KA200 Memory Items

Question 1

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

Answer 1

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

Question 2

ENGINE FIRE ON GROUND (ENG FIRE light*)

Answer 2

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

Question 3

EMERGENCY ENGINE SHUTDOWN ON THE GROUND

Answer 3

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

Question 4

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

Answer 4

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.

Question 5

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

Answer 5

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

Question 6

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

Answer 6

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

Question 7

ENGINE FLAMEOUT (2ND ENGINE)

Answer 7

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

Question 8

FUEL PRESSURE LOW L FUEL PRESS OR R FUEL PRESS

Answer 8

1. Standby Pump (failed side)………………………………………….. ON

Question 9

ELECTRICAL SMOKE OR FIRE

Answer 9

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

Question 10

ENVIRONMENTAL SYSTEM SMOKE OR FUMES

Answer 10

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

Question 11

AIRSTAIR DOOR/CARGO DOOR UNLOCKED DOOR UNLOCKED

Answer 11

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

Question 12

EMERGENCY DESCENT

Answer 12

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

Question 13

GLIDE

Answer 13

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

Question 14

DUAL GENERATOR FAILURE L DC GEN OR R DC GEN

Answer 14

1. Generators …………………………………………… RESET, THEN ON

Question 15

USE OF OXYGEN-CREW

Answer 15

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

Question 16

PRESSURISATION LOSS ALT WARN

Answer 16

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

Question 17

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

Answer 17

1. Passenger Manual Drop-Out ………………………………. PULL ON

Question 18

BLEED AIR FAIL L BLEED FAIL OR R BLEED FAIL

Answer 18

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

Question 19

SPINS

Answer 19

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

Question 20

UNSCHEDULED ELECTRIC ELEVATOR TRIM ACTIVATION

Answer 20

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

Question 21

UNSCHEDULED RUDDER BOOST ACTIVATION

Answer 21

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

Question 22

AUTOPILOT MISTRIM E OR A

Answer 22

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

Question 23

AUTOPILOT TRIM FAIL TRIM

Answer 23

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

Question 24

AUTOPILOT AUTOMATIC DISENGAGEMENT TRIM

Answer 24

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

Question 25

TAWS + WARNING

Answer 25

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

Question 26

Windshear approach to land

Answer 26

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)

Question 27

Winshear on takeoff

Answer 27

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.

Question 28

TCAS RA

Answer 28

Autopilot - disengage Smoothly follow TCAS prompt

Question 29

Aborted start

Answer 29

"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

Question 30

Stabilised Approach Criteria

Answer 30

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.