Pressurization Controller Fault (2 steps, 1 timing)
1) AUTO/MAN/DUMP to MAN
2) Wait 2 seconds
3) AUTO/MAN/DUMP to AUTO
Rapid Depressurization (4 steps)
OXYGEN MASK … DON/100%
MIC SWITCH … MASK
PASSENGER SIGNS … ON
EMERGENCY DESCENT … as req
EMERGENCY DESCENT (9 steps)
CABIN CREW … ADVISE
PASSENGER SIGNS … ON
LDG LIGHTS … ON
AIRPLANE HEADING .. AS REQ
ALT WINDOW … 10.000 ft OR MSA
POWER LEVERS … FLT IDLE
CONDITIONS LEVERS … MAX
AIRSPEED … Vmo
DESCENT … initiate
ENG OIL PRESS (1 step)
ENGINE FAILURE/SHUTDOWN … ACCOMPLISH
ENG FADEC FAIL (1 step)
ENGINE FAILURE/SHUTDOWN … ACCOMPLISH
ENGINE FAILURE/SHUTDOWN (5 steps)
Affected Engine:
POWER LEVER … FLIGHT IDLE
CONDITION LEVER … FUEL OFF
ALT FTHR … FTHR
T-HANDLE … PULL
AUX PUMP … OFF
OIL PRESSURE BELOW 44 PSI (1 step)
ENGINE FAILURE/SHUTDOWN … ACCOMPLISH
PROP GRD RANGE LIGHT CYCLING (1 step)
BOTH POWER LEVERS … ABOVE FLIGHT IDLE
UNSCHEDULDED PROPELLER FEATHER (1 condition, 1 step)
Above 400 ft
ENGINE FAILURE/SHUTDOWN … ACCOMPLISH
PROPELLER OVERSPEED (1 altitude restriction, variable steps with split)
Above 400 ft AGL:
AIRSPEED … REDUCE to MIN SPEED
Affected Engine:
POWER LEVER …………FLIGHT IDLE
CONDITION LEVER….START/FEATHER
ALT FEATHER…………..FTHR
Propeller feathered?
If YES
ENGINE FAILURE/SHUTDOWN (10.4)…..ACCOMPLISH
If NO
DO NOT SHUTDOWN ENGINE
ALT FTHR ………………….OFF
CONDITION LEVERS…..MAX
POWER LEVERS..………..OPERATE TOGETHER
Land immediately at the nearest suitable aerodrome.
ABORTED ENGINE START (2 steps)
CONDITION LEVER affected engine
………FUEL OFF
ENGINE START SELECT
………OFF
NO STARTER CUT OUT (2 steps)
ENGINE START SELECT………………………………………….OFF
DC EXT POWER………………………………………………………OFF
BAGGAGE COMPARTMENT SMOKE (4 steps)
OXYGEN MASKS ………..DON/100%
MIC SWITCH………………MASK
RECIRC FAN ………………OFF
ILLUMINATED EXTG SWITCH…………………..…PRESS
ENGINE FIRE (7 steps, 1 timing)
Affected Engine:
POWER LEVER…..………..FLIGHT IDLE
CONDITION LEVER…..…FUEL OFF
ALT FTHR……………………FTHR
T-HANDLE…………………..PULL
AUX PUMP ……..………….OFF
EXTG SWITCH……………..FWD BTL
If Fire Persists, wait Up To 30 Seconds:
EXTG SWITCH……………..AFT BTL
APU FIRE (2 steps, verify 5 items, 1 timing)
APU AUTO SHUTDOWN………CONFIRM
Advisory Lights:
- APU RUN OFF
- APU FAIL ON
- APU BTL LOW ON
- FUEL VALVE CLOSED LIGHT ON
If APU BTL ARM or APU FIRE Advisory Lights remain ON after 7 seconds:
EXTG SWITCH…………..PRESS
FUSELAGE FIRE, SMOKE OR FUMES (3 steps)
OXYGEN MASKS …………………………………………..DON/100%
MIC SWITCH……………………………………………………….. MASK
RECIRC FAN …………………………………………………………..OFF
ELEVATOR TRIM RUNAWAY (1 step)
ELEVATOR TRIM SHUT OFF … PUSH OFF
ELEVATOR JAM (6 steps, 1 limitation)
AUTOPILOT…………. DISENGAGE
FLAP AND AIRSPEED
–> MAINTAIN AT TIME OF JAM
CONTROL COLUMNS
–> BOTH PILOTS ATTEMPT TO
OVERCOME JAM
IF unable to overcome jam:
CONTROL COLUMN FORCE
–> RELAX
PITCH DISC HANDLE
–> PULL AND TURN 90°
CONTROL COLUMNS
–> BOTH PILOTS ATTEMPT PITCH
CONTROL
Pilot with free control column will fly the aircraft.
Maximum Airspeed with jammed elevator is 170 KIAS or
speed at which jam occurred, whichever is greater.
AILERON TRIM RUNAWAY (2 steps)
AIRSPEED ……………REDUCE
AILERON TRIM…..…OPPOSITE TO
RUNAWAY
ROLL CONTROL JAM (3 steps)
AUTOPILOT……………. DISENGAGE
ROLL DISC HANDLE …..PULL AND TURN 90°
CONTROL COLUMNS….BOTH PILOTS ATTEMPT ROLL CONTROL
Pilot with free control wheel will fly the aircraft
ROLL CONTROL MALFUNCTION (variable steps with split)
ROLL CONTROL…….. APPLY TO HOLD WINGS LEVEL
Continuous illumination of SPLR 1 or SPLR 2 PUSH OFF switchlights in wings-level flight?
If yes, then
ILLUMINATED SPLR SWITCHLIGHT………… PUSH OFF
If no, then
POWER ……….. APPLY
AIRSPEED………INCREASE
RUDDER ACTUATOR MALFUNCTION (1 step)
ILLUMINATED RUD SWITCHLIGHT
—> PUSH OFF
RUDDER TRIM ACTUATOR RUNAWAY (1 step)
RUDDER TRIM ………. OPPOSITE TO RUNAWAY
RUDDER JAM (1 warning, variable steps with split)
WARNING: Should the rudder pedal (rudder jam) suddenly break free, do not apply rudder pedal input in the opposite direction.
Apply normal push force on affected rudder pedal.
Rudder Pedal moves as required?
If YES
Reduce push force on affected rudder pedal and allow
rudder to center.
If NO
Rudder Pedal does not respond to normal push force (rudder remains jammed or rudder jam reoccurs)
–> Use roll control as req’d for
directional control.
