Limits Flashcards

1
Q
  • Max aircraft mass for normal landing, and max RoD.
  • C/Line, 2 crew, at what fuel is this mass achieved
A
  • 5900 kg, 780 ft/min
  • 1,050kg
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2
Q

What is the maximum take-off mass for the Hawk T-165 (at sea level)?

A

8561 kg

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3
Q

Max heavyweight landing mass and RoD

A

8561 kg
625 ft/min

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4
Q

Max cleared altitude

A

48,000’

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5
Q

Aircaft OAT operating limit

A

-26 to 50C

At ground level

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6
Q

Aircraft configuration restriction in visible icing

A

Full flap prohibited

Must land with half flap

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7
Q

Aircraft airspeed limits

A
  • 575KCAS up to 0.9M
  • 0.9M up to 500KCAS
  • 500KCAS up to 1.2M
  • 1.2M up to 48,000’

Basic aircraft

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8
Q

Gear Overspeed limits

A
  • 200-210 KCAS: continue sortie
  • > 210KCAS: abort sortie
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9
Q

Combat Flap speed limit

A

350KCAS/0.8M

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10
Q

Flaps G limits

A

Combat flap: -2 to +8G
1/2, 3/4, or full flap: 0 to +2.5G

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11
Q

Zero/negative G time limit

A

30sec

Must be followed by an eqaul or greater time of +ve G

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12
Q

Prohibited Manouvres

A
  • Flick/snap manouvres
  • Inverted spins
  • Stall turns
  • Tail slides
  • Autopilot with O/B stores and only wingtip fairings/clean wingtips
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13
Q

Max speed for rudder use to enhance manouvres

A

200 KCAS

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14
Q

Single aircraft crosswind limit

A

30kts for takeoff or landing (wet or dry)

If >25kts, brakechute must not be streamed, except for emergency on T/O

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15
Q

Formation crosswind limit

A

15kts

Takeoff or landing

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16
Q

EEC controlled RPM/T6 limit

A
  • 104% NH
  • 880 degC

108% NL

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17
Q

Ground start T6 limit

A

637 degC

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18
Q

Relight T6 limit

A

840 degC

19
Q

Transient RPM/T6 limit

A
  • 104.5% NH
  • 885 degC

108.5% NL

20
Q

Ground starting pressure altitude limit

A

0 to 10,000’

21
Q

Ground starting OAT limit

A

-26 to +50 degC

22
Q

Ground starting tailwind limit

A

15kts

23
Q

ISA (15degC) engine time limit to reach ground idle RPM

A

45sec to reach 95% (from 10% NH)

Provided throttle is opened before 10%

@30degC: limit is 64sec

24
Q

After start manual FADEC check: duration of switch set to MFC

A

MFC selected for 2-3 seconds

25
Q

Max RPM for assisted relight

A

20% NH

26
Q

Max RPM for starter engagement

A

20% NH

27
Q

Max RPM before switching batts off

A

10% NH

28
Q

Max alt for deliberate use of APU

A

25,000’

Max alt for starting is 20,000’ except for flight test (22,500’)

29
Q

Max airspeed with APU running

A
  • Below 10,000’: 380KCAS
  • Above 10,000’: 460KCAS
30
Q

G limit with APU running

A

0 to 8G

31
Q

Time limit with APU running inflight

A

1hr

32
Q

Min interval between APU starts, and why

A
  • 3min
  • To avoid overheating APU starter motor
33
Q

Max speed on ground

A

180kts

Tyre limit

34
Q

Max speed for streaming chute

A

160kts

35
Q

Max wind speed with canopy open

A

40kts

Combined wind+taxi speed

36
Q

Max crosswind for streaming chute

A

25kts

Except when required during an aborted takeoff

37
Q

OAT vs APU on/off

A

Above 32degC: APU must be running

Unless time between landing and shutdown is less than 5min.

38
Q

Min interval for stores release

A

80ms

39
Q

C/line tank G limits (<500kt/M0.8)

A

> 360kg: -3 to +5 (-2 to +5 with combat flap)
360 to 165kg: -3 to +5.5
<165kg: -3 to +8

Above 500kt/M0.8: linearly reducing to 0 to 3G, until <165kg: 0 to 5

40
Q

Time limit from Throttle-Idle to achieve an assisted relight

A
  • 30sec
  • Then: Throttle-Off and wait 30sec before attempting another assisted relight

30sec required for fuel to drain

41
Q

Airspeed limit with C/L tank

A

500KCAS/0.8M

42
Q

Max speed for brakechute jettison

(Unless in an emergency)

A

50kts

43
Q

Brakechute weak link speed

A

170kts