N403FE

Part: HINGE FITTING — CRACKED (LT MLG DOOR) · airframe 37,852 hrs · 31,675 cycles

LEFT MLG UNSAFE DOOR INDICATION ON T/O. THEN UNSAFE MLG INDICATION ON APPROACH. FOUND LT MLG CENTER HINGE FITTINGS FRACTURED AT ACTUATOR ATTACHEMENT LUG, AND CROSSOVER BEAM FITTING CRACKED. REMOVED AND REPLACED LT MLG CENTER HINGE FITTINGS AND CROSSOVER BEAM FITTING IAW DWG A53833516, A53811470, SRM 51-72-10.

Part: FILTER — CLOGGED (FUEL SYSTEM) · airframe 37,683 hrs · 31,556 cycles

REJECTED TAKEOFF AT 70 KTS FOR NR 2 ENGINE FUEL FILTER CLOG ALERT ON ECAM. REPLACED NR 2 ENGINE MAIN FUEL FILTER IAW MM 73-12-03-02 IDLE LEAK CHECKED GOOD. RAN NR 2 ENGINE AT TAKE OFF POWER IAW JRH. NO ECAM MESSAGES NOTED OK TO CONTINUE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 37,613 hrs · 31,498 cycles

DURING INSPECTION OF CIRCUMFERENTIAL SKIN JOINT AT FR 54 BETWEEN STGR 45 LT AND STGR 44 LT FASTENER HOLE 1EA WITH PRIOR BUSHING REPAIR IS ELONGATED. WORK IN CONJUNCTION WITH WORK CARD T 6-5330-29226 C P3. COMPLIED WITH EA 6-5330-160142 - FUSELAGE - MAIN SKIN AT FRAME 54 BETWEEN STGR 44 LT AND 45 LT - REPAIR REF WRI 53304110, REMOVED AND REINSTALLED FISH PLATE, SPACER WEB, AND CORNER BRACKET AT FR 54 TO FOM IAW SRM 51-40-21, PAR 7. REMOVED AND REINSTALLED SUPPORT RIBS TO FOM IAW SRM 51-40-21 PAR 7. REMOVED AND REINSTALLED HYD PUMP SUPPORT PLATE IAW SRM 51-40-21, PAR 7.

Part: SHOCK ABSORBER — GOUGED (LT MLG) · airframe 37,613 hrs · 31,498 cycles

LEFT MLG THRU HOLE FOR BOGIE BEAM PIN STRUT SIDE, LT INBD BUSHING GOUGED IN SEVERAL PLACES. DEEPEST GOUGE MEASURES .014" WITH MECHANICAL GAGE COMPLIED WITH EA 6-3210-160132 LANDING GEAR LT MLG BOGIE BEAM BUSH DAMAGE. ADDITIONAL WORK COMPLIED ON N00960.

Part: WEB — CRACKED (ZONE 400) · airframe 37,613 hrs · 31,498 cycles

NR 2 ENGINE PYLON OTBD LATERAL PANEL BETWEEN RIB 6 -7 HAS TWO CRACKS BOTH MEASURE .75 OF AN INCH. STOP DRILLED CRACKS IAW SRM 54-52-31, PG 212, 213, 214 CONFIG 1 INSTALLED. REPAIR DOUBLER IAW A310-200, 54-52-31, PG 215.

Part: FLOORBEAM — FAILED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

MAIN CABIN FLOORBEAM MISREPAIRED. REPAIRED IAW EA 6-5310-161396 COMPLING WITH PART 2 OF EA AND RDAS REF 70563824/003/2012 ISSUE A. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOORBEAM — MISREPAIRED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

FLOORBEAM MISREPAIRED. REPAIRED IAW EA 6-5310-161396 COMPLING WITH PART 1 OF EA AND RDAS REF 70563824/003/2012 ISSUE A. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — DAMAGED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

FRAME 24 AT STRINGER 13R WAS FOUND WITH VISIBLE DISTORTION TO UNDERLYING FRAME SPLICES. FOUND FRAME SECTION DAMAGE BEYOND ECONOMICAL REPAIR AND R & R FRAME SECTIONS BETWEEN STRINGERS 8R TO 22R IAW SRM 51-72-10, PAGES 1 TO 3, SRM 51-40-21, PG 10 TO 22, DRILLED ALL PARTS IAW SRM 51-40-44, PG 17.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

DURING INSTALLATION, FOUND FLOOR PANEL 252BF CRACKED. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 37,613 hrs · 31,498 cycles

RT ELEVATOR LOWER SKIN AT RIB 17 HAS 2EA AREAS OF DELAMINATION.

Part: WEDGE — DEBONDED (LT ELEVATOR) · airframe 37,613 hrs · 31,498 cycles

LEFT ELEVATOR T/E WEDGE AT RIB 11 AND 14 SPLICES UPPER AND LOWER SURFACES ARE DEBONDING AND CORRODED. REPAIRED IAW A300-600 SRM 55-21-11 C1 PARA. 5.I. FIG. 209.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

FLOOR CLEVIS ADAPTER BETWEEN SEAT TRACK 2R AND 3R INSTALLED NOT ALIGN AND HAS 2 EA ELONGATED FASTENER HOLES. R & R DUMMY TRACK IAW SRM 51-72-10.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

FLOOR SEAT TRACK 2R HAS 5 EA ELONGATED HOLES FROM FRAME 54 TO 54.2 AT RT FLANGE. R & R SEAT TRACK 2R BETWEEN FRAMES 54 AND 54.2 IAW SRM 51-72-10.

Part: FLOORBEAM — BENT (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

FLOORBEAM TOP FLANGE IS BENT 10 SQUARE INCHES AT CLEVIS ADAPTER BETWEEN SEAT TRACKS 2L AND 3L AND FRAME 37. CUT, REMOVED DAMAGED SECTION & SPLICED IN NEW SECTION OF CROSSBEAM IAW SRM 53-10-15, FIG 201, SHT 3.

Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

FLOORBOARD 231NG DELAMINATED IN MULTIPLE AREAS APPROX 30 SQUARE INCHES. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: SKIN — FAILED (NR 2 SLAT) · airframe 37,613 hrs · 31,498 cycles

RT WING NR 2 SLAT NOSE SKIN BETWEEN RIBS 35 TO 37 IS 4.3" X 2.8" MISREPAIRED. REPAIRED IAW SRM 57-43-11, FIG 202 SHEETS 6 AND 14 PAGES 219 AND 227. COMPLIED WITH EA 6-5750-157852. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — FAILED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

STRINGER 55 RIGHT MISREPAIRED. REPAIRED IAW SRM 53-10-14, FIG 201, PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — MISREPAIRED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

STRINGER 53 LEFT MISREPAIRED BETWEEN FRAMES 63 AND 64. REPAIRED IAW SRM 53-10-14, FIG 201 PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — MISREPAIRED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

STRINGER 56 LEFT MISREPAIRED. REPAIRED IAW SRM 53-10-14 FIG. 201 PGS. 205/206.

Part: STRINGER — MISREPAIRED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

STRINGER 55 LEFT MISREPAIRED. REPAIRED IAW A310 SRM 53-10-14 FIG. 201 PGS. 205/206.

Part: STRINGER — MISREPAIRED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

STRINGER 53L BETWEEN FRAMES 66 AND 69 MISREPAIRED. REPAIRED IAW SRM 53-10-14 FIG 201, PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — MISREPAIRED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

STRINGER 54 LEFT MISREPAIRED. REPAIRED IAW SRM 53-10-14 FIG. 201 PGS. 205/206

Part: FLOORBOARD — DAMAGED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

FLOORBOARD 162HF HAS IMPACT DAMAGE OVER 50 PERCENT OF PANEL. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005 REV J, REF DWG SRZ 25-011.

Part: STRINGER — MISREPAIRED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

STRINGER 53 LEFT MISREPAIRED BETWEEN FRAMES 61 TO 63. REPAIRED IAW SRM 53-10-14. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — MISREPAIRED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

STRINGER 51 LEFT MISREPAIRED BETWEEN FRAMES 61 TO 63. REPAIRED IAW SRM 53-10-14, FIG 201, PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — MISREPAIRED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

STRINGER 53 LEFT MISREPAIRED. REPAIRED IAW A310 SRM 53-10-14 FIG. 201 PGS. 205/206.

Part: STRINGER — MISREPAIRED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

STRINGER 54L BETWEEN FRAMES 65 AND 66 MISREPAIRED. REPAIRED SRM 53-10-14, FIG 201, PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

SEAT TRACK 3R UPPER SURFACE BETWEEN SCALLOPS CORRODED 2 EA AREAS BET, FR 38.2 AND FR.40 MEASURED 6 SQ". REMOVED LEVEL 1 CORROSION ON SEAT TRACK 3R (AREA 1)BET 38.2 AND FR 40 IAW SRM 51-74-10, PG 205. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, PG 103. R & R SEAT TRACK 3R BET FR 38.2 AND FR 40 IAW SRM 51-40-21, PARA 5 & 7 AND IAW SRM 51-49-00, PARA 3.

Part: STRINGER — MISREPAIRED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

STRINGER 47 LEFT MISREPAIRED, FRAMES 59 TO 60. REPAIRED PER SRM 53-10-14 FIG 201 PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — MISREPAIRED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

STRINGER 50 LEFT MISREPAIRED, FRAMES 59 TO 60. REPAIRED PER SRM 53-10-14 FIG 201 PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — MISREPAIRED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

STRINGER 53 LEFT, MISREPAIRED. REPAIRED PER SRM 53-10-14 FIG 201 PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

FLOORBOARD 231AH HAS FIVE CRUSHED AREAS. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

FLOORBOARD 242ZJ DELAMINATED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: STRINGER — MISREPAIRED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

STRINGER 51 LEFT MISREPAIRED. REPAIRED IAW SRM 53-10-14, FIG 201, PAGES 203-206.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

FLOORBOARD 231NH HAS THREE CRUSHED AREAS 5 INCHES LONG. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — DAMAGED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

FWD CARGO FLOORBOARD 132RF DAMAGE ON THE EDGE ABOUT 3 FT. LONG. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: SHEAR PLATE — CRACKED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

SHEAR PLATE LT SIDE WEB CRACKED BETWEEN FR79-FR80. R & R SHEAR PLATE WEB ON FLOOR LT SIDE BETWEEN FR79-FR80 IAW SRM 51-72-10, PG 1.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

FLOORBOARD 241MK CRUSHED ON EDGE & FOUR SEPARATE DELAMINATION AREAS ON UPPER SURFACE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: STRINGER — MISREPAIRED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

STRINGER 56 LEFT MISREPAIRED, FRAMES 73 TO 75. REPAIRED IAW SRM 53-10-14, FIG 201, PAGES 203 TO 206 FLAG NOTE 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOORBEAM — MISREPAIRED (ZONE 130) · airframe 37,613 hrs · 31,498 cycles

FLOORBEAM MISREPAIRED AT FRAME 36. REPAIRED IAW SRM 53-10-15, FIG 207, PAGES 237 TO 242. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOORBOARD — DAMAGED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

FLOORBOARD 162EF HAS COMPOSIT DAMAGE TO LOWER SURFACE AND HAS ONE DAMAGED HOLE GROMET, FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J & SRZ 25-011.

Part: STRINGER — MISREPAIRED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

STRINGER MISREPAIRED. REPAIRED IAW SRM 53-10-14, FIG 201, PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

FLOORBOARD 242EK DELAMINATED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: THRUST PLATE — CORRODED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

THRUST PLATE BETWEEN FRAME 34 AND 35 LOCATED BETWEEN SEAT TRACKS 5L AND 6L HAS 1 SQUARE INCH OF CORROSION. REMOVED CORROSION, ORIGINAL THICKNESS .094", 7EA AREAS MAX LOSS .008, REMAINING .086". AT AREA "7" MAX LOSS .016" REMAINING .078". R & R THRUST PLATE BETWEEN FR 32 & 33 AND Y2462 & Y1959 IAW SRM 51-72-10.

