CESSNA BOLDFACE Flashcards
1
Q
ENGINE FAILURE DURING TAKEOFF
A
- POWER LEVER – BETA RANGE,
- BRAKES – APPLY
2
Q
ENGINE FAILURE IMMEDIATELY AFTER T/O
A
- AIRSPEED – 85 KIAS WITH 20 DEGREES OF FLAPS
3
Q
ENGINE FAILURE DURING FLIGHT
A
- AIRSPEED – 95 KIAS
- POWER LEVER – IDLE
- PROP – FEATHER
- FUEL CONDITION LEVER – CUTOFF
4
Q
ENGINE FLAMEOUT DURING FLIGHT
A
- IF NG IS ABOVE 50%:
A. POWER LEVER – IDLE
B. IGNITION – ON
- IF NG BELOW 50%:
A. FUEL CONDITION LEVER CUTOFF
5
Q
SMOKE AND FIRE
A
- POWER LEVER – IDLE
- PROP – FEATHER
- FUEL CONDITION LEVER – CUTOFF
- FUEL SHUTOFF – PULL OFF
- CABIN HEAT FIREWALL SHUTOFF CONTROL – PULL OFF
6
Q
ELECTRICAL FIRE IN FLIGHT
A
- BATTERY SWITCH – OFF
- GENERATOR SWITCH – TRIP
- STANDBY POWER SWITCH –OFF
- VENTS – CLOSED
- BLEED AIR HEAT SWITCH – OFF
- FIRE EXTINGUISHER – ACTIVE
7
Q
CABIN FIRE
A
- BATTERY SWITCH – OFF
- GENERATOR SWITCH – TRIP
- STANDBY POWER SWITCH – OFF
- VENTS – CLOSED
- BLEED AIR HEAT SWITCH – OFF
- FIRE EXTINGUISHER – ACTIVATE
8
Q
ENGINE FIRE IN FLIGHT
A
- POWER LEVER – IDLE
- PROPELLER CONTROL LEVER – FEATHER
- FUEL CONDITION LEVER – CUTOFF
- FUEL SHUTOFF – OFF
- CABIN HEAT FIREWALL SHUTOFF CONTROL – PULL OFF
9
Q
WING FIRE
A
- 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
10
Q
CABIN FIRE DURING GROUND OPERATIONS
A
- POWER LEVER – IDLE
- BRAKES – AS REQUIRED
- PROPELLER CONTROL LEVER – FEATHER
- FUEL CONDITION LEVER – CUTOFF
- BATTERY SWITCH – OFF
- AIRPLANE – EVACUATE
7.
11
Q
ENGINE FIRE DURING START ON GROUND (RED ENGINE FIRE ANNUNCIATOR ON OR OFF)
A
- FUEL CONDITION LEVER – CUTOFF
- FUEL BOOST SWITCH – OFF
- STARTER SWITCH – MOTOR
12
Q
INADVERTENT ICING ENCOUNTER
A
- 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
13
Q
STATIC SOURCE BLOCKAGE (ERRONEOUS INSTRUMENT READING SUSPECTED)
A
- STATIC PRESSURE ALTERNATE SOURCE VALVE – PULL FULL ON
14
Q
FUEL CONTROL UNIT MALFUNCTION IN THE PNEUMATICE OR GOVERNOR SECTIONS (ENGINE POWER FALL BACK TO IDLE
A
- POWER LEVER – IDLE
- EMERGENCY POWER LEVER – AS REQUIRED (MAINTAIN 65% Ng MINIMUM DURING FLIGHT
15
Q
LOSS OF FUEL PRESSURE (AMBER FUEL PRESS LOW ANNUNCIATOR ON)
A
- FUEL BOOST SWITCH – ON