ABORT

THROTTLES - IDLE WHEEL BRAKES - AS REQUIRED

TWO ENGINE FAILURE (LOW ALTITUDE)

GLIDE 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 %

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 ___ lbs Solo ___ lbs

Minimum fuel at touchdown: Dual 250 lbs Solo 350 lbs

Emergency fuel at touchdown: Dual ___ lbs Solo ___ lbs

Emergency fuel at touchdown: Dual 200 lbs Solo 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