CESSNA BOLDFACE Flashcards

1
Q

ENGINE FAILURE DURING TAKEOFF

A
  1. POWER LEVER – BETA RANGE,
  2. BRAKES – APPLY
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2
Q

ENGINE FAILURE IMMEDIATELY AFTER T/O

A
  1. AIRSPEED – 85 KIAS WITH 20 DEGREES OF FLAPS
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3
Q

ENGINE FAILURE DURING FLIGHT

A
  1. AIRSPEED – 95 KIAS
  2. POWER LEVER – IDLE
  3. PROP – FEATHER
  4. FUEL CONDITION LEVER – CUTOFF
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4
Q

ENGINE FLAMEOUT DURING FLIGHT

A
  1. IF NG IS ABOVE 50%:

A. POWER LEVER – IDLE

B. IGNITION – ON

  1. IF NG BELOW 50%:

A. FUEL CONDITION LEVER CUTOFF

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5
Q

SMOKE AND FIRE

A
  1. POWER LEVER – IDLE
  2. PROP – FEATHER
  3. FUEL CONDITION LEVER – CUTOFF
  4. FUEL SHUTOFF – PULL OFF
  5. CABIN HEAT FIREWALL SHUTOFF CONTROL – PULL OFF
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6
Q

ELECTRICAL FIRE IN FLIGHT

A
  1. BATTERY SWITCH – OFF
  2. GENERATOR SWITCH – TRIP
  3. STANDBY POWER SWITCH –OFF
  4. VENTS – CLOSED
  5. BLEED AIR HEAT SWITCH – OFF
  6. FIRE EXTINGUISHER – ACTIVE
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7
Q

CABIN FIRE

A
  1. BATTERY SWITCH – OFF
  2. GENERATOR SWITCH – TRIP
  3. STANDBY POWER SWITCH – OFF
  4. VENTS – CLOSED
  5. BLEED AIR HEAT SWITCH – OFF
  6. FIRE EXTINGUISHER – ACTIVATE
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8
Q

ENGINE FIRE IN FLIGHT

A
  1. POWER LEVER – IDLE
  2. PROPELLER CONTROL LEVER – FEATHER
  3. FUEL CONDITION LEVER – CUTOFF
  4. FUEL SHUTOFF – OFF
  5. CABIN HEAT FIREWALL SHUTOFF CONTROL – PULL OFF
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9
Q

WING FIRE

A
  1. PITOT/STATIC HEAT SWITCH – OFF
  2. STALL HEAT SWITCH – OFF
  3. STROBE LIGHTS SWITCH – OFF
  4. NAVIGATION LIGHTS SWITCH – OFF
  5. LANDING AND TAXI LIGHT SWITCHES – OFF
  6. RADAR – OFF
  7. VENTILATION FANS (IF INSTALLED) – OFF
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10
Q

CABIN FIRE DURING GROUND OPERATIONS

A
  1. POWER LEVER – IDLE
  2. BRAKES – AS REQUIRED
  3. PROPELLER CONTROL LEVER – FEATHER
  4. FUEL CONDITION LEVER – CUTOFF
  5. BATTERY SWITCH – OFF
  6. AIRPLANE – EVACUATE
    7.
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11
Q

ENGINE FIRE DURING START ON GROUND (RED ENGINE FIRE ANNUNCIATOR ON OR OFF)

A
  1. FUEL CONDITION LEVER – CUTOFF
  2. FUEL BOOST SWITCH – OFF
  3. STARTER SWITCH – MOTOR
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12
Q

INADVERTENT ICING ENCOUNTER

A
  1. IGNITION SWITCH – ON
  2. INERTIAL SEPARATOR – BYPASS
  3. PITOT/STATIC HEAT SWITCH – ON
  4. STALL WARNING HEAT SWITCH – ON
  5. WINDHIELD ANTI-ICE SWITCH (ES) – AUTO
  6. PROPELLER ANTI-ICE SWITCH (IF INSTALLED) – AUTO SWITCHES ON (IF INSTALLED)
  7. IF ABOVE 20,000
    • AIRSPEED –160KIAS OR BELOW
    • ALTITUDE – DESCEND TO 20,000 FEET OR BELOW AS SOON AS PRACTCAL

BACK OR CHANGE ALTITUDE

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13
Q

STATIC SOURCE BLOCKAGE (ERRONEOUS INSTRUMENT READING SUSPECTED)

A
  1. STATIC PRESSURE ALTERNATE SOURCE VALVE – PULL FULL ON
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14
Q

FUEL CONTROL UNIT MALFUNCTION IN THE PNEUMATICE OR GOVERNOR SECTIONS (ENGINE POWER FALL BACK TO IDLE

A
  1. POWER LEVER – IDLE
  2. EMERGENCY POWER LEVER – AS REQUIRED (MAINTAIN 65% Ng MINIMUM DURING FLIGHT
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15
Q

LOSS OF FUEL PRESSURE (AMBER FUEL PRESS LOW ANNUNCIATOR ON)

A
  1. FUEL BOOST SWITCH – ON
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16
Q

FUEL FLOW INTERRUPTION TO FUEL RESERVOIR (RED RESERVOIR FUEL LOW ANNUNCIATOR ON)

A
  1. FUEL TANK SELECTORS – LEFT ON, RIGHT ON
  2. IGNITION SWITCHES – ON
  3. FUEL BOOST SWITCH ON
17
Q

FUEL TANK SELECTOR OFF DURING ENGINE START (RED FUEL SELECTOR OFF ANNUNCIATOR ON BOTH FUE SELECTOR WARNING HORNES ACTIVATED)

A
  1. LEFT AND RIGHT FUEL TANK SELECTORS – ON
18
Q

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

A
  1. LEFT AND RIGHT FUEL TANK SELECTORS – ON
19
Q

ASSYMETRIC FLAP EXTENSION OR SUDDEN FLAP RETRACTION ON ONE SIDE

A
  1. APPLY AILERON AND RUDDER TO STOP THE ROLL
  2. FLAP SELECTOR – UP
  3. AIRSPEED – SLOW TO 100 KIAS OR LESS
20
Q

BATTERY TEMPERATURE HIGH (AMBER BATTERY HOT ANNUNCIATOR ON) (NI-CAD BATTERY EQUIPPED AIRPLANES ONLY

A
  1. BATTERY SWITCH – OFF
21
Q

BATTERY OVERHEATED (RED BATTERY OVERHEAT ANNUNCIATOR ON) (NI-CAD BATTERY EQUIPPED AIRPLANES ONLY)

A
  1. BATTERY SWITCH – CHECK OFF
22
Q

STARTER CONTACTOR DOES NOT DISENGAGE AFTER ENGINE START (AMBER STARTER ENERGIZED ANNUNCIATOR ON)

A
  1. BATTERY SWITCH – OFF
  2. AUILLIARY POWER UNIT – OFF, THEN DISENGAGE
  3. FUEL CONDITION LEVER – CUTOFF
23
Q
A