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King Air 350ER > King Air 350ER > Flashcards

King Air 350ER Flashcards

1
Q

Minimum Speed for Reverse?

A

40 kts

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2
Q

Vmca (Flaps Approach) ?

A

98 kts

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3
Q

Vmca (Flaps Up) ?

A

101 kts

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4
Q

Vsse (Intentional One Engine Inop) ?

A

135 kts

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5
Q

Vyse ?

A

135 kts

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6
Q

Vx ?

A

135 kts

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7
Q

Maximum Glide Range Speed ?

A

135 kts

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8
Q

Vy ?

A

135 kts

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9
Q

Minimum Speed in Flight in Sustained Icing ?

A

140 kts

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10
Q

Vfe (Landing Flaps) ?

A

158 kts

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11
Q

Vlo (Retraction) ?

A

164 kts

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12
Q

Vb (Turbulence Penetration) ?

A

170 kts

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13
Q

Va (Flaps Up) ?

A

182 kts

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14
Q

Vlo (Extension) ?

A

182 kts

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15
Q

Vfe (Flaps Approach) ?

A

202 kts

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16
Q

Maximum Air Speed for Windshield De-Icing?

A

226 kts

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17
Q

Vmo (Below 24,000 ft) ?

A

245 kts

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18
Q

Mmo (Above 24,000 ft) ?

A

.58 Mach

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19
Q

Maximum Ramp Weight?

A

16,600 lbs

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20
Q

Maximum Takeoff Weight?

A

16,500 lbs

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21
Q

Maximum Landing Weight?

A

15,675 lbs

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22
Q

Maximum Zero Fuel Weight?

A

13,000 lbs

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23
Q

Maximum Baggage Compartment Weight?

A

550 lbs

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24
Q

Maximum Persons on Airstair Door?

A

One Person

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25
Q

Rudder Boost Limitation?

A

Must be operational for all phases of flight

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26
Q

Starter Limitations?

A

30 seconds On, 5 minutes Off
30 seconds On, 5 minutes Off
30 seconds On, 30 minutes Off

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27
Q

Propeller De-Ice Ammeter Limits?

A

26 to 32 amps (Normal Range)

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28
Q

Cabin Altimeter and Differential Limits?

A

6.6 psig (Maximum Cabin Differential)

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29
Q

Maximum ITT Limit Low Idle?

A

750°C

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30
Q

Maximum Reverse ITT Limit?

A

760°C

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31
Q

Recommended Cruise Climb ITT Limit?

A

785°C

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32
Q

Maximum Cruise ITT Limit?

A

820°C

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33
Q

Takeoff and Maximum Continuous ITT Limit?

A

820°C

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34
Q

Maximum Transient ITT Limit?

A

850°C for 20 seconds

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35
Q

Maximum ITT during Starting?

A

1000°C for 5 seconds

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36
Q

Oil Temperature Limit during Starting and Low Idle?

A

-40°C to 110°C

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37
Q

Normal Oil Temperature Limits?

A

0°C to 99°C

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38
Q

Maximum Oil Temperature Limit?

A

110°C

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39
Q

Maximum Transient Oil Temperature Limit?

A

99°C to 110°C for 10 minutes

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40
Q

Recommended Oil Temperature for Fuel Heater Operations at Takeoff?

A

55°C

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41
Q

Minimum Oil Pressure at Low Idle?

A

60 psi

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42
Q

Oil Pressure Caution Range?

A

60 to 90 psi (Torque Limited to 62%)

43
Q

Normal Oil Pressure Operating Range?

A

90 to 135 psi

44
Q

Maximum Starting Oil Pressure Limit?

45
Q

Normal Pneumatic Pressure Operating Range?

A

12 to 20 psi

46
Q

Maximum Pneumatic Pressure Limit?

47
Q

Normal Torque Operating Range?

A

0 to 100% (1000 to 1700 rpm)

48
Q

Maximum Transient Torque Limit?

A

156% (for 20 seconds)

49
Q

Maximum Torque Limit with Props Above 1700 rpm?

50
Q

Inadvertent Torque Excursions up to _______% are time limited to _____ minutes?

A

102%

7 minutes

51
Q

Minimum N1 Turbine Tach Speed at Low Idle?

