N452FE

Part: RIB — CORRODED (ZONE 600) · corrosion level 2 · airframe 56,738 hrs · 20,408 cycles

N16 MLG RT GEAR RIB 5, LUG WITH CORROSION UPON REMOVAL OF BUSHES E AND F. THE LUG BORE AND FACES WERE REPAIRED AS PER FEDEX EA 6-5710-126457.

Part: RIB — CORRODED (ZONE 500) · corrosion level 2 · airframe 56,738 hrs · 20,408 cycles

LT GEAR RIB 5, CORROSION FOUND UPON REMOVAL OF BUSH E AND F. A REPAIR IN ACCORDANCE WITH EA 6-5710-126452 WAS ACCOMPLISHED.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 56,592 hrs · 20,237 cycles

ON TAKEOFF FROM CDG GOT REVERSE UNLOCK LIGHT ON ECAM ALSO MATCHED WENT TO NR 2 ENG REVERSE. LIGHT WENT OUT THEN CAME BACK ON WITH POWER ADVANCE. LEFT NR 2 AT IDLE AND CAME BACK TO LAND ASAP CDG. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 22JUN08 "MEL 78-30-01-C: ENGINE (IDENTIFY 1 OR 2) NR 2 THRUST REVERSER, INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION.

Part: SWITCH — WORN (THRUST REVERSER) · airframe 56,593 hrs · 20,239 cycles

ON TAKEOFF FROM CDG GOT REVERSE UNLOCK LIGHT ON ECAM ALSO MATCHED WENT TO NR 2 ENG REVERSE. LIGHT WENT OUT THEN CAME BACK ON WITH POWER ADVANCE. LEFT NR 2 AT IDLE AND CAME BACK TO LAND ASAP CDG. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 22JUN08 (NO BUFFETING REPORTED). PERFORMED SEVERAL TIMES EXTENSION/RETRACTION OF THE THRUST REVERSER. INSPECTED CABLES FOR NO STRESS. CHECKED SWITCHES S303 AND S307: FOUND S3 07 INSIDE SPRING WEAK RD AND RD S307 AS PER MM78-3 1-18-4 03. TRIED SEVERAL TIMES THRUST REVERSER, NO ABNORMALITIES FOUND. MEL CLOSED/STICKER REMOVED.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 55,998 hrs · 19,688 cycles

MDCC - TRACK WITH CORROSION BETWEEN FRAMES 15A AND 19 AT Y-1959. THE CORRODED PART WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10.

Part: ARM — CORRODED (ZONE 300) · corrosion level 2 · airframe 55,998 hrs · 19,688 cycles

RUDDER HINGE ARM NR 5 WITH CORROSION. THE HINGE ARM WAS REPLACED IN ACCORDANCE WITH AMM 55-36-46.

Part: DOOR FRAME — CRACKED (ZONE 800) · airframe 55,998 hrs · 19,688 cycles

AFT CARGO COMPARTMENT DOOR FRAME WITH CRACK AT HEAD, FR 61A. REPAIR ACCOMPLISHED PER FEDEX EA 6-5230-112412.

Part: SEAT TRACK — WORN (ZONE 100) · airframe 55,998 hrs · 19,688 cycles

MDCC - FLOOR - WEAR AT TRACK Y-1456 BETWEEN FR 62 AND 63. REPAIRED IN ACCORDANCE WITH SRM 53-10-16 FIG 208 SHEET 1 - PAGE 243 TO 248.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 55,998 hrs · 19,688 cycles

N00528 MDCC - CABIN FLOOR - FLOORBEAM AT CABIN WITH CRACK AT FRAME 54.3 AND BETWEEN TRACKS Y-45 AND Y-953. IT WAS REPAIRED IN ACCORDANCE SRM 53-10-15 FIG 201 SHEET 8.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 55,998 hrs · 19,688 cycles

AFT COMPARTMENT, TRACK Y14710 WITH CORROSION BETWEEN FR 61 AND FR62. THE TRACK WAS REPLACED IN ACCORDANCE WITH AMM 25-52-21.

