Preflight Calculations

PQU PA44-180 Piper Seminole

Weight Arm Moment
Basic Empty Weight 2540.02 86.14 218817.14 → AIRCRAFT WEB

1¥ :..¥
Pilot and Front Pax 140 + 2121AM ) 352 -
-
80.5 28336
UNF
STRAIGPROPORTI
HT ONALLY Pax (aft) 118.1

III
10 ( BAGGAGE BELONGINGS)
-

+
--

LINEARayy
:O:'t:O:S
Is

. Baggage (200 lbs max) "" 142.8

or
ZERO FUEL WEIGHT (1) 06.351M -:w=A )
o

(
-

§ .¥¥⇐
Fuel (Max 108 gal) Glbs +
.
648 95.0 61560
Ramp ' ' " "" " " '

43.77%9 ? 77%9%144
' '

Start/Taxi (2.67 gal) "" × .

, 95.0
-

TAKE OFF (2) s -03574 87.881MW -

-
Al -
314084.24A
) £17442
¥96642.24
Fuel to Dest. 10.2g lhrlengine 95.0
)
I .5hr -
-

30.99×6=183.6
-

LANDING (3) 3390.4 -0 87.491M-:w=A )

WRITE 0900 VARIATION

ENSURE TO FOR
MAGNETIC
VALVE ADDED
DEPARTURE DATA 41
936 (BFC) 08 0800/101515
'

Elevation: ______________ Active Runway:______________ Wind Velocity: ______________ MAKE SURE TO ADD
TAKE-OFF RUN AVAILABLE AERODROME CHART ORCFS
Round -
up
Alt. setting: ____________
30.24 "Hg TORA: _____________________ Hdwnd component: __________ →

y ( O W VARIATION
2500 1014-5 '
Is ok , °

TAKE OFF DISTANCE AVAILABLE AERODROME CHART OR CFS

-

Pressure Alt.: ___________

642 TODA: _____________________ Xwnd component:___________
'

2500 2145 '

TO WIND
Temperature ° C: ________2°C Density Altitude: ____________
-

1289 CFI: ________________________

N/A ( FOR THE PURPOSE OF FLIGHT TEST ) -
'

CLIMB DATA ③5-22 045-23

go ⑤ 5-24 '

1540 FPM
"

ROC (Both engines): ______________ S.E. Service Ceiling:___________

6100 Fuel Used:_________
1.59
]→EusurE
TAKE DIFFERENT

[ ROC (Single engine): ______________

To

Bog FROM FIELD ELE → CRUISING ALT .

S.E. Absolute Ceiling:__________

Time to climb:_______
.

'
310 FPM 7100 3.1mm
'

'

045-23 045-23 O Vyse .

-
-
Vyxe

DEPARTURE PERFORMANCE
⑦ 5-16
' '
770
'

065-15 Ground run:___________________________ Take-off distance over 50':_____________

1600
'

1800
'
085-13 Normal Accelerate Stop:__________________ Single Engine Service Ceiling:____________
6100 045-23
'

⑨ 5- 't Short Field Ground Run:__________________

710 Short field T/O distance over 50':________ ④ 5-18
' '
l 1150

IMMEDIATE LANDING (USE -110 WEIGHT)

' '

Ground Roll: ___________________________

435 Landing distance:______________________
1200

BASED ON ← DESTINATION DATA

TAF BIC
Elevation: ______________Active Runway:______________Wind Velocity: ______________
inn :*::
"
.
Alt. setting: ____________ TORA: _____________________Hdwnd component: __________
Pressure Alt.: ___________TODA: _____________________Xwnd component:___________
Temperature ° C: ________Density Altitude: ____________CFI: ________________________

DESTINATION PERFORMANCE ( USE LANDING WEIGHT)

