SeaPort Airlines, Inc.
SeaPort Airlines, Inc.
Cessna 208 Series
Cessna 208 Series
EMERGENCY CHECKLIST
START MALFUNCTIONS
EMERGENCY CHECKLIST
ENGINE FAILURES
ENGINE FIRE DURING START ON
GROUND (ENGINE FIRE
Annunciator)
Condition ........................................... Cutoff
Boost Pump ............................................. Off
APU ............................................. Disconnect
External Power Switch ............................. Off
Starter ................................................. Motor
Starter ...................................................... Off
Fuel Shutoff ...................................... Pull Off
Battery ..................................................... Off
Airplane ..........................................Evacuate
Fire ................................................Extinguish
HOT START
Condition ........................................... Cutoff
Starter ................................................. Motor
HUNG START
Condition ........................................... Cutoff
Starter ................................................. Motor
IGNITION FAILURE
Condition ........................................... Cutoff
Starter ................................................. Motor
Starter ...................................................... Off
Battery ..................................................... Off
STARTER CONTACTOR DOES NOT
DISENGAGE AFTER ENGINE START
(STARTER ENERGIZED Annunciator
On)
Battery .................................................... Off
APU ..................................... Off & Disengage
Condition ............................................ Cutoff
Engine Shutdown ...........................Complete
ENGINE FAILURES (Con’t)
ENGINE FAILURE DURING TAKEOFF
ROLL
Power .................................................... Beta
Brakes .................................................. Apply
Flaps.................................................. Retract
If airplane cannot be stopped on
remaining runway
Condition ............................................ Cutoff
Fuel Shutoff ...................................... Pull Off
Fuel Selectors ................................. Both Off
Battery ..................................................... Off
ENGINE FAILURE IMMEDIATELY
AFTER TAKEOFF
o
Airspeed....................... 85 KIAS w/ 20 Flaps
Prop ..................................... Feather or Max
Flaps........................................................ A/R
Condition ............................................ Cutoff
Fuel Shutoff ...................................... Pull Off
Fuel Selectors ................................. Both Off
Battery ..................................................... Off
ENGINE FAILURE DURING FLIGHT
Airspeed................... Max Glide (95-71 KIAS)
Power ..................................................... Idle
Prop .................................................. Feather
Condition ............................................ Cutoff
Flaps.......................................................... Up
Boost Pump ............................................. Off
Fuel Shutoff ...................................... Pull Off
Ignition................................................. Norm
Standby Power......................................... Off
Electrical Load ................................... Reduce
Landing .................... Refer to Emer. Landing
........................................ w/o Engine Power
Page 1 of 12
Revised: 11/25/2011
ENGINE FLAMEOUT DURING
FLIGHT
If Ng is above 50%
Power ..................................................... Idle
Ignition...................................................... On
Power .......................................... As Desired
If zero fuel flow & low ITT, go to Engine
Failure Procedure
Fuel Flow .................................... 80-110 pph
Ignition ........................... Norm if Cause of
....................... Flameout has been corrected
If Ng is below 50%
Condition ............................................ Cutoff
Engine ............................................... Restart
AIRSTART STARTER ASSIST
Fuel Selectors .................................. Both On
Bleed Air Heat .......................................... Off
Condition ............................................ Cutoff
Prop ........................................................ Min
Power ..................................................... Idle
Emer. Power ..................................... Normal
Fuel Shutoff ............................................... In
Trim .................................. Desired Airspeed
Forward Switch Panel ......................... All Off
Battery ...................................................... On
Boost Pump .............................................. On
Standby Power......................................... Off
Ignition................................................. Norm
Avionics .................................................. A/R
Altitude .................................. 20,000 ft. Max
Starter ................................................... Start
Ng ...................................Stabilized 12% min
Condition ......................................... Low Idle
Starter ...................................................... Off
Condition ........................................ High Idle
Boost Pump ......................................... Norm
Page 2 of 12
ENGINE FAILURES (Con’t)
Prop ....................................................... Max
Power .......................................... As Desired
Standby Power ......................................... On
Electrical Equipment ............................... A/R
WINDMILLING AIRSTART
Airspeed .................................. 100 KIAS min
......................... (140 KIAS if prop feathered)
Generator ............................................... Trip
Standby Power ........................................ Off
Avionics .................................................. A/R
Emer. Power ..................................... Normal
Power ..................................................... Idle
Prop ........................................................ Min
Condition ............................................ Cutoff
Bleed Air Heat .......................................... Off
Fuel Shutoff .............................................. On
Fuel Selectors .................................. Both On
Battery ...................................................... On
Boost Pump .............................................. On
Ignition ..................................................... On
Do not attempt a restart w/o starter
assist if Ng indicates zero
Ng ............................................................. +0
Condition ......................................... Low Idle
Condition ........................................ High Idle
Prop ....................................................... Max
Power .......................................... As Desired
Ignition ....................................... Remain On
Generator ............................................ Reset
Electrical Equipment ............................... A/R
Revised: 11/25/2011
SeaPort Airlines, Inc.
