N405FE

Part: RELAY — MALFUNCTIONED (MLG) · airframe 37,649 hrs · 31,569 cycles

AT APPROX 400' AGL WHILE FLYING RNAV/GPS APP RWY 29. RECEIVED "TO LOW GEAR" CALL OUT. EXECUTED GO AROUND. SELECTED SYS NR 2 ON GEAR AND LANDED WITHOUT OTHER WARNINGS. PER TSM INSPECTED NLG MSW 79GB, NO DEFECTS NOTED. CLEANED AND RESEATED C/P ON SWITCH. REMOVED AND REPLACED RELAY 99GB PER TSM & PERFORMED OPS CHECK OF EGPWS SYS PER M/M 34-48 01-05; SYS OPS CHECK NORMAL WITH NO FAULTS NOTED.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 37,396 hrs · 31,374 cycles

FWD CARGO COMPARTMENT BETWEEN FR 38.2 AND FR 39 AND BETWEEN STRINGER 46L AND STRINGER 45L HAS A 2 SQ INCH OF CORROSION. REMOVED ALL EVIDENCE OF CORROSION IN FWD CARGO COMPT BETWEEN FR 38.2 AND FR 39 AND BETWEEN STR 45L AND STR 46L IAW SRM 51-74-10. REPAIRED FR 39 LOWER "T" SECTION FLANGE BETWEEN STR 45L AND STR 46L IAW SRM 53-15-17 PARA C PAGES 217 THRU 223, FIG 203.

Part: FRAME — CHAFED (ZONE 200) · airframe 37,396 hrs · 31,374 cycles

MAIN CARGO COMPT FRAME 36 AT LT LONGERON NR 10 HAS CHAFED AREA .015 IN DEP CUT OUT DAMAGE SECTION AT FRAME 36, LONGERON 10 LT IN MAIN UPPER DECK COMPT, FABRICATED REPAIR PARTS AND INSTALLED FRAME REPAIR-INNER FLANGE IAW SRM 53-10-13, FIG 202, PAGE 209.

Part: FITTING — CORRODED (R1 DOOR) · airframe 37,396 hrs · 31,374 cycles

R 1 DOOR EXTERIOR SIDE HAS CORROSION ON INSIDE HANDLE AREA BOX, 3 IN X 3 IN REMOVED LEVEL 1 CORROSION. REMOVED CORRODED FITTING ON R 1 DOOR HANDLE EXTERIOR BOX, FABRICATED REPLACEMENT PART IAW DRW A52111407201 AND INSTALLED PART IAW SRM 51-72-10.

Part: SKIN — DENTED (CARGO DOOR) · airframe 37,396 hrs · 31,374 cycles

BULK CARGO DOOR EXT SKIN AT LOWER FWD END HAS DENT 2.5 IN LONG X .20 IN WIDE X .004 IN DEEP CUT OUT DAMAGED SECTION OF EXT SKIN, FABRICATED REPAIR PARTS AND INSTALLED CORNER MEMBER TO SKIN REPAIR ON BULK CARGO DOOR FWD LOWER CORNER IAW SRM 52-30-00, FIG 207, PAGE 231/232.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 37,396 hrs · 31,374 cycles

MAIN CARGO COMPARTMENT SEAT TRACK NR3 RT BETWEEN FRAMES 45 AND 54 HAS 4 EA CRACKS ON UPPER SURFACE AREA, MAX LENGTH .50 IN. REMOVED DAMAGED TRACK AND REPLACED WITH NEW SEAT TRACK NR3 RT IN MAIN DECK BETWEEN FR 45 AND FR 54 IAW A310 SRM 51-72-10 PG 2.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,396 hrs · 31,374 cycles

MAIN DECK CARGO COMPT SEAT TRACK NR 5 RT BETWEEN FR 15 AND FR 19 HAS CORROSION, APPROX 56 SQ IN, REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED SECTION OF TRACK AND REPLACED WITH NEW TRACK AT TRACK NR5 RT BETWEEN FR 15 AND FR 19 IAW SRM 51-72-10, PAGE 2.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 37,396 hrs · 31,374 cycles

AFT CARGO PIT MDC FLOORBEAM FR 54.3 BETWEEN SEAT TRACK 2R-3R, CRACK LENGTH IS 0.125 IN ROUTED OUT CRACK FABRICATED, TREATED AND PRIMED AND INSTALLED REPAIR CHANNEL AT AFT CARGO PIT MDC FLOORBEAM FR 54.3 BETWEEN SEAT TRACK 2R-3R IAW SRM 53-10-15, PG 257-258, FIG 204.

Part: PLATE — CORRODED (ZONE 800) · corrosion level 2 · airframe 37,396 hrs · 31,374 cycles

LT OVERWING EMERGENCY EXIT DOOR, EXTERIOR HANDLE BOX AREA, ON AFT SIDE HAS 2 SQUARE INCHES OF CORROSION. REMOVED CORROSION FROM SEAL PLATE IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW SRM 52-20-00 FIG.101 (100 PERCENT MATERIAL LOSS). REMOVED INNER SKIN SEGMENT FOR FOM IAW SRM 51-40-21. R & R SEAL PLATE IAW SRM 51-40-21 & SRM 53-23-00 FIG 101. REINSTALLED INNER SKIN SEGMENT IAW SRM 51-40-21. REPROTECTED AREA IAW SRM 51-75-10.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,396 hrs · 31,374 cycles

MAIN DECK FLOOR NR 1 SEAT TRACK HAS 12 " LONG HEAVY CORROSION BETWEEN FR15A AND 16A. REMOVED CORROSION IAW SRM 51-74-10, TRACKS FOUND OUT OF LIMITS IAW SRM 53-10-10, FIG. 101. REPLACED TRACKS IAW SRM 51-72-10, SRM 51-40-44 PARA. 3A & SRM 53-12-16, FIG 1.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,396 hrs · 31,374 cycles

MAIN DECK CARGO SEAT TRACK CORROSION ON Y1959 BETWEEN FR 15B AND FR 15, REFER TO NON- ROUTINE N01238 DATED 03/28/10. AFTER CORROSION REMOVAL, THE SEAT TRACK PN Y1959 BETWEEN FR 15 AND FR 15B WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-16-10. REMOVED SEAT TRACK FROM FR 15A TO FR18 IAW SRM 51-40-21. FABRICATED NEW SEAT TRACK IAW DWG 12A53611650, LOCATED AND DRILLED NEW HOLES IAW SRM 51-40-44, ALODINED, PRIMED AND TOPCOATED IAW SRM 51-75-10. INSTALLED SEAT TRACK NR Y1959 BETWEEN FR.15A AND FR.18 IAW SRM 51-40-44. TOPCOATED FASTNERS IAW SRM 51-75-10. THIS WAS A MAJOR REPAIR IAW GMM 6-2-100. ALL WORK WAS ACCOMPLISHED ON NON-ROUTINE N01238.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,396 hrs · 31,374 cycles

MAIN DECK CARGO COMPT FLOOR SUPPORT BEAM HAS CORROSION APPROX 1.5 X 1.0 INCH BETWEEN FLOORBEAM 17L & 16L NEAR L1 DOOR. R & R FLOOR SUPPORT FRAME IAW SRM 51-72-10 , AND FABBED NEW T-CAP FROM 7075T6511-NSA348070 IAW DWG 12-A53611789. INSTALLED NEW TRACK IAW SRM 51-72-10, PARA 6A.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,396 hrs · 31,374 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK 5L BETWEEN FR 78 AND FR 79 HAS A 1 SQ INCH AREA OF CORROSION. REMOVED CORROSION FROM SEAT TRACK 5L BETWEEN FR 78 & FR 79 , CHECKED FOUND OUT OF LIMIT. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 207.

