Memory Items Flashcards
Engine Limit/Surge/Stall (L or R)
Associated A/T Arm switch____ OFF
Associated Thrust lever_______ RETARD
Aborted Engine Start
Associated Fuel Control Switch:
CUTTOFF
PM (FO) “confirm L or R Fuel Control switch”
PF (CPT) “CUTTOFF”
Turbulence Penetration Speeds
Above 25,000’ 280KIAS/0.82M
(Minimum 15 knots above minimum maneuvering speed)
Below 25,000’ 270KIAS
OCEANIC DIVERSION - Engines running
- Initiate drills and time critical checklists
- Declare emergency and request clearance
IF ATC CLEARANCE NOT OBTAINED:
Right turn 30 degrees 5NM off track
RIGHT OR LEFT IN OCA
RIGHT ONLY in China and Russia (Russia 30km or 16.2NM)
When established in offset, altitude level +/-500ft.
OCEANIC DIVERSION CHECKLIST
OCEANIC DIVERSION - Engine Out
- Initiate drills and time critical checklists
- Declare emergency and request clearance
IF ATC CLEARANCE NOT OBTAINED:
Right turn 30 degrees 5NM off track
RIGHT OR LEFT IN OCA
RIGHT ONLY in China and Russia (Russia 30km or 16.2NM)
Minimize decent until established in offset.
When established in offset, descend to below FL290 and maintain +/-500ft.
OCEANIC DIVERSION CHECKLIST
ENGINE INOP. CRUISE DRIFTDOWN
(EASTTER)
ENGINE- ENG OUT VNAV PG observe altitude and speed and EXECUTE ENG OUT.
ALTITUDE - New altitude from FMC ENG OUT page set in MCP - ENSURE VNAV.
SPEED - VNAV engaged. Observe aircraft is going to descend on ENG OUT VNAV profile.
THRUST - thrust ref on FMS is CON and AT maintains MCT
TALK - LIGHTS ON and Declare Mayday to ATC, 121.5, XPDR 7700.
EXECUTE TURN - If required for Oceanic Diversion or Terrain Escape charts require.
RECALL items - TIME CRITICAL DRILLS AND CHECKLISTS (ie. like the Oceanic Diversion Checklist)
TCAS TA and RA
TCAS RA on an approach
TA - look for traffic and reduce map range
Maneuver if required
AP - OFF
AT - OFF
TCAS RA - FOLLOW
ATC - Advise in a TCAS RA
————
AP - OFF
AT - OFF
THRUST - MAX
FLAPS - “FLAPS 20”
TCAS RA - FOLLOW
AFTER positive rate - “GEAR UP”
ATC - ADVISE
Clean up with the Go Around Drill
SMOKE, FIRE, or FUMES
- Oxygen Mask(which is also smoke goggles) _______ Don, 100%
- Crew and Cabin Crew communications_______ Establish
UPSET RECOVERY
nose high
- Recognize and confirm the developing situation
AP - disengage
AT - disengage
RECOVER:
Nose down
Reduce thrust if required
Roll if required to obtain nose down
Complete recovery:
When approaching horizon Roll wings level
Check airspeed and thrust
Establish pitch attitude
UPSET RECOVERY
nose low
Recognize and confirm the developing situation.
AP - Off
AT - Off
Recover:
Recover from stall if needed
Roll wings level in shortest direction. (Unload and roll)
Complete Recovery:
Apply nose up elevator
Apply nose up trim, if needed
Adjust thrust and drag, if needed
WINDSHEAR RECOVERY
MANUAL FLIGHT
Call “WINDSHEAR, TOGA”
AP - OFF
TOGA - PUSH
THRUST - MAX
AT - OFF
Wings level, pitch 15 degrees
Speedbrakes - retract
Flight director TOGA guidance - follow if available.
AUTOMATIC FLIGHT
Call “WINDSHEAR TOGA”
TOGA - PUSH
TOGA on FMA - Verify
GA THRUST - Verify
Speed brakes - RETRACT
monitor performance.
MANUAL OR AUTO FLIGHT
- Level aircraft as was configured until clear of WINDSHEAR
- Maintain wings level to maximize climb gradient unless turn required for obstacle
- Monitor vertical speed and altitude
- Do not attempt to regain lost airspeed until WINDSHEAR is no longer a factor.
