MH-65E STAN Exam - Closed Book

Question 1

A trnsformer rectifier powered from the No. 2 AC System provides power to the ________ if both starter/generators are inoperative.

Answer 1

BATTERY BUS

Question 2

With the START PROTECTION switch in the ON position, BATT RLY switches ON, and DC external power applied, the ————– light will extinguish indicating parallel operation.
A. BATT RLY 1
B. BATT RLY 2
C. BTC CLOSED
D. GEN FAIL

Answer 2

B. BATT RLY 2

Question 3

TRUE/FALSE:

Disconnecting the external DC Power with the spike suppression switch in the START PROTECTION position will result in a DC Bus Short

Answer 3

True

Question 4

A fully charged battery will power the DC system for approximately ———- However, securing DC powered equipment may extend the battery life beyond ————.

Answer 4

30 minutes

Question 5

If an actual lower fluid condition exists, placing the gear handle down before completing the appropriate emergency procedure will result in ————–.

Answer 5

Loss of braking accumulator pressure.

Question 6

Retraction of the landing gear will only take palce if ———— and all oleo struts are fully extended.
A. AFCS pitch and roll are engaged
B. the nosewheel is centered
C. the radar caution light is extinguished

Answer 6

B. the nosewheel is centered

Question 7

Display of the ———– warning light may indicate a fire hazard due to a bleed air leak.

Answer 7

HEATER O/HEAT

Question 8

The FD system utilizes imposed torque limitations when the AFCS is coupled to the FD. During forward fight above 80 KIAS, the torque limitation is set to ———.

Answer 8

83% Torque

Question 9

The FD system utilizes imposed torque limitations when the AFCS is coupled to the FD. During hover and transition flight below 80 KIAS, the torque limitation is set to ———.

Answer 9

95% torque

Question 10

When using the TRNG switch, the idled engine spools down to —– RPM N2 at a preprogrammed rate and the good engine will increase power up to approximately ——– % torque.

Answer 10

320 RPM
62% torque

Question 11

During normal operation, the engine idles at ——% N1.
A. 77.7
B. 68
C. 62
D. 75.5

Answer 11

B. 68% N1

Question 12

Personnel shall not be allowed within ——- ft of the radome with the radar operating

Answer 12

10 feet

Question 13

During preflight, the engine oil level should be between the ——– and —– lines on the sight glass if checking within —- minutes of shutdown and between ——– and —– lines if checking more than —— minutes after shutdown

Answer 13

Between the MIN and MAX lines within 15 minutes of shutdown
Between the bottom of sight glass and the **min **line if checking after 15 minutes