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|  STUDENT GUIDE FOR T-1A AIRCRAFT SYSTEMS
CHAPTER SEVEN
14. The cabin pressure high annunciator illuminates when the cabin pressure differential
exceeds ____________.
9.1 + 1.0 psi
a.
b.
9.1 + 1.5 psi
c.
9.1 + 0.1 psi
d.
None of the above
15. Where is the cabin pressure controller located?
16. The cabin pressure controller controls both _____________________ and
__________________.
17. The cabin rate of climb setting is adjustable between ______ and ______ FPM, but is
typically set to ____________ FPM.
18. The cabin may be depressurized to a maximum of _______________ feet.
19. If the CABIN PRESS HI annunciator illuminates, adjusting the MANUAL
PRESSURIZATION control may result in the annunciator extinguishing. (T/F)
20. Where are the cabin rate of climb and cabin pressure differential indicators located?
21. Where is the cabin dump valve located?
22. The EHS cannot be operated in flight. (T/F)
ENVIRONMENTAL CONTROL SYSTEMS 7-9
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