' '
419
Ground Roll:___________________________ Landing Distance over 50': _______________
1200
:=-
⑦
rlI!lel) FVEL AND POWER CHART - LYCOMING (L) 0-366-E SERIES (PER ENGINE) "e"e
>-
<eI) ."e
_t::: ..... rlI!l
el)rlI!l 't':=
rlI!lO
0"
"3:
eI»
Press. Std. Alt.
Alt.
Feet
99 BHP - 55% Rated Power 117 BHP - 65% Rated Power
Temp. Approx. Fuel Aow-9.3 Gal/ Hr.- Approx. Fuel Aow-IO.3 Gal/Hr.'
°e RPM AND MAN. PRESS. RPM AND MAN. PRESS.
135 BHP - 75% Rated Power Press.
Fuel Flow-I 1.2 Gal/ Hr.- Alt.
RPM AND MAN. PRESS. Feet
=>
•e :=
-
2100 2200 2300 2400 2100 2200 2300 2400 2200 2300 2400 rlI!l:=
3:>
rlI!l:::
3:w
CllIH "e
SL 15 22.2 21.7 21.2 20.7 24.5 24.0 23.4 22.9 26.4 25.8 25.2 SL -""
o
rlI!l. 1000 13 21.9 21.4 21.0 20.4 24.2 23.7 23.1 22.6 26.1 25.5 24.9 1000
o 2000 II 21.6 21.1 20.7 20.2 23.4 25.2 24.6 2000
rlI!lO
:=::0 23.9 22.9 22.3 25.8 :=
_-.I
rlI!l 3000 9 21.3 20.8 20.4 19.9 23.6 23.1 22.6 22.1 25.4 24.9 24.4 3000 "e
o
-
!,"fIO :=
:!lei) 4000 7 21.0 20.6 20.1 19.7 23.2 22.7 22.3 21.8 FT 24.7 24.1 4000 :=
\oC
-.I
OQrlI!l
5000 5 20.8 20.3 19.9 19.4 22.9 22.4 22.0 21.5 - FT 23.8 5000
>
\0
y,-
6000 3 20.5 20.2 19.6 19.2 22.6 22.1 21.7 21.3 - - FT 6000 S
'2 7000 I 20.2 19.7 19.3 18.9 FT 21.8 21.5 21.0 7000 2
8000 -I 19.9 19.5 19.1 18.6 FT 21.2 20.7 8000
>
Cll
9000 -3 19.6 19.2 18.8 18.4 - - FT 20.5 9000
10,000 -5 19.3 18.9 18.5 18.1 - - - FT 10,000
rlI!l 11,000 -7 FT 18.6 18.3 17.9 11.000

12.000 -9 - FT 18.0 17.6 12.000

"e
:= 13.000 ·11 - - FT 17.4 13,000
rlI!l
rlI!l
"e 14,000 -13 - - - FT 4,000 :=
o
:=
:; NOTE: To maintain constant power. add approximately 1% manifold pressure for each 6°e above
""
Oel)
::erll!l

y.:
w
Ute
<
0'\
standard, subtract approximately 1% for each 6°e below standard.

-Best Power
>::2
20
rlI!lUt
SECTION 6 PIPER AIRCRAFT CORPORATION
WEIGHT AND BALANCE PA-44-180, SEMINOLE

3800
MAX TO AND ...
89 90 91 92 93

3700
LANDING WEIGHT 1 /
88
I
I I
3600
87/ I I
3600
86/ I I
86/
3400-eli
I I
3300
m
...J I I
3200
:x::
C) I I
3100 3:
iii
I I
3000
t:
c( I IPI
2900 -$
II:
()
I /;
c(

2800 .84
I
2700
\ 1 7$
2600
'1\
\ I I
2600
0
Co I I 2559 lbs

2400 --CIll
:\ 7 86,7 in

2300
\ ! 1
84 86 86 87 88 89 90 91 92 93
for empty
OM-ARC

C.G. LOCATION (INCHES AFT DATUM)

C.G. RANGE AND WEIGHT

Figure 6-15

REPORT: VB·860 ISSUED: MARCH 23, 1978

6-12 REVISED: MARCH I, 1980
 ③
"

uq., PA-44-180 ÷'w !i

..
↳
PRESSURE ALT .

