Hawk127 Limitations Flashcards

1
Q

Max T/O Mass @ SL

A

20 062 lbs

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2
Q

Normal Max Landing Mass (<780/min ROD)

A

13007 lbs

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3
Q

Heavy Wt Landing (<624’/min RoD)

A

13007 - 20062 lbs

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4
Q

Max Altitude

A

48 000 ft

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5
Q

Max Speed

A

28 000 - 48 000 ft = 1.20M
11000 - 28000 ft = 500 KTS
2000-11000ft = 0.90M
0 - 2000 ft = 575 KTS

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6
Q

Max Speed LG down or travelling?

A

200 kts

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7
Q

Max Speed Flaps 1/2

A

250 KTS

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8
Q

Max Speed Flaps 3/4 or down?

A

200 kts

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9
Q

Max Speed Combat Flap

A

350 KTS/0.8M

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10
Q

Max speed brake chute streamed

A

160 kts

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11
Q

Max speed brake chute weak link

A

170 kts

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12
Q

Max Speed wheels ground speed

A

180 kts

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13
Q

Max Speed canopy open

A

40 kts

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14
Q

Max speed BAK 12/14 cable trampling

A

Walking Pace

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15
Q

Glide/Endurance speed

A

5 alpha, 190 kts

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16
Q

Speed Glide > 25000 ft

A

0.65M

17
Q

Spinning max alt

A

30000ft

18
Q

Min height to initiate recovery

A

15000 ft AGL

19
Q

Mn ejection height

A

5000 ft AGL

20
Q

Recovery after

A

1) 4 Turns
2) CAS increases to 200 kts
3) CAS decreases to 100 kts
4) Large transient side forces
5) Manual rudder - aerodynamic forces to large to hold
6) (TGT > 450 C) engine surge

21
Q

Symmetrical (<13650 lbs) g limits

A

0 - 500 kts /0.8M = +8 to -4G

500 - 575 KTS/0.8 M - 1.2M = +5 to 0 g

22
Q

G limits with external fuel tanks (>50lbs)

A

0 - 525 kts/0.8M = 5 to -1 g

0.8 - 0.85 M = 3 to 0 g

23
Q

G limits with empty external tanks (<50 lbs)

A

0 - 525 kts/0.8M = +6 to -1G

0.885M = +4 to 0 G

24
Q

Jettison (gear/flap up)

A

Fuel > 515 lbs = <350 kts/ < 10000 ft

Fuel < 515 lbts = 300-350 kts/ < 10,000 ft

25
Q

Prohibited Maneuvers

A

1) Flick or snap manoevres
2) Inverted Spinning
3) Stall Turns

26
Q

G limits with flaps extended

A

1/2, 3/4, Down = +2.5 to 0 G

Combat = +8 to -2G

27
Q

How long can the aircraft fly under zero or negative g

A

< 30s

28
Q

Max Crosswind:

1) Single Aircraft
2) Streaming Brake Chute
3) Formation

A

1) 30 kts
2) 25 kts
3) 15 kts (0 Standing Water)

29
Q

Engine Limits Max PWR:

1) RPM
2) TGT
3) Time limit
4) Permitted Transient

A

1) 1040 @ Nh
2) 600 +/-10 C
3) 30 min/hour
4) 106/645 C for 20 sec

30
Q

Engine Limits Max Cont:

1) RPM
2) TGT
3) Time limit
4) Permitted Transient

A

1) 100.0 % Nh
2) 550
3) -
4) -

31
Q

Engine Limits Idle:

1) RPM
2) TGT
3) Time limit
4) Permitted Transient

A

1) 55.0 +- 2
2) 450
3) -
4) -

32
Q

Engine Limits Start

1) RPM
2) TGT
3) Time limit
4) Permitted Transient

A

1) -
2) 550 C
3) -
4) 570 C/10’’

33
Q

Engine Limits Relight

1) RPM
2) TGT
3) Time limit
4) Permitted Transient

A

1) -
2) 600C
3) -
4) 645 C/10’’

34
Q

Immediate Relight limit

A

Any speed/altitude

35
Q

Unassisted (Windmill) Relight

A

< 25 000ft , 250 kts to 0.9 M, RPM Stagnates = increase airspeed/decrease altitude

36
Q

Assisted Relight limits

A

1G

37
Q

APU Limitations:

1) Max operating altitude
2) Max starting altitude (test flights)
3) Max starting altitude (normal operations)
4) G limit
5) In flight time limit

A

1) 25 000 ft
2) 22 500 ft
3) 20 000 ft
4) 0 to 8 G
5) 1 hour