Aborted engine start

Condition: During a ground start, an abort engine start condition occurs.

Objective: To shut down the engine and motor it.

1. Engine start lever (affected engine) .... CUTOFF

Airspeed unreliable

Condition: The pitch attitude is not consistent with the fase of flight, altitude, thrust and weight, or noise or low frequency buffeting is experienced.

Objective : to establish the normal pitch attitude and thrust setting for the phase of flight

1. Adjust the airplane attitude and thrust maintain airplane control
2. Probe heat switches ........... CHECK ON
3. Cross check the MACH and AIRSPEED indicators

APU FIRE

Condition: Fire is detected in the APU/

1. APU FIRE SWITCH ... CONFIRM ... PULL, ROTATE TO THE STOP AND HOLD FOR ONE SECOND
2. APU SWITCH ... OFF

CABIN ALTITUDE WARNING 

Condition : One or more of these occur: Cabin Altitude exceedance, inflight intermittent cabin altitude/configuration warning horn sounds of a cabin altitude light (if installed and operative) illuminates.

1. Don Oxygen mask and set regulators to 100%
2. Establish crew communications
3. Pressurization mode selector ... MAN
4. Outflow valve switch ... HOLD IN CLOSE until the outflow valve indication shows fully closed
5. If cabin altitude is unctrollable : 
   Passenger signs ... ON
6. If the cabin altitude exceeds or is expected to exceed 14 000 feet :
   Passenger oxygen switch ... ON
   Go to the emergency descent checklist on page 0.1 

EMERGENCY DESCENT

Condition : One or more of these occur :
- Cabin altitude can not be controlled when the airplane is above 14 000 feet

Or 

A rapid descent is needed

1. Announcing the emergency descent. The pilot flying will advise the cabin crew, on the PA system, of impending rapid descent. The pilot monitoring will advise ATC and obtain the area altiemter setting
2. Passenger Signs ...  ON
3. Without delay, descend to the lowest safe altitude or 10 000 feet whichever is higher
4. Engine Start switches ... BOTH CONT
5. Thrust levers ... BOTH reduce thrust to minimum or as needed for anti-ice
6. Speedbrakes ... Flight Detent
7.  Set target speed to MMO/VMO

(If structual integrity is in doubt limit speed as much as possible and avoid high manoeuvring loads).

Engine fire

Condition: One or more of these occur
- Engine fire warning

- Airframe vibrations with abornmal engine indications

- Engine seperation

1.  Auto-throttle ... DISENGAGE
2. Thrust lever (affected engine) ... CONFIRM ... Close
3.  Engine start lever (affected engine) ... CONFIRM ... CUTOFF
4.  Engine fire switch (affected engine) ... CONFIRM ... PULL 
   To manually unlock the engine fire switch press the override and pull
5. If the engine fire switch or engine overheat light stays illuminated 
   Engine fire switch ... Rotate to the stop and hold for 1 second
6. If after 30 seconds the fire switch of the overheat light stays illuminated 
   Engine fire switch ... ROTATE TO THE OTHER STOP and hold for 1 second
    

ENGINE LIMIT OR SURGE OR STALL

Condition : one or more of these occur :
- Engine indications are abnormal
- Engine indactions are rapidly approaching or exceeding limits

- Abnormal engine noises are heard possibly with airframe vibrations.

- There is no response to thrust lever movement or the response is abnormal
- Flames in the engine inlet or exhaust are reported

Objective : To attempt to recover normal engine operation or shut down the engine if recovery is not possible.