Part: GEARBOX — LEAKING (SLATS) · airframe 36,967 hrs · 31,074 cycles

SLAT SYS 1 & 2 FAULT DURING ACFT CONFIGURATION REMOVED AND REPLACED LEFT WING SLAT NR 2 LINE GEARBOX PER AMM 27-84-16. REMOVED AND REPLACED RT WING SLAT IN LINE GEARBOX PER AMM 27-84-16. REMOVED AND REPLA CED RIGHT WING PPU PER AMM 27-81-14. OPEN

Part: COMPUTER — FAILED (NR 2) · airframe 36,964 hrs · 31,070 cycles

FLAPS SYS 1 AND SYS 2 LIGHT CAME ON WHEN SELECTING FLAPS 20 ON APPROACH. FLAPS STUCK HALFWAY BETWEEN 15 AND 20. EXECUTED MISSED APPROACH, CYCLED FLAPS SUCCESSFULLY AND EXECUTED NORMAL SLAT/FLAPS 30/40 APPROACH. REMOVED AND REPLACED NR1 AND NR2 SFCC IN REF TO AMM 27-51-18-4. CHECK FLAP DRIVE SHAFTS FOR FREEDOM OF MOVEMENT WITH NO DISCREPENCIES NOTED. PERFORMED OPS CHECK OF FLAPS RUNNING THEM FROM 0-20 THRU 15 AND ON TO 40 SEVERAL TIMES WITH ENGINES RUNNING AND NO FAULTS NOTED. OPS CHECK IN REF TO AMM 27-54-00-5. PERFORMED BITE CHECK OF NR1 AND NR2 SFCC IN REF TO AMM, ALL TEST PASSED. ACFT OK FOR SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

FWD PIT LT SIDE PANEL SUPPORT HAS CORROSION ON LOWER SURFACE AT FR 36 LBL 50 REMOVED NUTPLATES AND CORROSION IAW FEDEX A310 SRM 51-40-21 AND 51-74-10. FOUND TO BE OUT OF LIMITS IAW FEDEX A310 SRM 53-10-00. REMOVED AND REINSTALLED LT SLANT PANELS CARGO GUIDE RAILS, TRANSITION PANELS, MOUNTS AND ROLLER TRAYS FROM FR 23-38.2 IAW FEDEX A310 AMM 25-54-10-2. FABRICATED T-CAP AND SPLICE ANGLE IAW FEDEX A310 SRM 53-10-15 ALODINED IAW FEDEX A310 SRM 51-21-10. PRIMED AND PAINTED IAW A310 SRM 51-23-10. INSTALLED T-CAP AND SPLICE ANGLE IAW FEDEX A310 SRM 53-10-15 AND 51-40-21. PDU OPS GOOD IAW FEDEX A310 AMM 25-52-26-4, MINOR REPAIR.

Part: STRINGER — CORRODED (AFT PIT) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

AFT PIT STRINGER 55L REQUIRES REPLACEMENT FROM FR 58 TO 63. STRINGER HAS HEAVY CORROSION REMOVED SHEAR TIES AT STATION 59, 60, 61. CUT OUT STRINGER 55L FROM FRAME 58 TO 63 IAW A310 SRM FIG 20. FABBED STRINGER AND COUPLINGS IAW A310 SRM 53-10-14 FIG 201. ALODINED PRIMED AND PAINTED REPAIR PARTS IAW A310 SRM 51-21-10 PARA 2, 51-23-10 PARA 3. PART MARKED AND INSTALLED REPAIR PARTS IAW A310 SRM 51-40-21 PARA 6 AND 7. REINSTALLED SHEAR TIES AT STRINGER 55L IAW A31 SRM 51-40-21 PARA 6 AND 7.

Part: SILL — FAILED (FWD PIT) · airframe 35,345 hrs · 29,942 cycles

FWD LOWER CARGO PIT ANGLE REPAIR AT FR 24 STRINGER 43R AT DOOR SILL JAMB. EVALUATED AND FOUND TO NOT MEET APPROVED FAA REQUIREMENTS. REMOVED AND REPLACED REPAIR ANGLE AT FR 24 STRINGER 43R IAW FEDEX EA NR 6-5310-112957 FUSELAGE FWD CARGO DOOR LOWER SILL INCOMING REPAIR.

Part: FRAME — CRACKED (ZONE 100) · airframe 35,345 hrs · 29,942 cycles

FRAME 38 CRACKED WHERE FRAME LEG ATTACHES TO FUSELAGE SKIN, BETWEEN STR 41L AND STR 42L. TRIMMED CRACKED FLANGE, FABRICATED AND INSTALLED REPAIR FALSE FLANGE IAW EA 6-5310-109195, FUSELAGE FRAME, FRAME 38 BETWEEN STRINGER 41 AND 42 CRACKED FLANGE, REPAIR.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

AFT PIT STRINGER 55L BETWEEN FRAMES 54.2 AND 54.3 CORRODED LEFT SIDE COMPLIED WITH EA 6-5310-112955 FUSELAGE AFT PIT STRINGERS P52L, P54L, P55L REPAIR.

Part: STRUCTURE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

AFT PIT BETWEEN FRAMES 66 AND 65 T CAP NUT PLATE JUST FWD OF FRAME 66 ABOVE STRINGER 45R CORRODED UNDERNEATH. REMOVED T-CAP IAW A310 SRM 51-40-21, RECEIVED NEW PROFILE P/N A5397426020451 PO J80248.1. INSTALLED NEW PROFILE IAW A310 SRM 51-40-21 PARA 7 AND PARA 13.

Part: SKIN — DENTED · airframe 35,345 hrs · 29,942 cycles

SKIN DIMPLED FRAME 38, LT SIDE STR 35L AROUND 3 FASTENERS. ACCOMPLISHED HFEC INSPECTION ON 3 EACH DENTS IAW A310 NTM 51-10-03 WITH NO DEFECTS NOTED. DRESSED OUT TWO DENTS AT STR 39 AND STR 40 IAW A310 SRM 51-73-10. BOTH DENTS FOUND TO BE WITHIN LIMITS IAW A310 SRM 53-10-12 FIG 110 AND DIAGRAM 109. 3RD DENT AT STR 41 FOUND TO BE OUT OF LIMITS IAW A310 SRM 53-10-12 FIG 110 AND DIAGRAM 109. CUT OUT DAMAGE AND TRIMMED 3RD DENT AND INSTALLED SKIN DOUBLER IAW FED EX A310 SRM 53-10-12.

Part: FLOORBEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

AFT PIT FRAME 58 T CAP LEFT SIDE ABOVE STRINGER 50L NUT PLATE CORRODED REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED CROSS BEAM AND SPLICE, FABBED CROSSBEAM T-CAP AND SPLICE ANGLES. TREATED REPAIR PARTS AND INSTALLED, IAW A31-200 SRM 51-74-10, 53-10-15 FIG 207, 51-21-10, 51-23-10 PARA 3, 51-40-21 PARA 5 AND 6.

