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15 Cards in this Set

  • Front
  • Back
Engine Oil Pressure:
_____ Minimum for N1 speeds below _______
_____ Minimum for N1 speeds between _______ to _______.
_____ Minimum for N1 speeds above _______.
_____ Min _____ Max (Red Lines)
Note:___________________________________(pg 5-2)_
Engine Oil Pressure:
_50_ Minimum for N1 speeds below _78%_
_90_ Minimum for N1 speeds between __78%_ to _94%__.
_115_ Minimum for N1 speeds above _94%_.
_50_ Min _130_ Max (Red Lines)
Note:_Cold WX may exceed 130 – but stay at idle until
Pressure is normal and temp above 0 c_ (pg 5-2)_
Engine Oil Temp:
_____ to _____ Continuous Operation.
_____ Maximum Red Line
Engine Oil Temp:
_ 0__ to _107_ Continuous Operation.
_107__ Maximum Red Line
XMSN Oil Pressure: XMSN Oil Temp:
___ to ___ Continuous Operation ___ to ___ continuous
___ Min __ Max (Red Lines) ___ Maximum Red Line
Pressure Lgt on <__(pg2-50) Temp Lgt come on at ___.
Note: (pg 2-49)
XMSN Oil Pressure: XMSN Oil Temp:
_30 to _50_ Continuous Operation _15 to _110_ continuous
_30 Min 70 Max (Red Lines) _110_ Maximum Red Line
Pressure Lgt on <30 (pg2-50) Temp Lgt come on at 110.
Note: During warm Wx lgt may come on if rotor <100 (pg 2-49)
Fuel Pressure:
____ psi Minimum
____ to ____ psi Continuous Operation
____ psi Maximum
____ psi Minimum – Type A, A1, JP5, JP8 below ____c to ____c
Fuel Pump Lgt will come on at ____+/-____ psi
Fuel Pressure:
_4_ psi Minimum
_4_ to _30_ psi Continuous Operation
_30_ psi Maximum
_8_ psi Minimum – Type A, A1, JP5, JP8 below -18c to -32c
Fuel Pump Lgt will come on at _4psi +/-_0.5psi
Load Meter:
_____% Maximum (Red Line)
Load Meter:
_70%_ Maximum (Red Line)
Fuel Quantity:
Red Line on ______
Fuel Quantity:
Red Line on Empty
Airspeed
_____ to _____ Continuous Operations
_____ Maximum Red Line ____ Maximum Blue Line Autos
Note: .
Airspeed_________________________________________
_0_ to _130_ Continuous Operations
_130_ Max Red Line _100_ Max Blue Line Autos
Note: (auto’s) >100kts result in high rate of decent &
Low rotor RPM
VMC Airspeed Limits (Pg5-13)
< 3000 lbs G/W : _____kts at SL to 3000 ft. then decreasing
____kts per/1000 ft above 3000 to a max Alt of __________
>3000 lbs G/W : ____kts at SL to 3000 ft. then decreasing
____kts per/1000 ft above 3000 to a max Alt of __________
_______ A/S is VNE with Torque above 85% to 100%.
___ kts Min Rate of Decent ___ kts Max Glide Distance

VNE is limited to ___kts with TQ above ____%
___ kts Min Rate of Decent ____ kts Max Glide Distance
VMC Airspeed Limits (Pg 5-13)
< 3000 lbs G/W : _130kts at SL to 3000 ft. then decreasing
_3.5 kts per/1000 ft above 3000 to a max Alt of 20,000 PA.
>3000 lbs G/W : _122kts at SL to 3000 ft. then decreasing
_7.0_kts per/1000 ft above 3000 to a max Alt of 13,500 DA.

VNE is limited to 80kts with TQ above _85_%
_52 kts Min Rate of Decent _69_ kts Max Glide Distance
TOT Limits:
Cont Ops: ___ to ___ Continuous Operation.
___ to ___ Take-off PWR range ( ___ minutes)
___ Maximum (Red Line)
___ to ___ ( ___ seconds transient) Non intentional use
Starting: ___ to ___ maximum for ___ seconds.

Note: (pg 5-4).
TOT Limits:
Cont Ops: 100 to 738 Continuous Operation.
738 to 810 Take-off PWR range ( 5 minutes)
810 Maximum (Red Line)
810 to 843 ( 6 seconds transient) Non intentional use
Starting: 810 to 927 maximum for 10 seconds.

Note: Red Lgt if exceed 810-927 for 10 sec or above 927 (pg 5-4).
Gas Producer (N1):
_____ to _____ Continuous Operation.
_____ Maximum Red Line
_____ to _____ Transient – ( _____ seconds Maximum)
Gas Producer (N1):
_62_ to _105_ Continuous Operation.
_105_ Maximum Red Line
_105_ to _106_ Transient – ( _15_ seconds Maximum)
Start Introduce Fuel at (N1%): Eng Starting Limits:
FAT Min N1 During start N1 must reach:
Above _____ c _____% ____% in _____sec.
____c to ____c _____% or (____)% in______sec.
Below _____c _____% if temp is below ___c
Start Introduce Fuel at (N1%): Eng Starting Limits:
FAT Min N1 During start N1 must reach:
Above _7_ c _15_% ( 58_)% in _45_sec.
_-18_c to _7_c _13_% or ( 58_)% in _60_sec.
Below _-18_c _12_% if temp is below _10_c
Engine Starter Limits (No rise in TOT) / (Yes rise in TOT)
External Power Battery Power / APU/Battery
__ sec on / __sec off __ sec on / __sec off __ min on / __min off
__ sec on / __sec off __ sec on / __sec off __ min on / __min off
__ sec on / __minoff __ sec on / __minoff __ min on / __min off
Engine Starter Limits (No rise in TOT) / (Yes rise in TOT)
External Power Battery Power / APU/Battery
25 sec on / 30sec off 40 sec on / 60sec off 1 min on / 1 min off
25 sec on / 30sec off 40 sec on / 60sec off 1 min on / 1 min off
25 sec on / 30minoff 40 sec on / 30minoff 1 min on / 30 minoff
Engine Techometer (N2):
____% Minimum
____% to ____% Continuous Operations
____% Maximum
Engine Techometer (N2):
_97% Minimum
_97% to _100% Continuous Operations
_100% Maximum
Rotor Limits:
____% Minimum
____% to ____% Accelerate through this range
____% to ____% Normal Operations
____% Maximum
Power on Transient Rotor Droop Limit is ___________________
Rotor Limits:
_90% Minimum
_50% to _60% Accelerate through this range
_90% to _107% Normal Operations
_107% Maximum
Power on Transient Rotor Droop Limit is 95% (5 seconds max)
Torquemeter:

_____ to _____ Continuous Operation.
_____ to _____ for _____ Min Operation power T/O range
_____ Maximum.
Transient TQ Limit is : ___% to ___% (___ Sec Max)
Intentional Use Is Prohibited.

VNE is limited to __kts with TQ above ____%
Torquemeter:

_0_ to _85_ Continuous Operation.
_>85_ to _100_ for _5_ Min Operation power T/O Range
__100_ Maximum.
Transient TQ Limit is : _100_% to _110_% (_5_ Sec Max)
Intentional Use Is Prohibited.

VNE is limited to 80kts with TQ above _85_%