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- Airbus
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- Service Bulletin
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- A300-54-0081
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CUSTOMER SERVICES DIRECTORATE AIRBUS INDUSTRIE • A300
TECHNICAL PUBLICATIONS 1 Rond Point Maurice BELLONTE 31707 BLAGNAC CEDEX FRANCE Tel: (33) 61-93-33-33 Telex : AIRBUS 530526 F
SERVICE BULLETIN CHANGE NOTICE S.B. No. A300-54-0081 REV_ DATED : May 05/95 Mod. No. 10431S20462 TITLE : NACELLES/PYLONS - PANELS IN THE UPPER CORNER AT RIB 8 - ADD A DOUBLER.
MODEL: ALL models Listed on S.B.
DESCRIPTION :
This notice is issued to inform the affected operators that subject Service Bulletin is changed as stated below.
SERVICE BULLETIN Page 8 - Para. 2.B. (3), Page 11-12 : Figure 1 and Page 13 - Para. 3.A. LIST OF COMPONENTS Should read : Item 6 : ASNA2314-4-13 Item 7 : ASNA2314-6-16 Item 9 : NAS1154-13 Instead of : Item 6 : ASNA2314-4-14 Item 7 : ASNA2314-6-18 Item 9 : NAS1154-14 This change will be incorporated in the next Revision of this Service Bulletin; however no revision is planned at the present time.
FILING INSTRUCTIONS Put this Change Notice in front of the Service Bulletin.
SERVICE BULLETIN No. : A300-54-0081 5 DATE : May 23/95 CHANGE NOTICE No. : O.A.
Printed in France
AIRBUS INDUSTRIE $ A300
PRODUCT SUPPORT DIRECTORATE 1 Rond Point Maurice BELLONTE 31707 BLAGNAC CEDEX FRANCE SERVICE BULLETIN SUMMARY Tel: (33) 61-93-33-33 Telex : AIRBU 530526 F This summary is for information only and is not approved for modification of the aircraft.
MODIFICATION No. 10431S20462 ATA SYSTEM : 54 TITLE : NACELLES/PYLONS - PANELS IN THE UPPER CORNER AT RIB 8 - ADD A DOUBLER.
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES On A/C fitted with GE pylon, cracks have been reported on pylon side panels (upper section) at Rib 8. The crack is starting from the top edge of the panel and running down to the fastener hole and in some cases is going beyond the hole.
For aircraft equipped with common GE and PW pylons, this Service Bulletin recommends the installation of an outer doubler on the undamaged structure of pylon side panels B (upper section) at Rib 8.
After accomplishment of this Service Bulletin, do an inspection program as per Service Bulletin No. A300-54-0075. STA726/RIB8
EFFECTIVITY DOUBLER This Service Bulletin is applicable to FWD the following operators :
AFR, AIC, AUS, AZA, CAL, COA, EAL,
FIN, GIA, IAC, IBE, IRA, JAS, KAL,
LGL, MSR, OAL, PAA, PAL, PIA, RKA, SAA, SAS, TAR, THA, VSP.
SERVICE BULLETIN/MODIFICATION TO BE
ACCOMPLISHED PREVIOUSLY OR
SIMULTANEOUSLY None.
5 DATE : Aug 11/93 SERVICE BULLETIN No. : A300-54-0081 REVISION No. : PAGE : 1 of 3 Printed in France
$ A300
SERVICE BULLETIN SUMMARY
REFERENCES/ REPERCUSSIONS TFU 54-51-31-001 LIFE LIMIT None OEB None LINE MAINTENANCE AFFECTED AOT None NO SIL None OTHERS None
NATURE OF THE MODIFICATION
AIRCRAFT YES
EQUIPMENT NO
HARD NO
SOFT NO
OBRM NO
COMPLIANCE Recommended.
MANPOWER (Per A/C) Manhours 48.0 Elapsed Time (Hours) 24.0 SERVICE BULLETIN No. : A300-54-0081 PAGE : 2 Printed in trance
$ A300
SERVICE BULLETIN SUMMARY Equipment Data None.
APPENDICES None - DATE : Aug 11/93 SERVICE BULLETIN No. : A300-54-0081 REVISION No. : PAGE : 3 Printed in france
AIRBUS INDUSTRIE $ A300
PRODUCT SUPPORT DIRECTORATE 1 Rond Point Maurice BELLONTE 31707 BLAGNAC CEDEX FRANCE SERVICE BULLETIN Tel: (33) 61-93-33-33 Telex : AIRBU 530526 F MODIFICATION No. 10431S20462 ATA SYSTEM : 54 TITLE : NACELLES/PYLONS - PANELS IN THE UPPER CORNER AT RIB 8 - ADD A DOUBLER.
1. PLANNING INFORMATION A. EFFECTIVITY
(1) Aircraft models : B2-203, B2K-3C, B4-2C, B4-103, B4-120, B4-203, B4-220, C4-203, F4-203.