Part: VANE — NONE (ZONE 500) · airframe 55,998 hrs · 19,688 cycles

WING LT, FLAP INBD, PREVIOUS REPAIR FOUND LOCATED ON FLAP VANE UPPER SKIN IN BETWEEN RIB 17-18. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR CONFORMS TO FEDEX ENGINEERING AUTHORIZATION 6-5720-112413. THIS SDR SUBMITTED IN ERROR- ADMINISTRATOR.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 55,998 hrs · 19,688 cycles

AFT COMPARTMENT, TRACK Y140 WITH DEEP CORROSION BETWEEN FR 61 AND FR 62. THE TRACK WAS REPLACED IN ACCORDANCE WITH AMM 25-52-21.

Part: CROSSBEAM — UNKNOWN (ZONE 100) · airframe 55,998 hrs · 19,688 cycles

CROSSBEAM CRACKED AT FR 35 BETWEEN Y-450 AND Y-953. CROSSBEAM WAS REPAIRED IN ACCORDANCE WITH SRM SUPP 53-10-15 FIG 201 SHEET 2. ON THE JASC/ATA CODE ABOVE PLEASE CONSIDER 5320 INSTEAD OF 5230.

Part: FLAP — NONE (ZONE 600) · airframe 55,998 hrs · 19,688 cycles

WING RT, FLAP INBOARD, PREVIOUS FLUSH REPAIR LOCATED ON FLAP VANE LEADING EDGE BETWEEN RIB 6 - 8. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR CONFORMS TO EXISTING FEDEX EA 6-5750-65125.

Part: FLOORBEAM — NONE (ZONE 100) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR LOCATED ON THE FLOORBEAM FS 1067 - 1184 FR 12A - 14 AND Y-953. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR CONFORMS TO FEDEX EA 6-5310-106718.

Part: FLAP — NONE (ZONE 500) · airframe 55,998 hrs · 19,688 cycles

LT WING, KRUEGER FLAP, PREVIOUS PATCH REPAIR FOUND LOCATED ON KRUEGER FLAP BETWEEN RIB 2A AND RIB3, WS 67. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR CONFORMS TO EXISTING FEDEX EA 6-5750-81817.

Part: SKIN — WORN (LT WING) · airframe 55,998 hrs · 19,688 cycles

LT WING, AILERON ACTUATORS ACCESS PANEL AREA LOWER SKIN WITH BURROWS WITHOUT MARGINAL DISTANCE. IT WAS REPAIRED IN ACCORDANCE WITH FEDEX EA 6-570-106714.

Part: PANEL — CRACKED (ZONE 300) · airframe 55,998 hrs · 19,688 cycles

THS PANEL 331BB WITH CRACK AT RIB NR 3 P/N A55178013-004. REPAIRED IN ACCORDANCE WITH FEDEX EA 6-5510-112411.

Part: PANEL — CRACKED (ZONE 300) · airframe 55,998 hrs · 19,688 cycles

THS PNL 331BB WITH CRACK AT RIB NR 4, P/N A55178014-004. REPAIRED IN ACCORDANCE WITH FEDEX EA 6-5510-112411.

Part: SPOILER — MISREPAIRED (ZONE 600) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON RT UPPER WING SURFACE INBD OF SPOILER 4 WS 935-996 RIB 15-16. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO A SRM REPAIR. REPAIR DOUBLER WAS REMOVED AND NO DAMAGE WAS FOUND. NEW OVERSIZE FASTENERS WERE INSTALLED ON EXISTING HOLES PER SRM 51-40-23.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED RT FS 3514-3567 FR65-66 AND STR33-38. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 53-10-12, FIG 225 (SHEET 2). REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED MAJOR.

Part: AILERON — NONE (ZONE 500) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON LT LWR WING SURFACE, AILERON WS 482-513 RIB8-9. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 57-61-12 FIG 201, PAGE 204.

Part: SKIN — MISREPAIRED (NR 3 SLAT) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON LT WING, L/E OF SLAT 3 WS 1835-1868 RIB 30-31. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 57-44-11 FIG 201, SHEET 2 AND 3.

Part: NONE — NONE (NONE) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON LT LWR WING SURFACE T/E OF INBOARD FLAP WS0-139 RIB1-3. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR CONFORMS TO EXISTING FEDEX EA 6-5750-81810. SDR SUBMITTED IN ERROR- ADMINISTRATOR.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON LT LWR WING SURFACE OF INBOARD FLAP WS 339-409 RIB 6-7. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAIR ACCOMPLISHED IN ACCORDANCE WITH FEDEX EA 6-5710-112425.

