MH60R Limits (01 FEB 23) Flashcards

1
Q

Engines are limited by

A

Ng
Np
TGT
Oil Px
Oil temperature

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2
Q

A start cycle is defined as

A

Starter initiation

Acceleration in Ng

Starter dropout/disengagement

A 60 second delay between start attempts is required any time a starter is aborted, except in emergencies

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3
Q

For crossbleed starts, the receiving engine SHALL be at or above XX% Nx prior to advancing PCL to IDLE

A

24% Ng

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4
Q

The start TGT limit is

A

851*C until idle speed is attained

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5
Q

Engine operation with gust lock…

A

Engaged is prohibited

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6
Q

Minimum planned fuel

A

On landing shall be no less than 600 pounds

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7
Q

Operation of the APU in flight shall be limited to _____ operations only.

Acceptable in flight us includes:

A

Essential

  • emergency procedures
  • single-engine training
  • practice autorotations
  • powering the ECS during extreme temperature operations.
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8
Q

Turbine Gas Temperature (TGT)

A

0-810 Continuous // Green
810-851 30 Mins // Yellow
851-878 10 Mins // Red
878-903 2.5 Mins // Red
903-949 12 Seconds //Red
949 MAX // Red

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9
Q

Power Turbine Speed (Np)

A

<96% Avoid // Red

96-105% Continuous // Green (yellow above 101%)

105-117% 20 Seconds // Yellow

117-120% 12 Seconds // 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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10
Q

Main Rotor Speed (Nr)

A

<96% Avoid // Red
96-101% Continuous // Green
101-120% Precautionary // Yellow
120% MAX // Red

123% Max for FCF Only // Red
127% Overspeed Latch // Red

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11
Q

Dual-Engine Torque (TRQ)
< 80 KIAS

A

0-120% Continuous // Green

120-144% 10 Seconds // Yellow

144% MAX // Red

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12
Q

Dual-Engine Torque (TRQ)
> 80 KIAS

A

0-106% Continuous // Green

106-127% 10 Seconds // Yellow

127% MAX // Red

Note: Dual Engine Torque Limits apply when both engines are above 65% torque.

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13
Q

Single-Engine Torque

A

0-135% Continuous // Green

135-144% 10 Seconds // Red

144% MAX // Red

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14
Q

Gas Generator Speed (Ng)

A

0-102.2% Continuous // Green

> 102.2-106% 2.5 Mins // Yellow

> 106-107% 12 Seconds // Red

107% MAX // Red

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15
Q

Gas Generator Speed (Ng)

A

0-102.2% Continuous // Green

> 102.2-106% 2.5 Mins // Yellow

> 106-107% 12 Seconds // Red

107% MAX // Red

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16
Q

Transmission Temperature (XMSN T)

A

-50 - 105*C Continuous // Green

105-120*C Precautionary // Yellow

120*C MAX // Red

17
Q

Transmission Pressure (XMSN P)

A

20 PSI Minimum // Red
20-30 PSI Idle and transient // Yellow

30-65 PSI (45-60 in level flight) Continuous // Green

65-130 PSI Precautionary // Yellow
130 PSI MAX // Red

18
Q

Engine Oil Temperature (ENG OIL T)

A

-50 - 135C Continuous // Green
135-150
C 30 Mins // Yellow
150*C MAX // Red

19
Q

Engine Oil Pressure (ENG OIL P)

A

22 PSI MINIMUM // Red
22-26 PSI Precautionary // Yellow
26-100 PSI Continuous // Green
100-120 PSI Precautionary // Yellow
120 PSI MAX // Red

20
Q

Engine Start

A

<16*C
60 Seconds
60 Seconds
60 Seconds
30 Minutes

16-52*C
60 Seconds
30 Minutes

21
Q

Engine Motor (ignition off)

A

Any Temperature

2 Mins engaged
5 Mins disengaged

2 Mins engaged
30 Mins disengaged

times for motoring are cumulative within a 5-minute period

22
Q

The Transmission is limited by

A

Nr
Torque
Oil px
Oil temp

Operation is governed by whichever limit is reached first

23
Q

During any operating condition, no maintenance action is required if main transmission oil (px/temp) is in the precautionary range continuously for XX minutes or less.

A

Temperature

5 minutes or less

24
Q

Prolonged hovering in hot weather, XXF (XXC) may cause main transmission oil temperature to rise into the precautionary range.

Operation in the precautionary range for less than XX minutes during any one flight under this condition is acceptable and ____ maintenance action is required.

A

86F (30C)

Less than 30 minutes

No maintenance action is required