ENGINE FAILURE DURING TAKEOFF
- POWER LEVER – BETA RANGE,
- BRAKES – APPLY
ENGINE FAILURE IMMEDIATELY AFTER T/O
- AIRSPEED – 85 KIAS WITH 20 DEGREES OF FLAPS
ENGINE FAILURE DURING FLIGHT
- AIRSPEED – 95 KIAS
- POWER LEVER – IDLE
- PROP – FEATHER
- FUEL CONDITION LEVER – CUTOFF
ENGINE FLAMEOUT DURING FLIGHT
- IF NG IS ABOVE 50%:
A. POWER LEVER – IDLE
B. IGNITION – ON
- IF NG BELOW 50%:
A. FUEL CONDITION LEVER CUTOFF
SMOKE AND FIRE
- POWER LEVER – IDLE
- PROP – FEATHER
- FUEL CONDITION LEVER – CUTOFF
- FUEL SHUTOFF – PULL OFF
- CABIN HEAT FIREWALL SHUTOFF CONTROL – PULL OFF
ELECTRICAL FIRE IN FLIGHT
- BATTERY SWITCH – OFF
- GENERATOR SWITCH – TRIP
- STANDBY POWER SWITCH –OFF
- VENTS – CLOSED
- BLEED AIR HEAT SWITCH – OFF
- FIRE EXTINGUISHER – ACTIVE
CABIN FIRE
- BATTERY SWITCH – OFF
- GENERATOR SWITCH – TRIP
- STANDBY POWER SWITCH – OFF
- VENTS – CLOSED
- BLEED AIR HEAT SWITCH – OFF
- FIRE EXTINGUISHER – ACTIVATE
ENGINE FIRE IN FLIGHT
- POWER LEVER – IDLE
- PROPELLER CONTROL LEVER – FEATHER
- FUEL CONDITION LEVER – CUTOFF
- FUEL SHUTOFF – OFF
- CABIN HEAT FIREWALL SHUTOFF CONTROL – PULL OFF
WING FIRE
- PITOT/STATIC HEAT SWITCH – OFF
- STALL HEAT SWITCH – OFF
- STROBE LIGHTS SWITCH – OFF
- NAVIGATION LIGHTS SWITCH – OFF
- LANDING AND TAXI LIGHT SWITCHES – OFF
- RADAR – OFF
- VENTILATION FANS (IF INSTALLED) – OFF
CABIN FIRE DURING GROUND OPERATIONS
- POWER LEVER – IDLE
- BRAKES – AS REQUIRED
- PROPELLER CONTROL LEVER – FEATHER
- FUEL CONDITION LEVER – CUTOFF
- BATTERY SWITCH – OFF
- AIRPLANE – EVACUATE
7.
ENGINE FIRE DURING START ON GROUND (RED ENGINE FIRE ANNUNCIATOR ON OR OFF)
- FUEL CONDITION LEVER – CUTOFF
- FUEL BOOST SWITCH – OFF
- STARTER SWITCH – MOTOR
INADVERTENT ICING ENCOUNTER
- IGNITION SWITCH – ON
- INERTIAL SEPARATOR – BYPASS
- PITOT/STATIC HEAT SWITCH – ON
- STALL WARNING HEAT SWITCH – ON
- WINDHIELD ANTI-ICE SWITCH (ES) – AUTO
- PROPELLER ANTI-ICE SWITCH (IF INSTALLED) – AUTO SWITCHES ON (IF INSTALLED)
- IF ABOVE 20,000
- AIRSPEED –160KIAS OR BELOW
- ALTITUDE – DESCEND TO 20,000 FEET OR BELOW AS SOON AS PRACTCAL
BACK OR CHANGE ALTITUDE
STATIC SOURCE BLOCKAGE (ERRONEOUS INSTRUMENT READING SUSPECTED)
- STATIC PRESSURE ALTERNATE SOURCE VALVE – PULL FULL ON
FUEL CONTROL UNIT MALFUNCTION IN THE PNEUMATICE OR GOVERNOR SECTIONS (ENGINE POWER FALL BACK TO IDLE
- POWER LEVER – IDLE
- EMERGENCY POWER LEVER – AS REQUIRED (MAINTAIN 65% Ng MINIMUM DURING FLIGHT
LOSS OF FUEL PRESSURE (AMBER FUEL PRESS LOW ANNUNCIATOR ON)
- FUEL BOOST SWITCH – ON
FUEL FLOW INTERRUPTION TO FUEL RESERVOIR (RED RESERVOIR FUEL LOW ANNUNCIATOR ON)
- FUEL TANK SELECTORS – LEFT ON, RIGHT ON
- IGNITION SWITCHES – ON
- FUEL BOOST SWITCH ON
FUEL TANK SELECTOR OFF DURING ENGINE START (RED FUEL SELECTOR OFF ANNUNCIATOR ON BOTH FUE SELECTOR WARNING HORNES ACTIVATED)
- LEFT AND RIGHT FUEL TANK SELECTORS – ON
FUEL LEVEL LOW WITH SINGLE TANK SELECTED (RED FUEL SELECT OFF AND AMBER LEFT OR RIGHT FUEL LOW ANNUNCIATORS ON THE FUEL SELECTOR (WARNING HORN ACTIVATED
- LEFT AND RIGHT FUEL TANK SELECTORS – ON
ASSYMETRIC FLAP EXTENSION OR SUDDEN FLAP RETRACTION ON ONE SIDE
- APPLY AILERON AND RUDDER TO STOP THE ROLL
- FLAP SELECTOR – UP
- AIRSPEED – SLOW TO 100 KIAS OR LESS
BATTERY TEMPERATURE HIGH (AMBER BATTERY HOT ANNUNCIATOR ON) (NI-CAD BATTERY EQUIPPED AIRPLANES ONLY
- BATTERY SWITCH – OFF
BATTERY OVERHEATED (RED BATTERY OVERHEAT ANNUNCIATOR ON) (NI-CAD BATTERY EQUIPPED AIRPLANES ONLY)
- BATTERY SWITCH – CHECK OFF
STARTER CONTACTOR DOES NOT DISENGAGE AFTER ENGINE START (AMBER STARTER ENERGIZED ANNUNCIATOR ON)
- BATTERY SWITCH – OFF
- AUILLIARY POWER UNIT – OFF, THEN DISENGAGE
- FUEL CONDITION LEVER – CUTOFF