Part: FLOORBEAM — MISREPAIRED (CARGO BAY) · airframe 37,613 hrs · 31,498 cycles

FLOORBEAM MISREPAIRED. REPAIRED IAW SRM 53-10-15, FIG 207, PG 241/242. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — MISREPAIRED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

STRINGER 40 LEFT MISREPAIRED FRAMES 73 TO 74. REPAIRED IAW SRM 53-10-14, FIG 201, PAGES 203 TO 206 FLAG NOTE 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOORBOARD — CORRODED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

FLOORBOARD 251GH HAS CORROSION AT HONEYCOMB CORE OUTER EDGES. FABRICATED REPLACEMENT FLOORBOARD IAW SRZ 25-005, REV J.

Part: FLOORBOARD — DELAMINATED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

MLG WHEEL WELL FLOORBOARD 147AF TOP COATING IS DEBONDED ABOUT 12 FT SQUARE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

FLOORBOARD 232NG HAS 7 PUNCTURES ON TOP SURFACE, FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

FLOOR PANEL 232YH UPPER SURFACE GOUGED 8 SQUARE INCHES. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

FLOOR PANEL 242UJ HAS TWO, 10 INCH CRACKS. FABRICATED FLOOR PANEL 242 UJ IAW DWG NR SRZ 25-005, REV J.

Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

FLOORBOARD 231HG UPPER SURFACE DISBONDED AT AFT OTBD CORNER 10 SQUARE INCHES. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: FLOORBEAM — MISREPAIRED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

FLOORBEAM MISREPAIRED. REPAIRED PER SRM 53-10-15 FIG 203 SHEETS 1-2 PG'S 245-252.

Part: FLOOR SUPPORT — MISREPAIRED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

FLOOR SUPPORT MISREPAIRED. REMOVED FLOOR SUPPORT ASSY AND INSTALLED NEW IAW SRM 51-72-10 PAGES 1 TO 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOOR SUPPORT — MISREPAIRED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

FLOOR SUPPORT LONGERON 3L BETWEEN FRAMES 12A TO 15A MISREPAIRED. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-72-10. REPAIR IS A MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — MISREPAIRED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

SEAT TRACK 5L Y1959 BETWEEN FRAMES 15A TO 17 MISREPAIRED. R & R SEAT TRACK IAW SRM 51-72-10, PAGES 1 TO 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — FAILED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

SKIN AT FRAMES 35 TO 36 & BETWEEN STRINGERS 54 LT TO 54 RT MISREPAIRED. REPAIRED SKIN WITH NEW DOUBLER IAW SRM 53-10-12, FIG 225, SHEET 1, PAGES 357 TO 362.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

SKIN MISREPAIRED, REPAIRED IAW SRM 53-10-12, FIG 225, SHEET 1, PAGES 357 TO 362. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

FLOOR PANEL 252WH HAS ONE, NINE INCH CRACK, FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005 REV J

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

FLOOR PANEL 251RT BROKEN ACROSS ENTIRE MID-SECTION OF PANEL FABRICATED. REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — CHAFED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

FLOOR PANEL 231EF HAS THIRTY TWO SQUARE INCHES OF CHAFFING ON UPPER SKIN. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

FLOOR PANEL 252PH HAS ONE, TEN INCH CRACK. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 37,613 hrs · 31,498 cycles

FLOOR PANEL 231CF HAS 28 INCHES OF CHAFFING SKIN & A 7 INCH CRACK. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

FORWARD CARGO COMPARTMENT FLOOR PANEL 131QF HAS PUNCTURE ALONG AT TIRE EDGE (BACK SIDE). FABRICATEDED FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 37,613 hrs · 31,498 cycles

FORWARD CARGO COMPARTMENT FLOOR PANEL 131ZF HAS FOUR AREAS OF DELAMINATION ON EDGES. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,997 hrs · 30,322 cycles

SEAT TRACK 6R AT FRAME 47 HAS 1 HOLE WITH EXPOSED METAL WITH CORROSION PRESENT ON TOP AND BOTTOM OF MOUNT HOLE. REMOVED CORROSION IAW SRM 51-74-10. CHECKED LIMITS FOUND OUT OF LIMITS IAW SRM 53-10-16. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 205.

Part: FITTING — CORRODED (ZONE 100) · airframe 35,997 hrs · 30,322 cycles

AVIONICS COMPT FR 15A TO FR 17,STR 44 RT HAS CORROSION ALONG VERT LEG AND BASE. REMOVED LEVEL 1 CORROSION. R & R 2 EA FITTINGS TO FRAME ATTACHMENT AT FR 15A AND FR 17, STR 44RT IAW SRM 51-40-21. FITTING P/N'S A5361060720793 AND A5361060720501.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 35,997 hrs · 30,322 cycles

CORROSION ON SEAT TRACK RT SIDE MAIN UPPER DECK CARGO FR 16 TO FR 18 TRACK NR 4 REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED SECTION OF SEAT TRACK NR 4 RT, FABRICATED REPLACEMENT PART IAW DWG 53610798 AND REPLACED SEAT TRACK NR 4 RT SECTION BETWEEEN FR 16 AND FR 18 IAW SRM 53-40-21.

Part: SUPPORT — CORRODED (DOOR FRAME) · airframe 35,997 hrs · 30,322 cycles

BULK CARGO DOOR INTERNAL STRUCTURE AFT LOWER FRAME HAS CORROSION IN AND AROUND FASTENER HOLE, 1.5 SQ IN REMOVED LEVEL 1 CORROSION. R & R BULK CARGO DOOR AFT LOWER EDGE SUPPORT SECTION IAW SRM 51-40-21.

Part: DOOR FRAME — CORRODED (ZONE 100) · airframe 35,997 hrs · 30,322 cycles

CORROSION ON BULK CARGO DOOR INTERNAL FRAME AROUND FWD FASTENER HOLE 1 IN X 2 IN AND LOWER AFT FASTENER HOLE 1IN X 1IN REMOVED LEVEL 1 CORROSION. R & R BULK CARGO DOOR LOWER FWD EDGE SECTION PROFILE IAW SRM 51-40-21.

Part: FRAME — CORRODED (ZONE 100) · airframe 35,997 hrs · 30,322 cycles

BULK CARGO DOOR INTERNAL STRUCTURE AFT LOWER FRAME HAS CORROSION IN AND AROUND FASTENER HOLE,1.5 SQ IN REMOVED LEVEL 1 CORROSION. R & R BULK CARGO DOOR AFT LOWER EDGE SUPPORT SECTION IAW SRM 51-40-21.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 35,997 hrs · 30,322 cycles

LWR AFT CARGO FLOORBEAM, FR 63 FWD FLANGE HAS 6 SQUARE INCHES OF CORROSION AT 30"-34" LT OF CTR ON LOWER SURFACE OF FLANGE (IN AND AROUND FASTENER HOLES) REMOVED CORROSION IAW SRM 51-74-10, CHECKED LIMITS FOUND OUT OF LIMITS IAW SRM 53-10-15, PB 101 AND 53-10-00 PB 101 TABLE 102, PAGE 106. R & R CROSSBEAM FR 63 IAW SRM 51-72-10.

Part: FRAME — DAMAGED (ZONE 200) · airframe 35,997 hrs · 30,322 cycles

UPPER FUSELAGE FRAME 34R FROM STR 13R TO 22R HAS NUMEROUS SMALL GOUGES AND BARE METAL APPROX 4 SQ IN THROUGHOUT ENTIRE FRAME ON INSIDE OF ACFT DEEPEST OF THE GOUGES IS APPROX .005" BLENDED OUT GOUGES ON FRAME 34R BETWEEN STR 13R TO 22R CHECK LIMITS FOUND OUT OF LIMITS IAW SRM 53-14-13 AND 53-10-00. REPAIRED FR 34R IAW SRM 53-10-13 AND SRM 51-73-10.

Part: TRACK — CORRODED (CARGO DOOR) · airframe 35,997 hrs · 30,322 cycles

LWR AFT CARGO DOOR LWR JAMB BETWEEN FR 61 -62 THERE IS A 8 IN X 1 IN AREA OF CORROSION ADJACENT TO AND GOING UNDER THE CLOSE OUT PANEL. REMOVED CORROSION ON AFT CARGO LOWER JAMB IAW SRM 51-74-10. CHECKED FOUND OUT OF LIMITS IAW SRM 53-10-15. R & R TRACK ASSY A2577503000051 IAW SRM 51-40- 21, PARA 5 PG 7.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 35,997 hrs · 30,322 cycles

UPPER MAIN DECK FLOOR SEAT TRACK 3 RT AT FR 54 TO FR 54.2 HAS 1 EA AREA OF CORROSION IN AND AROUND SCALLOPS. REMOVED LEVEL 1 CORROSION. R & R WITH NEW TRACK IAW SRM 51-40-21 AND SRM 53-15-16, PG 201 - PG 216.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 35,997 hrs · 30,322 cycles

MAIN DECK CARGO COMPT SEAT TRACK 5 LT 2 INCHES AFT OF FR 16A HAS 2 IN X 1 IN AREA OF CORROSION. REMOVED LEVEL 1 CORROSION. FABRICATED REPLACEMENT SEAT TRACK IAW DWG 53611640 AND R & R TRACK 5 LT BETWEEN FR 15A AND FR 18 IAW SRM 51-40- 21, PG 22 AND 51-72--10.

Part: ATTACH ANGLE — CORRODED (ZONE 100) · airframe 35,997 hrs · 30,322 cycles

FR 67, STR 47, RT ATTACH ANGLE HAS EXFOILIATION CORROSION ON AFT INBD ATTACH POINT REMOVED LEVEL 1 CORROSION. FABRIACTED REPLACEMENT ANGLE FOR BULK CARGO FR 67 ATTACHMENT AT STR 47 RT IAW DWG 53978111 AND INSTALLED IAW SRM 53-17-15 AND SRM 51-21-10.

Part: BEARING — DAMAGED (RUDDER HINGE) · airframe 35,997 hrs · 30,322 cycles

NR 2 RUDDER HINGE ARM ON VERTICAL STAB END HAS 2 EA BAD BEARING. R & R 2 EA BEARINGS ON NR 2 RUDDER HINGE ARM IAW E.A.6-5540-135192.

Part: CROSSBEAM — CRACKED (ZONE 100) · airframe 35,997 hrs · 30,322 cycles

AFT CARGO COMPARTMENT CROSSBEAM FR 58 HAS CORROSION UNDER ROLLER TRAY 58 IN RT OF CTR, APPROX 4 SQ IN. REMOVED LEVEL 1 CORROSION. DURING REMOVAL OF CORROSION FOUND 1 INCH CRACK ON CROSSBEAM. REMOVED DAMAGED SECTION OF CROSSBEAM AT FT 58 BETWEEN STR 44 RT AND STR 50 RT AND INSTALLED CARGO FLOOR CROSSBEAM SPLICE REPAIR IAW SRM 53-10-15, FIG 207.

Part: CROSSBEAM — CORRODED (ZONE 100) · airframe 35,997 hrs · 30,322 cycles

LWR AFT CARGO FLOOR BEAM FR 63 HAS CORROSION ON FASTENER HOLES ON FLANGE, 14 SQ INCH AREA REMOVED LEVEL 1 CORROSION. R & R DAMAGED CROSSBEAM AT FR 63, LWR AFT CARGO COMPARTMENT IAW SRM 51-72-10, PG 2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,997 hrs · 30,322 cycles

AFT CARGO COMPT FLOORBEAM FR 66,28'' TO 44'' LT OF CTR LINE FWD FLANGE LWR HAS CORROSION IN AND AROUND FASTENER HOLES APROX 8 SQ IN. REMOVED CORROSION IAW SRM 51-74-10 CHECK AND FOUND FLOORBEAM AT FR 66 OUT OF LIMIT IAW SRM 53-10-00, TABLE 102. REPLACED BEAM WITH A NEW FLOORBEAM AT FR 66 IAW SRM 53-10-15, FG 104.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,997 hrs · 30,322 cycles

CABIN SEAT TRACK 3R FROM FRAME 46-54 HAS NUMOUROUS AREAS OF MODERATE TO SEVERE CORROSION AND AREAS OF BARE METAL APROX 125 SQ IN. REMOVED CORROSION IAW SRM 51-74-10 CHECK SEAT TRACK 3R LIMITS FOUND OUT OF LIMITS IAW SRM 53-10-16, FG 101. R & R SEAT TRACK 3R BETWEEN FR46-FR54 IAW SRM 53-10-16 AND SRM 51-40-21 AND 51-72-10.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 35,997 hrs · 30,322 cycles

COMPLY WITH T CARD REPAIR IAW EA T 6-5310-113006 PART 2,WRI 53102241. ACCOMPLISHED REPAIR ON FUSELAGE FRAME 46 IAW EA 6-5310-113006C PART 2 - FUSELAGE - AD2009-18-16 - EO 6-5310-7-5020. FRAMES 44 TO 46 FOOT FITTINGS CRACKS -REPAIR.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 35,997 hrs · 30,322 cycles

AFT CARGO COMPT. BILGE FR 64 TO FR 65, STR 55R HAS CORROSION ON VERTICAL LEG (APPROX 30 SQ IN TOTAL). REMOVED CORROSION IAW SRM 51-74-10. CHECKED LIMITS AND FOUND OUT OF LIMITS IAW SRM 53-10-14. REPAIRED STR 55R BETWEEN FR 64 AND FR 65 IAW SRM 53-10-14 FIG 201.