SeaPort Airlines, Inc.
Cessna 208 Series
Cessna 208 Series
EMERGENCY CHECKLIST
ENGINE FAILURES (Con’t)
EMERGENCY CHECKLIST
ENGINE FAILURES (Con’t)
FORCED LANDING
EMERGENCY LANDING W/O
ENGINE POWER
Seat Belts, Shldr Harnesses .............. Secured
Airspeed................... Max Glide (95-71 KIAS)
Fuel Selectors ................................. Both Off
Power ..................................................... Idle
Prop ............................................. As Desired
Condition ............................................ Cutoff
Fuel Shutoff ...................................... Pull Off
Boost Pump ............................................. Off
Ignition................................................. Norm
Standby Power......................................... Off
Non-Essential Equipment ........................ Off
Flaps........................................................ A/R
Crew Doors ...................................Unlatched
Radio ................................. Mayday on 121.5
ELT .................................................. Press On
Battery ..................................................... Off
Generator ............................................... Trip
Standby Power......................................... Off
Touchdown ......................... Slightly Tail Low
Power ............................. Beta then Reverse
Condition ............................................ Cutoff
Brakes ..................................... Apply Heavily
DITCHING
Seat Belts, Shldr Harnesses .............. Secured
Heavy Objects in Cabin ...................... Secure
Flaps........................................................ Full
Airspeed......................... 80 KIAS w/300 fpm
Crew Doors ...................................Unlatched
Radio ................................. Mayday on 121.5
ELT .................................................. Press On
Approach
High Winds ............................. Into the Wind
Light Winds, Hvy Swell ...................... Parallel
....................................................... To Swells
Face ......................... Cushion at Touchdown
Touchdown ...................................... No Flare
Airplane ..........................................Evacuate
Life Vests .................... Inflate Outside Cabin
SMOKE AND FIRE
SMOKE AND FIRE (Con’t)
ENGINE FIRE IN FLIGHT (ENGINE
FIRE Annunciator)
Fire Detection C/B (#32) ......................... Pull
Cabin Heat Firewall Shutoff .............. Pull Off
Engine Fire ........................ Verify Actual Fire
At pilot’s discretion
Power ..................................................... Idle
Prop .................................................. Feather
Condition ............................................ Cutoff
Fuel Shutoff ...................................... Pull Off
Side Vents ............................................. Close
Overhead Vents ................................... Open
Ventilation Fans ........................................ On
o
o
Flaps.................................................. 20 -30
Airspeed....................................... 80-85 KIAS
Forced Landing .................................Execute
ELECTRICAL FIRE
PRECAUTIONARY LANDING WITH
ENGINE POWER
Battery ..................................................... Off
Standby Power......................................... Off
Generator ............................................... Trip
Vents ...................................................Closed
Bleed Air Heat .......................................... Off
Fire Extinguisher .............................. Activate
Avionics ................................................... Off
All Other Electrical Switches .................... Off
On Final
Flaps........................................................ Full
Airspeed............................................ 80 KIAS
Crew Doors ...................................Unlatched
Radio ................................. Mayday on 121.5
ELT .................................................. Press On
If fire appears out and electrical power
is necessary for continuance of flight
Battery ...................................................... On
Standby Power.......................................... On
Generator ............................................ Reset
Circuit Breakers ................................... Check
Radios ...................................................... Off
Avionics .................................................... On
Radio & Electrical Switches ............... On one
..................................... at a time, with delay
Vents .................................................... Open
Bleed Air Heat .............................. As Desired
When landing assured
Battery ..................................................... Off
Touchdown ......................... Slightly Tail Low
Brakes ..................................... Apply Heavily
Seat Belts, Shldr Harnesses .............. Secured
o
Flaps......................................................... 10
Airspeed............................................ 90 KIAS
Select Field....................................... Fly Over
All Electrical Switches .............................. Off
....................... (except Battery & Generator)
Page 3 of 12
Revised: 11/25/2011
CABIN FIRE
In Flight
Battery ..................................................... Off
Standby Power ........................................ Off
Generator ............................................... Trip
Vents................................................... Closed
Bleed Air Heat .......................................... Off
Fire Extinguisher .............................. Activate
Land .............................. As Soon As Possible
During Ground Operations
Power ..................................................... Idle
Brakes ..................................................... A/R
Prop .................................................. Feather
Condition ............................................ Cutoff
Battery ..................................................... Off
Airplane .......................................... Evacuate
Fire ................................................ Extinguish
WING FIRE
Pitot/Static Heat ...................................... Off
Stall Heat ................................................. Off
Strobes..................................................... Off
Navigation Lights ..................................... Off
Landing & Taxi Lights ............................... Off
Radar ....................................................... Off
Ventilation Fans ....................................... Off
Page 4 of 12
Revised: 11/25/2011
SeaPort Airlines, Inc.
