould be pre-arranged and
confirmed prior to arrival.
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:::::'vs CONCORDE LANDING DATA QNH RIYADH
AID Elev 2049ft
Mu wt Permitted (For pre flight planning) 111130kg
RUNWAY 15L 15R
STATUS (E) (E)
WAT limit: VREF / VREF + 7kt 40°/45° 40<y45 °
Landing Distance Available 4200m/1378Oft 4200m /13786ft
Slope .15 ON .11 ON
Notes Note 1;2 Note 1;2
Manual VREF + 7kt 10kt 10kt
Manual VREF 10kt 10kt
Autoland VREF 10kt 10kt
Manual Slippery VREF 10kt 10kt
Autoland Slippery VREF 10kt 10kt
Fuel Saving ldg Weight VREF
Red'n per extra kt TW
Incperkt HW
TOZSev 2033ft 2049ft
GS/HtatTHR 3°/55ft 3°/5Sft
APPROACH DA DH/(HAT) RVR DA DH/(HAT) RVR
(ft) (ft) (ft) (ft)
ILSC1 . 2240 (207) 600m 22S0 (201) 600m
ILSH No Flt/Dir . 2340 (307) 700m 23S0 (301) 700m
lLZ .. 2470 (437) 1200m 2470 (421) 1200m
VOR DME . 2490 (457) 1500m 2510 (461) 1500m
Circling/Visual (radius S.3nm) .. NOT AUTHORISED NOT AUTHORISED
0T IS00T
RWY DlRECnON 150
APPROACH WAY PT(15nm) N2S011.5 N2S011.2
E046°33.8 E046°32.2
TOUCHDOWN WAY PT N24°S8.5 N24°SS.2
E046°42.1 E046°40.S.
1. ILS Rwys 15L/R: IFMM/TOl/RCl inop RVR becomes 800m.
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AlJrNAYS CONCORDE LANDING DATA QNH SANTA MARlA
AID Elev 308ft
Max wt Permitted (For pre flight planning) 111130kg
RUNWAY 18 36
STATUS (A)
WAT Limit VREF / VREF + 7kt 49"/48" 49"/48"
Landing Distance Available 3048m /1 OOOOft 3048111/100000
Slope NIL NIL
Notes Note 1 Note 1
Manual.................................. VREF + 7kt 10kt 10kt
Manual.............................................VREF 10kt 10kt
~ Autoland ..........................................VREF
Manual Slippery...............................VREF 3kt 3kt
Autoland Sfippery ............................VREF
Fuel Saving Ldg Weight...................VREF
Red'n per extra kt1W 3500kg 3500kg
Ine per kt HW
TDZElev 284ft 283ft
~ GS/HtatTHR 2.75"1500
APPROACH DA DH/(HAT) RVR DA DH/IHAT) RYR
1ft) (ft) (ft) (ft)
ILSel ...................................................... 490 12061 700rn
ILSH No Flt/Dir ......................................... 590 13061 900m
~- LLZ ........................................................... 640 13561 1100m
VOR.......................................................... 770 1486) 1200m 660 1377) 1000m
NOB ......................................................... 690 1406) 1100m 690 (4071 1100m
