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HAC Study - The Gauntlet > NATOPS Limits and Emergency Procedures > Flashcards

NATOPS Limits and Emergency Procedures Flashcards

1
Q

If a limit is exceeded to the extent that a red “XXX” is indicated..

A

Land as soon as practicable

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2
Q

Starter delay after aborted start

A

60 seconds (except emergencies)

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3
Q

Receiving engine shall be at or above _____ prior to advancing PCL to IDLE

A

24% Ng

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4
Q

TGT (DECU)

A 
0-810 (Cont/Yellow)
810-851 (30 min)
851-903 (2.5 min)
903-949 (12 sec)
949 Max
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5
Q

TGT (EDECU)

A 
0-810 (Cont/Yellow)
810-851 (30 min)
851-903 (2.5 min)
851-878 (10 min as required for Max Power and limiter checks)
903-949 (12 sec)
949 Max
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6
Q

Np

A
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7
Q

Nr

A

120 (123% max for FCF only)

127, 137, 142 (Ovspd latch)

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8
Q

Dual-engine TQ (

A

0-120% (Cont)
120-144 (10 s)
144(max)

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9
Q

Dual-engine TQ (>80 KIAS)

A

0-106% (Cont)
106-127 (10s)
127 (Max)

Applies when both engines are above 65%

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10
Q

Single-Engine TQ

A

0-135% (Cont)
135-144 (10s)
144 (Max)

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11
Q

Ng

A

0-98% (Cont)
98-102.2 (Cont/Yellow)
>102.2-105.1 (12 sec)
105.1 (Max)

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12
Q

XMSN Temp

A

-50-105 C (Cont)
105-120 (Prec)
120 Max

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13
Q

XMSN Press

A 
20 psi (Min)
20-30 (Idle and Transient)
30-65 (45-60 in level flight) (Cont)
65-130 (Prec)
130 Max
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14
Q

ENG Oil T

A

-50-135 C (Cont)
135-150 (30 min)
150 Max

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15
Q

ENG Oil Press

A 
22 psi (min)
22-26 (Prec)
26-100 (Cont)
100-120 (Prec)
120 (Max)

Normal idle range 22-55 psi

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16
Q

Starter Limits

A
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17
Q

Minimum planned fuel on landing

A

No less than 600 lbs

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18
Q

APU operation shall be limited to

A

Essential operations only. Includes EPs, Single-engine training, practice autos, powering the ECS during extreme temp operations.

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19
Q

XMSN Note on hovering in hot weather

A

Prolonged hovering in hot WX (95 F / 35C) and high gross weight may cause temps to rise into yellow/prec. Ops in prec. range for less than 30 min during any one flight is acceptable.

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20
Q

XMSN Oil PX limits

A

Steady-state level pitch: XMSN oil px should be 45-60 psi. The following is not immediate emergency situation but is indicative of a degraded system. Any discrepancy shall be documented on a MAF.

1) Steady px outside 45-60 but within 30-65;
2) Fluctuations not to exceed 10 psi but within 30-65

During transient-pitch or steady nose-high attitudes, fluctuations (momentary below 30 psi or below 20 psi for up to 1 sec) are acceptable. Operations with psi below 30 psi shall be limited to 30 min.

21
Q

Rotor Engagement/Disengagement

A

45 knots any direction

22
Q

Vne

A

180 KIAS

23
Q

Sideward/rearward flight

A

35 knots

24
Q

Max speed (autorotation)

A

100 KIAS

25
Q

Boost off (Vne)

A

140 KIAS

26
Q

Two SAS Inop in IMC

A

125 KIAS

27
Q

Either PRI SERVO PRESS

A

125 KIAS

28
Q

Searchlight in position other than stowed

A

160 KIAS

29
Q

Searchlight in transition

A

100 KIAS

30
Q

Dome at trail

A

70 KIAS/ 45 AOB

31
Q

Dome below trail

A

70 KIAS/ 15 AOB

32
Q

Door opening/closing

A

60 KIAS

33
Q

Hovering limits

A

1) Prolonged rearward flight or downwind hovering should be avoided
2) Hovering turns >30 deg/sec
3) Dipping ops at other than 70’
4) Transducer towing limits: 8 KGS folded / 4 KGS unfolded

34
Q

Angle of Bank

A

Normal - 45 deg
Above 10,000’ DA: 30
Either PRI SERVO PRESS: 30
Boost off: 30

35
Q

Altitude

A

13,000 feet

36
Q

Prohibited maneuvers

A

1) Aerobatic flight
2) Practice full autos
3) Intentional approaches into or inducement of RBS

37
Q

Rotor brake ops

A

Max: 76% Nr
Routine: 30-50 Nr
Routine stops should be limited to 180 psi

38
Q

Blade-fold cooling time

A

10 minutes

39
Q

Landing limits

A
  • 19,500 lbs: 480 fpm
  • Sloped: 360 fpm
  • Max touchdown speed: 75 KGS with tailwheel locked; 20 KGS unlocked
  • Taxi: 40 w/ shimmy damper; 20 w/o
  • Slopes: 9 deg up/12 deg cross/6 deg down
  • Downwind should be avoided
40
Q

Gross weight

A

Max: 23,500
Aviation ships: 23,500
Air-capable and amphibs: 22,500

41
Q

External loads

A

Cargo hook: 6000 lbs

Hoist: 600 lbs

42
Q

Required equipment for night flight over water

A
  • LAWS

- Altitude hold

43
Q

Icing

A

Equipped with operable anti- and de-icing equipment permitted to fly in trace or light icing conditions. All installed equipment SHALL be operable prior to flight.

44
Q

APU Temp limits

A

43 C and above with rotors turning limited to 30 minutes. Unrestricted to 51 C with engine/rotors not turning.

45
Q

Backup HYD Pump

A

33-38 C: 24/72

38-60: 16/48

46
Q

The following should be performed for all emergencies

A

1) Maintain control of the aircraft
2) Alert crew
3) Determine the precise nature of the problem
4) Complete the applicable emergency procedure or take action appropriate for the problem
5) Determine landing criteria and land as required

47
Q

Land immediately

A

Execute a landing without delay. The primary consideration is to ensure the survival of the occupants

48
Q

Land as soon as possible

A

Land at the first site at which a safe landing can be made

49
Q

Land as soon as practicable

A

Extended flight is recommended. The landing site and duration of the flight is as the discretion on the pilot in command.

HAC Study - The Gauntlet (4 decks)

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