SeaPort Airlines, Inc.
Cessna 208 Series
Cessna 208 Series
EMERGENCY CHECKLIST
LANDING GEAR MALFUNCTIONS
LANDING WITH FLAT MAIN TIRE
Airplane .................. Fly to Lighten Fuel Load
Fuel Selectors ............... Lighten Side w/ Flat
Approach .......................................... Normal
Touchdown ....................... Inflated Tire First
Directional Control ............... Maintain using
.................. Brake on Wheel w/ Inflated Tire
LANDING WITH FLAT NOSE TIRE
Passengers & Baggage ................... Move Aft
Approach .......................................... Normal
Touchdown ................................... Nose High
Brakes ........................................... Minimum
EMERGENCY CHECKLIST
ICING
INADVERTENT ICING ENCOUNTER
AT WEIGHTS ABOVE 8550 POUNDS
Ignition...................................................... On
Inertial Separator ............................... Bypass
Pitot/Static, Stall, W/S, & Prop Anti-ice .... On
Altitude/Course ................................ Change
Boot Pressure ............... Auto & Release A/R
INADVERTENT ICING ENCOUNTER
AT ALT. ABOVE 20,000 FT
Ignition...................................................... On
Inertial Separator ............................... Bypass
Pitot/Static, Stall, W/S, & Prop Anti-ice .... On
Airspeed.................................. 160 KIAS Max
Altitude ................ Descend below 20,000 ft.
Boot Pressure ............... Auto & Release A/R
Ignition.................................. Off after 5 min
Operate in accordance with NORMAL
PROCEDURES
Do not climb above 20,000 ft. with any
residual ice on the airplane, regardless of
atmospheric conditions
INERTIAL SEPARATOR
MALFUNCTION
Inertial Separator ............................... Bypass
Engine Torque............... Monitor (for Proper
.......................... ops by noting torque drop)
If Inertial Separator fails to operate to
the BYPASS mode:
Ignition...................................................... On
Icing Conditions ................. Exit Immediately
ICING (Con’t)
ICING (Con’t)
PROPELLER ANTI-ICE SYSTEM
MALFUNCTION
If uneven anti-icing of the propeller
blades is indicated by excessive
vibration:
Prop Control Lever ............... Cycle then Max
Prop Anti-Ice C/B’s ........................ Pushed In
Prop Anti-Ice Ammeter ........................ Check
............... Should indicate 20-24 amps for 90
.......................... sec, then 0 amps for 90 sec
If ammeter continuously indicates 0
amps:
Prop Anti-Ice ........................... Verify AUTO
If ammeter still indicates 0 amps:
Prop Anti-Ice ......................Manual and hold
............................ for 90 sec, then 90 sec off,
................................................... then repeat
Icing Conditions ................... Exit as Practical
If ammeter still indicates 0 amps:
Icing Conditions ................. Exit Immediately
Note: Low Airspeed Awareness system will
be inoperative
If ammeter reading is below the green
arc:
Prop Anti-Ice ............................................ Off
Prop Control Lever ............................ Cycle at
......................................... frequent intervals
Icing Conditions ................. Exit Immediately
PNEUMATIC DE-ICE BOOT
MALFUNCTION
The de-ice pressure annunciator should
illuminate 3 times, approx. 3 seconds each
time, during the 18-second cycle
De-ice Boot C/B ............................ Pushed In
Suction Gage ........................................ Check
Page 5 of 12
Revised: 11/25/2011
Page 6 of 12
If suction is below normal and/or there
is an audible leak in the forward cabin
or left wing root area, expect a broken
engine bleed-air line and:
Icing Conditions ................. Exit Immediately
If suction is normal:
Boot Pressure .................... Manual for 9 sec
Leading Edges ..................... Visually observe
................... for simultaneous inflation of all
............................ visible leading edge boots
De-Ice Annunciator ............. Observe (should
................. illuminate within 6 seconds after
......................... activating BOOT PRESSURE)
If de-ice annunciator does illuminate:
Boot Pressure .............. Manual and Release
Icing Conditions ................... Exit as Practical
If de-ice annunciator does not illuminate
or any of the leading edge boots do not
inflate:
Icing Conditions ................. Exit Immediately
Airspeed .................................. 120 KIAS Min
