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
WINDSHEAR WARNING
During T/O , after Vr , during Initial Climb
„MAX THRUST“ -> CALL PF
„MAX THRUST SET“
WINDSHEAR ESCAPE GUIDANCE -> FOLLOW
Escape guidance commands override all other
FD modes
Escape guidance commands override all other HGS modes
Follow commands presented on the PFD or HGS combiner ->
DO NOT EXCEED AMI
WINDSHEAR WARNING
During Approach / Landing
„MAX THRUST“ -> CALL PF
simultaneously press TOGA switch
„MAX THRUST SET“
FLIGHT SPOILERS -> RETRACT
WINDSHEAR ESCAPE GUIDANCE -> FOLLOW
A/C CONFIGURATION-> MAINTAIN
FLIGHT INST -> MONITOR (call out changes)
Escape guidance commands override all other HGS modes
Follow commands presented on the PFD or HGS combiner ->
DO NOT EXCEED AMI
TCAS TRAFFIC ADVISORY DURING FLIGHT
„TRAFFIC, TRAFFIC“
TFC switch -> PRESS BOTH
„TCAS, I HAVE CONTROL“ -> CALL PF
TCAS WARNING INHIBITIONS
„INCREASE DESCENT“ ->
inhibit
below 1450 ft AGL (descent) or
below 1650 ft AGL (climb)
„DESCENT“ ->
inhibit
below 1000 ft AGL (descent) or
below 1200 ft AGL (climb)
TA ONLY ->
inhibit
below 900 ft AGL (descent)
below 1100 ft AGL (climb)
TA‘s -> inhibit below 380 ft AGL
TCAS aural advisories - >
inhibit
below 400 ft AGL (descent)
below 600 ft AGL (climb)
