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Luftfart 0122 > DA42 Memory items > Flashcards

DA42 Memory items Flashcards

1
Q

SUSPICION OF CARBON MONOXIDE IN THE CABIN

A
  1. Cabin heat & Defrost………………………………………………………………………………OFF
  2. Ventilation…………………………………………………………………………………………..open
  3. Emergency windows……………………………………………………………………………..open
  4. Forward canopy………………………………….unlatch, push up and lock in “cooling-gap” …………………………………………………………………………………………………………….position
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2
Q

ENGINE FIRE ON GROUND

A
  1. ENGINE MASTER…………………………………………………………………………….both OFF
  2. FUEL SELECTOR……………………………………………………………………………..both OFF
  3. ELECT. MASTER……………………………………………………………………………………..OFF
    - AFERT STANDSTILL –
  4. CANOPY……………………………………………………………………………………………..open
  5. AIRPLANE…………………………………………………………………… evacuate immediately
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3
Q

ENGINE FIRE DURING TAKE-OFF / IN FLIGHT

A
  1. Cabin heat & Defrost………………………………………………………………………………OFF
    Proceed according to 4-10 - ENGINE FAILURE DURING TAKE-OFF
    /Proceed according to 4-13 - ENGINE FAILURES IN FLIGHT and shut down the engine according to 4-5 - ENGINE SECURING (FEATHERING) PROCEDURE
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4
Q

ELECTRICAL FIRE ON GROUND

A
  1. ELECT. MASTER……………………………………………………………………………………..OFF
    - IF THE ENGINE IS RUNNING –
  2. POWER lever…………………………………………………………………………………both IDLE
  3. ENGINE MASTER……………………………………………………………………………. both OFF
  4. FUEL SELECTOR……………………………………………………………………………. both OFF
    - WHEN THE ENGINE HAS STOPPED / AFTER STANDSTILL –
  5. Canopy……………………………………………………………………………………………….open
  6. Airplane……………………………………………………………………… evacuate immediately
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5
Q

ELECTRICAL FIRE IN FLIGHT

A
  1. EMERGENCY SWITCH………………………………………………………………………………ON
  2. AVIONIC MASTER…………………………………………………………………………………..OFF
  3. ELECT. MASTER……………………………………………………………………………………..OFF
  4. Cabin heat & Defrost………………………………………………………………………………..OFF
  5. Emergency windows……………………………………………………………….open if required
  6. Land at the next suitable airfield
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6
Q

ABNORMAL ENGINE BEHAVIOUR

A
  1. FULL POWER………………………………………………………………………………………apply
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7
Q

ENGINE SECURING (FEATHERING) PROCEDURE

A
  1. Affected engine………………………………………………………………………. identify & verify
  2. ENGINE MASTER affected engine………………………………………………………………OFF
    CAUTION
    Do not shut down an engine with the FUEL SELECTOR valve. Otherwise the high pressure fuel pump can be damaged.
    Securing the feathered engine:
  3. Alternator affected engine……………………………………………………………………….OFF
  4. Fuel pump…………………………………………………………………………………….check OFF
  5. FUEL SELECTOR affected engine………………………………………………………………..OFF
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8
Q

ENGINE FAILURE DURING TAKE-OFF (Ground Roll)

A

a) Engine Failure During Ground Roll
1. POWER lever…………………………………………………………………………….. IDLE / BOTH
2. Rudder…………………………………………………………………..maintain directional control
3. Brakes…………………………………………………………………………………………as required
CAUTION
If sufficient time is remaining, the risk of fire in the event of a collision with obstacles can be reduced as follows:
4. ENGINE MASTER …………………………………………………………………………….both OFF
5. FUEL SELECTOR……………………………………………………………………………..both OFF
6. ELECT. MASTER……………………………………………………………………………………..OFF

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9
Q

ENGINE FAILURE DURING TAKE-OFF (After liftoff)

A
  1. POWER lever………………………………………………………………………………………..MAX
  2. Rudder…………………………………………………………………maintain directional control
  3. Airspeed……………………………………………………………….VYSE = 85 KIAS / as required
  4. Landing gear……………………………………………………………UP to achieve positive ROC
  5. FLAPS……………………………………………………………………………………………check UP
  6. Inoperative engine…………………………………………..secure according to 4-5 - ENGINE …………………………………………………………………SECURING (FEATHERING) PROCEDURE
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10
Q

ENGINE FAILURES IN FLIGHT (Initial Climb)

A
  1. Rudder…………………………………………………………………maintain directional control
  2. Airspeed………………………………………………………………………………VYSE = 85 KIAS / …………………………………………………………………………..above VMCA = 71 KIAS (flaps UP) …………………………………………………………..….. or VMCA = 68 KIAS (flap APP) as required
  3. Operative engine…………………………………………………..increase power as required if ……………………………………………….………………Directional control has been Established
  4. Inoperative engine………………………………………………………………Secure according to ……………………………………………..4-5 - ENGINE SECURING (FEATHERING) PROCEDURE
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11
Q

