Emergency Shutdown

1.  Power Lever - Idle

2.  Condition Lever - Fuel Shutoff

3.  Pull Fuel Off Handle - Pull

1.  Crew Oxygen Mask & Goggles - 100% and ON

2.  ICS Switch Mask - Establish Communications

3.  Dome Light Switch - On

4.  Emer LTS Switch - On

5.  Fasten Belt Switch - On

1.  Power Levers (4) - DISC

2.  Braking - As Required

3.  Reverse - As Required

1.  Power Levers (4) - Max Available

2.  Landing Gear (after Positive rate) - UP

*3.  Airspeed - V2

4.  Confirm Auto Feather No Fire

    If failed engine did not feather

5. Condition Lever (failed engine) - Fuel Shutoff

    After commencement of 3rd segment, Min 400' AGL

*6.  Airspeed - Accelerate to Vclimb

7.  Flaps (on profile) - Select UP

8.  Emergency Shutdown (affected engine) - Complete

9.  EXTG Switch - (if required) FWD BTL (Wait 30 seconds) - If fire Persists -              EXTG Switch - AFT BTL

ENGINE MALFUNCTION OR PRECATIONARY ENGINE SHUTDOWN DURING FLIGHT

* = PF

1.  Synchrophase Switch - OFF

*2. Power - As Required

3.  Affected Engine - Identify

4.  Emergency Shutdown (affected engine) - Complete

TWO ENGINE INOPERATIVE OPERATIONS

* = PF

*1.  Condition Levers (fwd 3) - Max RPM

*2.  Power - Max Available

3.  Affected Engine - Identify

4.  Emergency Shutdown (affected engine) - Complete

TWO ENGINE GO-AROUND OR MISSED APPROACH PROCEDURE

* = PF

*1.  Power Levers (4) - Maximum Available

 2.  Landing Gear - Up

 3.  Flaps - UP

*4.  Airspeed - 118 KIAS

*5.  Bank Angle - 30 Degrees Maximum

1.  Airspeed - 1.3 VS

OVERTEMPERATURE (OTHER THAN STARTING)

If T5 exceeds 800 degrees C and cannot be controlled by reducing the Power Levers:

1.  ENGINE MALFUNCTION OR PRECAUTIONARY ENGINE SHUTDOWN DURING FLIGHT CHECKLIST - Complete

ENGINE Ng OVERSPEED

1.  SYNCHROPHASE Switch - OFF

2.  POWER lever (affected engine) - FLT IDLE 

If there is no response to the power lever movement:

3.  PULL FUEL OFF HANDLE - PULL 

below 1500 FT/LB Torque:  

4. Condition Lever (affected engine) - FUEL SHUTOFF 

In the event of low oil pressure indication or illumination of the oil pressure caution light ... perform the following:

If engine OIL PRESS is confirmed below 75 PSI:

Complete ENGINE MALFUNCTION OR PRECAUTIONARY ENGINE SHUTDOWN DRUING FLIGHT or land as soon as practical using mimimum power on that engine.

PROPELLER OVERSPEEED

* = PF

1. SYNCROPHASER SWITCH - OFF

*2. POWER LEVER (affected engine) - FLT IDLE 

*3. Airspeed - Reduce

4.  Condition Lever (affected engine) - Start Feather

If propeller does not feather:

5.  Condition Lever (affected engine) - Fuel Shut Off

ENGINE FIRE OR SEVERE ENGINE DAMAGE ON GROUND

ALL PF DUTIES

Engine Fire or Severe Engine Damage in Flight

* = PF Duties

1.  SYNCHROPHASE Switch - OFF

*2. Power - As required

3. Affected Engine - Identify

4.  EMERGENCY SHUTDOWN (affected engine) - Complete

5.  EXTG Switch - FWD BTL  (wait 30 seconds) if fire persists - AFT BTL

1. APU FIRE PUSH Switch light - Press for 1 second and release.

2.  APU ON indicator - Not illuminated

If APU FIRE PUSH indicator is still illuminated:

3.  APU FIRE BOTTLE Switch - Activate

4.  Master BATTERY Switch - OFF

5.  DC EXT PWR Switch - OFF

6.  APU DC GEN ON Switch - OFF

7.  Evacuate Aircraft

1.  DETECTOR LOOP Switch - Select Non-illuminated loop position.

2.  Fire Warning Test - Conduct

(if the non-illuminated light comes on together with the ENGINE FIRE warning, MASTER CAUTION & CHECK FIRE DET caution lights, all PULL FUEL OFF handles & selected all LOOP lights ... a loop failure only has occurred. Leave DETECTOR LOOPS selected Loop position.)  