Part: BEARING — WORN (RUDDER) · airframe 35,997 hrs · 30,322 cycles

NR 2 RUDDER HINGE ARM ON VERT STAB END, 2 EA BRGS WITH SIDEPLAY. R & R 2 EA BRGS ON NR 2 RUDDER HINGE ARM IAW EA 6-5540-135192, RELEASE DATE MAY 06,2010.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 35,997 hrs · 30,322 cycles

LWR FWD CARGO CEILING AREA FR 36 FLOORBEAM ,ON FWD SIDE ,28'' LT OF CTR. THE VERTICAL STIFFENER IS CRACKED AT THE TOP CRACK LENTH APROX .6250'' LONG. ROUTED OUT CRACK FROM VERTICAL STIFFENER ON FLOORBEAM AT FR 36 IAW SRM 53-10-15, FG 203 NDT AREA VEREFIED NO CRACKS IAW NTM 51-10-08. REPARIED FLOORBEAM IAW SRM 53-10-15, FG 203.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 35,997 hrs · 30,322 cycles

LWR FWD CARGO CEILING AREA FRAME 38 FLOOR BEAM, FWD SIDE 67" LT OF CTRLINE THE VERTICAL STIFFENER IS CRACKED AT THE TOP (CRACK LENGTH APPROX. .3750 IN. LONG) SMOOTH AND BLENDED CRACKED AREA IAW SRM 51-73-10. NDT CHECKED AND FOUND NO CRACKS. FABRICATED REPAIR PARTS AND REPAIRED CROSSBEAM AT FRAME 38 AND 67" LT OF C/L IAW SRM 53-10-15 FIG 203, PAGE 249/250. INSTALLED PARTS IAW SRM 51-40-21.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 35,997 hrs · 30,322 cycles

LWR FWD CARGO CEILING FRAME 25 FLOORBEAM FWD SIDE 27" RT OF CTRLINE THE VERTICAL STIFFENER IS CRACKED AT THE TOP (APPROX. LENGTH IS 1/4IN) BLENDED CRACK AT FRME 25 IAW SRM 51-73-10. NDT VERIFIED REMOVAL OF CRACK. FABRICATED REPAIR ANGLE AND REPAIRED CROSSBEAM AT FR 25 AND 27" RT OF CTRLINE IAW SRM 53-10-15 FIG 203, SHEET 1.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 35,997 hrs · 30,322 cycles

AFT CARGO COMPT BILGE,FRAME RF64-FR65,STR 51R HAS CORROSION ON VERTICAL LEG. REMOVED CORROSION ON STR 51R BETWEEN FR64-FR65 CHECK FOUND TO BE OUT OF LIMIT IAW SRM 53-10-00, FIG 106, TABLE 2 R & R DAMAGE STR 51R, BETWEEN FR FR64-FR65 IAW SRM 53-10-14 PARA 2 SEC A -B.

Part: SKIN PANEL — DENTED (CARGO BAY) · airframe 34,465 hrs · 29,227 cycles

MAIN CARGO DOOR UPPER END, OUTER SKIN DENTED, 9.4 IN LONG, 2 IN WIDE AND .100 IN DEEP, LOCATED 2 IN AFT OF FR 22 CUT OUT DAMAGED AND ACCOMPLISHED SKIN REPAIR IAW FEDEX EA 6-5230-118119, RELEASE DATE 28 MARCH, 2008.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,462 hrs · 29,226 cycles

MAIN DECK CARGO DOOR HINGE MOUNTING SURFACE (A/C FUSELAGE) HAS ELONGATED FASTENER HOLE ONE INCH FWD OF FRAME 23 (OUTBD). REPAIRED ELONGATED FASTENER HOLE IAW FED EX A310-200 EA 6-5230-1169118, DOORS-MAIN DECK CARGO DOOR HINGE DAMAGE-INTERIM REPAIR FOR FERRY FLIGHT.

Part: HINGE — DAMAGED (CARGO DOOR) · airframe 34,462 hrs · 29,226 cycles

MAIN CARGO DOOR HINGE SEGMENT DAMAGED FOWARD OF DOOR ACTUATOR. ACCOMPLISHED INTERIM REPAIR PER EA 6-5230-116948, PART 1. INSTALLED A STRAP IN PLACE OF HINGE NR 2 - 22 WITH BOLTS. MAIN CARGO DOOR AND ALL HINGES TO BE REPLACED AT A LATER DATE PER PART 2 OF EA 6-5230-116948.

Part: FRAME — DAMAGED (ZONE 200) · airframe 34,462 hrs · 29,226 cycles

HOLE NR 5 FRAME 44 LT HAS CRACK INDICATION IN FRAME REAMED HOLE NR 5 TO .375 IAW FEDEX EA 6-5310-113006. COLD WORKED HOLE NR 5 AND REAMED TO .400 IAW FEDEX EA 6-5310-113006. INSTALLED BUSHING IAW FEDEX EA 6-5310-113006. INSTALLED NEW FOOT FITTING AND BRACKETS IAW A310-200 SRM 51-40-21 PAR 7, AND FEDEX EA 6-5310-113006AND FEDEX EA 6-5310-7-5020 PT1.

Part: FRAME — CRACKED (ZONE 200) · airframe 34,462 hrs · 29,226 cycles

HOLE NR 22 FRAME 45 LT HAS CRACK INDICATION IN FRAME, REAMED HOLE 22 FR 45L TO .376 IAW FEDEX EA 6-5310-113006 COLD WORKED HOLE IAW FEDEX EA 6-5310-113006 AND A310-200 SRM 51-40-41. FINAL REAMED HOLE TO .401 IAW FEDEX EA 6-5310-113006. INSTALLED BUSHING IAW FEDEX EA 6-5310-113006. INSTALLED FASTENER NSA 5351-5-9 IAW FEDEX EA 6-5310-113006. ORIGINAL EA ATTACHED TO N/R N01419. ITEM 5A SHOULD READ FRAME AND ITEM 5C SHOULD READ A53870033200 FOR THE FRAME SECTION.

Part: FRAME — CRACKED (FUSLEAGE) · airframe 34,462 hrs · 29,226 cycles

HOLE NR 5 FRAME 44 RT HAS CRACK INDICATION IN FRAME FOOT REAMED HOLE NR 5 LT TO .316 IAW FEDEX EA 6-5310-113006. COLD WORKED HOLE IAW A310- 200 SRM 51-40-41 AND FEDEX EA6-5310-113006. REAMED HOLE TO .323 IAW FEDEX EA 6-5310- 113006. INSTALLED BUSHING IAW FEDEX EA 6-5310-113006. REMOVED AND INSTALLED FOOT FITTING AND BRACKETS IAW A310-200 SRM 51-40-21 PARA 7 AND FEDEX EA 6-5310-113006.

Part: FRAME — CORRODED (BS 1870) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

FWD LOWER CARGO PIT FRAME 34 RBL 56 "T" CAP CORRODED REMOVED CORROSION IAW A310 SRM 51-74-10 ORIGINAL THICKNESS .125 REMAINING THICKNESS .094. REMOVED .031 FOUND TO BE OUT OF LIMITS IAW A310 SRM 53-10-00 TABLE 102 MATERIAL ID T-CAP LN9497.420. REPAIR PROFILE LN 9496.310 IAW A310 SRM 53-14-15 AND 53-10-15, TREATED IAW A310 SRM 51-21-10 AND 51-23-10. INSTALLED IAW A310 SRM 51-10-30.

Part: FRAME — CORRODED (BS 1923) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

FWD LOWER CARGO OIT FR35 LBL56 T-CAP CORRODED REMOVED CORROSION IAW A310 SRM 51-71-10, FOUND TO BE OUT OF LIMITS IAW A310 SRM 53-10-00 ORIGINAL .126 REMAINING .090 REMOVAL OF .036 REMOVED T-CAP IAW SRM 51-40-21 MATERIAL ID LN 9497A420 IAW A310SRM 53-10-15. FABBRICATED IAW A310 SRM 53-10-15. ALODINED IAW A310 SRM 51-21-10. PRIMED AND PAINTED IAW A310 SRM 51-23-10 INSTALLED IAW A310 SRM 53-10-15

Part: FAILSAFE — CRACKED (R1 DOOR) · airframe 34,462 hrs · 29,226 cycles

RT FWD PASSENGER/CREW DOOR CUT OUT FASTENER HOLE ON FAIL-SAFE RING RTA 1285/FR16A 2ND HOLE FROM FIGURE 10 G1 (KIR AO1) CRACK INDICATION FOUND USING BOLT HOLE INSPECTION NTM 53-30-53 PT6 ALL MAINTENANCE ACCOMPLISHED IAW FEDEX EA 6-5330-113003 EA TITLE; FUSELAGE AD2007-11-12 SKIN UNDER R1 DOOR SCUFF PLATE AT FRAME 16A REPAIR.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,462 hrs · 29,226 cycles

CRACK INDICATION IN FR 43A RT SIDE LOWER HOLE EXTENDING FWD AND DOWNWARD APPROX 45 DEGREE, 2 CRACK INDICATIONS IN UPPER CRUCIFORM FITTING AT FR 43A LOWER HOLE RT SIDE BOTH EXTENDING UPWARD APPROX 30 DEGREE, ONE FWD AND ONE AFT, CRUCIFORM CRACKS BEGIN AT INBD FACE OF CRUCIFORM AND EXTEND OUTWARD INTO CRUCIFORM 1/8 INCH LOCATIONS MARKED. REAMED HOLE (BOTTOMHOLE) IN FITTING TO .401 BHEC ACCOMPLISHED BY NDT CRACK IS STILL PRESENT, REAMED HOLE TO .433 CRACK STILL PRESENT. REMOVED FITTING FROM AIRCRAFT FOUND FITTING TO BE CRACKED. FABBED NEW FITTING ON FEDEX NONROUTINE NO1367, LOCATED DRILLED UP AND INSTALLED FITTING IAW A310 SRM 51-40-23 PARAGRAPH 7. RESTORED CIC IAW A310 AMM 51-22-00-0.

Part: FRAME — CORRODED (BS 2029) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

FWD LOWER CARGO PIT FR37 LBL 56 "T" CAP CORRODED UNDER NUT PLATES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW A310 SRM 53-10-00 ORIGINAL .126 REMAINING .092 REMOVED .034. REMOVED T-CAP IAW A310 51-40-21 MATERIAL ID LN9497A420 FOR T-CAP FRAME LN9496B310 IAW A310 SRM 53-10-15. ALODINED IAW A310 SRM 51-21-10. PRIMED AND PAINTED IAW A310 SRM 51-23-10. INSTALLED T-CAP IAW A310 SRM 53-10-15.

Part: BRACKET — CRACKED (ZONE 200) · airframe 34,462 hrs · 29,226 cycles

MAIN CABIN CORNER BRACKET CRACKED BELOW EMERGENCY EXIT DOOR AT FR 43R. REMOVED CRACKED BRACKET IAW A310-200 SRM 51-40-21 PARA 7. FABED BRACKET IAW AIRBUS DWG A53870064. ALODINED IAW A310-200 SRM 51-21-10, PRIMED AND PAINTED IAW A310-200 SRM 51-23-10 AND INSTALLED BRACKET IAW A310-200 SRM 51-40-21 PARA 7 PART MARKED BRACKET IAW FEDEX GMM 7-0-1000.