Part: FITTING — CRACKED (ZONE 100) · airframe 35,345 hrs · 29,942 cycles

FWD PIT, FRAME FITTING CRACKED, FR 36, (STA. X1976) BL 60L (Y1520). 09-04-07 REMOVED AND REPLACED FRAME FITTING IAW A310-200 SRM51-40-21, PART 6 & 7.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

AFT CARGO PIT, STR 54L CORRODED BETWEEN FR 58 AND FR61 (STA X3143 AND STA X3302) CUT OUT CORRODED SECTION OF STR 54L FROM STA X3143 TO STA X3302. FABRICATED AND SPLICED IN REPAIR SECTION IAW A310-200 SRM 53-10-14 FIG 201, 51-21-10 AND 51-23-10.

Part: FITTING — CRACKED (ZONE 100) · airframe 35,345 hrs · 29,942 cycles

FWD PIT, FRAME FITTING CRACKED, FR38 (X2082), BL 60L (Y1520), AT PIT FLOOR LEVEL.. REMOVED CRACKED FITTING IAW FEDEX A31 SRM 51-40-21 LOCATED DRILLED NEW FITTING PO 583026.6 IAW FEDEX SRM 51-40-44 PARA2. INSTALLED NEW FRAME FITTING IAW FEDEX SRM 51- 40-27 PARA 7.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

AFT CARGO PIT, STR 45R CORRODED, FR 54.2 TO FR 54.3 (X3037 TO X3090) CUT OUT CORRODED SECTION OF STRINGER 45R, FROM STA X2984 TO X 3090, FABRICATED AND SPLICED IN REPAIR SECTION, IAW A310-200 SRM 53-10-14 FIG 201, 51-71-30 FIG 202, 51-40-21 PAR 6, 51-21-10 AND 51-23-10.

Part: SKIN — MISREPAIRED · airframe 35,345 hrs · 29,942 cycles

EXTERNAL REPAIR DOUBLER LT FUSELAGE FR26/32 STR39L-40L REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA VISUALLY INSPECTED REPAIR DOUBLER LT FUSELAGE FR26/32 STR39L-40L. FOUND NOT TO BE WITHIN ANY FAA APPROVED DATA. REMOVED AND REPLACED REPAIR DOUBLER ON FEDEX EA 6-5330-109186, SKIN PANEL DAMAGE FORWARD OF FR 26/32 STRG 39L-40L REPAIR.

Part: SKIN — CRACKED (ZONE 500) · airframe 35,345 hrs · 29,942 cycles

LEFT WING BOTTOM SKIN PANEL NR 2, SKIN CRACKED I/B OF RIB 11, AFT OF REAR SPAR, WRI 57-10 9572, W/C T 6-5710-91017. STOP DRILLED CRACK, AND PERFORMED HFEC INSPECTION IAW A310 NTM 51-10-08 PT6, TO CONFIRM NO CRACK PAST STOP DRILLED AREA. INSTALLED SKIN DOUBLER IAW BA AIRBUS DWG R57249152, REF: E.A. 6-5710-91017, WINGS LT WING BOTTOM SKIN PANEL NR 2 SKIN, CRACK INBD OF RIB 11, AFT OF REAR SPAR.

Part: STRINGER — CORRODED (AFT PIT) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

AFT LOWER CARGO PIT, CORROSION ON STRINGER 53L BETWEEN FR 64 AND 65. REMOVED, FABRICATED REPAIR SECTION OF STRINGER AND COUPLING AND INSTALLED PER A310-200 SRM 51-40-11, 53-17-14, 51-40-44, 51-40-21DAN 50-04, DAN320B14.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

AFT LOWER CARGO PIT STRINGER 52R HAS CORRODED ANGLE WITH MISSING FASTENERS BETWEEN FR 58 AND 59. [08-29-07] REMOVED STRINGER SECTION AND ANGLE IAW A310-200 51-40-21 PARA 6. FABRICATED NEW STRINGER 52R SECTION AND COUPLING IAW SRM 51-10-14 FIG 201. ALODINED IAW A310 SRM 51-21-10. PRIMED AND PAINTED IAW A310 SRM 51-23-10. INSTALLED STRINGER AND COUPLING IAW A310 SRM 53-10-14 FIG 201. ANGLE IS NOT EFFECTIVE TO THIS A/C PER AIRBUS DRAWING A53974202 WAS NOT RE-INSTALLED

Part: STRINGER — CORRODED (ZONE 100) · airframe 35,345 hrs · 29,942 cycles

ALC STR 52L CORRODED BETWEEN FR 64 AND 65. REMOVED CORROSION IAW A310 SRM 51-40-11. FOUNDED OUT OF LIMITS IAW A310 SRM 53-17-14. NEW MATERIAL ID FOR STRINGER IS DANS 0B09P0081641.218 COUPLING THAT IS DAN 200IT 79511 MAT EXTRUSION PO NR 580294.2. FABRICATED IAW A310 SRM 51-40-44. INSTALLED STRINGER AND ASSOCIATED PARTS IAW A310 SRM 53-1014.

Part: FRAME — CORRODED (ZONE 100) · airframe 35,345 hrs · 29,942 cycles

AFT PIT T CAP FRAME 60, CENTER, ABOVE S57 CORRODED. REMOVED CORROSION PER A310-200 SRM 51-74-10. FOUND TO BE OUT OF LIMITS PER A310-200 SRM 53-10-00 PG 123. REMOVED DAMAGED CROSSBEAM, FABBED NEW CROSSBEAM SECTION. INSTALLED NEW CROSSBEAM SECTION PER A310-200 SRM 53-10-15.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

FWD PIT CORRODED ON FLOORBEAM LATERAL ANGLE AT FR 38 UNDER ROLLER TRAY, RBL 28R TO 34R REMOVED CORRODED PART, FABBED REPAIR PARTS AND INSTALLED REPAIR ANGLE PER A310-200 SRM 51-74-10 PARA 6B, 53-14-15 FIG 41, 51-31-20 FIG 17, 53-10-15.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

AFT PIT BETWEEN FRAME 66 AND 65 STRINGER 46L CORRODED REMOVED CORRRODED STRINGER. FABBED REPAIR PARTS. INSTALLED REPAIR PARTS PER A310-200 51-40-21, 53-10-14 PG 203, 51-21-10, 51-23-10.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

AFT PIT FRAME 63 STRINGER 48R CORRODED REMOVED CORRODED AREA FABBED REPAIR PARTS (STRINGER AND COUPLING) INSTALLED REPAIR PER A310-200 SRM 53-10-14, 51-21-10, 51-23-10, AND DRAWING A53974202.

Part: STRINGER — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

ALC STR 48R CORRODED BETWEEN FR 58 AND FR 60 REMOVED CORRODED AREA PER A310-200 SRM 51-40-21. FABBED REPAIR (STRINGER AND COUPLING) PER A310-200 SRM 53-10-14 PG 203, 51-21-10,51-23-10. INSTALLED REPAIR PARTS PER A310-200 SRM 53-10-14.

Part: STRINGER — CORRODED (AFT PIT) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

ALC STR 49L CORRODED BETWEEN FR 58 AND FR 60 REPLACED STRINGER 49L BETWEEN FRAME 58 AND 60 IN AFT PIT IAW A310-200 SRM 53-10-14, FIG 201 PG 203/204.

