KING AIR
350-350C
(EFIS 85)
Revision 0.4
MEMORY FLASH CAR­­DS
Copyright © 2014, FlightSafety International, Inc.
Unauthorized reproduction or distribution is prohibited. All rights reserved.
NOTICE
These commodities, technology or software were exported from the
United States in accordance with the Export Administration Regulations.
Diversion contrary to U.S. law is prohibited.
INSERT LATEST REVISED CARDS, DESTROY SUPERSEDED CARDS
LIST OF EFFECTIV­E CARDS
Dates of issue for original
Original............0.......................... May 2006
Revision............01....................March 2008
Revision...........0.1............. November 2013
and changed pages are:
Revision...........0.2....................... May 2014
Revision...........0.3.................. August 2014
Revision...........0.4................. January 2016
TOTAL NUMBER OF CARDS IN THIS SET IS 72
CONSISTING OF THE FOLLOWING:
Card No.
*Revision
Title...............................................
ii—iv..............................................
E-1—E-4.......................................
E-4A..............................................
No.
0.3
0.3
0.3
0.4
Card No.
*Revision
E-5—E-13.....................................
E-14..............................................
E-14A—E-24A..............................
L-1—L-46A...................................
*Zero in this column indicates an original card.
Revision 0.3
FOR TRAINING PURPOSES ONLY
ii
No.
0.3
0.4
0.3
0.3
Active Index
ACTIVE INDEX
Section
Page
Emergency.............................................. E-1
START
Revision 0.3
Section
Page
Limitations............................................... L-1
King Air 350-350C (EFIS 85)
FOR TRAINING PURPOSES ONLY
iii
INTENTIONALLY LEFT BLANK
MENU RETURN
Revision 0.3
King Air 350-350C (EFIS 85)
FOR TRAINING PURPOSES ONLY
iv
Emergency
FAA Approved Airplane Flight Manual Supplement
Collins FCS-65 Automatic Flight Control System
(P/N 130-590031-19)
ENGINE FAILURE
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-1
FAA Approved Airplane Flight Manual Supplement
Collins FCS-65 Automatic Flight Control System
(P/N 130-590031-19)
ENGINE FAILURE
1.
2.
3.
4.
5.
Disengage autopilot.
Follow Pilot’s Operating Handbook engine failure procedures.
Retrim.
Re-engage autopilot.
Disengage autopilot for large power or airspeed variations.
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-1A
Emergency
ENGINE FIRE OR FAILURE IN FLIGHT
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-2
ENGINE FIRE OR FAILURE IN FLIGHT
Affected Engine:
1. Condition Lever.................................................... FUEL CUTOFF
2. Prop Lever......................................................................FEATHER
3. Firewall Fuel Valve............................................................. CLOSE
4. Fire Extinguisher (if fire warning persists)................. ACTUATE
[DISCHARGED] - ILLUMINATED
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-2A
Emergency
ENGINE FIRE ON GROUND
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-3
ENGINE FIRE ON GROUND
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
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-3A
Emergency
EMERGENCY ENGINE SHUTDOWN
ON THE GROUND
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-4
EMERGENCY ENGINE SHUTDOWN
ON THE GROUND
1.
2.
3.
4.
5.
Condition Levers................................................. FUEL CUTOFF
Prop Levers...................................................................FEATHER
Firewall Fuel Valves..........................................................CLOSE
Master Switch (gang bar)..................................................... OFF
Battery Bus..............................................................EMERG OFF
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.4
FOR TRAINING PURPOSES ONLY
E-4A
Emergency
ENGINE FAILURE DURING TAKEOFF
(AT OR BELOW V1)—TAKEOFF ABORTED
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-5
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)
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-5A
Emergency
ENGINE FAILURE DURING TAKEOFF
(AT OR ABOVE V1)—TAKEOFF CONTINUED
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-6
ENGINE FAILURE DURING TAKEOFF
(AT OR ABOVE V1)—TAKEOFF CONTINUED
1.
2.
3.
4.
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
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-6A
Emergency
ENGINE FAILURE IN FLIGHT BELOW AIR
MINIMUM CONTROL SPEED (VMCA)
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-7
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
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-7A
Emergency
ELECTRICAL SMOKE OR FIRE
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-8
ELECTRICAL SMOKE OR FIRE
1.