52
Q

Maximum N1 Turbine Tach Speed?

53
Q

Maximum Transient N1 Turbine Tach Speed?

54
Q

Maximum DC Power Limit between 62% and 70% Torque?

55
Q

Maximum DC Power Below 34,000 feet?

56
Q

Maximum DC Power Above 34,000 feet?

57
Q

Normal Volts DC Power?

A

27.5 to 29 VDC

58
Q

Minimum Prop RPM Limit at Idle?

59
Q

Normal Prop RPM Operating Range?

A

1450 to 1700 RPM

60
Q

Maximum Prop RPM in Reverse?

61
Q

Maximum Prop RPM ?

62
Q

Maximum Prop RPM Transient?

A

1870 RPM for 5 seconds

63
Q

Prop RPM range to avoid during Ground Operations?

A

400 to 1050 RPM

64
Q

Maximum Fuel Imbalance?

65
Q

Minimum Fuel in each Main for Takeoff?

66
Q

Maximum Operating Time with the Fuel Press Light Illuminated?

67
Q

Maximum Usable Fuel Quantity?

A

775 gallons/5192 lbs

68
Q

Approximate Range with Full Fuel?

69
Q

Approximate Endurance with Full Fuel?

70
Q

Maximum Operating Altitude?

A

35,000 feet

71
Q

ENGINE FIRE/FAILURE IN-FLIGHT

A

1 CONDITION LEVER - CUTOFF
2 PROPS - FEATHER
3 FIREWALL VALVE - CLOSE
4 EXTINGUISHER (IF FIRE WARNING PERSISTS) - ACTUATE

72
Q

ENGINE FIRE ON THE GROUND

A

1 CONDITION LEVER - CUTOFF
2 FIREWALL VALVE - CLOSE
3 STARTER - STARTER ONLY
4 EXTINGUISHER (IF FIRE WARNING PERSISTS) - ACTUATE

73
Q

EMERGENCY ENGINE SHUTDOWN ON THE GROUND

A 
1  CONDITION LEVERS - CUTOFF
2  PROPS - FEATHER
3  FIREWALL VALVES - CLOSE
4  MASTER SWITCH - OFF
5  BATT BUS - EMER OFF
6  ESIS - OFF
74
Q

TAKEOFF ABORT

A

1 POWER- GROUND FINE

2 BRAKES - AS REQUIRED

75
Q

ENGINE FAILURE TAKEOFF CONTINUED

A 
1  Vr - ROTATE 
2  POWER - MAX ALLOWABLE 
3  GEAR - UP
4  AIRSPEED - V2 TO ACCEL HEIGHT (400FT MIN AGL)
5  PROP (INOP ENG) - VERIFY FEATHERED
76
Q

ENGINE FAILURE IN FLIGHT BELOW MINIMUM CONTROL SPEED (Vmca)

A

1 POWER - REDUCE AS REQUIRED TO MAINTAIN CONTROL

2 NOSE - LOWER TO ACCELERATE ABOVE Vmca

77
Q

ELECTRICAL FIRE OR SMOKE

A

1 OXYGEN MASK(S) - DON
2 MASK SELECTOR SWITCH - EMER
3 MIC SWITCH(ES) - OXY

78
Q

ENVIRONMENTAL SMOKE/FUMES

A

1 OXYGEN MASK - DON
2 MASK SELECTOR SWITCH - EMER
3 MIC SWITCH - OXY

79
Q

AIRSTAIR DOOR/CARGO DOOR UNLOCKED

A

1 ALL OCCUPANTS - SEATED WITH SEATBELTS SECURELY FASTENED

80
Q

EMERGENCY DESCENT

A 
1  POWER LEVERS - IDLE
2  PROPS LEVERS - FULL FORWARD 
3  FLAPS (202 KTS MAX) - APPROACH
4  LANDING GEAR (182 KTS MAX) - DOWN
5  AIRSPEED - 182 KTS MAX
81
Q

