Memory Items and Manouvers Flashcards
1
Q
ABORTED ENGINE START QRH- 7.1
A
- FUEL CONTROL switch (affected side)…………………CUTOFF
2
Q
CABIN ALTITUDE or Rapid Depressurization QRH- 2.1
A
- Don the oxygen masks
- Establish crew communications
- Check the cabin altitude and rate
- If the cabin altitude is uncontrollable
- If PAX:
- PASS OXY switch - Push and hold for 1 second
- Emergency descent - Initiate
- Thrust levers (both) - Idle
- Speedbrake - UP
- If PAX:
- If structural damage is not suspected:
- Target speed - VMO/MMO
- If strutural damage is suspected:
- Target speed - At or less than current IAS
- Limit airspeed and avoid high manouvering loads
- If JA605F:
- SPeedbrakes may autostow to 50% at 320kts. Do not override until speed less than 315kts
- Transponder - 7700
- Descend to the lowest safe altitude or 10,000ft whichever is higher
3
Q
Dual Engine Failure QRH 7.3
A
- ENG START selectors (both)………………………………………….FLT
- Thrust levers (both)…………………………………………………………Idle
- FUEL CONTROL switches (both)………….CUTOFF then RUN
- IF engine appears stalled OR EGT approaches the maximum EGT limit (960’c) of the Standby Engine Indicator:
- Repeat above step as needed
4
Q
Engine Limit or Surge or Stall QRH 7.7
A
- A/T ARM switch - OFF
- Until engine indications stay within limits or the thrust lever is at idle
- Thrust lever (affected side) - Confirm - Retard
5
Q
ENGINE FIRE or Engine Severe Damage or Separation QRH 8.2
A
- A/T ARM switch - OFF
- Thrust lever (affected side) - Confirm - Idle
- Fuel control switch (affected side) - Confirm - CUTOFF
- Engine fire switch (affected side) - Confirm - Pull
- If the engine fire warning light is illuminated:
- Engine fire switch (affected side) - Rotate to the stop and hold for 1 second
- If after 30 seconds the engine fire warning light stays illuminated:
- Engine fire switch (affected side) - Rotate to the other stop and hold for 1 second
6
Q
UNSCHD STAB TRIM QRH 9.1
A
STAB TRIM CUT OUT switches (both) - CUT OUT
7
Q
Airspeed Unreliable QRH 10.1
A
- Check the pitch attitude and thrust
- If pitch attitude or thrust is not normal for phase of flight:
- Autopilot disengage SW - Push to disengage
- Autothrottle disconnect SW - Push to disconnect
- F/D switches (both) - OFF
- Establish normal pitch attitude and thrust setting for phase of flight
8
Q
AUTOMATIC UNLOCK QRH 1.1
A
- FLT DK DOOR lock selector - Rotate to DENY and hold for 1 second
9
Q
Non-normal Flow
A
- Checklist- Non Normal
- EICAS
- Checklist- Normal
- ATC- Wx & App info- STBY INTENTIONS
- Intentions-Advise
- ATC- Clearance
- Advise Company
- Set CDU- RTE Check
- LDG ALT
- LDG Dist
- RECALL
- LDG setup (Flap, App SPD, Auto-brakes, set your side)
- Set Own side- APP brief, SPDS
- Descent Checklist
- Approach checklist
10
Q
FCC Fail
A
- Lose- ADI, HSI (Not blank, just lose F/D on ADI & Track info on HSI)
- NO LAND 3 appears on ASA
- ACTION- “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”
- INTENTION
- CONTACT COMPANY TO ADVISE
11
Q
ADC Fail
A
- ASI- Blanks, 260 set on SPD
- ALT- Blanks
- VSI- Blanks
- ‘L ENG EEC MODE’ ‘R ENG EEC MODE’
- ACTION- “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______”
12
Q
Go-Around
A
- “Go Around” ( GA SW push)
- “3 GA, Flap 20” “Flap 20, Positive” “Gear Up” “F/D ON” (If rejected LDG) “Gear Up”, Gears Up”
- @ 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” A/S checked, Flap 1” “Flap 1, Flap 1”
- “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”
13
Q
Rejected Take-Off
A
- 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
14
Q
GPWS Warning (‘PULL UP’, ‘TERRAIN TERRAIN PULL UP’ or ‘OBSTACLE OBSTACLE PULL UP’)
A
- Disengage A/P
- Disconnect A/T
- Aggressively apply maximum thrust
- Simultaneously roll wings level and rotate to an initial pitch atttude of 20’
- Set the SPEEDBRAKE lever to 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 is 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’D
- DO NOT USE F/D COMMANDS
15
Q
Windshear Escape Maneuver MANUAL FLIGHT
A
- Disengage A/P
- Push G/A switch
- Aggressively apply MAX thrust
- Disconnect A/T
- Simultaneously ROLL wings LVL and rotate toward an initial pitch ATT of 15’
- Speedbrake lever DOWN
- Follow 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