2.
3.
4.
Oxygen Mask(s).................................................................... DON
Mask Selector Switch...................................... EMERG Position
Headset(s)......................... DON, OR AUDIO SPEAKER(S)—ON
Mic Switch(es)................................................... OXYGEN MASK
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-8A
Emergency
ENVIRONMENTAL SYSTEM
SMOKE OR FUMES
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-9
ENVIRONMENTAL SYSTEM
SMOKE OR FUMES
1.
2.
3.
4.
Oxygen Mask(s).................................................................... DON
Mask Selector Switch...................................... EMERG Position
Headset(s)......................... DON, OR AUDIO SPEAKER(S)—ON
Mic Switch(es)................................................... OXYGEN MASK
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-9A
Emergency
AIRSTAIR DOOR/CARGO
DOOR UNLOCKED
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-10
AIRSTAIR DOOR/CARGO
DOOR UNLOCKED
1. All Occupants............................................... SEATED WITH SEAT
BELTS SECURELY FASTENED
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-10A
Emergency
EMERGENCY DESCENT
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-11
EMERGENCY DESCENT
1.
2.
3.
4.
5.
Power Levers........................................................................ IDLE
Prop Lever........................................................ FULL FORWARD
Flaps (202 knots maximum).....................................APPROACH
Landing Gear (184 knots maximum)................................DOWN
Airspeed................................................. 184 KNOTS MAXIMUM
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-11A
Emergency
GLIDE
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-12
GLIDE
1. Landing Gear........................................................................... UP
2. Flaps......................................................................................... UP
Do not feather second engine propeller if a
No Starter Assist Air Start is to be conducted.
3. Prop Levers..............................................................FEATHERED
4. Airspeed.....................................................................135 KNOTS
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-12A
Emergency
SINGLE INVERTER FAILURE
OR
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-13
SINGLE INVERTER FAILURE
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
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-13A
Emergency
DUAL INVERTER FAILURE
AND
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.4
FOR TRAINING PURPOSES ONLY
E-14
DUAL INVERTER FAILURE
1. Attitude/Heading Control.......... USE BACKUP INSTRUMENTS
2. AC Bus Circuit Breakers (if tripped)............................... RESET
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-14A
Emergency
DUAL GENERATOR FAILURE
AND
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-15
DUAL GENERATOR FAILURE
1. Instrument Emergency Lights (if required)...........................ON
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
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-15A
Emergency
UNSCHEDULED ELECTRIC
PITCH TRIM ACTIVATION
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-16
UNSCHEDULED ELECTRIC
PITCH TRIM ACTIVATION
1. Airplane Attitude.......MAINTAIN USING ELEVATOR CONTROL
2. AP/Trim Disconnect........................................ DEPRESS FULLY
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-16A
Emergency
UNSCHEDULED RUDDER
BOOST ACTIVATION
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-17
UNSCHEDULED RUDDER
BOOST ACTIVATION
1. AP/Trim Disconnect...... DEPRESS TO 1ST LEVEL AND HOLD
2. Rudder Boost......................................................................... OFF
If Condition Persists:
3. Rudder Boost Circuit Breaker............................................PULL
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-17A
Emergency
USE OF OXYGEN
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-18
USE OF OXYGEN
Crew
1. Oxygen Mask(s).................................................................... DON
2. Headset(s)............................ DON, OR AUDIO SPEAKER(S) ON
3. Mic Switch(es)................................................... OXYGEN MASK
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-18A
Emergency
PRESSURIZATION LOSS
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-19
PRESSURIZATION LOSS
1.
2.
3.
4.
5.
