EP SHIT

Question 1

EMERGENCY SHUTDOWN

Answer 1

• ECL - OFF (SIMULTANEOUS).
• T-HANDLE - ARM.
• ROTOR BRAKE - ON.
  Unless the reason for the emergency shutdown is due to an ICDS fail, or midwing fire, or midwing accessories
• APU - STOP (AS REQUIRED).
• BATTERY - OFF.
• EGRESS - AS REQUIRED.

Question 2

MAP

Answer 2

Maneuver Severity - REDUCE.
Airspeed - <200 KCAS.
PFCS - RESET.

Question 3

MP

Answer 3

Maneuver Severity - REDUCE.
PFCS - RESET.

Question 4

LAND IMMEDIATELY

Answer 4

Execute landing WITHOUT DELAY… Primary consideration is to assure SURVIVAL OF OCCUPANTS.

Question 5

LAND AS SOON AS POSSIBLE

Answer 5

Execute landing at the NEAREST AVAILABLE AREA AT WHICH A SAFE LANDING CAN BE MADE.

Question 6

LAND AS SOON AS PRACTICAL

Answer 6

Extended flight is not recommended. Landing site and duration of flight is at DISCRETION OF THE PILOT-IN-COMMAND.

Question 7

ENGINE COMPARTMENT OR NACELLE FIRE ON GROUND

Answer 7

1. ECL - OFF (AFFECTED ENGINE).
2. T-HANDLE - ARM
   If fire persists:
3. DISCHARGE BUTTON - PRESS.

Question 8

DUAL ENGINE FAILURE IN FLIGHT, NACELLE <60DEG

Answer 8

1. APLN - 84%.
2. AIRSPEED - 170 KCAS.
3. FLAPS - AUTO.
4. APU - EMERGE RUN/ENGAGE.

Question 9

ENGINE FIRE IN FLIGHT

Answer 9

1. SINGLE ENGINE FAILURE PROFILE - ESTABLISH.
2. ECL - OFF (AFFECTED ENGINE).
3. T-HANDLE - ARM.
   If fire persists:
4. DISCHARGE BUTTON - PRESS.

Question 10

UNCOMMANDED NACELLE MOVEMENT

Answer 10

1. NACELLE MOVEMENT - ATTEMPT TO OVERRIDE.
2. NAC CONTR DSBL SWITCHES - DEPRESS.

Question 11

SINGLE ENGINE FAILURE PROFILE:

• THRESHOLD CONFIG MIN PWR LDG

Answer 11

• FLAPS - AUTO
• NACELLE - 75DEG
• ASPD- 75KTS

Question 12

SINGLE ENGINE FAILURE PROFILE:

• CONV

Answer 12

• FLAPS - AUTO
• NACELLE - 60DEG
• ASPD - 90KTS

Question 13

SINGLE ENGINE FAILURE PROFILE:

• APLN MAX CLIMB

Answer 13

• FLAPS - AUTO
• Nr - 100%
• AOA - 80%

Question 14

SINGLE ENGINE FAILURE PROFILE:

• EN ROUTE

Answer 14

• FLAPS - AUTO
• Nr - 84%
• ASPD - AS REQ

Question 15

VRS - Cause, Stages and corrections

Answer 15

Caused by high sink rate + low airspeed.
SINK RATE aural annunciation comes on at <60KCAS ; >800fpm sink

Stage I
- characterized by increased vibration levels, pitch bucking, or sluggishness of aircraft response to control inputs
- corrective action - increase TCL; trim nacelles forward to max rate for 2sec (~15deg forward); fly out with forward stick

Stage II
- aural cues (rumbling onset), markedly increased descent rate, or improper roll control response as VRS gets worse
- corrective actions - trim the nacelles forward at max rate for two seconds (~15 deg forward); simultaneous and immediate forward stick to fly out of condition
*Increasing TCL in late stages of VRS may aggravate the condition and cause a roll-off

Stage III
- characterized by rapid uncommanded roll and corresponding large pitch; each rotor operating at very different aerodynamic conditions (known as “roll-off”)
- correction: nacelles should be rotated forward at max rate for 2 secs (~15 deg forward) and unusual attitude recovery procedures should be performed

Question 16

Stall practice pwr on

Answer 16

-min alt 5000 AGL
-recovery no lower than 3000 AGL
-APLN ONLY
-84 Nr, flaps 0 or auto
-wings level
-max decel 5 per sec
-max pitch 35
Max pwr 61% or level flight

Question 17

Stall pwr on

Answer 17

-Min alt 5000 AGL
-recover no lower than 3000 AGL
-APLN ONLY
-84% Nr, flaps 0 or auto
-wings level 150 KCAS
-min pwr
- maintain alt/raise nose
-stall buffet
Recover