N814FD

Part: HINGE — CORRODED (RT AILERON) · airframe 46,931 hrs · 19,329 cycles

RT AILERON NR 4 HINGE BEARING BORE HAS PITTING CORROSION WITH EXFOLIATION REMOVED CORROSION FROM BORE FOUND TO OUT OF LIMITS. REPAIRED BEARING BORE PER FED EX EA 6-5750-12450 RAS/BAE/1009828/2009.

Part: HINGE — CORRODED (RT AILERON) · airframe 46,931 hrs · 19,329 cycles

RT AILERON NR 1 HINGE BEARING BORE HAS PITTING CORROSION REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED BEARING BORE PER FED EX EA 6-5750-12450 AND RAS/BAE 1009828/2009.

Part: SKIN — DENTED (CARGO DOOR) · airframe 46,931 hrs · 19,329 cycles

BULK CARGO DOOR EXTERNAL SKIN HAS 7 DENTS ON LOWER FWD CORNER DEEPEST DENT .025 MAPPED AND EVALUATED DENTS,2 DENTS FOUND TO BE OUT OF LIMITS. REPAIRED 2 DENTS IAW SRM 52-30-00. APPLIED DENT DOTS IAW GMM 6-3-101 REF WRI NUMBER 52302308 FOR DAMAGE TRACKING.

Part: SMOKE DETECTOR — FAILED (E&E BAY) · airframe 46,060 hrs · 18,772 cycles

MIN EQUIPMENT BAY SMOKE INDICATION CAME ON INTERMITTENTLY, THEN STAYED ON CONSTANT. RAN ECAM ITEMS AND CHECKLIST (QRH). NO VISIBLE INDICATIONS OF SMOKE. PROBLEM CLEARED ITSELF AFTER ABOUT 2 MINS. REMOVED AND REPLACED MIN EQPT BAY SMOKE DET (12WA) PER M/M 26-15-12-4. OPS CHECK GOOD. ALSO, CLEANED UP EXCESSIVE WATER UNDER ACCESS PANEL 134AR AND SURROUNDING AREA BY DET 12WA.

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,098 hrs · 18,188 cycles

CORROSION FINDINGS ON CENTER WING BOX LOWER PANEL LT AT C47 IN SEVERAL HOLES (NR 1- NR 21). REPAIR PERFORMED BY BLEND OUT AND REAM UP HOLES IAW EA 6-5710-103305 AND RAS 046071/006/2006 ISSUE "A".

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,097 hrs · 18,187 cycles

HEAVY CORROSION ON THE TOP CAP BEAM AT C24 LT. TOP CAP BEAM REPAIR PERFORMED IAW SRM 53-10-15 / FIG 207 AND SRM 51-72-10.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 45,098 hrs · 18,188 cycles

CORROSION FINDINGS ON BOTTOM SKIN PANEL NR 1 AND NR 2, RIB 17-19 AND RIB 21-24. REPAIR PERFORMED BY BLEND OUT CORROSION IAW EA 6-5720-103322 AND RAS/BAE/1003249/2006 ISSUE "A".

Part: FRAME — CRACKED (ZONE 100) · airframe 45,098 hrs · 18,188 cycles

FOUND CRACK IN FRAME SEGMENT C74, P'26 RT. REPAIR PERFORMED BY REPLACEMENT OF AFFECTED FRAME SEGMENT IAW SRM 51-72-10.

Part: STRINGER — TOOL DAMAGE (ZONE 100) · airframe 45,097 hrs · 18,187 cycles

MISDRILLED HOLE IN STRINGER P54 AT C59. STRINGER REPAIR PERFORMED IAW SRM 53-10-14/FIG 201.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 45,098 hrs · 18,188 cycles

CORROSION FINDINGS ON BOTTOM SKIN PANEL NR 1 AND NR 2, RT WING, RIB 17-27. REPAIR PERFORMED BY BLEND OUT AND OVERSIZING FASTENER HOLE RIB 28A-29 IAW EA 6-5720-103284 AND RAS/BAE/1003245/2006 ISSUE "A".

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 45,097 hrs · 18,187 cycles

AN OLD REPAIR DOUBLER BETWEEN C76-C77, P22-P23 LT WAS NOT CONFORM TO THE INDICATED REFERENCE: SRM 53-10-12/FIG 202. DOUBLER REPAIR HAS BEEN RENEWED IAW SRM 53-10-12/FIG 225, APPROVED BY EA 6-5318-101262.