Part: FITTING — CRACKED (FUSELAGE) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

FRAME FITTING C38.2 CRACKED AND CORRODED AT LBL 60 IN FWD PIT UNDER T-CAP REMOVED AND REPLACED FITTING IAW A310-200 SRM 51-40-21 PARA 6 PO NR 583026.5.

Part: FITTING — CRACKED (FUSELAGE) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

FRAME FITTING C38.1 IS CRACKED AND CORRODED AT LBL 60 IN FWD PIT UNDER T-CAP REMOVED AND REPLACED FITTING IAW A310-200 SRM 51-40-21 PARA 5-7 PO NR 583026.8.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

AFT PIT, STR 55R CORRODED FROM FR 61 TO FR 63 (STA X 3302 - X 3408). THIS SDR ALSO INCORPORATES DISCREPANCY AND REPAIR DONE ON NON ROUTINE NR N000443, W/O 00037436, (STR 55R CORRODED FROM FR61 - 62). REMOVED AND REPLACED CORRODED SECTION OF STR 55R FROM FR 61 TO FR 63 (STA X 3302 - X 3408) IAW A310-200 SRM 53-17-14 AND 51-10-14.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

ALC, FR 64, T-CAP CORRODED, BL 36R. (-Y910) REMOVED AND REPLACED T-CAP SECTION IAW A310-200 SRM 51-21-10 AND 53-10-15.

Part: FRAME — DENTED (ZONE 100) · airframe 35,345 hrs · 29,942 cycles

AFT PIT FRAME 67 BETWEEN STRINGER 49R AND 50R DENTED FORMED FRAME TO ORIGINAL CONTOUR REF: A310-200 SRM 51-73-10. PERFORMED HFEC, INSPECTION OF AREA IAW A310-200 NTM 51-10-08, NO CRACKS NOTED.

Part: FRAME — CRACKED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

FRAME FITTING C35 IS CRACKED AT LBL 60 IN FWD PIT UNDER T-CAP REMOVED FITTING, FWD LOWER LT AT FR 35 REF A310 SRM 51-40-21 PARA 6. LOCATED AND DRILLED NEW FITTING REF A310 SRM 51-40-44 PARA 2. INSTALLED NEW FITTING REF A310 SRM 51-40-21 PARA 7.

Part: FITTING — CRACKED (ZONE 100) · airframe 35,345 hrs · 29,942 cycles

FRAME FITTING C38.1 CRACKED AT RBL 60, FWD PIT FLOOR. REMOVED AND REPLACED FRAME FITTING IAW A310-200 SRM 51-40-24 PAR 7.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

AFT PIT FRAME 66 T CAP ABOVE STRINGER 46L CORRODED REMOVED AND REPLACED T-CAP PER A310-200 SRM 53-17-15 FIG 11 SHEET2 , 51-72-10, ALODINED AND PRIMED PER A310-200 51-21-10, 51-23-10.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,345 hrs · 29,942 cycles

FRAME FITTING C35 IS CRACKED AT RBL 60 FWD PIT FLOOR LEVEL. REMOVED AND REPLACED FRAME FITTING PER A310-200 SRM 51-40-21 PARAGRAPH 6.

Part: VANE — CHAFED (TE FLAPS) · airframe 35,345 hrs · 29,942 cycles

RT WING I/B FLAP VANE BULL NOSE CENTER DOUBLER CHAFED. 08-30-07 REMOVED DAMAGED DOUBLER, INSPECTED AREA , FABRICATED REPLACEMENT DOUBLER AND INSTALLED PER EA 6-5750-112956. FLAP VANE P/N A57970651201

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

T-CAP CORRODED FR35 AT RBL 56 TO 62 FWD PIT REMOVED AND REPLACED T-CAP PER A310-200 SRM 51-40-21 PARAGRAGH 7 AND 53-10-15, PAGE 241 AND 242.

Part: SEAT TRACK — CRACKED (CABIN) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

ARTICULATING SEAT TRACK AT Y1456 BETWEEN FR 38.2 AND FR 40 IS CRACKED ON UPPER FLANGE FWD EDGE REMOVED AND REPLACED ARTICULATING SEAT TRACK PER A310-200 SRM 51-40-44, 51-40-21, ALODINED AND PRIMED PER A310-200 SRM 51-21-10.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

T-CAP CORRODED FR35 AT RBL 56 TO 62 FWD PIT REMOVED AND REPLACED T-CAP PER A310-200 SRM 51-40-21 PARAGRAGH 7 AND 53-10-15, PAGE 241 AND 242.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,345 hrs · 29,942 cycles

FRAME FITTING C37 IS CRACKED AT RBL 60 FWD PIT FLOOR LEVEL REMOVED AND REPLACED FITTING PER A310-200 SRM 51-40-21 PARAGRAGH 5 AND 6.

Part: PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

PNL 438BL HAS SURFACE CORROSION AND BARE METAL EXPOSED REMOVED CORROSION FOUND OUT OF LIMITS IAW A310-200 SRM 54-55-51. FABRICATED NEW PANEL IAW A310-200 SRM AND GMM 7-1-1001. ALODINED AND PRIMED PER 51-23-10 AND 51-21- 10.

Part: PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

PNL 486BR HAS FRETTING CORRSION AND BARE METAL EXPOSED REMOVED CORRSION FOUND TO OUT OF LIMITS IAW A310-200 SRM 54-55-51. FABRICATED NEW PANEL IAW A310-200 SRM AND GMM. ALODINED AND PRIMED IAW A310-200 SRM 51-21-10 AND 51-23-10.

Part: PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

PNL 486BR HAS FRETTING CORROSION AND BARE METAL EXPOSED REMOVED CORROSION FOUND TO OUT OF LIMITS IAW A310-200 SRM 54-55-51. FABRICATED NEW PANEL IAW A310-200 SRM AND GMM. ALODINED AND PRIMED IAW A310-200 SRM 51-21-10 AND 51-23-10.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

FOUND ALC STR 51L CORRODED BETWEEN FR 58 AND FR 61. [08-20-07] REMOVED AND REPLACED STRINGER 51L BETWEEN FRAMES 58 AND 65 IAW SRM 51-40-21 PG1 AND 53-10-14.

Part: FRAME — CRACKED (ZONE 100) · airframe 35,345 hrs · 29,942 cycles

FRAME FITTING C36 (STA 1976) IS CRACKED AT RBL 60 (-Y 15200) FWD PIT FLOOR LEVEL. [08-09-07] REMOVED AND REPLACED FRAME FITTING IAW A310-200 SRM 51-40-21 PAR 6.

Part: STRINGER — CORRODED (ZONE 100) · airframe 35,345 hrs · 29,942 cycles

AFT PIT STR 54R CORRODED BETWEEN BS 3143-3302, REMOVED AND REPLACED STRINGER PER A310-200 SRM 53-10-14 PG 203 AND 204. ALODINED AND PRIMED AND TOP COATED PER A310-200 SRM 51-23-10 AND 51-21-10.

Part: STRINGER — CORRODED (ZONE 100) · airframe 35,345 hrs · 29,942 cycles

AFT PIT, STR 53R CORRODED BETWEEN BS 3146-3302, REMOVED AND REPLACED STRINGER PER A310-200 SRM 53-10-14 AND 53-12-14. ALODINED AND PRIMED PER A310-200 SRM 51-23-10 AND 51-21-10.

