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King Air 350 Emergency Procedures (Proline 21 and EFIS)
EPs for Proline-21 and EFIS King Air 350s (per the Pilot's Operating Handbook)
34
Aviation
Professional
07/29/2011
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Cards

Term

ENGINE FIRE OR FAILURE IN FLIGHT

(EFIS & PL-21)

Per POH P/N 130-590031-71B10, rev. Feb 2007 (pg. 3-3)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-3)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-3)

 Definition

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
Term

 ENGINE FIRE ON GROUND

(EFIS & PL-21)

Per POH P/N 130-590031-71B10, rev. Feb 2007 (pg. 3-4)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-4)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-4)

 Definition

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
Term

EMERGENCY ENGINE SHUTDOWN ON THE GROUND

(EFIS)

Per POH P/N 130-590031-71B10, rev. Feb 2007 (pg. 3-4)

 Definition

1. Condition Levers - FUEL CUTOFF

2. Prop Levers - FEATHER

3. Firewall Fuel Valves - CLOSE

[EXTINGUISHER PUSH] & [CLOSED] - ILLUMINATED

4.  Master Switch (gangbar) - OFF

5.  Battery Bus – EMER OFF
Term

EMERGENCY ENGINE SHUTDOWN ON THE GROUND

(PL-21)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-4)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-4)

 Definition

1. Condition Levers - FUEL CUTOFF

2. Prop Levers - FEATHER

3. Firewall Fuel Valves - CLOSE

[EXTINGUISHER PUSH] & [CLOSED] - ILLUMINATED

4.  Master Switch (gangbar) - OFF

5.  Battery Bus - EMER OFF

6.  ESIS Power – OFF
Term

ENGINE FAILURE DURING TAKEOFF

(AT OR BELOW V1)- TAKEOFF ABORTED

(EFIS & PL-21)

Per POH P/N 130-590031-71B10, rev. Feb 2007 (pg. 3-4)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-4)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-4)

 Definition

1. Power Levers – GROUND FINE

2. Braking – MAXIMUM (or as required to achieve stopping distance)
Term

ENGINE FAILURE DURING TAKEOFF

(AT OR BELOW V1)- TAKEOFF CONTINUED

(EFIS & PL-21)

Per POH P/N 130-590031-71B10, rev. Feb 2007 (pg. 3-5)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-5)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-5)

 

 Definition

1.  VR Speed – ROTATE TO APPROXIMATELY 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
Term

ENGINE FAILURE IN FLIGHT BELOW VMCA

(EFIS & PL-21)

Per POH P/N 130-590031-71B10, rev. Feb 2007 (pg. 3-5)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-5)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-5)

 

 

 Definition

1.  Power – REDUCE AS REQUIRED TO MAINTAIN CONTROL

2.  Nose – LOWER TO ACCELERATE ABOVE VMCA

 
Term

ELECTRICAL SMOKE OR FIRE

(EFIS)

Per POH P/N 130-590031-71B10, rev. Feb 2007 (pg. 3-6)

 Definition

1.  Oxygen Mask(s) – DON

2.  Mask Selector Switch – EMERG Position

3.  Headset(s) – DON, OR AUDIO SPEAKER(S) - ON

4.  Mic Switch(es) – OXYGEN MASK

 

[Not boldface:

    5.  Instrument Emergency Lights (if required) – ON

    5A.  (With ISR mod) MISSION POWER Switch – OFF

    6.  Avionics Master – OFF

    7.  Generators – OFF]
Term

ELECTRICAL SMOKE OR FIRE

(PL-21)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-7)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-7)

 

 Definition

1.  Oxygen Mask(s) – DON

2.  Mask Selector Switch – EMERG Position

3.  Mic Switch(es) – OXY

 

[Not boldface:

    4.  Instrument Emergency Lights (if required) – ON

    4A.  (With ISR mod) MISSION POWER Switch – OFF

    5.  Generators – OFF]
Term

ENVIRONMENTAL SYSTEM SMOKE OR FUMES

(EFIS)

Per POH P/N 130-590031-71B10, rev. Feb 2007 (pg. 3-8)

 

