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|  CHAPTER THREE
STUDENT GUIDE FOR T-1A AIRCRAFT SYSTEMS
27. If the left engine fails while the synchronization system is on, there will be a maximum
_______ fan or turbine RPM spool down of the right engine.
28. The engine synchronization system should be on for takeoff and landing. (T/F)
29. How many engine instruments are provided to monitor each engine?
30. Which instrument(s) provide(s) both digital and analog information?
31. During takeoff, the ITT should not exceed _____ degrees C.
32. During a cold engine start, the oil pressure may exceed _____ psi; however, after attaining
engine idle, the pressure must read a minimum of _____ psi.
33. TRT may be used for ________________.
a.
1 minute at TRT setting
b.
1 minute starting when the throttle is first advanced to TRT
c.
5 minutes starting when the throttle is first advanced to TRT
d.
no limit
34. Normal oil pressure is ______ to ______ psi at _____ speeds above _____ %.
a.
60; 83; N1; 52
b.
60; 83; N2; 52
c.
83; 95; N1; 60
d.
60; 83; N2; 60
35. Under cold starting conditions, oil pressure between _____ and _____ psi is limited to
_____ seconds.
a.
60; 83; 90
b.
40; 60; 95
c.
83; 90; 95
d.
83; 95; 90
36. What are the ITT limits during engine starts?
37. What are the oil temperature limits for
a.
Takeoff:
_________________
b.
MCT:
_________________
c.
Idle:
_________________
d.
Transient:
_________________
3-10
ENGINES
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