N433FE

ATA 5730

Part: PANEL — MAINT ERROR (ZONE 500) · airframe 44,032 hrs · 20,130 cycles

WHILE DRILLING HEAD FROM STRIPPED SCREW A HOLE WAS ELONGATED IN WING PLANK COMMON TO PANEL 550 JB COMPLIED WITH EA6-5700-106331 PT1 BY PERFORMING REPAIR IAW AIB TD /J1/S1/04141/2007 ISSUE A.

ATA 5330

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 44,031 hrs · 20,127 cycles

PREVIOUS REPAIR, LWR RT SIDE FUSELAGE SKIN JUST BELOW AFT LAV ACCESS DOOR BETWEEN FR 78 AND FR 79, STR 49 RT TO STR 50 RT HAS EXTERNAL REPAIR DOUBLER MEASURING 13.4 IN BY 6.8 IN BELOW CUTOUT AND ABOVE THE LAP SEAM PREVIOUSLY INSTALLED REPAIR WAS DETERMINED NOT TO BE IAW A310 SRM 53-10-16 FIG 216 SHEETS 1 AND 2 AND FIG 217 SHEET 3, DUE TO REPAIR ENDING ON TOP OF LAP SEAM STRINGER 50 RT AND CRACK STOPPER, BASED ON VISUAL EVALUATION WITH THE REPAIR INSTALLED. REMOVED EXISTING REPAIR AND REPAIRED SKIN IAW A310 SRM 53-10-12 FIG 216 SHEETS 1 AND 2 AND FIG 217 SHEET 3.

ATA 5230

Part: SKIN — MISREPAIRED (CARGO DOOR) · airframe 44,031 hrs · 20,127 cycles

PREVIOUS REPAIR FWD CARGO DOOR EXTERIOR AFT SKIN, BETWEEN FR 25 AND 25A ABOVE BEAM 4 HAS EXTERNAL. REPAIR DOUBLER MEASURING 5.6IN * 8.4 IN DUE TO PREVIOUSLY INSTALLED REPAIR LOCATED AT FWD CARGO DOOR EXTERIOR AFT SKIN BETWEEN FS 25 AND 25A ABOVE BEAM 4 WAS DETERMINED NOT TO BE IAW A310 SRM 52-30-00 FIG 203 DUE TO INCORRECT THICKNESS USED. REMOVED AND REPLACED REPAIR DOUBLER IAW A310 SRM 52-30-00 FIG 203.

ATA 2550

Part: TRACK — CORRODED (ZONE 100) · airframe 44,031 hrs · 20,127 cycles

AFTER REMOVAL OF FLOORBOARDS FOR MOD E6-5320-7-5001 PT2, FWD PIT ROLLER TRACK 2R INBD SIDE OF TRACK (FLANGE) HAS 7 AREAS OF CORROSION AS MARKED BETWEEN FR 34 AND FR 38.2. REMOVED CORROSION IAW A310 SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW A310 SRM 53-10-15. REMOVED AND REPLACED ROLLER TRACK IAW A310 SRM 51-72-10.

ATA 5330

Part: SKIN — GOUGED (FUSELAGE) · airframe 44,031 hrs · 20,127 cycles

SKIN GOUGE AT FS 76 - 77 LT SIDE JUST AFT OF L2 DOOR APPROX 10 INCHES L BY .10W BY .085D BETWEEN STRINGERS 25 TO 28 LT REF N00426. REPAIRED SKIN IAW A310 SRM 53-10-12 FIG 228 SHEET 3. REPROTECTED SURFACE IAW A310-200 SRM 51-75-10.

ATA 2550

Part: ROLLER TRAY — CORRODED (ZONE 100) · airframe 44,031 hrs · 20,127 cycles

AFTER REMOVAL OF FLOORBOARDS FOR MOD E6-5320-7-5001 PT2 - FWD PIT ROLLER TRACK 1R OTBD SIDE OF TRACK (FLANGE) HAS 9 EA AREAS OF CORROSION AS MARKED BETWEEN FS 34 AND 6" AFT OF FS 38.2. REMOVED CORROSION 11 PLACES FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED ROLLER TRACK IAW A310-200 AMM25-52-24-4, 25-52-57-4, 25-52-34-4 SRM 51-74-10, 53-10-15, 51-21-10, 51-75-10.