 Definition

1.  Oxygen Mask(s) – DON

2.  Mask Selector Switch – EMERG Position

3.  Headset(s) – DON, OR AUDIO SPEAKER(S) - ON

4.  Mic Switch(es) – OXYGEN MASK
Term

ENVIRONMENTAL SYSTEM SMOKE OR FUMES

 (PL-21)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-8)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-8)

 Definition

1.  Oxygen Mask(s) – DON

2.  Mask Selector Switch – EMERG Position

3.  Mic Switch(es) – OXY
Term

AIRSTAIR DOOR/CARGO DOOR UNLOCKED

[DOOR UNLOCKED]

(EFIS & PL-21)

Per POH P/N 130-590031-71B10, rev. Feb 2007 (pg. 3-9)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-9)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-9)

 

 Definition

1.  All Occupants – SEATED WITH SEAT BELTS SECURELY FASTENED
Term

EMERGENCY DESCENT

(EFIS & PL-21)

Per POH P/N 130-590031-71B10, rev. Feb 2007 (pg. 3-9)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-9)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-9)

 

 Definition

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
Term

GLIDE

(EFIS & PL-21)

Per POH P/N 130-590031-71B10, rev. Feb 2007 (pg. 3-11)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-11)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-11)

 

 Definition

1.  Landing Gear - UP
2.  Flaps - UP

3.  Prop Levers - FEATHERED

4.  Airspeed - 135 KIAS
Term

SINGLE INVERTER FAILURE

[#1 AC BUS] or [#2 AC BUS]

(EFIS)

Per POH P/N 130-590031-71B10, rev. Feb 2007 (pg. 3-11)

 Definition

1.  AC Bus Circuit Breakers - CHECK

If circuit breaker is not tripped:

2.  Failed Inverter – SELECT BUS TRANSFER

 

If circuit breaker is tripped:

3.  Circuit breaker - RESET
Term

DUAL INVERTER FAILURE

[#1 AC BUS] and [#2 AC BUS]

(EFIS)

Per POH P/N 130-590031-71B10, rev. Feb 2007 (pg. 3-12)

 Definition

1.  Attitude/Heading Control – USE BACKUP INSTRUMENTS

2.  AC Bus Circuit Breakers (if tripped) - RESET
Term

DUAL GENERATOR FAILURE

[L DC GEN] and [R DC GEN]

(PL-21 with Keith Products ECS)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-11)

 Definition

1.  Instrument Emergency Lights (if required) – ON

1A. (With ISR mod)  MISSION POWER SWITCH – OFF

2.  Generators – 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
Term

DUAL GENERATOR FAILURE

[L DC GEN] and [R DC GEN]

(EFIS & PL-21 [with normal ECS])

Per POH P/N 130-590031-71B10, rev. Feb 2007 (pg. 3-11)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-11)

 Definition

1.  Instrument Emergency Lights (if required) – ON

1A. (With ISR mod)  MISSION POWER SWITCH – OFF

2.  Generators – RESET, THEN ON

 

If either generator will reset:

3.  Operating Generator Loadmeter – MONITOR

 

If neither generator will reset:

4.  Non-essential equipment – OFF
Term

USE OF OXYGEN

(EFIS)

Per POH P/N 130-590031-71B10, rev. Feb 2007 (pg. 3-17)

 Definition

1.  Oxygen Mask(s) – DON

2.  Headset(s) – DON, OR AUDIO SPEAKER(S) ON

3.  Mic Switch(es) - OXYGEN MASK

 
Term

USE OF OXYGEN

(PL-21)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-15)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-15)

 

 Definition

1.  Oxygen Mask(s) – DON

2.  Mic Switch(es) - OXY
Term

PRESURIZATION LOSS

[CABIN ALT HI]

(PL-21)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-17)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-17)

 

 Definition

1.  Oxygen Mask(s) – DON

2.  Mic Switch(es) – OXY

3.  Passenger Manual Drop-Out – PULL ON

[PASS OXYGEN ON] - ILLUMINATED

3.  Descend – AS REQUIRED

 
Term

HIGH DIFFERENTIAL PRESSURE

[CABIN DIFF HI]

(EFIS & PL-21)

Per POH P/N 130-590031-71B10, rev. Feb 2007 (pg. 3-17)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-17)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-17)

 

 

