N817FD

Part: HINGE FITTING — NICKED (NLG DOOR) · airframe 35,177 hrs · 14,798 cycles

NOSE LANDING GEAR, RT AFT DOOR HINGE FITTING, BEARING HOLE FOUND TWO NICKS. REPAIRED IAW EA 6-5310-99725B PART 2.

Part: WIRE HARNESS — FAILED (MLG BRAKE) · airframe 34,746 hrs · 14,514 cycles

AFTER TOUCHDOWN, DURING ROLLOUT NR 5 AND NR 6 TIRES BLEW. ACFT REMAINED ON CENTERLINE. REMOVED AND INSTALLED AND ROUTED LT MLG HARNESS LOOM THRU NR 5 AND NR 6 BOGIES IN POSITION IAW MM 32-11-43-04.

Part: SHEAR PLATE — CORRODED (ZONE 400) · corrosion level 2 · airframe 33,840 hrs · 13,913 cycles

FWD END SHEAR PLATE FOUND CORRODED AT SEVERAL LOCATIONS FROM BS 410 TO 440, BL 0 TO LBL 24.75 FWD END SHEAR PLATE REPAIRED IAW EA F-5310-157901.

Part: COMPUTER — MALFUNCTIONED (FUEL QTY) · airframe 33,764 hrs · 13,861 cycles

APPROX 1.5 HRS INTO FLIGHT, RT OTBD FUEL TANK QTY BEGAN TO DECREASE RAPIDLY. TANK WENT TO EMPTY, XX, AND REMAINED UNTIL IN DESCENT AT 16,000 FT, THEN QTY RETURNED TO 6.42. TROUBLESHOOTING VERIFIED FUEL LEVEL IN RT OTBD TANK ON RT NR 2 & NR 3 MAGNETIC LEVEL INDICATORS IAW AMM 12-11-28-3. RESET FUEL QUANTITY COMPUTER OPS CHECKED GOOD IAW AMM 28-42-38-5. ACFT IS OK TO CONTINUE.

Part: FLOORBEAM — DAMAGED (ZONE 100) · airframe 33,239 hrs · 13,533 cycles

BULK CARGO COMPARTMENT, FR 63 FLOORBEAM BOTTOM CEILING PANEL ATTACHMENT BETWEEN SEAT TRACK 1 AND 2L HAS A DRILL START. COMPLIED WITH EA 6-5310-145342 PT1.

Part: SEAL — CRACKED (FUEL CELL) · airframe 33,239 hrs · 13,533 cycles

METALLIC VAPOR SEAL CRACKED ON LT SIDE AT FR 42-43, R & R METALLIC VAPOR SEAL ON LT SIDE FR 42-43.

Part: STRINGER — GOUGED (ZONE 100) · airframe 33,239 hrs · 13,533 cycles

AFT CARGO COMPARTMENT LT SIDE FWD OF FR 54.1, STR 37 HAS GOUGE. REMOVED, REPAIRED AND RE-INSTALLED STRINGER SECTION IAW SRM 53-10-14, PGS 201 THROUGH 231 SRM 51-21-10, PG 2, SRM 51-40-44, PG 1 AND SRM 51-75-10, PG 204.

Part: WEB — DAMAGED (CARGO BAY) · airframe 33,239 hrs · 13,533 cycles

AFT PIT FR 69 RBL 26 VERTICAL WEB PUNCTURED AT CARGO FLOOR LEVEL REMOVED AND REPLACED VERTICAL WEB AT FR 69 RBL 26 IAW SRM 51-40-21

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 33,239 hrs · 13,533 cycles

RIGHT SEAT TRACK NR6 BETWEEN FRAME 19 & 20 HAS CORRSION 1 SQ INCH. REMOVED LEVEL 1 CORROSION FROM RT NR 6 SEAT TRACK BETWEEN FRAME 19 & 20 AND FOUND BEYOND LIMITS IAW SRM 53-10-16. REPAIRED IAW EA 6-5310-145630.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,239 hrs · 13,533 cycles