'(l'"":;C'i.'l'MB'P'ERFORMANCE
o
Iii ii

, BOTH ENGINES '':Ii 0-

"=<' i
=
Example:
Press. alt.. 680 ft.
OPERATING - GEAR UP
2700 RPM & FULL
,,0
::Z
>Ul
= Outside air temp.. S·C
Weight: 3430 Ibs.
., , , , BOTH ENGINES .--'--....-
COWL FLAPS OPEN· WING FLAPS 0°
' Z

= "
."
o
Rate of climb: 1570 ft.l min. MIXTURE FULL RICH ABOVE 75%R
POWER & BEST POWER MIXTURE
BELOW 75% POWER :::+
:": 88 KIAS --.J

>
:2 BEST POWER MIXTURE LEANED 2soF
0' RICH OF PEAK E.G,T.
'"
(JQ

E;>=
n"O
•

-
t'2'J

-
"
C Il-

..
OCll -
:2

Z
'Il>'
,:0' ";6>
-="."
.
»

I
CIl FULL RICH liJ
o "',
,f': f':
'!' i!' . '!'
000
::>
=" "> 00-=

-
$'
,,=
_N
:::2
Z ::=
->
--
'00'00
QIllQlll
- 40 -30 -20 ·10 "
OUTSIDE AIR TEMPERATURE - ·C
0 tto 20 30 40 o 400 BOO 1200
RATE OF CLIMB - FEET/MINUTE
.
1600 2000
0-
e"'0
[!I!JZ
'
EACH SQUARE -
- 40
,,- ④ PA-44-180 au..u
-=
("'}
I.!J!'r:IJ !:""
we . . . ..
;::i
r:lJl.!J!' 3: CLIMB "'I.!J!'
I.!J!'O
0" PERFORMANCE
=>
"3: I.!J!'
... ONE ENGINE 0_
.. "
>>>
,,("'} "
0
IoJ! -.;
OPERATING r:IJ("'}
I.!J!'"
3:»
f=::c -GEAR UP
.Ow. "3:» '""'.
\
.'

2700 RPM FULl. THROTTLE

-1oJ!

--
-N
'Sl COWL FLAP OPEN 0
Z (OPERATING ENGINE) !:""("'}

.
1010 ("'} COWL FLAP CLOSEO l'J!SO

"
ClID..., I.!J!' (INOPERATIVE ENGINE)
-ClID MIXTURE FULl. RICH
'0'
"TJO
AIOVE 71" POWER 0
_·Z

.-"»
MIXTURE lEST
POWER IELOW
71" POWER
ril.!J!'
uoz
PROP FEATHERED ON
INOPERATIVE ENGINE 0
" 88 KIAS 0" FLAPS .z
UOz 1!.
3' ••• !lANK TOWARD
OPERATIVE ENGINE
I.!J!'
0
I.!J!'
- Example:
Press. alt.. 6S0 ft.

"-» ,--' Outside air temp.. SoC

Weight: 3430 lbs.

"
I.!J!'
Z
, Rate of climb: 340 ft.lmln. ."
l'J!S
0

"-<
:;
c:':l
•
c:':l
"
IoJ!
Or:IJ

'fl. 3:("'}
I.!J!' "I.!J!'
>-
= "e=: -40 -30 ·20 ·10 #
0 0 20 30 40 ·200 0 200
1
400 800
»:::1
2 0
NO.
wO ." RATE OF CLIMB - FEET/MINUTE
OUTSIDE AIR TEMPERATURE - °C
("'}Z
• tsIJ «It

EACH SQUARE 20
'
=
 ⑤
.
I.I'lID
wlIS .,.
o
PA-44-·180
FUEl, TIME AND DISTANCE TO CLIMB
BOtH ENGINES 2700 RPM" FULL THROTTLE WING FLAPS O' - COWL FLAPS OPEN
AIRPORT PRES
AIRPORT OAT
.
ALT
= -

20C
.
=
642
'

lIDn
"S!!:::!

..lID
-I
LANDING GEAR RETFIACTED CLIMB SPEED 88 KIAS
NO WIND
CRUISE PRES Ah =
4180
CQ
lIDZ
al: UI
< .

z>
'
4500

i
-

320

,...,1Ii. TSIN PRES Art .

.

