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### 15 Cards in this Set

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 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_%