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Cessna 208 > Phase One's > Flashcards

Phase One's Flashcards

1
Q

ENGINE FAILURE DURING TAKEOFF ROLL (AIRSPEED BELOW DECISION SPEED)

A
  1. Power Lever: BETA RANGE
  2. Brakes: APPLY
  3. Wing Flaps: RETRACT
    If airplane cannot be stopped on the remaining runway
  4. Fuel Condition Lever: CUTOFF
  5. Fuel Shutoff: OFF
  6. Fuel Tank Selectors: OFF (warning horn will sound)
  7. Battery Switch: OFF
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2
Q

ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF (AIRSPEED BELOW DECISION SPEED)

A
  1. Power Lever: IDLE
  2. Airspeed: 85-90 KIAS
  3. Wing Flaps: FULL DOWN
  4. Airspeed: 80 KIAS
  5. Touchdown: SLIGHTLY TAIL LOW
  6. Brakes: APPLY HEAVILY
  7. Wing Flaps: RETRACT
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3
Q

ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF (ALTITUDE <700ft AGL AND AIRSPEED ABOVE DECISION SPEED. NO TURN-BACK)

A
  1. Power Lever: IDLE
  2. Airspeed: 85-90 KIAS
  3. Emergency Power Lever: UNSTOW & GO
    (maintain 65% Ng minimum during flight)
  4. Airspeed: 85 KIAS
    If no response from the Emergency Power Lever, then re-stow and:
  5. Propeller Control Lever: FEATHER
  6. Wing Flaps: FULL DOWN
  7. Fuel Condition Lever: CUT OFF
  8. Fuel Shutoff: OFF (pull out)
  9. Fuel Tank Selectors: OFF (warning horn will sound)
  10. Battery Switch: OFF
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4
Q

ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF (ALTITUDE 700-1000ft AGL AND AIRSPEED ABOVE DECISION SPEED. TURN-BACK AVAILABLE)

A
  1. Airspeed: 95 KIAS
  2. Attitude: IMMEDIATELY PITCH 10* NOSE DOWN AND ROLL INTO A 45* LEFT OR RIGHT BANK TOWARD TURN-BACK HEADING
  3. Begin looking for runway or landing point
  4. Power Lever: IDLE
  5. Emergency Power Lever: UNSTOW & GO
    If no response from EPL, re-stow and:
  6. Propeller Control Lever: FEATHER
  7. Airspeed: 85 KIAS
  8. Attitude: REACHING TURN-BACK HEADING, ROLL WINGS LEVEL
  9. Begin looking for runway or landing point
  10. Wing Flaps: FULL DOWN / AS REQ
  11. Fuel Condition Lever: CUT OFF
  12. Fuel Shutoff: OFF (pull out)
  13. Fuel Tank Selectors: OFF (warning horn will sound)
  14. Battery Switch: OFF
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5
Q

ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF (ALTITUDE 1000-2000 ft AGL AND INSUFFICIENT RUNWAY REMAINING. TURN-BACK AVAILABLE)

A
  1. Airspeed: BEST GLIDE SPEED
  2. Attitude: LEFT OR RIGHT TURN
  3. Power Lever: IDLE
  4. Ignition Switch: ON
  5. Standby Vac Pump: ON
  6. Ng: CHECK
    If Ng below 50% proceed from #11, if above 50% then:
  7. Begin looking for runway or landing point
  8. Power Lever: AS REQUIRED
    If no response from Power Lever, then:
  9. Power Lever: IDLE
  10. Emergency Power Lever: UNSTOW & GO
    (maintain 65% Ng minimum during flight)
    If no response from the Emergency Power Lever, then re-stow and:
  11. Airspeed: 85 KIAS
  12. Propeller Control Lever: FEATHER
  13. Wing Flaps: FULL DOWN
  14. Fuel Condition Lever: CUT OFF
  15. Fuel Shutoff: OFF (pull out)
  16. Fuel Tank Selectors: OFF (warning horn will sound)
  17. Battery Switch: OFF
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6
Q

POWER LOSS / ENGINE FAILURE DURING FLIGHT

A
  1. Airspeed: MONITOR
  2. Power Lever: IDLE
  3. Ignition Switch: ON
  4. Standby Vac Pump: ON
  5. Ng: CHECK
    If Ng below 50% proceed from #10 below, if above 50% then:
  6. Power Lever: AS REQUIRED
  7. Attitude: LEFT OR RIGHT TURN
    (Immediately initiate a left or right descending turn back toward the runway or other suitable forced landing sight)
    If no response from Power Lever, then:
  8. Power Lever: IDLE
  9. Emergency Power Lever: UNSTOW & GO
    (Maintain 65% Ng minimum during flight)
    If no response from the Emergency Power Lever, then re-stow and:
  10. Airspeed: 85 KIAS
  11. Propeller Control Lever: FEATHER
  12. Fuel Condition Lever: CUT OFF
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7
Q