GLIDE

A

1 LANDING GEAR - UP
2 FLAPS - UP
3 PROP LEVERS - FEATHERED
4 AIRSPEED - 135 KTS

82
Q

USE OF OXYGEN

A

1 OXYGEN MASK(S) - DON

2 MIC SWITCH(ES) - OXY

83
Q

PRESSURIZATION LOSS

A

1 OXYGEN MASK(S) - DON
2 MIC SWITCH(ES) - OXY
3 PASSENGER MANUAL DROPOUT - PULL ON
4 DESCEND - AS REQUIRED

84
Q

HIGH DIFFERENTIAL PRESSURE

A

1 BLEED AIR VALVES - ENVIR OFF
2 OXYGEN (CREW AND PASSENGERS) - AS REQUIRED
3 DESCEND - AS REQUIRED

85
Q

AUTO DEPLOYMENT OXYGEN SYSTEM FAILURE

A

1 PASSENGER MANUAL DROPOUT - PULL ON

86
Q

DUAL GENERATOR FAILURE

A

1 INSTRUMENT EMERGENCY LIGHTS (IF REQUIRED) - ON
2 MISSION POWER SWITCH - OFF
3 NEBULA POWER SWITCH (IF INSTALLED) - OFF
4 GENERATORS - RESET, THEN ON
If either generator will reset
5 OPERATING GENERATOR LOADMETER - MONITOR
If neither generator will reset
6 ECS MODE - OFF
7 COCKPIT/CABIN BLOWER - AUTO
8 NON-ESSENTIAL EQUIPMENT - OFF

87
Q

BLEED AIR FAIL

A

1 BLEED AIR VALVE (AFFECTED ENGINE) - PNEU & ENVIR OFF

88
Q

SPINS

A

1 CONTROL COLUMN - FULL FORWARD, AILERONS NEUTRAL
2 FULL RUDDER - OPPOSITE THE DIRECTION OF THE SPIN
3 POWER LEVERS - IDLE
4 RUDDER - NEUTRALIZE WHEN ROTATION STOPS
5 EXECUTE A SMOOTH PULLOUT

89
Q

UNSCHEDULED ELECTRIC PITCH TRIM ACTIVATION

A

1 AIRPLANE ATTITUDE - MAINTAIN USING ELEVATOR CONTROL

2 AP/TRIM DISCONNECT - DEPRESS FULLY AND HOLD [TRIM] ILLUMINATED

90
Q

UNSCHEDULED RUDDER BOOST ACTIVATION

A

1 AP/TRIM DISCONNECT - DEPRESS TO 1ST LEVEL AND HOLD
2 RUDDER BOOST - OFF
If condition persists
3 YD/AP DISC (ON FLIGHT GUIDANCE PANEL) - PULL DOWN

91
Q

AUTOPILOT MISTRIM [E] OR [A]

A

1 FLIGHT CONTROLS - HOLD FIRMLY

2 AP - DISENGAGE

92
Q

AUTOPILOT TRIM FAIL [TRIM]

A

1 FLIGHT CONTROLS - HOLD FIRMLY

2 AP - DISENGAGE

93
Q

AUTOPILOT AUTOMATIC DISENGAGEMENT

A

1 MAINTAIN AIRPLANE CONTROL

2 AP/TRIM DISCONNECT - DEPRESS TO 1ST LEVEL TO CANCEL HORN

94
Q

EGPWS TERRAIN WARNING

A 
In IMC or at night
1  WINGS - LEVEL
2  POWER - MAX ALLOWABLE 
3  PITCH - INCREASE, ADJUST TO MAINTAIN 135 KIAS
4  GEAR AND FLAPS - UP
95
Q

Max Temperature Limit Sea Level to 25,000’ ?

A

ISA +37°C

96
Q

Max Temperature Above 25,000’ ?

A

ISA +31°C

97
Q

Pneumatic Boot Limit?

A

No Operations Below -40°C

98
Q

G Load Limitations Flaps Up?

A

-1.21 to 3.01

99
Q

G Load Limitations Flaps Down?

A

0.0 to 2.0

100
Q

DC Power Limitation at 62% to 70% Tach N1 Speed?

A

75% Maximum

101
Q

Maximum DC Power Below 34,000’ ?

102
Q

Maximum DC Power Above 34,000’ ?

103
Q

Normal VDC ?

A

27.5 to 29.0 VDC

104
Q

Maximum Crosswind for Takeoff?

King Air 350ER (1 decks)

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