Flashcards in Memory Items and Manouvers Deck (29)
ABORTED ENGINE START(Memory Item)QRH- 7.1
FUEL CONTROL switch (affected side)....CUTOFF
CABIN ALTITUDE or Rapid Depressurization(Memory Item)QRH- 2.1
Dual Engine Failure(Memory Item)QRH- 7.3
ENG START selectors (both).....FLTThrust levers (both)......................IdleFUEL CONTROL switches (both).....................CUTOFF then RUNIF engine appears stalled OR EGT approaches the maximum EGT limit (960'c) of the Standby Engine Indicator:Repeat above step as needed
Engine Limit or Surge or Stall(Memory Item)QRH- 7.7
A/T ARM switch........OFFUntil engine indications stay within limits or the thrust lever is at idle,Thrust lever(affected side).....Confirm....Retard
(L, R) ENGINE FIRE or Engine Severe Damage or Separation(Memory Item)QRH- 8.2
UNSCHD STAB TRIM(Memory Item)QRH- 9.1
STAB TRIM CUT OUT switches (both)........CUT OUT
Airspeed Unreliable(Memory Item)QRH- 10.1
Check the pitch attitude and thrustIf pitch attitude or thrust is not normal for phase of flight:Autopilot disengage SW..........Push to disengageAutothrottle disconnect SW....Push to disconnectF/D switches (both)...................OFFEstablish normal pitch attitude and thrust setting for phase of flight.
AUTOMATIC UNLOCK(Memory Item)QRH- 1.1
FLT DK DOOR lock selector....Rotate to DENY and hold for 1 second
Checklist- Non NormalEICASChecklist- NormalATC- Wx & App info- STBY INTENTIONSIntentions-Advise ATC- ClearanceAdvise CompanySet CDU- RTE CheckLDG ALT, RECALLLDG setup (Flap, App SPD, Auto-brakes, set your side)Set Own side- APP brief, SPDSDescent Checklist, Approach checklist?
Lose- ADI, HSI (Not blank, just lose F/D on ADI & Track info on HSI)NO LAND 3 appears on ASAACTION- "Left ADI/ HSI blank, check Right side". "Right side normal""You have control (Modes)""______ FCC Fault, FLT DIR (C,R)""Left ADI, HSI normal, I have control". "You have control""Check EICAS message"INTENTIONCONTACT COMPANY TO ADVISE
ASI- Blanks, 260 set on SPDALT- BlanksVSI- Blanks'L ENG EEC MODE'R ENG EEC MODEACTION- "Air SPD, Altimeter, Vertical SPD failure, check Right side". "Right side normal""You have control (Modes)""______ ADC Fail, ____ ADC SW ALTN"AIRSPEED_____, ALT______, VS______". "Same as right side""Left Side back on normal, I have control" "You have control""Check EICAS message". "L & R ENG EEC MODE""ENG EEC MODE CHECKLIST""Check EICAS MSG""Left ADC FAIL, now flying with RIGHT ADC, non RVSM, Contact ATC and advise Unable RVSM request next highest level to FL290""Contact company advise situation, request fuel figures for FL______"
"Go Around" ( GA SW push) "3 GA""3 GA, Flap 20" "Flap 20, Positive""Gear Up""F/D ON" (If rejected LDG) "Gear Up", Gears Up no light"@ OR ABV 400ft"LNAV/ HDG SEL" "LNAV/ HDG SEL"@1500ft"Set CLB Thrust"@ ALT CAP"SPD, ALT CAP""SPD Set to VREF+60"@ VREF + 20"A/S Checked, Flap 5" "Flap 5, Flap 5 no light"A/S checked, Flap 1" "Flap 1, Flap 1 no light""ATO CHECKLIST""Check Weather/ APP INFO""Request RV ILS""Set CDU, ILS RWY ___, INTC CF___ , CRS ___, MAP _____ft""VREF 30 is ____ Bug set""RV ILS ____, procs same as before""Check Recall""Descent & APP checklist"
-THRUST LEVERS- CLOSE (Disconnect A/T if BLW 80kts)-VERIFY OPERATION OF AUTOBRAKES OR APPLY MAXIMUM ALLOWABLE BRAKING-MAXIMUM ALLOWABLE REVERSE THRUST(If speed brake lever did not move UP automatically)SPEEDBRAKE LEVER UP-Continue maximum braking till A/C is decelerated sufficiently-when flight is not continued perform after LDG procedures-When flight is continued see T/O weight limit by brake temp as described in chapter 2
GPWS Warning('PULL UP', 'TERRAIN TERRAIN PULL UP' or 'OBSTACLE OBSTACLE PULL UP')
Disengage A/PDisengage A/TAggressively apply MAX thrustSimultaneously roll wings LVL & pitch to 20'SPEEDBRAKE lever DOWN-If terrain remains a threat, continue rotation up to pitch limit indicator, stick shaker or initial buffet.-Do not change flap or gear configuration until terrain separation assured.-Monitor RADALT for sustained or increasing terrain separation.-When clear of terrain, slowly decrease pitch attitude and accelerate.FLIGHT AT STICK SHAKER MAY BE REQ'DDO NOT USE F/D COMMANDS
Windshear Escape Maneuver MANUAL FLIGHT
Disengage A/PPush G/AAggressively apply MAX thrustDisconnect A/TSimultaneously ROLL wings LVL and rotate toward an initial pitch ATT of 15'Speedbrake lever DOWNFollow FD guidance (If avail)-Do not change GEAR & FLAP config until WS no longer a factor.-Monitor VS and ALT-Do not attempt to regain lost A/S until WS no longer a factor
Windshear Escape ManeuverAUTOMATIC FLIGHT
Push G/A Verify GA mode annunciationVerify thrust levers advance to GA powerSpeedbrake Lever- DOWNMonitor system performance-Do not change GEAR & FLAP config until WS no longer a factor.-Monitor VS and ALT-Do not attempt to regain lost A/S until WS no longer a factorIF GA MODE UNAVAIL FLY MANUALLY!
