SAAB 340 A NORMAL CHECKLIST

PREFLIGHT DESCENT

External Power................................ Checked and On FO Cabin Pressure................................................... Set PM

Avionic/FMS .......................................................... ON FO CTOT..................................................... Set for GIA PM
Flight Instruments ........................... Checked and Set C/FO Landing Bugs................................ Checked and Set PF/PM
Engine Instruments/Ignition .......... Checked and OFF c Briefing ..................................................... Complete PF
Cabin Pressure ..................................................... Set FO

BEFORE START APPROACH

Parking Brake ....................................................... Set c Altimeters............................................... QNH_Set PF/PM

Cabin Signs........................................................... ON c Cabin Signs ........................................................ ON PM
Fuel .................................................. Checked KGS c Autocoarsen ....................................................... ON PM
Trim ....................................................... Set Units c
Power/Condition Levers.......... Ground Idle/Fuel OFF c LANDING
Briefing ........................................................ Complete PF
____CLEARED FOR START____ Landing Gear........................... Down, Three Green PF
Doors............................................................... Closed c Flaps .................................................................... 20 PF
Air Conditioning................................................... OFF c HP Valves ..................................................... Closed PM
Avionics................................................................. Set c Landing Signal............................................... Given PM
Beacon .................................................................. ON c
Hydraulic Pump................................................. AUTO c

AFTER START PARKING

Engine Instruments ...................................... Checked c Parking Brake .....................................................Set c

Ice Protection .......................................... As Required c Radar ............................................................. STBY FO
Autocoarsen .......................................................... ON c Ice Protection................................................... OFF FO
Air Conditioning................................................. AUTO FO Autocoarsen ·····················································oFF FO
Emergency lights ............................................. Armed FO Ignition .............................................................. OFF FO
Condition Levers ................................................. MAX c Beacon ·····························································oFF FO
Takeoff Bugs ................................... Checked and Set C/FO Generators........................................................ OFF FO
CWP/Overhead Caution Lights.................... Checked c Seatbelt Sign .................................................... OFF FO
Air Conditioning ................................................ OFF FO
BEFORE TAKEOFF Emergency Lights............................................. OFF FO
Hydraulic Pump ................................................ OFF FO
Flaps........................................................._ c Condition Levers....................................... Fuel OFF FO
Air Conditioning....................................... As Required FO
TIO signal.......................................................... Given FO
Flight Controls .............................................. Checked C/FO

AFTER TAKEOFF SECURE

Landing Gear ......................................................... Up PM Emergency Lights............................................. OFF FO

Flaps ...................................................................... Up PM Oxygen ·····························································oFF FO
Takeoff Inhibit ....................................................... Out PM Main lnverter..................................................... OFF FO
Autocoarsen ........................................................... Off PM FMS/Avionics.................................................... OFF FO
CTOT ..................................................................... Off PM Batteries ........................................................... OFF FO
Air Conditioning..................................................... Set PM External Power ................................................. OFF FO
Cabin Pressure ............................................ Checked PM Batteries ···························································oFF FO
 PREFLIGHT/FIRST FLIGHT GO-AROUND

Documents ................................................... Onboard FO Landing Gear ..................................................... Up PM

Technical Log ............................................... Checked c Flaps ··································································up PM
Gear handle ....................................................... Down FO Air Conditioning....................................... Set PM
Flap handle ............................................................ Up FO Autocoarsen....................................... As Required PM
Emergency / Safety Equipment.................... Checked FO CTOT ................................................ As Required PM
Circuit Breakers ............ Checked Left/Checked Right C/FO Fuel .......................................................... Checked C
Batteries ................................................................ On FO Inform PAX & FA .................................. Completed PM
External Power ................................ Checked and On FO
Avionics/FMS......................................................... ON FO
Side Panels ................................................ Checked C/FO
Oxygen ...................................................... ON/ 100% C/FO
Overhead panel ............................................ Checked FO
Test........................................................... Completed FO
Flight Instruments and Altimeters... Checked and Set C/FO
Engine Instruments and Ignition ... Checked and OFF c
Pedestal........................................................ Checked FO
Hydraulics and ANTISKID ..................... OFF and ON c
Cabin Pressure......................................................Set FO
Walk Around ............................................. Completed C/FO

