1. ABORT

2. THROTTLES - IDLE WHEEL BRAKES - AS REQUIRED

3. TWO ENGINE FAILURE (LOW ALTITUDE)

4. GLIDE - 100 KNOTS MINIMUM GEAR - DOWN THROTTLES - CUT-OFF

5. ONE ENGINE FAILURE, FIRE OR OVERHEAT DURING TAKEOFF (AFTER AIRBORNE)

6. FLAPS - 50% GEAR - UP FLAPS – UP 100 KNOTS MINIMUM

7. ENGINE FIRE OR OVERHEAT WARNING DURING FLIGHT (AFFECTED ENGINE)

8. THROTTLE - RETARD FUEL SHUTOFF T-HANDLE - PULL- OFF THROTTLE - CUT-OFF

9. EJECTION

10. HANDGRIPS - RAISE TRIGGERS - SQUEEZE

11. EMERGENCY AIRSTART

12. STARTER - AIR FUEL SYSTEM - EMERGENCY STARTER AND IGNITION - GND - ON AND HOLD UNTIL 30% RPM

13. SINGLE ENGINE GO-AROUND

14. THROTTLE - MILITARY SPEED BRAKE - IN FLAPS - 50% GEAR - UP FLAPS - UP 100 KNOTS MINIMUM

15. SMOKE AND FUME ELIMINATION

16. OXYGEN – 100%

17. ELECTRICAL FIRE

18. BATTERY AND GENERATORS - OFF

19. RPM for full throttle operation is ____% to ____ %

20. RPM for full throttle operation is 98.5% to 101.5 %

21. Above 95% RPM may be maintained for ____ minutes

22. Above 95% RPM may be maintained for 30 minutes

23. RPM range for continuous operation is ___% to ___%

24. RPM range for continuous operation is 38% to 95%

25. A ___% decrease in maximum obtainable engine RPM is acceptable above ______ feet.

26. A 3% decrease in maximum obtainable engine RPM is acceptable above 20,000 feet.

27. Engine overspeed occurs when ___% is exceeded

28. Engine overspeed occurs when 103% is exceeded

29. Normal ground idle operation RPM is ___% to ___%

30. Normal ground idle operation RPM is 36% to 40%

31. Instantaneous EGT limit for starting and acceleration is ___°C

32. Instantaneous EGT limit for starting and acceleration is 780°C

33. EGT range for continuous operation is ___°C to ___°C

34. EGT range for continuous operation is 280°C to 650°C

35. Minimum EGT for takeoff not required a 781 write-up is ___°C

36. Minimum EGT for takeoff not required a 781 write-up is 600°C

37. Maximum EGT for flight for ___ minutes at Military is ___°C

38. Maximum EGT for flight for 30 minutes at Military is 680°C

39. Minimum EGT for flight is ___°C

40. Minimum EGT for flight is 280°C

41. Minimum oil pressure at idle is ___PSI

42. Minimum oil pressure at idle is 3 PSI

43. Continuous operation range for oil pressure is ___PSI to ___PSI

44. Continuous operation range for oil pressure is 10 PSI to 45 PSI

45. Oil Pressure fluctuations of ___PSI are allowable if ____________________ _________________________________

46. Oil Pressure fluctuations of 10(+/-5) PSI are allowable if the mean pressure is within the continuous operating range

47. Maximum oil pressure is ___PSI

48. Maximum oil pressure is 65 PSI

49. Normal operating range for hydraulic pressure is ___PSI to ___PSI

50. Normal operating range for hydraulic pressure is 1250 PSI to 1550 PSI

51. Maximum hydraulic pressure is ___PSI

52. Maximum hydraulic pressure is 1750 PSI

53. 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 __________ ________________________________

54. 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

55. G Limits Positive ___

56. G Limits Positive 6.67

57. G Limits Negative ___

58. G Limits Negative 2.67

59. G Limits Assymetric ___

60. G Limits Assymetric 4.80

61. Maximum allowable airspeed is ___ KIAS

62. Maximum allowable airspeed is 275 KIAS

63. Limiting structural airspeed is ___ KIAS or ___ MACH, whichever occurs first

64. Limiting structural airspeed is 382 KIAS or.70 MACH, whichever occurs first

65. Maximum loadmeter reading for takeoff is ___.

66. Maximum loadmeter reading for takeoff is.8.

67. Maximum loadmeter reading after ___ minutes of flight is ___.

68. Maximum loadmeter reading after 10 minutes of flight is.5.

69. Difference between loadmeters should not exceed ___.

70. Difference between loadmeters should not exceed.2.

71. Minimum fuel at touchdown: Dual ___ lbs Solo ___ lbs

72. Minimum fuel at touchdown: Dual 250 lbs Solo 350 lbs

73. Emergency fuel at touchdown: Dual ___ lbs Solo ___ lbs

74. Emergency fuel at touchdown: Dual 200 lbs Solo 200 lbs

75. Maximum acceptable fuel imbalance in-flight ___lbs

76. Maximum acceptable fuel imbalance in-flight 160 lbs

77. Limiting airspeeds: Landing Gear ___ KIAS

78. Limiting airspeeds: Landing Gear 150 KIAS

79. Limiting airspeeds: Flaps ___ KIAS

80. Limiting airspeeds: Flaps 135 KIAS

81. Limiting airspeeds: Landing lights ___ KIAS

82. Limiting airspeeds: Landing lights 135 KIAS

83. Limiting airspeeds: Canopy ___ KIAS

84. Limiting airspeeds: Canopy 40 KIAS

85. Max. crosswind for dry / wet runway ___ Kts / ___ Kts

86. Max. crosswind for dry / wet runway 17.5 Kts / 13 Kts

87. Max. crosswind for icy/standing water on runway ___ Kts

88. Max. crosswind for icy/standing water on runway 10 Kts

89. Max. crosswind for student solos and formation wing takeoff/landing ___ Kts

90. Max. crosswind for student solos and formation wing takeoff/landing 13 Kts

91. Minimum runway for T-37 operations ___ feet

92. Minimum runway for T-37 operations 5000 feet

93. Thunderstorm prevention airspeed ___ Kts.

94. Thunderstorm prevention airspeed 180 Kts.

95. Icing Restrictions: Cruising or holding in conditions more severe than ______________________. or climbs or descents through conditions more severe than _________________ is prohibited.

96. 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.

97. PROHIBITED MANEUVERS

98. 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

99. DUAL ONLY MANEUVERS

100. 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