ATA 5100

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 44,031 hrs · 20,127 cycles

PREVIOUS REPAIR, LEFT OF AFT PAX DOOR EXTERIOR SKIN LWR AFT CORNER HAS EXTERNAL REPAIR DOUBLE MEASURING 9.2IN BY 7.3IN. PREVIOUSLY INSTALLED REPAIR LOCATED AT AFT PAX DOOR EXTERIOR SKIN LOWER AFT CORNER WAS DETERMINED NOT TO BE IAW A310 SRM 52-10-00 FIG 203, DUE TO THE OUTER ROW OF FASTENERS WERE MISSING 7 RIVETS BASED ON A VISUAL EVALUATION WITH THE REPAIR INVOLVED. DRILLED AND COUNTERSUNK 7 NEW HOLES AND INSTALLED 7 NEW RIVETS PER A310 SRM 52-10-00 FIG 203.

ATA 5414

Part: PANEL — DENTED (NR 1 NACELLE) · airframe 44,031 hrs · 20,127 cycles

A DENT EXIST AT NR 1 ENG PYLON UPPER FWD FIXED L/E PNL MEASURING 6 INCH BY 4 INCH BY 0.350 INCH REMOVED AND REINSTALLED FIXED PANEL IAW A310 SRM 51-40-21. REWORKED DENT IAW A310 SRM 54-50-00 FIG 201 AND EA 6-5480-106313 PT1.

ATA 3240

Part: BRAKE ASSY — SMOKE (MLG) · airframe 43,818 hrs · 20,010 cycles

ON LANDING, THE RIGHT TIRES GOT HOT WHILE THE LEFT SIDE STAYED BELOW 100' ON TAXI IN THE NR 4 GOT TO 375', NO FANS. TOWER REPORTED SMOKE COMING FROM THE RIGHT SIDE ON LANDING, SO FIRE CREW DID A PRECAUTIONARY INSPECTION. ALL OK. AFTER A/C BLOCKED IN AND FIRE CREW RELEASED A/C, CHECKED TIRE PRESSURES, NONE OVER 200 PSI. INSPECTED TIRES AND BRAKES FOR LEAKS OR EVIDENCE OF SKIDDING OR DAMAGE. NONE FOUND. TEMPS WERE ALL BELOW 250'. OK FOR SERVICE.

ATA 2612

Part: CONTROL UNIT — MALFUNCTIONED (FIRE DETECTION) · airframe 43,370 hrs · 19,805 cycles

DURING TAKEOFF ABOUT 90 KIAS ECAM FLASHING NAC HEAT WAS ABOVE 100 DEGS. COMPLETED ABORT. NO ABNORMAL ENGINE INDICATIONS NOTED. REPLACED NR 2 FIRE DETECTION CONTROL UNIT IAW A310 MM 26-12-11-04 AND EA 6-2610-72097. RAN NR 2 ENGINE IAW CHAPTER 5 AND 6-11 A310 JRH, NO DISCREPANCIES NOTED AT THIS TIME. BOTH NACELLE TEMPS WERE IDENTICAL FOR NR 1, NR 2 ENGINES AT MAX POWER (40).

ATA 5270

Part: WARNING LIGHT — FALSE INDICATION (CARGO DOOR) · airframe 42,432 hrs · 19,266 cycles

FWD CARGO DOOR LIGHT CAME ON DURING TAKEOFF. RTO (LIGHT CAME ON & OFF.) AC RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 11JUL05 DOOR CLOSED & LOCKED INDICATION ON ECAM DOOR PAGE - INOPERATIVE. DOOR VISUALLY CHECKED CLOSED & LOCKED. DOOR VISUALLY VERIFIED CLOSED AND LOCKED PRIOR TO DEPARTURE. (OPEN)