MDC UNDERFLOOR TEE HAS 1 SQ INCH OF CORROSION FWD OF SEAT TRACK NR LT AT FR 12A. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. REMOVED AND REPLACED TEE FWD OF SEAT TRACK NR 3 AT FR 12A IAW SRM 51-72- 10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,239 hrs · 13,533 cycles

MDCC SEAT TRACK, NR 6, RT CORRODED INSIDE TRACK. REMOVED LEVEL 1 CORROSION ON SEAT TRACK NR 6 AT FR 19 AND FOUND TO BE OUT OF LIMITS IAW AIRBUS SRM 53-10-16. REPAIRED NR 6 SEAT TRACK AT FR 19 IAW EA 6-5310-145630.

Part: SEAT TRACK — CRACKED · airframe 33,239 hrs · 13,533 cycles

SEAT TRACK NR 3 LT CORRODED AT FR 19. REMOVED CORROISON FROM NR 3 SEAT TRACK AT FR 19 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REMOVED AND REPLACED NR 3 LT SEAT TRACK SECTION AT FR 19 IAW SRM 51-72-10.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 33,239 hrs · 13,533 cycles

MDC SEAT TRACK 5R HAS 2 GOUGES AT SCALLOPS, 1 AT 54.2 AND 1 7 INCHES AFT OF 54.2. BLENDED DAMAGED AREAS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 5R SECTION AT FR 54.2 INCLUDING 17 INCHES AFT OF FR 54.2.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 33,239 hrs · 13,533 cycles

SEAT TRACK 2R AT FRAME 54.2 HAS GOUGE AT SCALLOP. BLENDED GOUGED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 2R SECTION AT AT FR 54.2 IAW SRM 51-72-10.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 33,239 hrs · 13,533 cycles

SEAT TRACK 4L AT FRAME 54.3 HAS DAMAGE TO TACK AND SCALLOPS. BLENDED DAMAGED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 4L SECTION AT FR 54.3 IAW SRM 51-72-10.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 33,239 hrs · 13,533 cycles

2 EA GOUGES ON SEAT TRACK 3R FROM FRAME 54.2 TO FRAME 55/58. BLENDED GOUGED AREAS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 3R SECTION AT FR 54.2

Part: FITTING — CORRODED (NR 1 PYLON) · airframe 33,239 hrs · 13,533 cycles

NR 1 PYLON SPIGOT RECEPTACLE FITTING HAS PITTING CORROSION ON UPPER PLATE. REMOVED NR 1 PYLON IAW AMM 54-50-00-4. REMOVED AND REPLACED UPPER AND LOWER SPIGOT FITTINGS IAW S/B 54-2020 PARA B(6). REINSTALLED NR 1 PYLON IAW AMM 54-50-00-4. COMPLIED WITH EA-5450-1456609.

Part: FITTING — CORRODED (NR 2 PYLON) · airframe 33,239 hrs · 13,533 cycles

NR2 PYLON SPIGOT RECEPTACLE FITTING HAS PITTING CORROSION ON UPPER PLATE. REMOVED NR 2 PYLON IAW AMM 54-50-00-4 REMOVED AND REPLACED UPPER AND LOWER SPIGOT FITTING IAW S/B 54-20-20 PAR. B(6) REINSTALLED NR 2 PYLON IAW AMM 54-50-00-4 COMPLIED WITH FEDEX EA 6-5450-145609.

Part: SEAT TRACK — MISINSTALLED (ZONE 200) · airframe 33,239 hrs · 13,533 cycles

MAIN CABIN SEAT TRACK NR 2 LT Y450 BETWEEN FRAMES 47/48 TO 49 HAS AN EXISTING REPAIR WITH INCORRECT FASTENERS INSTALLED ON TOP FLANGE. REMOVED AND REPLACED 20 EACH RIVETS AND INSTALLED 20 EACH LOCK FASTENERS ON TOP FLANGE OF SEATTRACK REPAIR BETWEEN FRAMES 47/48 AND FR 49 ON NR 2 LT Y450 PER A310 SRM 53-10-16,FIG 205,PG 227 TO 232.

