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Aircraft/Flying > King Air 350 > Flashcards

King Air 350 Flashcards

0
Q

Engine failure

A 
• disengage the autopilot
• follow engine failure procedure
• retrim 
• re-engage autopilot
Dis-engage autopilot for large power or airspeed variations
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1
Q

GPU amps

A

1000 momentary

300 continuous

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2
Q

Engine fire or failure in flight

A
  • Condition lever…. Fuel cutoff
  • Prop lever…. Feather
  • Firewall fuel valve….Close
  • Fire extinguisher….Actuate if warning persists
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3
Q

Engine fire on the ground

A
  • Condition lever…Fuel cutoff
  • Firewall fuel valve….Close
  • Starter switch….Starter only
  • Fire extinguisher…Actuate if warning persists
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4
Q

Emer engine shutdown on the ground

A
  • Condition lever…Fuel cutoff
  • Prop lever…Feather
  • Firewall fuel valve…Close
  • Battery/Generators…Gang bar off
  • Battery bus…emer off
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5
Q

Engine failure during takeoff at or below V1 - abort takeoff

A
  • Power levers…ground fine

* Brakes….maximum

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6
Q

Engine failure during takeoff at it above V1 - take off continued

A
  • Vr speed….Rotate to approx 10 degrees pitch
  • Landing gear…up with a positive rate
  • Airspeed…V2 until 400’ AGL
  • Propeller….verify feathered with gauge
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7
Q

Engine failure in flight below Vmca

A
  • Power…reduce as needed to maintain control

* Nose…Lower to accelerate above Vmca

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8
Q

Electrical smoke or fire

A
  • O2 masks….Don
  • Mask selector switch…Emer position
  • Headset…Put back on or audio panel to speaker
  • Mic switches….O2 masks
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9
Q

Environmental system smoke or fumes

A
  • O2 masks…Don
  • Mask selector switch…Emer position
  • Headset…put back on or audio panel to speaker
  • Mic switches….O2 masks
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10
Q

Airstair/cargo door unlocked

A

• All occupants…seated with seat belts secure

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11
Q

Emergency descent

A
  • Power levers….Idle
  • Prop levers….Full forward
  • Flaps (202 KIAS max)….Approach
  • Landing gear (184 KIAS max)…Down
  • Airspeed….184 KIAS max
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12
Q

Glide

A
  • Landing gear…Up
  • Flaps….UP
  • Prop levers….Feathered
  • Airspeed….135 KIAS
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13
Q

Single inverter failure

A
  • AC bus circuit breakers…Check
  • If breaker is tripped….Reset
  • If cb not tripped..Select bus transfer for failed inverter
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14
Q

Dual inverter failure

A
  • Attitude/heading…use backup instruments

* AC bus circuit breakers…Reset if tripped

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15
Q

Dual generator failure

A
  • instrument emer lights…on if needed
  • Generators….Reset then on
  • if either generator resets…monitor
  • if neither resets…non-essential equipment off
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16
Q

Unscheduled electric pitch trim activation

A
  • Airplane attitude…maintain with elevator control

* AP/trim disconnect…depress fully

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17
Q

Unscheduled rudder boost activation

A
  • AP/trim disconnect…Depress to first level
  • Rudder boost switch…Off
  • If condition persists…pull rudder boost CB
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18
Q

Use of O2

A
  • Crew:
  • O2 masks…Don
  • Headset…put back on or audio panel to speaker
  • Mic switches…O2 masks
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19
Q

Loss of pressurization

A
  • O2 masks…Don
  • Headset…Put back on or audio panel to speaker
  • Mic switches….O2 masks
  • Passenger manual drop-out…Pull on
  • Altitude…Descend as required
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20
Q

High differential pressure

A
  • Bleed air valves…Environmental off
  • O2 crew and pax…As required
  • Altitude…descend as required to lower differential pressure
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21
Q

Auto- deployment oxygen system failure

A
  • Cabin Alt Hi annunciator illuminated with the Pas Oxy On annunciator extinguished:
  • Passenger manual drop-out….Pull on
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22
Q

Bleed air failure

A

• Bleed air valve affected side..Pneu & Envir off

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23
Q

Spins

A
  • Control column..Full forward/ailerons neutral
  • Rudder…Full opposite spin direction
  • Power levers…Idle
  • Rudder….Neutral when rotation stops
  • Elevator…smooth pull out from dive
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24
Q

Enhanced ground proximity warning system (EGPWS): verbal warning of “Terrain” or “Pull up”

A
  • Wings….Level
  • Power…max allowable
  • Pitch….20 - 25 degrees up till slowed to 125 KIAS
  • Airspeed…Maintain 125 KIAS
  • Gear and flaps…Up
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25
Q

Va

A

184 KIAS

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26
Q

Flaps approach speed

A

202 KIAS

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27
Q

Full flaps/Vfe

A

158 KIAS

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28
Q

Vlo (down)

A

184 KIAS

29
Q

Vlo (Up)

A

166 KIAS

30
Q

Vle

A

184 KIAS

31
Q

Vmca (flaps up)

A

94 KIAS

32
Q

Vmca (flaps approach)

A

93 KIAS

33
Q

Vmo ( sea level to 21,000)

A

263 KIAS

34
Q

Mmo (FL210 - FL350)

A

0.58 Mach

35
Q

Power lever limitations

A

Do not lift in flight ( moving them up over the flight gate into ground can cause a massive slow down and loss of aircraft control)