Part: SEAT TRACK — GOUGED · airframe 34,462 hrs · 29,226 cycles

MAIN CABIN SEAT TRACK Y1959 SCALLOPS GOUGED AND ELONGATED FRAME 20 TO 21. BLENDED SCALLOPS IAW FEDEX A310-200 SRM 53-10-16. FOUND TO BE OUT OF LIMITS IAW FEDEX A310-200 SRM 53-10-16. REMOVED ENTIRE DAMAGED SEAT TRACK SECTION FR 18 -FR 26 MADE CUT IAW FEDEX A310-200 EA 6-5310- 109235 AND REINSTALLED NON DAMAGED PART OF SEAT TRACK FR 20 8 - FR 26 IAW FEDEX A310-200 SRM 51-40-21 PARA 7. FABRICATED NEW SEAT TRACK FR 18 TO FR 20, 8 AND REPAIR SPLICE IAW FEDEX A310-200 EA 6-5310-109235. INSTALLED ALL REPAIR PARTS IAW FEDEX A4310-200 EA 6-5310-109235. APPLIED FR PRIMER IAW FEDEX A310-200 SRM 51-21-10 AND TOP COATED IAW FEDEX A310-200 SRM 51-23-10.

Part: FAILSAFE — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

RT FWD PASSENGER/CREW DOOR CUT OUT AREA AROUND FAIL SAFE RING AND ADJACENT SKIN (SCUFF PLATE AREA) HAS 9 EACH AREAS OF SURFACE CORROSION AND TOOL MARKS. REMOVED CORROSION FROM 9 EACH NOTED AREAS IAW FEDEX A310-200 SRM 51-74-10. 7 OF THE 9 AREAS WERE IN CLOSE PROXIMITY OF EACH OTHER ON THE LOWER PORTION OF THE FAIL SAFE RING AND WERE FOUND TO BE OUT OF LIMITS IAW FEDEX A310-200 SRM 53-12-81 FIG 101. REMOVED AND REPLACED THE LOWER FAIL SAFE RING IAW FEDEX A310-200 SRM 53-12-81 PARA 5C AND AIRBUS DWG 12R53610174 REV F. 2 AREAS OF CORROSION ON SKIN FOUND TO BE WITHIN LIMITS IAW FEDEX A310-200 FRM 53-12-12 DIAG 103 AND FIG 108. RE PROTECTED AREAS IAW FEDEX A310-200 AND 51-23-10 AND 51-21-10.

Part: FRAME — CRACKED (ZONE 200) · airframe 34,462 hrs · 29,226 cycles

HOLES NR 25 AND NR 27 FRAME 46 RT HAS CRACK INDICATIONS IN FRAME FEET. REAMED HOLES 26 AND 27 TO ELIMINATE CRACK INDICATIONS IAW EA 6-5310-113006. REMOVED FOOT FITTING AND BUSHED HOLE 27 IAW EA 6-5310-113006. INSTALLED FOOT FITTING IAW SRM 51-40-21 OAR 7, EA 6-5310-113006 AND W/C E 6-5310-7-5020 PT 2.

Part: FRAME — CRACKED (ZONE 200) · airframe 34,462 hrs · 29,226 cycles

FRAME 46 LT HOLE NR 24 CRACK INDICATION IN FITTING ATTACH ANGLE, HOLE NR 25 CRACK INDICATION IN FRAME FOOT AND ATTACH ANGLE, HOLE NR 27 INDICATION IN FRAME FOOT AND HOLE NR 29 INDICATION IN FRAME FOOT. REAMED HOLES 25 AND 29 IAW EA 6-5310-113006, INSTALLED BUSHINGS IAW EA 6-5310-113006. REAMED HOLES TO .250 IAW EA 6-5310-113006. INSTALLED FASTENERS NSA-5351-4-9 IAW EA 6-5310-113006. LOCATED AND DRILLED NEW FRAME STRAP (HOLES 24 AND 27 IN FRAME STRAP) AND INSTALLED IAW A310-200 SRM 51-40-21 PAR 7.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

AFT PIT STR 49R, FRAME 59 HAS CORROSION. REPAIRED STR 49R AT FR 59 IAW A310 SRM 53-10-14 FIG 201, REPLACED STR 49R FROM FR 58 TO FR 60.

Part: FRAME — CRACKED (ZONE 200) · airframe 34,462 hrs · 29,226 cycles

HOLE NR 21 FRAME 45 RT HAS CRACK INDICATION IN FRAME FOOT. REAMED HOLE 21 FR 45R TO .314 IAW EA 6-5310-113006. COLD WORKED HOLE IAW EA 6-5310-113006 AND SRM 51-40-41 PF 5/6 TABLE 1. FINAL REAMED HOLE TO .339 IAW EA 6-5310-11306. INSTALLED FASTENER IAW EA 6-5310-113006.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 34,462 hrs · 29,226 cycles

ULTRASONIC INSPECTION INDICATED A CRACK IN THE LOWER FILLET RADIUS OF THE LATERAL PANEL STRINGER 36 JUST FORWARD OF FRAME 54 BETWEEN THE 4TH AND 5TH FASTENER HOLES, CRACK LENGTH ESTIMATED AT 1 INCH. REPAIRED AREA AT FRAME 54 STRINGER 36R IAW EA NR 6-5330-112997 "FUSELAGE -AD 98-26-01 SKIN PANEL AT FRAME 54 AND STRINGER 36R REPAIR".

Part: KEELBEAM — CRACKED (ZONE 100) · airframe 34,462 hrs · 29,226 cycles

NOSE GEAR WELL, RT BULKHEAD STRAP CRACKED BETWEEN FR 13A AND FR 14 UNDER E/E COMPT FLOOR PANEL NR 122NF. REMOVED & REINSTALLED HARDWARE FOR NOSE GEAR UPLOCK SUPPORT REF SRM 51-40-21. REMOVED AND REINSTALLED RT NLG GROUND CONTROL TORQUE TUBE REF AMM 32-31-00-2 & SRM 51-40-21. PERFORMED NLG DOOR GROUND OPEN & CLOSE, OPS CHECK REF AMM 32-31-00-5. OPS CHECK GOOD COMPLIED WITH EA 6-5310-109234.

Part: HINGE — CRACKED (ZONE 700) · airframe 34,462 hrs · 29,226 cycles

RT AFT NLG DOOR FWD HINGE FITTING CRACKED REMOVED AND REPLACED FWD HINGE FITTING ASSY. ON RT AFT NLG DOOR REF A310-200, CMM 52-82-12 AND AIRBUS INDUSTRY PMS 01-05-58.

Part: SKIN — DENTED (CARGO DOOR) · airframe 34,462 hrs · 29,226 cycles

BULKPIT DOOR SKIN HAS TWO DENTS ON TOP OF DOOR CENTER. DENT OUT OF LIMITS. FABRICATED REPAIR PARTS IAW A310 SRM 52-30-00. ALODINED, PRIMED, INSTALLED AND PAINTED REPAIR IAW A310 SRM 51-21-00, 51-23-10, 51-40-21 AND 51-23-20.

Part: HINGE FITTING — CRACKED (NLG DOOR) · airframe 34,462 hrs · 29,226 cycles

LT AFT NLG DOOR, AFT HINGE CRACKED. REMOVED AND REPLACED LT AFT NLG AFT HINGE FITTING IAW A310-200 CMM 52-82-12 P 204.

Part: SKIN — DENTED (CARGO DOOR) · airframe 34,462 hrs · 29,226 cycles

FOUND BULK PIT DOOR SKIN DENTED AT FWD LOWER EDGE. DENT FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 52-30-00 PAGE 108. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW A310-200 SRM 52-30-00 FIG 206, AND SRM 51-40-21.

Part: FITTING — CRACKED (ZONE 100) · airframe 34,462 hrs · 29,226 cycles

FWD LOWER CARGO COMP, FR 37 RT FRAME TO CROSSBEAM CONNECTION FITTING CRACKED. REMOVED FITTING IAW A310-200 SRM 51-72-10 PG 2 PARA 5A LOCATED AND DRILLED NEW FITTING P/N 5377364420100 P.O. NO 598023.1 IAW A 310-200 SRM 51-72-10 PG 2 PARA 6A. INSTALLED NEW FITTING IAW A 310-200 SRM 51-40-30.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 34,462 hrs · 29,226 cycles

FUSELAGE FLUSH REPAIR DOUBLER AT FR 34-35 STR 43/45 LT. REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED FLUSH REPAIR AT FR 34/35 STGR 43/45 LT. FOUND NOT TO BE WITHIN FAA APPROVED DATA. REMOVED REPAIR AND ACCOMPLISHED EXTERNAL REPAIR IAW A310 SRM 53-10-12 FIG 225.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

LT FWD ENTRY DOOR OPENING, LWR FWD CORNER HAS DEFECT INDICATION FROM EDDY CURRENT INSPECTION, IN CORNER STRAP EDGE. REMOVED AND REPLACED CORRODED CORNER STRAP (GUSSET) IAW A310-200 SRM 51-40-21 PAR 7. MACHINED CORNER STRAP, AND FORMED TO CONTOUR, IAW AIRBUS DWG NR 12A 53611517, REV "D" AND ABS 5032.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

LT FWD ENTRY DOOR OPENING LOWER AFT CORNER HAS DEFECT INDICATION FROM EDDY CURRENT CORNER STRAP EDGE. CLEANED AREA IAW FEDEX A310-200 SRM 51-74-10. AREA WAS FOUND TO HAVE SEVERE INTERGRANULAR CORROSION REQUIRING COMPONENT REPLACEMENT. REMOVED STRAP IAW FED EX A310-200 SRM 51-40-21 PAR 7. MAT ID 2024 T351 IAW AIRBUS DWG 12A536101516 REV D AND ABS 5032. MACHINED CORNER STRAP IAW AB DWG 12A536 11576 REV D. FORMED CORNER STRAP IAW AB DWG 12A53611516 REV D. ALODINED, PRIMED AND PAINTED CORNER STRAP IAW FED EX A310-200 SRM 51-75-10. INSTALLED CORNER STRAP IAW FED EX A310-200 SRM 51-40-21 PARA 7.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 34,462 hrs · 29,226 cycles

FUSELAGE EXTERNAL REPAIR DOUBLER AT FR 18-19 STRINGERS 38/39 RT FWD OF FWD CARGO DOOR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. VISUALLY INSPECTED EXISTING REPAIR DOUBLER AT FRAME 18/19 RT BETWEEN STRINGERS 38-39 AND FOUND THAT REPAIR DID NOT CONFORM TO APPROVED REQUIREMENTS. REMOVED AND REPLACED EXTERNAL REPAIR DOUBLER IAW A310-200 SRM 53-10-12 FIG 225.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

AVIONICS COMPARTMENT FLOOR, FR 17 ( X1315 ) STR 43L, FITTING CORRODED. REMOVED AND REPLACED STRINGER END FITTING IAW A310-200 SRM 51-40-21, 51-24-00 AND 51-43-00 TABLE 1.

Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

FWD LOWER CARGO PIT "T" CAP CORRODED FR 38.2 (X2187) BL 56R ( -Y1420) UNDER NUT PLATE. REMOVED AND REPLACED "T" CAP ( EXTRUSION ) IAW A310-200 SRM 53-10-15 PAGE 237-242.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

MAIN CABIN, FLOOR SUPPORT CORRODED FROM FR12 TO FR 16A, (STA X1067 TO X1285) BL 56L (Y1456 ), REMOVED AND REPLACED FLOOR SUPPORT IAW A310-200 SRM 51-40-21 PAR 6 AND 7.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

CABIN, SEAT TRACK CORRODED STA X1240 TO X1340 LBL Y450. REMOVED AND REPLACED SEAT TRACK IAW A310-200 SRM 51-40-21 PAR 6 AND 7.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

AFT CARGO PIT FLOORBEAM CORRODED, FR 64 ( STA. X3461) BL 32 R ( -Y810 ) REMOVED AND REPLACED FLOORBEAM IAW A310-200 SRM 51-40-21 PG 7, 15, & 26, AND A310- 200 SRM 51-40-44 PG 9.