Part: STRINGER — CORRODED (ZONE 100) · airframe 35,345 hrs · 29,942 cycles

AFT PIT, STR 46R CORRODED AT BS 3037. REMOVED AND REPLACED CORRODED SECTION OF S46R FR 54.2 TO 54.3 IAW FEDEX A310-200 SRM 53-10-14 PG 203/204. TREATED AND PRIMED AND TOP COATED PER A310-200 SRM 51-21-10, 51-23-10

Part: FRAME — CRACKED (ZONE 100) · airframe 35,345 hrs · 29,942 cycles

FRAME FITTING C38 (STA 2082) IS CRACKED AT RBL 69 (-Y1520) FWD PIT, FLOOR LEVEL. [08-06-07] REMOVED AND REPLACED FRAME FITTING AT C38 IAW A310-200 SRM 51-40-20.

Part: FRAME — CRACKED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

FRAME FITTING C33 IS CRACKED AT RBL 60 FWD PIT FLOOR LEVEL. 08-30-07 REMOVED SLANTE PANEL 132JW, XY GUIDE, RAILS, TRANSITION PANEL TO FOM. REMOVED FITTING, RECEIVED NEW FITTING A5377364420100 PO 582198.2. LOCATED AND DRILLED FITTING IAW A310 SRM 51-40-40, INSTALLED FITTING IAW A310 SRM 51-40-21 PARA 7, INSTALLED TRANSITION PANEL IAW A310 SRM 51-40-21 PARA 7. INSTALLED LATCH XY GUIDE AND RAILS IAW A310 AMM 25-52-44-4 AND 25-52-48-4. INSTALLED SLANTE PANEL 132JW IAW FEDEX A310 AMM 52-54-10-2 PART 2 B1.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

T-CAP IS CORRODED ON END AT FRAME 38.2 RBL60. [08-17-07] FABBED AND REMOVED AND REPLACED T-CAP, A310-22-00 SRM 53-10-00, 53-10-15, 51-74-10.

Part: FLOORBEAM — CORRODED (ZONE 300) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

FWD PIT FLOORBEAM UPPER TEE CORRODED FR 34 AT RBL 60. [08-14-07] REMOVED AND REPLACED UPPER TEE AND SPLICE PER A310-200 SRM 53-10-15 PG 241/242

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

AFT PIT FRAME 68 TO 65 STRINGER 56 RIGHT CORRODED. REMOVED CORRODED STRINGER IAW A310 SRM 51-40-21. INSTALLED NEW STRINGER IAW A310 SRM 53-10-14 PG 203.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

FLOORBEAM UPPER TEE CORRODED ON LOWER SIDE AT FRAME 36 RBL 60. [08-08-07] REMOVED CORROSION FOUND OUT OF LIMITS IAW A310-200 SRM 53-10-00, REMOVED CORRODED SECTION AND REPLACED WITH NEW UPPER TEE IAW A310-200 SRM 53-10-15 PG241/242

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

ALC UNDER FLOOR CORROSION ON S49L BETWEEN FRAME 64 AND 65. REMOVED CORRODED SPLICE IAW A310 SRM 51-40-21 PG 23. INSTALLED NEW SPLICE IAW A310 SRM 53-10-14 FIG 201.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

AFT PIT STRINGER 49L BETWEEN FRAME 58 AND 54.3 CORRODED. [08-06-07] REMOVED AND REPLACED AFT PIT STRINGER 49L BETWWEN FRAME 54.3 AND 58 IAW A310 SRM 53-10-14 FIG. 201, PG 203/204.

Part: STRINGER — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

MAIN DECK CARGO COMPT SEAT TRACK FLANGE CORRODED AT FRAME 50/51 STA 2733 Y1446. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW A310 SRM 53-10-16 PG 101. FABRICATED SPLICES AND REPLACEMENT SEAT TRACK SECTION IAW A310 SRM 51-10-16 PG 201. INSTALLED SEAT TRACK REPAIR IAW A310 SRM 53-10-16.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

AFT PIT STRINGER 51L BETWEEN FRAMES 58 AND 54.3 CORRODED. [08-06-07] REMOVED AND REPLACED AFT PIT STRINGER 51L BETWEEN FR 54.3 AND FR 58 IAW A310 SRM 53-10-14 FIG 201 PG 203/204

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

AFT PIT BETWEEN FRAME 66 AND FRAME 65 STRINGER 49L CORRODED REMOVED CORRODED STRINGER 49L BETWEEN FRAME 65-66 IAW A310-200 SRM 51-40-21 PG 23. INSTALLED NEW STRINGER IAW A310-200 SRM 53-10-14 FIG 201.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

ALC STR 55 L CORRODED BETWEEN FR 59 AND FR 61 IN WORK. ALL WORK WAS ACCOMPLISHED ON THIS N/R. CUT OUT STRINGER 55L BETWEEN FRAME 58 AND FRAME 63 IAW A310 SRM 53-10-44 FIG 201. FABRICATED STRINGERCOUPLINGS IAW A310 SRM 53-10-14 FIG 201, ALODINED, PRIMED AND PAINTED REPAIR PARTS IAW A310 SRM 51-21-10 PAR3, PART MARKED INSTALLED STRINGER 55L IAW A310 SRM 51-40-21 PARA 6 AND7, INSTALLED SHEAR TIE FRAME 59,60,61 IAW A310 SRM 51-40-21PARA 6 AND 7.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

ALC STR 56L CORRODED BETWEEN FR 63 AND FR 64 IN WORK. 09-04-07 FOUND TO BE OUT OF LIMITS IAW FED EX A310 SRM 51-741-10. REMOVED DAMAGED SECTION OF STRINGER 56L FROM FR 58- 64 IAW FED EX A310 SRM 51-40-21 PG 23-24. FABRICATED AND INSTALLED REPAIR PARTS FOR STR 56L FROM FR 58-64 IAW FED EX A310 SRM 53-10-14 MAJOR REPAIR

Part: STRINGER — CORRODED (ZONE 100) · airframe 35,345 hrs · 29,942 cycles

ALC STR 51 L CORRODED BETWEEN FR 58 AND FR 61 IN WORK. 09-04-07 FABRICATED NEW STRINGER SECTION IAW SRM 51-40-44, LOCATED DRILLED AND TREATED PRIMED AND PAINTED REPAIR PARTS IAW A310 SRM 51-40-44, 51-21-10,51-23-10, INSTALLED STRINGER 51L AND SPLICE IAW A310 SRM 51-40-21 AND 53-10-14 FIG 210.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

ALC STR 56 R CORRODED BETWEEN FR 58 AND FR 61. REMOVED CORROSION IAW FEDEX A310 51-74-10 PG 204, FOUND TO BE OUT OF LIMITS IAW FEDEX SRM 51-74-10, REMOVED DAMGED PORTIONS OF STRINGER 56R FROM FROM FR58- FR64 IAW FEDEX SRM A310 SRM 51-40-21 PG 23 AND 24, FABRICATED AND INSTALLED REPAIR PARTS FOR STRINGER 56R FROM FRAME 58 TO FRAME 64 IAW FEDEX SRM A310 SRM 53-10-14

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

ALC UNDER FLOOR CORROSION ON STR 49 L BETWEEN FR 64 AND 65 IN WORK. 09-04-07 REMOVED CORRODED STRINGER IAW A310 SRM 51-40-21 PG 23, LOCATED DRILLED AND INSTALLED STRINGER AND SPLICE IAW A310 SRM 53-10-14 PG 201, 51-40-40.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

