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ABORT

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.

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ABORT

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  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

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