 Definition

1.  Bleed Air Valves – ENVIR OFF

2.  Oxygen (crew and passengers) – AS REQUIRED

3.  Descend - AS REQUIRED

 
Term

AUTO-DEPLOYMENT OXYGEN SYSTEM FAILURE

[CABIN ALT HI] ILLUMINATED

[PASS OXYGEN ON] EXTINGUISHED

(EFIS & PL-21)

Per POH P/N 130-590031-71B10, rev. Feb 2007 (pg. 3-17)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-17)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-17)

 Definition

1.Passenger Manual Drop-Out – PULL ON

 
Term

BLEED AIR FAIL

[L BLEED FAIL] or [R BLEED FAIL]

(EFIS & PL-21)

Per POH P/N 130-590031-71B10, rev. Feb 2007 (pg. 3-18)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-18)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-18)

 Definition

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

[L BLEED FAIL] or [R BLEED FAIL] – ILLUMINATED
Term

SPINS

(EFIS & PL-21)

Per POH P/N 130-590031-71B10, rev. Feb 2007 (pg. 3-19)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-19)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-19)

 

 Definition

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 a smooth pullout
Term

UNSCHEDULED ELECTRIC PITCH TRIM ACTIVATION

(EFIS)

Per POH P/N 130-590031-71B10, rev. Feb 2007 (pg. 3-16)

 

 Definition

1.Airplane Attitude – MAINTAIN USING ELEVATOR CONTROL

2.AP/Trim Disconnect – DEPRESS FULLY

[PITCH TRIM OFF] - ILLUMINATED
Term

UNSCHEDULED ELECTRIC PITCH TRIM ACTIVATION

(PL-21)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-19)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-19)

 

 Definition

1.Airplane Attitude – MAINTAIN USING ELEVATOR CONTROL

2.AP/Trim Disconnect – DEPRESS FULLY & HOLD

[TRIM] –ILLUMINATED
Term

UNSCHEDULED RUDDER BOOST ACTIVATION

(EFIS)

Per POH P/N 130-590031-71B10, rev. Feb 2007 (pg. 3-16)

 Definition

1.AP/Trim Disconnect – DEPRESS TO 1STLEVEL AND HOLD

2.Rudder Boost - OFF

 

If condition persists:

3.Rudder Boost circuit breaker – PULL

 
Term

UNSCHEDULED RUDDER BOOST ACTIVATION

(PL-21)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-20)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-20)

 Definition

1.AP/Trim Disconnect – DEPRESS TO 1STLEVEL AND HOLD

2.Rudder Boost - OFF

 

If condition persists:

3.YD/AP DISC (on Flight Guidance Panel) – PULL DOWN
Term

AUTOPILOT MISTRIM [E] OR [A]

(PL-21)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-20)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-20)

 Definition

1.Flight Controls – HOLD FIRMLY (Control forces may exceed 25 pounds)

2.A/P – DISENGAGE

 
Term

AUTOPILOT TRIM FAIL [TRIM]

(PL-21)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-21)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-21)

 

 Definition

1.Flight Controls – HOLD FIRMLY

2.A/P – DISENGAGE

 
Term

AUTOPILOT AUTOMATIC DISENGAGEMENT

(PL-21)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-22)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-22)

 Definition

1.Maintain airplane control

2.  AP/TRIM Disconnect – DEPRESS TO 1ST LEVEL TO CANCEL HORN

 

 
Term

ENHANCED GROUND PROXIMITY WARNING SYSTEM

(PL-21)

Per POH P/N 130-590031-181A3, rev. Apr 2006 (pg. 3-34)

Per POH P/N 130-590031-235A2, rev. May 2007 (pg. 3-34)

 

 Definition

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 20-25°.
  • Adjust as required to avoid continuous buffeting and/or stall warning.
  • Adjust to maintain 125 KIAS.

4.Gear and Flaps – UP
Term

PRESURIZATION LOSS

[CABIN ALT HI]

(EFIS)

Per POH P/N 130-590031-71B10, rev. Feb 2007 (pg. 3-18)

 

 Definition

1.Oxygen Mask(s) – DON

2.Headset(s) – DON OR AUDIO SPEAKER(S) ON

3.Mic Switch(es) – OXYGEN MASK

4.Passenger Manual Drop-Out – PULL ON

[PASS OXYGEN ON] - ILLUMINATED

5.Descend – AS REQUIRED

 
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