Saab 340 Limitations

Front 1

Max ramp weight

Back 1

29,300lbs

Front 2

Max takeoff weight

Back 2

29,000lbs

Front 3

Max zero fuel weight

Back 3

26,500lbs

Front 4

Max landing weight

Back 4

28,500lbs

Front 5

Max operating altitude

Back 5

25,000ft PA

Front 6

Flaps may be extended up to

Back 6

13,999 MSL

Front 7

Max tailwind component for takeoff and landing is

Back 7

10 kts

Front 8

Max operating speed (Vmo) from 0 to 16,000ft MSL

Back 8

250 KIAS

Front 9

Max operating speed (Vmo) at 25,000ft MSL

Back 9

210 KIAS

Front 10

Flaps extended speed (Vfe) for flaps 7 or 15 degrees

Back 10

175 KIAS

Front 11

Flaps extended speed (Vfe) for flaps 20 degrees

Back 11

165 KIAS

Front 12

Maneuvering speed

Back 12

180 KIAS

Front 13

Landing gear retraction speed (Vlor)

Back 13

150 KIAS

Front 14

Landing gear extension speed (Vloe)

Back 14

200 KIAS

Front 15

Landing gear extended speed (Vle)

Back 15

200 KIAS

Front 16

Emergency extension speed (Vloee)

Back 16

200 KIAS

Front 17

Rough air penetration speed (Vra) up to 21,000ft

Back 17

190 KIAS

Front 18

Rough air penetration speed (Vra) above 21,000ft

Back 18

Vmo pointer - 30 kts

Front 19

Minimum climb speed in icing conditions

Back 19

Vclean + 15 kts (160 KIAS best)

Front 20

Minimum en route speed in icing conditions

Back 20

160 KIAS

Front 21

Minimum approach speed with ice

Back 21

Vref + 10 kts

Front 22

Take off power with APR or go around (5 minutes max)

Back 22

107 percent torque
940 degrees C ITT

Front 23

Take off power with APR or go around (2 minutes max)

Back 23

107 percent torque
950 degrees C ITT

Front 24

Takeoff power (5 minutes max)

Back 24

100 percent torque
917 degrees C ITT

Front 25

Takeoff power (2 minutes max)

Back 25

100 percent torque
927 degrees C ITT

Front 26

Max continuous power (OEI)

Back 26

100 percent torque
940 degrees C ITT

Front 27

Transient except takeoff (max 12 seconds)

Back 27

112 percent torque
965 degrees C ITT

Front 28

Maximum ITT at engine start

Back 28

965 degrees C

Front 29

At takeoff power, what is the min-max engine oil pressure?

Back 29

30-100 psi

Front 30

At takeoff power, what is the min-max engine oil temperature?

Back 30

35-122 degrees C

Front 31

At takeoff power, what is the min-max propeller oil pressure?

Back 31

25-140 psi

Front 32

At takeoff power, what is the min-max propeller oil temperature?

Back 32

45-77 degrees C

Front 33

Total usable fuel per tank

Back 33

2845 lbs

Front 34

Total usable fuel (both tanks)

Back 34

5690 lbs

Front 35

Fuel temperature range

Back 35

-40 to +43 degrees C

Front 36

FUEL LOW TEMP light must be off for

Back 36

Takeoff

Front 37

For takeoff and landing X FEED and CONN VALVE shall be

Back 37

Off and closed

Front 38

Max fuel imbalance between tanks

Back 38

200 lbs

Front 39

Minimum oil temperature for starting

Back 39

-40 degrees C

Front 40

Prop RPM limitation on ground, unless needed for normal taxi

Back 40

1070-1220 rpm

Front 41

Two start attempts with fuel introduced require how much cooling between, and how much cooling before subsequent starts

Back 41

3 minutes and 25 minutes

Front 42

Three 30 second dry motoring with ______ cooling between each, then a ____ cooling period between subsequent starts or motoring

Back 42

3 minutes and 1 hour

Front 43

Time to lightoff from fuel introduction to ITT rise is

Back 43

20 seconds maximum

Front 44

Minimum time between starts is

Back 44

1 minute

Front 45

You must notify maintenance after ____ hung starts

Back 45

Two

Front 46

Takeoff is prohibited with with either L or R battery above

Back 46

64 degrees C

Front 47

Cross generator start with either L or R battery is prohibited above

Back 47

60 degrees C

Front 48

Battery start is prohibited with either L or R battery temp min/max

Back 48

Between -20 degrees C and +57 degrees C

Front 49

Minimum battery temperature for takeoff is

Back 49

-20 degrees C

Front 50

Max load on DC generators for 5 minutes is

Back 50

600 amps

Front 51

DC generator voltage range is

Back 51

27.5 to 29 volts

Front 52

External power voltage range is

Back 52

28 to 29.5 volts

Front 53

Takeoff is prohibited after a failed

Back 53

battery start

Front 54

Maximum tire ground speed is

Back 54

165 knots

Front 55

Min dispatch oxygen pressure below 10,000 ft MSL is

Back 55

800 psi

Front 56

Maximum cabin differential pressure is

Back 56

7.5 psi

Front 57

X VALVE use is limited to

Back 57

Ground operations only

Front 58

Aft supplemental air conditioning unit may not be used above

Back 58

17,500 ft MSL

Front 59

After an aborted takeoff with normal braking, _____ cooling time is adequate

Back 59

15 minutes

Front 60

Engine anti-ice must be ON when the plane is in visible moisture and the temperature is

Back 60

+10 degrees C or colder

Front 61

After exiting icing conditions, engine anti-ice must remain on for

Back 61

5 minutes

Front 62

During AP operations in icing conditions, the only vertical mode to be used during climb is

Back 62

FD/AP IAS

Front 63

When is AP and yaw damper operation not authorized

Back 63

Takeoff, landing, and go-around

Front 64

Minimum altitude for AP operations en route is

Back 64

500 ft AGL

Front 65

Minimum AP operating altitude for approaches is

Back 65

50 ft below MDA/DA

Front 66

Minimum autopilot operation altitude for takeoff or go-around is

Back 66

500 ft