: •.
'$"
'
CRUISE
FD
ALT OAT
AT 4500
.

'
= -
40C &l
g :§.
i
lIS
'IL
.-....
>

a
Sic
n_ :!
CIJ
'"
lIS
:5
CIJ_
VlI
.-1
Z :f\.'
lISCIJ &l lID
..CCIJ d
.,,'QI!1. Example:
",lID
n

e5
ClJlIS Airport press. alt.. 680 ft.
»
lISC
.. Airport outSide elr temp.. 8°C
Cruise press. alt.: 5500 ft.
J.."S!!

EH!
",00°' ,..-1
lISi: f!S Cruise outBlde air temp.: -2"C .... n
i:>
•• ""'i =
Fuel to climb: 2.5 minus 1.0 1.5 gal.
=
Time to climb: 4.5 minus 1.2 3.3 min. Ji
lISn
Ill: " Distance to climb: 7 minus 1.4 5.6 NM =
-w al:lID

--
Ji"J-
.........
'0.
-40 ·20 0
OUTSIDE AIR TEMPERATURE - "C
-

4
20 40
F I. '7 0.2
T
-
-

-
-
3.5
-

-
=

0.4--3.1
o
1.5g
min
F T D
- -
10 20
TIME DISTANCE AND FUEL TO CLIMB
30 40
->
2::3
go
!)1'12:
D 5.9-1.0--4.9 NM
-
-
 PIPER AIRCRAFT CORPORATION SECTION 5
SEMINOLE PERFORMANCE
⑥
133:1 - 30N'lfJ.Sla 110Y aNnOY£>
§ i §
I
0
:
0
E
N N .,.. II- UI
",II)
... 1-
Q 0
-fH
-- oZ
Yrlj-
E
-'Sf ... :lII:
0-ti -
Q
I I
::1 ",0
.. :flJ Z
H_
-- -- '.( I-.;.. , i
0
(ONIM ount liN 11
-:! -' i I ,.1
Ft
II
- I g
'" 0
Nil)
Z
:;)
§2
PI I
!i:
gUi
--
--
i
"<I
- 1
- - ,i'l.
- "41;-
...
f
-it!"
0
Ny
.
±⇐
- I
W
IX:
.
tt
.
' =p C(
n E t &ft .. tON
"" ... '" IX:
.
if
"
t - W
- -
--- -;p -
G-
:l:
Te ''
Ii oW
Not 't" l\
Q t
7
z
No I 88 88 I
-1-
I
E
E

2
E N
E3

= ..
, ff 0
"f
o
1- W
e
E = e D
er
IF
3
I
NORMAL PROCEDURE TAKEOFF GROUND ROLL (0° FLAPS)
Figure 5·9
ISSUED: MARCH 23, 1978 REPORT: VB·860
REVISED: SEPTEMBER 14, 1979 5·1S
 "

Airport PRESSURE,f?? 2%2

tII:a:I
':"I:!!J
O'-oe
Q
:a:I
2
Q
WIND COMPONENT
TIO WEIGHT
=

=
10kt ( HW )

3574
'

PA-44..180
⑦ I:!!JI:!!J
:::en
"l'l";
Q-
:::eO
='
-<
"::=
>
NORMAL PROCEDURE
TAKEOFF DISTANCE OVER 50 FT. BARRIER
::=2
> til
= I
ClO
l':""
oe
'F=I+l=t
WEIGHT LIFT OFF
2700 RPM 8t FULL THROTTLE BEFORE BRAKE RELEASE
BARRIER WING FLAPS O·
'J::±t:tu
·.Iiil. rlt::'
2
lie POUNDS SPEED KIAS SPEED KIAS pAVED leyEL DRY , ;t+.r:;::;:.rJ:t:: r':l
I:!!J
Q 3800 75 88 j-.... +- ....:p:.1 '.::±±±:
r':l -,
'1000
3400 71 83
88 78
d ..
CAUTION ;:
- t __ -t-'-o Best one engIne 'n--'-;-
__ :':-tt+-
,r,.,..-- "--I :,::':'::::::::
I:!!J
2800 62 73 ' oper.tive rate of ' J __ ,..., _
=0 *"a,Tmm'
>e
-.._. tffmC
climb •• I_thIIn60
FPM if T.O. wt. i. ,n '
- _ _ the ehaded ---

> " I -i..

