Limitations Flashcards

1
Q

Max sea level Ambient temp

A

53 degrees

Decrease 2 degrees/1000 feet

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2
Q

Minimum ambient temp

A

-54 degrees for any altitude

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3
Q

Engine de icing

A

4.4 degrees visible moisture

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4
Q

Altitude limit

A

20 000 feet pres alt

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5
Q

Airspeed limitations

A

7500 pounds sea level: 120kts decrease 3kts/1000,
7500 to 8500 pounds sea level: 115kts decrease 3kts/1000’
8500 pounds and above sea level 110kts decrease 3kts/1000’
Doors locked open or removed: 100kts to 3300’ decrease 3kts/
1000’ there after
MCP 47.5 psi 80kts for all weights

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6
Q

Max gross internal

A

9500 lbs

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7
Q

Max gross ext

A

10500 lbs

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8
Q

N1 RPM MAX

A

102% structural limit

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9
Q

N2 RPMs

A

Min 91% 6000 RPM permissable 0 to 30 kts
Min 97% 6400 RPM continuous
Max 100% 6600 RPM

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10
Q

Fuel pres

A

5 to 35 psi

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11
Q

Oil pres

A

25 psi min 40% to 71% N1
25 psi to 80 psi min 71% to 85% N1
80 to 100 psi max 80% max N1
100 psi max

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12
Q

Oil temp Engine

A

15 degrees min
15 to 93 degrees operation
93 degrees max

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13
Q

Torque limitations

A

12 to 47.5 psi continuous operation
47.5 to 54 psi 5 min limit
54 psi max

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14
Q

Shaft horsepower

A

47.5 psi torque 1100 shp

54 psi torque 1250 shp

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15
Q

EGT VS OAT LIMITATIONS

A

Never exceed 626 degrees during start

Refer to gauge for take off and mcp EGT compared to OAT

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16
Q

Ignition limitations

A
2 min on
2 min off
2 min on 
23 min off
Engine start may not be successful below -12.2 degrees or above 8000’ pres jet A
17
Q

Starter limitations

A
35 sec on
3 min off 
35 sec on
30 min off
35 sec off
18
Q

Loadmeter limitations

A

Max 0.5 (150 amp) red radial

19
Q

Trans limitations oil pressure

A

30 psi min
30 to 40 psi below flight idle rpm
40 to 70 psi continuous operation
70 psi max

20
Q

Transmission limitations oil temp

A

15 to 110 degrees continuous operation

110 degrees max

21
Q

Rotor limitations

A
Power on 
Minimum 91% permissible 0 to 30kts 
Minimum 97% 
Maximum 100% 
Power off
Min 91% 
Max 104.5%