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Saab 340 > Limitations > Flashcards

Limitations Flashcards

1
Q

Max takeoff weight

A

29000 28500

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2
Q

Max landing

A

28500 27200

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3
Q

Max zero fuel

A

26500 25700

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4
Q

Vmo

A

250 16000 210 fl250

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5
Q

Vleo vle

A

200

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6
Q

Vlor

A

150

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7
Q

Vra

A

190kts up to FL210 then Vmo minus 30 KIAS

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8
Q

Va

A

180

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9
Q

Vfe

A

175 7 or 15 degrees

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10
Q

Vfe 20

Vfe 35

A

165

140

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11
Q

Max operating altitude

A

25000

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12
Q

Airport pressure altitude

A

-1,000ft (Pen Air -2,000 ft.) to 8,000ft

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13
Q

Temperature Envelope

A
  • 55oC to +47°C -1,000 to 1,500ft pressure altitude

- 60oC to -2oC FL 250​

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14
Q

Operational Limits

A

Operational Limits
Runway Slope
Takeoff -2% to +1.5%
Landing -2% to +2%

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15
Q

Load Limits

A

Load Limits
Flaps UP +2.75g to -1.0g
Flaps DOWN +2.0g to 0g

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16
Q

Max tail

A

10

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17
Q

Fuel Limitations

A 
Total useable fuel         5,690 lb.
Max fuel imbalance        200 lb.
Max refueling pressure    50 psi
Max defueling pressure    -15 psi
Fuel temperature    -40oC to +43oC
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18
Q

Windshield Wiper Operation

A

Low Mode 130 kts

High Mode 160 kts (Pen Air only uses High Mode)

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19
Q

Maximum differential cabin pressure

A

7.6 psi

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20
Q

Auto Mode maximum differential

A

7.1 psi

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21
Q

Max negative differential pressure

A

-0.5 psi

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22
Q

Max differential pressure for landing

A

0.2 psi

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23
Q

Max taxi weight A/B

A

29300 28800

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24
Q

Maximum Load DC Gen Elec

A

600 amps up to 5 min

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25
Q

Normal Load DC Gen Elec

A

400 amps

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26
Q

External Min Max voltage

A

28- 29.5 VDC

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27
Q

Max Current

A

1600 amp for engine start

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28
Q

min Current

A

1400 amp for engine start

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29
Q

Main Batterires

No Bat Start
Max temp for cross gen start
Max start for TO
Bat HOT Light

A

57 c
60 c
64 c
71 c

30
Q

Main Batteries

Min temp for TO
Min temp for engine start
Min emergency light bat temp for TO

A
  • 20 c
  • 20 c
  • 18 c
31
Q 
Autopilot
TO and GA
Enroute
Non Precision
ILS
A

200’ agl
500’ agl
50’ below MDA
70’ AGL

32
Q

Starter

Motoring

A

Two starts with three (3) minutes cooling between, then 25 minutes cooling before subsequent starts.

Motoring: Three 30-second ventilations with 3 minutes cooling between each, then a one-hour cooling period before subsequent starts or motoring.

33
Q

Time to light off

Max time with engaged starter engaged

A

Time to light-off (from initial Ng rotation to ITT rise), 20 seconds maximum.

Maximum time with engaged starter is 70 seconds of which max 30 seconds plain motoring.

34
Q

Flap Fault or Flap lights on

if flaps are split

A
  1. The split may be reduced by re-selecting previous flap setting
35
Q

HYDR Light on

If ember and main pressure are both Low
Caution leave flaps in actual position

When speed below 200 kts

A
  1. HYDR Pump Switch —Off
  2. Check Hydraulic Indicators
    If ember and main pressure are both Low
    Caution leave flaps in actual position
    When speed below 200 its
  3. Landing Gear Handle–Down
  4. Emerg LDG Handle— Pull
36
Q

Hydraulic Fluid Loss

A
  1. HYDR Pump Switch—-OFF
37
Q

No Light Up, start sequence Interupted, Hung start, Hot start

A
  1. Condition Lever—- Fuel Off
  2. Ign—— OFF
  3. Motor Engine to ITT below 175 c or for minimum of 10 seconds
38
Q

Engine Shutdown

A
  1. Power Lever—- Reduce to 20-30%
  2. Condition Lever—- Fuel OFF

ITT above 540c or combustion after shut down motor until 175c

Propeller not feathered ensure Auto coarsen switch is off and set propeller pump switch to main feather, hold until full featherd position

39
Q

Compressor Stall

A
  1. CTOT—-OFF
    • Turn CTOT knob gently fully counter clockwise then select CTOT switch OFF
  2. Power—Reduce to 20-30%
    • Retard Power Lever Slowly
40
Q

Uncommanded Engine Operation

A
  1. Power—–Reduce to 20-30%
    - If erratic TRQ indication set PL approx 1/2” above FLT IDLE

Caution keeping condition lever in T/M position will cause fuel to be vented overboard