EVACUATION

Parking brake.................................... Set c

Evacuation................................... Order c
Tower....................................... Notified FO
Battery Switches (both) ...................... OFF c
Condition Levers (both Off)......... Fuel OFF FO
Emergency Panel (all) Switches .......... ON FO
Fire Handles (both) ......................... PULL FO
Fire Extinguisher Switches (both)......... ON FO
 Gross mass correction factor, Flaps 15 and Flaps O (all bleed combinations)
Take-off Speed Increments (KIAS) Flaps 0
I
Type I, II and IV de-/anti-icing fluid
TJ£Pe II and IV de-/anti-icing fluid With power against brakes
Pressure Altitude from SL to 2000 ft. SPEED INCR. RUNWAY CONDITIONS
°
OAT( C) KTS DRY WET CONT/ LF
Mass (kg) -25 -20 -15 -10 -5 0 5 1 0.98 0.98 0.97
9000 0 0 0 0 0 0 0 2 0.97 0.96 0.93
9500 2 2 2 2 2 2 1 3 0.96 0.96 0.92
10000 5 4 4 4 4 3 2 4 0.96 0.95 0.91
10500 6 5 5 4 3 3 2 5 0.96 0.95 0.90
11000 5 5 4 4 3 2 2 6 0.95 0.94 0.89
11500 5 4 4 4 3 2 1 7 0.95 0.94 0.88
12000 4 4 4 3 2 2 1 8 0.94 0.94 0.87
12500 4 4 3 3 2 1 1 9 0.94 0.93 0.86
12700 4 3 3 3 2 1 0 10 0.94 0.93 0.85
Table 2B 11 0.93 0.92 0.84
12 0.93 0.92 0.83
13 0.92 0.91 0.82
Take-off Speed Increments (KIAS) Flaps 15 14 0.92 0.91 0.81
!Yotlde-/anti-icing fluid I
Without power against brakes
15 0.91 0.90 0.80
Pressure Altitude from SL to 2000 ft
OAT("C) Table 5
Mass {kl!) -25 -20 -15 -10 -5 0 5
9000 2 0 0 0 0 0 0
9500 2 0 0 0 0 0 0
10000 3 0 0 0 0 0 0 Takeoff distance correction factor, Flaps 15 and Flaps O (all bleed combinations)
10500 4 0 0 0 0 0 0
Type I, II and IV de-/anti-icing fluid
11000 5 0 0 0 0 0 0
11500 6 0 0 0 0 0 0
0 0 0 0
SPEED INCR. RUNWAY CONDITIONS
12000 6 2 0
12500 7 2 0 0 0 0 0 KTS DRY WET CONT/ LF
12700 6 2 0 0 0 0 0 1 1.07 1.09 1.10
2 1.13 1.15 1.16
Table JA
3 1.14 1.17 1.20
4 1.16 1.19 1.23
Take-off Speed Increments (KIAS) Flaps 15
!Yotlde-/anti-icing fluid I
With power against brakes
5
6
1.18
1.19
1.21
1.23
1.26
1.29
Pressure Altitude from SL to 2000 ft 7 1.21 1.25 1.32
OAT('CI 8 1.22 1.27 1.35
Mass (kg) -25 -20 -15 -10 -5 0 5 9 1.24 1.29 1.38
9000 0 0 0 0 0 0 0 10 1.26 1.31 1.41
9500 0 0 0 0 0 0 0 11 1.27 1.33 1.45
10000 0 0 0 0 0 0 0 12 1.29 1.35 1.48
10500 0 0 0 0 0 0 0 13 1.30 1.37 1.51
11000 0 0 0 0 0 0 0 14 1.32 1.39 1.54
11500 1 0 0 0 0 0 0 15 1.34 1.41 1.57
12000 2 0 0 0 0 0 0
12500 3 1 0 0 0 0 0 Table 6
12700 3 1 0 0 0 0 0
Table 36
 MAX CRUISE POWER MAX CRUISE POWER
1230 PRPM 1230 PRPM
ENG A/l OFF ECSON ENG A/l ON ECSON
FLT TORQUE (%) vs SAT (-C) TORQUE (%) vs SAT (-C)
FLT
LVL LVL
250
250
240
240
230
220 230
210 220
200 210
190 200
180
190
170
160 180
150 170
140 160
130 150
120 140
110 130
100 120
90 110
80 100
70 90
60 80
50 70
40 60
30 50
20 40
10 30
20
10
Note: The ITT limits for cruise are: 840 °C below 15 000 ft
850 °C at or above 15 000 ft
Note: The ITT limits for cruise are: 840 °C below 15 000 ft
850 °C at or above 15 000 ft
 MAX CLIMB POWER MAX CLIMB POWER
1230 PRPM 1230PRPM
140 KIAS 140 KIAS
ENG A/l OFF ECSON ENG A/l ON ECSON