Part: STRAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

AFT CARGO PIT FLOOR SUPPORT STRAP CORRODED AT FR 64 ( STA X3461) BL 32R (-Y810). REMOVED AND REPLACED FLOOR SUPPORT STRAP, FR 64 TO FR 67, (STA X3461 - X3620 ) BL 32R ( -Y810 ) IAW A310-200 SRM 51-40-21 PG 7, 15 & 26, AND A310-200 SRM 51-40-44 PG 9.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

BULK PIT FLOORBEAM CORRODED AT FR 65 ( X3514 ) BL 21L TO 35L ( -Y530 TO -Y890) REMOVED AND REPLACED FLOORBEAM IAW A310-200 SRM 51-40-21 PG 26 & 39, AND A310-200 SRM 51-40-44 PG 7.

Part: LONGERON — CRACKED (ZONE 200) · airframe 34,462 hrs · 29,226 cycles

RT LONGERON 11 HAS DEFECT INDICATION ON INNER FLANGE BETWEEN 2 RIVETS AT APPROXIMATE STA 4051. REMOVED COVER PLATE TO GAIN ACCESS TO INNER FLANGE. REMOVED DAMAGE, REPAIRED AREA AND INSTALLED DOUBLE FILLER AND COVER PLATE IAW SRM AB310/200 53-18-18 FIG 205C PAGE 235.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

CABIN SEAT TRACK CORRODED FROM STATION 1240CM TO 1280 CM, Y 5.0CM. BLENDED AREA IAW A310-200 SRM 51-74-10 AND FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 51-10-16 FIG 101. REMOVED AND REPLACED SEAT TRACK IAW A310-200 SRM 51-40-21 PARA 6 AND 7.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 34,462 hrs · 29,226 cycles

MAIN CABIN SEATTRACK ADAPTER AT FR 60/61, Y - 1456 IS CRACKED REMOVED ADAPTER IAW A310-200 SRM 51-40-21 PARA 7. LOCATED AND DRILLED NEW ADAPTER REF A310-200 SRM 51-40-44 PARA 2. INSTALLED NEW ADAPTER REF A310-200 SRM 51-40-21 PARA 7.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 34,462 hrs · 29,226 cycles

FWD LOWER CARGO COMPARTMENT, FLOORBEAM FITTING CRACKED AT FR 34 (X1870) BL 60L (Y1520).

Part: TRACK — GOUGED (ZONE 200) · airframe 34,462 hrs · 29,226 cycles

MAIN CABIN FLOOR ADAPTER TRACK GOUGED AT FR38.1 (STA X2135) BL 44L (Y1120) REMOVED AND REPLACED ADAPTER REF: A310-200 SRM 51-40-21 PAR 6 AND 7.

Part: ATTACH FITTING — CRACKED (ZONE 100) · airframe 34,462 hrs · 29,226 cycles

FWD LOWER CARGO COMPARTMENT, FLOORBEAM FITTING CRACKED AT FR 34 (X1870) BL 60L (Y1520). REMOVED FITTING IAW A310 SRM 51-72-10 PG 2 PARAGRAPH 5A LOCATED AND DRILLED NEW FITTING PN A5377364420100 IAW A310 SRM 51-72-10 PG 2 PARAGRAPH 6A. INSTALLED NEW FITTING IAW A310 SRM 51-40-30.

Part: ADAPTER — CRACKED (ZONE 200) · airframe 34,462 hrs · 29,226 cycles

MAIN DECK CARGO TIE-DOWN ADAPTER CRACKED AT FR54.3, (STA X3090) RBL -Y685. REMOVED AND REPLACED ADAPTER REF: A310-200 SRM 51-40-21 PAR 6 AND PAR 7.

Part: TRACK — GOUGED (ZONE 200) · airframe 34,462 hrs · 29,226 cycles

MAIN DECK FLOOR, ADAPTER TRACK GOUGED AT FR37, (STA X2029) BL 44L (Y1120). REMOVED AND REPLACED ADAPTER REF: A301-200 SRM 51-40-21 PAR 6 AND 7.

Part: STRINGER — CORRODED (ZONE 100) · airframe 34,462 hrs · 29,226 cycles

AFT CARGO PIT BILGE AREA, STRINGER 55L CORRODED, FR 54.3 T0 FR 58 (STA X3090 TO STA X3143). REMOVED COROSION ON STRINGER 55L BETWEEN FRAMES 54.3 AND 58 IAW SRM 51-74-10 AND CHECKED LIMITS STRINGER 52L FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. CUT OUT DAMAGED SECTION OF STRINGER 52L BETWEEN FRAME 54.1 TO 58 IAW SRM 51-40-40. FABBED REPAIR COUPLINGS IAW SRM 53-10-14 FIG 201 A. ALODINED STRINGER AND REPAIR PARTS IAW SRM 51-21-10, TOPCOAT AND PRIMED STRINGER AND REPAIR PARTS IAW SRM 51-23-10. INSTALLED NEW STRINGER SECTION AND REPAIR PARTS IAW SRM 53-10-14 PG 204A/204B.

Part: STRINGER — CORRODED (ZONE 100) · airframe 34,462 hrs · 29,226 cycles

AFT CARGO PIT BILGE AREA, STRINGER 57L CORRODED, FR 54.2 TO FR 54.3 (STA X3037 TO STA X3090). COMPLIED WITH EA 6-5310-113000.

Part: STRINGER — CORRODED (ZONE 100) · airframe 34,462 hrs · 29,226 cycles

AFT CARGO PIT, STRINGER 53L CORRODED, FR 58 TO FR 59 (STA X3143 TO STA X3196). REMOVED COUPLING AND STRINGER SECTION. REMOVED SHEAR TIE. FABBED COUPLING AND STRINGER SECTION IAW SRM 53-10-14. ALODINED IAW SRM 51-21-10. PRIMED & PAINTED IAW SRM 51-23-10. INSTALLED COUPLING AND STRINGER SECTION AND SHEAR TIE IAW SRM 51-40-21.

Part: STRINGER — CORRODED (ZONE 100) · airframe 34,462 hrs · 29,226 cycles

AFT CARGO PIT, STRINGER 53L CORRODED BETWEEN FRAME 54.3 AND FRAME 58 (STA X3090 TO STA X3143 ). REPAIRED STRINGER 53L AT FRAME 54.3 TO FRAME 58 IAW A310 SRM 53-10-14 PG 204A/204B FIG 201A.

Part: TRACK — CRACKED (ZONE 200) · airframe 34,462 hrs · 29,226 cycles

MAIN DECK FLOOR, ADAPTER TRACK CRACKED, STA X3143, BL -Y685 TO -Y910. REMOVED AND REPLACED ADAPTER TRACK IAW A310-200 SRM 51-40-21 PAR 6, AND 51-40-44 PAR 2.

Part: STRINGER — CORRODED (ZONE 100) · airframe 34,462 hrs · 29,226 cycles

AFT CARGO PIT BILGE AREA, STR 54L CORRODED BETWEEN FR 58 AND 59 ( X3143 TO X3196 ). REMOVED COUPLING AND STRINGER. REMOVED ATTACH ANGLE. FABBED STRINGER SECTION IAW SRM 53-10-14. FABBED COUPLING IAW SRM 53-10-14. ALODINED COUPLING AND STRINGER IAW SRM 53-21-10. PRIMED AND PAINTED IAW SRM 51-23-10 INSTALLED COUPLING AND STRINGER IAW SRM 51-40-21.

Part: ADAPTER — CRACKED (FUSELAGE) · airframe 34,462 hrs · 29,226 cycles

MAIN DECK, ADAPTER TRACK CRACKED, FR 66 (STA X3567) BL 0 TO BL 7L (Y0 TO Y180). REMOVED AND REPLACED ADAPTER IAW A310-200 SRM 51-40-21 PAR 7, AND SRM 51-40-44 PAR 2.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

AFT CARGO PIT BILGE AREA, STR 52L CORRODED FROM FR 54.2 TO FR 58. ( X3037 TO X3143). REMOVED CORROSION IAW A310 SRM 51-74-10 ,OUT OF LIMITS IAW A310 SRM 53-10-00, REMOVED FSATENERS TO SUB STRUCTURE COMMON TO THE REPAIR AREA, REMOVED STRINGER SECTION FROM FRAME 54.1 TO FRAME 60, FABBED NEW STRINGER AND ALL REPAIRE PARTS IAW A310 SRM 53-10-14 201/201A, ALODINED IAW A310 SRM 51-21-10 PRIMED AND PAINTED IAW A310 SRM 51-23-10, INSTALLED STRINGER AND REPAIR PARTS IAW A310 SRM 53-10-14 FIG 201/201A REINSTALLED ALL FASTERNERS AND SUBFRAME PREVIOUSLY REMOVED IAW A310 SRM 51-40-21.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 34,462 hrs · 29,226 cycles

AFT PIT, BETWEEN FR 64/3461 AND 63/3408 STR 52R CORRODED. REMOVED CORROSION IAW A310-200 SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW A310- 200 SRM 51-10-00. REMOVED AND REPLACED STRINGER SECTION IAW A310-200 SRM 53-10- 14 PG 203/204

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,462 hrs · 29,226 cycles

FWD LWR CARGO COMP, FR 38 RT FRAME TO CROSS BEAM CONNECTION FITTING CRACKED. REMOVED FITTING IAW A310-200 SRM 51-72-10 PG 2 PARAG 5A LOCATED AND DRILLED NEW FITTING P/N AS5377364420100 PO 598232.1 IAW A310-200 SRM 51-72-10 PG 2 PARAG. 6A INSTALLED FITIING IAW A310-200 SRM 51-40-30

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,462 hrs · 29,226 cycles

FWD LWR CARGO COMP, AT FR STAT 36 RT FRAME TO FLOORBEAM CONNECTION FITTING CRACKED. REMOVED FITTING IAW A310-200 SRM 51-72-10. LOCATED AND DRILLED NEW FITTING P/N A5377364420100 IAW A310-200 SRM 51-72-10 PG 2 PARAG 6A INSTALLED NEW FITTING IAW A310-200 SRM 51-40-30

Part: STRINGER — GOUGED (FUSELAGE) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

FOUND AFT PIT STR 47R AT FRAME 59 IS GOUGED ON UPPER SURFACE. REMOVED GOUGE ON STRINGER 47R IAW FEDEX A310 SRM 51-73-10, STRINGER 47R OUT OF LIMITS IAW A310 SRM 53-10-00. REMOVED IEA SHEAR TIE AT FRAME 59 BETWEEN STRINGER 47R AND 48R IAW A310 SRM 51-40-21 PG 23-27. REMOVED DAMAGE STRINGER SECTION IAW A310 SRM 52-10-14 203/204 FIG201. LOCATED AND DRILLED NEW STRINGER SECTION IAW A310 FABBED REPAIR COUPLING IAW A310 53-10-14PG 203/204 FIG 201 ALODINED REPAIR PARTS IAW A310 SRM 51-21-10 PRIMED AND TOP COATED REPAIR PARTS IAW A310 SRM 51-23- 10 INSTALLED NEW STRINGER SECTION AND COUPLING IAW A310 53-10-14 PG203/204 FIG201. INSTALLED SHEAR TIE IAW A310 SRM 51-40-21 PG 23-27.

