Airframe Limits Flashcards

1
Q

AOA for inverted spins?

A

0 units

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2
Q

AOA for NORMAL DESCENT at 75% and 250 KIAS?

A

8 units

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3
Q

AOA for MAX RANGE?

A

9 units

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4
Q

AOA for L/Dmax CLEAN?

A

9 units

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5
Q

AOA for MAX ENDURANCE?

A

10 units

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6
Q

Approx AOA for Clean and Level Flight at 250 KIAS?

A

10 units

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7
Q

AOA for Max Glide Range with 5 stores?

A

10 units

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8
Q

AOA for buffet onset in the clean configuration?

A

11 units (20-30 KIAS prior to stall)

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9
Q

AOA for stall recovery clean?

A

11 units

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10
Q

AOA for Hard Turns?

A

9-11 units (energy sustaining at light buffet, alt dependent

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11
Q

AOA for flaperon popup in-flight w/flaps up?

A

12 units

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12
Q

AOA for No FLAP/SLAT approach and waveoff?

A

13 units

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13
Q

AOA for break turn?

A

13-14 units or 4Gs (whichever is less)

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14
Q

AOA for L/Dmax DIRTY?

A

15 units

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15
Q

AOA for dirty stall recovery?

A

16 units

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16
Q

AOA maintained by APC?

A

17 units

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17
Q

AOA for normal approach?

A

17 units

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18
Q

AOA for single engine approach?

A

17 units

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19
Q

AOA for flaperon popup in-flight w/flaps down?

A

21 units

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20
Q

AOA indication for Erect Spins?

A

30 units (pegged)

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21
Q

How many KIAS prior to stall does the stall warning horn go off?

A

Flaps 30deg: 6-20 KIAS prior to stall

Flaps 20deg: 6 KIAS prior to stall

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22
Q

When do you disregard AOA indications?

A

With a right engine failure (also inhibit the stall warning horn)

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23
Q

The stall warning horn is enabled when?

A

The gear is down and locked.

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24
Q

What is the max permissible altimeter error/discrepancy?

A

+/-75’ of the field & between STBY and RESET

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25
Q

Minimum altitude to drop wingman off?

A

300’ AGL

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26
Q

RADALT SOP?

A

T/O: 400’, 1,500’, 3,000’, and 5,000’

Below platform: Assigned or MDA - 10%, or DH

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27
Q

What is the minimum altitude to engage Stab Aug?

A

1,000’ AGL

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28
Q

Eject below what altitude and airspeed on dual engine failure?

A
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29
Q

Eject below what altitude with no relight (dual engine failure)?

A

5,000’ AGL

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30
Q

EFC may not maintain EGT below ________?

A

10,000’ MSL and >25deg C OAT

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31
Q

Max altitude for cabin dump?

A
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32
Q

Dump cabin pressure before lowering the gear above what altitude?

A

8,000’ MSL

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33
Q

Total Altitude loss during a spin is approximately:

A

9,000-12,000’

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34
Q

Spin Altitude loss per rotation is?

A

1,100 - 1,500’

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35
Q

Max Gross Weight for field takeoff?

A

61,500 lbs

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36
Q

Max Gross Weight for Catapult Launch?

A

58,600 lbs

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37
Q

Max Gross Weight for min rate of descent landing?

A

51,000 lbs for 600 fpm down or less at touch down

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38
Q

Max gross weight for Field/FCLP landing?

A

45,500 lbs

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39
Q

Max gross weight for arrested landing

A

45,500 lbs

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40
Q

Max gross weight to slow to 150 KIAS without stalling?

A

43,000 lbs

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41
Q

Block 89A zero fuel weight?

A

34,000 lbs

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42
Q

Max weight differential for a section go?

A

3,000 lbs

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43
Q

MK 7 Mod 1 Barricade

A

38,000 lbs

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44
Q

MK 7 Mod 2 & 3 Barricade

A

45,500 lbs

45
Q

SATS Mod 21 Barricade

A

45,500 lbs

46
Q

Max airspeed CLEAN / NO STORES?

A

Max attainable

47
Q

Max airspeed with AG-88 HARM?

A

Max attainable

48
Q

Max airspeed for Pods/Drops

A

0.86 IMN / 550 KIAS

49
Q

Max airspeed with BLIVOT?

A

0.80 IMN / 525 KIAS

50
Q

Clean Bingo Climb airspeed?

A

0.7 IMN

51
Q

Max airspeed for emergency RAT Retraction?

A

475 KIAS

52
Q

Wingman max rendezvous closure speeds?

A

50 KIAS within 1 NM
25 KIAS within 0.5 NM
10 KIAS within 0.3 NM or on bearing line

53
Q

Max airspeed for RAT Deployment?

A

300 KIAS

54
Q

Max airspeed for section approach?

A

300 KIAS

55
Q

Turn ASR off by what A/S?