FLT TORQUE (%) vs SAT (°C) CORR. FOR TORQUE (%) vs SAT (°C) CORR. FOR
DEVIATION FLT DEVIATION
FROM
LVL FROM
140 KIAS
LVL 140KIAS

250 250
240 240
230
230
220
210 220
210 ±1%
200 per
190 ±1% 200 20kts
180 per 190
170 30kts
180
160
170
150
140 160
130 150
120 140
110
130
100
90 120
80 110
70 100
60 ±1%
90
per ±1%
50 40kts 80 per
40 30kts
70
30
20 60
10 50
40
30
20
10
 MAX CONTINUOUS POWER MAX CONTINUOUS POWER
1384 PRPM 1384 PRPM
130 ± 20 KIAS 130 KIAS
ENG A/I OFF ECSON
ENG A/I OFF ECSOFF
TORQUE(%) VS SAT {° C) CORR. FOR
TORQUE(%) vs SAT ( ° C) FLT DEVIATION
FLT FROM
LVL
LVL -45 -40 -35 -3 0 -25 -20 -15 -10 -5 0 5 10 15 20 25 30 -45 -40 -35 -30 -25 -20 -15 -10 -5 0 5 10 15 20 25 30
130KIAS

150 89 90 90 89 87 85 83 81 78 74 71 67 64 250 59 58 57 55 54 51 49 46 43

140 93 94 94 93 91 89 87 84 81 78 74 70 67 240 62 61 59 58 56 54 52 49 46

130 96 97 97 96 95 93 91 88 85 81 77 73 70 66 230 64 63 62 61 59 57 55 52 49

120 100 100 100 100 99 97 95 92 89 85 81 77 74 70 220 67 66 65 64 62 60 57 55 52 49

110 100 100 99 96 93 89 85 81 77 74 70 66 210 69 69 68 67 65 63 60 58 54 51

100 HM) 100 97 93 89 84 80 77 73 70 200 72 72 71 70 68 66 63 60 57 54 51

90 ltMl 97 92 88 84 80 77 73 190 75 75 74 73 71 69 67 64 60 57 54
± 1%
80 100 95 92 88 84 80 76 180 78 78 77 76 74 72 70 67 64 60 57 per
70 100 99 96 92 88 84 80 170 81 82 81 79 78 76 73 70 67 63 60 55 20 kts
60 100 100 IIMI 96 92 87 83 160 84 85 84 83 81 79 77 74 70 66 63 59

50 100 95 91 87 150 87 88 87 86 84 82 80 77 73 69 66 63 59
40 IIHI 99 95 91 140 91 92 91 90 88 86 84 81 77 73 69 66 63
30 IOI> 99 94 130 95 95 95 93 92 90 88 84 80 77 73 69 66

20 100 98 120 98 99 99 97 95 93 91 88 84 80 76 72 69 65
10 ltMl
110 IIMI 100 IIHI l<Ml 99 98 95 92 88 84 80 76 72 68 65 62

99 95 91 87 83 79 75 72 69 65
,_1QQ_
100 100

ENG A/I ON ECSOFF 90 100 100 96 91 87 83 79 76 72 69

FLT TORQUE(%) vs SAT ('C) 80 100 96 91 87 83 79 76 72

LVL 100 95 91 87 83 79 75
-45 -40 -35 -30 -25 -20 -15 -10 -5 0 5 10 15 20 25 30
,_lQ_
150 87 86 85 83 82 79 76 72 68 65 62 60 100 99 95 90 86 83 78 ± 1%
per
140 91 90 88 87 85 83 80 76 72 68 65 50 100 HM) 99 94 90 86 82
30 kts
130 94 93 92 91 89 87 83 80 76 72 69 64 40 100 98 94 90 85

