FRC (Indications)

Question 1

_____________landing in which the primary consideration is continued control of the aircraft and survival of the occupants. More urgent than land as soon as possible

Answer 1

Land without delay

Question 2

__________ landing at the nearest suitable landing area without delay. Primary consideration is to ensure the survival of occupants

Answer 2

Land as soon as possible

Question 3

__________ landing at a suitable landing area. Urgency of the emergency

Answer 3

Land as soon as practicable

Question 4

FADEC-F

Answer 4

Fly the aircraft
Alert the crew
Diagnose
Execute the emergency procedure
Communicate
Fly the aircraft

Question 5

INDICATIONS:

-Right Yaw with associated loss of yaw control

-Immediate loss of AC generators (GEN 1 & Gen 2)

-Immediate loss of hydraulics (PRI & UTIL HYD)

Answer 5

Main XMSN Tail Rotor Bevel_Idler gear set failure

1. EMERG HYD button- press on
2. Collective Reduce- Compromise between rate of turn and rate of descent
3. POWER LEVERS- OFF 10-20 ft above TD
4. Collective- Increase to cushion

-LAND WITHOUT DELAY

Question 6

INDICATIONS

-Hydraulic Fail warning

-Increased force or inability to move flight controls in all axes

-Primary and utility hydraulic pressures <1260 + BUCS FAIL caution + FMC DISENGAGE caution

Answer 6

Hydraulic Failure - Primary & utility hydraulic PSI low

1. EMERG HYD button- Press On

-LAND WITHOUT DELAY

Question 7

INDICATIONS

-LOW ROTOR RPM warning + LOW ROTOR rpm with possible loss of AC services

-ENGINE 1 OUT and ENGING 2 OUT warning

-Reduction in noise and audible change in rotor RPM

Answer 7

Dual Engine Failure

1. Autorotate
2. Chop button- reset

Question 8

INDICATIONS

-ENGINE OUT warning

-Rapid torque increase with flashing TQ displayed on HDU & FLT page (unaffected engine)

-Low and/decreasing TGT, Np, ENG OIL PSI, and Ng less than 63% (Affected Eng)

-Reduction in engine noise and possible audible change in rotor RPM

Answer 8

Single Engine Failure

1. Achieve safe singe engine flight conditions or land

-LAND AS SOON AS PRACTICABLE

Question 9

INDICATIONS

-Increase in Np, TGT, Ng, and TQ (clutch engaged) on affected ENG. ENGINE OVERSPEED warning

-Possible EDECU FAIL caution + EDECU FAIL + ? for TQ, TGT, and Np indications

-Possible HIGH ROTOR RPM warning + ROTOR RPM HIGH and an increase in rotor noise

Answer 9

Eng 1 or Eng 2 overspeed

1. Collective - adjust

-LAND AS SOON AS PRACTICABLE

Question 10

INDICATIONS

-LOW ROTOR RPM warning + change in rotor noise

-TQ, TGT, and Ng significantly lower than unaffected engine with sustained Ng >63%

-Possible flashing torque displayed on HDU & FLT page

-Possible ENGINE OUT warning + Engine out “VOICE”

Answer 10

Np Failed Low - Low Rotor RPM

1. Collective- Adj

-LAND AS SOON AS PRACTICABLE

Question 11

INDICATIONS

-Noticeable bank or popping noise

-Rapid increase in TGT and fluctuations Ng, TQ, and Np readings on affected engine

-Possible aircraft yaw

Answer 11

Engine Compressor Stall

1. Collective- Reduce

-LAND AS SOON AS PRACTICABLE

Question 12

INDICATIONS

-Illuminated APU FIRE button + APU fire “VOICE”

-Possible smoke/fumes, visual confirmation

Answer 12

APU Fire - In Flight

1. Illuminate APU FIRE button - Press
2. FIRE DISCH button (s)- Press

-LAND AS SOON AS POSSIBLE

Question 13

INDICATIONS

-Illuminated ENG FIRE button + ENG FIRE “voice”

-Possible high TGT on affected engine, smoke/fumes, visual confirmation

Answer 13

Engine 1 or Engine 2 Fire - In Flight

1. Achieve safe single engine flight conditions or land
2. Illuminated ENG FIRE button - Press
3. FIRE DISCH button (s)- Press

-LAND AS SOON AS POSSIBLE

Question 14

INDICATIONS

-Smell of burning insulation and/or acid smoke in crew station

Answer 14

Electrical Fire - In Flight

-LAND AS SOON AS POSSIBLE

Question 15

INDICATIONS

-Illuminated AFT FIRE button and one of the following

-AFT FIRE warning

-PASS-THRU BAY FIRE warning

-TAILBOOM FIRE warning

-Possible smoke/fumes

-Visible flames noted by wingman or ground crew

Answer 15

AFT Fire or Fuselage Fire - In Flight or On Ground

-LAND AS SOON AS POSSIBLE

Question 16

INDICATIONS

-Smoke and/or fumes in crew station

Answer 16

Smoke and Fume Elimination

-LAND AS SOON AS POSSIBLE

Question 17

INDICATIONS

-Illuminated ENG FIRE button + ENG FIRE “voice”

