Student Activity Guide - Cont'd

16. The maximum allowable fuel flow during start is _______________.

17. After light off, the engine must reach the minimum idle RPM in _______________

seconds.

18.

The minimum idle RPM is _______________ % and the maximum idle RPM is (B)

_______________.

19.

Normal oil pressure at idle is ________________ to _______________ psi.

20. An engine RPM of 105% would require an _______________ and _______________ at

squadron level.

21. An engine RPM of 107% would require a _______________ change.

22. An engine temperature of _______________ deg Cent can be maintained for 30 minutes.

23. The maximum allowable EGT for continuous power operations is _______________ deg

Cent.

24. Total usable JP5 fuel in the T2 is __________ lbs. The fuselage ___________ lbs., the

wings hold ___________ lbs., and the tips hold lbs.

25. Two electrical boost pumps are located in the _______________ fuel tank and supply fuel

under pressure to the _______________ _______________ fuel pumps.

26. The low fuel warning light will illuminate when fuel in the _______________ tank drops

to between __________ and __________ lbs.

27. The _______________ and _______________ tanks can be gravity refueled.

28.

The tip and wing tanks transfer fuel directly to the _______________ tank.

29. Tip tank fuel level is checked by the use of two _______________ located on each tip tank.

30. The maximum allowable pressure fueling pressure is __________ psi.

31. With a dual fuel boost pump failure, fuel is supplied to the engine driven fuel pumps by

_______________ and _______________.

32. With a complete electrical failure, fuel is transferred from the tip and wing tanks

_______________ by engine bleed air.

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