Fire or Smoke Emergencies

IN AFT BAGGAGE COMPARTMENT

1.  SMOKE & FUMES ACTIONS - COMPLETE

Fire or Smoke Emergencies

IN FLIGHT COMPARTMENT

Fire or Smoke Emergencies

IN CABIN

Fire or Smoke Emergencies

UNKNOWN SOURCE OF SMOKE

Fire or Smoke Emergencies

ELECTRICAL SYSTEM SMOKE OR FIRE IN FLIGHT

Electrical Emergencies

PRIMARY INVERTER FAILED

Electrical Emergencies

SECONDARY INVERTER FAILED

1.  INV SEL Switch - R Bus

2.    115v BUS TIE circuit breaker (2nd row right ovhd panel) - Pull

Electrical Emergencies

AUXILIARY INVERTER FAILED

1. 115v BUS TIE circuit breaker (2nd row right ovhd panel) - Pull

Electrical Emergencies

TWO INVERTERS FAILED

1.  STORM/DOME light switch - STORM.

2. PANEL LIGHTING circuit breakers (8) center ovhd - Pull.

Emergency Descent

NO STRUCTURAL DAMAGE INVOLVED

* = PF

1. SYNCROPHASE switch - OFF

*2.  POWER Levers - FLT IDLE

*3.  Condition levers - MAX RPM

*4.  Airspeed - VMO.

Emergency Descent

STRUCTURAL DAMAGE INVOLVED

* = PF

1.  SYNCHROPHASE switch - OFF

*2.  POWER levers - FLT IDLE

*3.  Condition levers - MAX RPM

*4.  Airspeed - 124 KIAS (M6) 120 KIAS (M4)

5.  FLAP selector - Select 15 (below 147 KIAS)

6.  LANDING GEAR handle - DN (below 147 KIAS)

7.  FLAP selector - Select 25 (below 124 KIAS M6 120 M4)

Flight Controls

ROLL AXIS JAM OR MALFUNCTION - CONTROL WHEEL IMMOVABLE

All PF duties

Flight Controls

AIRCRAFT ROLLS WITH NO CONTROL WHEEL INPUT

1.  AUTOPILOT - Disengage

Flight Controls

IF ROLL SPLR SWITCH LIGHT IS ON:

Flight Controls

ELEVATOR CONTROL JAM IN FLIGHT

* = PF

*1.  Autopilot - Disengage

*2.  Control column - Apply pressure call out "PITCH JAM HELP"

*3.  Airspeed and flap setting - Maintain

*4.  Control column - Apply pressure against jam

If jam persists ... relax control column force momentarily  *5.  PITCH DISC T handle - Pull and rotate 90 degrees Elevator forces will be lighter and pitch control will be degraded withone elevator only

*6.  Pilot with free control column flies teh aircraft.

Flight Controls

FAILURE OF ANY ONE TRAILING FLAP SEGMENT TO RETRACT FROM 45 TO 25 DEGREE POSITION

All PF duties

1.  Airspeed on go-around - 98 KIAS maximum

Flight Controls

AILERON TRIM TAB RUNAWAY

PF Duties

1. Autopilot - Disengage

Flight Controls

RUDER CONTROL MALFUNCTION RUD 1 OR RUD 2 switch light illuminated:

Flight Controls

RUDDER TRIM ACTUATOR RUNAWAY

Pressurization Malfunctions

IF CABIN PRESSURIZATION IS LOST WHEN POERATING ABOUT 10,000', PERFORM THE FOLLOWING:

1.  1 minute on - 1 minute off

2.  1 minute on - 1 minute off

3.  1 minute on - 1 minute off

4.  1 minute on - 1 minute off

5.  1 minute on - 15 minute off

TORQUE LIMITS                                   TIME LIMIT

Maximum           4860                           5 Minutes

Transient            5900                           20 Seconds

Continuous          4223             

Max Climb/Cruise 4417

Caution                660 - 870

Normal                870 - 1210

Maximum             1210

Max Transient       1445

T5 LIMITS                            TIME LIMIT

T5 LIMITS                              TIME LIMIT

Take-Off      800                       5 minutes

Continuous   800

Max Climb    770

Max Cruise   770

Transient     850                        2 seconds

Max Starting 1000                      5 seconds

Max Reverse 800                       1.5 minutes

Ng LIMITS                               TIME LIMIT

OIL TEMPERATURE                    TIME LIMIT

Minimum               75

Normal                 80 - 100

Caution                 75 - 80

Maximum              100

Normal                   0 - 4.26

Caution                   4.26 - 4.7

Maximum                4.7

Take-Off     15

Landing      10

Flaps Retracted  2.53 to -1

Flaps Extended   2 to 0

Uphill      2%

Downhill  2%

Ramp (RC-7B)    49000

Ramp (EO-5B)    47100

Take-Off            47000

Landing             45000

Landing (Flaps 45) 42000

Zero Fuel Weight   39000

500 LBS

All Engines                22 KTS

1 Engine Inoperative  18 KTS

Outboard Spoiler       18 KTS

Va                         161

Vb                         171

Vfe (Flaps 15)          147

     (Flaps 25)          124/120 (M6/M4)

     (Flaps 45)          110

Vle                        161

Vlo                        147

Vmo (Below 7500      231 Above 7500 decrease by 4KT/1000 lbs

DV Window              160

"I" Sensors Extended  160

Max Tire Speed         139