A

300 KIAS

56
Q

Max airspeed for HARM jettison?

A

0.60 IMN / 300 KIAS

57
Q

Max airspeed for Stores Jettison?

A

0.86 IMN / 300 KIAS

58
Q

Climbout Airspeed?

A

250-300 KIAS

59
Q

Normal Approach Speed (single)

A

250 KIAS

60
Q

PAR Approach speed on downwind?

A

250 KIAS

61
Q

Max airspeed for FLAP / SLAT extension?

A

250 KIAS

62
Q

Max airspeed for FLAP / SLAT retraction?

A

250 KIAS

63
Q

Max airspeed for canopy jettison?

A

250 KIAS

64
Q

No Turn > 10 deg AOB until clean and above ______

A

250 KIAS

65
Q

Max airspeed for hook to fully extend?

A

230-280 KIAS

66
Q

Minimum airspeed to rotate with two transmitters?

A

220 KIAS

67
Q

Reliable airstart airspeed at all altitudes below 33K’?

A

0.5 IMN / 200 KIAS

68
Q

Minimum airspeed with stab shift failure?

A

200 KIAS

69
Q

Max airspeed for flaps to 20 degrees?

A

200 KIAS

70
Q

Max airspeed to retract landing gear?

A

200 KIAS

71
Q

Max airspeed for rain removal system?

A

200 KIAS

72
Q

Minimum airspeed to rotate for one transmitter?

A

192 KIAS

73
Q

Minimum airspeed for FLAP / SLAT Retraction?

A

185 KIAS

74
Q

Maximum airspeed for Emergency Flap / Slat Extension

A

180 KIAS

75
Q

Max tire rotational speed?

A

175 kts

76
Q

Max Ground speed for a no flap/slat LDG?

A

175 kts

77
Q

Max airspeed for emergency gear extension?

A

150 KIAS

78
Q

PAR approach speed (dirty)

A

150 KIAS

79
Q

Airspeed in an erect spin?

A
80
Q

Airspeed in an inverted spin?

A
81
Q

Minimum Airspeed in the pattern for a simulated single engine approach?

A

150 KIAS

82
Q

Minimum airspeed to windmill engines to Power Flight HYDS?

A

140 KIAS

83
Q

Minimum airspeed for RAT to generate power?

A

110 KIAS

84
Q

Cutoff for HIGH/LOW speed aborts?

A

100 KIAS

85
Q

Minimum airspeed for ejection seat separation?

A

80 KIAS

86
Q

Minimum airspeed for rudder effectiveness?

A

80 KIAS

87
Q

Max airspeed for canopy open during Taxi?

A

60 KIAS

88
Q

Max Cross Wind component without a waiver?

A

47 kts

89
Q

Anti skid works until _____ with Right WOW failure?

A

10 - 15 kts (light will not be illuminated)

90
Q

Max cross wind component for aerodynamic braking?

A

10 kts

91
Q

Max rate of closure during inflight refueling?

A

5 kts

92
Q

Max airspeed for emergency RAT deployment?

A

LBA

93
Q

Load factor limits for less than 0.86 IMN symmetrical?

A

-2.4 to 5.5 g

94
Q

Load factor limits for less than 0.86 IMN admin?

A

-1.0 to 4.5 g

95
Q

Load factor limits for less than 0.86 IMN rolling?

A

-1.0 to 4.4 g

96
Q

Load factor limits for greater than 0.86 IMN symmetrical?

A

-1.0 to 4.5 g

97
Q

Load factor limits for greater than 0.86 IMN rolling?

A

-1.0 to 3.6 g

98
Q

Load factor limits with a blivot?

A

-1.0 to 3.0 g

99
Q

Load factor limits with Gear/Flaps DOWN?

A

0.0 to 2.0 g

100
Q

Load factor limit with MATT/IDM in use?

A

0.5 to 3.0 g

101
Q

Ejection Seat Colors?

A

Pilot - Brown
ECMO 1 - Purple
ECMO 2 - Orange
ECMO 3 - White

102
Q

Time delay for seat firing?

A

0.4 seconds

103
Q

Command Eject in ECMO, who will eject everyone?

A

ECMO 1 and Pilot will eject everyone

104
Q

Parachute Auto deployment altitude?

A

13,000 +/- 1,500’ MSL

105
Q

When does the parachute deploy below 11,500’ MSL?

A

2 seconds after ejection

106
Q

What is the SEAT MOTOR DUTY CYCLE?

A

60 seconds ON then 10 minutes OFF

107
Q

Pitch and roll limits for RADALT?

A

+/-40deg Pitch & +/-30deg Roll

108
Q

Pitch and roll limits for Radar?

A

+/-25deg Pitch & +/-45deg Roll

109
Q

Pitch and roll limits for ATT Limit?

A

+/-15deg Pitch & +/-20deg Roll