(2) Aircraft Customer and MSN Kit No. Qty Fleet No. 540081 of Kits AFRO62,064 175,183 A01 04 AIC101-103 177,180,190 A01 06 AUS004,005 196,218 A01 04 AZA158 173 A01 02 CAL001-006 193,197,221,232,179,171 A01 12 COA970-972 250,262,289 A01 06 EAL223-225 154,155,158 A01 06 EAL226-231 161,204,207,211,216,220 A01 12 EAL232-235 259,261,271,274 A01 08 FIN001,002 299,302 A01 04 GIA001-006 159,164,165, 166,167,168 A01 12 GIA007-009 213,214,215 A01 06 IAC051,052 181,182 A01 04 IBE251-256 130,133,135,136,156,170 A01 12 IRA003 185 A01 02 DATE : Aug 11/93 SERVICE BULLETIN No. : A300-54-0081 REVISION No. : PAGE : 1 of 14 Printed in France
$ A300
SERVICE BULLETIN Customer and MSN Kit No- Qty Fleet No. 540081 of Kits IRA005,006 187,226 A01 04 JAS004-006 160,163,176 A01 06 JAS007-009 209,244,253 A01 06 JAS101,103 256,169 A01 04 JAS104,106 174,194 A01 04 JAS107,108 239,178 A01 04 KAL101,102 277,292 A01 04 LGL001 269 A01 02 MSR004,005 199,200 A01 04 MSR007,008 240,255 A01 04 OAL007,008 184,189 A01 04 PAA001-006 195,227,198,247,234,236 A01 12 PAA007-012 304,305,238,235,208,210 A01 12 PALO03 125* A01 01 PAL004,005 203,219 A01 04 PIA003 099* A01 01 PIA012 268 A01 02 RKA552,553 243,282 A01 04 SAA052,053 192,222 A01 04 SAA101 212 A01 02 SAS201,202 079,094 A01 04 SAS204 128 A01 02 TAR001 188 A01 02 THA010,012 249,265 A01 04 DATE : Aug 11/93 SERVICE BULLETIN No. : A300-54-0081 REVISION No. : PAGE : 2 Printed in France
• A300
SERVICE BULLETIN customer and MSN Kit No. Qty Fleet No. 540081 of Kits VSP001-003 202,205,225 A01 06 This modification (retrofit scheme) is applicable by Service Bulletin only on aircraft listed above fitted with common pylon.
* A/C 099, 125 : Modification of the right pylon only.
NOTE: Kit No. 540081A01 is valid for one pylon.
Modification of one aircraft requires :
2 Kits No. 540081A01.
(3) Spares None - B. REASON
(1) History On A/C fitted with GE pylon, cracks have been reported on pylon side panels (upper section) at Rib 8. The crack is starting from the top edge of the panel and running down to the fastener hole and in some cases is going beyond the hole.
(2) Objective/Action For aircraft fitted with common GE and PW pylon, this Service Bulletin recommends the installation of a doubler on left pylon 1 and right pylon 2, on pylon side panels (upper section) at Rib 8.
(3) Advantages After accomplishment of this Service Bulletin, do an inspection program as per Service Bulletin No. A300-54-0075.
(4) Accomplishment Timescale Accomplishment at the earliest opportunity where manpower and facilities are available.
DATE : Aug 11/93 SERVICE BULLETIN No. : A300-54-0081 REVISION No. : PAGE : 3 Printed in trance
G A300
SERVICE BULLETIN C. DESCRIPTION Accomplishment of this Service Bulletin consists in carrying out the following jobs on the aircraft :
On left pylon 1 and right pylon 2, on pylon side panels (upper section), at Rib 8.
(1) Gain access to the working area.
(2) Installation of the doubler on pylon side panels (upper section) at Rib 8.
(3) Close-up-
(4) Inspection program after accomplishment of this Service Bulletin as per Service Bulletin No. A300-54-0075.
D. APPROVAL This Service Bulletin relates to the change(s) referenced on page 1 which has (have) been approved under the authority of DGAC Design Organisation Approval No. C 01.
The technical information contained in this Service Bulletin has been approved under the authority of DGAC Design Organisation Approval NO. C 01.
E. MANPOWER Manhours (Per A/C) Gain access 8-0 Doubler installation 30.0 close-up 10.0 TOTAL MANHOURS 48.0 ELAPSED TIME (HOURS) 24-0 NOTE: This Service Bulletin assumes that the aircraft has been placed in a maintenance status. The manhours/elapsed time estimates do not include preparation for the modification, non-productive elapsed time, or administrative functions.
DATE : Aug 11/93 SERVICE BULLETIN No. : A300-54-0081 REVISION NO. : PAGE : 4 Printed in France
$ A300
SERVICE BULLETIN F. MATERIAL - COST AND AVAILABILITY
(1) Material Operators with aircraft listed under paragraph 1.A. (2) above should submit a purchase order quoting this Service Bulletin to :
AIRBUS INDUSTRIE
SPARES SUPPORT CENTER WEG BEIM JAEGER 150 D2000 HAMBURG 63
GERMANY
(2) Cost and availability Kit No. Cost Availability * (US Dollars) 540081A01 1,004.00 180 The sales terms (cost and availability) are estimated in relation to economic conditions at the issue date of the Service Bulletin.
