Limits Flashcards

1
Q

Exceeding Operating Limitations

A

Anytime an operational limit is exceeded, an appropriate entry shall be made on a MAF. The entry shall state what limits were exceeded and include range, duration, and any additional information that would aid maintenance personnel.

The flight display’s digital readout will display XXX in red when a torque or TGT limit is exceeded.

If a limit is exceeded to the extent that a red XXX is flashing, the crew shall land as soon as practicable.

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2
Q

Engine Limitations

A

The engines are limited by Ng, Np, TGT, oil px and oil temp. Specified temperature limitations ensure that engines are operated at internal temperatures that will not shorten the service life expectancy of engine components.

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3
Q

Engine Starter Limitations

A

A start cycle is defined as starter initiation, acceleration of the output drive, and starter dropout. A 60 second delay between start attempts is required any time a start is aborted, except during emergencies.

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4
Q

Engine Start Limitations

A
  1. The single and dual engine start envelopes are presented in figure 4-3. For crossbreed starts, the receiving engine shall be at or above 24% Ng prior to advancing PCL to idle.
  2. Engine start with the main rotor blades or tail rotor pylon folded is prohibited.
  3. The start TGT limit is 851 deg C until idle speed is attained
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5
Q

Engine idle limitations with gust lock engaged

A

Engine operation with gust lock engaged is prohibited

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6
Q

TGT

A
0-810 continuous green
810-851 30 min yellow
851-878 2.5 min (10 min for max power and limiter checks only) red
878-903 2.5 min red
903-949 12 sec red
949 max red
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7
Q

Np

A
<96% avoid red
96 to 105% continuous green (yellow above 101%)
105 to 117% 20 sec yellow 
117 to 120% 12 sec yellow
120% max red

CAUTION
during engagement, extended operations in the 20 to 40% and 60 to 75% ranges may cause engine damage

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8
Q

Nr

A
<96% avoid red
96-101% continuous green
101 to 120% precautionary yellow
120% max red
>120% max for FCF only, red
127% overspend latch red
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9
Q

Dual engine torque <80 KIAS

A

0 to 120% continuous green
120 to 144% 10 sec yellow
144% max red

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10
Q

Dual engine torque >80 KIAS

A

0 to 106% continuous green
106 to 127% 10 sec yellow
127% max red

NOTE
dual engine tq limits apply when both engines are above 65% tq

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11
Q

Single engine torque

A

0 to 135% continuous green
135 to 144% 10 sec red
144% max red

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12
Q

Ng

A

0-102.2% continuous green
>102.2-106% 2.5 min yellow
>106-107% 12 sec red
107% max red

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13
Q

XMSN Temperature

A

-50 to 105 continuous green
105 to 120 precautionary yellow
120 max red

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14
Q

XMSN Pressure

A
20 psi min red
20 to 30 psi idle and transient yellow
30 to 65 psi (45 to 60 psi in level flight) continuous green
65 to 130 psi precautionary yellow 
130 psi max red
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15
Q

Engine oil temperature

A

-50 to 135 continuous green
135 to 150 30 min yellow
150 max red

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16
Q

Engine oil pressure

A
22 psi minimum red
22 to 26 psi precautionary yellow
26 to 100 psi continuous green
100 to 120 psi precautionary yellow
120 psi max red
17
Q

Engine Start Cycle

A

<16 deg 3x60sec, 1x30 min

16 to 52 deg, 60 sec, 30 min

18
Q

Engine Motor (ignition off)

A

Any temp - 2 min on, 5 off; 2 min on, 30 min off

NOTE

  1. A start cycle is defined as starter initiation, acceleration and dropout
  2. Times for motoring are cumulative within a 5 min period
19
Q

Minimum planned fuel on landing

A

Minimum planned fuel on landing shall be no less than 600 pounds

20
Q

APU Limitations

A

The APU is no intended for routine in flight use. Operation of the APU in flight shall be limited to essential operations only. Acceptable in flight use includes emergency procedures, single engine training, practice autorotations, and powering the ECS during extreme temperature operations.

21
Q

ORM Process

A
  1. Identify Hazards
  2. Assess Hazards
  3. Make Risk Decisions
  4. Implement Controls
  5. Supervise and watch for change