Oxygen Mask(s).................................................................... DON
Headset(s)............................ DON, OR AUDIO SPEAKER(S) ON
Mic Switch(es)................................................... OXYGEN MASK
Passenger Manual Drop-Out....................................... PULL ON
Descend............................................................... AS REQUIRED
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-19A
Emergency
HIGH DIFFERENTIAL PRESSURE
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-20
HIGH DIFFERENTIAL PRESSURE
1. Bleed Air Valves.......................................................... ENVIR OFF
2. Oxygen (crew and passengers)............................AS REQUIRED
3. Descend.................................................................AS REQUIRED
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-20A
Emergency
AUTODEPLOYMENT OXYGEN
SYSTEM FAILURE
AND
ILLUMINATED
EXTINGUISHED
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-21
AUTODEPLOYMENT OXYGEN
SYSTEM FAILURE
1. Passenger Manual Drop-Out....................................... PULL ON
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-21A
Emergency
BLEED AIR FAIL
OR
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-22
BLEED AIR FAIL
1. Bleed Air Valve (affected engine)................PNEU & ENVIR OFF
[L BL AIR OFF] or [R BL AIR OFF] - ILLUMINATED
NOTE
The BLEED FAIL annunciator will not extinguish after
closing the Bleed Air Valve.
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-22A
Emergency
SPINS
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-23
SPINS
1.
2.
3.
4.
5.
Control Column......... FULL FORWARD, AILERONS NEUTRAL
Full Rudder..................... OPPOSITE THE DIRECTION OF SPIN
Power Levers........................................................................ IDLE
Rudder........................ NEUTRALIZE WHEN ROTATION STOPS
Execute a smooth pullout.
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-23A
Emergency
ENHANCED GROUND PROXIMITY
WARNING SYSTEM (EGPWS)
Continuous “PULL UP, PULL UP” Voice Warning
Or
“TERRAIN, TERRAIN, PULL UP” or “OBSTACLE,
OBSTACLE, PULL UP” Voice Warning
AND
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-24
ENHANCED GROUND PROXIMITY
WARNING SYSTEM (EGPWS)
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
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
E-24A
Limitations
AIRSPEED LIMITATIONS
Maneuvering Speed VA
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-1
AIRSPEED LIMITATIONS
Maneuvering Speed VA
184 KIAS
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-1A
Limitations
AIRSPEED LIMITATIONS
Maximum Flap Extension/Extended Speed (VFE)
Approach ............................................................................................... ?
Full Down .............................................................................................. ?
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-2
AIRSPEED LIMITATIONS
Maximum Flap Extension/Extended Speed (VFE)
Approach ................................................................................. 202 KIAS
Full Down ................................................................................ 158 KIAS
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-2A
Limitations
AIRSPEED LIMITATIONS
Maximum Landing Gear Operating Speed (VLO)
Extension ............................................................................................... ?
Retraction .............................................................................................. ?
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-3
AIRSPEED LIMITATIONS
Maximum Landing Gear Operating Speed (VLO)
Extension ................................................................................. 184 KIAS
Retraction ................................................................................ 166 KIAS
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-3A
Limitations
AIRSPEED LIMITATIONS
Maximum Landing Gear Extended Speed (VLE)
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-4
AIRSPEED LIMITATIONS
Maximum Landing Gear Extended Speed (VLE)
184 KIAS
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-4A
Limitations
AIRSPEED LIMITATIONS
Air Minimum Control Speed (VMCA)
(Propeller Feathered)
Flaps Up ................................................................................................ ?
Flaps Approach ..................................................................................... ?
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-5
AIRSPEED LIMITATIONS
Air Minimum Control Speed (VMCA)
(Propeller Feathered)
Flaps Up .................................................................................... 94 KIAS
Flaps Approach ......................................................................... 93 KIAS
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-5A
Limitations
AIRSPEED LIMITATIONS
Maximum Operating Speed (VMO)
Sea Level to 21,000 feet ....................................................................... ?
21,000 to 35,000 feet ............................................................................ ?
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-6
AIRSPEED LIMITATIONS
Maximum Operating Speed (VMO)
Sea Level to 21,000 feet .......................................................... 263 KIAS
21,000 to 35,000 feet ...................................................... 263–194* KIAS
(* 0.58 MACH)
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-6A
Limitations
POWER LEVERS
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-7
POWER LEVERS
Do not lift power levers in flight. Lifting the power levers in flight, or
moving the power levers in flight below the flight idle position, could
result in a nose-down pitch and a descent rate leading to aircraft
damage and injury to personnel.
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-7A
Limitations
ENGINE OPERATING LIMITS
% Torque
Takeoff ................................................................................................... ?