Part: FITTING — CORRODED (FUSELAGE) · airframe 34,462 hrs · 29,226 cycles

FWD LWR CARGO COMP, FR 38.1 RT FRAME TO CROSS BEAM CONNECTION FITTING CORRODED. REMOVED FITTING IAW A310-200 SRM 51-72-10 PG 2 PARAG 5A LOCATED AND DRILLED NEW FITTING P/N A5377364420100 PO 598232.3 IAW A310-200 SRM 51-72-10 PG 2 PARAG 6A INSTALLED NEW FITTING IAW A310-200 SRM 51-40-30

Part: ATTACH FITTING — CRACKED (FUSELAGE) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

FWD LWR CARGO COMP, FR 38.1 LT FRAME TO CROSS BEAM CONNECTION FITTING CRACKED. CLEANED AREA IAW AMM12-21-2, REMOVED, LOCATED & INSTALLED FITTING IAW SRM 51-72-10 PG 2 PARA 5.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,462 hrs · 29,226 cycles

FWD LWR CARGO COMP, FR 37 LT FRAME TO CROSS BEAM CONNECTION FITTING CRACKED. CLEANED AREA IAW A310-200 SRM 51-72-10 LOCATED & DRILLED NEW FITTING P/N 5377364420000 PO# 598020.3 IAW A310-200 SRM 51-72-10 INSTALLED FITTING IAW A310-200 SRM 51-72-00 CORROSION LEVEL MISTAKENLY CHECKED THIS ITEM NOT CORROSION.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,462 hrs · 29,226 cycles

FWD LWR CARGO COMP AT FR 35 RT FRAME TO FLOORBEAM CONNECTION FITTING CRACKED. REMOVED FITTING IAW A310-200 SRM 51-72-10 PG 2 PARAG. 5A LOCATED AND DRILLED NEW FITTING P/N AS377364420100 PO3 598232.2 IAW A310-200 SRM 51-72-10 PG 2 PARAG. 6A ISTALLED FITTING IAW A310- 200SRM 51-40-30.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

AFT PIT STR 51R CORRODED AT FRAME 59. REPAIRED STRINGER PER SRM 53-10-14 FIG 201. REMOVED CORROSION PER SRM 51-74-10. CHECKED LIMITS FOUND OUT OF LIMITS. LOCATED AND DRILLED PER SRM 51-40-44. FABBED COUPLING SPLICE PER SRM 53-10-14. ALODINED, PRIMED AND PAINTED PER SRM 51-21-10 AND 53-23-10.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

FOUND AFT PIT STR 51R , FRAME 54.3-58 STRINGER CORRODED. CUT OUT CORRODED SECTION AND SPLICED IN NEW SECTION IAW SRM 53-10-14 AND SRM 51-40-44.

Part: FITTING — CORRODED (FUSELAGE) · airframe 34,462 hrs · 29,226 cycles

FWD LWR CARGO COMP AT FR STA 34 LT FRAME TO FLOORBEAM CONNECTION FITTING CORRODED, FITTING FOUND TO BE CRACKED ALSO. REMOVED AND REPLACED FITTING IAW A310-200 SRM 51-72-10 PG 2.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

FWD PIT FRAME STA 38.2 RT FRAME TO FLOORBEAM CONNECTION FITTING CORRODED. REMOVED ALL SUBSTRUCTURE AND CARGO SYS COMPONENTS COMMON TO FRAME FITTING AREAS FROM FR 33 - 38.2 RT IAW A310-200 AMM 25-52-48-4,44-4,26-4 AND A310-200 AMM 25-52-48-4 AND A310-200-SRM 51-40-21. REMOVED AND REPLACED FRAME FITTING AT FR 38.2 RT IAW A310-200-SRM 51-72-10. REINSTALLED ALL PREVIOUSLY REMOVED SUBSTRUCTURE AND CARGO SYS COMPONENTS IAW A310-200-AMM 25-52-48-4, AND A310-200 SRM 51-40-21. A310- 200 AMM 25-52-44-4, A310-200 AMM 25-52-26-4. MAJOR REPAIR.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

FWD LWR CARGO COMP AT FR STAT 38.2 LT FRAME TO FLOORBEAM CONNECTION FITTING CRACKED. REMOVED FITTING IAW SRM 51-72-10 PG 2 PARAG 5A LOCATED AND DRILLED NEW FITTING IAW SRM 51-72-10 PG 2 PARAG 8 .6A INSTALLED NEW FITTING IAW SRM 51-40-30.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

FWD PIT FRAME STA 35 LT FRAME TO FLOORBEAM CONNECTION FITTING CORRODED. REMOVED ALL SUBSTRUCTURE AND CARGO SYS COMPONENTS FROM FR 24 -38.2 L/H TO FACILITATE FITTING REPLACEMENTS IAW A310-200 AMM25-52-44-4,26-4,21-4, AND A310-200 SRM 51-20--41. REMOVED AND REPLACED FRAME FITTING AT FR 35 L/H IAW A310-200 SRM 51-72- 10.REINSTALLED ALL PREVIOUSLY REMOVED SUBSTRUCTURE AND CARGO SYS COMPONENTSIAW A310-200 AMM 25-52-44-4,26-4,21-4 AND A310 -200 SRM 51-20-41 MAJOR REPAIR.

Part: FITTING — CRACKED (FUSELAGE) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

FOUND FWD LWR CARGO COMP AT FR STAT 33 RT FRAME TO FLOORBEAM CONNECTION FITTING CRACKED. CRACKED REMOVED AND REPLACED FITTING IAW A310-200 SRM`S 51-72-10 AND 51-40-30.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

AFT CARGO BILGE CORROSION ON STR - 52L, FR 58 TO FR -59. REMOVED CORROSION IAW A310 SRM 51-74-10 FOUND TO BE OUT OF LIMITS IAW A310 SRM 53-10-00.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

CORROSION ON STR-56R, FR-59 TO FR-60 -AFT CARGO BILGE. REMOVED CORROSION IAW SRM 51-74-10. FOUND TO OUT OF LIMITS IAW SRM 53-10-00. CUT OUT DAMAGE SECTION OF STRINGER IAW SRM 53-10-74. LOCATED AND DRILLED NEW SECTION OF STRINGER IAW SRM 51-40-44, FABBED SPLICE REPAIR IAW SRM 53-10-14. ALODINED REPAIR PARTS IAW SRM 51-21-10, PRIMED AND TOP COATED REPAIR PARTS IAW SRM 51-23-10. INSTALLED NEW STRINGER SECTION AND SPLICE IAW SRM 53-10-14.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

AFT CARGO BILGE, CORROSION ON STR-56R, FR-58 TO FR-59. STRINGER WAS REPLACED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

FOUND AFT PIT STR 54R CORRODED AT FRAME 58 -59. REPAIRED IAW SRM 53-10-14 FIG 210.

Part: ADAPTER — CRACKED (SEAT TRACK) · airframe 34,462 hrs · 29,226 cycles

MAIN CABIN AT FRAME 45(X2506) LBL-36 (Y-910) SEAT TRACK ADAPTER IS CRACKED. REMOVED AND REPLACED ADAPTOR TRACK IAW A310 SRM 51-40-21.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

FUSELAGE SKIN/INTERIOR SURFACE BETWEEN FRAME 78 AND 79 AT STRINGER 50R HAS CORROSION. REMOVED CORROSION ON INTERNAL DOUBLER IAWA310 SRM 51-74-10 FOUND TO BE OUT OF LIMITS IAW A310 SRM 53-10-00 REPLACED INTERNAL DOUBLER FROM FRAME 78-80 STRINGER 45R IAW A310 SRM 51-40-21, 51-26-00, 51-27-00, 51-40-44, 51-21-10. REMOVED AND REINSTALLED STRINGER 45R FROM FRAME 78 TO 80, STRINGER 47AND 48R FROM FRAME 79-80 STRINGER 50R FROM FRAME 78-80, SHEAR TIE ON FRAME 79 FROM FRAME 50R TO 45R, PAN FROM FRAME 78 TO 79 STRINGER 45R TO 50R, DRAIN MAST IAW A310 SRM 51-40-21, 51-21-10, WDM30-71-02, AMM 30-71-11-4 TO FOM,

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

AFT PIT STRINGER 50R CORRODED AT FRAME 59. REMOVED CORROSION IAW A310 SRM 51-74-10 FOUND TO BE OUT OF LIMITS IAW A310 SRM 53-10-00 UT GUAGE T 8225B. REMOVED DAMAGED SECTION OF STRINGER IAW A310 SRM 53-10-14 FIG 201. FABRICATED REPAIR COUPLING AND LOCATED AND DRILLED STRINGER SECTION IAW A310 SRM 53-10-14 FIG 201. ALODINED REPAIR PARTS IAW A310 SRM 51-23-10. PRIMED REPAIR PARTS IAW A310 SRM 51-23-10 PAINTED REPAIR PARTS IAW A310 SRM 51-23-10. INSTALLED REPAIR AND STRINGER SECTION IAW A310 SRM 53-10-14 FIG 201.

Part: ADAPTER — CRACKED (CABIN SEAT TRACK) · airframe 34,462 hrs · 29,226 cycles

FLOORBEAM ADAPTER BETWEEN SEAT TRACK AT LBL17 AND LBL 37 AT FRAME 46 IS CRACKED. REMOVED AND REPLACED ADAPTER IAW A310 SRM 51-40-21 PAR 6.

Part: ADAPTER — CRACKED (SEAT TRACK) · airframe 34,462 hrs · 29,226 cycles

CARGO TIE DOWN ADAPTER CRACKED AT FRAME 44 (STA 2824) BL36R (-Y900) REMOVED CRACKED TIE DOWN ADAPTER IAW A310-200 SRM 51-40-21 PAR 5. RECIEVED NEW CUSTOMER FURNISHED PART NR R538D104820200 P/O NR 597285.1. INSTALLED NEW CARGO TIE DOWN ADAPTER IAW A310-200 SRM 51-40-21 PAR 5.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

AFT PIT STRINGER 52R CORRODED AT FRAME 58 TO 59. REMOVED CORROSION PER SRM 51-74-10. CHECKED LIMITS ORIG MATERIAL .110. REMAINING MATERIAL .097. REMOVED .013 FOUND TO OUT OF LIMITS PER SRM 53-10-00. REMOVED DAMAGED STRINGER AND REPLACED WITH NEW REPAIR PER SRM 53-10-14. JOGGLED NEW STRINGER PER SRM 51-26-20. LOCATED AND DRILLED PER SRM 51-40-44. ALODINED PRIMED AND PAINTED PER SRM 51-23-10-AND 51-21-10.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

AFT PIT STRINGER 49R CORRODED BETWEEN FRAME 60 AND 62. FABRICATED REPAIR STRINGER SECTION AND COUPLING, AND REMOVED AND REPLACED CORRODED STRINGER SECTION IAW A310-200 SRM 53-10-14 PG 203 / 204, & SRM 51-40-21.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

AFT PIT STRINGER 50R CORRODED I/B SIDE AT FRAME 58. REMOVED CORROSION IAW A310-200 SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00 STRINGER REPLACEMENT ACCOMPLISTED ON FED EX NON ROUTINE N00357.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

AFT PIT STRINGER 48R CORRODED AT FRAME 58. REMOVED CORROSION IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. CUTOUT DAMAGE IAW SRM 53-10-14. LOCATED AND DRILLED NEW STRINGER SECTION IAW SRM 51-40-44. FABBED COUPLING IAW 53-10-14. ALODINED IAW SRM 51-21-10. PRIMED AND PAINTED IAW SRM 51-23-10. INSTALLED REPAIR IAW SRM 53-10-14 FIG 201.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

AFT PIT STRINGER 45R , FRAME 58 HAS CORROSION ON STRINGER. REMOVED CORROSION IAW A310 SRM 51-74-10. CORROSION OUT OF LIMITS PER A310 SRM 53-10-00 PG 106. REMOVED WEB FR54.3 TO 58 STRINGER 45R FOR ACCESS PER A310 51- 40-21 PG 15. CUT OUT DAMAGED SECTION OF STRINGER 45R, FABBED NEW SECTION OF STRINGER 45R, FABBED PLICE DOUBLER PER A310 SRM 53-10-14 FIG 201, INSTALLED NEW SECTION OF STRINGER 45R SPLICE AND WEB FRAME 54.3 TO FRAME 58 PER A310 SRM 53-10-14 FIG 201, A310 SRM 51-40-21 PAGE 36 AND A310 SRM 51-40-21 PAGE 9, STATION 3090 TO 3143.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

FOUND AFT PIT STRINGER 47R AT FRAME 58, CORRODED. REMOVED CORROSION IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. CUT OUT DAMAGED SECTION IAW SRM 53-14-00 FIG 201. LOCATED AND DRILLED NEW SECTION OF STRINGER IAW SRM 51-40-44. FABBED COUPLING IAW SRM 53-10-14. ALODINED, PRIMED AND PAINTED IAW SRM 51-21-10, 51-23-10. INSTALLED REPAIR IAW SRM 53-14-10 FIG 201.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 34,462 hrs · 29,226 cycles

