King Air 350i Memory Items M.F.Ö Flashcards
King Air 350i ProLine 21
Flash Cards with Memory Items
::: FLYRIGHT ::::
::: M.F.Ö :::
INTENTIONALLY LEFT BLANK
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EMERGENCY AIRSPEEDS
One-Engine-Inoperative
Best-Angle-of-Climb (VXSE)..
Best-Rate-of-Climb (VYSE)…
Enroute Climb…
125
125
125
EMERGENCY AIRSPEEDS
Air Minimum Control Speeds (VMCA)
Flaps Up ..
Flaps Approach ..
Flaps Up ..94 Knots
Flaps App..93 Knots
EMERGENCY AIRSPEEDS
Emergency Descent …
184 Knots
EMERGENCY AIRSPEEDS
Maximum Range Glide..
135 Knots
ENGINE FAILURE
ENGINE FIRE
OR
FAILURE IN FLIGHT
Affected Engine:
- Condition Lever… FUEL CUTOFF
- Prop Lever…FEATHER
- Firewall Fuel Valve…CLOSE
- Fire Extinguisher (if fire warning persists)… ACTUATE
ENGINE FAILURE
ENGINE FIRE ON GROUND
Affected Engine:
- Condition Lever…FUEL CUTOFF
- Firewall Fuel Valve…CLOSE
- Starter Switch…STARTER ONLY
- Fire Extinguisher(if fire warning persists)…ACTUATE
ENGINE FAILURE
EMERGENCY ENGINE SHUTDOWN
ON THE GROUND
- Condition Levers…FUEL CUTOFF
- Prop Levers… FEATHER
- Firewall Fuel Valves…CLOSE
- Master Switch (gang bar)…OFF
- Battery Bus…EMERG OFF
- ESIS Power…OFF
ENGINE FAILURE
ENGINE FAILURE DURING TAKEOFF
AT OR BELOW V1
TAKEOFF ABORTED
- Power Levers…GROUND FINE
2. Brakes …MAXIMUM
ENGINE FAILURE
ENGINE FAILURE DURING TAKEOFF
AT OR ABOVE V1
TAKEOFF CONTINUED
- VR Speed..ROTATE TO APPROX. 10° PITCH ATTITUDE
- Landing Gear (when positive climb established)…UP
- Airspeed…MAINTAIN V2 TO 400 FT AGL
- Propeller (inoperative engine)… VERIFY FEATHERED
ENGINE FAILURE
ENGINE FAILURE IN FLIGHT BELOW
AIR MINIMUM CONTROL SPEED
VMCA
- Power.REDUCE AS REQUIRED TO MAINTAIN CONTROL
2. Nose ….LOWER TO ACCELERATE ABOVE VMCA
ENGINE FAILURE
ELECTRICAL SMOKE OR FIRE
- Oxygen Mask(s) ……DON
- Mask Selector Switch …EMERG
- Mic Switch(es)…. OXY
ENGINE FAILURE
ENVIRONMENTAL SYSTEM
SMOKE OR FUMES
- Oxygen Mask(s) ……DON
- Mask Selector Switch …EMERG
- Mic Switch(es)…. OXY
AIRSTAIR DOOR/CARGO DOOR
UNLOCKED [DOOR UNLOCKED]
If The [DOOR UNLOCKED] illuminates, or if an unlatched airstair door / cargo door is suspected:
- All Occupants-.. SEATED WITH SEAT BELTS
SECURELY FASTENED
EMERGENCY DESCENT
- Power Levers ..IDLE
- Prop Levers ..FULL FORWARD
- Flaps (202 knots maximum)…APPROACH
- Landing Gear (184 knots maximum)…DOWN
- Airspeed….184 KNOTS MAXIMUM
GLIDE
- Landing Gear … UP
- Flaps… UP
- Prop Levers … FEATHERED
- Airspeed …..135 KNOTS
ELECTRICAL
DUAL GENERATOR FAILURE
[L DC GEN] & [R DC GEN]