Max Continuous .................................................................................... ?
Transient ................................................................................................ ?
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-8
ENGINE OPERATING LIMITS
% Torque
Takeoff ........................................................................................... 100%
Max Continuous ............................................................................ 100%
Transient ....................................................... 156% FOR 20 SECONDS
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-8A
Limitations
ENGINE OPERATING LIMITS
Maximum ITT Temp (°C)
Starting ..................................................................................................
Idle ........................................................................................................
Takeoff ...................................................................................................
Max Continuous ....................................................................................
Transient ................................................................................................
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-9
?
?
?
?
?
ENGINE OPERATING LIMITS
Maximum ITT Temp (°C)
Starting ......................................................... 1000°C FOR 5 SECONDS
Idle ............................................................................................... 750°C
Takeoff .......................................................................................... 820°C
Max Continuous ........................................................................... 820°C
Transient ....................................................... 850°C FOR 20 SECONDS
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-9A
Limitations
ENGINE OPERATING LIMITS
Gas Generator RPM (% N1)
Minimum Idle .........................................................................................
Takeoff ...................................................................................................
Max Continuous ....................................................................................
Transient ................................................................................................
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-10
?
?
?
?
ENGINE OPERATING LIMITS
Gas Generator RPM (% N1)
Minimum Idle ................................................................................... 62%
Takeoff ........................................................................................... 104%
Max Continuous ............................................................................ 104%
Transient ........................................................................................ 104%
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-10A
Limitations
ENGINE OPERATING LIMITS
Propeller RPM (N2)
Takeoff .................................................................................................... ?
Max Continuous ..................................................................................... ?
Transient ................................................................................................. ?
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-11
ENGINE OPERATING LIMITS
Propeller RPM (N2
Takeoff .................................................................................... 1700 RPM
Max Continuous ..................................................................... 1700 RPM
Transient ................................................. 1870 RPM FOR 20 SECONDS
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-11A
Limitations
ENGINE OPERATING LIMITS
Oil Pressure (PSI)
Starting ...................................................................................................
Takeoff ....................................................................................................
Max Continuous .....................................................................................
Transient .................................................................................................
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-12
?
?
?
?
ENGINE OPERATING LIMITS
Oil Pressure (PSI)
Starting ..................................................................................... 0–200
Takeoff .................................................................................... 90–135
Max Continuous ..................................................................... 90–135
Transient ....................................................................................... 200
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-12A
psi
psi
psi
psi
Limitations
ENGINE OPERATING LIMITS
Oil Temperature (°C)
Starting ...................................................................................................
Takeoff ....................................................................................................
Max Continuous .....................................................................................
Transient .................................................................................................
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-13
?
?
?
?
ENGINE OPERATING LIMITS
Oil Temperature (°C)
Starting ......................................................................... –40°C (minimum)
Takeoff ......................................................................................... 0–110°C
Max Continuous .......................................................................... 0–110°C
Transient ...................................................................................... 0–110°C
Temperatures between 99°C and 110°C are
limited to a maximum of 10 minutes.
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-13A
Limitations
EXTERNAL POWER LIMITS
Volts ....................................................................................................... ?
Amps ..................................................................................................... ?
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-14
EXTERNAL POWER LIMITS
Volts ................................................................................ 28.0–28.4 Volts
Amps .............................................................. 1000 Amps (Momentary)
300 Amps (Continuous)
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-14A
Limitations
GENERATOR LIMITS
Maximum Generator Load In Flight
Sea Level to 34,000 feet altitude ........................................................... ?
Above 34,000 feet altitude ..................................................................... ?
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-15
GENERATOR LIMITS
Maximum Generator Load In Flight
Sea Level to 34,000 feet altitude ................................................... 100%
Above 34,000 feet altitude ............................................................... 95%
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-15A
Limitations
GENERATOR LIMITS
Maximum Load Ground Operation
62–70% N1 ............................................................................................ ?
70–100% N1 .......................................................................................... ?
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-16
GENERATOR LIMITS
Maximum Load Ground Operation
62–70% N1 ...................................................................................... 75%
70–100% N1 .................................................................................. 100%
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-16A
Limitations
STARTER LIMITS
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-17
STARTER LIMITS
30 seconds ON
5 minutes OFF
30 seconds ON
5 minutes OFF
30 seconds ON
30 minutes OFF
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-17A
Limitations
FUEL LIMITS
Approved Engine Fuels............................................................................?