ENGINE FLAMEOUT OR FUEL CONTROL UNIT MALFUNCTION DURING FLIGHT

A 
(Gas Generator Speed “Ng” Above 50%)
1. Airspeed: MONITOR
2. Power Lever: IDLE
3. Ignition Switch: ON
4. Standby Vac Pump: ON
5. Power Lever: AS REQUIRED
(Satisfactory relight as evidenced by normal ITT and Ng)
If no response, then:
6. Power Lever: IDLE
7. Emergency Power Lever: UNSTOW &amp; GO
(Maintain 65% Ng minimum during flight)

(Gas Generator Speed “Ng” Below 50%)

  1. Propeller Control Lever: FEATHER
  2. Fuel Condition Lever: CUT OFF
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8
Q

FUEL CONTROL UNIT RUNAWAY DURING FLIGHT

Engine goes to un-commanded full power

A
  1. Power Lever: IDLE
  2. Wing Flaps: UP
  3. Ng: CHECK
  4. Fuel Flow Gauge: CHECK
    If safe Runway/Airfield or Alternate landing area exist:
  5. Airspeed: NOT BELOW 85 KIAS
  6. Fuel Condition Lever: CUT OFF
  7. Propeller Control Lever: FEATHER
    If no safe landing area exist:
  8. Gauges: RECHECK
  9. Propeller Control Lever: REDUCE RPM TO 1600
    (Carefully cycle RPM to Coarse (1600), NOT FEATHERED)
    If still no control of Fuel Control Unit:
  10. Emergency Power Lever: UNSTOW & CYCLE
    If no decrease in fuel flow from the Emergency Power Lever, then re-stow and:
  11. Power Lever: CYCLE (if no control of Fuel Control Unit)
  12. Airspeed: NOT BELOW 85 KIAS
  13. Fuel Condition Lever: CUT OFF
  14. Propeller Control Lever: FEATHER
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9
Q

ENGINE FIRE IMMEDIATELY AFTER TAKEOFF

ALTITUDE <500ft AGL, AIRSPEED ABOVE DECISION SPEED

A

If suitable landing area exists

  1. Airspeed: 85-90 KIAS
  2. Power Lever: IDLE
  3. Propeller Control Lever: FEATHER
  4. Fuel Condition Lever: CUT OFF
  5. Fuel Shutoff: OFF (pull out)
  6. Cabin Heat Firewall Shutoff Control: PULL OFF
  7. Wing Flaps: FULL DOWN
  8. Fuel Tank Selectors: OFF (warning horn will sound)
  9. Battery Switch: OFF

If terrain is not suitable for an immediate forced landing, a return for landing using engine power may be appropriate.
1. Airspeed: 85 KIAS
2. Power Lever: MINIMUM POWER (as required to maintain altitude, or climb to avoid obstacles)
3. Heading: TURN BACK TOWARD RUNWAY
When landing assured:
4. Power Lever: IDLE
5. Propeller Control Lever: FEATHER
6. Fuel Condition Lever: CUT OFF
7. Fuel Shutoff: OFF (pull out)
8. Cabin Heat Firewall Shutoff Control: OFF ( pull out)
9. Forward Side Vents: CLOSE
10. Wing Flaps: FULL DOWN
11. Fuel Tank Selectors: OFF (warning horn will sound)
12. Battery Switch: OFF

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10
Q

ENGINE FIRE IN-FLIGHT

ABOVE 2000ft AGL

A

FIRST ACTIONS: DON’T TOUCH ANYTHING.
Look for a second indication of fire in gauges or outside.
1. Gauges: CHECK
2. Power Lever: IDLE

If signs of fire DO exist, then:

  1. Propeller Control Lever: FEATHER
  2. Fuel Condition Lever: CUT OFF
  3. Fuel Shutoff: OFF (pull out)
  4. Cabin Heat Firewall Shutoff Control: OFF (pull out)
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11
Q

ELECTRICAL FIRE IN-FLIGHT

A
  1. Battery Switch: OFF
  2. Generator Switch: TRIP and RELEASE
  3. Standby Power Switch: OFF
    (Without electrical power, all electrically-operated gyros and engine instruments, fuel boost pump, annunciation lights, wing flaps and all avionics will be inoperative. Vacuum-driven gyros are the pilot’s horizon gyro and right-hand directional gyro)
  4. Vents: CLOSED
  5. Bleed Air Heat Switch: OFF
  6. Fire Extinguisher: ACTIVATE
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12
Q

CABIN FIRE - UNKNOWN SOURCE OF FIRE

A
  1. Battery Switch: OFF
  2. Generator Switch: TRIP and RELEASE
  3. Standby Power Switch: OFF
    (Without electrical power, all electrically-operated gyros and engine instruments, fuel boost pump, annunciation lights, wing flaps and all avionics will be inoperative. Vacuum-driven gyros are the pilot’s horizon gyro and right-hand directional gyro)
  4. Vents: CLOSED
  5. Bleed Air Heat Switch: OFF
  6. Fire Extinguisher: ACTIVATE
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13
Q

