Memorization Sheet Flashcards

1
Q

N1 Limits

A

100% max continuous

101.5% transient for 10s

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2
Q

N2 Limits

A

100% takeoff
100% max continuous
97% minimum
101.5% transient for 10s

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3
Q

Fuel Burn

A

700 lbs./hr.

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4
Q

Fuel Cells

A

5 tanks = 220 gal. (217 usable)
1 aux = 90 gal.

Total = 307 usable

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5
Q

Fuel Low Light

A

50 lbs. remaining = 10 min @ cruise

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6
Q

ITT 5 Minute Both Turbine

A

765°C to 810°C for 5 min.

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7
Q

ITT 30 Minute Single Engine

A

765°C to 810°C for 30 minutes

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8
Q

ITT Max Continuous

A

765°C continuous 1 or 2 engines

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9
Q

ITT Power Change Transient

A

810°C to 850°C for 5s

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10
Q

ITT Starting Transient Limit

A

2s above 810°C not to exceed 1090°C

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11
Q

Engine Starter Limits

A

30 on, 60 off
30 on, 5m off
30 on, 15m off

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12
Q

Twin Engine Torque Limits

A

87.5% max continuous
87.5% to 104.3 for 5 min takeoff
100% maximum

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13
Q

Single Engine Torque Limits

A

63.9% max continuous
63.9% to 71.8% for 30 min
71.8% maximum

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14
Q

Torque Split

A

4% cursor width normal operation

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15
Q

Engine Cooldown

A

3 minutes at ground idle

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16
Q

Cargo Hook Weight Limit

A

5000 lbs. or placarded weight

17
Q

Minimum Voltage for Start

A

Use external power if below 20 V

18
Q

Max Gross Weight

A

11,200 lbs. (~ 5000 useful)

19
Q

Max Operating Altitude

A

20,000 PA (14,000 DA)

20
Q

Main Rotor Diameter

A

48 ft.

21
Q

Ambient Air Temp Limits

A

Max sea level temp 51.7°C (125°F)
Decreases 2°C/1000 ft.
Min ambient temp at all altitudes is -54°C (-65°F)

22
Q

Min Crew Weight

A

170 lbs.

23
Q

Baggage Compartment Loading

A

400 lbs., not to exceed 100 lbs./sq. ft.

24
Q

Cabin Loading

A

100 lbs./sq. ft.
Deck tiedowns: 1250 lbs. vertical, 500 lbs. horizontal
Bulkhead: 1250 lbs. at 90° to bulkhead and 500 lbs. in any direction parallel to bulkhead

25
Q

Critical Wind Azimuth

A

40° to 135° right of the nose (1:30 to 4:30)

26
Q

Rotor Brake Limits

A

Application below 40% (20% for TEMSCO)

27
Q

Airspeed Limits

A

Vne < 7500 lbs. GW: 130 KIAS
Vne > 7500 lbs. GW: 100 KIAS

Vne decreases linearly from 130 kts to 100 kts

Vne decreases 3 kts per 1000 ft above 3000 DA

Vne 80 KIAS above 87.5% torque

28
Q

Rotor Speed Limits

A

Power off: 91% (294) to 104.5% (339)

Power on: 97% (314) to 100% (324)