1. The maximum payload weight for a C-17 is ________ pounds
B. 170,900
2. For specific aircraft, Maximum Payload is Zero Fuel Weight minus Operating Weight
A. True
B. False
A. True
3. When any engine is operating in the N2 mode, pilots should monitor N2 RPM when moving the throttle to prevent
C. Possible overboost
4. ____ thrust is the recommended rating for engine out climbs
A. INT
5. Which thrust rating is recommended for normal climb?
B. MCT
6. DRT will be less than MAX and equal to or greater than
D. MCT
7. The THRUST LOSS warning will extinguish when the ______ is reset
D. MASTER CAUTION
8. If an ENGINE STABILITY X message on the WAP is illuminated, throttle movement should be slow and deliberate to prevent possible
D. Engine surge or stall
9. In the event of boost pump failure, fuel can be suction fed by the engine driven fuel pump at ____ thrust rating up to an altitude of ____ ft and at a pitch angle no greater than 21.5 degrees
A. MAX; 10,000
10. When the start sequence is initiated, ignition is energized when the associated
A. ENG SHUT OFF selector is turned on
11. The engine starting system can be used in flight as well as on the ground.
A. True
B. False
A. True
12. The starter is designed to start the engine with normal starting loads. Excessive loads are applied when the engine driven hydraulic pumps are on. A ______ may result if the pumps are on during engine start.
D. Hung Start
13. Each engine thrust reverser system has two sets of blocker doors, sleeves and cascades. Sleeves at the back of the fan and core exhausts move aft, exposing cascades to the diverted airflow. The cascades direct the airflow up and forward
C. Providing reverse thrust
14. Each throttle is mechanically linked to a dual resolver within the throttle quadrant. There
A. Is no mechanical linkage to the engine B. Is also a mechanical linkage to the engine
C. Is a switch to mechanically link the engine to the throttles
D. Is a mechanical link to only the number 2 and 3 engines
A. Is no mechanical linkage to the engine
15. If any engine electronic engine control (EEC) is in the N2 mode