EFB / PERSONAL ELECTRONIC DEVICE (PED) SMOKE OR FIRE

A
  1. PED Power: OFF (IF POSSIBLE)
  2. Charger: DISCONNECT
  3. Secure Isolation Kit: RETRIEVE and OPEN
  4. Heat Resistant Gloves: PUT ON
  5. LIPO Bag: PLACE PED IN AND SEAL
    If the use of the secure isolation kit does not extinguish the fire:
  6. Consider dropping the PED out of the window: NON-POPULATED AREA and RELEASE
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14
Q

WING FIRE

A
  1. Pitot/Static Heat Switch: OFF
  2. Stall Heat Switch: OFF
  3. Strobe Light Switch: OFF
  4. Navigation Lights Switch: OFF
  5. Landing and Taxi Light Switches: OFF
  6. Radar: OFF
  7. Ventilation Fans: OFF
    Perform a sideslip as required to keep flames away from the fuel tank and cabin. Land the airplane
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15
Q

Cabin Fire During Ground Operations

A
  1. Power Lever: IDLE
  2. Brakes: AS REQUIRED
  3. Propeller Control Lever: FEATHER
  4. Fuel Condition Lever: CUT OFF
  5. Battery Switch: OFF
  6. Airplane: EVACUATE
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16
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
17
Q

INADVERTENT ICING ENCOUNTER

A
  1. Ignition Switch: ON
  2. Inertial Separator: BYPASS
  3. Pitot/Static, Stall, Windshield, Prop Anti-Ice: ON
  4. If above 20000 ft:
    a. Airspeed: 160 KIAS MAXIMUM
    b. Altitude: DESCEND
  5. Turn back or change altitude to obtain an outside air temperature that is less conducive to icing
18
Q

STATIC SOURCE BLOCKAGE

ERRONEOUS INSTRUMENT READING SUSPECTED

A
  1. Static Pressure Alternate Source Valve: PULL FULL ON
19
Q

FUEL CONTROL UNIT MALFUNCTION IN THE PNEUMATIC OR GOVERNOR SECTIONS
(ENGINE POWER FALLS BACK TO IDLE)

A
  1. Power Lever: IDLE
  2. Emergency Power Lever: UNSTOW & GO
    (Maintain 65% Ng minimum during flight)
20
Q

LOSS OF FUEL PRESSURE

AMBER FUEL PRESS LOW ANNUNCIATOR ON

A
  1. Fuel Boost Switch: ON
21
Q

FUEL FLOW INTERRUPTION TO FUEL RESERVOIR

RED RESERVOIR FUEL LOW ANNUNCIATOR ON

A
  1. Fuel Tank Selectors: LEFT ON, RIGHT ON
  2. Ignition Switch: ON
  3. Fuel Boost Switch: ON
22
Q

FUEL TANK SELECTOR OFF DURING ENGINE START

RED FUEL SELECT OFF ANNUNCIATOR ON AND BOTH FUEL SELECTOR WARNING HORNS ACTIVATED

A
  1. Left and Right Fuel Tank Selectors: ON
23
Q

FUEL LEVEL LOW WITH SINGLE TANK SELECTED

RED FUEL SELECT OFF AND AMBER LEFT OR RIGHT FUEL LOW ANNUNCIATORS ON AND FUEL SELECTOR WARNING HORN ACTIVATED

A
  1. Left and Right Fuel Tank Selectors: ON

Turning both fuel tank selectors ON will extinguish the red FUEL SELECT OFF annunciator and silence the warning horn

24
Q

ASYMMETRIC 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)
25
Q

STARTER CONTACTOR DOES NOT DISENGAGE AFTER ENGINE START

AMBER STARTER ENERGISED ANNUNCIATOR ON

A
  1. Battery Switch: OFF
  2. Auxiliary Power Unit: DISENGAGE
  3. Fuel Condition Lever: CUTOFF
26
Q

UPPER HALF OF CARGO DOOR OR UPPER HALF OF PASSENGER AIRSTAIR DOOR OPEN
(RED DOOR WARNING ANNUNCIATOR ON)

A
  1. Airspeed: MAINTAIN LESS THAN 100 KIAS
  2. Wing Flaps: FULL
    (Wing downwash with flaps extended will move the doors near their normally closed position)
  3. If available or practical, have a second crew member go aft to close and latch door.
  4. If landing is required with door open:
    a. Approach and Landing: NORMAL
27
Q

LOWER HALF OF PASSENGER AIRSTAIR DOOR OPEN

A
  1. Airspeed: MAINTAIN LESS THAN 100 KIAS
  2. Flight Controls: MANOEUVRE (for return landing)
  3. Wing Flaps: FULL
  4. Approach: NORMAL
  5. Landing: SLIGHTLY TAIL LOW (avoid nose high flare)
28
Q

RIGHT OR LEFT CREW DOORS OPEN

A
  1. Airspeed: MAINTAIN LESS THAN 125 KIAS

2. Door: PULL CLOSED AND LATCH

Cessna 208 (3 decks)

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