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Revised King Air > Limits > Flashcards

Limits Flashcards

1
Q

MIN CREW

A

ONE PILOT

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2
Q

PAX SEATING LIMITATIONS

A

15 PAX MAX

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3
Q

LOAD FACTOR FLAPS DOWN NEGATIVE

A

0 Gs

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4
Q

LOAD FACTOR FLAPS DOWN POSITIVE

A

1.1 Gs

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5
Q

LOAD FACTOR FLAPS UP NEGATIVE

A

-1.24 Gs

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6
Q

LOAD FACTOR FLAPS UP POSITIVE

A

3.1 Gs

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7
Q

MAX OPERATING ALTITUDE WITH AVGAS AND BOTH STBY BOOST PUMPS OPERATIVE

A

35,000 FT

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8
Q

MAX OPERATING ALTITUDE

A

35,000 FT

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9
Q

MAX OPERATING ALTITUDE AVGAS EITHER STBY BOOST PUMT INOP

A

FLIGHT PROHIBITED

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10
Q

MAX ALLOWABLE TAKEOFF WEIGHT

A

15,000 LBSOR AS LIMITED BY:-TAKEOFF CLIMB REQUIREMENTS-TIRE SPEED-BRAKE ENERGY-TAKEOFF FIELD LENGTH

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11
Q

MAX LANDING WEIGHT

A

15,000 LBSOR AS LIMITED BY:-MAX LANDING WIEGHT TO ACHIEVE CLIMB GRADIENTS-MAX LANDING DISTANCE - FLAPS DOWN

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12
Q

MAX RAMP WEIGHT

A

15,100 LBS

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13
Q

MAX ZERO FUEL WEIGHT

A

12,500 LBS

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14
Q

EMERGENCY AIRSPEEDS (15,000 LBS)ONE ENGINE INOP BEST ANGLE OF CLIMB (VXSE)

A

125 KIAS

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15
Q

EMERGENCY AIRSPEEDS (15,000 LBS)ONE ENGINE INOP BEST RATE OF CLIMB (VYSE)

A

125 KIAS

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16
Q

EMERGENCY AIRSPEEDS (15,000 LBS)ONE ENGINE INOP ENROUTE CLIMB

A

125 KIAS

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17
Q

EMERGENCY AIRSPEEDS (15,000 LBS)AIR MIN CONTROL SPEED (VMCA): FLAPS UP

A

94 KIAS

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18
Q

EMERGENCY AIRSPEEDS (15,000 LBS)AIR MIN CONTROL SPEED (VMCA): FLAPS APPROACH

A

93 KIAS

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19
Q

EMERGENCY AIRSPEEDS (15,000 LBS)EMERGENCY DESCENT SPEED

A

184 KIAS

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20
Q

EMERGENCY AIRSPEEDS (15,000 LBS)MAX RANGE GLIDE SPEED

A

135 KIAS

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21
Q

MAX DEMO’D CROSSWIND

A

20 KTS

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22
Q

MAX TAILWIND

A

10 KTS

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23
Q

SINGLE ENGINE ENROUTE CLIMB

A

125 KIAS

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24
Q

MANEUVERING SPEED (VA)

A

184 KTS

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25
Q

MAX FLAP EXTENSION/EXTENDED SPEED (VFE) APPROACH

A

202 KIAS

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26
Q

MAX FLAP EXTENSION/EXTENDED SPEED (VFE) FULL

A

158 KIAS

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27
Q

MAX LANDING GEAR EXTENDED SPEED (VLE)

A

184 KIAS

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28
Q

MAX LANDING GEAR OPERATING SPEED (VLO) EXTENSION

A

184 KIAS

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29
Q

MAX LANDING GEAR OPERATING SPEED (VLO) RETRACTION

A

166 KIAS

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30
Q

AIR MIN CONTROL SPEED (VMCA) PROP FEATHERED FLAPS UP

A

96 KIAS

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31
Q

AIR MIN CONTROL SPEED (VMCA) PROP FEATHERED FLAPS APPROACH

A

94 KIAS

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32
Q

MAX OPERATING SPEED (VMO)

A

263 KIAS/0.58 MACH

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33
Q

AIRCRAFT HEIGHT

A

14’ 4”

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34
Q

AIRCRAFT LENGTH

A

46’ 8”

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35
Q

AIRCRAFT WINGSPAN

A

57’ 11”

