EP TEST

Question 1

Lightning Strike EP

Answer 1

Question 2

If the ENG 1 OIL PRESS or ENG 2 OIL PRESS caution appears, the pilot on the controls would immediately accomplish which of the following?

Answer 2

Question 3

Loss of Tail Rotor Thrust or T/R QUAD FAIL Caution appears with loss of control at low air-speed/Hover (Right Rotation)

Answer 3

Question 4

DEC/EDECU Low Side Failure EP

Answer 4

Question 5

PRI SERVO 1 FAIL or PRI SERVO 2 FAIL caution appears. Appearance of PRI SERVO 1 FAIL or PRI SERVO 2 FAIL caution can be caused by inadvertently placing the SERVO OFF switch in 1ST STG or 2ND STG position. What is the EP?

Answer 5

Question 6

Landing at the nearest suitable landing area (e.g. open field) without delay. (The primary consideration is to ensure the survival of the occupants), is the definition of…

Answer 6

Question 7

During a main transmission failure, if NR decreases from 100% to 96% with an increase in Q during steady flight with no engine malfunction, the main transmission planetary carrier may have failed. During a main transmission planetary carrier failure, it may be impossible to maintain NR at 100%.

From the options below, select ALL the underlined immediate action steps for this emergency.

Answer 7

Question 8

Flight Control/Main-Rotor System Malfunctions EP

Answer 8

Question 9

Landing at a suitable landing area. (The primary consideration is the urgency of the emergency.) is the definition of which term?

Answer 9

Question 10

Loss of Control at Low Airspeed/Hover or T/R QUAD FAIL caution Appears (Left Rotation)

Answer 10

Question 11

Uncommanded nose up pitch attitude occurs

Answer 11

Question 12

DEC/EDECU High Side Failure

Answer 12

Question 13

ENG 1 OIL BYPASS or ENG 2 OIL BYPASS caution Appears EP

Answer 13

Question 14

Uncommanded nose down pitch attitude occurs

Answer 14

Question 15

If the ENG 1 OIL HOT or ENG 2 OIL HOT caution appears, the pilot on the controls would immediately accomplish which of the following?

Answer 15

Question 16

Engine/Fuselage Fire on Ground EP

Answer 16

Question 17

Engine Compressor Stall

Answer 17

Question 18

Hardover failure of the collective boost servo will increase control forces (as much as 150 pounds) in the collective. Which of the following choices reflect the underlined immediate action step in accomplishing this emergency procedure?

Answer 18

Question 19

Appearance of the BOOST SERVO OFF caution with no other cautions appearing indicates a pilot valve jam. Given this, what is the only underlined immediate action step to accomplish the emergency procedure?

Answer 19

Question 20

Engine High-speed Shaft Failure

Answer 20

Question 21

Manual control of engine RPM while bypassing DEC/EDECU functions is the definition of which term?

Answer 21

Question 22

If the T/R SERVO 1 FAIL caution appears and BACK UP PUMP ON advisory does NOT appear or T/R SERVO 2 ON advisory does NOT appear.

Because of the limited yaw control range available, a roll-on landing at 40 KIAS or above is required.

What is the underlined immediate action step for this emergency?

Answer 22

Question 23

Which ONE of the following component failures listed below will result in — LAND AS SOON AS POSSIBLE?

Answer 23

Question 24

Dual EGI Failure

Answer 24

Question 25

CHIP L INPUT MDL or CHIP R INPUT MDL caution Appears EP

Answer 25

Question 26

FLT DIR FAIL, FD COUPLE FAIL cautions Appear EP

Answer 26

Question 27

Select one of the following choices that is an underlined immediate action step associated with 9-25e Electrical Fire In Flight?

Answer 27

Question 28

Loss of Tail Rotor Thrust in Cruise Flight EP

Answer 28

Question 29

The term EMER APU START is defined as APU start to accomplish an emergency procedure. Given the options listed below, which one is NOT an underlined immediate action step to accomplish?

Answer 29

Question 30

Which one of the following choices is NOT one of the underlined immediate action steps associated with 9-25a Engine Fire In Flight?

Answer 30

Question 31

Which one of the following choices is NOT one of the underlined immediate action steps associated with 9-25a Engine Fire In Flight?

Answer 31

Question 32

Single Engine Failure EP

Answer 32

Question 33

There are two underlined immediate action steps for an APU compartment fire. The first step is \_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_\_. The second step is FIRE EXTGH switch — MAIN/RESERVE as required.

Answer 33

Question 34

If the MAIN XMSN PRESS caution appears, the pilot on the controls will immediately perform which of the following?

Answer 34

Question 35

If the STAB UNLOCKED Caution Appears in flight the immediate action step to perform is:

Answer 35

Question 36

Establish Single Engine Airspeed Steps

Answer 36

Question 37

FUEL 1 PRESS LOW or FUEL 2 PRESS LOW caution Appears EP

Answer 37

Question 38

The term EMER ENG SHUTDOWN is defined as engine shutdown without delay. Given the options listed below, which one is NOT an underlined immediate action step to accomplish?

Answer 38

Question 39

Should a T/R QUAD FAIL caution appear in cruise flight: Loss of one tail rotor cable will be indicated by appearance of the T/R QUAD FAIL caution. What is the underlined immediate action step for this emergency?

Answer 39

Question 40

A malfunction within the yaw boost servo or tail rotor servo can produce much higher force at the pedals and the affected servo must be turned off. A hardover failure of the yaw boost servo will increase control forces as much as 250 pounds on the pedals. Which of the following is the underlined immediate action step for this emergency?

Answer 40