HII+It11'!tIT'Pi+1HI " .:;':liIH11:IIUilL i0
-:e
liQ"1:!!J {
II:
oe
n-I:!!J ,
III
!:! oe
. t' ,,;.0
III
Z
Ii I:!!J
:::; 3000 0
_
:Ii
-
CIJ
CIJ
oe-
CIJCIJ
..'{r,'iI'ii ,fi:e
-
II: lli
II: C.L'
ID

ffi ->
:a:I
r':l
e > 2000 III
(.) "'Cl:=
I:!!J 2 ,¢
!;' """ ."l'l
r':l '.;..
I:!!J Iii
::= Q
''':0' is ':"r':l
QOQ
>
:a:I -<
I:!!J Example: .' , " . ,. , , ... WinifcicimpoOfint:5 'kt: headwInd ...
1000 u..
.::":::e
r':l :a:I A,rport press. alt: 6S0 ft. We,ght 3430 Ibs. ClJoe
::c OutsIde a'r temp.. S·C Total distance over 50 ft. bamer: 1750 ft.
I:!!JO
::=:e
-
til
<:>
ztm.am ->
I · t'

Is0
N
-40 ·20 20 40 3500 3000 2500 0 5 10 15
;:i OUTSIDE AIR TEMPERATURE - ·C WEIGHT - POUNDS WIND- KNOTS
2..;
Q-
l':""Q
- .I
ClO 1:!!J2
 "

Airport PRESSURE,f? ?
'
2%2
-
00
00
e o
Z
:=
WIND COMPONENT
TIO WEIGHT =
= 10kt ( HW )

3574
'

PA-44-180
④ >-
."I:l
Arfl
t-",
> NORMAL PROCEDURE - ACCELERATE ;>
e_
r" . AND STOP DISTANCE :=
> oon
:= := I I I
rfl:=
n o BOTH ENGINES 2700 RPM
::: n °NOTE
-"!l
oZ..,
REDUCE ACCEl. 80 STOP DIST. AND FULL THR01TlE
w I:'
BY 10% IF HEAVY DUTY
=... MIXTURE FUll RICH

-...,
BRAKES ARE INSTALLED. r"n
e i!! WING FLAPS O·
MAX. BRAKING rflO
:=
\0
QO
IU
Z
::;
COWL FLAPS OPEN
PAVED LEVEL DRY RUNWAY
ABORT SPEED 75 KIAS
'1.,."1:
o '"
"I:l

"Tl> .>'.,"
IU
_.n ,U
'Z IU
4000

.
OQ("j IU :z
nr"
"g;;
IU
::;
IU
U
lu
w
o
2
ili
.>.,
3000 I
w
u
['.I!j
sTD:TEMP".
>
:z 2000
C .
..,....
' '" Q
Example:
:= Alrpon pressure altitude: 680 ft. "e
o rfl
"I:l
Outside air temperature: S·C 1000 :=
o WeIght. 3430 lbs.

-..,
"!l
:= C Wind component: 5 kt. headwind 000
:; 00 Accel. & stop dist.. 2050 ft.
I! ! ! ! ! ! ! ! ! I! ! ! ! i ! "
I0
! I I ! I II ! ! ! I I ! I ! I ! I I! II
o >::!
< > -40 ·30 ·20 ·10 10 20 30 40 3500 3000 2500 5 10 15
=
til •
• QO
Z
("j
TEMPERATURE - ·C
-2
WEIGHT - POUNDS WIND COMPONENT - KNOTS 2 0
Z
nrfltll
f'I';l
\<ole
 "

2%2
⑥
Airport PRESSURE
-c::
,

I II III WIND COMPONENT = 10kt ( HW ) "'>-

="'=
III :::c WEIGHT
' ."'=
l'!!l
o TIO =
3574 &.l'!!l
t"::c
!;' ..., ;>
::
> -
"l'j
l'!!l
f""
C
=-
::c
g;n
n ->
:::c l'!!l 2"'fj
"l'j 0'"
"'fj LIFT OFF f""n
o
-
..,..,
PEED KIAS l'!!l0
::c ::c
-:-1...
I ,Q
70
"'=

''
ClIO 66
62
o
"Tl> 58
:lOOO ti
w .">.,
II
s::l'!!l

.. 52
u.
riO "'::;po 7 2500 I
U\"'fj = " , .....