- Instrument Emergency Lights (if required)…ON
- Generators … RESET, THEN ON
If Either Generator Will Reset: - Operating Generator Loadmeter…MONITOR
DUAL GENERATOR FAILURE
[L DC GEN] & [R DC GEN]
(continued)
If Neither Generator Will Reset:
- ECS Mode……………………………………………………………..OFF
- Cockpit/Cabin Blower…………………………………………AUTO
- Non-essential Equipment………………………………………OFF
ENVIRONMENTAL SYSTEMS
USE OF OXYGEN
CREW
- Oxygen Mask(s)……….DON
2. Mic Switch(es)…….OXY
ENVIRONMENTAL SYSTEMS
PRESSURIZATION LOSS
[CABIN ALT HI]
- Oxygen Mask(s)………DON
- Mic Switch(es)…….OXY
- Passenger Manual Drop Out… PULL ON
- Descend…. AS REQUIRED
ENVIRONMENTAL SYSTEMS
HIGH DIFFERENTIAL PRESSURE
[CABIN DIFF HI]
- Bleed Air Valves…..ENVIR OFF
- Oxygen (crew and passengers)… AS REQUIRED
- Descend …… AS REQUIRED
ENVIRONMENTAL SYSTEMS
AUTO-DEPLOYMENT
OXYGEN SYSTEM FAILURE
[CABIN ALT HI] ILLUMINATED,
[PASS OXYGEN ON] EXTINGUISHED
- Passenger Manual Drop Out…… PULL ON
ENVIRONMENTAL SYSTEMS
BLEED AIR FAIL
[L BLEED FAIL] OR
[R BLEED FAIL]
- Bleed Air Valve (affected engine).. PNEU&ENVIR OFF
SPINS
- Control Column..FULL FORWARD,AILERONSNEUTRAL
- Full Rudder… OPPOSITE THE DIRECTION OF SPIN
- Power Levers….IDLE
- Rudder….NEUTRALIZE WHEN ROTATION STOPS
- Execute a smooth pullout.
FLIGHT CONTROLS
UNSCHEDULED ELECTRIC
PITCH TRIM ACTIVATION
- Airplane Attd..MAINTAIN USING ELEVATOR CONTROL
2. AP/Trim Disconnect …. DEPRESS FULLY AND HOLD
FLIGHT CONTROLS
UNSCHEDULED RUDDER BOOST
ACTIVATION
- AP/Trim Disconn. DEPRESS TO 1ST LEVEL AND HOLD
- Rudder Boost ….OFF
If Condition Persists: - YD/AP DISC (on Flight Guidance Panel)….PULL DOWN
AVIONICS
AUTOPILOT FAILURES
AUTOPILOT MISTRIM [E] OR [A]
If A Mistrim Indication Continues For
More Than A Few Seconds
- Flight Controls…HOLD FIRMLY
2. AP ..DISENGAGE
AVIONICS
AUTOPILOT TRIM FAIL [TRIM]
- Flight Controls…..HOLD FIRMLY
2. AP…DISENGAGE
AVIONICS
AUTOPILOT AUTOMATIC
DISENGAGEMENT
If An Automatic Disengagement Occurs:
- Maintain airplane control.
AP /TRIM Disconnect………..DEPRESS TO 1ST LEVEL TO
CANCEL HORN
AVIONICS ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) (IF INSTALLED) In IMC Or At Night:
- Wings…LEVEL
- Power…MAX ALLOWABLE
- Pitch…INCREASE
• Promptly and smoothly increase pitch towards an initial pitch attitude of 20º to 25º.
AVIONICS (CONTINUED)
ENHANCED GROUND PROXIMITY
WARNING SYSTEM
EGPWS) (IF INSTALLED
In IMC Or At Night:
• Adjust as required to avoid continuous buffeting and/or
stall warning.
• Adjust to maintain 125 KIAS.
4. Gear and Flaps…… UP
