Red Pages

Question 1

ICING CONDITIONS

Answer 1

Helicopter…………………………..Fly clear of Icing conditions

(non-memory)
ENG ANTI-ICE switch………..ON
PITOT HEAT switch……………ON
TOT………………………………………Maintain within limits
If icing persists:
Helicopter………………………..Land as soon as possible

Question 2

CHIP FAULT, ENG CHIP, TR CHIP, TRANS CHIP

Answer 2

CHIP FAULT caution light switch……….Press then release
If lights persist
Helicopter……………………………………..Land as soon as possible

(non-memory)
If lights extinguish:
Clock…………………………………………….Start
Consult checklist for specifics

Question 3

BATTERY HOT

Answer 3

BAT switch……………………………………OFF
Helmet visor…………………………………Down
Helicopter…………………………………….Land as soon as possible
Do an emergency shutdown
Avoid battery compartment area

Question 4

BATTERY TEMP

Answer 4

(NOT A RED PAGE)
BATT switch………..OFF (Remains OFF until caution light extinguishes)
Helmet visor………..Down
If frequent and repetitive illumination:
Helicopter……………Land as soon as practical

Question 5

GEN FAIL

Answer 5

(NOT A RED PAGE)
Loadmeter……………………..Check
GEN FIELD and GEN RESET C/Bs…….Check IN
GEN switch…………………………………………..RESET then ON
If light remains illuminated:
GEN switch…………………..OFF
Load shed…………………….All electrical components OFF
Required systems ON
(transponder, anti-ice, landing lights, pulse)
Altitude………………………….Reduce to below 6000’ Hp
Helicopter……………………..Land as soon as practical
Consider remaining battery power

Question 6

FUEL PUMP

Answer 6

Fuel pressure………Check
If no indication of fuel pressure (dual pump failure)
Helicopter………..Land as soon as possible
A dual pump failure can cause the loss of head pressure to the engine-driven fuel pump and result in power loss

(non-memory)
If an indication of fuel pressure (single pump failure)
Altitude…………….Descend below 6000’ Hp
Helicopter………..Land as soon as practical

Question 7

FUEL FILTER

Answer 7

Helicopter……Land as soon as practical

Be prepared for an engine failure at any time

Question 8

AF FUEL FILTER

Answer 8

(NOT A RED PAGE)

Helicopter………………….Land as soon as practical

Question 9

TRANS OIL TEMP

Answer 9

Collective……………………Reduce power
Monitor gage
If light remains on:
Helicopter……………….Land as soon as possible

(non-memory)
If light goes out:
Helicopter……………….Land as soon as practical

Question 10

TRANS OIL PRESS

Answer 10

Helicopter…………………Land as soon as possible
Monitor gage

FYI - AVOID AGGRESSIVE COLLECTIVE MOVEMENTS

Question 11

ENG OIL PRESSURE

Answer 11

Engine oil pressure and temperature gage………Monitor gage
Helicopter……………………….Land as soon as possible

(non-memory)
If engine oil pressure within limits but fluctuates:
Engine oil pressure and temperature gage………Monitor gage
Helicopter……………………….Land as soon as practical

Question 12

ENG OIL TEMPERATURE

Answer 12

(NOT A RED PAGE)
Engine oil pressure and temperature gage………Monitor gage
BLOWER A/C switch……………………OFF
Helicopter……………………………………..Land as soon as practical

FYI - Engine damage may occur if temp above 107C for more than 10 minutes or exceeds 120C for any length of time - LAND AS SOON AS POSSIBLE

Question 13

FREE-WHEEL UNIT FAILURE

Answer 13

Helicopter…………………………Establish autorotation
Collective………………………….Maintain 90% to 107% Nr
Throttle……………………………..Idle

(non-memory)
If time and altitude permit:
Throttle…………………………Open
If Nr and N2 rise together:
Limited powered flight can be possible
Helicopter…………………Land as soon as possible
If unable to maintain powered flight
Helicopter…………………Establish autorotation
Follow engine failure procedure