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-18
FUEL LIMITS
Approved Engine Fuels..............................................................................
COMMERCIAL GRADES............................... Jet A, Jet A-1, Jet B,
MILITARY GRADES .............................................. JP-4, JP-5, JP-8
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-18A
Limitations
EMERGENCY ENGINE FUEL LIMITS
Limitations on the use of Aviation Gasoline
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-19
EMERGENCY ENGINE FUEL LIMITS
Limitations on the use of Aviation Gasoline
1. Operation is limited to 150 hours between engine overhauls.
2. Operation is prohibited if either standby fuel pump
is inoperative.
3. Crossfeed capability is required for flight above 20,000 feet
pressure altitude (FL200).
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-19A
Limitations
FUEL MANAGEMENT
Usable Fuel (Gallons x 6.7=lb)
Total Usable Fuel Quantity ..................................................................... ?
Each Main Fuel Tank System ................................................................. ?
Each Auxiliary Fuel Tank ........................................................................ ?
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-20
FUEL MANAGEMENT
Usable Fuel (Gallons x 6.7=lb)
Total Usable Fuel Quantity .......................... 539 gal/2040 liter (3611 lb)
Each Main Fuel Tank System ........................ 190 gal/719 liter (1273 lb)
Each Auxiliary Fuel Tank ................................ 79.5 gal/301 liter (533 lb)
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-20A
Limitations
FUEL MANAGEMENT
Fuel Imbalance
Maximum allowable fuel imbalance
between wing fuel systems .................................................................... ?
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-21
FUEL MANAGEMENT
Fuel Imbalance
Maximum allowable fuel imbalance
between wing fuel systems ........................................................... 300 lb
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-21A
Limitations
FUEL MANAGEMENT
Fuel Crossfeed
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-22
FUEL MANAGEMENT
Fuel Crossfeed
Crossfeeding of fuel is permitted only when one engine is inoperative.
WARNING
One operative standby fuel pump is required for takeoff when using approved engine
fuels, but in such a case, crossfeed of fuel will not be available from the side of the
inoperative standby fuel pump. Two operative standby fuel pumps are required for
takeoff when operating on emergency engine fuels.
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-22A
Limitations
FUEL MANAGEMENT
Fuel Gages in the Yellow Arc
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-23
FUEL MANAGEMENT
Fuel Gages in the Yellow Arc
Do not take off if fuel quantity gages indicate in yellow
arc or indicate less than 265 lbs (120 Kg) of fuel in each
wing system.
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-23A
Limitations
FUEL MANAGEMENT
Auxiliary Fuel
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-24
FUEL MANAGEMENT
Auxiliary Fuel
Do not put any fuel into the auxiliary tanks unless the
main tanks are full.
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-24A
Limitations
FUEL MANAGEMENT
Operating with Low Fuel Pressure
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-25
FUEL MANAGEMENT
Operating with Low Fuel Pressure
Operation of either engine with its corresponding fuel pressure
annunciator (L FUEL PRES LO or R FUEL PRES LO) illuminated
is limited to 10 hours before overhaul or replacement of
the engine-driven fuel pump. Windmilling time need not be
charged against this limit.
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-25A
Limitations
PROPELLER ROTATIONAL SPEED LIMITS
Transients not exceeding 20 seconds.....................................................?
Reverse....................................................................................................?
All other conditions..................................................................................?
Minimum idle speed.................................................................................?
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-26
PROPELLER ROTATIONAL SPEED LIMITS
Transients not exceeding 20 seconds.......................................1870
Reverse......................................................................................1650
All other conditions....................................................................1700
Minimum idle speed...................................................................1050
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-26A
rpm
rpm
rpm
rpm
Limitations
PROPELLER ROTATIONAL
OVERSPEED LIMITS
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-27
PROPELLER ROTATIONAL
OVERSPEED LIMITS
Sustained propeller overspeeds faster than 1700 rpm indicate
failure of the primary governor. Flight may be continued at
propeller overspeeds up to 1768 rpm, provided torque is
limited to 96%. Sustained propeller overspeeds faster than
1768 rpm indicate failure of both the primary governor and the
secondary governor, and such overspeeds are not approved.