-IO"IO\. '
2000 S
Ill:
,.Y'"",'C.':'
slOP'' ' ,

-B. .
::c 1500 C
o Z
c:: ;;, 1000 Ill:
:;)
o
2 ' . "",,'i:!::::--,
. --.--
C , <) - ' C1
';1 -=_._=- -'--..?'- .. "o
'
'

u.
500 u.
::c
of"" "T'
- o
l'!!l
•
,
, .
,,'t-;, :".::-- ---r-r-
o
W
lIl: -=
l'!!l
f""
....... !r' "o
"'fj

::cl'!!l
III

=' ::n
l
"'fj

y,f
< f""
>
"'=
-40 ·20
OUTSIDE AIR TEMPERATURE _ °C
0 20 40
l
3500 3000
WEIGHT - POUNDS
2500 0 5
WIND - KNOTS
10 15 >::2
20
n2
• QO
-llJ'I
--
III -

2
3574lb l'!!ly,
 SECTION 5 PIPER AIRCRAFT CORPORATION
PERFORMANCE PA-44-180, SEMINOLE
⑦ ÷
5
Es
'
=
¥

of
IT
E e
E E
EE

s.

¥
- -
E E
E = e D
E EF
3
①
SHORT FIELD EFFORT TAKEOFF DISTANCE OVER 50 FT.
BARRIER (0° FLAPS)
Figure 5-1:>
REPORT: VB-860 ISSUED: MARCH 23, 1978
5-18
 '
"" 642
3390.40
④ Airport PRESSURE,¥Y (
-

Lamina
-

an

ua:;e
N"'d
o
WIND COMPONENT
TIO WEIGHT
=

=
10kt HW )

3574
'
④ "'drJ'J
:;en
0-
PA-44-180 :=0
::::2
< Examp I:
1LANDING GROUND ROLL >UI
If' Alrpo rt press. alt.. 6S0 ft.
Out air temp.. soc BRAKES - ..
2
n
! Win component: 5 kts. headwind SHORT fiELD EffORT ' ,+-t t'l'

E""
We ,.: 3430 Ibs.
Lan ,lOg ground roll: 480 ft. l WING FLAPS 40° POWER OFF
....+
ff
'::1":._..;..
COWL FLAPS OPEN j ..

>
2
PAVED LEVEL DRY RUNWAY
o ltNOTE
REDUCE LANDING GROUND ROLL
BV 31% IF omONAl LANDING
FULL STALL TOUCHDOWN

GEAR HEAV\' DUTY GROUP NO.1

IS INSTAWD. ISEE EQUIPMENT
USTl
:!
..g
800
ri:;e SS· loti
VlO
m 0 ... Iii
"'d
f'i'l
J,..e
..... 2 III
i w :=
o - 0
Yo
>
,,- III
Z
II:
III
700 I
;;
. ::l n
::::I
:=
<rJ'J
_e Q ..;
III
III
11 g "'Cj:=
E""
E""
II:
..;
III
'J'() »."!l
II: ;)
tool
u:: 0

FIFE
0" •
II:
c:J -n
CleO
::>
>:;e 'fo '600
c:J
Z .?"
,,("'} is rJ'J"'d
n::c z4(
... ::::e
f'i'lQ

= :*
:eN ->
2,.,
|
.
,:a}N
-40 ·30 ·20 ·10 0 10 20 30 40 3600 13390 3000 2600 o 5 10 15 400 0-
OUTSIDE AIR TEMPERATURE - °C WEIGHT - POUNDS WIND COMPONENT - KNOTS E""Q
-2 t2l2
e Clll
 "
' "" "" """ ""
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oat
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