FYI - Identified by N2 greater than Nr, dropping TQ, N1 around 81%, and TOT lower than normal, and Nr is responding to collective inputs

Question 14

ENGINE COMPRESSOR STALL

Answer 14

Collective…………………………..Reduce
ENG ANTI-ICE switch……….ON
HEAT VENT switch…………..ON
BLOWER A/C switch…………OFF
If problem continues:
Helicopter………………………Land as soon as possible
Be prepared for engine failure at any time

(non-memory)
If problem stops:
Helicopter………………………Monitor TOT and N1
Land as soon as practical

FYI - random power fluctuations, rumbling or popping, vibrations, dropping Nr, rising TOT, fluctuating N1. Likely to occur on an overshoot with minimal fwd airspeed.

Question 15

ENGINE RESTART (In-flight)

Answer 15

Altimeter………………………..Check for sufficient altitude
Collective………………………Maintain 90% to 107% Nr
Helicopter………………………Reduce airspeed to 52-69 KIAS
Throttle…………………………..Close
ENG ANTI-ICE switch……OFF
PITOT HEAT switch……….OFF
GEN switch…………………….OFF
Engine…………………………….Proceed with normal start
If engine idles normally:
Throttle………………………Open slowly to FULL
TOT…………………………….Monitor
Helicopter………………….Land as soon as possible
If no relight:
FUEL VALVE switch….OFF
BAT switch…………………OFF
Helicopter………………….Complete autorotation landing

Question 16

EMERGENCY SHUTDOWN

Answer 16

Throttle………………………Close and hold until N1 is 0
FUEL VALVE switch….OFF
BAT switch…………………OFF
Rotor brake………………..Engage
Allow rotors to stop
Helicopter…………………..Open or jettison doors and egress

Question 17

DITCHING (Power-OFF)

Answer 17

Helicopter……………………..Establish autorotation
Collective………………………Maintain 90% to 107% Nr
BLOWER A/C switch…….OFF
Doors……………………………..Open and Locked
Cyclic……………………………..Reduce groundspeed to 0 before touchdown
Maintain level attitude
Collective………………………Maintain rate of descent as
rotorcraft settles into the water
Helicopter……………………..Allow rotors to stop and egress

Question 18

HYDRAULIC SYSTEM HARDOVER

Answer 18

HYDRAULIC SYSTEM switch……..OFF

Helicopter……………………………………..Land as soon as possible

Question 19

HYDRAULIC SYSTEM FAILURE

Answer 19

(NOT A RED PAGE)
Helicopter……………………………………Reduce AS to 61-69 KIAS
HYDRAULIC SYSTEM switch…….Confirm ON
HYD BOOST CB…………………………OUT
If hydraulic pressure is not regained:
HYD BOOST CB……………………..IN
HYDRAULIC SYSTEM switch…OFF
Helicopter…………………………………Land as soon as practical
Minimize flight control
movements
Approach………………………………….Shallow to normal
Terminate in a run-on landing
Landing……………………………………..A run-on landing at 10-15
KIAS is recommended
MAX 10kt Groundspeed
with SKIS

Question 20

PEDALS LOCKED AT HOVER (LEFT)

Answer 20

Cyclic……………………………..Eliminate drift
Collective……………………….Lower
Throttle…………………………..Maintain power to decrease the rate of left rotation
Landing………………………….Accept left rotation on touchdown

Question 21

PEDALS LOCKED AT HOVER (RIGHT)

Answer 21

Throttle………………………….Idle
Cyclic…………………………….Eliminate drift
Collective……………………..Cushion landing

Question 22

PEDALS LOCKED IN FLIGHT

Answer 22

(NOT A RED PAGE)
Helicopter…………….Maintain controllable AS above 60KIAS
FOD check…………..Complete
Landing area………..Suitable site
Avoid built up areas or trees on-route
Approach………………Shallow to normal
Landing………………….Use procedures for PL@H