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-27A
Limitations
PROPELLER AUTOFEATHER
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-28
PROPELLER AUTOFEATHER
The propeller autofeather system must be operable for
all flights and must be armed for takeoff, climb, approach
and landing.
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-28A
Limitations
CABIN DIFFERENTIAL PRESSURE GAGE
Green Arc (Normal Operating Range)......................................................?
Red Arc (Unapproved Operating Range).................................................?
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-29
CABIN DIFFERENTIAL PRESSURE GAGE
Green Arc (Normal Operating Range)..........................................0–6.6 psi
Red Arc (Unapproved Operating Range).................................... 6.6 psi to
end of scale
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-29A
Limitations
PNEUMATIC PRESSURE GAGE
Green Arc (Normal Operating Range) .................................................... ?
Red Arc (Maximum Operating Range) ................................................... ?
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-30
PNEUMATIC PRESSURE GAGE
Green Arc (Normal Operating Range) ...................................... 12–20 psi
Red Arc (Maximum Operating Range) ........................................... 20 psi
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-30A
Limitations
VACUUM GAGE
Narrow Green Arc
(Normal from 35,000–15,000 ft)..............................................................
Wide Green Arc
(Normal from 15,000 ft to Sea Level)......................................................
35K marked on face of gage at..............................................................
15K marked on face of gage at..............................................................
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-31
?
?
?
?
VACUUM GAGE
Narrow Green Arc
(Normal from 35,000–15,000 ft)......................................... 2.8–4.3
Wide Green Arc
(Normal from 15,000 ft to Sea Level)................................. 4.3–5.9
35K marked on face of gage at................................................ 3.0
15K marked on face of gage at................................................ 4.3
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
in. Hg
in. Hg
in. Hg
in. Hg
L-31A
Limitations
PROPELLER DEICE AMMETER
Green Arc (Normal Operating Range)..................................................... ?
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-32
PROPELLER DEICE AMMETER
Green Arc (Normal Operating Range).................................. 26–32 amps
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-32A
Limitations
WEIGHT LIMITS
Maximum
Maximum
Maximum
Maximum
Zero Fuel Weight ...................................................................
Ramp Weight .........................................................................
Landing Weight .....................................................................
Takeoff Weight .......................................................................
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-33
?
?
?
?
WEIGHT LIMITS
Maximum
Maximum
Maximum
Maximum
Zero Fuel Weight .......................................................12,500
Ramp Weight ........................................................... 15,100
Landing Weight ....................................................... 15,000
Takeoff Weight ......................................................... 15,000
Or as limited by Performance Limitations:
1. Max T/O Weight to Achieve T/O Climb Requirements.
2. Max T/O Weight as Limited by Tire Speed.
3. Take-off Field Length.
For 14CFR Part 135 Operations:
Take-off Flight Path Requirements to 1500 ft AGL
Service Ceiling—One Engine Inoperative
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-33A
lb
lb
lb
lb
Limitations
WEIGHT LIMITS
Maximum Weight in Baggage Compartment
B300:
When Equipped With Fold-up Seats......................................................
When Not Equipped With Fold-up Seats................................................
B300C:
When Equipped With Toilet and Fold-up Seat........................................
When Equipped With Toilet.....................................................................
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-34
?
?
?
?
WEIGHT LIMITS
Maximum Weight in Baggage Compartment
B300:
When Equipped With Fold-up Seats............................................
When Not Equipped With Fold-up Seats......................................
B300C:
When Equipped With Toilet and Fold-up Seat..............................
When Equipped With Toilet...........................................................
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
510 lbs
550 lbs
510 lbs
550 lbs
L-34A
Limitations
MANEUVER LIMITS
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-35
MANEUVER LIMITS
The Models B300 and B300C are Commuter Category
Airplanes. Acrobatic maneuvers, including spins, are
prohibited.
