King Air 350i Memory Items M.F.Ö Flashcards

1
Q

King Air 350i ProLine 21

Flash Cards with Memory Items

::: FLYRIGHT ::::
::: M.F.Ö :::

A

INTENTIONALLY LEFT BLANK

;)

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2
Q

EMERGENCY AIRSPEEDS

One-Engine-Inoperative

Best-Angle-of-Climb (VXSE)..
Best-Rate-of-Climb (VYSE)…
Enroute Climb…

A

125
125
125

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3
Q

EMERGENCY AIRSPEEDS

Air Minimum Control Speeds (VMCA)

Flaps Up ..
Flaps Approach ..

A

Flaps Up ..94 Knots

Flaps App..93 Knots

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4
Q

EMERGENCY AIRSPEEDS

Emergency Descent …

A

184 Knots

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5
Q

EMERGENCY AIRSPEEDS

Maximum Range Glide..

A

135 Knots

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6
Q

ENGINE FAILURE

ENGINE FIRE
OR
FAILURE IN FLIGHT

A

Affected Engine:

  1. Condition Lever… FUEL CUTOFF
  2. Prop Lever…FEATHER
  3. Firewall Fuel Valve…CLOSE
  4. Fire Extinguisher (if fire warning persists)… ACTUATE
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7
Q

ENGINE FAILURE

ENGINE FIRE ON GROUND

A

Affected Engine:

  1. Condition Lever…FUEL CUTOFF
  2. Firewall Fuel Valve…CLOSE
  3. Starter Switch…STARTER ONLY
  4. Fire Extinguisher(if fire warning persists)…ACTUATE
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8
Q

ENGINE FAILURE

EMERGENCY ENGINE SHUTDOWN
ON THE GROUND

A
  1. Condition Levers…FUEL CUTOFF
  2. Prop Levers… FEATHER
  3. Firewall Fuel Valves…CLOSE
  4. Master Switch (gang bar)…OFF
  5. Battery Bus…EMERG OFF
  6. ESIS Power…OFF
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9
Q

ENGINE FAILURE

ENGINE FAILURE DURING TAKEOFF
AT OR BELOW V1
TAKEOFF ABORTED

A
  1. Power Levers…GROUND FINE

2. Brakes …MAXIMUM

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10
Q

ENGINE FAILURE

ENGINE FAILURE DURING TAKEOFF
AT OR ABOVE V1
TAKEOFF CONTINUED

A
  1. VR Speed..ROTATE TO APPROX. 10° PITCH ATTITUDE
  2. Landing Gear (when positive climb established)…UP
  3. Airspeed…MAINTAIN V2 TO 400 FT AGL
  4. Propeller (inoperative engine)… VERIFY FEATHERED
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11
Q

ENGINE FAILURE

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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12
Q

ENGINE FAILURE

ELECTRICAL SMOKE OR FIRE

A
  1. Oxygen Mask(s) ……DON
  2. Mask Selector Switch …EMERG
  3. Mic Switch(es)…. OXY
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13
Q

ENGINE FAILURE

ENVIRONMENTAL SYSTEM
SMOKE OR FUMES

A
  1. Oxygen Mask(s) ……DON
  2. Mask Selector Switch …EMERG
  3. Mic Switch(es)…. OXY
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14
Q

AIRSTAIR DOOR/CARGO DOOR
UNLOCKED [DOOR UNLOCKED]

If The [DOOR UNLOCKED] illuminates, or if an unlatched airstair door / cargo door is suspected:

A
  1. All Occupants-.. SEATED WITH SEAT BELTS

SECURELY FASTENED

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15
Q

EMERGENCY DESCENT

A
  1. Power Levers ..IDLE
  2. Prop Levers ..FULL FORWARD
  3. Flaps (202 knots maximum)…APPROACH
  4. Landing Gear (184 knots maximum)…DOWN
  5. Airspeed….184 KNOTS MAXIMUM
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16
Q

GLIDE

A
  1. Landing Gear … UP
  2. Flaps… UP
  3. Prop Levers … FEATHERED
  4. Airspeed …..135 KNOTS
17
Q

ELECTRICAL

DUAL GENERATOR FAILURE
[L DC GEN] & [R DC GEN]