Part: SKIN — MISREPAIRED (LT WING) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON LT WING UPPER SURFACE, OUTB OF SPOILER 3 WS935 RIB 15. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO A SRM REPAIR. NEW OVERSIZE FASTENERS WERE INSTALLED ON EXISTING HOLES IN ACCORDANCE WITH SRM 51-40-23.

Part: NONE — NONE (NONE) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON RT WING, L/E OF SLAT 1 WS270-339 RIB 5-6. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. INSPECTION OF FILLER WAS PERFORMED IN ACCORDANCE WITH SRM 57-40-00. REPAIRS IS COVERED BY WRI 5750/4864. REQUIRES INSPECTION OF FILLER AT NEXT C-CHECK. RE-INSPECTION TRACKED UNDER WRI 5750/6797.

Part: SLAT — NONE (ZONE 500) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON LT WING, L/E OF SLAT 1 WS 139-207 RIB 3-4. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 57-42-11 FIG 202 SHEET 2, PAGE 213.

Part: SPOILER — MISREPAIRED (ZONE 600) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON RT UPPER WING SURFACE INBD OF SPOILER 3 WS 737-813 RIB 12-13. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO A SRM REPAIR. REPAIR DOUBLER WAS REMOVED AND NO DAMAGE WAS FOUND. NEW OVERSIZE FASTENERS WERE INSTALLED ON EXISTING HOLES IN ACCORDANCE WITH SRM 51-40-23.

Part: NONE — NONE (NONE) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON RT LOWER WING SURFACE OF INBOARD FLAP WS 139-207 RIB 3-4. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR CONFORMS TO EXISTING FEDEZ EA 6-5750-81811. SDR SUBMITTED IN ERROR- ADMINISTRATOR.

Part: NONE — NONE (NONE) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON RT WING, L/E OF SLAT 3 WS 1246-1311 RIB 20-21. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 57-40-00 FIG 102 - SHEET 7. SDR SUBMITTED IN ERROR- ADMINISTRATOR.

Part: FLAP — NONE (ZONE 500) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON LT LWR WING SURFACE OUTBOARD FLAP WS935-996 RIB15-16. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR CONFORMS TO EXISTING FEDEX ENGINEERING AUTHORIZATION EA 6-5750-81815.

Part: FLAP — MISREPAIRED (ZONE 600) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON RT LOWER WING SURFACE OF OUTBOARD FLAP WS 874-935 RIB 14-15. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. THE JASC/ATA CODE INDICATED SHOULD BE 5750. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 57-53-12 FIG 208 AND FEDEX EA 6-5710-112416.

Part: CROSSBEAM — MISREPAIRED (ZONE 800) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON FWD CARGO COMPARTMENT DOOR FR 21-21A BETWEEN BEAM 3 AND 4. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 52-30-00 FIG 203.

Part: NONE — NONE (NONE) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON RT WING, L/E OF SLAT 1 WS 139-207 RIB 3-4. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. INSPECTION OF FILLER WAS PERFORMED IAW SRM 57-40-00. REPAIR IS COVERED BY WRI 5750/4864. REQUIRES INSPECTION OF FILLER AT NEXT C-CHECK. RE-INSPECTION TRACKED UNDER WRI 5750/6797. SDR SUBMITTED IN ERROR- ADMINISTRATOR.

Part: FLAP — MISREPAIRED (ZONE 600) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON RT UPPER WING SURFACE T/E OF INBOARD FLAP WS0-67 RIB 1-2. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. THE PRESENT SDR CONCERNS THE SAME NR AS SDR 07-2202. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 57-52-12 FIG 204.

Part: SKIN — NONE (ZONE 800) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON FWD RT PAX/CREW DOOR AT AFT LOWER CORNER. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 52-10-00 FIG 203.

Part: SKIN — UNKNOWN (ZONE 100) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED LT FS 3249-3302 FR 60-61 AND STR43-40. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. INFO: ON THE UPPER RIGHT CORNER, ITEM NON ROUTINE NR 202 SHOULD BE NON ROUTINE NR 207. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-10-12 FIG 228 SHEET2, PAGE401/402.