  1. Condition lever—–T/M then Set
  2. Autocoarsen—-OFF
41
Q

Engine Fire

A
  1. Power Lever—–Reduce 20-30
  2. Condition Lever— Fuel OFF
  3. Fire Handle—– Pull
  4. Fire EXTG Switch—- ON

Fire still on after 30 sec, discharge fire EXTG on opposite side

Feather Prop, ensure auto coarsen switch is off and set pro pump switch to MAN Feather, hold until fully feathered

42
Q

Air Conditioning Smoke

A
  1. Oxygen Masks and Regulators—ON and 100%
  2. Smoke Goggles— ON
  3. Communications—- Establish
43
Q

Avionics or Electrical Smoke or Fire

A
  1. Oxygen Masks and Regulators—ON and 100%
  2. Smoke Goggles— ON
  3. Communications—- Establish
44
Q

Tailpipe Hot Light on

A
  1. Power Lever— Reduce
45
Q

Cargo Compartment Smoke

A
  1. Cargo Extinguisher switch—-ON
46
Q

Rapid Depressurization- Emergency Descent

A
  1. OX Mask and Regulators— ON and 100%

2. Communications—– Establish

47
Q

Both Engines Flame out

A
  1. Power Levers(both) —–Flight Idle
  2. Condition Levers—– Fuel OFF
  3. Airspeed—- 130 kias
  4. BAT switches—- OVRD
  5. Fuel STBY Pump switches—- OVRD
  6. Autocoarsen Switch—- OFF
  7. L condition Lever— Start
  8. Start Switch—– LH
48
Q

Engine Failure

A
  1. Power Power —- Reduce 20-30
  2. Condition Lever—- Fuel offCAUTION: If Propeller has not feathered, ensure AUTOCOARSEN switch is OFF and set PROPELLER PUMP Switch to MAN FEATHER. Hold switch until the propeller is in the fullfeathered position.
49
Q

Elevator System Jammed

A
  1. Auto Pilot—– Disengage
    Be prepared for trim transients
  2. Interconnect Unit
    Both pilots shall act on the controls the pilot on the side not failed can control the aircraft by overpowering the interconnect unit
  3. Pitch Disconnect Handle—- Pull
    The pilot on the side not failed can control the ac
50
Q

Aileron System Jammed

A
  1. AutoPilot ………………… DISENGAGE
    2. INTERCONNECT UNIT ……… OVERPOWER
    - Both Pilots shall act on the controls. The Pilot on the side not jammed can control the aircraft by overpowering the Interconnect Unit.
    3. ROLL DISCONNECT HANDLE ……………… PULL
    - The Pilot on the side not failed can control the aircraft.
51
Q

Loss of Both Generators (both engines running)

A
  1. BUS TIE switch …………. SPLIT
  2. LH GEN switch ……….. RESET then ON
    - Max two reset attempts.
  3. RH GEN switch ……………… RESET then ON
    - Max two reset attempts.
52
Q

Max Altitude for unpressurized flight

53
Q

Takeoff Power with APR
Max 5 minutes TRQ 107, ITT 940, RPM 102, 1396 Prop RPM
Max 2 minutes TRQ 107, ITT 950

54
Q

Takeoff Power
Max 5 minutes TRQ 100, ITT 917, E RPM 101, 1397
Max 2 Minutes TRQ 100, ITT 927,

55
Q

Config, water land

A

W 3 crew i obs, 28 Land 30, 33 or 34

56
Q

135 Payload

57
Q

Vmcl

A

106 flaps 20 and 35

58
Q

Dowety props avoid rpm on the ground

A

1070- 1220

59
Q

Prop speeds

A

1397 max, 1384 normal max, 1456 max continuous power for up to one hour

60
Q

Engine oil Max temp for 15 min
Min prop oil temp for ground ops and to after 5 min
max prop oil temp for 15 min

A

132 c
25 c
93 c

61
Q

Hydraulic temps light on and off

A

Light on 116, off 93

62
Q

Fuel anti ice additives

A

.06 to .15 % by by max volume

63
Q

Compartment temperature auto

A

18c to 29c

64
Q

Vertical speed up and down

A

2500 fpm max up

1500 fpm max dwn

65
Q

Cargo Fire Protection

A

70 min for aft lab two bottles
60 min fwrd lab two bottle
40 min external cargo two bottles
35 for all other

Basic 30-40

66
Q

AHRS Limits

A

not moved during initialization 70 sec
no TO if both EADI and stby are more than 3 degree
heading on the compass card is slewing away from ac
wait 2 mina after initialization

67
Q

FD

A

use of FD info in GA mode for TO is prohibited

68
Q

No Auto pilot

A

speeds below 1.3x stall in HDG mode

if in icing accretion vertical mode in climb IAS mode must be used

69
Q

No Yaw damp

70
Q

Flaps

A

normal landing before 300’

71
Q

STBY Pitot tube icing protection

A

obtained 5min after

72
Q

Radar limitations

A

180’ of other aircraft being refueled

90’ of personnel

Saab 340 (12 decks)

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