Red Pages - BOLD Face Flashcards
These cards may never stand alone and is an addition to the FRC! (AL21)
APU BAY FIRE ON THE GROUND
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)
ENGINE BAY FIRE ON THE GROUND
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
ENGINE FIRE POST SHUTDOWN
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
ELECTRICAL FIRE AND SMOKE ON THE GROUND
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
APU BAY FIRE IN FLIGHT
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
ENGINE BAY FIRE IN FLIGHT
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
ENGINE BAY FIRE IN TEC FLIGHT
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
FUMES, SMOKE AND/OR FIRE IN COCKPIT/CABIN
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
FUMES, SMOKE AND/OR FIRE IN COCKPIT/CABIN - SYSTEMS AVAILABLE
APU ON - EMERG/NORM EMERG - GEN1&2 OFF
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
FUMES, SMOKE AND/OR FIRE IN COCKPIT/CABIN - SYSTEMS UNAVAILABLE
APU ON - EMERG/NORM EMERG - GEN1&2 OFF
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
ENGINE FAILURE IN FLIGHT
Check and control NR
Jettison external load if required
Achieve safe OEI flight condition or conduct vertical/forward reject
ENGINE FAILURE DURING TEC FLIGHT
Check and control NR
Achieve safe TEI (level flight may not be possible)
Start APU
BLEED switch to APU
DOUBLE ENGINE FAILURE IN FLIGHT
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
TRIPLE ENGINE FAILURE IN FLIGHT
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)
ENGINE ELECTRONIC CONTROL UNIT FAILURE
(EECU)
Check and control NR
Achieve safe OEI flight
Practicable
ENGINE OIL PRESSURE LOW
Achieve safe OEI flight
Check oil temperature and pressure on affected engine
Practicable
MAIN GEARBOX OIL PRESSURE LOW
Achieve safe flight condition
GEN 2 switch OFF (see Note 1)
ASAP
MAIN GEARBOX OIL TEMPERATURE HIGH
Achieve safe flight condition
INTERMEDIATE GEARBOX OIL PRESSURE LOW
Achieve safe flight condition
INTERMEDIATE GEARBOX OIL TEMPERATURE HIGH
Achieve safe flight condition
TAIL GEARBOX OIL TEMPERATURE HIGH
Achieve safe flight condition
ROTOR RPM LIMITS
“ROTOR ROTOR” or “ROTOR HIGH”
Check rotor speed
Adjust collective to maintain rotor RPM within limits
ROTOR RPM LIMITS
“OVERSPEED”
Check rotor speed
Adjust collective to maintain rotor RPM within limits
ROTOR DE-ICING - Failure of RIPS
Check prevailing icing conditions
TAIL ROTOR DRIVE FAILURE - IN THE HOVER
Lower collective
Stop any drift using cyclic
Land emmediately
or
If height/time permit, enter autorotation
Shutdown engines
Conduct EOL
TAIL ROTOR DRIVE FAILURE - IN FORWARD FLIGHT
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
TAIL ROTOR CONTROL JAM/FAILURE - IN FORWARD FLIGHT
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
TAIL ROTOR CONTROL JAM/FAILURE - IN THE HOVER
Lower collective
Stop any drift using cyclic
Land immediately
DOUBLE AC GENERATOR FAILURE
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
DITCHING
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)
SEVERE VIBRATION
In flight
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
SEVERE VIBRATION
On the ground (wheels in contact)
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
POST LIGHTNING STRIKE PROCEDURES
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
FLYING CONTROL MALFUNCTION
See Card R16 reverse
