1.1 - Fennec EP's (NYE) BOLD FACE ONLY Flashcards
COLLECTIVE - LOWER
NR - 320-430 RPM
AIRSPEED - ADJUST
AIRCRAFT - IN TRIM
Caution: The pilot may have to jettison external loads depending on circumstances.
AUTOROTATE
TWIST GRIP - FUEL CUT OFF
- Relight engine at pilot’s discretion
If no relight
FUEL SHUT OFF LEVER - PULL
FUEL P1 AND FUEL P2 - OFF
GEN - OFF
INV - OFF
If there is a smell of burning
CUT OFF - PRESS
D BAT - OFF
WARNING: If an engine failure occurs at night do not cut off the battery. Switch on the LDG / Search Light below 1000’ AGL.
NOTE: If possible perform a MAYDAY call prior to cutting off battery power.
COLLECTIVE - MAINTAIN
TOUCH DOWN - CUSHION
COLLECTIVE - LOWER
AIRSPEED - INCREASE
TOUCH DOWN - CUSHION
FUEL P1 AND FUEL P2 - ON
GEN - ON
NORMAL START - ACCOMPLISH
NG must be below 30% before normal starting procedure
NOTE: In order to avoid any jerk on re-synchronization, accelerate the engine progressively, when NTL approaches Nr.
AUTOROTATE
TWIST GRIP - EMERGENCY RANGE (70% NG)
COLLECTIVE - RAISE (NR 350 RPM)
TWIST GRIP - INCREASE (NR GREEN ARC)
COLLECTIVE/TWIST GRIP - TRIM (NR GREEN ARC)
- Land as soon as practical
NOTE: It is not possible to reach the emergency range unless the emergency range slide switch is pressed. A slight rotation of the twist grip to the right may be necessary to obtain unlocking.
COLLECTIVE - MAINTAIN/RAISE
TWIST GRIP - REDUCE (NR GREEN ARC)
COLLECTIVE/TWIST GRIP - TRIM (NR GREEN ARC)
- Land as soon as practical
NOTE: It is possible to adjust the twist grip during the landing phase.
COLLECTIVE - LOWER
If surging persists
TWIST GRIP - REDUCE (NR GREEN ARC)
If surging persists
LAND - AS SOON AS POSSIBLE
Fire confirmed:
TWIST GRIP - FUEL CUT OFF
FUEL SHUT OFF LEVER - PULL
ROTOR BRAKE SAFE - RELEASE
ROTOR BRAKE - APPLY
FUEL P1 AND FUEL P2 - OFF
CRK - PRESS FOR 10 SEC
CUT OFF - PRESS
D BAT - OFF
- Extinguish fire if feasible
Fire not confirmed:
- Normal shutdown
Fire confirmed:
AUTOROTATE
TWIST GRIP - FUEL CUT OFF
FUEL SHUT OFF LEVER - PULL
FUEL P1 AND FUEL P2 - OFF
GEN - OFF
INV - OFF
If there is a smell of burning
CUT OFF - PRESS
D BAT - OFF
Fire not confirmed:
LAND - AS SOON AS POSSIBLE
WARNING: If an engine fire occurs at night do not cut off the battery. Switch on the LDG / Search Light below 1000’ AGL.
NOTE: If possible perform a MAYDAY call prior to cutting off battery power.
CORRESPONDING SYSTEM - SHUT OFF
FIRE EXTINGUISHER - USE IF NECESSARY
CABIN - VENTILATE
- Land as soon as practical
NOTE: Ventilate the cabin by opening the front ventilator, the ventilation louvers and the bad weather window.
HEATING AND DEMISTING - OFF
CABIN - VENTILATE
If smoke does not clear
CUT OFF - PRESS
D BAT - OFF
At pilots discretion when smoke has cleared
ESSENTIAL EQUIPMENT - RESET
- Land as soon as practical
NOTE: Ventilate the cabin by opening the front ventilator, the ventilation louvers and the bad weather windows.
NOTE: Prior to resetting essential equipment ensure that all electrical switches are OFF, close all cabin ventilation and then turn on the required equipment one by one in order to identify the malfunctioning system.
IGE
TWIST GRIP - IDLE
TOUCH DOWN - CUSHION
OGE
COLLECTIVE - LOWER
AIRSPEED - INCREASE
If able, transition to forward flight and proceed with TAIL ROTOR DRIVE FAILURE IN FLIGHT EP, otherwise
TOUCH DOWN - CUSHION
CAUTION: During an OGE drive failure, if unable to transition to forward flight and time permits, consider moving the twist grip to idle in order to cancel out torque during the cushion.
COLLECTIVE - LOWER
COLLECTIVE/AIRSPEED - TRIM (COORDINATED FLIGHT)
LANDING AREA - SELECT (STEEP APPROACH)
On final
AUTOROTATE
TWIST GRIP - IDLE (WHEN LDG ASSURED)
TOUCHDOWN - CUSHION
AIRSPEED - 70 KTS LEVEL FLIGHT
HYD TST - PRESS
HYD TST - RESET AFTER 5 SEC
- Land as soon as practical
- Shallow approach with left sideslip
- Run-on landing
CAUTION: Landing is made easier with a right-quartering headwind. If the airspeed is lower than 20 KIAS, go-around is impossible due to the decreased efficiency of the fin.
