FUS DUCT HOT LIGHT
- ON GROUND, SECURE GROUND AC AND ALL ENGINE AND APU BLEED AIR, AND RETURN TO THE LINE
- IN FLIGHT, CLOSE ALL ENGINE BLEED AND FUSELAGE SHUTOFF VALVES
START VALVE LIGHT ON AFTER START
CHECK OVERHEAD PANEL FOR INDIVIDUAL START CONTROL VALVE OPEN LIGHT
NTS INOPR
- CONTINUE HOLDING OUT FEATHER BUTTON
- EMERGENCY SHUTDOWN HANDLE-PULL
- FEATHER BUTTON-PUSH
1, 2, 3, OR 4 STARTER CONTROL VALVE OPEN LIGHT
IF LIGHT REMAINS ON OR COMES ON AFTER START, SECURE ENGINE BY PULLING EMERGENCY SHUTDOWN HANDLE
FIRE OF UNKNOWN ORIGIN
- ALERT THE CREW, ACTIVATE THE FIRE BILL
2. CABIN EXHAUST FAN-OFF
RAPID DECOMPRESSION
- PRESSURIZATION GROUND CHECK SWITCH-TEST
2. GROUND AC- ON
EMERGENCY DEPRESSURIZATION
- AUX VENT-OPEN
- OUTFLOW VALVE-OPEN
- EDCS-DUMP
- AUX VENT- CLOSE AT 1 IN DIFFERENTIAL
W/O ELECTRICAL POWER - FREEFALL CHUTE-OPEN
EMERGENCY DESCENT
- AUTOPILOT-DISENGAGED
- POWER LEVERS-IDLE
- LANDING GEAR-AS REQUIRED (DOWN)
- AIRSPEED-AS REQUIRED (300 KTS)
- PRESSURIZATION-AS REQUIRED
BRAKE FIRE
- REQUEST GROUND FIREFIGHTING EQUIPMENT
2. STOP THE AIRCRAFT
ENGINE FIRE ON THE GROUND
- EMERGENCY SHUTDOWN HANDLE-PULL
- HRD-DISCHARGED
CALL FOR ENGINE FIRE ON THE GROUND CHECKLIST
EMERGENCY SHUTDOWN PROCEDURE
- EMERGENCY SHUTDOWN HANDLE-PULL
- HRD (FIRE ONLY)-DISCHARGED
CALL FOR SHUTDOWN CHECKLIST CHECKLIST
SHIFTING TO BOOST OFF
- DISCONNECT THE AUTOPILOT
- ATTEMPT TO ATTAIN A SAFE ALTITUDE
- SET CONDITION V
- TRIM TAB SETTING- CHECK FOR NORMAL POSITION
IF ABNORMAL FORCES STILL PRESENT - BOOSTER SHIFT HANDLE- PULL
INDICATIONS OF A PROP MALFUNCTION
PROP PUMP LIGHT, LEAK OR AN OFFSPEED CONDITION DETECTED AUDIBLY. CONSIDERED OFFSPEED IF FLUX IS +/- 1% OF MECHANICAL OR ELECTRICAL GOVERNING OR ANY SUSTAINED OSCILLATION OCCURS
2 WARNINGS WITH PROP PUMP
- IF SIGNIFICANT AIRFRAME VIBRATION ACCOMPANIES LIGHT OR LEAK, CONSIDER EMERGENCY SHUTDOWN
- IF OVERSPEEDS ABOVE 115%, REDUCE AIRSPEED AS SOON AS POSSIBLE, NO LESS THAN 150 KIAS. GO TO OPS WITH PITCHLOCKED PROP
PROPELLER MALFUNCTIONS
- IF RPM AT OR ABOVE 115%- REDUCE AIRSPEED (150 KIAS MIN) AND PERFORM OPERATION WITH A PITCHLOCKED PROP PROCEDURE, PARAGRAPH 15.12.2
- IF RPM IS BELOW 115%- SMOOTHLY ADVANCE AFFECTED POWER LEVER AND INCREASE TAS, NOTING ENGINE INDICATIONS
PROP FAILS TO FEATHER
- FEATHER BUTTON-IN
- PCO-PRESS
- ALTERNATE BUS (1&4)- SELECT
- PROP FEATHER CIRCUIT BREAKERS- CHECK IN
- AIRSPEED- DECREASE TOWARDS 150 KIAS
IF FEATHER BUTTON LIGHT REMAINS ON - PROP FEATHER CONT CB- PULL
LOSS OF ALL AIRSPEED INDICATION
- CHECK PITOT HEAT-ON
OUT OF CONTROLLED FLIGHT
- POWER LEVERS-IDLE
- FLIGHT CONTROLS-NEUTRALIZE
- AIRSPEED, AOA, TURN NEEDLE-CHECK
IF IN A SPIN - RUDDER-FULL OPPOSITE TURN NEEDLE
AS SOON AS YAWING MOTION STOPS - CONTROLS-NEUTRALIZE
- UNUSUAL ATTITUDE-RECOVER
TCAS RESOLUTION ADVISORY PROCEDURE
AUTOPILOT-DISCONNECT
POWER LEVERS-AS REQUIRED
COMPLY WITH VERTICAL GUIDANCE
ATTEMPT TO GAIN AND MAINTAIN VISUAL CONTACT WITH TRAFFIC
WINDSHEAR ESCAPE PROCEDURE
MAX POWER-SET
PITCH ATTITUDE-10 DEGREES UP
LANDING GEAR-UP
FLAPS- DO NOT CHANGE UNTIL OUT OF WINDSHEAR
SPLIT FLAP PROCEDURE
IF UNCONTROLLABLE, RESET FLAPS TO PREVIOUS POSITION
IF CONTROLLABLE, LAND WITH THE FLAP HANDLE IN THE SELECTED POSITION
2 ENGINE WAVEOFF
A/S- 145 KIAS MINIMUM
POWER LEVERS-ADVANCE TO MAX POWER AS SOON AS DIRECTIONAL CONTROL IS GAINED
RAISE THE WING WITH THE INOPERATIVE ENGINES SUFFICIENTLY TO OPTIMIZE CONTROL AND CLIMB PERFORMANCE (UP TO 5 DEGREES, IF NECESSARY)
WING FLAP LEVER-APPROACH
LANDING GEAR LEVER-UP
WING FLAP LEVER-MANUVER, THEN UP (145 KIAS MIN)
PRESSURIZATION LOSS
DON SMOKE MASKS
ALERT CREW
(NOT ASTERICK)
VERIFY OBSTACLE CLEARANCE
INVESTIGATE PRESSURIZATION LOSS
FLIGHT WITH CRACKED FRONT WINDSHIELD
TURN OFF HEAT OF AFFECTED PANELS
HELMETS ON, VISORS DOWN