Answer 17

Engine 1 or Engine 2 Fire - On Ground

1. POWER LEVERS - OFF
2. Illuminated ENG FIRE button- Press and RDY light illuminates
3. FIRE DISCH button (s)- Press

Question 18

INDICATIONS

-Illuminated APU FIRE button + APU FIRE “voice”

Answer 18

APU Fire - On Ground

1. APU - OFF
2. Illuminated APU FIRE button - Press
3. FIRE DISCH button (s)- Press

Question 19

INDICATIONS

-Rapid right yaw
-Possible GRBX VIBRATION caution

Answer 19

Loss of Tail Rotor Thrust - Continued Flight Not Possible

1. Collective - Reduce (compromise between rate of turn and rate of descent)
2. POWER LEVERS- OFF (5-10 ft above TD)
3. Collective - increase to cushion

Question 20

INDICATIONS

-Right yaw with associated loss of yaw control

-Possible GRBX VIBRATION caution

Answer 20

Loss of Tail Rotor Thrust - Continued Flight Possible

1. Airspeed- 100 KTAS min (until 10-20 ft above TD)

-LAND AS SOON AS PRACTICABLE

Question 21

INDICATIONS

-Loss of yaw control

-Possible TAIL ROTOR HYD warning + TAIL ROTOR HYD FAILURE “voice”

Answer 21

Tail Rotor Fixed Pitch - Low Airspeed or Hover

1. Collective - Adj to min yaw rate
2. Cyclic - minimize drift

If pedals are jammed
3. Break into BUCS

Question 22

INDICATIONS

-Loss of yaw control

-possible TAIL ROTOR HYD warning + TAIL ROTOR HYD FAILURE “voice”

Answer 22

Tail Rotor Fixed Pitch - Forward Flight

1. Collective - Adj to min yaw
2. Cyclic - oppose yaw

If pedals are jammed
3. Break into BUCS

-LAND AS SOON AS PRACTICABLE

Question 23

INDICATIONS

-Sudden increase in main rotor vibration and/or unusual noise

-Severe main rotor flapping

-Abnormal control response (Feeback or Resistance)

Answer 23

Main Rotor Components

-LAND AS SOON AS POSSIBLE

Question 24

INDICATIONS

-Uncommanded flight control inputs

-Resistance or increased force required to move the flight controls

-Sluggish flight control response

Answer 24

Flight Control Malfunction

1. FMC release button - press

(Uncommanded inputs - LAND AS SOON AS PRACTICABLE)

(Restriction - LAND AS SOON AS PRACTICABLE)

Question 25

INDICATIONS FAILS TO ENGAGE -No TQ indication on affected engine or Np exceeds rotor RPM (Nr) FAILS TO DISENGAGE -Np does not drop below rotor RPM (Nr) with POWER LEVER (affected engine) at IDLE

Answer 25

Main XMSN Input Drive Clutch Failure- on ground FAILS TO ENGAGE 1. Power lever (affected eng)- off 2. Check NG 3. Normal eng shutdown- perform FAILS TO DISENGAGE 1. POWER LEVERs- OFF BOTH ENGINES

Question 26

INDICATIONS -Erratic or no TQ indication on affected engine -Np exceeds rotor RPM (Nr) -Np does not drop below rotor RPM (Nr) with POWER LEVER (affected engine) at IDLE -Possible ENGINE OVERSPEED (sudden disengagement)

Answer 26

Main XMSN Input Drive Clutch Failure - In Flight 1. Achieve safe single engine flight conditions or land Np drops below Nr -LAND AS SOON AS PRACTICABLE Np does not drop below Nr -LAND AS SOON AS POSSIBLE

Question 27

INDICATIONS -Loss of FLIR image -Possible NVS FAIL message on HAD -Possible loss of PNVS elevation control (PNVS elevations mirror failure)

Answer 27

NVS Failure 1. Exit NOE flight conditions 2. Pilot on controls, NVS select SW- Select alternate sensor (PNVS or TADS)

Question 28

INDICATIONS -PLT FORMAT or CPG FORMAT will flash for 3 seconds and remain displayed in HMD FORMAT OWNER CUE section of the HAD in both crew stations

Answer 28

Single MP operation 1. NVS select sw- Reselect 2. Crewmember (not on controls) - Assume control

Question 29

INDICATIONS -NO COMMUNICATIONS WITH MP + loss of HDU symbology/imagery + loss of FMC inputs + loss of MPDs + non-operational KU/EUFD

Answer 29

Dual MP Failure - MP 1 and MP 2 Fail 1. Exit NOE environment -LAND AS SOON AS POSSIBLE

Question 30

Abort start reasons..

Answer 30

- Apparent that TGT will exceed 851 before Ng Idle speed (63% or more) - TGT does not increase within 45 seconds after moving power lever to idle - No Np within 45 seconds after moving power lever to idle (Unless rotor is locked) - No positive oil pressure 45 seconds - Eng 1 or 2 starts advisory is removed prior to 52% NG