Flaps ......................................................... Up
If unable to maintain this airspeed in
level flight:
Attitude ......................................... Decrease
or
o
Flaps ........................................................ 10
Airspeed .................................. 105 KIAS Min
WARNING
IN HEAVY ICING CONDITIONS, IT MAY NOT
BE POSSIBLE TO MAINTAIN ALTITUDE OR
PROPER GLIDE PATH ON APPROACH; IN
THIS CASE, IT IS IMPERATIVE THAT A SAFE
AIRSPEED BE MAINTAINED. THE AURAL
STALL WARING HORN MAY NOT
FUNCTION.
Revised: 11/25/2011
SeaPort Airlines, Inc.
SeaPort Airlines, Inc.
Cessna 208 Series
Cessna 208 Series
EMERGENCY CHECKLIST
ICING (Con’t)
EMERGENCY CHECKLIST
ICING (Con’t)
LEADING EDGE DE-ICE BOOTS
REMAIN INFLATED (DE-ICE
PRESSURE)
HEATED STALL WARNING
MALFUNCTION
Boots ................................................ Observe
If any of the boots remain inflated:
De-Ice Boot C/B ...................................... Pull
Boots ................................................ Observe
If any boots remain inflated:
Icing Conditions ................. Exit Immediately
If all boots deflated:
Boots ..................... Observe after each Cycle
WINDSHIELD ANTI-ICE PANEL
MALFUNCTION
W/S Anti-Ice ............. Cycle (OFF then AUTO)
W/S Anit-Ice C/B’s ........................ Pushed In
W/S Anti-Ice Annunciator .................... Check
If W/S anti-ice annunciator does not
illuminate:
W/S Anti-Ice ...................... Manual and Hold
If ice remains on windshield:
Landing Approach ................ Plan Straight-in
Landing .............................. Forward Slip A/R
HEATED PITOT/STATIC TUBE
MALFUNCTION
Pitot Heat C/B’s ............................ Pushed In
Flight Instruments............... Compare LH/RH
Alt Static Air .......................................Pull On
If ice is observed forming on the stall
warning vane or its mounting plate:
Stall Warning C/B .......................... Pushed In
With Continued Ice Buildup ................Expect
....................... no Stall Warning horn during
.................................. Slow Speed operation
Approach Speeds ............................. Monitor
LOW AIRSPEED (BELOW ICING MIN
SPD AND AURAL WARNING)
Enroute (flaps up):
Autopilot ..................................... Disconnect
Power .............................................. Increase
Icing Conditions ................. Exit Immediately
Airspeed................................... 110 KIAS Min
Autopilot ...................................... As Desired
CAUTION
FLAPS MUST BE EXTENDED TO A
o
MINIMUM OF 10 ANYTIME AIRSPEED IS
BELOW 110 KIAS
o
o
Approach (flaps 10 or 20 ):
Autopilot ..................................... Disconnect
Power .............................................. Increase
o
Airspeed........................ 120 KIAS & 10 Flap
Airspeed........................................... Monitor
Autopilot ...................................... As Desired
Below Icing Min Spd Light ..................... Push
................................... when landing assured
ENGINE MALFUNCTIONS
INADVERTENT ENCOUTER WITH
FREEZING RAIN OR FREEZING
DRIZZLE OR OTHER PERFORMANCE
CRITICAL ICING SITUATION
LOSS OF OIL PRESSURE (OIL PRESS
LOW Annunciator On)
Enroute (flaps up):
Power ................................. Increase to Max
Airspeed................................... 120 KIAS Min
Ignition Switch ......................................... ON
Inertial Separator ............................... Bypass
Pitot/Static, Stall, W/S, & Prop Anti-ice .... On
De-Ice Boots ......................................... Cycle
ATC ... Notify and Request Priority Handling
Icing Conditions ................. Exit Immediately
o
Oil Pressure Gauge .............................. Check
GEAR BOX CONTAMINATION (CHIP
DETECTOR Annunciator On)
Engine Gauges ................. Carefully Monitor
FCU/(P3) MALFUNCTION
Power ..................................................... Idle
Emer. Power Lever ................................. A/R
............ (Maintain 65% Ng min during flight)
o
Approach (flaps 10 or 20 ):
Power ...................................... Increase A/R
Airspeed................................... 120 KIAS Min
o
Flaps......................................................... 10
Ignition Switch ......................................... ON
Inertial Separator ............................... Bypass
Pitot/Static, Stall, W/S, & Prop Anti-ice .... On