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-35A
Limitations
FLIGHT LOAD FACTOR LIMITS
FLAPS UP
? positive Gs
? negative Gs
FLAPS DOWN
? positive Gs
? negative G
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-36
FLIGHT LOAD FACTOR LIMITS
FLAPS UP
3.1 positive Gs
1.24 negative Gs
FLAPS DOWN
2.0 positive Gs
0.00 G
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-36A
Limitations
MAXIMUM OPERATING ALTITUDE LIMITS
Normal Operation.....................................................................................?
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-37
MAXIMUM OPERATING ALTITUDE LIMITS
Normal Operation........................................................................ 35,000 ft
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-37A
Limitations
MAXIMUM OPERATING ALTITUDE LIMITS
Yaw Damp System
Inoperative .............................................................................................. ?
Operative ................................................................................................ ?
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-38
MAXIMUM OPERATING ALTITUDE LIMITS
Yaw Damp System
Inoperative ................................................................................... 5000 ft*
Operative .................................................................... On above 5000 ft,
except for takeoff and landing*
* If Dual Aft Body Strakes are installed, refer to STC
Supplement 91-111.
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-38A
Limitations
MAXIMUM OPERATING ALTITUDE LIMITS
Operation with Aviation Gasoline
Both Standby Fuel Pumps Operative......................................................?
Either Standby Fuel Pump Inoperative....................................................?
Climbs Without Crossfeed Capability......................................................?
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-39
MAXIMUM OPERATING ALTITUDE LIMITS
Operation with Aviation Gasoline
Both Standby Fuel Pumps Operative......................................... 35,000 ft
Either Standby Fuel Pump Inoperative..........................Flight prohibited
Climbs Without Crossfeed Capability......................................... 20,000 ft
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-39A
Limitations
MAXIMUM OPERATING AIR
TEMPERATURE LIMITS
Sea Level to 25,000 ft pressure altitude..................................................?
Above 25,000 ft pressure altitude............................................................?
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-40
MAXIMUM OPERATING AIR
TEMPERATURE LIMITS
Sea Level to 25,000 ft pressure altitude................................. ISA + 37°C
Above 25,000 ft pressure altitude........................................... ISA + 31°C
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-40A
Limitations
RUDDER BOOST
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-41
RUDDER BOOST
Must be operational for all flights.
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-41A
Limitations
LANDING GEAR CYCLE LIMITS
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-42
LANDING GEAR CYCLE LIMITS
Landing gear cycles (1 Up—1 Down) are limited to one
every 5 minutes for a total of 6 cycles, followed by a
15 minute cool-down period.
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-42A
Limitations
ICING LIMITATIONS
Minimum Ambient Temperature
for Operation of Deicing Boots .............................................................. ?
Minimum Airspeed for Sustained Icing Flight ........................................ ?
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-43
ICING LIMITATIONS
Minimum Ambient Temperature
for Operation of Deicing Boots ...................................................... –40°C
Minimum Airspeed for Sustained Icing Flight ......................... 140 knots
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-43A
Limitations
AFT-FACING SEATS
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-44
AFT-FACING SEATS
The seat back of each occupied aft-facing seat must be
in the upright position and the headrest fully extended for
takeoff and landing.
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-44A
Limitations
AUTOPILOT
Maximum speed limit for autopilot operation..........................................?
Do not use autopilot below the following altitudes:
Cruise.......................................................................................................?
Approach..................................................................................................?
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-45
AUTOPILOT
Maximum speed limit forautopilot operation............... Unchanged from
airplane maximum airspeed limit (VMO/MMO)
Do not use autopilot below the following altitudes:
Cruise........................................................... 1000 ft above ground level
Approach........................................................ 200 ft above ground level
Do not use autopilot or yaw damper during takeoff or landing.
Pilot must be seated at the controls with the seat belt fastened during
autopilot operations.
Autopilot preflight check must be conducted and found satisfactory prior
to each flight on which the autopilot is to be used.
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-45A
Limitations
EFIS
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-46
EFIS
1. The pilot EADI and EHSI must be operational in the normal
mode for takeoff. Auxiliary Drive may be used if the Primary Drive
has failed.
2. The composite mode is to be used only after failure of an
EADI or EHSI.
3. The Airspeed readout is not to be used as the primary reference.
MENU RETURN
King Air 350-350C (EFIS 85)
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-46A