Immediate Action Items

Front 1

Immediate Action Items
In all cases

Back 1

Maintain Aircraft Control
Analyze the Problem
Take Appropriate Action
Maintain Situational Awareness

Front 2

Cabin Altitude Warning / Abnormal Pressurization

Back 2

Oxygen Masks and Regulators … On / 100%
Crew Communications … Establish

Front 3

Warning Horn (Intermittent) or Warning Light - Cabin Altitude or Takeoff Configuration

Back 3

If an intermittent warning horn sounds or a CABIN ALTITUDE warning light (if installed and operative) illuminates in flight at an aircraft altitude above 10,000 feet MSL:
Oxygen Masks And Regulators...ON / 100%
Crew Communications...Establish
Accomplish The Cabin Altitude Warning / Abnormal Pressurization Immediate Action Items And Checklist (Page A-15). (STOP)
If the intermittent warning horn sounds or a TAKEOFF CONFIG warning light (if installed and operative) illuminates on the ground:
Assure Correct Aircraft Takeoff Configuration. (STOP)

Front 4

Aborted Engine Start
(Reasons to Abort)

Back 4

Start Lever… Cutoff
If the engine start switch is in GRD:
After motoring the engine for 60 seconds:
   Start Switch… OFF
If the engine start switch is in OFF:
After N2 decreases below 20%:
Start Switch… GRD
After motoring the engine for 60 seconds:
Start Switch… OFF

Front 5

Abort the engine start if any of the following conditions occur:

Back 5

• No N1 before the start lever is raised to IDLE.
• No increase in EGT within 10 seconds (ground) or 30 seconds (in flight) after the start lever raised to IDLE . (On the ground, the EEC automatically cuts off fuel and ignition 15 seconds after the start lever is raised to IDLE  if there is no EGT increase).
• EGT rapidly approaching the start limit (the white box surrounding the EGT digital readout flashes).
• EGT exceeding 725* start limit (EGT dial and digital readout turn red. On the ground, the EEC automatically cuts off fuel and ignition to the engine).
• Engine tailpipe fire
• No/very slow increase in N1  or N2 , after EGT indication.
• No oil pressure indication by the time the engine has stabilized at idle.
• When directed for any other condition.

Front 6

Engine Limit / Surge / Stall

Back 6

1. (NG) Autothrottle (if engaged)…Disengage
2. Thrust Lever… Retard to Maintain Limits

Front 7

Dual Engine Failure

Back 7

1. Start Switches…FLT
2. Start Levers…CUTOFF
EGT Decreasing:
3. Start Levers…IDLE
If EGT reaches 930*C (CL) or 950*C (NG) or there is no increase in EGT in 30 seconds:
Repeat the above steps as necessary

Front 8

Engine Overheat

Back 8

1. (NG) Autothrottle (if engaged)…Disengage
2. Thrust Lever…Close
Then:
If OVERHEAT light remains illuminated:
Accomplish the Engine Fire / Severe Damage / Separation / Seizure Immediate Action Items and Checklist, Page G-13 (CL) G-11 (NG)."

Front 9

APU Fire

Back 9

1. APU Fir Warning Switch…Pull, Rotate, and Hold 1 Second.
2. APU Switch…OFF

Front 10

Airspeed Unreliable

Back 10

1. Airspeed Attitude / Thrust…Adjust
2. Probe Heat…Confirm ON
3. Mach/Airspeed Indicators…Crosscheck

Front 11

Engine Fire/Severe Damage/Separation/Seizure

Back 11

1. (NG) Autothrottle (if engaged)…Disengage
2. Thrust Lever…Close
3. Start Lever…CUTOFF
4. Engine Fire Warning Switch…Pull
If the fire warning light or OVERHEAT light remains illuminated:
     Engine Fire Warning Switch…Rotate L or R and Hold 1 Sec
     If after 30 seconds, the fire warning light or OVERHEAT light remains illuminated:
          Engine Fire Warning Switch…Rotate to remaining bottle and Hold 1 Sec

Front 12

Smoke/Fire/Fumes on the Aircraft
Lavatory Smoke/Fire

Back 12

1. Oxygen Masks and Regulators…ON/100%
2. Smoke Goggles (if required)…ON

Front 13

Runaway Stabilizer

Back 13

1. Control Column…Hold Firmly
2. Autopilot (if engaged)…Disengage
If runaway stabilizer continues:
     3. Stabilizer Trim Cutout Switches…CUTOUT
     If runaway stabilizer continues:
          4. Stabilizer Trim Wheel…Grasp and Hold

Front 14

Uncommanded Roll (Spindle Failure)

Back 14

1. Autopilot (if engaged)…Disengage
2. Maintain Control of the Aircraft With All Available Flight Controls. If Roll Is Uncontrollable, Immediately Reduce Pitch / AOA and Increase Airspeed. Do Not Attempt to Maintain Altitude Until Control Is Recovered.
3. Thrust…Verify Symmetrical
4. Go-Around…Initiate

Front 15

Reject Takeoff (No Longer a Memory Item)
Captain

Back 15

QRH P-9
Simultaneously perform the following:
• Close the thrust levers.
• Disengage the autothrottles.
• Apply maximum manual wheel brakes or verify operation of the RTO autobrake system.
• If RTO autobrake is selected, monitor system performance and apply manual wheel brakes if the AUTO BRAKE DISARM light illuminates or deceleration is not adequate.
Without delay:
• Raise the speedbrake lever.
• Apply reverse thrust up to the maximum amount consistent with conditions.
• Continue maximum braking until certain the airplane will stop on the runway.

Front 16

Reject Takeoff (No Longer a Memory Item)
First Officer

Back 16

QRH P-9
[Note Groundspeed]
Verify action as follows:
• Thrust levers closed.
• Autothrottles disengaged.
• Maximum brakes applied.
• Speedbrake lever is up, and call “Extended.”
If speedbrake lever is not up, call “No Speedbrake.”
When both green REV lights are illuminated, call “Deployed.”
If a green REV light is not illuminated, call “No Reverse.”
Note: The “No Reverse” call only applies to the operating engine.
Note: The “No Reverse” call does not apply to thrust reversers deferred by Maintenance.
If the AUTO BRAKE DISARM light illuminates:
• Call “Autobrake Disarm.”
• Call out any omitted action items.

• Call “60 knots.”
• Communicate the reject decision to the control tower.

• Note the speed, call for response if required, remind the CA not to set the parking brake if not evacuating, accomplish the QRH checklist items for the abort, refer to P-9 afterwards.