120 97 96 95 94 93 90 87 83 80 76 72 68 30 100 98 93 89
110 HHI 10<) 99 98 97 94 91 87 83 80 76 71 97 93
---1Q_
IOO

100 HM) 100 100 98 95 91 87 83 79 75

10 100 97
90 IIHI 99 95 91 87 83 78

80 IIHI 99 95 90 87 81
Note: Limited to ITT 917 °C
70 ltMl 99 94 90 84

60 100 98 93 87

50 IIMI 100 97 91

40 )0(1 95

30 100 99

20 ltHI

10 IIMI

Note: Limited to ITT 917 °C

 HOLDOVER TIMES FOR DE-ICING / ANTI-iCING FLUIDS
MAX CONTINUOUSPOWER Type II Fluid Type IV Fluid
1384PRPM Type I Fiuid (coiorfess) (green)
Weather mw
130±20KIAS Condition (orange or Type II Type II Type II Type IV Type IV Type IV
ENG A/l ON ECSON coiorless) 50\50 75\25 100 S0\50 75\25 100

FLT TORQUE (%) vs SAT ("C)

LVL

250
240
230
220 0:15- 0:25- 0:35- 0:15- 1:00- 1:20-
210 0:30 1:00 1:30 0:35 1:45 3:10
0:25- 0:20. 0:25-
200 Freezing Fog
0:50 1:05 0:50
0:20-
1:20
190 0:15- 0:15-
180 0:35 0:40

170 -3° and above

0:05- 0:15- 0:20- 0. 07- 0:30- 0:35-
0:15 0:30 0:45 0:15 0:55 1:15
160 Snow or
0:10- 0:20- 0:25-
Snow Grains/
150 Snow Pellets
0:20
0:15- 0:35 0:50
140 0:30
0:15-
0:30
130
0:08- 0:20- 0:30- 0:10- 0:35- 0:45-
120 Freezing 0:15 0:45 0:55 0:20 1:05 1:30
110 Drizzle
0:15- 0:20- 0:15- 0:20-
0:30 0:45
100 1:00 1:00
0:05- 0:10- 0:15- 0:07-
90 Light 0:09 0:25 0:30 0:10
0:25-
0:35
0:25-
0:40
Freezing
80 Rain 0:08- 0:10- 0:10- 0:10-
70 0:15 0:20 0:25 0:25
Rain on cold
60 Soaked Wing
+1° and above
0:05-
0:25
0:08-
0:40
0:09- 0:10-
0:50 1:15
50
40 Onestepde-icing/anti-icingoperation: Holdovertimebeginsatthestartofthede-icing/anti-icingoperation.
30 Twostepanti-icingoperation: Holdovertimebeginsatthestartoffinalanti-icingoperation.
20 Notes:
1. In lightrain and snowconditionsuse LightFreezingRain holdovertimes.
10 2. If positive identification of Freezing Drizzle is not possible. use Light Freezing Rain holdover times,
3. Noholdoyertimeguidelinesexistfor:Heavysnow,icepellets, hail,moderateandheavyfreezingrain.
4. Table holdover times range from moderate to light conditions.
Note: Limited to ITT 917 °C
Use of fluids below -25°C:
1 Type II and IVfluids may not be used below -25°C in active frost conditions.
2.Type IIandIVfluidmaybeusedbelow-25°C(exceptactivefrostconditions)providedtheLOUTofthefluid
is respected. ConsideruseofType I fluid/watermixturewhenType II or IVfluid cannotbe used.
Lowest Operational Use Temperature (LOUT)
The lowest operational use temperature (LOUTJ is the higher (warmer) of:
1.Thelowesttemperatureatwhichthefluidmeetstheaerodynamicacceptancetestfora givenaircrafttypeor
2 Thefreezingpointofthefluidplusthefreezingpointbufferof 10°CforType I fluidand7;CforType IIorIV