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36
Q

AFT FACING SEATS TAKEOFF RESTRICTION

A

IF OCCUPIED FOR T/O, HEADRESTS MUST BE FULLY EXTENDED

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37
Q

AUTOPILOT MAX COUPLED INTERCEPT ANGLE FOR BACK COURSE

A

70°

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38
Q

AUTOPILOT MAX COUPLED INTERCEPT ANGLE FOR NAV/LOC

A

LESS THAN 90°

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39
Q

AUTOPILOT MIN ALT FOR APPROACH

A

79 FT AGL

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40
Q

AUTOPILOT MIN ALT FOR CRUISE

A

1,000 FT AGL

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41
Q

AUTOPILOT MIN ALT FOR STEEP APPROACH

A

160 FT AGL

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42
Q

Below ______ volts, battery must be recharged prior to attempting engine start.

A

20 VDC

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43
Q

EXTERNAL POWER AMPS LIMITS: MOMENTARY

A

1,000 AMPS

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44
Q

EXTERNAL POWER AMPS LIMITS: CONTINUOUS

A

300 AMPS

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45
Q

EXTERNAL POWER VOLTAGE RANGE

A

28 TO 28.4 VOLTS

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46
Q

GENERATOR LOAD LIMITS ABOVE 34,000 FT

A

95%

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47
Q

GENERATOR LOAD LIMITS IN GROUND AT 62%-70% N1

A

75%

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48
Q

GENERATOR LOAD LIMITS IN GROUND AT 70%-100% N1

A

100%

49
Q

GENERATOR LOAD LIMITS SL TO 34,000 FT

A

100%

50
Q

MIN BATTERY VOLTS FOR BATTERY START

A

23 VDC

51
Q

STARTER DUTY CYCLE

A

-30 SEC ON/5 MIN OFF-30 SEC ON/5 MIN OFF-30 SEC ON/30 MIN OFF

52
Q

For fuel system, fill the _______ tanks first.

A

MAIN

53
Q

For fuel system, do not takeoff if fuel gauges in the ______ arc or indicate less than _____ lbs in each wing system.

A

YELLOW265

54
Q

FUEL CROSSFEED PERMITTED ONLY WHEN

A

ONE ENGINE INOP

55
Q

MAX FUEL IMBALANCE

A

300 LBS

56
Q

AUX SYSTEM FUEL QUANTITY

A

79.5 U.S. GAL / 533 LBS

57
Q

MAIN SYSTEM FUEL QUANTITY

A

190 U.S. GAL / 1,273 LBS

58
Q

TOTAL USABLE FUEL QUANTITY

A

539 U.S. GAL / 3,611 LBS

59
Q

WHEN IS ENGINE ANTI-ICE REQUIRED?

A

+5° C IN VISIBLE MOISTURE…NOT permitted for T/O operations above 10C

60
Q

MIN TEMP FOR DEICING BOOTS OPERATIONS

A

-40° C

61
Q

MIN AIRSPEED FOR SUSTAINED OPS IN ICING

A

140 KTS

62
Q

MAIN LANDING GEAR STRUT EXTENSION (INCHES)

A

3.23 TO 3.49 INCHES

63
Q

NOSE LANDING GEAR STRUT EXTENSION (INCHES)

A

3.77 TO 4.06 INCHES

64
Q

BRAKES DEICE TEMP OPERATION LIMITE

A

NOT ABOVE 15° C

65
Q

LANDING GEAR CYCLE LIMITS

A

1 CYCLE (UP/DOWN) EVERY 5 MIN FOR TOTAL OF 6 FOLLOWED BY 15 MIN COOL-DOWN

66
Q

MAX CABIN PRESSURE DIFFERENTIAL

A

6.6 PSI

67
Q

CABIN DIFFERENTIAL PRESSURE (GREEN ARC)

A

0 TO 6.6 PSI

68
Q

CABIN DIFFERENTIAL PRESSURE (RED ARC)

A

6.6 PSI AND UP

69
Q

When does the “CABIN ALTITUDE” light illuminate?

A

ABOVE 10,000 FT CABIN ALT

70
Q

When does the “CABIN ALTITUDE HI” light illuminate?

A

ABOVE 12,000 FT CABIN ALT

71
Q

When do the passenger mask automatically deploy?

A

ABOVE 12,500 FT CABIN ALT

72
Q

Cabin altitude is limited to _____ Ft as long as air is coming into pressure vessel.

A

13,000 FT

73
Q

The “CABIN DIFF HI” light illuminates at what PSID?