* Calendar days from receipt of order G. TOOLING - PRICE AND AVAILABILITY None.
H. WEIGHT AND BALANCE MEW : + 1.7 Kg (+ 3.74 (b) Effect on balance : + 46.3 Kgm (+ 334.92 lb.ft.)
I. REFERENCES Aircraft Maintenance Manual : 06-21-54, 20-21-12, 20-31-00, 24-00-00, 24-41-00, 36-00-00, 36-11-15 Service Bulletin No. A300-54-0075 J. PUBLICATIONS AFFECTED Structural Repair Manual : 54-10-00 DATE : Aug 11/93 SERVICE BULLETIN No. : A300-54-0081 REVISION No. : PAGE : 5-6 Printed in France
$ A300
SERVICE BULLETIN
2. ACCOMPLISHMENT INSTRUCTIONS A. GENERAL
(1) Preparation
(a) De-energize the aircraft electrical circuits (Ref. AMM 24-41-00, P. Block 301) and electrically ground the aircraft (Ref. AMM 24-00-00, P. Block 301).
(b) Install access platform for access to engine pylons.
(c) Remove access doors (Ref. AMM 06-21-54) :
For L pylon GE engines : 413DL, 413EL, 413GL, 415AL, 414DR, 414ER, 416AR PW engines : 413DL, 413EL, 413GL, 415AL, 414DR, 414ER, 476AR For R pylon with GE and PW engines :
423DL, 423EL, 423GL, 425AL, 424ER, 424DR, 426AR.
(d) Remove bleed air precooler cold air inlet duct (Ref. AMM 36-11-15, P. Block 401 and AMM 36-00-00, P. Block 401).
(2) Standard procedures
(a) To clean the surface to be sealed using Mat. No. 11-003 (Ref. AMM 20-31-00).
(b) To apply sealant Mat. No. 09-013 (Ref. AMM 20-31-00).
(c) To renew the protection finish with Mat. No. 16-001, 16-018 and 16-020 (Ref. AMM 20-31-00).
(d) To torque standard fasteners (Ref. AMM 20-21-12).
DATE : Aug 11/93 SERVICE BULLETIN No. : A300-54-0081 REVISION No. : PAGE : 7 Printed in France
$ 4300
SERVICE BULLETIN B. MODIFICATION Installation of the doubler on left pylon 1 and right pylon 2, on pylon side panels (upper section), at Rib 8.
NOTE: The description is given for the left pylon. The right pylon is equivalent.
Refer to Figure 1
(1) Remove rivets and bolts in the area of the doubler to be installed.
(a) Remove :
8 + 8 rivets Item (12) (discard) 3 + 3 bolts Item (6) (discard) 3 + 3 nuts Item (10) (discard) 2 + 2 bolts Item (8) (discard) 4 + 4 bolts Item (7) (discard) 4 + 4 nuts Item (11) (discard)
(2) Offer-up and put in position on panels at Rib 8 :
1 doubler A5461255220000 Item 1 1 doubler A5461255220100 Item 2 Drill, ream, deburr and attach the doublers Item 1 and Item 2 with interfay of Mat. No. 09-013 (Ret. AMM 20-31-00) and :
3 + 3 washers A5461255420000 Item 3 3 + 3 bolts ASNA2314-4-14 Item 6 3 + 3 nuts NAS 1726-4E Item 10 2 + 2 washers A5461255520000 Item 5 2 + 2 bolts NAS1153E3 Item 8 1 + 1 bolt NAS1154-14 Item 9 1 + 1 nut NAS1726-4E Item 10 8 + 8 rivets NSA5414-36-20 Item 12 4 + 4 washers A5461255320000 Item 4 4 + 4 bolts ASNA2314-6-18 Item 7 4 + 4 nuts NAS1726-6E Item 11 C. INSPECTION PROGRAM
(1) Do the inspection program after accomplishment of this modification as per Service Bulletin No. A300-54-0075.
DATE : Aug 11/93 SERVICE BULLETIN No. : A300-54-0081 REVISION No. : PAGE : 8 Printed in France
G A300
SERVICE BULLETIN D. TESTS None.
E_ CLOSE-UP
(1) Make certain that the work areas are clean and clear of tools and miscellaneous items of equipment.
(2) Install bleed air precooler cold air inlet duct (Ref. AMM 36-11-15, P. Block 401 and AMM 36-00-00, P. Block 401).
(3) Install access doors (Ref. AMM 06-21-54) :
For L pylon GE engines : 413DL, 413EL, 413GL, 415AL, 414DR, 414ER, 416AR PW engines : 413DL, 413EL, 413GL, 415AL, 414DR, 414ER, 476AR For R pylon with GE and PW engines :
423DL, 423EL, 423GL, 425AL, 424ER, 424DR, 426AR.
(4) Remove access platforms.
(5) Disconnect the aircraft electrical ground connection (Ref. AMM 24-00-00).
F. DOCUMENTATION Write in the applicable aircraft record that you have done all the work in this Service Bulletin.
DATE : Aug 11/93 SERVICE BULLETIN No. : A300-54-0081 REVISION No. : PAGE: 9-10 Printed in France