ALC STRINGER 52 R CORRODED BETWEEN FR 58 AND FR 61. [08-06-07] REMOVED AND REPLACED STRINGER SECTION FR 59 TO FR 61 STR 52 R IAW A310 SRM 53-10- 14 PG 203

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

AFT PIT FRAME 67, STRINGER 54R CORRODED. REMOVED AND REPLACED STRINGER 54R FR 67 IAW A310 SRM 53-10-14 PG 203/204 FIG 201.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

ALC STR 50 L CORRODED BETWEEN FR 58 AND FR 60. [08-14-07] REPLACED STRINGER IAW A310 SRM 53-10-14, FIG 201, PG 203/204

Part: STRINGER — CORRODED (ZONE 100) · airframe 35,345 hrs · 29,942 cycles

FWD PIT LEFT SIDE BILGE AREA S53L HAS CORROSION BETWEEN FRAME 35 AND 36. [08-29-07] REMOVED CORROSION IAW A310-200 SRM 51-74-10 PAGE 201. FOUND TO BE OUT OF LIMITS A310-200 SRM 53-14-14. REMOVED STR. 53L FROMFRAME 35 TO 37 IAW A310-200 SRM 51-40-21 PARA. 5. FABRICATED IAW A310-200 SRM 53-10-14 FIG. 201. INSTALLED IAW A310-200 SRM 51-40-21 PARA. 7. LEAK CHECK GOOD IAW A310-200 MM 21-51-00-5.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

A L C AT FR 61 SHEAR TIE CORRODED BETWEEN S52R AND S53R. SHEAR TIE CORROSION OUT OF LIMITS IAW A310 SRM 53-10-00 TABLE 102. REMOVED AND REPLACED SHEAR TIE IAW A310 SRM 51-72-10.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

AFT PIT STRINGER 54 R AT FRAME 70 CORRODED. [08-20-07] REMOVED AND REPLACED STRINGER 54R AT FR 70 PER A310 SRM 53-10-14 PG 203/204 FIG 201

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

FWD PIT LEFT SIDE S45L HAS CORROSION BETWEEN FRAME 38.1 AND FRAME 38.2. REMOVED AND REPLACED S45L IAW A310-200 SRM 53-10-14 PG 203/204.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

AFT PIT STRINGER 52L BETWEEN FRAMES 61 AND 62 CORROSION IN WORK. [08-06-07] REMOVED AND REPLACED STRINGER 52L BETWEEN FR 61-63 IAW A310 SRM 53-10-14 PAGE 203/204.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

BULK CARGO BAY STR 55 L CORRODED BETWEEN FR 64 AND 65. REMOVED CORROSION IAW A310 SRM 51-74-10 STRINGER 55L CONNECTING SECTION AT FR 65 OUT OF LIMITS IAW A 310 SRM 53-17-14 PG101. REMOVED CONNECTING SECTION IAW A310 51-40-21 FIG 8 INSTALLED NEW CONNECTING SECTION PN A5397422820090 IAW A310 SRM 53- 10-14 FIG 201

Part: STRINGER — CORRODED (ZONE 100) · airframe 35,345 hrs · 29,942 cycles

FWD PIT LEFT SIDE BILGE AREA S53L HAS CORROSION BETWEEN FRAME 36 TO FRAME 37. [08-29-07] ALL WORK ACCOMPLISHED ON FEDEX N/R N00610.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

AFT PIT FR 67 STRINGER 53 L CORRODED. [08-07-07] REMOVED CORROSION REF A310 SRM 51-74-10, OUT OF LIMITS. ORG MAT THICKNESS .078, MAT LOSS .028 REMANING .050. REMOVED AND FABRICATED NEW STRINGER AND SPLICE PER A310 SRM 53-10-14. ALODINED, PRIMED AND TOPCOATED REF A310 SRM 51-21-10 AND 51-23-10. INSTALLED NEW STRINGER AND SPLICE REF A310 SRM 53-11-14, AND 51-40-21

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

ALC STR 50 L CORRODED BETWEEN FR 63 AND FR 64. 09-04-07 REMOVED CORROSION FROM STRINGER FOUND TO BE OUT OF LIMITS, REMOVED STRINGER 50L FROM FRAME 62 TO 65, RECEIVED NEW STRINGER , LOCATED DRILLED TREATED PRIMED AND INSTALLED NEW STRINGER. IAW 51-40-11, 53-17-14, 51-40-21, DAN50-04, 53-21-14 AND 53- 10-14

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

AFT PIT, STR 54L FRAME 68 TO 70 CORRODED. [08-07-07] REMOVE AND REPLACED STRINGER 54L FRAME 68 TO 70 IAW SRM 53-10-14 PG 203/204. 09-04-07

Part: SEAT TRACK — CORRODED (BS 3888-3938) · corrosion level 2 · airframe 35,345 hrs · 29,942 cycles

RIGHT AFT MAIN DECK CARGO COMPARTMENT SEAT TRACK UPPER SURFACE HAS CORROSION BETWEEN C72-C73 BL 00 REMOVED FLOOR PANEL 252/251WH TO GAIN ACCESS TO DAMAGED SEAT TRACK GOT MATERIAL FOR SEAT TRACK AND U SECTION. LOCATED AND DRILLED SEAT TRACK AND U SECTION. INSTALLED SEAT TRACK AND U SECTION IAW AIR BUS 310/200 SRM 51-40-21 MATERIAL ID SEAT TRACK (PO NR 577763-1) PART NR FOR U SECTION (R5327049020000).

Part: LINE — LEAKING (HYD SYSTEM) · airframe 35,266 hrs · 29,890 cycles

ON LANDING WITH MEDIUM AUTOBRAKES, LOST ALL GRN SYS HYD QTY GREEN HYD PUMPS WERE SHUT DOWN WITHIN 30 SECONDS. LARGE HYD LEAK SEEN ON RT LANDING GEAR. INVESTIGATING ORIGIN OF LEAK. LOCATED HYD LINE ON RT MLG AT TOP OF GEAR P/N A3241014500000 RUPTURED. REMOVED LINE AND CAPPED. RAN GRN SYS HYD WITH ELEC AND ENG PUMPS AFTER SERVICING GREEN HYD SYS. NO FURTHER LEAKS DETECTED. AWAITING NEW HYD LINE TO EFFECT REPAIR. ALSO, INSPECTED ENG PUMP DELTA P'S NONE WERE POPPED. REMOVED AND REPLACED RUPTURED HYD LINE AS REQUIRED, LEAK CHK GOOD ON GROUND AT THIS STATION, REF A310 MM 20-23-12-0, 29-00-00-4 AND SMP.

Part: SLIDE — CONTAMINATED (R1 DOOR) · airframe 34,449 hrs · 29,430 cycles

REMOVED SLIDE FROM R1 DOOR. REMOVAL FROM A/C ONLY. SLIDE UNIT REMOVED FROM AIRCRAFT AND BEING SENT TO VENDOR FOR FURTHER INVESTIGATION. SLIDE UNIT WILL HAVE NEW SLIDE UNIT INSTALLED TO RETURN A/C TO SERVICE. EMERGENCY EVACUATION WAS DUE TO ATA 21 AND BEING CONTAMINATED BY HYDRAULIC FLUID.