De-Ice Boots ......................................... Cycle
ATC ... Notify and Request Priority Handling
Airspeed........ Maintain 120 KIAS, if possible
STATIC SOURCE BLOCKAGE
Pitot/Static Heat ....................................... On
Alt. Static Air Source ..........................Pull On
Autopilot ................ Disengage Altitude Hold
MINIMUM SPEED IN ICING
CONDITIONS
Flaps Up .......................................... 120 KIAS
o
Flaps 10 ......................................... 105 KIAS
o
Flaps 20 ........................................... 95 KIAS
If ice begins to form near the pitot port:
Indicated Airspeed .................... Not Reliable
Page 7 of 12
ICING (Con’t)
When climbing to exit icing conditions
Flaps Up .......................................... 110 KIAS
o
Flaps 10 ........................................... 95 KIAS
o
Maximum Bank Angle .............................. 30
Revised: 11/25/2011
Page 8 of 12
Revised: 11/25/2011
SeaPort Airlines, Inc.
SeaPort Airlines, Inc.
Cessna 208 Series
Cessna 208 Series
EMERGENCY CHECKLIST
EMERGENCY CHECKLIST
FUEL SYSTEM MALFUNCTIONS
FLAP SYSTEM MALFUNCTION
LOSS OF FUEL PRESSURE (FUEL
PRESS LOW & AUX FUEL PUMP ON
Annunciators On)
ASYMMETRIC FLAP EXTENSION OR
SUDDEN FLAP RETRACTION ON
ONE SIDE
Fuel Selectors .................................. Both On
Boost Pump .............................................. On
Ignition...................................................... On
Apply Aileron & Rudder to Stop Roll
Flaps.......................................................... Up
Airspeed.................................. 100 KIAS Max
FUEL FLOW INTERRUPTION TO
FUEL RESERVOIR
(RESERVOIR FUEL LOW
Annunciator On)
If both flaps cannot be retracted to
symmetrical setting
Airspeed..................................... 90 KIAS min
Land ..............................As Soon As Practical
Fuel Selectors .................................. Both On
Boost Pump .............................................. On
Ignition...................................................... On
FLAPS FAIL TO EXTEND OR
RETRACT
FUEL TANK SELECTOR OFF DURING
START (FUEL SELECTOR OFF
Annunciator On & Both Fuel
Selector Warning Horns Activated)
If flaps still fail to extend or retract and
takeoff or landing conditions requires flaps
Standby Flap Motor Switch .................. STBY
Flap Motor Up/Dn Switch ....................... A/R
Flap & STBY Flap Motor C/B’s .................... In
ELECTRICAL POWER
MALFUNCTIONS
EMERGENCY DESCENT
GENERATOR MALFUNCTION
(GENERATOR OFF & STBY ELECT
PWR ON Annunciators On)
Generator ................................. Trip & Reset
If annunciators remain illuminated
Gen. Cont. & Fld. C/B’s ........................ Reset
Generator ................................. Trip & Reset
If annunciators still remain illuminated
Avionics Stby Power ................................. On
Avionics Bus Tie ........................................ On
Avionics ................................................... Off
Volt/Ammeter(ALT) ............................. Check
Load Limit ....................... Less than 75 amps
ROUGH AIR
Seat Belts, Shldr Harnesses.............. Secured
Power ..................................................... Idle
Prop ....................................................... Max
Flaps ......................................................... Up
Airspeed ........................ Va (148 - 112 KIAS)
SMOOTH AIR
Seat Belts, Shldr Harnesses.............. Secured
Power ..................................................... Idle
Prop ....................................................... Max
o
Flaps ........................................................ 10
Airspeed ................................. 175 KIAS Max
STANDBY POWER MALFUNCTION
(STBY ELECT PWR INOP
Annunciator On)
Standby Power......................... Off, Then On
Fuel Selectors .................................. Both On
If annunciator remains illuminated
Standby Power......................................... Off
Flight .................... Complete Using Gen. Pwr
FUEL LEVEL LOW WITH SINGLE
TANK SELECTED (FUEL SELECTOR
OFF & FUEL LEVEL LOW
Annunciators On & Fuel Selector
Warning Horn Activated)
Fuel Selectors .................................. Both On
Boost Pump .............................................. On
Ignition...................................................... On
Page 9 of 12
Revised: 11/25/2011
Page 10 of 12
Revised: 11/25/2011
SeaPort Airlines, Inc.