Question 23

LOSS OF TAIL ROTOR EFFECTIVENESS

Answer 23

Helicopter………………Establish autorotation
Complete controllability check
If adverse yaw is encountered:
Helicopter………….Resume autorotation
Throttle………………Close for landing
Helicopter………….Land as soon as possible

Consult checklist for specifics

Question 24

MAIN DRIVESHAFT FAILURE

Answer 24

Helicopter……………………..Establish autorotation
Collective………………………Maintain 90% to 107% Nr
Throttle………………………….Maintain 97% to 100% N2
BLOWER A/C switch……OFF
Helicopter…………………….Complete autorotation landing

Question 25

LOW ROTOR RPM

Answer 25

Collective…………………………….Reduce
Throttle…………………………………FULL
GOV RPM (beep) switch…….Increase to maximum
BLOWER A/C switch…………..OFF
If RPM still decreasing:
Helicopter………………………..Treat as an engine failure

Question 26

LOW SIDE GOV FAILURE

Answer 26

Collective………………………Maintain 90% to 107% Nr
Throttle………………………….FULL
GOV RPM switch………….Increase to maximum
BLOWER A/C switch……OFF
If unable to maintain powered flight:
Throttle……………………..Close
Helicopter……………………..Establish autorotation
Collective………………………Maintain 90% to 107% Nr
Helicopter…………………….Complete autorotation landing
If powered flight can be maintained:
Helicopter………….Land as soon as possible

Question 27

ENGINE FAILURE AT HOVER OR TAXI

Answer 27

Pedals……………..Align skids
Cyclic……………….Control direction, attitude and drift
Collective………..Cushion landing

Question 28

ENGINE FAILURE IN FLIGHT

Answer 28

Helicopter………………Establish autorotation
Collective………………………Maintain 90% to 107% Nr
BLOWER A/C switch……OFF
STARTER switch…………..Engage
(Attempt immediate restart within 10 seconds if failure is not mechanical)
If engine fails to restart:
Throttle…………………………Closed
Helicopter…………………….Complete autorotation landing
If time permits:
Passengers and Crew….Alert
Radio……………………………..Transmit MAYDAY
Engine…………………………..Attempt Engine restart (in-flight procedure)

Question 29

ENGINE FIRE

Answer 29

Helicopter………………Establish autorotation
Throttle…………………………Close
Collective………………………Maintain 90% to 107% Nr
BLOWER A/C switch……OFF
FUEL VALVE switch….OFF
BAT switch……………………OFF
GEN switch…………………..OFF
Helicopter…………………….Complete autorotation landing

Question 30

CABIN FIRE

Answer 30

Helicopter………………Start descent
BLOWER A/C switch……OFF
Vents………………………………Open
Windows……………………….Open
Helicopter………….Land as soon as possible
DO an emergency shutdown

Question 31

ELECTRICAL FIRE

Answer 31

GEN switch…………………..OFF
BAT switch……………………OFF
If fire, smoke fumes persist:
Vents……………………………..Open
Windows……………………….Open
If fire goes out and smoke fumes clear:
Helicopter……………………..Land as soon as practical

Question 32

ENGINE HOT START

Answer 32

STARTER switch……………Engage and hold
Throttle…………………………..Close
FUEL VALVE switch………OFF
IGN ENG circuit breaker…..OUT
STARTER switch………………..Remains engaged until TOT is less than 200C for a minimum of 10 seconds
Shutdown……………………….Complete
BAT switch…………………….OFF
Ground power unit……….OFF
Record maximum TOT and duration

Question 33

EXTERIOR ENGINE FIRE

Answer 33

Throttle…………………………..Close
STARTER switch……………Release
FUEL VALVE switch………OFF
BAT switch…………………….OFF
Ground power unit……….OFF
Rotor brake…………………….Engage
Allow rotors to stop
Helicopter………………………Egress
Note
At pilot’s discretion, fight fire with the on-board fire extinguisher