Part: SKIN — CRACKED (RT WING) · airframe 45,098 hrs · 18,188 cycles

CRACK FINDING ON PYLON REINFORCEMENT PLATE, RIB 8-9, RT WING (HOLE 1, CRACK LENGTH 14MM; HOLE 4 CRACK LENGTH 20MM). REPAIR PERFORMED BY REAM UP HOLES IAW EA 6-5720-101271 AND RAS/BAE/1003147/2006 ISSUE "A".

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,097 hrs · 18,187 cycles

FOUND CORROSION ON FITTING C59A, P44-46 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 45,098 hrs · 18,188 cycles

CORROSION ON PYLON REINFORCING PLATE ON THE LT WING, UNDERNEATH THE SPIGOT FITTING. REPAIR PERFORMED BY BLEND OUT THE CORROSION IAW EA 6-5720-103303 AND RAS/BAE/1002985/2006 ISSUE "A".

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,098 hrs · 18,188 cycles

CRACK FINDINGS DURING ACCOMPLISHMENT OF EO 6-5310-7-5020, SB A310-53-2124, RHS, C43 RT HOLE H2 CRACK LENGTH 7MM; C45 HOLE H22 CRACK LENGTH 7MM; C46 HOLE H25 CRACK LENGTH 8MM; C46 HOLE 27 CRACK LENGTH 6MM REPAIR PERFORMED BY FRAME FOOT REPLACEMENT ON C43, C46 BY OVERSIZING HOLE 22, C45 AND BUSHING INSTALLATION IN DOUBLER AND FRAME ON C46, HOLE H25 AND H27 IAW EA 6-5315-103304 AND RAS 045755/022/2006 ISSUE "A".

Part: SKIN — MISALIGNED (LT WING) · airframe 45,098 hrs · 18,188 cycles

AT LT WING REAR SPAR, FOUR MISDRILLED HOLES WHILE INSTALLING REINFORCING PLATE R573-49237-202, -203 IAW SB A310-57-2081. REPAIR PERFORMED BY OVERSIZING THE HOLES IAW EA 6-5710-103264 AND RAS/BAE/1003170/2006 ISSUE "A".

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 45,097 hrs · 18,187 cycles

CORROSION AROUND THE INBOARD (RIB 13-14) AND OUTBOARD (RIB 27-28) OVERWING REFUELING PORTS OF THE LT AND RT WINGS. REPAIR PERFORMED BY LOCALIZED BLENDING AND SOME SUIT LOCALLY MANUFACTURED PACKERS IAW EA 6-5720-103301 AND RAS/BAE/1002880/2006 ISSUE "A".

Part: SKIN — TOOL DAMAGE (ZONE 600) · airframe 45,098 hrs · 18,188 cycles

RT WING REAR SPAR, MISDRILLED HOLE ON BOTTOM SKIN DURING EMBODIMENT OF SB 57-2081. REPAIR WAS PERFORMED BY OVERSIZING THE HOLE IAW EA 6-5710-103285 AND RAS/BAE/1003241/2006 ISSUE "A".

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,097 hrs · 18,187 cycles

CORROSION ON TOP CAP BEAM UPPER FLANGE LT AT C38 AND C38.1. REPAIR PERFORMED IAW 53-10-15/FIG 207 AND SRM 51-72-10.

Part: PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 45,097 hrs · 18,187 cycles

CORROSION ON LT BOTTOM WING PANEL NR 2, RIB 28/30. REPAIR PERFORMED BY BLEND OUT IAW 6-5720-101273 AND RAS/BAE/1002867/2006 ISSUE "A".

Part: FAILSAFE — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,097 hrs · 18,187 cycles

CORROSION ON RT FWD PAX DOOR FAIL/SAFE RING UPPER HALF. REPAIR PERFORMED BY REWORK AND OVERSIZING IAW EA 6-5312-101257 AND RAS 044737/013/2006 ISSUE "A".

Part: PANEL — CRACKED (ZONE 400) · airframe 45,097 hrs · 18,187 cycles

CRACKS ON PYLON NR 2 LATERAL PANEL AT RIB 8 RT. REPAIR WAS PERFORMED IAW SRM 54-51-31/FIG 201, APPROVED BY EA 6-5450-101300.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,096 hrs · 18,186 cycles

TWO PREVIOUS REPAIRS FOUND AT STRINGER P56 LT/RT, C76-C77 WITH NEW CORROSION ON P56 LT/RT. REPAIR PERFORMED BY CORROSION REMOVAL AND L-ANGLE INSTALLATION IAW EA 6-5318-101239 AND RAS/DAHAM/4020755/2006 ISSUE "A".

