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ABN-31 x DISPLAY UNIT FAILURE 00012044.0002001 16 AUG 10
Criteria: P6578, SA
Applicable to: , , , , , , , , , , , ,
, , , , , , , , , , , , , ,
, , , , , , , , , , , , , ,
, , , , , , , , , , , , , ,
, , , , , , , , , , , , , ,
, , MSN,,,
Impacted DU: NONE
Reason for issue:
This Temporary Documentary Unit (TDU) is created to provide operators with TDU
example for R0).
It does not provide operational information.
(1) Evolution code
(2) Temporary information
2/2
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
PRELIMINARY PAGES
LIST OF EFFECTIVE TEMPORARY
DOCUMENTARY UNITS 30 AUG 10
Intentionally left blank
A318/A319/A320/A321 FLEET
1/2
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
PRELIMINARY PAGES
LIST OF EFFECTIVE OPERATIONS
ENGINEERING BULLETIN 30 AUG 10
A318/A319/A320/A321 FLEET
M(1) Identification T(2) E(3) Rev. Date Title
OEB1 issue 1 R 09 MAR 10 Erroneous Radio Altimeter (RA) Height Indication -
Approval
Criteria: SA
Applicable to: ALL
(1) Evolution code
(2) Ecam Importance Type
(3) Documentary Unit Impacted by Ecam
2/2
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
PRELIMINARY PAGES
LIST OF EFFECTIVE OPERATIONS
ENGINEERING BULLETIN 30 AUG 10
Intentionally left blank
A318/A319/A320/A321 FLEET
1/2
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
PRELIMINARY PAGES
AIRCRAFT ALLOCATION TABLE 30 AUG 10
A318/A319/A320/A321 FLEET
This table gives, for each delivered aircraft, the cross reference between:
- The Manufacturing Serial Number (MSN).
- The Fleet Serial Number (FSN) of the aircraft as known by AIRBUS S.A.S.
- The registration number of the aircraft as known by AIRBUS S.A.S.
- The aircraft model.
M(1) MSN FSN Registration Number Model
3307 321-213
(1) Evolution code
2/2
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
PRELIMINARY PAGES
AIRCRAFT ALLOCATION TABLE 30 AUG 10
Intentionally left blank
A318/A319/A320/A321 FLEET
1/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
PRELIMINARY PAGES
LIST OF MODIFICATIONS 30 AUG 10
A318/A319/A320/A321 FLEET
M(1) MODIFICATION Linked SB Incorp. Date Title
P2590 30 AUG 10 NAVIGATION - INSTALL A BENDIX TCAS II COLLISION
AVOIDANCE SYSTEM
, POST SB
K0066 30 AUG 10 AIR CONDITIONING - CARGO COMPARTMENT
VENTILATION
- INSTALL VENTILATION SYSTEM IN FWD CARGO
COMPARTMENT
, POST SB
P7175 30 AUG 10 ELECTRICAL POWER - GENERAL - INSTALL A
COMMERCIAL
SHEDDING PUSH-BUTTON SWITCH IN COCKPIT
, POST SB
P3511 30 AUG 10 AUTO FLIGHT - FAC - INSTALL TWO FACS P/N BAM 0509
, POST SB
P5451 30 AUG 10 ELECTRICAL POWER - GENERAL - AC-DC MAIN
DISTRIBUTION - INSTALL AC-DC SHEDDABLE BUSBARS
, POST SB
P4502 30 AUG 10 INFORMATION SYSTEM - AIR TRAFFIC AND
INFORMATION
SYSTEM (ATIMS) - INSTALL ATSU COMPUTER FOR ACARS
, POST SB
J0071 30 AUG 10 WINGS-WING TIP FENCES-INTRODUCE WING TIPS
INCLUDING FENCES-
, POST SB
P8303 30 AUG 10 NAVIGATION - DDRMI - REMOVE DDRMI VOR/ADF/DME
INDICATORS
, POST SB
P4885 34-1189 30 30 AUG 10 NAVIGATION - GPWS - ACTIVATE ENHANCED
FUNCTIONS
OF THE EGPWS
, POST SB
P5638 34-1261 12 30 AUG 10 NAVIGATION-STANDBY DATA : ALTITUDE
AND HEADING
- INSTALL INTEGRATED STANDBY INSTRUMENT SYSTEM
(ISIS)
, POST SB
K0064 30 AUG 10 LIGHTS - EXTERIOR LIGHTS - INSTALL SYNCHRONIZED
STROBE LIGHTS
, POST SB
P5669 34-1177 17 30 AUG 10 NAVIGATION - TCAS - INSTALL ALLIED
SIGNAL TCAS
COMPUTER P/N 066-50000-2220 (WITH CHANGE 7.0)
, POST SB
P3686 30 AUG 10 AUTO FLIGHT-FAC-INTRODUCE FAC P/N BAM 510
, POST SB
K6345 30 AUG 10 GENERAL - DESIGN WEIGHTS - INCREASE A321-200
DESIGN
WEIGHTS TO 77.8 T MLW AND 73.8 T MZFW (WEIGHT
VARIANT 002)
, POST SB
K2113 30 AUG 10 FUSELAGE - REAR FUSELAGE SECTION 16A - DEFINE
A321
BASIC STRUCTURE
, POST SB
P4801 30 AUG 10 ELECTRICAL POWER-GENERAL-DEFINE NEW
ELECTRICAL
GENERATION CONCEPT FOR SINGLE AISLE A/C
, POST SB
P8483 30 AUG 10 AUTO FLIGHT - FMGC - INSTALL A NEW FMS2 THALES
SMITH S3 STANDARD ON CFM A/C
, POST SB
P2316 30 AUG 10 AUTO FLIGHT - ACTIVATE WINDSHEAR FUNCTION
, POST SB
P4539 30 AUG 10 AUTOFLIGHT-FLIGHT CONTROL UNIT- (FCU)
INTRODUCE
SEXTANT MODULAR FCU
, POST SB
P6703 30 AUG 10 AUTO-FLIGHT-FLIGHT AUGMENTATION
COMPUTER-INTRODUCE FAC SOFTWARE STANDARD P/N
B397BAM0515
, POST SB
P7519 30 AUG 10 AUTOFLIGHT-FMGC-INSTALL FMGC CFM C13042AA01
(EQUIPPED WITH FMS2) HONEYWELL
　
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