CNATRAINST 1542.8J
19 March 2001
OUTLINE OF INSTRUCTION
1.87
State the sea level rated thrust of each T-37B
J69-T-25A engine.
1.88
State the instrument indications for the sea level
rated thrust of the T-37B J69-T-25A engine.
1.89
Define thrust excess and power excess.
1.90
State the effects of a thrust excess or a power
excess.
1.91
State the conditions necessary to achieve the maximum
thrust excess and maximum power excess for a turbojet
and a turboprop airplane.
1.92
Describe the effects of changes in weight on thrust
required, power required, thrust available, and power
available.
1.93
Describe the effects of changes in weight on maximum
thrust excess and maximum power excess, and on the
airspeeds necessary to achieve maximum thrust excess
and maximum power excess.
1.94
Describe the effects of changes in altitude on thrust
required, power required, thrust available, and power
available.
1.95
Describe the effects of changes in altitude on maximum
thrust excess and maximum power excess, and on the
airspeeds necessary to achieve maximum thrust excess
and maximum power excess.
1.96
Describe the effects of changes in configuration on
thrust required, power required, thrust available, and
power available.
1.97
Describe the effects of changes in configuration on
maximum thrust excess and maximum power excess, and on
the airspeeds necessary to achieve maximum thrust
excess and maximum power excess.
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