Part: UNKNOWN — SMOKE · airframe 34,449 hrs · 29,430 cycles

SHORTLY AFTER BOTH ENGINE START, SMOKE AND FUMES APPEARED. DONNED OXYGEN COMPLETED EVAC CHECKLIST. R1 DOOR/SLIDE JAMMED WOULD NOT OPEN, L1 OPENED NORMALLY, SLIDE DEPLOYED. (SLIDE ADDRESSED IN ANOTHER SDR) T/S SMOKE/FUMES TO NR 1 PACK, CONTAMINATION FROM AIR CHECK VALVE TO HYD RES HEAD PRESS SYS. REPAIRED BY REPLACING ALL CK VALVES AND CLEANING AIR LINES AND CLEANED PACK DUCKS. THE DISCOVERED DAMAGE/CRACK IN DUCTING TO BE REPAIRED IN B-CK.

Part: SKIN — PUNCTURED (ZONE 200) · airframe 33,537 hrs · 28,929 cycles

PUNCTURE AND DENT IN SKIN APPROX FR 44 RT STRINGERS 6-7. DAMAGE APPROX 5.00 IN X 3.2 IN. CUT OUT DAMAGE IAW A310-200 SRM 53-27-00. NDT FOR CRACKS IAW NTM 51-10-08. NO CRACKS NOTED. INSTALLED REPAIR DOUBLER IAW A310-200 SRM 53-10-12 FIG. 228. WORK DOCUMENTED ON NRC N00063.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 32,732 hrs · 28,367 cycles

UPON CLEANING FOR CPC ON NRC00393/FEDEX EA 6-5100-84269 FOUND CORROSION ON STRINGERS 53L AND 54L BETWEEN FRAMES 54 TO 54.2. REPAIRED IAW FEDEX EA 6-5315-85997 PART 1.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 32,732 hrs · 28,367 cycles

AFT PIT FR60 STRINGER 48 RT JUST BELOW DOOR FRAME CORRODED. REPLACED CORRODED STRINGER, THREE SPLICE ANGLES, AND TWO BRACKETS IAW A310-200 SRM 53-10-14. RESTORED PROTECTIVE COATING IAW A310-200 SRM 51-23-00.

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,732 hrs · 28,367 cycles

AFT PIT BETWEEN FR 54.1 & FR 54.2 BILGE CENTER ON SKIN AND STR 55L TO STR 55R CORROSION FOUND UPON CLEANING AREA FOR CPC ON NRC 00393/FEDEX EA 6-5100-84269. REPAIRED IAW FEDEX EA 6-5315-85997 PART 1.

Part: RIB — CORRODED (ZONE 300) · corrosion level 2 · airframe 32,732 hrs · 28,367 cycles

VERTICAL STAB R&L TIP ATTACH FLANGES CORRODED AROUND HOLES AND UNDER NUT PLATES. REMOVED AND REPLACED RIB FLANGES IAW A310-200 SRM 51-72-10. APPLIED SURFACE PROTECTION IAW A310-200 SRM 51-73-10.

Part: SKIN — DAMAGED (ZONE 600) · airframe 32,732 hrs · 28,367 cycles

RIGHT I/B FLAP LWR T/E DELAMINATED. REMOVED EXISTING REPAIR. DRIED HONEYCOMB CORE IAW A310-200 SRM 51-77-10 PARA 2(G). INSTALLED DOUBLER ON UPPER AND LWR SKINS IAW A310-200 SRM 57-53-12 PARA 11. INSTALLED RIVETS IN T/E IAW A310-200 SRM 51-40-21.

Part: BULKHEAD — CORRODED (ZONE 100) · corrosion level 2 · airframe 32,732 hrs · 28,367 cycles

BULKHEAD 39 INTERIOR SIDE HAS CORROSION ON LWR FLANGE AND RT STRINGERS 43, 45, 46, 47, 49-50. REMOVED FWD AND AFT STRINGER TIES, BULKHEAD T-CHORD SPLICE ANGLES IAW A310-200 SRM 51-40-21. CLEANED CORROSION IAW A310-200 SRM 51-74-10 AND FOUND BULKHEAD WEB AT STR 51 OUT OF LIMITS. REMOVED DAMAGED SECTION AND INSTALLED FILLER, SHIMS, AND DOUBLER IAW EA6-5315-85548. REPLACED STR 55 END FITTING. REMAINING PARTS SERVICEABLE IAW EA 6-5315-86003. TREATED CORROSION AND PRIMED REMAINING STRUCTURE IAW A310-200 SRM 51-21-00. RE-ASSEMBLED BULKHEAD IAW A310-200 SRM 51-40-21. TOPCOATED AFFECTED AREA IAW A310-200 SRM 51-21-00.

Part: MOUNT — CORRODED (ZONE 400) · airframe 32,732 hrs · 28,367 cycles

NR 1 ENGINE PYLON FWD ENGINE MOUNT FITTING HAS CORROSION ON MOUNTING FACE AND AROUND MOUNTING HOLES UPPER SIDE. REMOVED CORROSION FROM MOUNT FACE IAW A310-200 SRM 51-74-10, FOUND TO BE WITHIN LIMITS A310-200 SRM 54-51-81 FIG 104. SPOT-FACED UPPER AFT I/B & O/B HOLES IAW A310-200 SRM 51-11-80. FOUND AFT O/B HOLE TO BE WITHIN LIMITS IAW A310-200 SRM 54-51-81 FIG 104 SHT 1. FOUND AFT I/B HOLE BEYOND LIMITS A310-200 SRM 54-51-81 FIG 104 SHT 1. AFT I/B HOLE IS ACCEPTABLE IAW FEDEX EA 6-5450-85609 AND AIRBUS INTERIM RAS 034934/010/2005. PERFORMED DYE PENETRANT INSPECTION IAW A310-200 NDT 51-91-00. NO CRACKS NOTED. APPLIED CADMIUM PLATING AND HI-TEMP PLATING IAW A310-200 SRM 51-75-10.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 32,732 hrs · 28,367 cycles

MDDC FLOORBEAM AT FR37 LT SIDE CRACKED AT VERTICAL STIFFENER, FWD SIDE. REPAIRED FLOORBEAM BY INSTALLATION OF REPAIR ANGLES IAW A310-200 SRM 53-10-15 FIG 201, SH2.

Part: ATTACH FITTING — DAMAGED (ZONE 300) · airframe 32,732 hrs · 28,367 cycles

RIGHT HORIZONTAL STABILIZER UPPER SPAR AT RIB 5 HAS DAMAGED HOLE THROUGH SPAR CAP AND ELEVATOR ATTACH FITTING. STOP-DRILLED HOLE TO 0.4350. FABRICATED ONE COUNTERSINK TYPE -A- BUSHING AND ONE SHOULDER TYPE -C- BUSHING AND SHRUNK FIT BUSHINGS INTO SPAR AND ELEVATOR ATTACH FITTING, RESPECTIVELY. OPENED BUSHING HOLE TO 0.250 NOMINAL SIZE AND INSTALLED BLUE PRINT FASTENER. ALL WORK PERFORMED IAW FEDEX EA 6-5510-85484 AND AIRBUS RAS/CASA/3942/2005 AND DOCUMENTED ON NRC N00530.

