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ABORT
• THROTTLES - IDLE
• WHEEL BRAKES - AS REQUIRED
TWO ENGINE FAILURE (LOW ALTITUDE)
• GLIDE - 100 KNOTS MINIMUM
• GEAR - DOWN
• THROTTLES - CUT-OFF
ONE ENGINE FAILURE, FIRE OR OVERHEAT DURING TAKEOFF
(AFTER AIRBORNE)
• FLAPS - 50%
• GEAR - UP
• FLAPS – UP 100 KNOTS MINIMUM
ENGINE FIRE OR OVERHEAT WARNING DURING FLIGHT
(AFFECTED ENGINE)
• THROTTLE - RETARD
• FUEL SHUTOFF T-HANDLE - PULL-OFF
• THROTTLE - CUT-OFF
EJECTION
• HANDGRIPS - RAISE
• TRIGGERS - SQUEEZE
EMERGENCY AIRSTART
• STARTER - AIR
• FUEL SYSTEM - EMERGENCY
• STARTER AND IGNITION - GND - ON AND HOLD UNTIL 30%
RPM
SINGLE ENGINE GO-AROUND
• THROTTLE - MILITARY
• SPEED BRAKE - IN
• FLAPS - 50%
• GEAR - UP
• FLAPS - UP 100 KNOTS MINIMUM
SMOKE AND FUME ELIMINATION
OXYGEN – 100%
ELECTRICAL FIRE
BATTERY AND GENERATORS - OFF
RPM for full throttle operation is ____% to ____ %
RPM for full throttle operation is 98.5% to 101.5 %
Above 95% RPM may be maintained for ____ minutes
Above 95% RPM may be maintained for 30 minutes
RPM range for continuous operation is ___% to ___%
RPM range for continuous operation is 38% to 95%
A ___% decrease in maximum obtainable engine RPM is acceptable
above ______ feet.
A 3% decrease in maximum obtainable engine RPM is acceptable above
20,000 feet.
Engine overspeed occurs when ___% is exceeded
Engine overspeed occurs when 103% is exceeded
Normal ground idle operation RPM is ___% to ___%
Normal ground idle operation RPM is 36% to 40%
Instantaneous EGT limit for starting and acceleration is ___°C
Instantaneous EGT limit for starting and acceleration is 780°C
EGT range for continuous operation is ___°C to ___°C
EGT range for continuous operation is 280°C to 650°C
Minimum EGT for takeoff not required a 781 write-up is ___°C
Minimum EGT for takeoff not required a 781 write-up is 600°C
Maximum EGT for flight for ___ minutes at Military is ___°C
Maximum EGT for flight for 30 minutes at Military is 680°C
Minimum EGT for flight is ___°C
Minimum EGT for flight is 280°C
Minimum oil pressure at idle is ___PSI
Minimum oil pressure at idle is 3 PSI
Continuous operation range for oil pressure is ___PSI to ___PSI
Continuous operation range for oil pressure is 10 PSI to 45 PSI
Oil Pressure fluctuations of ___PSI are allowable if ____________________ _________________________________
Oil Pressure fluctuations of 10(+/-5) PSI are allowable if the mean pressure
is within the continuous operating range
Maximum oil pressure is ___PSI
Maximum oil pressure is 65 PSI
Normal operating range for hydraulic pressure is ___PSI to ___PSI
Normal operating range for hydraulic pressure is 1250 PSI to 1550 PSI
Maximum hydraulic pressure is ___PSI
Maximum hydraulic pressure is 1750 PSI
A difference of ___PPH or greater between fuel flow indicators and/or above normally expected flow constitutes high fuel flow. Acceptable fuel flow fluctuations are __________ ________________________________
A difference of 200 PPH or greater between fuel flow indicators and/or above normally expected flow constitutes high fuel flow. Acceptable fuel flow fluctuations are those not accompanied by EGT or RPM fluctuations, or actual engine surges
G Limits
Positive ___
G Limits
Positive 6.67
G Limits
Negative ___
G Limits
Negative 2.67
G Limits
Assymetric ___
G Limits
Assymetric 4.80
Maximum allowable airspeed is ___ KIAS
Maximum allowable airspeed is 275 KIAS
Limiting structural airspeed is ___ KIAS or ___ MACH, whichever occurs
first
Limiting structural airspeed is 382 KIAS or .70 MACH, whichever occurs
first
Maximum loadmeter reading for takeoff is ___ .
Maximum loadmeter reading for takeoff is .8 .
Maximum loadmeter reading after ___ minutes of flight is ___.
Maximum loadmeter reading after 10 minutes of flight is .5 .
Difference between loadmeters should not exceed ___.
Difference between loadmeters should not exceed .2 .
Minimum fuel at touchdown:
Dual ___ lbsSolo ___ lbs
Minimum fuel at touchdown:
Dual 250 lbsSolo 350 lbs
Emergency fuel at touchdown:
Dual ___ lbsSolo ___ lbs
Emergency fuel at touchdown:
Dual 200 lbsSolo 200 lbs
Maximum acceptable fuel imbalance in-flight ___lbs
Maximum acceptable fuel imbalance in-flight 160 lbs
Limiting airspeeds:
Landing Gear ___ KIAS
Limiting airspeeds:
Landing Gear 150 KIAS
Limiting airspeeds:
Flaps ___ KIAS
Limiting airspeeds:
Flaps 135 KIAS
Limiting airspeeds:
Landing lights ___ KIAS
Limiting airspeeds:
Landing lights 135 KIAS
Limiting airspeeds:
Canopy ___ KIAS
Limiting airspeeds:
Canopy 40 KIAS
Max. crosswind for dry / wet runway ___ Kts / ___ Kts
Max. crosswind for dry / wet runway 17.5 Kts / 13 Kts
Max. crosswind for icy/standing water on runway ___ Kts
Max. crosswind for icy/standing water on runway 10 Kts
Max. crosswind for student solos and formation wing takeoff/landing ___ Kts
Max. crosswind for student solos and formation wing takeoff/landing 13 Kts
Minimum runway for T-37 operations ___ feet
Minimum runway for T-37 operations 5000 feet
Thunderstorm prevention airspeed ___ Kts.
Thunderstorm prevention airspeed 180 Kts.
Icing Restrictions:
Cruising or holding in conditions more severe than ______________________.
or climbs or descents through conditions more severe than _________________ is prohibited.
Icing Restrictions:
Cruising or holding in conditions more severe than forecast trace .
or climbs or descents through conditions more severe than forecast or reported light rime is prohibited.
PROHIBITED MANEUVERS
• N egative G’s for more than 30 seconds• O ne engine only maneuvers• T rim only maneuvers• T rimming in a dive within 20 knots of limiting structural airspeed unless essential to relieve excessive stick forces• W hip stalls• I ntentional fishtail maneuvers• S nap rolls• S pinning with a fuel imbalance of more than 70 lbs and/or 1400 lbs total fuel
DUAL ONLY MANEUVERS
•Stalls•Straight-in approaches•Slow flight•Spins•Stability demonstration•Simulated runaway trim•Simulated single engine maneuvers•Simulated lost wingman (as wingman)•No flap patterns/landings•Nose high recoveries•Nose low recoveries•Low closed patterns•Rolling takeoffs
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