Remark: De-idng service provider shallrespect the LOUTandprovide de/anli-icing procedures accordingly.
 COLO TEMPERATURE ALTITUDE CORRECTIONS

Heiaht above the Elevationof the Altimeter settinQ source (feet)

Take-off Speed Increments (KIAS) �
AD
temp C 200 300 400 500 600 700 800 900 1000 1500 2000 3000 4000 5000
o·c 20 20 30 30 40 40 50 50 60 90 120 170 230 280 Tvne II and IV de-/anti-icing fluid I Without nower aaainst brakes
-1o·c 20 30 40 50 60 70 80 90 100 150 200 290 390 490 Pressure Altitude from SL to 2000 ft.
-2o·c 30 50 60 70 90 100 120 130 140 210 280 420 570 710 OATl C\
0

-3o·c 40 60 80 100 120 140 150 170 190 280 380 570 760 950 -25 -20 -15 -10 ·5 0 5
-4o•c 50 80 100 120 150 170 190 220 240 360 480 720 970 1210
Mass fkal
9000 11 2 0 0 0
-5o·c 60 90 120 150 180 210 240 270 300 450 590 890 1190 1500
6 3
9500 11 6 4 3 0 0 0
10000 10 6 5 4 1 0 0
10500 11 7 6 5 2 0 0
11000 12 8 7 6 3 1 0
11500 12 9 8 6 4 2 1
12000 12 9 8 7 5 3 2
CROSSWIND LIMITATIONS 12500 12 9 8 6 4 3 2
12700 10 8 7 5 4 2 1
Friction Max crosswind Nonnative FC ,_ I Table 1A
Braking action ---i---..
coefficient
0.40orabove
0.39-0.35
comoonent
35 kt
25 kt
Good
Medium to Good
/Russian FCl
0.60-0.55
0.54-0.45 I l " Take-off Speed Increments (KIAS) Flaps 15
0.34-0.30
0.29-0.25
20 kt
15 kt
Medium
Medium to Poor
0.44-0.40
0.39-0.35
'-I-l/ I\.
Tvne II and IV de-/anti-icing fluid
Pressure Altitude from SL to 200ft.
With nower aaainst brakes

0.24-0.20 5 kt Poor 0.34-0.30 I ,l's.

I\
Mass (ka) -15
OAT(0C)
below 0.15 0 kt Extremelv Poor below 0.30
X -25 -20 -10 -5 0
0

)JJ.. I
5
9000 0 0 0 0 0 0
f'\ I I>
o
9500 1 0 0 0 0 0 0
:
0
�I',.
' I/ ' I \v 10000
10500
1
3
0
0
0
0
0
0
0
0
0
0
0
0
/ 11000 4 1 0 0 0 0 0
I IV I\ I/\
v
0 11500 4 2 2 2 1 0 0
MAXIMUM CONTAMINATION DEPTH
12000 5 4 4 2 1
ON RUNWAY
..,._ l/i.// \ , .\- 12500 5 4
3 2
1 1
STANDING WATER 9 mm
I,V\/�
3 3 2
12700 5 4 2 1 0
'/
3 3
SLUSH 7mm V Table 1B
rt�/ _...!!L--1--
WET SNOW 10mm
DRY SNOW 14mm
::.--- L--..-

�"
,---e-�
� � • Take-off Speed Increments (KIAS) Flaps 0

Ji---..
.__,,r---. Tvoe II and IV de-/anti-icing fluid I Without aower a11ainst brakes
C -10 l Pressure Altitude. from SL to 2000 ft,
z
\ \\ � l's. /�
" ,I
I OATt°Cl

� -20
y �
/'
l'v �! "i-- Mass lko\
9000
-2 5
2
-20
1
-15 -10
1
-5
1
0
1
5
0
\ \ f \,/i'--r--,
1
I- 9500 4 4 4 4 4 3 3
10000 5 4
-30
_, v <i \,;\ I " 10500
6
7
6
7
6
6
6
6 5 4
3
3
11000 7 6 6 5 4
'y

10 lO 30 40 6 3
11500 7 6 6 5 4 3 2
12000 6 6 5 5 4 3 2
12500 6 6 5 5 3 2 2
12700 6 5 5 4 3 2 1
Table 2A