Limitations Flashcards

1
Q

Kinds of Operations

A

Transport Category A land operations including over water operations in accordance with RFMS No. 19
Transport Category B land operations including over water
Water operations, limited to landing and takeoff only. Amphibious operations are prohibited.
VFR
IFR in accordance with RFMS No. 9
External load operations

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2
Q

Weight Limits

A

Category B: 20,000 pounds
External Loads: 22,000 pounds
Cargo Hook: 11,500 pounds

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3
Q

Ambient Temp Limits

A

43.5*C max

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4
Q

Starter Limits

A

Except in emergency conditions, continuous operation of starter for longer than 30 seconds is prohibited.
Attempting more than 3 starts in any 30 minute period is prohibited.

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5
Q

Ng Limits

A

Overspeed limit range (15 seconds): 103.6-105.3%
Overspeed limit: 105.3%
Max permitted speed for 2.5 OEI: 103.6%

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6
Q

Nf Limits

A

Max permitted (15 seconds): 118.5%

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7
Q

PTIT Limits

A

Starting: 949*C for 2 seconds

Transient, over-temperature: 766*C for 15 seconds for topping check

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8
Q

Engine Oil Limits

A

Max temp: 121*C
Max press: 75 psi
Min press: 8 psi
MIL-PRF-23699

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9
Q

Transmission Limits

A

Max oil temp: 110C
Min temp: -43
C with MIL-PRF-23699 (SRM Transmission)
Max press: 85 psi
Min press: 20 psi

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10
Q

Fuel Boost Pump Limits

A

Boost pumps must be operative and ON for flight. In even of boost pump failure, flight is permitted only below 4,000’ PA

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11
Q

Unusable Fuel

A

175 gallon tank: 2 gallons

190 gallon tank: 1.3 gallons

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12
Q

Fuel Pressure Limits

A

Max: 995 psi
Min: 190 psi

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13
Q

Rotor Limits - Power OFF

A

Max: 113% Nr
Normal range 6,000’ PA and below: 92-113% Nr
Normal range above 6,000’ PA: 100-113% Nr
Transient range: 88-92% Nr below 6,000’ PA

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14
Q

Rotor Limits - Power ON

A

Max: 100% Nr
Max of 109% Nr is permitted for MX flights
Normal operating range up to 6,000’ PA: 92-100% Nr
Above 6,000’ PA: 100% only
Transient range: 88-92% Nr below 6,000’ PA
External load operations: 100% Nr only

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15
Q

Density Altitude Limits - Cat B

A

Takeoff: 12,500’ DA
Enroute, below 19,000 pounds: 13,000’ DA
Enroute, 19,000 pounds to 20,000 pounds: 10,000’ DA
Landing: 12,500’ DA

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16
Q

Density Altitude Limits - External Loads

A

0-19,000 pounds: 13,000’ DA
19,000-20,000 pounds: 10,000 DA
20,000-21,000 pounds: 7,500’ DA
21,000-22,000 pounds: 6,000’ DA

17
Q

External Load Pickup

A

Vertical accelerations of the helicopter that result in rapid load pickup are prohibited

18
Q

Min Crew

A

Minimum crew is 2 pilots required for flight

19
Q

Aerobatic Maneuvers

A

Aerobatic maneuvers are prohibited

20
Q

Icing

A

Flight into known icing is prohibited

21
Q

Fuel Crossfeed

A

Fuel crossfeed is permitted only during emergency operation. Crossfeed operation is to be ceased at 400 pounds of fuel remaining in selected tank

22
Q

Engine Inlet Screens

A

With inlet screens installed, flight is prohibited when OAT is below 2*C if visible moisture is present

23
Q

Engine Inlet Anti-Ice and Pitot Heat

A

Engine anti-ice and pitot heat must be ON during operations at temperatures less than 4*C

24
Q

Engine Anti-Ice

A

Engine anti-ice must be ON during operation with OAT at 4*C and below

25
Q

Starting/Stopping Rotor Limits

A

Max steady state wind speed is 52 knots

Max permitted horizontal gust velocity is 15 knots

26
Q

Low G

A

Negative g maneuvers are prohibited

27
Q

Thunderstorms

A

Flight into known thunderstorms or areas of moderate to severe turbulence is prohibited

28
Q

Rotor Brake Application

A

Rotor brake application below 40% Nr is prohibited