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ATPL > KA200 Memory Items > Flashcards

KA200 Memory Items Flashcards

1
Q

ENGINE FIRE OR FAILURE IN FLIGHT (ENG FIRE light*)

A

Affected Engine:
1. Condition Lever ………………………………………… FUEL CUTOFF
2. Prop Lever ……………………………………………………….. FEATHER
3. Firewall Shutoff Valve ………………………………………….. CLOSE
If fire warning persists:
4. Fire Extinguisher ……………………………………………… ACTUATE

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2
Q

ENGINE FIRE ON GROUND (ENG FIRE light*)

A

Affected Engine:
1. Condition Lever ………………………………………… FUEL CUTOFF
2. Firewall Shutoff Valve …………………………………………… CLOSE
3. Ignition and Engine Start ………………………… STARTER ONLY
4. Fire Extinguisher (if fire warning persists) …………. ACTUATE

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3
Q

EMERGENCY ENGINE SHUTDOWN ON THE GROUND

A
  1. Condition Levers ……………………………………….. FUEL CUTOFF
  2. Prop Levers …………………………………………………….. FEATHER
  3. Firewall Shutoff Valves ………………………………………… CLOSE
  4. Master Switch (gang bar) …………………………………………… OFF
  5. ESIS Power ………………………………………………………………. OFF
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4
Q

ENGINE FAILURE DURING TAKEOFF (AT OR BELOW V1) TAKEOFF ABORTED

A
  1. Power Levers ……………………………………………. GROUND FINE
  2. Brakes … AS REQUIRED TO ACHIEVE STOPPING DISTANCE
    3.Operative Engine ………………………………. MAXIMUM REVERSE
    WARNING – Extreme care must be exercised when using single engine reversing on surfaces with reduced traction.
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5
Q

ENGINE FAILURE DURING TAKEOFF (AT OR ABOVE V1) - TAKEOFF CONTINUED

A
  1. Power …………………………………………. MAXIMUM ALLOWABLE
  2. Airspeed ……………………… MAINTAIN (take-off speed or above)
  3. Landing Gear (when positive climb) …………………………….. UP
  4. Propeller (inoperative engine) …………… VERIFY FEATHERED
  5. Above Obstacles ………………………………………….. SPEED VYSE
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6
Q

ENGINE FAILURE IN FLIGHT BELOW AIR MINIMUM CONTROL SPEED (VMCA)

A
  1. Power …… REDUCE AS REQUIRED TO MAINTAIN CONTROL
  2. Nose ……………………. LOWER TO ACCELERATE ABOVE VMCA
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7
Q

ENGINE FLAMEOUT (2ND ENGINE)

A
  1. Power Lever ……………………………………………………………… IDLE
  2. Prop Lever …………………………………………… DO NOT FEATHER
  3. Condition Lever …………………………………………. FUEL CUTOFF
  4. Conduct Air Start Procedure in ABNORMAL PROCEDURES
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8
Q

FUEL PRESSURE LOW L FUEL PRESS OR R FUEL PRESS

A
  1. Standby Pump (failed side)………………………………………….. ON
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9
Q

ELECTRICAL SMOKE OR FIRE

A
  1. Oxygen Mask(s) ………………………………………………………. DON
  2. Mask Selector Switch …………………………… EMERG POSITION
  3. Mic Switch(es) …………………………………………………………..OXY
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10
Q

ENVIRONMENTAL SYSTEM SMOKE OR FUMES

A
  1. Oxygen Mask(s) ………………………………………………………. DON
  2. Mask Selector Switch …………………………… EMERG POSITION
  3. Mic Switch(es) …………………………………………………………..OXY
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11
Q

AIRSTAIR DOOR/CARGO DOOR UNLOCKED DOOR UNLOCKED

A

WARNING – Do not attempt to check the security of the airstair door or cargo door in flight. Remain as far from the door as possible with seatbelts securely fastened. If the DOOR UNLOCKED annunciator is displayed, or if an unlatched airstair door/cargo door is suspected:
1. All Occupants ………………………….. SEATED WITH SEAT BELT
……………………………………………………….. SECURELY FASTENED

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12
Q

EMERGENCY DESCENT

A
  1. Power Levers………………………………………………………….. IDLE
  2. Prop Levers …………………………………………… FULL FORWARD
  3. Flaps (200 kts maximum) ………………………………. APPROACH
  4. Landing Gear (181 kts maximum) …………………………… DOWN
  5. Airspeed ……………………………………………. 181 KTS MAXIMUM
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13
Q

GLIDE

A
  1. Landing Gear ……………………………………………………………… UP
  2. Flaps …………………………………………………………………………. UP
    WARNING – Determine that procedures for restarting first and
    second failed engines are ineffective before feathering second
    engine propeller.
  3. Propellers ……………………………………………………. FEATHERED
  4. Airspeed …………………………………………………………….. 135 KTS
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14
Q

DUAL GENERATOR FAILURE L DC GEN OR R DC GEN

A
  1. Generators …………………………………………… RESET, THEN ON
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15
Q

USE OF OXYGEN-CREW

A
  1. Oxygen Mask(s)……………………………………………………….. DON
  2. Mic Switch(es) ………………………………………………………….. OXY
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16
Q

PRESSURISATION LOSS ALT WARN

A
  1. Oxygen Mask(s)…………………………………………………………DON
  2. Mic Switch(es) ………………………………………………………….. OXY
  3. Passenger Manual Drop-Out ………………………………………. PULL ON …………… ….. PASS OXY ON ILLUMINATED
  4. Descend …………………………………………………… AS REQUIRED
17
Q

