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1. Anti-ice may be used for de-ice? False 2. When engine driven generator fails or is off, AC generator will be inoperative True 3. Which anti-ice features are electrically heated? AOA probe & stall warning vanes 4. Which anti-ice features are heated with bleed air? Engine flow straightener vanes 5. What is automatically heated with weight of wheels? Pitot tubes 6. How is the starter/generator rated? 28V 400A 7. Batteries are normally connected in _______ but during start they are in _____. Parallel/series 8. How is the instrument inverter rated? 1000 V/A 9. If you have total inverter failure the ac-generator provides back-up power? False 10. DC essential bus is powered by _____. Paralleling bus 11. Radar altimeter is set to ________ during t/o 400 feet 12. Any configuration change (gear, flaps, trim) has to be checked verbally and visually. True
13. When you check the speedbrake/aux hydraulic system during Before Taxi Checklist which hydraulic gauge should move with AUX SYS switch ON? Both (normal and aux hydraulic gauge are moving) 14. What do you verbalize on takeoff roll B – off the peg, 60 knots, v1 (in knots) 15. When do you configure on the ILS approach One dot below 16. For V ref: single engine, stuck slats and no flaps are cumulative. False 17. Altitude calls must be made 1000‘ prior to every level off above 1000‘ msl and 200‘ prior to every level off below 1000‘ agl. True 18. What is the initial altitude for course rules at NPA? 2000‘ MSL 19. What is the low break altitude and when can you descent to it? 1000‘ MSL/3 DME 20. The normal hydraulic system supplies all of the following, except _____ . Flaps 21. Mach/airspeed warning horn/clacker is used on ground for _____? Hydraulic system 22. Which bus powers the hydraulic pump and which bus powers the hydraulic pump switch? Paralleling bus/DC essential bus 23. The main hydraulic gauge shows 2650 psi and the aux hydraulic gauge shows 3400 psi. On the annunciator panel the HYD PWR OFF light illuminates. WHY? Pump operating more then 1 minute 24. The hydraulic pump still works with total electrical power failure. False 25. Natops procedures are concerned to be best but if you encounter multiple emergencies, adverse weather, terrain clearance etc. use _________. Sound judgement 26. What is the minimal controllable airspeed? 115 knots 27. Which switch must be off during airstart to allow starter to be engaged (assistance 10-20 % rpm) Airstart switch 28. Which control surface is actuated hydraulically? None 29. What is take off trim setting? 0,4 up,0 30. Flaps are controlled and actuated mechanically. False 31. T-39N is prohibited to land with more then 25 knots x-wind. False 32. What do you look for during stall warning test? Ruder shakers/lights in the starter buttons 33. The fuselage tank gravity feeds both wing tanks. True 34. The 9th stage bleed air is used for ________. Pressurization and anti/de-ice 35. Weight on wheels is required for thrust reverser operation. False 36. Which thrust reverser switch position directs hydraulic pressure to the T/R? EMERG STOW 37. The aux hydraulic system powers ___________. NWS/wheelbrakes 38. The hydraulic pump switch is powered by __________. DC essential bus 39. Anti skid is available with emergency brakes. False 40. The aux air conditioner works with only 1 generator online. False 41. The door seal pressurization is lost during dual generator failure. False
RH throttle
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