ENGINE FAILURE IN FLIGHT EP - ACCOMPLISH
DOORS - OPEN
BEFORE WATER CONTACT - DOORS JETTISON
Upon water contact with minimum forward A/S
COLLECTIVE - APPLY FULL PITCH AS HELICOPTER SETTLES
CREW AND PASSENGERS - EXIT WHEN ROTOR STOPS TURNING
- Jettison the doors at a hover
- Crew and passengers except pilot EXIT helicopter
- Hover to safe distance from personnel
- Switch off all electrical switches
- Pull the fuel shut off lever
- Autorotate
Upon water contact with minimum forward A/S:
COLLECTIVE - APPLY FULL PITCH AS HELICOPTER SETTLES
PILOT - EXIT WHEN ROTOR STOPS TURNING
WARNING/CAUTION PANEL - TEST
If ENG P light does not illuminate and torque meter low/zero:
AUTOROTATE
ENGINE - SHUT DOWN
If torque meter correct, or ENG P light illuminates and torque meter low/zero:
LAND - AS SOON AS POSSIBLE
- Shut down the engine immediately after landing
If ENG P light illuminates and torque meter correct:
- Monitor ENG P light
- Land as soon as practical
POWER - REDUCE
AIRSPEED - ADJUST (80 KIAS)
LAND - AS SOON AS POSSIBLE
ENGINE - SHUT DOWN
OIL PRESSURE INDICATOR - CHECK
If oil pressure is low:
LOW ENG OIL PRESSURE EP - ACCOMPLISH
If oil pressure is normal maintain Ng below the following:
- Land as soon as practical
If Nr and NTL values agree:
COLLECTIVE - LOWER
If reading does not rise to governed value:
- Refer to Governor Failure EP’s
TORQUE - MAINTAIN ABOVE 10%
NR - READ ON NTL POINTER
LAND - AS SOON AS POSSIBLE
- Slowly move collective (torque above 10%)
If Nr does not remain in governed range:
LAND - AS SOON AS POSSIBLE
If Nr remains in governed range:
- Land as soon as practical
In hover
HYD PRESSURE SWITCH - OFF
LAND - NORMALLY
In flight
HYD PRESSURE SWITCH - OFF
HYD LIGHT EP - ACCOMPLISH
CAUTION: Hovering HYD OFF is extremely demanding and should only be attempted if absolutely necessary. In the event of a Yaw servo-control slide-valve seizure in a hover with no rotation consider maintaining hydraulic pressure throughout the landing.
NOTE: Load feedback will be felt immediately and may be heavy if the helicopter is flying at high speed:
Collective pitch: Approximately 20 kg load increase.
Cyclic: Approximately 7-12 kg left-hand cyclic load and 2-4 kg forward cyclic load.
Yaw pedals: Practically no load in cruising flight.
TRIM RELEASE SWITCH - PRESS AND HOLD
If blockage persists
SHEAR PIN - BREAK (+10 KG FORCE)
- Land as soon as practical
If blockage disappears
- Press the FEEL REL pushbutton
- Continue flight in accordance with MEL
Avoid abrupt maneuvers and maintain angle of bank below 30°.
AUTOPILOT - DISENGAGE
In flight
AIRSPEED - ADJUST
HYD PRESSURE SWITCH - OFF
- Land as soon as practical
- Fly a shallow approach
- Perform a run-on landing at low speed
- Perform a normal engine shut down
Hover IGE, Takeoff and Final (if landing within 30 sec. is possible):
- Land normally
- Perform a normal engine shut down
WARNING: As control loads increase, be careful not to inadvertently move twist grip out of flight position.
WARNING: Do not depress HYD TEST as this will result in heavy pedal control loads.
WARNING Do not attempt hover flight or any low speed maneuvers as this will result in excessive pilot workload, poor aircraft control and possible loss of aircraft control.
CAUTION: The pilot may have to jettison external loads if control load is found to be too significant at safe speed.
NOTE: Accumulators will compensate hydraulic pressure loss for a limited operation of the main rotor controls allowing to secure flight conditions and to establish hydraulic failure safety speed (40-60 KIAS). Each control input will deplete HYD pressure in the accumulators. If unsure whether the landing can be accomplished before HYD pressure depletion, or if failure occurs in hover OGE, consider proceeding to forward flight.
NOTE: Do not silence the horn with the HORN switch. The horn will be silenced when the pilot selects the hydraulic system cut-off switch to OFF.
NOTE: Speed may be increased as necessary, but control loads will increase with speed.
POWER - REDUCE
LAND - AS SOON AS POSSIBLE
NOTE: The MGB has passed a bench test consisting in running the gearbox for 45 min. with zero oil pressure at the power corresponding to minimum power in level flight (at 55 KIAS).
WARN./CAUTION PANEL - TEST
If MGB P light does not illuminate:
POWER - REDUCE
LAND - AS SOON AS POSSIBLE
If MGB P light illuminates:
- Land as soon as practical
BATTERY - OFF
- Check voltage
If above 31.5 volts:
- Battery pushbutton to ON
- Generator pushbutton to OFF
- Reduve electrical load as applicable
- Monitor voltage (22 minimum)
- Land as soon as practical
If normal:
- Land as soon as practical
POWER - REDUCE
OIL PRESS AND TORQUE - CHECK
If both are low or zero:
AUTOROTATE
ENGINE - SHUT DOWN
If either or both are correct:
LAND - AS SOON AS POSSIBLE
LAND - AS SOON AS POSSIBLE
POWER - REDUCE
If light remains on:
LAND - AS SOON AS POSSIBLE
If light goes out:
- Continue flight at reduced power
- Land as soon as practical