Part: SKIN — UNKNOWN (ZONE 100) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED LT FS 2029-2082 FR 37-38 AND STR 39-42. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAIR WAS ACCOMPLISHED PER SRM 53-10-12 FIG 228 SHEET 1.

Part: NONE — NONE (NONE) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON LT WING UPPER SURFACE, SPOILER 2 WS 270-339 RIB5-6. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. A VISUAL INSPECTION AND A TAP TEST WERE PERFORMED IN ACCORDANCE WITH FEDEX EA 6- 5770-106717. SDR SUBMITTED IN ERROR- ADMINISTRATOR.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON RT LWR LATERAL PANEL FS 1212-1236, FR 15-15A. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT TO BE IN ACCORDANCE WITH SRM 53-12-12 FIG 203. REPAIR CONFORMS TO FEDEX ENGINEERING AUTHORIZATION EA 6-5330-106716.

Part: FLAP — DELAMINATED (ZONE 600) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON RT UPPER WING SURFACE INBD OF OUTBOARD FLAP WS 663-737 RIB 11-12. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. THE PRESENT SDR CONCERNS THE SAME NR AS SDR 07-2201. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 57-53-12 FIG 208.

Part: STRINGER — NONE (ZONE 100) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON LOWER AFT CARGO COMP´T FR 59-61 STRG 54 RT. REPAIR REQUIRES EVALUATION FOR MAJOR /MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-10-14, FIG 201, PAGE 203/204.

Part: NONE — NONE (NONE) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON LT LWR WING SURFACE T/E OF INBOARD FLAP WS207-270 RIB4-5. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR CONFORMS TO EXISTING FEDEX EA 6-5750-81810. SDR SUBMITTED IN ERROR- ADMINISTRATOR.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON RT UPPER WING SURFACE INBD OF SPOILER 3 WS 737-813 RIB 12-13. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO A SRM REPAIR. REPAIR DOUBLER WAS REMOVED AND NO DAMAGE WAS FOUND. NEW OVERSIZE FASTENERS WERE INSTALLED ON EXISTING HOLES IAW SRM 51-40-23.

Part: SKIN — MISREPAIRED (LT WING) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON LT WING UPPER SURFACE, INBD OF SPOILER 3 WS 737 RIB 12. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW OVERSIZE FASTENERS WERE INSTALLED ON EXISTING HOLES IN ACCORDANCE WITH SRM 51-40-23.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED LT FS 1870-1923 FR 34-35 AND STR 35-37. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FEDEX EA 6-5330-112415A. THE NON ROUTINE NUMBER INDICATED IN THE RIGHT TO CORNER SHOULD BE N00210 AND NOT N00202. THE JASC/ATA CODE SHOULD READ 5330 INSTEAD OF 52.

Part: STRINGER — NONE (ZONE 100) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON LOWER AFT CARGO COMP´T FR 59-60 STRG 52 RT. REPAIR REQUIRES EVALUATION FOR MAJOR /MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-10-14, FIG 201, PAGE 203/204.

Part: SKIN — MISREPAIRED (CARGO DOOR) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON INNER SKIN OF LOWER AFT CARGO COMP´T DOOR ON FR 60 BETWEEN LONGERON 1-2. REPAIR REQUIRES EVALUATION FOR MAJOR /MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED IN ACCORDANCE WITH FEDEX ENGINEERING AUTHORIZATION 6-5230-112412.

Part: SKIN — NONE (ZONE 200) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED LT FS 1285 FR16A STR20-23. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 53-12-81 FIG 203.

Part: SPOILER — MISREPAIRED (ZONE 600) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON RT UPPER WING SURFACE OUTB OF SPOILER 4 WS 1119-1182 RIB 18-19. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. REPAIR DOUBLER WAS REMOVED AND NO DAMAGE WAS FOUND. NEW OVERSIZE FASTENERS WERE INSTALLED ON EXISTING HOLES IN ACCORDANCE WITH SRM 51-40-23.

Part: FLAP — MISREPAIRED (ZONE 500) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON LT LWR WING SURFACE T/E OF OUTBOARD FLAP WS 874-935 RIB 14-15. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 57-53-12 FIG 208.