ENGINE FAILURES IN FLIGHT (During flight)

A
  1. Rudder…………………………………………………………………..maintain directional control
  2. Airspeed…………………………………………………………………………………….as required …………………………………………………………………………..above VMCA = 71 KIAS (flaps UP) ………………………………………………………………………………..or VMCA = 68 KIAS (flap APP)
  3. Operative engine…………………………………………………….increase power to 92% load
    Establish minimum / zero sideslip condition. (approx. half ball towards good engine; 3-5 bank).
    If icing conditions exists:
  4. Leave the icing area (by changing altitude or turning back, or even continuing the same course if clear air is known to be immediately ahead).
  5. DE-ICE………………………………………………………………………………………………HIGH
    Then:
  6. Inoperative engine…………………………………………………………….Secure according to ………………………….………………….4-5 - ENGINE SECURING (FEATHERING) PROCEDURE
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12
Q

Propeller overspeed

A
  1. POWER setting…………………………………………………………………..reduce as required
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13
Q

COMPLETE FAILURE OF THE ELECTRICAL SYSTEM

A
  1. Leave the icing area (by changing altitude or turning back, or even continuing the same course if clear air is known to be immediately ahead).
  2. Circuit breakers……………………………………………………….check if all OK (pressed in)
    If there is still no electrical power available:
  3. EMERGENCY SWITCH………………………………………………………………………………ON
  4. Flood light, if necessary……………………………………………………………………………ON
  5. POWER…………………………………………set based on lever positions and engine noise
  6. Prepare landing with flaps in the given position.
  7. Land on the nearest suitable airfield
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14
Q

STARTER MALFUNCTION

A
  1. POWER lever affected engine…………………………………………………………………… IDLE
  2. ENGINE MASTER affected engine………………………………………………………………OFF
  3. ELECT. MASTER……………………………………………………………………………………..OFF
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15
Q

AUTOPILOT OR ELECTRIC TRIM MALFUNCTION/FAILURE

A
  1. Airplane control stick……………………………….grasp firmly and regain Airplane control
  2. AP DISC switch………………………………………………………………..DEPRESS AND HOLD
  3. Trim………………………………………………………….retrim airplane manually as required
  4. AUTOPILOT circuit breaker………………………………………………………………………..pull
  5. AP DISC switch………………………………………………………………………………..RELEASE
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16
Q

AUTOPILOT OVERSPEED RECOVERY (yellow MAXSPD on PFD)

A
  1. POWER lever……………………………………………………………………………reduce power
17
Q

AUTOPILOT OUT OF TRIM

A
  1. AP DISC switch……………………………………………………………….DEPRESS AND HOLD …………………………………………………………………………While grasping control stick firmly
  2. Airplane attitude……………………………………………..maintain / regain airplane control ……………………………………………………………..use standby attitude indicator if necessary
  3. Pitch trim……………………………………………….retrim if necessary, using the trim wheel
  4. AUTOPILOT circuitbreaker………………………………………………………………………PULL
  5. AP DISC switch………………………………………………………………………………..RELEASE
18
Q

FUEL SUPPLY FAILURE

A
  1. FUEL SELECTOR………………………………………………….CROSSFEED / affected engine
19
Q

GO-AROUND / BALKED LANDING WITH ONE ENGINE INOP.

A
  1. POWER lever………………………………………………………………………………………….MAX
  2. Rudder…………………………………………………………………..maintain directional control
  3. Airspeed……………………………………………………………….VYSE = 85 KIAS / as required
  4. Landing gear…………………………………………………………………………………UP / retract
  5. FLAPS……………………………………………………………………………………………………UP
    If a positive rate of climb cannot be established:
    - Land so as to keep clear of obstacles.
    If time allows the following steps can reduce the risk of fire in an even of collision with obstacles after touchdown:
  6. ENGINE MASTER……………………………………………………………………………. both OFF
  7. FUEL SELECTOR……………………………………………………………………………..both OFF
  8. FLAPS…………………………………………………………………………APP or LDG, as required
  9. Approach Speed:
    Up to 1900 kg…………………………………………………………………..min. 84 KIAS flaps APP ………………………………………………………………………………………..min. 84 KIAS flaps LDG …………………………………………………………………………………………………….88 KIAS if ICE*
    Above 1900 kg………………………………………………………………….min. 88 KIAS flaps APP ………………………………………………………………………………………..min. 86 KIAS flaps LDG ……………………………..…………………………………………………………………….90KIAS if ICE*
    If landing with landing gear extended:
  10. LANDING GEAR……………………………………………………………DOWN, check 3 green
  11. ELECT. MASTER……………………………………………………………………………………OFF
  12. Touch down………………………………………………………………..lowest practical speed
    If landing with landing gear retracted:
  13. LANDING GEAR…………………………………………………………………………………….UP
  14. Touch down…………………………………………………………………lowest practical speed
    Immediately after touch down:
  15. ELECT. MASTER……………………………………………………………………………………OFF
20
Q

