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Exam (elaborations)

AMT 287 FINAL QUESTIONS AND ANSWERS 2026

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AMT 287 FINAL QUESTIONS AND ANSWERS 2026

Institution
AMT 287
Course
AMT 287









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Institution
AMT 287
Course
AMT 287

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Uploaded on
December 30, 2025
Number of pages
7
Written in
2025/2026
Type
Exam (elaborations)
Contains
Questions & answers

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AMT 287 FINAL LATEST
where does the greatest negative thrust occur when computing thrust
with the thrust distribution method - ANSWERS-turbine


what does the thrust horsepower computation convert - ANSWERS-the
power factor of a thrust producing engine to horsepower


if knowing the THP enables one to determine how much HP is required
to propel an aircraft at certain speeds, why can't Fg be used in the THP
formula - ANSWERS-because MPH is zero


propulsive efficiency is known as the ______ efficiency of a turbine
engine - ANSWERS-external


thermal efficiency is known as the ______ efficiency of a turbine engine
- ANSWERS-internal


overall efficiency is defined as propulsive efficiency ______ thermal
efficiency - ANSWERS-times


factors such as OAT, altitude, and airspeed all affect thrust because they
have the greatest effect on inlet - ANSWERS-air density


END OF
PAGE 1

, AMT 287 FINAL LATEST
what cockpit gauge east indicates the thermal efficiency of an operating
engine - ANSWERS-fuel flow


when compared to thermal efficiency, what is overall efficiency -
ANSWERS-a lesser percentage value


the best compressor pressure ratio occurs when compressor and turbine
efficiency is high. What contributes most to this? - ANSWERS-low fuel
flow


the four factors that affect thrust - ANSWERS-altitude, ambient temp,
engine rpm, airspeed


when an aircraft ascends to altitude, what will its gas turbine engines do?
- ANSWERS-lose thrust


who first developed gas turbine type accessory for aircraft use -
ANSWERS-Moss


Aircraft from first turbojet propelled flight in GB - ANSWERS-Gloster
E-28/29


END OF
PAGE 2

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