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· Repeat until landing configuration is reached.
No flaps no slats landing is a fairly simple procedure, however more room is required for
maneuvering. The flap handle should be placed in the CONF 1 position so that FD
go-around modes (SRS and GA TRK) are available in the event of a go-around. During
approach the aircraft pitch attitude will be unusually high, therefore a tail strike is more of a
concern and only a minimal flare is required.
Consider fuel available and the quantity that may be required if a diversion is necessary with
flaps and/or slats jammed.
The autopilot may be available but monitor its operation closely as it is only authorized for
use in normal configuration. However, do not use the autopilot below 500 ft AGL.
A319/A320/A321
FLIGHT CREW TRAINING MANUAL
1.03.27 Page 2
REV 21 MAY 98
ABNORMAL OPERATION BRIEFINGS
FLIGHT CONTROLS
CHAP03\27
ABNORMAL FLAPS/SLATS CONFIGURATION (END)
06 - COMPLETION STANDARDS
· Correctly responds to failure ensuring a safe flight path and speed.
· Performs ECAM actions and QRH procedures in a methodical manner.
· Makes correct adjustments to VAPP and selects appropriate configuration.
· Makes smooth and accurate approach and lands within the touchdown zone at the correct
speed (+10 / - 0 kts).
07 - COMMON ERRORS
· Rushing procedure.
· Starting approach before completing all procedures.
· Selected speed not used immediately at failure recognition.
· Wrong VAPP selection on MCDU.
· Rough handling.
· Use of managed speed on final approach
· Incorrect go around procedure.
A319/A320/A321
FLIGHT CREW TRAINING MANUAL
1.03.27 Page 3
REV 21 MAY 98
ABNORMAL OPERATION BRIEFINGS
FLIGHT CONTROLS
CHAP03\27
RECONFIGURATION LAWS - RECOVERY FROM APPROACH TO STALL
01 - TRAINING OBJECTIVE
· To recognize the indications of an impending stall.
· To take immediate and appropriate actions to recover to controlled flight.
02 - SCHEDULE
Briefing duration : 20 minutes
03 - EQUIPMENT
DOC references :
· FCOM 1.27.30 (Abnormal control laws)
· FCOM 3.04.27 (Supplementary Techniques - Flight controls)
04 - INSTRUCTOR’S ACTIONS
Briefing of the following key points.
MAIN
· Stall possible only in Alternate and Direct laws ("Fly-by-wire" aircraft).
· Speed scale symbols change (VSW) and aural warning.
· Recovery technique according to altitude and configuration.
SECONDARY
· Control of pitch
· Risk of secondary stall
A319/A320/A321
FLIGHT CREW TRAINING MANUAL
1.03.27 Page 4
REV 21 MAY 98
ABNORMAL OPERATION BRIEFINGS
FLIGHT CONTROLS
CHAP03\27
RECONFIGURATION LAWS - RECOVERY FROM APPROACH TO STALL (CONT’D)
05 - TRAINEES’ ACTIONS
The conventional stall is only possible in alternate and direct control laws, because of the
protections provided in normal law. Alternate or direct law will be indicated by ECAM and the
changes on the PFD ; bank angle and pitch limitation replaced by amber X, low speed
indications change from alpha prot. to VSW. VSW is load factor dependant and will increase
with increase in pitch up rate or bank angle.
Also, an aural warning is produced on entering the stall regime. This aural warning is
produced by the AOA sensors not the FACs. It is possible to experience "false warnings" if
pitch control is rough during the recovery from the stall. VSW indications are always correct
as these are generated by the FACs.
INDICATION ........................................................................................"STALL, STALL, STALL"
THRUST LEVERS...............................................................................TOGA
At the same time :
PITCH ATTITUDE................................................................................REDUCE
BANK ANGLE......................................................................................ROLL WINGS LEVEL
SPD BRAKES......................................................................................CHECK RETRACTED
If a danger of ground contact exists, reduce pitch attitude no more than necessary to allow
airspeed to increase.
After initial recovery, maintain speed close to VSW until it is safe to accelerate.
If below 20,000 ft, and in clean configuration, select CONF 1.
Out of stall when there is no threat of ground contact:
LANDING GEAR..................................................................................UP
Recover to normal speed and retract flaps as required.
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