Circling/Visual (radius 5.3nm)................ 1150 1842) 800m 1150 (842) 800m
RWY DIRECTION 171"T 351"T
APPROACH WAY PT(15nm) N37"13.9 N36"42.7
W 025°13.3 W025°07.2
TOUCHDOWN WAY PT N36°59.1 N36°57.5
W 025°10.4 W02S010.1
1. Circling Md Visual: WEST ofairfield only.
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AIRWAYS CONCORDE LANDING DATA QNH SHANNON
AID Elev 47ft
Max wt Permitted (For pre flight planning) 111130kg
RUNWAY 06 24
STATUS (E) (E)
~ WAT Umit: VREF I VREF + 7kt 49"/49· 49"/49·
Landing Distance Available 3200m 1105000 3060m 1100400
Slope .29 ON .29 UP
Notes
Manual..................................VREF + 7kt 10kt 10kt
Manual.............................................VREF 1Old 1Old
Autoland ..........................................VREF
~ 1Old 1Old
Manual Sfippery...............................VREF 5kt 4kt
Autoland Slippery ............................VREF Okt N/A
Fuel Saving Ldg Weight...................VREF
Red'n per extra kt TW 3500kg 3500kg
Incperkt HW
TOZElev 47ft 15ft
GS/HtatTHR 3·/54ft 3/54ft
APPROACH OA DH/(HAT) RVR DA DH/(HAT) RVR
(ft) (ft) (ft) (ft)
ILSel ...................................................... 250 (203) SOOm 220 (205) SOOm
ILSH No Flf/Dir ......................................... 350 (303) 900m 320 (305) 1000m
\.-t VORDME ................................................. 450 (403) 1100m 450 (435) 1200m
SRA (term 2nm)....................................... 500 (453) 1200m 520 (50S) 1300m
Circling I Visual (radius 5.3nm)................ S50 (S03) SOOm S50 (803) 800m
I RWY DIRECTION 052°T 232·T
~ APPROACH WAY PT(15nm) N52·32.3 N 52·51.8
W 009°15.9 WOOS·34.S
TOUCHDOWN WAY PT N 52°41.6 N 52·42.6
W 00S056.5 w OOS· 54.4
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=vs CONCORDE
AID Elev 4848ft
LANDING DATA QNH TAIF
Max wt Permitted (For pre flight planning) 111130kg
RUNWAY 07 17
STATUS
WAT Limit VREF /VREF + 7kt 13·/27· 13"/27·
Reduce Max Landing Weight hI' 500kg I 'c above Max WAT Limit Tcnmcrature
Landing Distance Available 3735m /12254ft 3350m/l0991ft
Slope .66DN .20 UP
Notes Notes 1,2 Note 2
ManuaL VREF + 7kt 10kt 10kt
Manual VREF 10kt 10kt
Autoland VREF
Manual Slippery VREF 3kt 109.4
Autoland Slippery VREF
Fuel Saving Ldg Weight VREF
Red'n per extra kt TW 3500kg 3500kg
I IncperktHW 600kg
~
TOZSev 4848ft 4753ft
GS/HtatTHR
APPROACH DA DH/(HAT) RYR DA DH/(HAT) RVR
1ft) 1ft) (ft) (ft)
VORDME .. 5370
(522) 2.4km 5330 (5771 2.8km
TACAN .. 5370
(522) 2000m 5330 (5771 2.8km
Circling / Visual (radius 5.3nml .. 5700
(852) 4km 5700 (8521 4km
RWY DIRECTION 075"T 173"T
APPROACH WAY PT (15nm) N21" 24.7 N21· 45.3
E040·15.6 E040· 30.5
TOUCHDOWN WAY PT N21·28.6 N21· 30.4
E040· 31.3 E040· 32.5.
1. Approach LiDhts Rwy07: IFALS inop thefoDowing RVR applies:- TACAN 2400m.
2.LANDING WEIGHTS: Published landing weights must beadjusted forWAT limitations as specified
above, inaddition to normal HWrrw adjustments.
2. Approach Lights Rwy 25: IFAlS inop the following RVR's apply:·ILS 1200m, lLZ 2BOOm, VOR DME
2BOOm, TACAN 2800m.
3. ILS Rwy 35: IFMMinop CA 50300 HAT 255ft RVR 1200m applies.
4. Approach Lights Rwy 35: IFAlS inop the following RVR applies:- TACAN 4000m.
5. LANDING WEIGHTS: Published landing weights must beadjusted forWAT limitations asspecified
above, in addition to normal HW/TW adjustments.
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::=5 CONCORDE LANDING DATA QNH VAL O'OR
AID Elev 1106ft
Max wt Permitted (For pre flight planning) 111130kg
RUNWAY 18 36
STATUS (B)
WAT Umit: VREF / VREF + 71d 47°/47° 47"/47°
Landing Distance Available 3048m /1 OOOOft 3048m /1 OOOOft
Slope .04 UP .04DN
Notes
Manual VREF + 71d 1Old 10kt
Manual VREF 1Old 10kt
Autoland VREF
Manual Slippery VREF lkt lid
Autoland Slippery VREF
Fuel Saving Ldg Weight VREF
Red'n per extra IdTW 3500kg 3500kg
Incperkt HW
TDZElev 1104ft 1106ft
GS/HtatTHR 3°/69ft
APPROACH DA DH/(HAT) RVR DA DH/(HA1) RVR
(ft) (ft) (ft) (ft)
ILSCI . 1310 (2061 2600ft
ILSH No Flt/Dir . 1410 (306) 3500ft
LLZDME .. 1530 (4261 1.25sm
LLZ/DME (BB) .. 1590 (484) 1.25sm
VOR DME . 1590 (484) 1.25sm
VOR .. 1690 (586) 1.25sm
NDB . 1730 (624) 1.75sm
Circling / Visual (radius 5.3nm) . 1950 (844) 2sm 1950 (844) 2sm
RWY DIRECTION 169°T 349°T
APPROACH WAY PT(15nm) N48°18.6 N47°47.7
W077 °57.5 WOn042.4
TOUCHDOWN WAY PT N48" 03.9 N48°02.4
W077°47.2 WOn046.7
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