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King Air 350 EP's
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ENGINE FIRE OR FAILURE INFLIGHT
Affected engine:
1 . Condition Lever — FUEL CUTOFF
2 . Prop Lever — FEATHER
3 . Firewall Fuel Valve — CLOSE
[EXTINGUISHER PUSH] & [CLOSED] —
ILLUMINATED
4 . Fire Extinguisher (if fire warning persists) —
ACTUATE [DISCHARGED] —
ILLUMINATED
ENGINE FIRE ON GROUND
Affected Engine:
1 . Condition Lever — FUEL CUTOFF
2 . Firewall Fuel Valve — CLOSE
[EXTINGUISHER PUSH] &[CLOSED] —
ILLUMINATED
3 . Starter Switch — STARTER ONLY
4 . Fire Extinguisher (if fire warning persists) —
ACTUATE [DISCHARGED] —
ILLUMINATED
EMERGENCY ENGINE SHUTDOWN ON THE GROUND
1 . Condition Levers — FUEL CUTOFF
2 . Prop Levers — FEATHER
3 . Firewall Fuel Valves — CLOSE
[EXTINGUISHER PUSH] & [CLOSED] —
ILLUMINATED
4 . Master Switch (gang bar) — OFF
5 . Battery Bus — EMER OFF
6 . ESIS Power — OFF
ENGINE FAILURE DURING TAKEOFF (AT OR BELOW V1) — TAKEOFF ABORTED
1 . Power Levers — GROUND FINE
2 . Brakes — MAXIMUM (or as required to achieve stopping distance
ENGINE FAILURE DURING TAKEOFF (AT OR ABOVE V1) — TAKEOFF CONTINUED
1 . VR Speed — ROTATE TO APPROXIMATELY 10º PITCH ATTITUDE
2 . Landing Gear (When positive climb established) — UP
3 . Airspeed — MAINTAIN V2 to 400 FT AGL
4 . Propeller (inoperative engine) — VERIFY FEATHERED
ENGINE FAILURE IN FLIGHT BELOW AIR MINIMUM CONTROL SPEED (VMCA)
1 . Power — REDUCE AS REQUIRED TO MAINTAIN CONTROL
2 . Nose — LOWER TO ACCELERATE ABOVE VMCA
GLIDE (BOTH ENGINES INOPERATIVE)
1 . Landing Gear — UP
2 . Flaps — UP
3 . Prop Levers — FEATHERED
4 . Airspeed — 135 KTS
DUAL GENERATOR FAILURE [L DC GEN] & [R DC GEN]
1 . Instrument Emergency Lights (if required) — ON
2 . Generator — RESET, THEN ON
If either Generator will reset:
3 . Operating Generator Loadmeter — MONITOR
If neither Generator will reset:
4 . ECS Mode — OFF
5 . Cockpit/Cabin Blower — AUTO
6 . Non-essential Equipment— OFF
UNSCHEDULED ELECTRIC PITCH TRIM ACTIVATION
1 . Airplane Attitude — MAINTAIN USING
ELEVATOR CONTROL
2 . AP/Trim Disconnect — DEPRESS FULLY AND
HOLD[TRIM] - ILLUMINATED
UNSCHEDULED RUDDER BOOST ACTIVATION
1 . AP/Trim Disconnect — DEPRESS TO 1ST
LEVEL AND HOLD
2 . Rudder Boost — OFF
If condition persists:
3 . YD/AP DISC (on Flight Guidance Panel) —
PULL DOWN
SPINS
1 . Control Column — FULL FORWARD,
AILERONS NEUTRAL
2 . Full Rudder — OPPOSITE THE DIRECTION
OF SPIN
3 . Power Levers — IDLE
4 . RUDDER — NEUTRALIZE WHEN ROTATION
STOPS
5 . Execute smooth pullout.
ELECTRICAL SMOKE OR FIRE
1 . Oxygen Mask(s) — DON
2 . Mask Selector Switch — EMERG
3 . Mic Switch(es) — OXY
ENVIRONMENTAL SYSTEM SMOKE OR FUMES
1 . Oxygen Mask(s) — DON
2 . Mask Selector Switch — EMERG
3 . Mic Switch(es) — OXY
AIRSTAIR/CARGO DOOR UNLOCKED
1 . All Occupants — SEATED WITH SEAT BELTS
SECURELY FASTENED
EMERGENCY DESCENT
1 . Power Levers — IDLE
2 . Prop Levers — FULL FORWARD
3 . Flaps (202 Kts maximum) — APPROACH
4 . Landing Gear (184 Kts maximum) — DOWN
5 . Airspeed — 184 KTS MAXIMUM
USE OF OXYGEN
Crew:
1 . Oxygen Mask(s) — DON
2 . Mic Switch(es) — OXY
Warning: The highest recommended cabin altitude for sustained flight is 25,000 ft.
PRESSURIZATION LOSS [CABIN ALT HI]
1 . Oxygen Mask(s) — DON
2 . Mic Switch(es) — OXY
3 . Passenger Manual Drop Out — PULL ON
[PASS OXYGEN ON] - ILLUMINATED
4 . Descend — AS REQUIRED
HIGH DIFFERENTIAL PRESSURE
1 . Bleed Air Valves — ENVIR OFF
2 . Oxygen (crew and passengers) — AS
REQUIRED
3 . Descend — AS REQUIRED
AUTO-DEPLOYMENT OXYGEN SYSTEM FAILURE
1 . Passenger Manual Drop out — PULL ON
BLEED AIR FAILURE
1 . Bleed Air Valve Switch (Affected Engine) — PNEU and ENVIR OFF
[L BLEED OFF] or [R BLEED OFF] —
ILLUMINATED
AUTOPILOT MISTRIM [E] OR [A]
if a Mistrim Indication continues for more than a few seconds:
1 . Flight Controls — HOLD FIRMLY(Control
forces may exceed 25 lbs)
2 . AP — DISENGAGE
AUTOPILOT TRIM FAIL [TRIM]
1 . Flight Controls — HOLD FIRMLY
2 . AP — DISENGAGE.
AUTOPILOT AUTOMATIC DISENGAGEMENT
if an Automatic Disengagement occurs:
1 . Maintain Airplane control.
2 . AP/TRIM Disconnect — DEPRESS TO 1ST LEVEL TO CANCEL THE HORN
ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) (IF INSTALLED)
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 20° to
25°.
•Adjust as required to avoid continuous
buffeting and/or stall warning.
•Adjust to maintain 125 KIAS.
4 . Gear and Flaps — UP
Author
johnswm
ID
255519
Card Set
King Air 350 EP's
Description
Emergency Procedures for King Air 350
Updated
2014-01-08T02:57:06Z
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