Part: NONE — NONE (NONE) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON RT UPPER WING SURFACE T/E OF INBOARD FLAP WS 67-139 RIB2-3. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR CONFORMS TO EXISTING FEDEX EA 6-5750-81811. SDR SUBMITTED IN ERROR- ADMINISTRATOR.

Part: SKIN — CRACKED (ZONE 800) · airframe 55,998 hrs · 19,688 cycles

AFT COMPARTMENT CARGO DOOR WITH INTERIOR SKIN SURFACE CRACKED AT TOP, CLOSE TO FR 62A HEAD. SKIN REPAIRED IN ACCORDANCE WITH FEDEX EA 6-5230-112412.

Part: FLAP — MISREPAIRED (ZONE 600) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON THE RT UPPER WING SURFACE T/E OF INBOARD FLAP WS 0 TO WS 67. REPAIR REQUIRES MAJOR/MINOR EVALUATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR WAS ACCOMPLISHED PER SRM 57-52-12 FIG 204.

Part: NONE — NONE (ZONE 600) · airframe 55,998 hrs · 19,688 cycles

PREVIOUS REPAIR FOUND LOCATED ON RT UPPER WING SURFACE INBD OF OUTBD FLAP WS 663-737 RIB 11-12. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 57-53-12 FIG 208. THIS SDR SUBMITTED IN ERROR- ADMINISTRATOR.

Part: FITTING — CRACKED (SPOILER) · airframe 55,651 hrs · 19,467 cycles

LT WING NR 4 SPOILER PANEL ACTUATOR FITTING BROKEN AND MISSING LUG. SPOILER WAS REPLACED PER AMM 27-61-51.

Part: GCU — MALFUNCTIONED (NR 1) · airframe 54,883 hrs · 18,947 cycles

DURING CLIMB ECAM SGU 1 -FAULT- LIGHT WITH ASSOC BLINKING ON/OFF, SELECTED ECAM 1 -OFF-. TURN OFF FP LO1/2, RO1/2 CTR 1/2 PER FUEL GRAV FEED FOR RO TANK. ACCOMP. FUEL FEED MAN CTL PROCD. RELEASED PER MEL CAT-B EXP 16APR06 MEL 24-11-01: GEN 1 - INOP. APU GEN MUST BE USED IN FLT. VERIFY IN AML/EAML OIL QTY OF DISC IDG, OP'G IDG, APU GEN CKD 1X EACH FLT DAY. C/B OF NAMED FUEL PUMPS POPPED GPCU FAULT -LT GEN WRONG PHASE SEQ- FPS C/B'S RESET. ENG RUNUP W/REMAINING SGU 1 OPS AND NML FPS OPS. GPCU READ -NO FAULT- 4APR06-ITEM CLEARED, T/S IAW TSM 24-00-00 FIG 171, WDM 24-22-01 & 24-22-03, FEEDER AND SENSE WIRING OK. REMOVED AND REPLACED GCU1 IAW 24-22-12-4. RAN NR 1 ENG PER JRH GEN NR 1 PARMS OK.

Part: CONTROLLER — MALFUNCTIONED (T/E FLAP) · airframe 54,076 hrs · 18,309 cycles

ON TAKEOFF FROM FRA, GOT FLAP SYSTEM 2 FAULT. RESELECTED FLAPS TO SLATS/FLAPS 20/20, WHICH DID NOT FIX THE PROBLEM. WENT TO HOLDING AND WORKED THE PROBLEM. RETURNED TO FRA AND LANDED. REMOVED AND REPLACED NR 2 SFCC PER MM 27-51-18-4. SYS OPS CHECK OK. PREMATURE REMOVAL/INSTALLATION OFF MFG 49-079-05.

Part: SWITCH — MALFUNCTIONED (L1 DOOR) · airframe 53,773 hrs · 18,093 cycles

PASSING APPROX 10,000 FT ON DEPARTURE, GOT SC AND ECAM WARNING FOR L1 DOOR UNSAFE. AFTER LEVELING OFF AND FOLLOWING ECAM PROCEDURE TO DEPRESSURIZE, FIRST OFFICER CHECKED THE DOOR WHICH INDICATED UNSAFE. UNEVENTFUL RETURN TO CDG. DESCENDING TO 4,000 FT WITH THE AIRCRAFT DEPRESSURIZED, L1 UNSAFE INDICATION AND ECAM WENT. FOUND LT DOOR HANDLE LOOSE. ADJ/TEST PERFORMED AS PER AMM:52-10-20-5. A/C RELEASED FOR SERVICE.