1. Auto-throttle (if engaged) ... DISENGAGE
2. Thrust lever (AFFECTED ENGINE) ... CONFIRM ... RETARD until engine indications stay within limits or the thrust lever is closed 

ENGINE OVERHEAT

Condition : An overheat is detected in the engine

1. Autothrottle (if engaged) ... DISENGAGE
2. Thrust lever (affected engine) ... CONFIRM ... CLOSE
3. IF the ENG OVERHEAT light stays illuminated : GO TO THE ENGINE FIRE OR ENGINE SEVERE DAME OR SEPERATION CHECKLIST

LANDING CONFIGURATION

LANDING CONFIGURATION

Condition : In flight, the steady warning horn sounds

1. Assure correct airplane landing configuration

LOSS OF THRUST ON BOTH ENGINES

Condition: Both of these occur :
- Both engines have a loss of thrust
- Both ENG FAIL alerts how

Objective: To restart at least one engine

1. ENGINE START SWITCHES (BOTH) ... FLT
2. ENGINE START LEVERS (BOTH) ... CUTOFF
3. When EGT decreases 
   ENGINE START LEVERS (BOTH) ... IDLE DETENT
4. If EGT reaches 950°C or there is no increase in EGT within 30 seconds :
   Engine start lever (affected engine) ... CONFIRM ... CUTOFF, then idle detent

IF egt again reaches 950°C or there is no inccraese in EGT within 30 seconds, repeat as needed 

RAPID DEPRESSURIZATION

Condition : One or more of these occur: Cabin Altitude exceedance, inflight intermittent cabin altitude/configuration warning horn sounds of a cabin altitude light (if installed and operative) illuminates.

1. Don Oxygen mask and set regulators to 100%
2. Establish crew communications
3. Pressurization mode selector ... MAN
4. Outflow valve switch ... HOLD IN CLOSE until the outflow valve indication shows fully closed
5. If cabin altitude is unctrollable : 
   Passenger signs ... ON
6. If the cabin altitude exceeds or is expected to exceed 14 000 feet :
   Passenger oxygen switch ... ON
   Go to the emergency descent checklist on page 0.1 

RUNAWAY STABILIZER

RUNAWAY STABILIZER

Condition : Uncommanded stabilizer trim movement occurs continuously

1. Control column ... Hold firmly
2. Autopilot (if engaged) ... disengage
   Do NOT re-engage the autopilot. Control airplane pitch attitude manually with control column and main electrim trim as needed.
3. Autothrottle (if engaged) ... Disengage
   Do NOT re-engage the auto throttle
4. If the runaway stops after the autopilot is disengaged : memory items completed
5. If the runaway continues after the autopilot is disengaged : 
   STAB TRIM CUTOUT switches (both) ... CUTOUT
6. If the runaway continues : 
   STABILIZER TRIM WHEEL ... GRASP AND HOLD 

TAKEOFF CONFIGURATION 

TAKEOFF CONFIGURATION

Condition : On the ground the intermittent cabin altitude/configuration warning horn sounds or a TAKEOFF CONFIG LIGHT (if installed and operative) illuminates when advancing the thrust levers to takeoff thrust.

1. Assure correct airplane takeoff configuration

UNCOMMANDED RUDDER/YAW OR ROLL

UNCOMMANDED RUDDER/YAW OR ROLL

Condition : Uncommanded rudder pedal displacement or pedal kicks, or uncommanded yaw or roll occurs.

1. Autopilot (if engaged) ... DISENGAGE
2. Maintain control of the airplane with all available flight controls. If roll is uncontrollable, immediately reduce pitch/angle of attack and increase airspeed. Do not attempt to maintainn altitude until control is recovered.
3. Autothrottle ... DISENGAGE
4. Vertify thrust is symmetrical

WARNING HORN (INTERMITTENT) OR WARNING LIGHT - CABIN ALTITUDE OR TAKEOFF CONFIGURATION

Condition : One of these occurs : 
- In flight, at an airplane flight altitude above 10 000 feet MSL the intermittent warning horn sounds on a CABIN altitude light illuminates

- On the ground the intermittent warning horn sounds or a TAKEOFF CONFIG light illuminates when advancing the thrust levers to takeoff thrust.

1. IF the intermittent warning horn sounds or a CABIN ALTITUDE LIGHT illuminates in flight at an airplane flight altitude above 10 000 feet MSL : 

Don the oxygen masks and set the regulators to 100%. 

Establish crew communications

Go to the cabin Altitude warning or rapid depressurization checklist on page 2.1

2. If the intermittent warning horn sounds or a TAKEOFF CONFIG light illuminates on the ground when advancing the thrust levers to takeoff thrust : 

Assure correct airplane takeoff configuration