M
V REV MOD MP TITLE
T SI VALIDITY
. 035 25888   A.P.U.-POWER PLANT-INTRODUCE
ALLIED SIGNAL APU 131.9IA1

6.2207
6.2209
6.2208
6.2331
6.2332
6.2335
6.2336
6.2337
6.2338
6.2333
6.2334
6.2219
6.2215
6.2220
6.2216
6.2217
6.2222
6.2221
6.2227
6.2226

NAVIGATION-ADIRS-INTRODUCE HONEYWELL
ADIRU 4 MCU ADO9
STD WITH HARDWARE P/N
6.2335
6.2336
6.2337
6.2338
6.2219
6.2220
6.2221
6.2228
6.2229
6.2230
6.6001
6.6002
6.6003
6.6005
6.6008
6.6007
6.6006

. 036 26001   NAVIGATION-ADIRS-INTRODUCE HONEYWELL
4 MCU P/N AC09
6.2335
6.2336
6.2337
6.2338
6.2219
6.2220
6.2221
6.2228
6.2229
6.2230
6.6001
6.6002
6.6003
6.6005
6.6008
6.6007
6.6006
. 027 26335   FLIGHT CONTROLS-GENERAL
DELETION OF L.A.F. FEATURE FROM
A320 A/C (SERIAL SOLUTION
6.2207
6.2209
6.2208
6.2335
6.2336
6.2337
6.2338
6.2219
6.2220
6.2221
6.2228
6.2229
6.2230
6.6001
6.6002
6.6003
6.6005
6.6008
6.6007
6.6006

NAVIGATION - GPWS - ACTIVATE ENHANCED FUNCTIONS OF THE EGPWS ALL

M
V REV MOD MP TITLE
T SI VALIDITY
. 035 26728   INDICATING/RECORDING SYSTEM - FWC -
INTRODUCE FWC STANDARD H2E2
6.2217 6.2227 6.2229 6.6002 6.6008
6.2222 6.2226 6.2230 6.6003 6.6007
6.2221 6.2228 6.6001 6.600S 6.6006
NAVIGATION-TCAS-INSTALL COLINS TCAS II TTR921 P/N 822.1293-320 WITH COLLINS ATC TPR720 OR TPR900
6.2221
 . 033 26910   FLIGHT CONTROL -ELAC SYSTEM
INTRODUCE E.L.A.C. WITH ENHANCED RELAYS
6.2219 6.221S 6.2220
6.2216 6.2217 6.2222
6.2221 6.2227 6.2226
6.2228 6.2229 6.2230
6.6001 6.6002 6.6003
6.600S 6.6008 6.6007
6.6006
AUTO FLIGHT-FMGC-INTRODUCE FMGC CAM0102 FOR A319 AUTOLAND AND GPS/ACARS FOR CFM ENGINES
ALL
 . 030 26999   NAVIGATION - MMR - INSTALL COLLINS MMR
PROVIDING ILS AND GPS FUNCTION
6.2331 6.2332 6.233S
6.2336 6.2337 6.2338
6.2333 6.2334 6.2219
6.221S 6.2220 6.2216
6.2217 6.2222 6.2221
6.2227 6.2226 6.2228
6.2229 6.2230 6.6001
6.6002 6.6003 6.600S
6.6008 6.6007 6.6006
FLIGHT CONTROLS-ELAC SYSTEM-INTRODUCE ELAC SOFTWARE "L80"
ALL

M
V REV MOD MP TITLE
T SI VALIDITY
ELECTRICAL POWER - GENERAL - AC-DC MAIN DISTRIBUTION - INSTALL AC-DC SHEDDABLE BUSBARS
 6.2209 6.2208 6.2331
 6.2332 6.233S 6.2336
 6.2337 6.2338 6.2333
 6.2334 6.2219 6.221S
 6.2220 6.2216 6.2217
 6.2222 6.2221 6.2227
 6.2226 6.2228 6.2229
 6.2230 6.6001 6.6002
 6.6003 6.600S 6.6008
 6.6007 6.6008
NAVIGATION-STANDBY DATA : ALTITUDE AND HEADING - INSTALL INTEGRATED STANDBY INSTRUMENT SYSTEM (ISIS1
 6.2230 6.6001 6.6002
 6.6003 6.600S 6.6008
 6.6007 6.6008
NAVIGATION - MMR - INSTALL SEXTANT MMR PROVIDING ILS (FM IMMUNE1
ALL
NAVIGATION - TCAS - INSTALL ALLIED SIGNAL TCAS COMPUTER P/N 066.S0000-2220 (WITH CHANGE 7.01
 6.2331 6.2332 6.2333
 6.2334 6.221S 6.2216
 6.2217 6.2222 6.2227
6.2226
PNEUMATIC-ENGINE BLEED AIR SUPPLY SYSTEM-INTRODUCE NEW TEMPERATURE CTL THERMOSTATS (SERIAL AND RETROFITI
ALL
NAVIGATION - TCAS - INSTALL COLLINS TCAS COMPUTER TTR-920 P/N 622.8971-322 MTN CHANGE 71
 6.2207 6.2209 6.2208
 6.2336 6.2336 6.2337
 6.2338 6.2219 6.2220

M
V REV MOD MP TITLE
T SI VALIDITY
NAVIGATION - TCAS - INSTALL COLLINS TCAS TTR921 WITH COLLINS ATC TPR901
 6.2228 6.2229 6.2230
 6.6001 6.6002 6.6003
 6.6005 6.6008 6.6007
6.6009
LANDING GEAR-NORMAL BRAKING-INTRODUCE STD 8 BSCU (TWIN VERSION
 6.2219 6.2220 6.2216
 6.2217 6.2222 6.2221
　
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