AUTO-DEPLOYMENT OXYGEN SYSTEM FAILURE ALT WARN ILLUMINATED PASS OXY ON EXTINGUISHED

A
  1. Passenger Manual Drop-Out ………………………………. PULL ON
18
Q

BLEED AIR FAIL L BLEED FAIL OR R BLEED FAIL

A
  1. Bleed Air Valve (affected engine) ……….. PNEU & ENVIR OFF
19
Q

SPINS

A
  1. Control Column ………. FULL FORWARD, AILERON NEUTRAL
  2. Full Rudder ……………….OPPOSITE THE DIRECTION OF SPIN
  3. Power Levers …………………………………………………………… IDLE
  4. Rudder ………………… NEUTRALISE WHEN ROTATION STOPS
  5. Execute a smooth pullout
20
Q

UNSCHEDULED ELECTRIC ELEVATOR TRIM ACTIVATION

A
  1. Airplane Attitude …. MAINTAIN USING ELEVATOR CONTROL
  2. AP/Trim Disconnect ………………….. DEPRESS FULLY & HOLD
21
Q

UNSCHEDULED RUDDER BOOST ACTIVATION

A
  1. Directional Control ………. MAINTAIN USING RUDDER PEDALS
  2. Rudder Boost …………………………………………………………… OFF
    If Condition persists:
  3. Rudder Boost Circuit Breaker ……………………………………PULL
22
Q

AUTOPILOT MISTRIM E OR A

A

WARNING – Intentional or automatic disengagement of the autopilot without restraining the control wheel during a Mistrim condition will produce a significant airplane response in the direction of the mistrm force.
1. Flight Controls ………………………………………………. HOLD FIRMLY
(control forces may exceed 25 lbs)
2. A/P ………………………………………………………………….. DISENGAGE

23
Q

AUTOPILOT TRIM FAIL TRIM

A
  1. Flight Controls …………………………………………… HOLD FIRMLY
  2. A/P ………………………………………………………………. DISENGAGE
24
Q

AUTOPILOT AUTOMATIC DISENGAGEMENT TRIM

A

If an Automatic Disengagement Occurs:
1. Maintain airplane control
2. AP/YD Disconnect ………………………………… DEPRESS TO 1ST
………………………………………………………………………………….. LEVEL TO CANCEL HORN

25
Q

TAWS + WARNING

A

In IMC or at Night
1. Wings……………………………………………………………………. LEVEL
2. Power ………………………………………………….. MAX ALLOWABLE
3. Pitch ………………………………………………………………. INCREASE
* Promptly and smoothly increase pitch towards an initial pitch attitude of 20⁰-25⁰
* Adjust as required to avoid continuous buffeting and/or stall warning
* Adjust to maintain 100 kts
4. Gear and Flaps …………………………………………………………… UP

26
Q

Windshear approach to land

A

Power Levers - Takeoff Setting
* Go-Around Button – Depress
* Rotate aircraft to initiate a climb and stop aircraft descent where possible contact with terrain exists. Accept a lower than normal airspeed, up to the stall tone
* Once no possibility of ground contact exists
* Normal Go-Around – Initiate (FLAP APPROACH, GEAR UP etc)

27
Q

Winshear on takeoff

A

Before V1
* Abort the Takeoff
Between V1 and VR
* Power Levers confirm at takeoff setting
* Aircraft rotate (Should commence no later than 600m (2000 ft) before the end of the runway, even if speed is below VR.
After VR
* Power Levers confirm takeoff power selected
During Initial Climb
* Power Levers/advance as required
* Autopilot Disconnect
Subsequent Actions
* Flight instruments. Monitor the vertical flight path indications, airspeed trend and attitude
* Pitch attitude. Maintain, adjust as required to stop aircraft descent while possible contact with terrain exists. Accept a lower than normal airspeed, up to the stall tone.
* Configuration. Maintain the current configuration until clear of wind shear indications.

28
Q

TCAS RA

A

Autopilot - disengage
Smoothly follow TCAS prompt

29
Q

Aborted start

A

“Abort Start”
- Ignition and starter…….OFF
No light off, fuel PX too high or low, start not engaged, hot start, hung start, no oil pressure, no ITT rise within 10 seconds, unusual noise/vibration

30
Q

Stabilised Approach Criteria

A
  1. The aircraft is on the correct flight path;
  2. Only small changes in heading/pitch are required to maintain the correct flight path;
  3. The aircraft speed is no more than VREF + 20 kts indicated airspeed and not less than VREF;
  4. The aircraft is in the correct landing configuration;
  5. Sink rate is no greater than 1,000 ft per min; if an approach requires a sink rate greater than 1,000 ft per min, a special briefing should be conducted;
  6. Power setting is appropriate for the aircraft configuration and is not below the minimum power for approach as defined by the aircraft operating manual;
  7. All briefings and checklists have been conducted;
  8. Specific types of approaches are stablised if they also fulfill the following: instrument landing system (ILS) approaches must be flown within one dot of the glideslope and localizer; during a circling approach, wings should be level on final when the aircraft reaches 300 ft above airport elevation; and,
  9. Unique approach procedures or abnormal conditions requiring a deviation from the above elements of a stablised approach required a special briefing.

ATPL (8 decks)

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