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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 52)_ 
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 52)_ 

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 <__(pg250) Temp Lgt come on at ___. Note: (pg 249) 
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 (pg250) Temp Lgt come on at 110. Note: During warm Wx lgt may come on if rotor <100 (pg 249) 

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 (Pg513)
< 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 513)
< 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 ___ Takeoff PWR range ( ___ minutes) ___ Maximum (Red Line) ___ to ___ ( ___ seconds transient) Non intentional use Starting: ___ to ___ maximum for ___ seconds. Note: (pg 54). 
TOT Limits:
Cont Ops: 100 to 738 Continuous Operation. 738 to 810 Takeoff 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 810927 for 10 sec or above 927 (pg 54). 

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_% 