Part: ATTACH BRACKET — CORRODED (ZONE 500) · corrosion level 2 · airframe 45,096 hrs · 18,186 cycles

CORROSION FOUND IN THE ATTACHMENT HOLES OF LT WING NR 3 FLAP JACK MOUNTING STRUCTURE. REPAIR PERFORMED BY OVERSIZING THE HOLES AND BUSH INSTALLATION IAW EA 6-5751-103263 AND RAS/BAE/1003177/2006 ISSUE "A".

Part: PANEL — CORRODED (ZONE 400) · corrosion level 2 · airframe 45,097 hrs · 18,187 cycles

CORROSION ON PYLON NR 2 INBOARD SIDE PANEL, RIB 10-18. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5451-101322 AND RAS 045345/010/2006 ISSUE "A".

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,097 hrs · 18,187 cycles

CORROSION ON CORNER FITTING AT C33, P44 LT/RT (P/N A537-73644-202, -203) REPAIR PERFORMED BY REPLACEMENT IAW SRM 51-72-10.

Part: STIFFENER — CORRODED (ZONE 600) · corrosion level 2 · airframe 45,096 hrs · 18,186 cycles

CORROSION ON RT WING HINGE ARM FITTING AND TOP SKIN PANEL. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5722-103262 AND RAS/BAE/1003079/2006 ISSUE "A" (ALTERNATE MATERIAL DAN 26H30 IN PLACE OF 7150-T651 FOR STIFFENER A572-42583-203) AND RAS/BAE/1003026/2006 ISSUE "A" (CORROSION BLEND OUT).

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,097 hrs · 18,187 cycles

FOUND CORROSION ON STRINGER P56, C69-C71. STRINGER REPAIR PERFORMED IAW SRM 53-10-14/FIG 201 AND CLIP (P/N A539-73791-224-91) REPLACEMENT ON C70 IAW SRM 51-72-10.

Part: SKIN — DELAMINATED (ZONE 600) · airframe 45,096 hrs · 18,186 cycles

SEVERAL DENTS WITH DELAMINATION ON RT INBOARD FLAP BOTTOM SKIN, T/E. REPAIR WAS PERFORMED IAW SRM 57-53-12/FIG 208, APPROVED BY EA 6-5752-101287 AND RAS/DABRE/7006662/2006 ISSUE "A".

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,097 hrs · 18,187 cycles

CORROSION AND MATERIAL DEVIATIONS ON OLD AFT CARGO DOOR SILL BEAM REPAIR, C59-C60 RT. REPAIR PERFORMED BY CUT OUT AND REPLACING PARTS IAW SRM 53-17-18/FIG 202 AND RAS/DAHAM/4015666/2002 ISSUE "A".

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,097 hrs · 18,187 cycles

CORROSION ON KEEL BEAM BOX AND MLG DOOR ATTACHMENT BRACKETS LT/RT. REPAIR PERFORMED BY BLEND OUT AND SPOT FACING ON ALL AFFECTED FASTENER HOLES IAW EA 6-5315-103286 AND RAS 045294/020/2006 ISSUE "A".

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,096 hrs · 18,186 cycles

CORROSION ON STRINGER P46 RT, C59-C60, STRINGER REPAIR PERFORMED IAW EA 6-5317-101240 AND RAS/DAHAM/4020719/2006 ISSUE "B".

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 45,097 hrs · 18,187 cycles

IMPACT AND CORROSION AROUND ACCESS HOLES OF LT WING BOTTOM SKIN BETWEEN RIB 22-23, RIB 28A-29 AND RIB 29-30. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5720-101243 ISSUE "A" AND RAS/BAE/1002786/2006 ISSUE "A".

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 45,097 hrs · 18,187 cycles

CORROSION ON AN OLD REPAIR LT WING BOX FWD OF FRONT SPAR, BETWEEN RIB 28A-29. REPAIR PERFORMED BY REAM UP THE AFFECTED HOLES AND OVERSIZING IAW EA 6-5720-101242 AND RAS/BAE/1002718/2006 ISSUE "A".