ENG Failure in Final APP?
-Advance operating ENG to GA position-Retract to Flaps 20-Maintain VREF 30+10kts (Equivalent to VREF Flap 20)DECIDE GA or CONTINUEGA- Maintain VREF 30+10kts & execute GA proc(Flap5, "positive" gear up)CONTINUE- Maintain SPD conduct OEI LDG.
If manoeuvring is Req'dA/P- DISENGAGEA/T- DISCONNECTSmoothly adjust pitch & thrust to satisfy RA command-If stick shaker occurs, accomplish stall recovery procedure-If high speed buffet occurs, relax pitch force to reduce buffet but continue the manoeuvre-Do not use F/D commands until clear of conflict
CLB RA in LDG CONFIG
A/P- DISENGAGEA/T- DISCONNECTT/L- FULL FORWARDCall "Flaps 20"Smoothly adjust pitch to satisfy the RA command. "POSITIVE""GEAR UP"
Nose HIGH Recovery
Recognize & ConfirmDISENGAGE A/P & A/TApply as much FULL DOWN ELEVATOR/ TRIMREDUCE ThrustROLL to obtain nose down pitch rate-When approaching HORIZON, roll wings LVL-Check A/S & adjust Thrust-Establish pitch ATT
Nose LOW Recovery
Recognize & ConfirmDISENGAGE A/P & A/TRECOVER from Stall (if req'd)ROLL in shortest direction to wings LVLRECOVER to LVL flight-apply nose up elevator/ trim-adjust thrust/drag as req'd
What is an UPSET defined as?
>25' Nose UP>10' Nose DOWNAOB> 45'A/S inappropriate for conditions
Approach to Stall or Stall Recovery
Initiate the Recovery:-Hold control column firmly-Disengage A/P A/T-Smoothly apply NOSE DOWN elevator to reduce AOA until buffet or stick shaker stops (Trim may be req'd)Continue the Recovery:-ROLL in shortest direction to wings LVL-ADVANCE thrust-SPEEDBRAKE - DOWN-Do not change Gear & Flap except during liftoff if Flaps are UP call for Flaps 1Complete the Recovery:-Check A/S and adjust thrust as req'd-Establish pitch ATT-Return to desired flight path-Re-engage A/P & A/T
Aborted Engine Start
-No EGT increase by 25 sec after fuel cont switch is moved to run-No N1 rotation by 30 seconds after N2 is stabalized at idle-EGT quickly or near exceeds the start limit-Oil pressure indication is not normal by time the engine is stabalized at idle
What are the two indications A/C is in WIndshear?
1.) "WINDSHEAR, WINDSHEAR, WINDSHEAR"Immediate alertExcessive Windshear at A/P current positionEnabled BLW 1,500ft RAD ALTDetection begins at rotation2.) Unacceptable flight path deviations
What are Unacceptable flight path deviations?
Uncontrolled changes from normal steady state flight conditions BLW 1,000ft AGL in excess of:15 KIASVS 500fpm5' pitch ATT1 dot displacement from GSUnusual thrust lever position for a significant amount of time.
Steep turn method?
-Cabin sign ON-VOR mode (PF)-A/S=250ktsDES & APP CheckPWR- 66% (280t-61%)ATT- 2- 2.5'ROLLING INTO TURN (Use fast slow pointer if 250kts bugged)ADD PWR- 3%(280t-64%)ATT- 2.5- 3'ROLLING OUT OF TURN15' to go start rolloutPWR- 66% (280t-61%)ATT- 2- 2.5'
"GO AROUND WINDSHEAR AHEAD"
Enabled during APP BLW 1,200ft AGLWindshear within 1.5 nm & DIRECTLY ahead of planeIf WX not selected on HSI, PWS symbology will auto pop upshows position & size only when HSI in VOR,APP,MAP,CTR MAP mode.Perform Windshear escape maneuver