Red Pages - BOLD Face Flashcards

These cards may never stand alone and is an addition to the FRC! (AL21)

1
Q

APU BAY FIRE ON THE GROUND

A

ECS - MASTER switch OFF
Deselect APU START/STOP button
APU FUEL switch OFF
Start clock - time for 30 seconds

Warning remains

Select FIRE extinguisher to XFEED
(Fire extinguisher automatically discharges)

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2
Q

ENGINE BAY FIRE ON THE GROUND

A

ECS - MASTER switch OFF
ENG * engine condition switch OFF
ENG * FUEL switch OFF
Press illuminated FIRE button
Start clock - time for 30 seconds

Warning remains
Select FIRE extinguisher to XFEED
Press illuminated FIRE button again

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3
Q

ENGINE FIRE POST SHUTDOWN

A

Confirm Fire warnings not illuminated
ENG 1, 2 and 3 engine condition switches OFF
ENG 1, 2 and 3 FUEL switches OFF
APU status READY indicator illuminated
BLEED switch to APU
On affected engine, select engine condition switch to
VENT for 30 seconds
Confirm fire extinguished and select engine condition
switch OFF

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4
Q

ELECTRICAL FIRE AND SMOKE ON THE GROUND

A

ECS - MASTER switch OFF
ENG 1, 2 and 3 engine condition switch OFF
ENG 1, 2 and 3 FUEL switch OFF
Deselect APU START/STOP button
APU FUEL switch OFF
BATT switch OFF
Evacuate aircraft

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5
Q

APU BAY FIRE IN FLIGHT

A

Achieve safe flight condition
ECS - MASTER switch OFF
APU FUEL switch OFF
Press illuminated APU FIRE button
Start clock - time for 30 second

Warning remains/Warning re-appears
Select fire extinguisher to XFEED
Press illuminated APU FIRE button again.
Start clock - time for 30 seconds

Warning remains
Check for positive signs of fire

With positive signs of fire
Land immediately

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6
Q

ENGINE BAY FIRE IN FLIGHT

A

Achieve safe OEI flight condition
ECS - MASTER switch OFF
ENG * engine condition switch OFF
ENG * FUEL switch OFF
Press illuminated FIRE button
Start clock - time for 30 seconds

Warning remains/Warning re-appears
Select fire extinguisher to XFEED
Press appropriate FIRE button again.
Start clock - time for 30 seconds

Warning remains
Check for positive signs of fire

With positive signs of fire
Land immidiately

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7
Q

ENGINE BAY FIRE IN TEC FLIGHT

A

Achieve safe flight condition
ECS - MASTER switch OFF
ENG * engine condition switch OFF (see Note 1)
ENG * FUEL switch OFF
Press illuminated FIRE button
Start clock - time for 30 seconds
Start APU
Confirm READY indicator illuminated
EMERG/NORM switch EMERG
BLEED switch to APU
No 3 engine DRIVE switch to MAIN, MI MAIN (see CAUTION)
Restart No 3 Engine

Warning remains after 30 seconds
or
Warning re-appears

Select fire extinguisher to XFEED
Press illuminated FIRE button again
Start clock - time for 30 seconds

Warning remains

Check for positive signs of fire

With positive signs of fire

Land immediately

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8
Q

FUMES, SMOKE AND/OR FIRE IN COCKPIT/CABIN

A

Achiece safe flight condition and prepare for descent and landing if required
If smoke or fire severe - Land Immediately
ECS - MASTER switch OFF
CREW FAN switch OFF
Start the APU
Prepare to use fire extinguisher(s)
Ventilate cockpit and cabin

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9
Q

FUMES, SMOKE AND/OR FIRE IN COCKPIT/CABIN - SYSTEMS AVAILABLE

APU ON - EMERG/NORM EMERG - GEN1&2 OFF

A

AP - certain cruise modes only
ASE (FCC 1 only)
ASMC 1+2
Cockpit emergency lighting and flood lights
EGI
IDU 1/4/6
Navigation lights
Pilot’s CCU
Pilot landing light
Rad Alt 2
Radios

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10
Q

FUMES, SMOKE AND/OR FIRE IN COCKPIT/CABIN - SYSTEMS UNAVAILABLE

APU ON - EMERG/NORM EMERG - GEN1&2 OFF

A

ACSR
Co-pilot’s CCU
Co-pilot landing light
DVS
External floodlights
IDU 2/3/5
Night/NVG dimming illumination
Rad Alt 1
SAR console CCU

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11
Q

ENGINE FAILURE IN FLIGHT

A

Check and control NR
Jettison external load if required
Achieve safe OEI flight condition or conduct vertical/forward reject

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12
Q

ENGINE FAILURE DURING TEC FLIGHT

A

Check and control NR
Achieve safe TEI (level flight may not be possible)
Start APU
BLEED switch to APU

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13
Q

DOUBLE ENGINE FAILURE IN FLIGHT

A

Check and control NR
Jettison external load if required
Achieve safe TEI (level flight may not be possible) or
conduct vertical/forward reject
BLEED switch to APU