Part: SKIN — DELAMINATED (ZONE 600) · airframe 45,097 hrs · 18,187 cycles

DELAMINATION ON SPOILER NR 3 LT, NR 4 RT END RIB. REPAIR PERFORMED IAW SRM 51-77-11, APPROVED BY EA 6-5772-101289 AND RAS 045027/006/2006 ISSUE "A" (NR 3 LT) AND RAS 045027/007/2006 ISSUE "A" (NR 4 RT).

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,096 hrs · 18,186 cycles

FOUND CORROSION ON TOP CAP BEAM (UPPER FLANGE) AT C33. REPAIR PERFORMED BY REPLACEMENT IAW SRM 51-72-10.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,097 hrs · 18,187 cycles

CORROSION ON STRINGER P55, C70-C71. STRINGER REPAIR PERFORMED IAW SRM 53-10-14/FIG 203.

Part: PANEL — CRACKED (ZONE 400) · airframe 45,097 hrs · 18,187 cycles

CRACK FOUND ON PYLON NR 1 LATERAL PANEL AT RIB 8 LT/RT. REPAIR WAS PERFORMED IAW SRM 54-51-31/FIG 201, APPROVED BY EA 6-5450-101299.

Part: SKIN — DELAMINATED (ZONE 500) · airframe 45,097 hrs · 18,187 cycles

TWO AREAS WITH DELAMINATION ON LT INBOARD FLAP BOTTOM SKIN T/E, RIB 3-5 AND RIB 8-9. REPAIR PERFORMED BY METAL SKINNED CORE REPAIR IAW SRM 57-53-12/FIG 207/209, APPROVED BY EA 6-5752-101288 AND RAS/DABRE/7006663/2006 ISSUE "A".

Part: SPAR — CORRODED (ZONE 400) · corrosion level 2 · airframe 45,097 hrs · 18,187 cycles

CORROSION ON UPPER SPAR OF RT PYLON AT RIB 14. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5451-101244 ISSUE "A" AND RAS 044734/013/2006 ISSUE "A".

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,096 hrs · 18,186 cycles

CORROSION FOUND IN ZONE 150 AFT CARGO COMPARTMENT, C54-C62, P46-P53 LT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 / FIG 201 ON THE RELATED STRINGER; CONNECTING SECTIONS, C54.1-C55/58, P44-P51 REPLACED IAW SRM 51-72-10 AND SEVERAL CLIPS REPLACED IAW SRM 51-72-10.

Part: FAILSAFE — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,097 hrs · 18,187 cycles

CORROSION ON LT FWD PAX DOOR FAIL/SAFE RING UPPER HALF. REPAIR PERFORMED BY REWORK AND OVERSIZING IAW EA 6-5312-101257 AND RAS 044737/013/2006 ISSUE "A".

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,078 hrs · 18,173 cycles

DEVIATIONS AND CORROSION ON THE TOP SKIN PANEL OF THE CENTER WING BOX, LT/RT, FROM C42 TO C47. REPAIRS PERFORMED IAW SRM 57-10-12 FIG 101 SH 3 AND SRM 51-40-21, COVERED BY EA 6-5710-99220 AND RAS 044669/016/2006 ISSUE "A".

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 45,078 hrs · 18,173 cycles

FOUND CORROSION ON LT WING BOTTOM SKIN PANEL 2 IN THE AREA OF RIB 1-4 AROUND SEVERAL FASTENERS. REPAIR PERFORMED BY BLEND OUT CORROSION IAW EA 6-5720-101272 AND SRM 57-00-00 4.C.3(B), APPROVED BY RAS/BAE/1002868/2006 ISSUE "A".

Part: BULKHEAD — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,080 hrs · 18,174 cycles

FOUND CORROSION AT FRAME 39 BULKHEAD LOWER T-PROFILE AND ON PARTS OF BULKHEAD PANEL IN AREA OF THE T-PROFILE. REPAIRS OF ALL AFFECTED AREAS MENTIONED AND PERFORMED IAW EA 6-5314-99221AND RAS 014851/020/2001 ISSUE "A".

Part: FRAME — CHAFED (ZONE 100) · airframe 45,078 hrs · 18,173 cycles

FOUND CRACKED FRAME-SEGMENT AT C74, P26 LT. REPLACEMENT OF THE AFFECTED FRAME-SEGMENT.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,078 hrs · 18,173 cycles

HEAVY CORROSION ON Y-Z LATCH SUPPORT AT C25A RT. REPAIR PERFORMED IAW SRM 53-13-13/FIG 203 (PN: R537-00089-200-EF).