Part: FITTING — DAMAGED (A/C ACCESS DOOR) · airframe 53,592 hrs · 17,963 cycles

ACCOMPLISH MAINTENANCE "C" CHECK #003 ENT BY: 067708 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 29SEP04 14:53:57:6 BY:067708 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 162248 ON: 29OCT04 12:31:08:0 S=M. AIR COND, SEVERAL HOLES OF FITTINGS AT ACCESS DOORS (148 CZ) TO AIR COND COMPT DAMAGED. REPAIRED IAW EA 6-5315-82534.

Part: SKIN — DENTED (KRUEGER FLAP) · airframe 53,592 hrs · 17,963 cycles

ACCOMPLISH MAINTENANCE "C" CHECK, NR 003 ENT BY: 067708, PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 29SEP04 14:53:57:6 BY:067708 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 162248 ON: 29OCT04 12:31:08:0 S=M. LEFT WING, KRUEGER FLAP OUTER SURFACE FOUND DENTED. REPAIRED IAW EA 6-5750-81817.

Part: FAIRING — DAMAGED (T/E FLAP) · airframe 53,592 hrs · 17,963 cycles

REPAIR, NR 4 FLAP TRACK MOVABLE FAIRING. COMPLY WITH EA 6-5720-49991 REV NO. POS P2 ENT BY: EMMD24 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 20OCT04 15:38:48:9 BY:195875 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 478289 ON: 31OCT04 20:44:51:3 S=M. COMPLIED EA 6-5720-49991.

Part: STRUCTURE — DAMAGED (T/E FLAP) · airframe 53,592 hrs · 17,963 cycles

COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 24NOV04 16:00 MC1 R, DETACHED FROM WORK ORDER 00027509. INSPECTION COMPLIED WITH AT TAP; AWAITING FAA APPROVAL TO UPDATE THE OPS SPEC. ENT BY: 067708 LT WING, REPAIRS (2 EA) LT INBD FLAP T/E LOCATED ON EITHER SIDE OF INBD CANNOE. EXISTING COMPOSITE REPAIRS PERFORMED IAW EA 6-5500-50325, DATED 06/23/2000. REPAIRED IAW EA 6-5750-81810.

Part: FAIRING — DAMAGED (T/E FLAP) · airframe 53,592 hrs · 17,963 cycles

REPAIR, NR 2 FLAP TRACK MOVABLE FAIRING. COMPLY WITH EA 6-5720-49992 REV NO POS P2 ENT BY: EMMD24 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 20OCT04 15:38:56:3 BY:195875 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 478289 ON: 31OCT04 20:45:04:9 S=M. COMPLIED WITH EA 6-5720-49992.

Part: FITTING — DAMAGED (A/C ACCESS DOOR) · airframe 53,592 hrs · 17,963 cycles

ACCOMPLISH MAINTENANCE "C" CHECK NR 003 ENT BY: 067708 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 29SEP04 14:53:57:6 BY:067708 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 162248 ON: 29OCT04 12:31:08:0 S=M. AIR COND SEVERAL HOLES OF FITTINGS AT ACCESS DOORS (147 CZ) TO AIR COND COMPT DAMAGED. REPAIRED IAW EA 6-5315-82534.

Part: SKIN — WORN (FUSELAGE) · airframe 53,592 hrs · 17,963 cycles

ACCOMPLISH MAINTENANCE "C" CHECK NR 003 ENT BY: 067708 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 29SEP04 14:53:57:6 BY:067708 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 162248 ON: 29OCT04 12:31:08:0 S=M. FUSELAGE, WEAR AT EXTERIOR FUSELAGE SKIN SURFACE ON FWD SURROUNDED OF FWD CARGO DOOR BETWEEN STRG 36 RT AND 39 RT. REPAIRED IAW EA 6-5310-81816.