36
Q

Engine torque limitations

A

Take off: 100%
Max continuous: 100%
Transient: 156% for 20 seconds

37
Q

Max ITT limitations

A
  • Starting: 1000 degrees for 5 seconds
  • Idle: 750 degrees
  • Takeoff: 820 degrees
  • Max continuous: 820 degrees
  • Transient: 850 degrees for 20 seconds
38
Q

% N1 limitations

A
  • Minimum idle: 62%
  • Takeoff: 104%
  • Max continuous: 104%
  • Transient: 104%
39
Q

Prop limitations

A
  • Take off: 1700 RPM
  • Max continuous: 1700 RPM
  • Transient: 1870 RPM for 20 sec
  • Reverse: 1650 RPM
  • Min Idle: 1050 RPM
  • Sustained at 1768 RPM: primary governor is failed; limit torque to 96%
  • RPM more than 1768: primary and overspeed governors failed
40
Q

Auto-feather limitations

A

• Must be on for takeoff/climb/approach/landing

41
Q

Prop de-ice amps

A

26 - 32 amps is the green arc

42
Q

Oil pressure limitations

A
  • Starting: 0 - 200 PSI
  • Takeoff: 90 - 135 PSI
  • Max continuous: 90 - 135 PSI
  • Transient: 200 PSI
43
Q

Oil temperature limitations

A
  • Starting: -40 degrees
  • Takeoff: 0 - 110 degrees
  • Max continuous: 0 - 110 degrees
  • Transient: 0 - 110 degrees
  • Temps between 99 - 110 are limited to 10 minutes
44
Q

External power use limitations

A
  • Voltage: 28 - 28.4
  • Amps: 1000 momentary, 300 continuous
  • Battery should be on before turning on external power switch.
  • Never turn external power switch on when a generator is on line.
  • Battery must have 20 amps min to use external power.
45
Q

Generator limitations

A
  • Sea level to FL340: 100%
  • Above FL340: 95%
  • 62 - 70% N1: 75%
  • 70 - 100% N1: 100%
  • Increase N1 if using A/C on the ground.
46
Q

Starter limitations

A

30 seconds on, 5 minutes off, 30 seconds on, 5 minutes off, 30 seconds on, 30 minutes off

47
Q

Approved normal fuel

A

• Jet A, Jet A1, Jet B, JP 4, JP 5, JP 8

48
Q

Emergency fuel limitations (Avgas)

A
  • 150 hours max between engine overhauls
  • Not allowed if either standby pumps is inop.
  • Crossfeed capability is required above FL 200
49
Q

Fuel Capacity

A
  • Each main tank: 190 gallons/1273 pounds
  • Each aux tank: 79.5 gallons/533 pounds
  • Total: 539 gallons/3611 pounds
50
Q

Fuel management

A
  • Max allowable imbalance: 300#
  • Crossfeeding is only allowed when one engine is inop.
  • Takeoff prohibited if the main tank gauges are in the yellow arc (less than 265#)
  • Operation with low fuel pressure is limited to 10 hours between overhauls.
51
Q

Cabin differential gauge

A
  • Green arc: 0 - 6.6 psi

* Red arc: 6.6 - end of scale

52
Q

Pneumatic pressure gauge

A
  • Green arc: 12 - 20 psi

* Red line: 20 psi

53
Q

Vacuum gauge markings

A
  • Narrow green arc (15K - FL350): 2.8 - 4.3 inches Hg
  • Wide green arc (sea level - 15K): 4.3 - 5.9 inches Hg
  • 35K mark: 3.0 inches Hg
  • 15K mark: 4.3 inches Hg
54
Q

Max ramp weight

A

15,100 pounds

55
Q

Max takeoff weight

A

15,000 pounds

56
Q

Max landing weight

A

15,000 pounds

57
Q

Max zero fuel weight

A

12,500 pounds

58
Q

Max baggage area weight

A

550 pounds

59
Q

N344L operational weight

A

10,005 pounds

60
Q

N344L empty weight

A

9,465 pounds

61
Q

G limitations

A
  • Flaps up: -1.24 - +3.1

* Flaps down: 0.0 - +2.0

62
Q

Altitude limitations

A
  • Max….FL 350
  • Yaw damp inop….FL 190
  • One standby pump inop…use of avgas prohibited
  • Cross feed inop…FL 200 with avgas
63
Q

Max operating temperatures

A
  • Sea level to FL 250: ISA +37C

* Above FL 250: ISA +31c

64
Q

Rudder boost limitations

A

• Must be operational for all flights.

65
Q

Landing gear cycle limitations

A

• 1 up and down cycle every 5 minutes for a total of 6 cycles then a 15 minute cool down period.

66
Q

Icing limitations

A
  • Min temp for deice boot operation: -40C

* Min airspeed in sustained icing conditions: 140 KIAS

67
Q

Aft facing seat limitations

A

• Aft facing seats must be upright and the head rest fully extended for takeoff and landing.

68
Q

Autopilot limitations

A
  • Max speed: Vmo/Mmo
  • Min altitude in cruise: 1000 feet agl
  • Min altitude on approach: 200 feet agl
  • Use prohibited during takeoff and landing.
  • One pilot must be at the controls with seat belt fastened during autopilot operations.
  • Autopilot preflight checks must be satisfactory before each flight autopilot will be used on.
69
Q

Yaw damp limitations

A
  • Must be off for takeoff and landing.

* Must be operational for flights above FL190.

70
Q

EFIS limitations

A
  • The pilot EADI and EHSI must be operational in normal mode for takeoff.
  • Auxiliary drive may be used if the primary drive as failed.
  • The composite mode is to be used only after the failure of an EADI or EHSI.
  • The airspeed readout on the EADI is not to be used as the primary airspeed reference.

Aircraft/Flying (9 decks)

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