Part: SPAR — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 32,732 hrs · 28,367 cycles

RT HORIZONTAL STAB UPPER TRAILING EDGE LOWER SURFACE FROM INBOARD END AND EXTENDING OUTBOARD 31.0 INCHES. THERE IS LIGHT TO SEVERE CORROSION AROUND AND BETWEEN NUT PLATES. REMOVED CORROSION IAW A310-200 SRM 51-74-10 AND FOUND A SECTION OUT OF LIMITS IAW A310-200 SRM 55-10-00. CUT OUT DAMAGED SECTION (RIB 3 TO RIB 5) AND FABRICATED REPAIR PARTS IAW A310-200 SRM 55-11-21 FIG 219. INSTALLED REPAIR PARTS IAW A310-200 SRM 55-11-21 AND 51- 40-21.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 32,732 hrs · 28,367 cycles

FR72-FR73 RIGHT STG 55 HAS CORROSION (FOUND DURING CPC APPLICATION). CLEANED CORROSION, FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 53-10-00. CUT OUT DAMAGED SECTION AND SPLICED IN NEW STRINGER SECTION IAW A310-200 SRM 53-10-14 FIG 201. ALODINED, PRIMED AND TOP COATED IAW A310-200 SRM 51-23-00.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 32,732 hrs · 28,367 cycles

FWD CARGO PIT ENTRYWAY LWR SILL HAS CRACKED SUPPORT AT FR22. CRACK IS ON LOWER SIDE AND IS 2.5 INCH LONG. REMOVED AND REPLACED SUPPORT IAW A310-200 SRM 51-72-10. ALODINED, PRIMED, AND TOPCOATED AS REQUIRED IAW A310-200 SRM 51-21-10. REAPPLIED CPC IN AFFECTED AREA IAW A310-200 SRM 51-23-20.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 32,732 hrs · 28,367 cycles

FR54-FR54.1 RT STR 44 CORROSION ON STRINGER (FOUND DURING CLEANUP FOR CPC APPLICATION). CLEANED CORROSION, FOUND TO BE OUT OF LIMITS PER A310-200 SRM 53-10-00. SPLICED IN NEW STRINGER SECTION WITH NEW END FITTING IAW A3010-200 SRM 53-10-14 FIG 201. ALODINED, PRIMED, AND TOP COATED IAW A310-200 SRM 51-23-00. WORK DOCUMENTED ON NRC N00646.

Part: SPAR — CORRODED (ZONE 300) · corrosion level 2 · airframe 32,732 hrs · 28,367 cycles

VERTICAL FIN REAR SPAR R & L PANEL SUPPORT STRUCTURE HAS MODERATE CORROSION AT PANEL ATTACH POINTS. REMOVED CORROSION IAW A310-200 SRM. APPLIED SURFACE PROTECTION IAW A310-200 SRM 51-23-10. AT RT SIDE RIB 26, TRIMMED OUT DAMAGED SECTION OF TOP FLANGE, INSTALLED 2024-T3 FILLER, AND 2024-T3 0.063 STRAP IAW EA 6-5530-85551 DATED 01/04/05.

Part: CONTROL LEVER — FAULTY (BRAKE SYS) · airframe 31,891 hrs · 27,821 cycles

DURING TAKEOFF ROLL, GOT TAKEOFF CONFIGURATION WARNING WITH ECAM PARKING BRAKE ON WARNING. REJECTED TAKEOFF PRIOR TO TAKEOFF. TAKEOFF CONFIG CHECK SHOWED NORM FOR T/O. NOTE ACARS FLIGHT LOG PAGE NEVER SHOWED BLOCK OUT. REMOVED AND REPLACED 7GG PARKING BRAKE CONTROL LEVER & SWITCH ASSY, RIG AND OPS CHECKED REF AMM 32-45-11-4 AND OPS CK AMM 32-45-00-5 & 32-42-00-5.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 30,464 hrs · 26,933 cycles

IMMEDIATELY AFTER LEVEL OFF AT FL350, NR 2 ENG EXPERIENCED SEVERE COMPRESSOR STALLS. PWR WAS REDUCED, WHEN PWR WAS INCREASED STALL RETURNED. F/F & EGT FLUX WAS EVIDENT AND N1 & 2 MOVED ACCORD. QRH PROC WAS ACCOMPL DURING DESCENT AND RETURNED TO ABQ. WHEN HP VLV WAS SEL OFF PER QRH THERE WERE NO MORE STALLS, ACFT WAS NOW BELOW FL300. INSPECTED VSV ACTUATION SYSTEM, NO DAMAGE NOTED. INSPECTED MAGNETIC GEARBOX PLUG PER MM. NOTABLE MATTER FOUND. INSPECTED SCAV OIL FILTER PER MM, NO DEBRIS FOUND.

Part: LANDING GEAR — FAILED (NOSE) · airframe 28,692 hrs · 25,757 cycles

AFT NORM GEAR EXTEND, NOSE GEAR DID NOT EXTEND & 2 UNSAFE GEAR IND.

Part: SKIN — WORN (HORIZONTAL STAB) · airframe 28,684 hrs · 25,751 cycles

SKIN DAMAGED AND CUTTING ANTI-CHAFING PLATE BENEATH RT HORIZONTAL STAB. INSTALLED DOUBLER ON FUSELAGE PER EA NR 6-5319- 50270.

Part: SKIN — WORN (TAIL) · airframe 28,684 hrs · 25,787 cycles

SKIN DAMAGED AND CUTTING ANTI-CHAFING PLATE BENEATH RT HORIZONTAL STAB. INSTALLED DOUBLER ON FUSELAGE PER EA NR 6-5319-20270.

Part: DUCT — RUPTURED (NR 2 ENGINE)

STA-OAK: ON CLIMB 250 KTS/10000. ADVANCED THROTTLE FOR CLIMB AND NR 2 ENG FIRE WARNING ILLUMINATED B-LOOP WAS CHECKED AND TURNED OFF. LEVELED OFF THEN STARTED TO CLIMB AGAIN. FIRE WARNING ILLUMINATED AGAIN THEN GOT HOT AIR SUPPLY OVERHEAT. RETURNED TO OAK. FOUND RUPTURED HIGH PRESS DUCT. REMOVED AND REPLACED DUCT PERFORM ENG RUN PER JRH. NO LEAKS NOTED.

Part: RETRACT MECH — LACK OF LUBE (NLG)

FINAL APPROACH AT IND ECAM MSG, GEAR NOT DOWN L/G GRAVITY EXTENTION. COMPLETED L/G UNSAFE INDICATED. BOTH SYS 1 AND SYS 2 IND NOSE GEAR UNLOCKED. COMPLETED L/G GRAVITY EXTENTION GEAR DID NOT COME DOWN. FLEW BOX PATTERN IN SHARP HIGH G-TURN, HEARD NOSE GEAR LOCK IN PLACE. SYS 1 AND SYS 2 INDICATED DOWN. ECAM MSG, NO NOSE GEAR STEERING. CONFIRMED NO NOSE GEAR STEERING ON ROLLOUT/TAXI. PINNED AND TOWED IN, L/G EXTENTION AND RETRACTION TEST, LUBED NLG BEARINGS AND ALL RELATED COMPONENTS. OPERATION NOW OK.

Part: DEPRESSURE VALVE — FAILED (CABIN)

DURING CLIMB, COULD NOT PRESSURIZE THE AIRCRAFT. MANUAL DEPRESSURIZATION VALVE SHOWED OPEN ON ECAM. RETURNED TO MC. *S/D* REMOVED AND REPLACED VALVE 93 HM IAW M/M 21-31-15 AND PERFORMED TEST IAW M/M 21-31-00, NO DISCREPANCIES NOTED.