Part: STRUCTURE — MISREPAIRED (VERTICAL STAB) · airframe 53,592 hrs · 17,963 cycles

VERTICAL STAB TOO LARGE COMPOSITE REPAIR ON LT SIDE L/E. EXISTING COMPOSITE REPAIRS PERFORMED IAW EA 6-5500-50375, DATED 06/23/2000. DAMAGED STEEL COVER WAS REPAIRED BY NEW ONE, IAW EA 6-5500-50375.

Part: FAIRING — DAMAGED (NR 2 PYLON) · airframe 53,592 hrs · 17,963 cycles

ACCOMPLISH MAINTENANCE "C" CHECK, 003 ENT BY: 067708 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 29SEP04 14:53:57:6 BY:067708 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 162248 ON: 29OCT04 12:31:08:0 S=M. PYLON NR 2, LOWER AFTER FAIRING WITH INTERIM REPAIR ON OUTER SKIN SURFACE LT AT AFT AREA. REPAIRED IAW EA 6-5480-81814.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 53,592 hrs · 17,963 cycles

PYLON LOWER SPAR, INSP FOR COMPLY WITH E.O. 6-5450-7-3302 REV NO. B3 POS PT3 ENT BY: 067708. NR 1 PYLON, LOWER AFT FAIRING WITH LOOSE RVTS, CRK'D AND PAINT IN BAD CONDITION. LOWER FAIRING REPAIRED IAW EA 6-5480-81814. REINSTALLED IAW AMM 54-55-00. PAINTED IAW SRM 51-75-10.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 53,592 hrs · 17,963 cycles

COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1 ENT BY: 067708 INFO 24 NOV0 16:00 MC1 R. DETACHED FROM WORK ORDER 00027509. INSPECTION COMPLIED WITH AT TAP; AWAITING FAA APPROVAL TO UPDATE THE OPS SPEC ENT BY: 067708. REPAIR APPROX FS 59 FWD OF RT AFT CARGO DOOR (LWR) NOT LISTED ON FEDEX MAJOR REPAIR REPORT. REPAIR PERFORMED IAW EA 6-5317-40001, DATED FROM 09/22/98.

Part: SKIN — DAMAGED (TE FLAP) · airframe 53,592 hrs · 17,963 cycles

REPAIR RT OUTBOARD TE FLAP LOWER SURFACE OUTBOARD OF NR 2 CANOE FAIRING. REPAIRED IAW EA 6-2750-50362, DATED JUNE/16/2000.

Part: SKIN — ACTIVATED (T/E FLAP) · airframe 53,592 hrs · 17,963 cycles

COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 24NOV04 16:00 MC1 R. DETACHED FROM WORK ORDER 00027509. INSPECTION COMPLIED WITH AT TAP; AWAITING FAA APPROVAL TO UPDATE THE OPS SPEC. ENT BY: 067708. REPAIR RT INBD FLAP UPPER SURFACE ON INBD SIDE. INBOARD, REPAIRED IAW SRM 57--, FIG 202. OUTB, REPAIRED IAW EA 6-5750-81811.

Part: STRUCTURE — GOUGED (THRUST REVERSER) · airframe 53,592 hrs · 17,963 cycles

NR 1 ENGINE, THRUST REVERSER RT FOUND WITH WEAR CLOSE TO BREATHER. ACCOMPLISHED IAW EA 6-7830-81809.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 53,592 hrs · 17,963 cycles

COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 24NOV04 16:00 MC1 R. INSPECTION COMPLIED WITH AT TAP; AWAITING FAA APPROVAL TO UPDATE THE OPS SPEC. ENT BY: 067708. RT WING REPAIR RT INBD FLAP LWR SURFACE. REPAIRED IAW EA 6-5750-81812.

Part: SWITCH — MALFUNCTIONED (NR 1 GENERATOR) · airframe 53,589 hrs · 17,961 cycles

RTD AT ESSA 19R FOR NR 1GEN FAULT AND MASTER CAUTION AT 60 KTS. ACCOMPLISHED RTO CKLST AND RETURNED TO GATE. NR 1 GEN, DID NOT AUTOCONNECT ON STARTUP, HAD TO ADVANCE THROTTLE AND RESET GEN 1 SW. ON TAXI BACK GEN 1 MADE CLICKING SOUND CONNECTING AND DISCONNECT SEVERAL TIMES AND FINALLY STAYED CONNECTED UNTIL SHUTDOWN. A/C RELEASED FOR SERVICE PER MEL 24-11-01. REMOVED AND REPLACED NR 1 GCU AS PER MM:24-22-12-4. NR 1 ENGINE RUN PERFORMED BY EMP NR 181214. NR 1 GEN CAME ON LINE NORMAL.

