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Skytrans DHC8 - 102 QRH Memory Items
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RAPID DEPRESSURISATION/EMERGENCY DESCENT
OXYGEN MASK - ON 100%
MIC SWITCH - MASK
PASSENGER SIGNS - ON
EMERGENCY DESCENT - ACCOMPLISH AS REQ'D
POWER LEVERS - FLT IDLE
CONDITION LEVERS - MAX
AIRSPEED - VMO
ON GROUND NON NORMAL
EMERG BRAKE - SET
ENGINE FIRE:
ENGINE FIRE (ON GROUND) - ACCOMPLISH
ENGINE FAILURE:
POWER LEVERS - FLT IDLE
AFFECTED ENGINE
:
CONDITION LEVER - FUEL OFF
PULL FUEL OFF HANDLE - PULL
TANK AUX PUMP - OFF
OTHER FAILURE:
APPROPRIATE ABNORMAL/EMERGENCY PROCEDURE(S) - ACCOMPLISH
ENGINE FIRE (ON GROUND)
EMERG BRAKE - SET
POWER LEVERS - FLT IDLE
CONDITION LEVERS - FUEL OFF
PULL FUEL OFF HANDLE (affected engine) - PULL
TANK AUX PUMPS #1 & #2 - OFF
EXTG SWITCH - FWD BTL
Wait up to 30 sec, if fire persists
EXTG SWITCH - AFT BTL
EVACUATION - ACCOMPLISH
EVACUATION
EMERG BRAKE - SET
POWER LEVERS - FLT IDLE
CONDITION LEVERS - FUEL OFF
PULL FUEL OFF HANDLES - PULL
EMERGENCY LIGHTS - ON
FASTEN SEAT BELTS LIGHTS - OFF
EVACUATION - INITIATE
AC/DC EXT PWR & APU - OFF
BATTERY MASTER - OFF
ABORTED ENGINE START
(Failure to Light up within 10 sec OR Imminent Overtemp OR Hung start)
CONDITION LEVER - FUEL OFF
PULL FUEL OFF HANDLE - PULL
IGNITION (affected engine) - OFF
Motor engine for 15 sec:
START SELECT - OFF
APU FIRE
(Sunstrand)
CONFIRM APU AUTOMATIC SHUTDOWN
(APU RUN ADVISORY LIGHTS OUT & APU BTL DISCHARGES)
IF APU BTL OR APU FIRE ADVISORY LIGHT REMAINS ILLUMINATED:
EXTG SWITCH - EXTG
APU FIRE
(Pats)
APU FIRE ADVISORY LIGHT ILLUMINATES INDICATING APU FIRE
:
BLEED AIR SWITCH - OFF
GEN SWITCH - OFF
STOP SWITCH - PRESS
IF APU HAS NOT SHUTDOWN AUTOMATICALLY
:
APU MASTER SWITCH - OFF
FIRE EXTG SWITCH (under cover) - EXTG
IF APU FIRE ADVISORY LIGHT CONTINUES TO ILLUMINATE, FOLLOW THE EMERGENCY PROCEDURES AS OUTLINED IN "ON GROUND NON-NORMALS"
OIL PRESSURE BELOW 40 PSI or #1 OR #2 ENG OIL PRESS (WARNING LIGHT)
AFFECTED ENGINE:
"ENGINE FAIL/FIRE/SHUTDOWN'' - ACCOMPLISH
PROPELLER OVERSPEED
Above 400 ft AGL [acceleration altitude]
:
SYNCHROPHASE - OFF
AIRSPEED - REDUCED
AFFECTED ENGINE:
POWER LEVER - FLT IDLE
CONDITION LEVER - START/FEATHER
ALTERNATE FEATHER (IF REQ'D) - FEATHER
IF PROPELLER FEATHERS
:
CONDUCT ENGINE SHUTDOWN DRILL
-END-
IF PROPELLER DOESN'T FEATHER
:
DON'T SHUTDOWN ENGINE
(
AFFECTED ENGINE
):
ALTERNATE FEATHER - NORM
CONDITION LEVER - MAX
POWER LEVER - ADVANCE (DO NOT EXCEED 1212RPM)
(
UNAFFECTED ENGINE
):
POWER LEVER - Power as required to maintain flight profile
- LAND IMMEDIATELY AT NEAREST SUITABLE AIRPORT
UNSCHEDULED PROPELLER FEATHERING
(May be indicated by high torque)
Above 400 ft AGL [acceleration altitude]:
AFFECTED ENGINE
:
POWER LEVER - FLT IDLE
"ENGINE FAIL/FIRE/SHUTDOWN'' - ACCOMPLISH
PROPELLER GROUND RANGE LIGHT CYCLING
POWER LEVERS - ADVANCE ABOVE FLT IDLE
ENGINE FAIL/FIRE/ENGINE SHUTDOWN
(IN FLIGHT)
AFFECTED ENGINE
:
POWER LEVER - FLT IDLE
CONDITION LEVER - FUEL OFF
ALTERNATE FEATHER (if required) - FEATHER
PULL FUEL OFF HANDLE - PULL
TANK AUX PUMP - OFF
IF FIRE
:
FIRE EXTINGUISHER (affected engine) - FWD BTL
IF FIRE PERSISTS AFTER 30 SEC
:
FIRE EXTINGUISHER - AFT BTL
SMOKE WARNING LIGHT OR FUSELAGE FIRE, FUMES OR SMOKE
OXYGEN MASKS - ON/100%
SMOKE GOGGLES (if applicable) - ON
MIC SWITCH - MASK
RECIRC FAN - OFF
AILERON TRIM TAB RUNAWAY
AIRSPEED - REDUCE
AILERON TRIM - OPPOSITE TO RUNAWAY
ROLL CONTROL MALFUNCTION A
(Continuous Illumination of SPLR Switchlights)
(Airplane Rolls with No Control Input)
ROLL CONTROL - APPLY TO HOLD WINGS LEVEL
IF SPLR 1 OR SPLR 2 PUSH OFF SWITCHLIGHTS ILLUMINATE CONTINUOUSLY IN WINGS LEVEL FLIGHT:
ILLUMINATED PUSH OFF SWITCHLIGHTS - PUSH OFF
ROLL CONTROL MALFUNCTION B
(Illumination of SPLR Switchlights Not Continuous)
IF SPLR 1 OR SPLR 2 PUSH OFF SWITCHLIGHTS DO NOT ILLUMINATE CONTINUOUSLY IN WINGS LEVEL FLIGHT:
POWER - APPLY
AIRSPEED - INCREASE
ROLL CONTROL JAM
AUTOPILOT - DISCONNECT
ROLL DISCONNECT HANDEL - PULL & ROTATE 90°
CONTROL WHEEL - BOTH PILOTS ATTEMPT ROLL CONTROL
- The pilot with the free control wheel will fly the aircraft
GROUND SPOILER MALFUNCTION IN FLIGHT
(Illumination of Ground Spoiler Advisory Light)
ROLL CONTROL - HOLD WINGS LEVEL
POWER - APPLY AS REQ'D
AIRSPEED - INCREASE
PITCH CONTROL JAM
AUTOPILOT - DISCONNECT
FLAP & AIRSPEED - MAINTAIN AT TIME OF JAM
CONTROL COLUMNS - BOTH PILOTS ATTEMPT TO OVERCOME JAM
IF UNABLE TO OVERCOME JAM:
RELAX CONTROL COLUMN FORCE
PITCH DISCONNECT HANDLE - PULL & TURN 90°
CONTROL COLUMN - BOTH PILOTS ATTEMPT PITCH CONTROL
- The pilot with the free control column will fly the aircraft
ELEVATOR CONTROL MALFUNCTION
(Loss of elevator and manual trim control)
STBY ELEVATOR TRIM - ARM
NOSE DOWN/NOSE UP - AS REQ'D
RUDDER CONTROL JAM
WARNING
: Should the rudder pedal (rudder jam) suddenly break free, do NOT apply rudder pedal input in the opposite direction.
AFFECTED RUDDER PEDAL - APPLY NORMAL PUSH FORCE
RUDDER PEDAL MOVES AS REQUIRED
:
AFFECTED RUDDER PEDAL - REDUCE PUSH FORCE AND ALLOW RUDDER TO CENTRE
-
END
-
RUDDER PEDAL DOES NOT RESPOND TO NORMAL PUSH FORCE
:
(
Rudder remains jammed or rudder jam reoccurs
)
- USE ROLL CONTROL AS REQUIRED FOR DIRECTIONAL CONTROL
AIRSPEED - MINIMUM 1.3V(min)
Author
thegov
ID
332956
Card Set
Skytrans DHC8 - 102 QRH Memory Items
Description
DASH 8 100 QRH Memory Items as at 05/May/2017
Updated
2017-07-18T08:29:37Z
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