A
  1. Instrument Emergency Lights (if required)…ON
  2. Generators … RESET, THEN ON
    If Either Generator Will Reset:
  3. Operating Generator Loadmeter…MONITOR
18
Q

DUAL GENERATOR FAILURE
[L DC GEN] & [R DC GEN]
(continued)

If Neither Generator Will Reset:

A
  1. ECS Mode……………………………………………………………..OFF
  2. Cockpit/Cabin Blower…………………………………………AUTO
  3. Non-essential Equipment………………………………………OFF
19
Q

ENVIRONMENTAL SYSTEMS

USE OF OXYGEN

CREW

A
  1. Oxygen Mask(s)……….DON

2. Mic Switch(es)…….OXY

20
Q

ENVIRONMENTAL SYSTEMS

PRESSURIZATION LOSS
[CABIN ALT HI]

A
  1. Oxygen Mask(s)………DON
  2. Mic Switch(es)…….OXY
  3. Passenger Manual Drop Out… PULL ON
  4. Descend…. AS REQUIRED
21
Q

ENVIRONMENTAL SYSTEMS

HIGH DIFFERENTIAL PRESSURE
[CABIN DIFF HI]

A
  1. Bleed Air Valves…..ENVIR OFF
  2. Oxygen (crew and passengers)… AS REQUIRED
  3. Descend …… AS REQUIRED
22
Q

ENVIRONMENTAL SYSTEMS

AUTO-DEPLOYMENT
OXYGEN SYSTEM FAILURE
[CABIN ALT HI] ILLUMINATED,
[PASS OXYGEN ON] EXTINGUISHED

A
  1. Passenger Manual Drop Out…… PULL ON
23
Q

ENVIRONMENTAL SYSTEMS

BLEED AIR FAIL
[L BLEED FAIL] OR
[R BLEED FAIL]

A
  1. Bleed Air Valve (affected engine).. PNEU&ENVIR OFF
24
Q

SPINS

A
  1. Control Column..FULL FORWARD,AILERONSNEUTRAL
  2. Full Rudder… OPPOSITE THE DIRECTION OF SPIN
  3. Power Levers….IDLE
  4. Rudder….NEUTRALIZE WHEN ROTATION STOPS
  5. Execute a smooth pullout.
25
Q

FLIGHT CONTROLS

UNSCHEDULED ELECTRIC
PITCH TRIM ACTIVATION

A
  1. Airplane Attd..MAINTAIN USING ELEVATOR CONTROL

2. AP/Trim Disconnect …. DEPRESS FULLY AND HOLD

26
Q

FLIGHT CONTROLS

UNSCHEDULED RUDDER BOOST
ACTIVATION

A
  1. AP/Trim Disconn. DEPRESS TO 1ST LEVEL AND HOLD
  2. Rudder Boost ….OFF
    If Condition Persists:
  3. YD/AP DISC (on Flight Guidance Panel)….PULL DOWN
27
Q

AVIONICS

AUTOPILOT FAILURES
AUTOPILOT MISTRIM [E] OR [A]
If A Mistrim Indication Continues For
More Than A Few Seconds

A
  1. Flight Controls…HOLD FIRMLY

2. AP ..DISENGAGE

28
Q

AVIONICS

AUTOPILOT TRIM FAIL [TRIM]

A
  1. Flight Controls…..HOLD FIRMLY

2. AP…DISENGAGE

29
Q

AVIONICS

AUTOPILOT AUTOMATIC
DISENGAGEMENT
If An Automatic Disengagement Occurs:

A
  1. Maintain airplane control.
    AP /TRIM Disconnect………..DEPRESS TO 1ST LEVEL TO
    CANCEL HORN
30
Q
AVIONICS
ENHANCED GROUND PROXIMITY
WARNING SYSTEM
(EGPWS) (IF INSTALLED)
In IMC Or At Night:
A
  1. Wings…LEVEL
  2. Power…MAX ALLOWABLE
  3. Pitch…INCREASE
    • Promptly and smoothly increase pitch towards an initial pitch attitude of 20º to 25º.
31
Q

AVIONICS (CONTINUED)

ENHANCED GROUND PROXIMITY
WARNING SYSTEM
EGPWS) (IF INSTALLED
In IMC Or At Night:

A

• Adjust as required to avoid continuous buffeting and/or
stall warning.
• Adjust to maintain 125 KIAS.
4. Gear and Flaps…… UP