Part: INDICATOR — FALSE INDICATION (NR 1 ENG LOW OIL) · airframe 52,212 hrs · 17,039 cycles

IN CRUISE NR 1 ENGINE LOW OIL PRESS (32) ON ECAM. NO CONFIRMING LOW OIL PRESS LIGHT. ENGINE OPERATED AT IDLE. A/C DIVERTED TO EDDF. NR 1 OIL QUANTITY DROPPED 3 QTS OIL, TEMP WAS 30 DEGREES HIGH. MOMENTARY DC ELEC ADVISORY NR 1 AMPS FLUCTUATING. REMOVED AND REPLACED NR 1 MAIN OIL FILTER AS PER MM 79-21-03-4. NO DECONTAMINATION FOUND. REMOVED AND REPLACED LOW OIL PRESSURE TRANSMITTER AS PER MM 79-33-11-4. PERFORMED HIGH POWER ENGINE RUN PER JRH. ALL PARAMETERS NORMAL.

Part: VALVE — CRACKED (HYDRAULIC SYS) · airframe 50,608 hrs

ON T/O, BLUE RESERVOIR LOW AIR PRESSURE ECAM ILLUMINATED. REMOVED AND REPLACED MANIFOLD VALVE PER MM 29-32-13-4. REFILLED BLUE SYS. OPS AND LEAK CHECK NORMAL.

Part: PITOT LINE — DIRTY · airframe 49,968 hrs · 15,649 cycles

01-254 AIRSPEED IND ON T/O ROLL ON CAPT'S PFD IND. STBY A/S & F/O'S A/S IND 75-80 KNOTS. BLEW AIR INTO PITOT SYSTEM, DIRT CAME OUT. PERF LEAK CK OF ADC 1 PITOT LINE, AIRSPEED ON PILOTS PFD WORK NORM.

Part: LEVER — BROKEN (A/C SYSTEM) · airframe 49,682 hrs · 15,511 cycles

ON LD MIN EQUIP BAY SMOKE LIGHT ON ECAM. FAULT TRACED TO BROKEN CRANK AT DEFLECT. MAN SELECT HELD OPEN FAULT CLEARED. PACK OPS NORM.

Part: SLAT — MALFUNCTIONED (WINGS) · airframe 48,574 hrs · 14,967 cycles

AFT SLAT RETRACTION APPROX 10,000 MSL SLT SYS NR 1 FAULT LIGHT ON OVERHEAD PANEL ILL. PERF PROBLEM WIRING CK LT ASYM PPU PER WDM 27-81-05. ALL CONDITIONS NORM.

Part: PICKUP — FAILED (NR 1 SLAT) · airframe 48,574 hrs · 14,987 cycles

NR 1 SLAT SYSTEM FAULT. REMOVED AND REPLACED LT PPU PER MM 27-86-11-4. INSP AND CLEANED CANNON PLUG PER 27-84-00-5.

Part: FLAP — STUCK (WING) · airframe 48,351 hrs · 14,847 cycles

DURING NORMAL FLAPS EXT AT SLC, FLAPS STUCK IN FULL UP POSTION. SYS 1 & 2 FLAP FAULT LIGHT ON.

Part: O RING — LEAKS (GREEN HYD SYS)

99-198 - LOST GREEN HYD FLUID LOSS. REPLACED O-RING IN RETURN BOSS PER SMP REQUIRES LEAK CK AND INSP OF GREEN HYD SYS MM 29-00-00 PG 320.

Part: RETRACT MECH — MALFUNCTIONED (TE FLAPS)

ON FLAP EXT AT PHX WHEN EXTEND FLAPS FAULT LIGHT AND BOTH FLAP SYS FAULT LIGHT ILLUM ON OVHD IND FLAPS STUCK. C/W ECAM QRM PROCEDURE INCLUDES MOD SPD DUE TO LOSS OF A/S MOOK.