Part: SKIN — CRACKED (ZONE 600) · corrosion level 2 · airframe 45,078 hrs · 18,173 cycles

CORROSION ON RT WING BOTTOM SKIN IN AREA OF RIB 4-5 AROUND SEVERAL FASTENERS. CRACKS WERE FOUND IN TWO HOLES. REPAIR PERFORMED BY REMOVING CORROSION AND REMOVING CRACKS AT HOLE NR 666 AND NR 1466 BY OVERSIZING IAW EA 6-5720-101321 AND RAS/BAE/1002865/2006 ISSUE "A".

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,078 hrs · 18,173 cycles

HEAVY CORROSION ON TOP CAP BEAM, C38.2 IN FWD CARGO COMPARTMENT. REPLACEMENT OF TOP CAP BEAM (A537-73651-212-00) IAW 51-72-10.

Part: SKIN — DAMAGED (ZONE 500) · airframe 45,033 hrs · 18,150 cycles

ELONGATED HYDRAULIC FITTING HOLES IN THE LOWER SKIN PANELS OF LT WING. REPAIR PERFORMED BY OVERSIZING AND BUSHING HOLES IAW EA 6-5720-99228, APPROVED BY RAS/BAE/1002610/2006 ISSUE "A".

Part: ATTACH FITTING — CRACKED (ZONE 200) · airframe 45,033 hrs · 18,150 cycles

CRACK ON CROSSBEAM ATTACHMENT FITTING AT FRAME 12A THROUGH 13 LT. REPAIR PERFORMED PERFORMED BY REPLACING NEW PART IAW SB A310-53-2116 AND SOG-W8-53-00-02, REFER TO DRW A53613845.

Part: DOUBLER — CORRODED (TAIL CONE) · corrosion level 2 · airframe 45,033 hrs · 18,150 cycles

SEVERAL AREAS OF CORROSION ON C95, ON INTERNAL DOUBLER BETWEEN C94-C95, P14-P16 LT AND ON EXTERNAL SKIN BETWEEN C95-C96, P15 LT ON FUSELAGE TAIL CONE, LISTED IN DR 0534-01-16-0200. REPAIR PERFORMED BY BLEND OUT, REPLACEMENT, CUT OUT WITH EXTERNAL AND INTERNAL DOUBLERS IAW EA 6-5319-99217, APPROVED BY RAS/DAHAM/4020768/2006 ISSUE "A", RAS/DAHAM/4020762/2006 ISSUE "A" AND RAS/DAHAM/4020742/2006 ISSUE "A".

Part: SKIN PANEL — CRACKED (ZONE 300) · airframe 45,033 hrs · 18,150 cycles

THE UPPER SKIN PANEL BETWEEN C103/104 IN AREA OF 317AL CUTOUT WAS CRACKED. REPAIR REMOVED BY REPLACED STRUCTURE.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 45,033 hrs · 18,150 cycles

CORROSION ON LOWER SKIN PANEL NR 2 AND REINFORCING STRUCTURE OF THE LT WING INBOARD RIB 1-3. REPAIRED BY BLENDING OUT AND TRIMMING OUT EXFOLIATION CORROSION IAW EA 6-5720-99216, APPROVED BY RAS/BAE/1002613/2006 ISSUE "A".

Part: LONGERON — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,033 hrs · 18,150 cycles

CORROSION ON LONGERON AT FLOOR STRUCTURE SEC 12 (Y-1959) BETWEEN C17/19 WAS OUT OF LIMIT. REPAIR PERFORMED IAW SRM 53-12-12/FIG 207.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 45,036 hrs · 18,151 cycles

FOUND CORROSION ON RT WING TOP SKIN IN AREA OF RIB 4/5 NEAR PICK UP FITTING. CORROSION REMOVED BY BLEND OUT AND INSTALLATION OF PACKING WASHERS FOR FLAT SEATING OF LOCALIZED SPOTFACING OF OVERWING BRACKET HOLES IAW EA 6-5720-99218, APPROVED BY RAS/BAE/1002737/2006 ISSUE "A".