GPWS WARNING
Call “FIREWALL”
AP - OFF
AT - OFF
Thrust - MAX
WINGS LEVEL, initial PITCH 20 degrees
Speedbrakes - Retract
** if Terrain remains a threat, continue rotation to PLI’s or even stick shaker until buffet.
*** DO NOT change aircraft config
Monitor radio ALT
When clear of terrain, slowly decrease pitch and accelerate.
Crew incapacitated
PA - “In-charge flight attendant report to the flight deck”
STABILIZER
Both STABILIZER CUTOUT switches:
CUTOUT
** DO NOT EXCEED CURRENT AIRSPEED
SMOKE or FIRE from Lithium Battery
If necessary transfer aircraft control
PA - “Backup to the flight deck, backup to the flight deck”
*** SMOKE, FIRE, FUMES likely imminent. Complete drill.
AIRSPEED UNRELIABLE
AP - OFF
AT Arm switches - OFF
FDs - Both OFF
Flaps Extended:
85% N1
Pitch 10 degrees up
Flaps Retracted:
70% N1
Pitch 4 degrees up
CABIN ALTITUDE
Oxygen masks - DON
CREW COMM - Establish
Check cabin altitude and Rate
If Uncontrollable:
PAX OXYGEN - ON
DESCEND - Minimum safe Alt or 10,000’, whichever is higher.
ENGINE FIRE
ENGINE SEVERE DAMAGE
ENGINE SEPERATION
All for the affected side engine (Left or Right).
AT ARM SWITCH - CONFIRM OFF
THRUST LEVER - CONFIRM IDLE
FUEL CONTROL SWITCH - CONFIRM CUTOFF
ENGINE FIRE SWITCH - CONFIRM PULL
If the FIRE ENG message shows:
ENGINE FIRE SWITCH - ROTATE to the stop and hold for 1 second.
Checklist..
GO AROUND after touchdown
(Touchdown but before thrust reverser selection) [BALKED LANDING]
Call - “GO AROUND, FLAPS ____” (landing flap or flap, as desired).
AP - OFF
AT - OFF
THRUST - Smoothly advance to GA thrust (config warning will sound due to flaps in the landing flap config)
**Verify SPEEDBRAKES RETRACT and AUTOBRAKES disarm
Maintain landing flap or select Flap 20.
At VREF - Rotate smoothly to 15 degrees
Once airborne:
TOGA BUTTON - PUSH (activates FD and re-engages AT in the THR mode).
Safely Airborne with a positive rate:
Continue normal GO-AROUND and Missed approach procedure.
** If Reverse Thrust is initiated following touchdown you must STOP.
CABIN PRESSURE LIMITS
MAX diff p (relief valves)
Max Cabin diff (TO and Landing)
9.1 PSI
0.11 PSI
Fuel imbalance
13-55
18-40
Max 1360kg when mains greater than 55791kg
Max 1814kg when mains equal or less than 40823kg.
- linear interpolation
Rejected T/O below 80knots
- Engine fail
- Engine fire
- Fire
- Master Warning/Caution
- System Failure
- Unusual noise or vibration
- Window opens
- Tire failure
- WINDSHEAR
- Abnormally slow acceleration
- Aircraft unsafe or unable to fly
- T/O config warning
Rejected T/O above 80kts and below V1
Engine Fail
Engine Fire
Windshear
Aircraft unsafe or unable to fly
MMO
0.89 Mach
VLE/MLE
VLO/MLO
270KIAS/0.82M
Maximum certified Altitude
43,100’
Flight Maneuvering Load Limits
Flaps up:
+2.5g
-1.0g
Flaps down:
+2.0g
-0.0g
With flaps 25-30 positive limits vary linearly from +2.0g at max landing weight to +1.5 at max Take-off weight
DUAL ENG FAIL/STALL
- FUEL CONTROL switches (both)
CUTOFF, then RUN - RAM AIR TURBINE switch
Push and hold for 1 second.
Checklist. Dual Eng fail/stall.
ENG AUTOSTART
Condition: one of these occurs:
AUTOSTART did not start the engine
Fuel control switch is in RUN at low engine RPM with the autostart switch OFF.
1 FUEL CONTROL switch (affected side).
Confirm!… CUTOFF
Fire ENG tailpipe L,R
Condition: an engine tailpipe fire occurs on the ground with no engine warning
- FUEL CONTROL (affected side)
CUTOFF - Advise the cabin.