MAIN DECK FLOOR, ADAPTER TRACK ( CROSSBEAM ) CRACKED, FR 50 ( STA X2718 ) BL 17L TO 37L ( Y430 - Y940 ). REMOVED AND REPLACED CROSSBEAM, REF: A310-200 SRM 51-40-21 PAR 5. LOCATED AND DRILLED NEW CROSSBEAM REF: A310-200 SRM 51-40-44 PAR 2.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 34,462 hrs · 29,226 cycles

MAIN DECK FLOOR, ADAPTER TRACK ( CROSS BEAM ) CRACKED, FR 52 ( X2825 ) BL 17L TO BL 37L ( Y430 - Y940 ). REMOVED AND REPLACED CROSS BEAM, REF: A310-200 SRM 51-40-21 PAR 5. LOCATED AND DRILLED NEW CROSS BEAM REF: A310-200 SRM 51-40-44 PAR 2.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 34,462 hrs · 29,226 cycles

MAIN DECK FLOOR, ADAPTER TRACK (CROSS BEAM) CRACKED AT FR 53 ( Z2878 ), BL 17L TO BL 37L ( Y430 - Y940 ). REMOVED AND REPLACED CROSSBEAM, REF: A310-200 SRM 51-40-21 PAR 5. LOCATED AND DRILLED NEW CROSS BEAM REF: A310-200 SRM 51-40-44 PAR 2.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

BULK CARGO PIT FLOOR SUPPORT (LONGITUDINAL PROFILE) CORRODED, FR 60 TO FR 65 ( X3514 TO X3567), BL 4L (Y100). REMOVED AND REPLACED CORRODED FLOOR SUPPORT SECTION IAW A310-200 SRM 51-40-21 PAR 9, & SRM 51-40-44 PG 9

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

BULK CARGO PIT, STRINGER 55 CORRODED AT FRAME 65 (STA X 3514). REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW A310 SRM 53-10-00. INSTALLED STRINGER REPAIR IAW A310 SRM 53-10-14 FIGURE 201.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

AFT PIT, STRINGER 57L CORRODED BETWEEN FR 54.2 AND FR 54.3 (STA X 3037 - 3090). ALL CORRECTIVE ACTION COMPLIED WITH ON EA 6-5310-113000.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

AFT CARGO PIT, STRINGER 52R CORRODED BETWEEN FR 54.2 AND FR 54.3 (STA X 3037 - 3090). FOUND CORROSOIN TO BE OUT OF LIMITS IAW A310-200 SRM 51-10-00 CUT OUT DAMAGED SECTION, FABBED ALL REPAIR PARTS IAW A310 SRM 53-10-14 FIG 201A. ALODINED AND PRIMED IAW A310 SRM 51-21-10. PAINTED PARTS IAW A310 SRM 51-21-23. INSTALLED REPAIR AND REPLACED STRINGER SECTION IAW A310 SRM 53-10-14 FIG 201A

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

AFT CARGO PIT BILGE AREA, STRINGER 56L CORRODED BETWEEN FR 60 T0 FR 61 (STA X 3249 - X3302). REMOVED CORROSION IAW A310 SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW A310 SRM 53-10-00. CUT OUT DAMAGE SECTION IAW A310 SRM 53-10-14. LOCATED AND DRILLED NEW STRINGER IAW A310 SRM 51-40-44. FABBED TWO REPAIR SPLICES IAW A310 SRM 53-10-44. ALODINED IAW A310 SRM 51-21-10, PRIMED AND TOP COATED IAW A310 SRM 51-23-10. INSTALLED STRINGER AND REPAIR PARTS IAW A310 SRM 53-10-14 REINSTALLED SHEAR TIE.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 34,462 hrs · 29,226 cycles

MAIN DECK FLOOR, ADAPTER TRACK ( CROSS BEAM ) CRACKED, FR 50 ( STA X2718 ) BL 17L TO 37L ( Y430 - Y940 ). REMOVED AND REPLACED CROSS BEAM, REF: A310-200 SRM 51-40-21 PAR 5. LOCATED AND DRILLED NEW CROSS BEAM REF: A310-200 SRM 51-40-44 PAR 2.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 34,462 hrs · 29,226 cycles

AFT PIT, BILGE AREA, STRINGER 51R CORRODED, FR 54.1 TO 54.3 (STA X 2984 - 3090). CUT OUT CORRODED SECTION AND SPLICED IN NEW SECTION IAW A310-200 SRM 53-10-14.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 34,462 hrs · 29,226 cycles

MAIN DECK FLOOR, CARGO TIE DOWN ADAPTER (CROSS BEAM) CRACKED, AT FR 50 (STA Z2718 ) BL 36R ( -Y 480 TO -Y920 ). REMOVED AND REPLACED CROSSBEAM, REF: A310-200 SRM 51-40-21 PAR 5. LOCATED AND DRILLED CROSSBEAM REF: A310-200 SRM 51-40-44 PAR 2.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,462 hrs · 29,226 cycles

AFT CARGO PIT, STRINGER 52R CORRODED AT FR 62 ( STA X 3355 ). REPAIRED IAW A310 SRM 53-10-14

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 33,077 hrs · 28,379 cycles

AFTER T/O, GOT SPOILER NR 3 NR 2 FAULT WITH NR 3 ON LEFT WING SHOWING UP-EXTENDED. COULD NOT RESET. NR 1 NR 4 SPOILER DEFERRED. DURING HOLDING, NOTICED THAT NR 3 SPOILER NOW SHOWED DOWN. SUCCESSFULLY RE-SET NR 3 NR 2. REPLACED DEFECTIVE EFCU PER AMM 27-61-34-4. SYSTEM CHECKS OK.

Part: SKIN — CORRODED (RT WING) · airframe 32,011 hrs · 27,715 cycles

RIGHT WING FUEL CUTOUT FOR PANEL 650HB HAS ONE EXISTING PLUG BROKEN ON ONE SIDE. REMOVED DOME NUT IAW A310 SRM 51-40-21. REMOVED PLUG IAW A310 SRM 51-40-51. REAMED HOLE TO 0.4215 TO REMOVE CRACK IAW A310-SRM 51-40-44. NO DEFECTS NOTED IAW NTM 51-10-01. REPAIRED HOLE IAW EA 6-5710-88828 PT1 AND TD J1/S1/00726/2005. INSTALLED DOME NUT IAW A310 SRM 51-40-21, DOME SEALED IAW A310 SRM 51-76-20. THIS IS A MAJOR REPAIR PER FEDEX GMM 6-2-100.

Part: SKIN — CORRODED (RT WING) · airframe 32,011 hrs · 27,715 cycles

RIGHT WING OUTER FUEL CUTOUT FOR PANEL 650PB HAS TWO HOLES DOUBLE DRILLED. CHAMFERED 1 EACH HOLE IAW SRM A310 51-40-44. FOUND TO BE WITHIN LIMITS IAW A310 SRM 57-20-12 FIG 201. REPAIRED 1 EACH HOLE WITH BUSHING IAW EA 6-5710-88828 PT1 AND TD/J1/S1/00726/2005. INSTALLED DOME NUT IAW A310 SRM 51-40-21. DOME SEALED IAW A310 SRM 51-76-20. THIS IS A MAJOR REPAIR IAW FEDEX GMM 6-2-100.

Part: SLAT TRACK — DAMAGED (RT WING) · airframe 32,011 hrs · 27,715 cycles

RIGHT WING NR 3 SLAT, NR 10 TRACK, SLAT ATTACH POINT FITTING DAMAGED ON REMOVAL OF SLAT KNUCKLE. UPON REMOVAL OF RT NR 3 SLAT, NR 10 TRACK ATTACH POINT FITTING WAS DAMAGED AND LOWER SKIN OF NR 3 SLAT NR 10 TRACK. BLENDED GOUGES FOUND TO BE WITHIN LIMITS. ALODINED, PRIMED AND TOP COATED. CUTOUT OF DAMAGED SKIN, NO CRACKS FOUND. FABBED FILLER AND DOUBLER, REMOVED AND REINSTALLED 2 EA BUSHINGS, ALL IAW FEDEX EA 6-5750-89194. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR PER FEDEX GM 6-2-100.

Part: BUSHING — CORRODED (ENGINE MOUNT) · airframe 32,011 hrs · 27,715 cycles

NR 1 ENGINE FWD MOUNT FITTING BOLTS LOWER AND TOP SURFACE OF HOLE HAS LITE CORROSION. REMOVED AND REPLACED 4 EACH BUSHINGS ON NR 1 ENGINE MOUNT PER A310 SRM 54-51-81 PG 205 AND EA 6-5450-89149. REMOVED CORROSION ON UPPER AND LOWER SURFACE AND 4 EA BOLT HOLES PER SRM A310 54-51-81 PG 107/108, 109/110. APPLIED CAD PLATING TO BARE METAL PER PS 01-02-21. APPLIED TOPCOAT PER A310 SRM 54-51-81 PG 103. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR PER FEDEX GMM 6-2-100.

Part: PANEL — WORN (LT WING) · airframe 32,011 hrs · 27,715 cycles

OFF A/C PART LEFT WING PNL 512AT HAS WEAR MARKS ON BOTTOM SIDE OF PNL. COMPLIED WITH EA6-5740-89200.

Part: FLAP TRACK — GOUGED (RT WING) · airframe 32,011 hrs · 27,715 cycles

RIGHT WING NR 5 FLAP TRACK OUTBOARD ROLLER TRACK HAS GOUGES IN BEND RADIUS OF TRACK. COMPLIED WITH EA 6-5720-88814 PT 1 AND RAS/DABRE/7005151/2005.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,011 hrs · 27,715 cycles

UNDER FLOOR AREA BAY BEHIND FWD PIT FR 38.2 SHEAR TIE BETWEEN STG 49R AND 50R HAS CORROSION ON ALL OF SURFACE EXTENDING AROUND AND UNDER FASTENERS FOUND WHILE CLEANING FOR CIC APPLICATION. REMOVED CORROSION ON SHEAR TIE, AFTER BLENDING PART WENT OUT OF LIMITS IAW A310-200 SRM 53-10-00 AND CORROSION REMOVAL IAW A310-200 SRM 51-74-10. REPLACED WITH NEW SHEAR TIE IAW A310-200 SRM 51-72-10 AND 51-40-21. RESTORED PROTECTIVE COATING IAW A310-200 SRM 51-75-10 AND 51-23-10. INSTALLED SOLID RIVETS 5 EA IAW A310-200 SRM 51-40-21.

Part: PLATE — DAMAGED (LT WING) · airframe 32,011 hrs · 27,715 cycles

LEFT WING LANDING PLATE AREA BETWEEN STA WAIX-7.35 AND STA WAIX-14.7 JUST FWD OF AILERON HAS 2 EACH HOLE OVERSIZED AT 0.328, AND CARD E6-5710-7-5008 A PT 3 MOD REQUIRES TO REAM THESE HOLES TO 0.313 DIAMETER. COMPLIED WITH EA 6-5730-88784 PART 1 AND RAS/BAE/100692/2005 ISSUE A.

Part: BRACKET — CRACKED (ZONE 600) · airframe 32,011 hrs · 27,715 cycles

LANYARD BRACKET ON L/E PANEL 612BB IS CRACKED. REMOVED AND REPLACED ANGLE BRACKET IAW A310-200 SRM 51-40-23.

Part: BRACKET — CRACKED (FUSELAGE) · corrosion level 2 · airframe 32,011 hrs · 27,715 cycles

COCKPIT STA 904/FR 7, NUT PLATE BRACKET IS CRACKED 0.5 INCH. REMOVED BRACKET IAW A310-200 SRM 51-40-21. FABRICATED NEW BRACKET IAW EA 6-5610- 89174. INSTALLED NEW BRACKET IAW A310-200 SRM 51-72-10. REMOVED AND REINSTALLED STRIP PANEL IAW A310-200 SRM 51-40-10. REPAIR IS CLASSIFIED AS A MINOR REPAIR.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 32,011 hrs · 27,715 cycles

AFT CARGO FORWARD LWR SLANT PANEL HAS CORROSION AROUND NUT PLATES ON LANDING AT STA 3196, BETWEEN FRAMES 59-60, JUST FWD BY DOOR FRAME. REMOVED CORROSION IAW A310-200 SRM 51-74-10. ANGLE OUT OF LIMITS IAW A310-200 SRM 53-10-12. REPLACED ANGLE IAW A310-200 SRM 51-72-10. TREATED AND PRIMED BARE METAL IAW A310-200 SRM 51-74-10.