Part: BEAM — DAMAGED (ZONE 100) · airframe 45,036 hrs · 18,151 cycles

DURING SB: A310-53-2095, FOUND ENLARGED HOLES ON AFT CARGO DOOR ACTUATOR BEAM BETWEEN C61-C62. REPLACEMENT OF EXISTING BEAM (A537-81256-002) BY NEW ONE IAW SRM 51-72-10.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 45,033 hrs · 18,150 cycles

CORROSION ON LOWER SKIN PANEL NR 2 AND REINFORCING STRUCTURE OF THE RT WING INBOARD RIBS 1-3. REPAIRED BY BLENDING OUT AND TRIMMING OUT EXFOLIATION CORROSION IAW EA 6-5720-99216, APPROVED BY RAS/BAE/1002613/2006 ISSUE "A".

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 45,028 hrs · 18,147 cycles

OLD REPAIRS WITH NO RECORDS AND NO SRM REFERENCE ON FLOOR STRUCTURE. Z-PROFILE REPAIR BETWEEN C11/12A (Y450/730) AND A FURTHER Z-PROFILE REPAIR BETWEEN C11/12A (1020/1200). REPAIR VERIFICATION, PERFORMED IAW RAS 045088/009/2006 ISSUE "A" AND EA 6-5312-101258.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,028 hrs · 18,147 cycles

OLD REPAIR BY A DOUBLER AND ANGLE DOUBLERS, INSTALLED ON FWD NLG WHEEL WELL, INSIDE E/E COMPARTMENT RT. REPAIR VERIFICATION, PERFORMED IAW RAS/AS/332/96 AND SIA-EN NO 10EN-53-6591. EA FOR TRACKING: 6-5312-101298.

Part: SPLICE — DENTED (FUSELAGE) · airframe 45,028 hrs · 18,147 cycles

FOUND OLD REPAIR OF AN EXTERNAL DOUBLER BETWEEN C91/92, ABOVE SKIN LAP BETWEEN P35 AND P41 LT. REPAIR VERIFICATION, PERFORMED IAW SIA-NRC: RAS/DAHAM/1020/99 ISSUE "A", EA FOR TRACKING: 6-5319-101259.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 45,031 hrs · 18,149 cycles

FOUND EXTENSIVE CORROSION ON RT WING BOTTOM FRONT SPAR OVERHANGS. LOOK FOR AFFECTED AREAS IN EA 6-5720-99230. REPAIR PERFORMED BY BLEND AND/OR CUT OUT AND INSTALLING REPAIR PLATES ALL IAW EA 6-5720-99230, APPROVED BY RAS/BAE/1002584/2006 ISSUE "A".

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 45,031 hrs · 18,149 cycles

EXTENSIVE CORROSION ON THE LT WING BOTTOM SKIN FRONT SPAR OVERHANGS. LOOK FOR AFFECTED AREAS IN MENTIONED EA. REPAIR PERFORMED BY BLEND OUT AND/OR CUT OUT AND INSTALLING REPAIR PLATES ALL IAW EA 6-5720-99230, APPROVED BY RAS/BAE/1002584/2006 ISSUE "A".

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 45,030 hrs · 18,148 cycles

FOUND CORROSION ON TOP SKIN RT WING. AFFECTED AREAS MENTIONED IN EA 6-5720-99229. REPAIR PERFORMED BY BLEND OUT AND OVERSIZING IAW EA 6-5720-99229 AND RAS/BAE/1002732/2006.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 45,028 hrs · 18,147 cycles

OLD REPAIRS ON FLOOR STRUCTURE, REPAIR ANGLES ON SEVERAL STRINGERS. SPECIAL PROFILE BETWEEN C11/12, BETWEEN C/L (Y232), SPLICE REPAIR BETWEEN C14/15 (Y-953) AND SPLICE REPAIR BETWEEN C14/15 (Y-1959). REPAIR VERIFICATION, PERFORMED IAW SRM 53-12-15/FIG 207.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,028 hrs · 18,147 cycles

CORROSION BLEND OUT REPAIR CAUSES OUT OF LIMIT PER SRM 53-10-00 ON STRINGERS P52 LT, BETWEEN C54.1- C55/58; P45 LT, BETWEEN C54.1-54.2 AND P52 RT BETWEEN C61/62-C62/63. STRINGER REPAIR PERFORMED BY SRM 53-10-14 AND MILL TO STRINGER IAW SRM 53-10-14 "B-B".