UNINTENTIONAL FLIGHT INTO ICING

A
  1. Leave the icing area (by changing altitude or turning back, on order to reach zones with a higher ambient temperature)
  2. PITOT HEAT…………………………………………………………………………………………….ON
  3. Cabin heat & Defrost……………………………………………………………………………….ON
  4. POWER lever……………………………increase power, in order to prevent ice build up on …………………………………………….the propeller blades, apply power changes periodically
  5. ALTERNATE AIR……………………………………………………………………………………OPEN
  6. Emergency windows…………………………………………………………………open if required
    CAUTION
    Ice build-up increases the stalling speed.
  7. ATC……………………………………………………………..advice if an emergency is expected
21
Q

FAILURE OF THE ICE PROTECTION SYSTEM

A
  1. Leave the icing area (by changing altitude or turning back, or even continuing on the same course if clear air is known to be immediately ahead.)
  2. Airspeed……………………………………………………………maintain 118 to 156 KIAS until ……………………………………………………………………………………final approach and landing
22
Q

SPIN RECOVERY

A
  1. POWER lever…………………………………………………………………………………………IDLE
  2. Rudder…………………………………………………..full deflection against direction of spin
  3. Elevator (control stick)…………………………………………………………………fully forward
  4. Ailerons……………………………………………………………………………………………neutral
  5. FLAPS…………………………………………………………………………………………………….UP
    When rotation has stopped:
  6. Rudder…………………………………………………………………………………………….neutral
  7. Elevator (control stick)…………………………………………………………………pull carefully
  8. Return the airplane from a decending into a normal flight attitude. Do not exceed the “never exceed speed”, VNE = 188 KIAS
23
Q

EMERGENCY DESCENT

A
  1. FLAPS……………………………………………………………………………………………………UP
  2. Gear…………………………………………………………………………………………………DOWN
  3. POWER lever………………………………………………………………………………………..IDLE
  4. Airspeed…………………………………………………………………………………….as required
24
Q

WINDSHEAR ENCOUNTER

A
  1. AP DISC SWITCH …………………………………………………………………….press and hold
  2. Perform established windshear escape procedures
    After Exiting Windshear:
  3. AP DISC SWITCH………………………………………………………………………………..release
  4. Autopilot / Yaw Damper…………………………………………………………………..if required
25
Q

UNLOCKED DOORS

A
  1. Airspeed…………………………………………………………………………reduce immediately

a) Canopy Unlocked
5. Airspeed……………………………………………………………………………….below 140 KIAS

c) Rear Passenger Door Unlocked
5. Airspeed……………………………………………………………………………….below 140 KIAS

d) Front Baggage Door Open
5. Airspeed…………………………………………..reduce, so that door is in a stable position

26
Q

ENGINES OUT LANDING

A
  1. ENGINE MASTER………………………………………………………………………………both OFF
  2. Alternator switches…………………………………………………………………………..both OFF
  3. Fuel pumps…………………………………………………………………………………….both OFF
  4. FUEL SELECTOR……………………………………………………………………………..both OFF
  5. AVIONIC MASTER…………………………………………………………………………………..OFF
  6. Safety harnesses…………………………………………………check fastened and tightened
    When sure of making landing area:
  7. FLAPS………………………………………………………………………..APP or LDG, as required
  8. Approach Speed:
    Up to 1900 kg……………………………………………………………………min. 84 KIAS flaps APP ………………………………………………………………………………………..min. 84 KIAS flaps LDG
    Above 1900 kg…………………………………………………………………..min. 88 KIAS flaps APP ………………………………………………………………………………………..min. 86 KIAS flaps LDG
    If landing with landing gear extended:
  9. LANDING GEAR…………………………………………………………….DOWN, check 3 green
  10. POWER lever…………………………………………………………………………………both IDLE
  11. ELECT. MASTER……………………………………………………………………………………OFF
  12. Touch down………………………………………………………………..lowest practical speed
    If landing with landing gear retracted:
  13. LANDING GEAR………………………………………………………………………………………UP
  14. POWER lever…………………………………………………………………………………both IDLE
  15. Touch down………………………………………………………………..lowest practical speed
    Immediately after touch down:
  16. ELECT. MASTER……………………………………………………………………………………OFF
27
Q

USP ACTIVE, Underspeed Protection is active

A
  1. Power levers…………………………….increase power as required to correct underspeed
28
Q

MINSPD, AFCS entered Minimum Airspeed Mode

A
  1. Power levers…………………………….increase power as required to correct underspeed
29
Q

High RPM

A
  1. Reduce power of affected engine

Luftfart 0122 (2 decks)

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