A

6.9 PSID

74
Q

ENGINE MODEL NUMBER AND TYPE

A

PT6A-60A, TURBOPROP

75
Q

PROPELLER TYPE

A

CONSTANT-SPEED, FULL-FEATHERING, REVERSING, COUNTER-WEIGHTED, AND HYDRAULICALLY ACTUATED

76
Q

MAX N1 CRUISE CLIMB

A

104%

77
Q

N1

A

62% MIN

78
Q

MAX N1 MAX CRUISE

A

104%

79
Q

MAX TRANSIENT N1

A

104%

80
Q

MAX ITT CRUISE

A

820° C

81
Q

MAX ITT CRUISE CLIMB

A

785° C

82
Q

MAX ITT IDLE

A

750° C

83
Q

MAX CONTINUOUS ITT

A

820° C

84
Q

MAX ITT REVERSE

A

760° C

85
Q

ENGINE STARTING MAX TRANSIENT ITT

A

1,000° C FOR 5 SEC

86
Q

MAX TAKEOFF ITT

A

820° C

87
Q

ENGINE MAX ITT TRANSIENT

A

850° C FOR 20 SEC

88
Q

NORMAL OIL PRESSURE FOR CRUISE CLIMB

A

90 TO 135 PSI

89
Q

ENGINE OIL PRESSURE IDLE

A

60 PSI MIN

90
Q

MAX CONTINUOUS OIL PRESSURE

A

90 TO 135 PSI

91
Q

MAX CRUISE OIL PRESSURE

A

90 TO 135 PSI

92
Q

MAX REVERSE OIL PRESSURE

A

90 TO 135 PSI

93
Q

ENGINE OIL PRESSURE STARTING

A

0 TO 200 PSI

94
Q

NORMAL TAKEOFF OIL PRESSURE

A

90 TO 135 PSI

95
Q

ENGINE OIL PRESSURE TRANSIENT

A

200 PSI

96
Q

ENGINE OIL TEMP CRUISE CLIMB

A

0° TO 110° C

97
Q

ENGINE OIL TEMP IDLE

A

-40° TO 110° C

98
Q

MAX CONTINUOUS OIL TEMP

A

0 TO 110° C

99
Q

ENGINE OIL TEMP MAX CRUISE

A

0 TO 110° C

100
Q

ENGINE OIL TEMP MAX REVERSE

A

0 TO 99° C

101
Q

ENGINE OIL TEMP MIN FOR FUEL HEAT AT T/O

A

55° C (RECOMMENDED)

102
Q

ENGINE PROP RPM (N2) CRUISE CLIMB

A

1,700 (UP TO 1,735 FOR 7 MINUTES)

103
Q

ENGINE PROP RPM (N2) IDLE

A

1,050 MIN

104
Q

ENGINE PROP RPM (N2) MAX CONTINUOUS

A

1,700 RPM (UP TO 1,735 FOR 7 MINUTES)

105
Q

MAX CRUISE N2

A

1,700 RPM (UP TO 1,735 FOR 7 MINUTES)

106
Q

MAX REVERSE N2

A

1,650 RPM

107
Q

MAX TAKEOFF N2

A

1,700 RPM (UP TO 1,735 FOR 7 MINUTES)

108
Q

MAX TRANSIENT N2

A

1,870 RPM FOR 20 SEC

109
Q

ENGINE TORQUE% MAX CONTINUOUS

A

100% (UP TO 102% FOR 7 MINUTES)

110
Q

MAX TORQUE% FOR TAKEOFF

A

100% (UP TO 102% FOR 7 MINUTES)

111
Q

ENGINE TORQUE LIMITE BELOW 1,000 RPM N2

A

62%

112
Q

If the shaft to the primary governor were to shear, what would happen to the propeller?

A

It would feather

113
Q

What is the range of the primary governor?

A

1,450 to 1,700 RPM

114
Q

The overspeed governor governs to _____.

A

1,768 RPM

115
Q

how many stby fuel pumps required for T/O

A

1 when using rec engine fuels…crossfeed will be unavailable from side without operative STBY pump

116
Q

engine anti ice shall be off for T/O in temps above

A

+10C

117
Q

de ice boots shall not be operated in temps below

A

below -40C

118
Q

brake de ice shall not be used above

A

15C

119
Q

electric heat must be turned off ___ prior to engine start

A

2 min

Revised King Air (3 decks)

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