Proficiency Items Flashcards
Crew Incapacitation COM 3.80.14
C—Call FA S—Secure or Remove Crew Member A—Attendant Stays if Crew Member Unmovable Dr—On Board Aircraft P—Pilot typed from our company onboard
Severe Turbulence COM 3.220.11
Signs …………………………………………………………..ON
AUTOPILOT………………………………………..KEEP ON
A/THR (if thrust changes become excs) …………OFF
Turbulence Speed ……………………………………….SET
ALTITUDE ……………………………………Do Not Chase
Descent………………………….Consider(Buffet Margin)
Approach: ……………A/THR in managed speed USE
Landing: ………………………Configuration FULL, or 3
One Engine Inop Strategy COM 3.10.18
IN CRUISE (DO NOT DECEL BELOW GREEN DOT) M—MCT all Thrust Levers A—A/THR: OFF H—HDG Set and Pull as Appropriate D—Determine Drift Down Altitude (PERF-CRZ PAGE) N—Notify ATC S—Start ECAM/OEB Actions When Appropriate DRIFT DOWN S—SPD on FCU: GREEN DOT - PULL A—ALT on FCU: Selected Cruise FL - PULL *If obstacle problem exists, continue drift down procedure. *When obstacles are cleared, accelerate to Long Range Speed. CRUISE LONG RANGE SPEED S—PD on FCU: SET A—/THR: ON DESCENT TO LANDING IDLE M.78/300kt/250kt
STALL WARNING AT LIFT OFF
“STALL TOGA 15°”
THRUST ………………………………………………….TOGA
PITCH ATTITUDE………………………………………….15°
BANK………………………………………….WINGS LEVEL
NOTE:When a safe flight path and speed are achieved and maintained, if stall warning continues, consider it as spurious.
Stall Recovery COM 3.10.26
“STALL I HAVE CONTROL”
NOSE DOWN PITCH CONTROL………………..APPLY
BANK………………………………………….WINGS LEVEL
- When out of stall (no longer stall indication):
THRUST ………INCREASE SMOOTHLY AS NEEDED
SPEED BRAKES …………………CHECK RETRACTED
FLIGHT PATH…………………..RECOVER SMOOTHLY
If in clean configuration and below 20,000 ft:
- FLAP 1 - SELECT
WINDSHEAR (RED FLAG/3 AURAL)
AT TAKEOFF:
Before V1…………………………………………..CONSIDER REJECT
AFTER V1:
“WINDSHEAR TOGA”
THR LEVERS…………………………………………………………..TOGA
REACHING VR……………………………………………………..ROTATE SRS ORDERS……………………………………………………..FOLLOW
Airborne, initial climb or landing:
THR LEVERS AT TOGA …………………………SET OR CONFIRM
AP (if engaged) ………………………………………………….KEEP ON
SRS ORDERS……………………………………………………..FOLLOW
• DO NOT CHANGE CONFIG TILL OUT OF WINDSHEAR
• CLOSELY MONITOR FLIGHT PATH AND SPEED
• RECOVER SMOOTHLY TO NORMAL CLIMB
FAC Functions
- Y—Yaw Control
- A—Airspeed Prot. Computations (⍺Prot/Hi-Lo)
- W—Windshear Protection
- L—Low Energy Warning
ADR Computers Provide
- B—Barometric Altitude
- O—Overspeed Warning
- A—Angle of Attack
- T—Temperature
- S—Speed/Mach
SEC Functions
- S—Speed Brakes/Ground Spoilers
- A—Alternate Pitch
- D—Direct Pitch
- D—Direct Roll
- A—Abnormal Attitude
- N—Normal Roll Via Spoilers
IR Computers Provide
- F—Flight Path Vector
- A—Attitude
- A—Acceleration
- T—Track
- H—Heading
- A—Aircraft Position
- G—Ground Speed
ELAC Functions
- N—Normal Elevator, Aileron, Pitch & Roll
- A—Alternate Pitch
- D—Direct Pitch & Roll
- A—Abnormal Attitude
- A—Aileron Droop
- A—Autopilot Orders
Normal Law Protections
- B—Bank Angle Protection
- S—Speed Protection
- L—Load Factor Protection
- A—Angle of Attack Protection (⍺Prot)
- P—Pitch Angle Protection
Alpha Prot
- A—⍺ is commanded instead of Load Factor
- S—Speed Brake is Retracted
- A—Autopilot is disengaged
- P—Pitch Trim is inhibited
Spoilers Inhibited When
- S—SEC 1 and SEC 3 Failure
- A—Alpha Prot. or Alpha Floor
- F—Flaps in Config Full
- E—Elevator Failure (1)
- T—TOGA Thrust
Hydraulic PTU Pump Fault Light
- O—Overheat Reservoir
- L—Low Reservoir Quantity
- L—Low Reservoir Air Pressure
Low Energy Warning Inhibited When
- F—Flaps 1 or 0
- A—Alpha Floor
- T—TOGA
- R—RA Failure
- A—Altitude above 2000 RA or below 100 RA
- G—GPWS Alert
- N—Normal Law Not Active
Hydraulic Engine Pump Fault Light
- P—Pump Low Pressure
- O—Overheat Reservoir
- L—Low Reservoir Quantity
- L—Low Reservoir Air Pressure
Electrical Priority
- G—Generator
- E—External Power
- A—APU
- R—RAT
- B—Batteries
Hydraulic Electric Pump Fault Light
- P—Pump Low Pressure
- O—Overheat Reservoir
- L—Low Reservoir Quantity
- L—Low Reservoir Air Pressure
- O—Overheated Pump
Wing Tip Brakes Engage (4 red collared breakers)
- R—Runaway
- O—Overspeed
- A—Asymmetry
- M—Movement Un-commanded
Engine Bleed Valve Closes
- A—APU Bleed On
- S—Starter Valve Open (Engine)
- O—Overpressure
- L—Leak (Bleed)
- O—Overheat
Ditching Push Button Closes
- C—Cargo Isolation Valve
- R—Ram Air Inlet
- A—Avionics Inlet and Extract Valve
- P—Pack Flow Control Valves
- O—Out Flow Valve
IDG Fault Light
- HOT—High Oil Temp
* LOP—Low Oil Pressure
Engine Starter Master Fault Light
- M—Malfunction of Thrust Lever
- A—Auto Start Abort
- D—Disagree Between HP Fuel Valve
Continuous Ignition Automatic When
- M—Master is Cycled
- E—EIU Data Failed
- E—Engine Flameout or Surge
- E—Eng. Anti-Ice On
- A—Approach Idle Selected
- T—Take Off Thrust Selected
ECAMS Not Inhibited During T/O or Landing
- F—Fire
- E—Engine Failure
- L—Low Oil Pressure
- E—Elevator Fault
- A—Auto Pilot Off
- C—Config Warning
- F—FWC Fault