Part: STRAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 32,011 hrs · 27,715 cycles

AFT CARGO COMPT STRAP FOR PANEL 151EC HAS EXFOLIATION CORROSION ON STRAP. REPLACED STRAP IAW A310-200 SRM 51-72-10.

Part: SLAT TRACK — WORN (LT WING) · airframe 32,011 hrs · 27,715 cycles

LEFT SLAT TRACK NR 8 WEAR IS BEYOND ALLOWABLE LIMITS PER A310-200 SRM 57-40-00 TABLE 101 AND FIGURE 108 AND REQUIRES REPLACEMENT PER NOTE ON EA 6-5740-49974A. REMOVED AND REPLACED SLAT TRACK AND BUSHINGS IAW A310-200 AMM 27-80-14-4 AND COMPLIED WITH EA 6-5750-88829, OPS CHECK GOOD IAW A310-200 AMM 27-80-00-05.

Part: PLATE — DAMAGED (RT WING) · airframe 32,011 hrs · 27,715 cycles

RIGHT WING AILERON LANDING PLATE AREA BETWEEN STA WAIX-7.35 AND WAIX-14.7 JUST FWD OF AILERON HAS 2 EACH HOLES OVERSIZED AT 0.328 AND 0.371 DIAMETER, WORK CARD E6-5710- 7-5008A PT 4 REQUIRES THESE HOLES TO BE REAMED UP TO 0.313 DIAMETER. COMPLIED WITH EA 6-5730-88784, RAS/BAE/1000692/2005 ISSUE A.

Part: BRACKET — CRACKED (ZONE 100) · airframe 32,011 hrs · 27,715 cycles

APU BLEED AIR DUCT ATTACH BRACKET AT FR 58 ON FLOORBEAM IN AFT PIT LT SIDE HAS A CRACK IN THE RADIUS. REMOVED EXISTING BRACKET AND REPLACED WITH NEW BRACKET IAW A310-200 SRM 51-72-10.

Part: STRAP — CORRODED (ZONE 300) · corrosion level 2 · airframe 32,011 hrs · 27,715 cycles

THS PANEL 341BB HAS AREAS OF CORROSION AROUND ANCHOR NUTS ON PANEL ATTACH POINT. REMOVED CORROSION IAW A310-200 SRM 51-74-10. MATERIAL IS OUT OF LIMITS IAW A310-200 SRM 55-10-00. FABRICATED PART IAW A55178690 DWG INSTALLED PART IAW A310-200 SRM 51-40-21.

Part: FAIRING — CRACKED (ZONE 400) · airframe 32,011 hrs · 27,715 cycles

UPON INSPECTION OF REMOVED PARTS ON TC 44C0204 FOUND STATOR VANE SPACER IS CRACKED AT TIP (OFF AIRCRAFT PART). REPLACED STATOR VANE SPACER TO BE INSTALLED ON N00682 IAW A310-200 AMM 72-23-00.

Part: STRINGER — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 32,011 hrs · 27,715 cycles

UNDER FLOOR AREA BEHIND FWD PIT FR 38.2 TO FR 39 STR 54L HAS CORROSION ON STRINGER EXTENDING AROUND AND UNDER FASTENERS, FOUND WHILE CLEANING FOR CIC APPLICATION. REMOVED CORROSION IAW A310-200 SRM 51-74-10. UPON CORROSION REMOVAL 17 AREAS ON ANGLE REINFORCEMENT WENT OUT OF LIMITS IAW A310-200 SRM 53-10-00. REMOVED AND REPLACED ANGLE AND SPLICE REPAIR IAW SRM 51-72-10 AND 51-71-40. RESTORED PROTECTIVE COATING AND PART MARKING IAW A310-200 SRM 51-75-10, 51-23-10, AND GMM CHAPTER 9.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,011 hrs · 27,715 cycles

AFT CARGO PIT FORWARD AREA L-ANGLE IS CORRODED, AFT OF FR 54. REMOVED CORROSION IAW A310-200 SRM 51-74-10. MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 53-10-00. REMOVED, FABRICATED AND INSTALLED L-ANGLE RT IAW A310-200 SRM 51-40-10. ALSO FOUND CENTER L-ANGLE CORRODED OUT OF LIMITS. REMOVED, FABRICATED AND INSTALLED CENTER L-ANGLE IAW A310-200 SRM 51-40-21. SURFACE TREATED IAW A310-200 SRM 51-21-10.

Part: GUSSET — CORRODED (ZONE 400) · corrosion level 2 · airframe 32,011 hrs · 27,715 cycles

NR 2 PYLON OUTBOARD SIDE RIBS 15A, 16A, AND 17A UPPER AREA OF PYLON HAVE CORROSION AROUND, IN FASTENER HOLES AND EXTENDING UNDER NUT PLATES AS MARKED. REMOVED AND REPLACED GUSSETS IAW A310-200 SRM 51-40-21 AND 51-72-10.

Part: WATER TRAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 32,011 hrs · 27,715 cycles

BAY BEHIND FWD CARGO COMPARTMENT DRAIN FOR FLOOR HAS EXFOLIATION CORROSION EXTENDING AROUND AND UNDER FASTENERS. REMOVED AND REPLACED 1 EA WATER TRAP FOR FORWARD CARGO COMPARTMENT DRAIN IAW A310-200 SRM 51-40-21.

Part: FITTING — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 32,011 hrs · 27,715 cycles

VERTICAL LEADING EDGE PANEL 322CL HAS CORROSION ON LOWER SPLICE FITTING. REMOVED NUT PLATES IAW A310-200 SRM 51-40-21, REMOVED CORROSION IAW A310-200 SRM 51-74-10. CHECKED MATERIAL LOSS OUT OF LIMITS IAW A310-200 SRM 55-30-00. REMOVED AND REPLACED SPLICE FITTING IAW A310-200 SRM 51-40-21.

Part: INDICATOR — INOPERATIVE (ENGINE N1) · airframe 30,232 hrs · 26,545 cycles

ON TAKEOFF ROLL AS TOGA WAS SELECTED ON AUTO THROTTLE SYSTEM (FOR FLEX POWER) NR 2 N1 ANALOG POINTER HUNG AT 40 PERCENT, ALSO NR 2 ENGINE SLOW TO ACCELERATE WITHIN 3-5 SECONDS. REJECTED TAKEOFF AT 95 KNOTS. FACT 11APR03 06:34 LAX, REMOVED AND REPLACED NR 2 N1 INDICATOR PER M/M 77-11-12-4, CHECKS OK ACCELERATION OK PER JRH 6-17 R/I 11APR03 06:35 LAX, SCHEDULED REMOVAL/INSTALLATION OFF MFG 63601-450-2 POS 2RH SRL 156 TAG 811648 ON MFG 63601-450-2 SRL 119, TAG 512880.

Part: SPAR — CORRODED (HORIZ STAB) · airframe 29,720 hrs · 26,232 cycles

BOTH L&R HORIZ STAB UPR & LWR CHORDS OF SPAR CORRODED ENTIRE LENGTH. R&R CHORD PER SRM 55-11-21.

Part: WARNING SYSTEM — FALSE INDICATION (COCKPIT) · airframe 28,832 hrs · 25,707 cycles

ON CLIMB APU GENERATOR FAULTED. PERFORMED BIT CHECK, NO FAULT FOUND. OK FOR SERVICE.

Part: DAMPENER — FAILED (RT MLG) · airframe 28,159 hrs · 25,258 cycles

AFT T/O GEAR WOULD NOT RETRACT USING EITHER POSITION 1 OR 2, SEL GEAR HANDLE WOULD NOT RETRACT BEYOND NEUTRAL. FOUND SERVICE IND ON RT GEAR POPPED. REMOVED AND REPLACED RT MLG PITCH DAMPNER PER IAW FX A310 MM 32-11-15-4-01 AND SERVICED IAW FX A310 MM 12-12-32-0. LUBED ALL PIVOT POINTS ON LWR PART OF GEAR.

Part: HANDLE — FAILED (MLG SELECTOR) · airframe 27,643 hrs · 24,885 cycles

ON DEPARTURE, LANDING GEAR HANDLE WOULD NOT RAISE ABOVE NEUTRAL POS DET SYS 1 & 2, BOTH TRIED NO HELP.

Part: SWITCH — INOP (NLG)

NR 2 REG FAULT LIGHT ILLUM DURING CLIMB ON PRESS PG. THE V/S WAS THE SAME AS A/C RATE OF CLIMB. A/C DIDN'T PRESS. RETURN TO LAS. REMOVED AND REPLACED PROS ELECT UNIT PER 32-31-71. CHECKED WIRING FROM PROX BOX TO COCKPIT AND FROM PROX BOX TO GROUND, DUE TO RESIST TO GROUND READINGS. REMOVED AND REPLACED NOSE GEAR SHOCK ABS PRO SWITCH 82GB AND 55GB. ALL SYS OPS CHECK NORM ON GROUND PER AMM 32-61-00. MAINT CHECK FLT OF SYS ALSO SUCCESSFUL.

Part: PROX COMPUTER — INOPERATIVE (E & E COMPT)

98-247 AFT T/O KRIC, NR 1 ATS SWITCH DROP OFF & WOULD NOT RESET. PROBE HEAT LIGHT FAILED. NR 2 PRESS SYS INOP. NR 2 PRESS DRS WON'T CLOSE. NO CHG DUR FINAL APPROACH INTO RIC. PERFORM BITE CK ON GRND PROX BOX COMPUTER. NO FAULT CODE PRESENT, RESET. ALL SYS RESET. CK NORM. OK FOR SERV.

Part: DOOR — NOT CLOSED (CABIN)

98-0171 - STA-MEM: ECAM DOOR NOT CLOSED IN FLT UPON VISUAL CK. NOTED AIR NOISE WARNING HORN, RED BAR. INSPECTED RT ENTRY DOOR. NO VISUAL DISP NOTED ON LOCKING MECHANISMS AND ASSOCIATED INDICATORS REMOVED DOOR LINING AND LUBED SPRINGS, ROLLER AND RODS. PERFORMED PULL TEST IAW M/M 52-10-11. ALL OK. REINSTALLED LINING.

Part: ADC — FAILED (NR 1)

AFTER GEAR RETRACTION CAPTAIN RED SPEED TAPE APPEARED RENDERING SPEED INFO INOP. SWITCHED ADC INSTRUMENT TO SYS, TWO SPEED INFO RECOVERED. NR 1 AND 2 AUTO THROTTLE TRIPPED, NR 2 ONLY RESET, BOTH LOWER ACCESS DOOR SHOW AMBER WITH CHIME. CABIN RATE OF CLIMB ABOUT THE SAME AS A/C RATE OF CLIMB, ECAM DOOR PAGE SHOWS GREEN PRIOR TO BLOCKOUT ELECTED TO RETURN TO IAH. REMOVED AND REPLACED NR 1 ADC AND C/W PITOT STASTIC CHECKS NORMAL, RED SPEED LIMIT LIGHT OK. FOUND ACCESS DOOR HANDLE TRIPPED, RESET OK.

Part: MUFFLER — CRACKED (APU)

APU EXHAUST ACOUSTIC INTERNAL LINER IS CRACKING AND DETERIORATED THROUGHOUT DUCT, PIECES AS LARGE AS 4 INCH BY 10 INCH ARE MISSING. REMOVED AND REPLACED APU EXHAUST MUFFLER AS PER AMM 49-81-15.

Part: FITTING — CRACKED (CARGO DOOR)

LOWER AFT CARGO DOOR ACTUATOR FITTING IS CRACKED AT AFT DRAIN HOLE JUST FWD OF FRAME 62, CRACK IS .102 INCH LONG GOING FWD AND O/B, REF EO 6-5310-7-3301. REPAIRED PER EO 6-5310-7-3301 PART 2, INSTALLED CEILING PANEL.