Abnormal & Emergency Procedures Flashcards
INITIATION OF PROCEDURES
Which procedures must still be performed as memory items because instant action is required?
- REJECTED TAKE OFF
- STABILIZER TRIM RUNAWAY
•EXCESSIVE ASSYMETRY OR LOSS OF
BREAKING
•CONFIGURATION WARNING
MONITORED ACTIONS
Monitored actions contained in the A + E List are only to be considered in-flight and are movement of :
• Thrust Levers (if leading to an engine shutdown within the procedure) • Eng Fire Push Switches • APU Fire Push Switches • Engine Boost Pumps • Eng Gen Switches / IDG disconnect switches / lights • Roll and Pitch disconnect handles • IRS switching • Landing Gear Manual Release Handle
HANDLING OF A AND E PROCEDURES DURING APPROACH
If during approach an abnormal or emergency condition occurs continue approach or initiate go-around - taking into account weather situation, runway condition, aircraft status and kind of malfunction
• DOWN TO 2.000 ft AGL :
Perform A and E Procedures
according QRC / QRH
• BETWEEN 2.000 ft AGL and 1000 ft AGL :
Immediate Action Items according QRC
• BETWEEN 1.000 ft AGL and TOUCHDOWN :
No Immediate Action Items during a
stabilized approach
PRINCIPLES
Priority for Crew actions to handle the situation is (7) :
- Fly the aircraft
- Red warnings
- Electrical failures
- Hydraulic failures
- Pneumatic failures
- Minor engine
- Others
ENGINE FAILURE DURING APPROACH
If an engine failure occurs during approach the following actions MAY be performed non
standard by heart. However A/C stabilization must be achieved at 1.000 ft AGL
• AUTOPILOT DISC PF
• THRUST LEVER / OPERATING
ENGINE ADVANCE PF
- FLAPS SELECT PM (Flaps 20)
- AIRSPEED ADJUST PF (Vref 45 + 12)
• GPWS / FLAPS OVRD switch SELECT PM
(to mute flap aural warning)
SINGLE ENGINE GO-AROUND
CREW COORDINATION
(to 600ft A/P ON)
“GO AROUND, FLAPS 8, MAX
THRUST”
—> “Max thrust set”
“POSITIVE CLIMB” —> “Gear Up”
“SPEED, HEADING, HALF BANK”
passing 600 ft
“AUTOPILOT ON” —> “AUTOPILOT IS ON”
SINGLE ENGINE GO-AROUND
CREW COORDINATION
(at acceleration altitude)
After accelerating to Vfto
“FLAPS 1” … “FLAPS 0”
“MAX CONTINUOUS THRUST”
—> “MAX CONTINUOUS THRUST SET”
HALF BANK OFF
“AFTER T/O CHECKLIST”
ENG FAIL AFTER V1 - CREW COORDINATION
“ENG FAILURE”
“MAX THRUST”
-> “Max thrust set”
“Rotate” -> “Pos climb” -> “gear up”
“SPEED , HEADING, HALF BANK”
at 600 ft “AUTOPILOT ON”
“WHATS THE PROBLEM ?”
-> “ENG FAIL NO. ..”
-> “ENG FAIL NO. .. IS CONFIRMED, INFORM
ATC”
“MAYDAY MAYDAY MAYDAY LH..., WE HAVE
AN ENGINE F...”
EOSID
REJECTED TAKE-OFF
A rejected take-off is required when the following situations occur.
- Thrust Loss
* A/C not controllable or not flyable
REJECTED TAKE-OFF
above 80 kts
- Fire Warning
- Unsafe Configuration
- Runway Intrusion
- Bird Strike danger (flicks of birds)
- Windshear
REJECTED TAKE-OFF
below 80 kts
- System failures
- Tire failure
- Unsual Noise or Vibration
• Caution light ON (depending on
fleet syst.)
STALL RECOVERY PROCEDURE
AUTOPILOT -> OFF
PITCH ATTITUDE -> LOWER
„STALL / MAX THRUST“ -> CALL OUT
ROLL -> WINGS LEVEL
FLIGHT SPOILERS -> RETRACT
PITCH ATTITUDE -> ADJUST
UPSET RECOVERY
NOSE HIGH
„UPSET“ -> CALL OUT
„I HAVE CONTROL“ -> PF
- A/P DISC
- Pitch Angle reduce
- Roll adjust as required (not exceeding 60^)
- Thrust as required
- Flight spoilers as required
UPSET RECOVERY PROCEDURE
NOSE LOW
„UPSET“ -> CALL OUT
„I HAVE CONTROL“ -> PF
• A/P DISC
• Pitch Angle PUSH TO UNLOAD and
recover to horizon
• Roll to shortest direction to wings level
• Thrust as required
• Flight spoilers as required
• Spoilers as required
• Pitch angle increase use control column
and pitch trim to bring the A/C back to level
flight. Avoid high load factors.
EGPWS ENCOUNTER
„MAX THRUST“ -> CALL PF
AP - DISC
INITIATE PULL UP
RETRACT FLIGHT SPOILERS
NO CONFIGURATION CHANGE UNTIL VERTICAL FLIGHT PATH IS UNDER CONTROL
CLIMB AT BEST CLIMB ANGLE RESPECT STICK SHAKER UNTIL ALL ALERTS CEASE
