CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES
GENERAL - DESIGN WEIGHTS -CERTIFICATION OF A321-200 DESIGN WEIGHT 89 T/75,5 T/71,5 T CORRECTION/ADDITION/AMPLIFICATION MODIFIED TEXT FOLLOWING REVISION OF SB 32-1007 (REV12). EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
32-41-00 EFFECTIVITY UPDATED 402- 404, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 409- 411
32-41-00 EFFECTIVITY UPDATED 631, 640-MOD.28136K5939 INCORPORATED 641, 647-GENERAL - INCREASE DESIGN WEIGHT TO : 655 70,0T MTOW, 62,5T MLW, 58,5T MZFW
(WV005)
LAYOUT IMPROVED/MATERIAL RELOCATED
EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
32-41-12 EFFECTIVITY UPDATED 401, 403-EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 404, 408-412
32-42-00 TOPIC CANCELLED 1-A045
32-42-00 01 DELETION OF CALL OUT POST SB 32-1232 01 1-A042 LANDING GEAR - NORMAL BRAKING - INTRODUCE STD 9 BSCU (TWIN VERSION) FROM STD 7. SUPERSEDED BY CONFIGURATION(S)
EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
32-42-00 02 MOD.20011P0003 INCORPORATED
1-94 ELECTRICS- GENERATION- DISTRIBUTION-V.U.'S AND AVIONICS- DEFINE SYSTEMS OF THE BASIC AIRCRAFT-MOD.20044P0024 INCORPORATED LANDING GEAR - MAIN LANDING GEAR (TWIN WHEEL)
-INSTALL MHB CARBON WHEELS AND BRAKES MOD.26925P4576 INCORPORATED LANDING GEAR-ALTERNATE BRAKING-INTRODUCE MODIFIED ALTERNATE BRAKING SYSTEMALL
ALL
001-049, 101-149, 151-199,
201-299, 301-399, 401-499,
151-199, 401-499,
ALL
001-049, 101-149, 151-199,
201-299, 301-399, 401-499,
001-049, 101-149, 151-199,
201-299, 301-399, 401-499,
001-049, 051-099, 101-149,
151-199, 201-299, 301-399,
001-049, 051-099, 101-149,
151-199, 201-299, 301-399,
001-049, 051-099, 101-149,
151-199, 201-299, 301-399,
401-499,
401-499,
401-499,
32-HIGHLIGHTS Page 11 of 28
REVISION NO. 30 Aug 01/05
CES
CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES
MOD.26965P4808 INCORPORATED LANDING GEAR-WHEELS AND BRAKES-INTRODUCE BSCU COMMON STD NEW TOPIC/NEW CONFIGURATION
32-42-00 MOD.26925P4576 INCORPORATED 303- 304, LANDING GEAR-ALTERNATE BRAKING-306, 308-INTRODUCE MODIFIED ALTERNATE 310 BRAKING SYSTEM
CIRCUIT BREAKER(S) DATA UPDATED EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
32-42-00 EFFECTIVITY UPDATED 402- 404, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 407- 408, 414- 415, 428
32-42-00 EFFECTIVITY UPDATED 501- 505, MOD.26925P4576 INCORPORATED 507- 542 LANDING GEAR-ALTERNATE BRAKING-
INTRODUCE MODIFIED ALTERNATE BRAKING SYSTEM MOD.33905P7832 INCORPORATED LANDING GEAR - BRAKE COOLING - INSTALL UNIVERSAL BRAKE COOLING FAN ASSY COMMON TO LR, WB AND SA PROGRAM A/C CIRCUIT BREAKER(S) DATA UPDATED EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
32-42-13 EFFECTIVITY UPDATED 401- 403, CIRCUIT BREAKER(S) DATA UPDATED 406- 410, 413, 416-EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 417
32-42-16 EFFECTIVITY UPDATED 402, 404-EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 405, 407, 409- 410, 412- 413, 416- 417, 427- 428
32-42-22 MOD.20011P0003 INCORPORATED 401- 409 ELECTRICS- GENERATION- DISTRIBUTION-
CES 401-499,
401-499,
ALL
401-499,
001-049, 051-099, 101-149,151-199, 201-299, 401-499,
ALL
051-099, 301-399, 401-499,
051-099, 301-399, 401-499,001-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
001-049, 051-099, 101-149,151-199, 201-299, 301-399,001-049, 051-099, 101-149,151-199, 201-299, 301-399,
004-049, 053-099, 101-149,151-199, 201-299, 301-399,401-499,
401-499,
32-HIGHLIGHTS Page 12 of 28 REVISION NO. 30 Aug 01/05CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES
V.U.'S AND AVIONICS- DEFINE SYSTEMS OF THE BASIC AIRCRAFT-MOD.20577P0907 INCORPORATED ELECTRICAL INSTALLATION-MODIFY CIRCUIT BREAKERS LO CATION IN 121VU MOD.26925P4576 INCORPORATED LANDING GEAR-ALTERNATE BRAKING-INTRODUCE MODIFIED ALTERNATE BRAKING SYSTEM NEW TOPIC/NEW CONFIGURATION
32-42-27 EFFECTIVITY UPDATED 402- 404, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 406, 409-411
32-42-27 EFFECTIVITY UPDATED 602- 603, MOD.26925P4576 INCORPORATED 605, 609, LANDING GEAR-ALTERNATE BRAKING-611- 613 INTRODUCE MODIFIED ALTERNATE
BRAKING SYSTEM CIRCUIT BREAKER(S) DATA UPDATED
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