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

17
Q

Spinning max alt

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
Prohibited Maneuvers
1) Flick or snap manoevres 2) Inverted Spinning 3) Stall Turns
26
G limits with flaps extended
1/2, 3/4, Down = +2.5 to 0 G | Combat = +8 to -2G
27
How long can the aircraft fly under zero or negative g
< 30s
28
Max Crosswind: 1) Single Aircraft 2) Streaming Brake Chute 3) Formation
1) 30 kts 2) 25 kts 3) 15 kts (0 Standing Water)
29
Engine Limits Max PWR: 1) RPM 2) TGT 3) Time limit 4) Permitted Transient
1) 1040 @ Nh 2) 600 +/-10 C 3) 30 min/hour 4) 106/645 C for 20 sec
30
Engine Limits Max Cont: 1) RPM 2) TGT 3) Time limit 4) Permitted Transient
1) 100.0 % Nh 2) 550 3) - 4) -
31
Engine Limits Idle: 1) RPM 2) TGT 3) Time limit 4) Permitted Transient
1) 55.0 +- 2 2) 450 3) - 4) -
32
Engine Limits Start 1) RPM 2) TGT 3) Time limit 4) Permitted Transient
1) - 2) 550 C 3) - 4) 570 C/10''
33
Engine Limits Relight 1) RPM 2) TGT 3) Time limit 4) Permitted Transient
1) - 2) 600C 3) - 4) 645 C/10''
34
Immediate Relight limit
Any speed/altitude
35
Unassisted (Windmill) Relight
< 25 000ft , 250 kts to 0.9 M, RPM Stagnates = increase airspeed/decrease altitude
36
Assisted Relight limits
1G
37
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
1) 25 000 ft 2) 22 500 ft 3) 20 000 ft 4) 0 to 8 G 5) 1 hour