SeaPort Airlines, Inc.
Cessna 208 Series
Cessna 208 Series
EMERGENCY CHECKLIST
INADVERTENT OPENING OF
DOORS IN FLIGHT
UPPER HALF OF CARGO OR
PASSENGER AIRSTAIR DOOR OPEN
(DOOR WARNING Annunciator On)
Airspeed.................................. 100 KIAS Max
Flaps........................................................ Full
No Smoking/Seat Belt Signs ...................... On
Approach & Landing ......................... Normal
EMERGENCY CHECKLIST
VACUUM FAILURE
LOW VACUUM
(VACUUM LOW Annunciator On)
AUTOPILOT MALFUNCTIONS
AUTOPILOT MALFUNCTION
Suction Gauge ..................... Verify Condition
Control Wheel .......................... Grasp Firmly
A/P Disc/Trim Inter .................. Press & Hold
A/P Disc/Trim Inter ........................... Release
If gauge indicates no vacuum
Autopilot .................................................. Off
Standby Vacuum .............................. Push On
Suction Gauge ...................................... Check
Autopilot ...................................... As Desired
If pitch trim wheel is in motion
A/P Disc/Trim Inter .................. Press & Hold
Servo C/B ................................................ Pull
Aircraft ............................... Retrim Manually
LOWER HALF OF PASSENGER
AIRSTAIR DOOR OPEN
ELECTRIC TRIM MALFUNCTION
A/P Disc/Trim Inter .................. Press & Hold
Servo C/B ................................................ Pull
Aircraft ............................... Retrim Manually
Airspeed.................................. 100 KIAS Max
Land ..............................As Soon As Practical
Flaps........................................................ Full
No Smoking/Seat Belt Signs ...................... On
Approach .......................................... Normal
Landing ............................... Slightly Tail Low
“CHECK PITCH TRIM” AURAL
WARNING
Airspeed.................................. 125 KIAS Max
Door ........................................ Close & Latch
CARGO POD DOOR(S) OPEN
Airspeed.................................. 125 KIAS Max
Land ..............................As Soon As Practical
Approach .......................................... Normal
Landing ............................... Slightly Tail Low
Page 11 of 12
RED “P”
A Red “P” is an indication that the pitch axis
of the autopilot has been disabled, and the
autopilot cannot be engaged.
RED “R”
A Red “R” is an indication that the roll axis
of the autopilot has been disabled, and the
autopilot cannot be engaged.
FLASHING “HDG”
Indication of failed heading input
HDG Button .......................................... Press
FLASHING ”NAV”, “APR” OR “REV”
Control Wheel .......................... Grasp Firmly
CWS Button ............................. Press & Hold
Trim Condition ..................................... Check
Trim ................................... Manually Retrim
CWS Button ...................................... Release
Autopilot Operation ........................ Monitor
RIGHT OR LEFT CREW DOOR OPEN
AUTOPILOT MALFUNCTIONS
(Con’t)
FLASHING “PT”
Aircraft Pitch Behavior ..................... Monitor
Indication of a flagged navigation source,
autopilot will default to ROL mode
NAV, APR, or REV Button ...................... Press
FLASHING “GS”
Indication of a flagged glideslope source,
autopilot will default to PIT mode. GS will
rearm automatically if a valid glideslope
signal is received.
If annunciator remains illuminated
Control Wheel .......................... Grasp Firmly
CWS Button ............................. Press & Hold
Trim Condition ..................................... Check
Trim ................................... Manually Retrim
CWS Button ...................................... Release
Autopilot Operation ........................ Monitor
Revised: 11/25/2011
Page 12 of 12
Revised: 11/25/2011