Part: FITTING — DAMAGED (RT WING) · airframe 45,031 hrs · 18,149 cycles

ELONGATED HYDRAULIC FITTING HOLES IN THE LOWER SKIN PANELS OF RT WING. REPAIR BY OVERSIZING AND BUSHING HOLES AS PER R572-49184 ISSUE "C" IAW EA 6-5720-99228, APPROVED BY RAS/BAE/1002610/2006.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 45,031 hrs · 18,149 cycles

EXTENSIVE CORROSION ON LT WING TOP SKIN. AFFECTED AREAS SHOWN ON PAGES 4 THROUGH 6 IN MENTIONED EA. REPAIR PERFORMED BY BLEND OUT AND OVERSIZING IAW EA 6-5720-101319, APPROVED BY RAS/BAE/1003173/2006 ISSUE "A".

Part: RIB — DAMAGED (TE FLAP) · airframe 45,031 hrs · 18,149 cycles

OLD REPAIR AT RIB 21 INNER FLAP LT. REPLACEMENT OF END RIB 21 IAW SB A310-57-2055, APPROVED BY EA 6-5752-103333.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 45,028 hrs · 18,147 cycles

OLD REPAIR, AN EXTERNAL DOUBLER INSTALLED NEAR APU DOOR BETWEEN C92/93 AND BETWEEN P18/19 RT. THIS DOUBLER IS NOT CONFORM TO SRM 53-19-12 FIG 202. REPAIR PERFORMED BY INSTALLATION OF A NEW REPAIR DOUBLER IAW SRM 53-19-12/FIG 201.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,028 hrs · 18,147 cycles

FOUND CORROSION BLEND OUT ON C80/82, P5 LT AND C87, P6 RT. THESE TWO SPOTS WERE OUT OF SRM LIMITS. REPAIR PERFORMED IAW EA 6-5319-101245 AND IS APPROVED BY RAS/DAHAM/4020774/2006 ISSUE "A".

Part: SKIN — CORRODED (ZONE 800) · airframe 45,025 hrs · 18,146 cycles

FOUND CORROSION ON RT FWD PASSENGER DOOR ARM ASSEMBLY. REPAIR PERFORMED BY BLEND OUT WITH DOUBLER INSTALLATION AND REPLACEMENT OF CORRODED PARTS IAW EA 6-5211-101326 AND IS APPROVED BY RAS 045586/005/2006.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,025 hrs · 18,146 cycles

CORROSION AT INNER DOUBLER A537-78731-206 OF GROUND SERVICE CONDITIONED AIR CONNECTION BETWEEN C37-38.1 LT IS OUT OF LIMIT IAW SRM 53-10-00. REPAIR PERFORMED IAW EA 6-5314-101290 AND RAS/DATLS/0003182/2006 ISSUE "A".

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 45,025 hrs · 18,146 cycles

OLD EXTERNAL REPAIR DOUBLER REPAIR BETWEEN C33/34, P54 LT AND P54 RT THAT INTERFERES WITH P TO F. INSTALLATION DRW R537B1610. DISCREPANCY PERFORMED BY INSTALLING REDESIGNED REPAIR DOUBLER IAW EA 6-5314-101241 AND IS APPROVED BY RAS/DABRE/7006565/2006 ISSUE "A".

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 45,025 hrs · 18,146 cycles

OLD REPAIR, EXTERNAL DOUBLER BETWEEN C66/67, P33/34 RT AND NOT CONFORM TO REPAIR REF: SRM53-10-12/FIG 203 REPAIR PERFORMED BY INSTALLING NEW DOUBLER IAW EA 6-5317-101260 AND SRM 53-10-12/FIG 225.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 45,025 hrs · 18,146 cycles

OLD REPAIR, EXTERNAL DOUBLER BETWEEN C66/67, P33/34 RT AND NOT CONFORM TO REPAIR REF: SRM53-10-12/FIG 203. REPAIR PERFORMED BY INSTALLING NEW DOUBLER IAW EA 6-5317-101260 AND SRM 53-10-12/FIG 225.

Part: FRAME — DENTED (ZONE 100) · airframe 45,025 hrs · 18,146 cycles

DENT (RIVETING MARK) AT C23, P41 LT. REPAIR PERFORMED BY INSTALLING FLUSH DOUBLER AND SPLICED STRINGER IAW EA 6-5313-101261, SRM 53-10-12/FIG 27 AND SRM 53-10-14/FIG 201.