1.1 - Fennec EP's (NYE) BOLD FACE ONLY Flashcards by Mikkel Dahlmann

COLLECTIVE - LOWER

NR - 320-430 RPM

AIRSPEED - ADJUST

AIRCRAFT - IN TRIM

Caution: The pilot may have to jettison external loads depending on circumstances.

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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.

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COLLECTIVE - MAINTAIN

TOUCH DOWN - CUSHION

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COLLECTIVE - LOWER

AIRSPEED - INCREASE

TOUCH DOWN - CUSHION

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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.

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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.

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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.

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COLLECTIVE - LOWER

If surging persists

TWIST GRIP - REDUCE (NR GREEN ARC)

If surging persists

LAND - AS SOON AS POSSIBLE

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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

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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.

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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.

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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.

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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.

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COLLECTIVE - LOWER

COLLECTIVE/AIRSPEED - TRIM (COORDINATED FLIGHT)

LANDING AREA - SELECT (STEEP APPROACH)

On final

AUTOROTATE

TWIST GRIP - IDLE (WHEN LDG ASSURED)

TOUCHDOWN - CUSHION

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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.

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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).