A319/A320/A321
onsalwil.,,
ABNORMAL AND EMERGENCY
REV 35
2.30
SEQ 001
RH AFT CABIN DOOR SLIDE DISARM
LEAST RISK BOMB LOCATION (LRBL) PREPARE
Build up a platform of solid baggage against the door up to about 25 cm (10 in) below the middle of the door.
On top of this, build up at least 25 cm (10 in) of wetted material such as blankets and pillows.
Place a single thin sheet of plastic (e.g. trash bag) on top of the wetted materials. This prevents any possible short circuit.
BOMB MOVE TO LRBL
Carefully carry in the attitude found and place on top of the wetted materials in the same attitude and as close to the door structure as possible.
LEAST RISK BOMB LOCATION COMPLETE
Place an additional single thin sheet of plastic over the bomb.
Build up at least 25 cm (10 in) of wetted material around the sides and on top of the bomb. DO NOT PLACE ANYTHING BETWEEN THE BOMB AND THE DOOR AND MINIMIZE AIRSPACE AROUND THE BOMB.
The idea is to build up a protective surrounding of the bomb, so that the explosive force is directed in the only unprotected area into the door structure.
Fill the area around the bomb with seat cushions and other soft materials such as hand luggage (saturated with water or any other inflammable liquid) up to the cabin ceiling, compressing as much as possible. Secure the LRBL stack in place using belts, ties, or other appropriate materials. The more material stacked around the bomb, the less the damage will be.
USE ONLY SOFT MATERIAL. AVOID USING MATERIALS CONTAINING ANY INFLAMMABLE LIQUID AND ANY METAL OBJECTS WHICH COULD BECOME DANGEROUS PROJECTILES.
EVACUATION/DISEMBARKATION EXECUTE
Evacuate through normal and emergency exits on the opposite side of the bomb location. Do not use the door just opposite the bomb.
Use all available airport facilities to disembark without delay.
A319/A320/A321
occilml.+7
ABNORMAL PROCEDURES
REV 36
2.31
SEQ 180
VAPP DETERMINATION
R • NORMAL CONFIGURATION (OR NO AVREF)
R The FMGS performs the following VAPP computation for landing in
R normal configuration (CONF 3 or CONF FULL). These VAPP also
R apply for failure cases without AVREF.
W(1000Kg)
44
48
52
56
60
64
68
72
76
VLS CONF FULL (KT)
111
113
117
122
126
130
134
138
142
VLS CONF 3 (KT)
113
118
123
128
132
137
141
145
149- - -
CORRECTION
1/3 HEADWIND
5KT (EXCLUDING GUST)
MAX=15KT
WHICHEVER IS HIGHER
-VAPP
VAPP = MAX(VLS + 5kt*; VLS + WIND CORR)
The 5 knot increment is required when the A/THR is used, or when an autoland is performed.
NOTE: * — In case of ice accretion, Vapp must not be lower than
— VLS + 5 knots in CONF FULL
— VLS + 10 knots in CONF 3
— In case of gusty crosswind greater than 20 knots, Vapp should be at least VLS + 5 knots.
R • ABNORMAL/EMERGENCY CONFIGURATION (WITH AVREF)
W(1000Kg)
44
48
52
56
60
64
68
72
76
VREF=VLS CONF FULL
111
113
117
122
126
130
134
138
142AVREF
WIND CORRECTION
AVREF> 20KT
AVREF< 20KT
NO WIND
CORRECTION
1/3 HEADWIND
( A VREF + WIND CORR
LIMITED TO 20KT)V APP = VREF + LVREF WIND CORRI
TO BE INSERTED ON MCDU PERF APPR PAGE
A319/A320/A321
ontTril.,,
ABNORMAL PROCEDURES
REV 36
2.32
SEQ 201
LDG CONF - APPR SPD
LDG DIST
CORRECTIONS FOR FAILURES
FLAPS LEVER
POSITION
FOR LDG
APPR SPD:
INCREMENT
TO VREF
(A VREF)
MULTIPLY
LDG DIST
CONF FULL BY
ELEC
EMER ELEC CONFIG
3
10
1.9
DC EMER CONFIG
NORM (1)
1.6
DC BUS 1 + 2
NORM (1)
1.6
DC BUS 2
NORM (1)
1.1
DC ESS BUS/AC BUS 1
NORM (1)
Negl.
FLT
CTL
ALTN LAW/DIRECT LAW
ELAC 1 + 2/
STAB JAM/ L + R ELEV FAULT
3
10
1.2
L(R) ELEV FAULT
3
15
1.2
One SPLR FAULT (except n° 5)
NORM (1)
1.1
Two or three SPLR FAULT
NORM (1)
1.1
More than three SPLR FAULT
NORM (1)
1.2
SEC 1 or 3 FAULT
NORM (1)
1.1
SEC 2 FAULT
NORM (1)
Negl.
SEC 1 + 3 FAULT 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A319/A320/A321 QUICK REFERENCE HAND BOOK(29)