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14
Q

TRIPLE ENGINE FAILURE IN FLIGHT

A

Rapidly lower collective fully to maintain NR
Jettison external load if required
Rear crew rotating seats - facing forward, plinth locked
Harnesses locked and tight
Initiate distress procedure (HF or V/UHF and IFF)

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15
Q

ENGINE ELECTRONIC CONTROL UNIT FAILURE

(EECU)

A

Check and control NR
Achieve safe OEI flight

Practicable

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16
Q

ENGINE OIL PRESSURE LOW

A

Achieve safe OEI flight
Check oil temperature and pressure on affected engine

Practicable

17
Q

MAIN GEARBOX OIL PRESSURE LOW

A

Achieve safe flight condition
GEN 2 switch OFF (see Note 1)

ASAP

18
Q

MAIN GEARBOX OIL TEMPERATURE HIGH

A

Achieve safe flight condition

19
Q

INTERMEDIATE GEARBOX OIL PRESSURE LOW

A

Achieve safe flight condition

20
Q

INTERMEDIATE GEARBOX OIL TEMPERATURE HIGH

A

Achieve safe flight condition

21
Q

TAIL GEARBOX OIL TEMPERATURE HIGH

A

Achieve safe flight condition

22
Q

ROTOR RPM LIMITS

“ROTOR ROTOR” or “ROTOR HIGH”

A

Check rotor speed
Adjust collective to maintain rotor RPM within limits

23
Q

ROTOR RPM LIMITS

“OVERSPEED”

A

Check rotor speed
Adjust collective to maintain rotor RPM within limits

24
Q

ROTOR DE-ICING - Failure of RIPS

A

Check prevailing icing conditions

25
Q

TAIL ROTOR DRIVE FAILURE - IN THE HOVER

A

Lower collective
Stop any drift using cyclic
Land emmediately
or
If height/time permit, enter autorotation
Shutdown engines
Conduct EOL

26
Q

TAIL ROTOR DRIVE FAILURE - IN FORWARD FLIGHT

A

Establish autorotation at 80 knots
Landing gear as required
Jettison external load
Shutdown engines
Rear crew rotating seats
- facing forward, plinth locked
Harness locked and tight
Initiate distress procedure
(HF or V/UHF and IFF)
Conduct EOL

27
Q

TAIL ROTOR CONTROL JAM/FAILURE - IN FORWARD FLIGHT

A

Change power/speed to control yaw
If yawing right, LOWER collective
If yawing left, RAISE collective
Use lateral cyclic if required to reduce yaw (cross control)
If collective forces increase place feet on pedals
(see CAUTION)

Sustained flight achievable?
(Cross control if required. May be significant side slip)

NO

Aircraft descending
Very low tail rotor thrust
Immediate autorotation may be required
If possible fly at 80 KIAS
Cross control to reach suitable landing area
Enter autorotation
Carry out EOL (see Note 1)

Aicraft climbing
Very high tail rotor thrust
Reduce speed until descending
Reduce NR to aid descent
Descend with high torque/low airspeed
Beware vortex ring
Wind from the right may assist
Land as soon as possible

28
Q

TAIL ROTOR CONTROL JAM/FAILURE - IN THE HOVER

A

Lower collective
Stop any drift using cyclic
Land immediately

29
Q

DOUBLE AC GENERATOR FAILURE

A

Achieve safe flight condition within ACSR OFF/degraded flight envelope (see Note 1)
ANTI ICE - ROTOR switch OFF
Start APU (See Note 2)
AC BUS to SPLIT
Attempt to reset generators by selecting GEN 1 and GEN 2 OFF then ON (two attempts permissible), (See Note 3)
If reset unsuccessful, select both generators to OFF

30
Q

DITCHING

A

Warn the crew - “PREPARE FOR DITCHING”
Rear crew rotating seats - facing forward, plinth locked
Check harness locked and tight
Jettison external load
Ramp and doors closed
Initiate distress procedures (HF or V/UHF and IFF)

31
Q

SEVERE VIBRATION

In flight

A

Relax grip on flying controls to minimize the possibility of bio-mechanical feedback (See Notes 1, 2 and 4)
Turn into wind (if possible) (see Note 5)
Establish steady level flight at 60 knots to 100 knots

32
Q

SEVERE VIBRATION

On the ground (wheels in contact)

A

Or, if conditions dictate:
(eg deck landing)
Take-Off immediately
Follow In Flight advice
(see WARNING 1 and Note 6

If possible:
Lower collective to MPOG
(relax grip and release trim)
(see Notes 1, 3 and 4)

Vibration remains
Shutdown immediately

Vibration eliminated
Continue sortie

33
Q

POST LIGHTNING STRIKE PROCEDURES

A

Achieve safe flight condition within ACSR OFF/Degraded flight envelope
Use the AFCS Lane/Axis PCU pushbuttons to clear OUT indications and indications of PArallel Actuator disengagement

34
Q

FLYING CONTROL MALFUNCTION

A

See Card R16 reverse