Part: BELLCRANK — DIRTY (LT MLG DOOR) · airframe 32,046 hrs · 12,779 cycles

LT MAIN GEAR DOOR WOULD NOT CLOSE ON T/O. RETURNED TO DEPARTURE. OPS CHECKED LT MLG DOOR IAW MM 32-12-11-5. OPS CHECKS NORMAL. DURING TROUBLESHOOTING, WERE ABLE TO DUPLICATE THIS PROBLEM BY OPERATING DOOR WITH GROUND CONTROL HANDLE, AFTER DISASSEMBLING, CLEANING AND LUBING OF GROUND CONTROL HANDLE BELLCRANK, DOOR OPERATION AND INDICATION NORMAL. WHEN GROUND CONTROL HANDLE WAS IN CLOSED POSITION, THE BINDING IN THE BELLCRANK DID NOT ALLOW THE DOOR SWITCHES TO MAKE CONTACT.

Part: IDG — UNDERSERVICED (NR 1) · airframe 31,385 hrs · 12,469 cycles

ON T/O ROLL AT APPROX 80 KNOTS RECEIVED ECAM ALERT, NR 1 IDG OIL PRESS W/ GEN 1 FAULT. RTO AND RETURNED TO BLOCKS. GEN 1 FAULT CLEARED BUT IDG NR1 FAULT KEPT FLICKERING. SERVICED NR 1 ENG IDG IAW AMM 12-13-24-0. RAN NR 1 ENG IAW JRH CHAP 5. NO LEAKS NOTED, OPS CK GOOD, ACFT OK FOR SERVICE.

Part: BUSHING — DAMAGED (ZONE 100) · airframe 30,877 hrs · 12,162 cycles

MAIN FRAME RT NOSE LANDING GEAR BEARING FITTING INSPECTION PER EA T6-5310-99725A, REQUIRES REMOVAL OF REPAIR BUSHING FOR INSPECTION. REMOVED REPAIR BUSHING, FABRICATED REPLACEMENT REPAIR BUSHING AND INSTALLED IAW FEDEX EA 6-5310-99725A, RELEASE DATE 07/20/06.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 30,877 hrs · 12,162 cycles

MAIN DECK CARGO COMPT SEAT TRACK NR 2 RT, 12 IN AFT OF FR 43 HAS 2 DAMAGED SCALLOPS. REMOVED DAMAGED SECTION OF SEAT TRACK NR 2 RT. FABRICATED REPLACEMENT SECTION AND INSTALLED BETWEEN FR 40 AND FR 45 IAW A310 SRM 53-10-16 AND SRM 51-40-21.

Part: TRANSMITTER — INOPERATIVE (HYD SYSTEM) · airframe 30,492 hrs · 11,851 cycles

ON FINAL APPROACH, RECEIVED SLAT SYS 1 AND 2 FAULT FOLLOWED UP SHORTLY W/GREEN HYD ECAM COMMAND TO TURN OFF BOTH GREEN HYD PUMPS. FAULTS ON OVERHEAD WERE AS FOLLOWS: GREEN SYS SERVO (GREEN PUMPS OFF), SLAT SYS 1 AND 2, SPOILER NR 5. DID GO AROUND FOUND RT MLG DOWNLOCK ACTUATOR FLEX HOSES LEAKING. RESERVOIR OVERSERVICED. DRAINED APPROX 3 GAL FROM GREEN SYS. REMOVED AND REPLACED GREEN SYS HYD XMITTER .25GQ. REF A310-300 MM 29-31-11-4, OPS AND LEAK CHECK NORMAL. STILL REQUIRES SERVICE AFTER OPS OF GREEN SYS. REMOVED AND REPLACED LEAKING DOWNLOCK HYD LINES. C/W LEAK CHECK AND OPERATIONAL CHECK OF GREEN SYSTEM HYDRAULICS. LEAK AND OPS CHECK GOOD. TOPPED OFF SYSTEM.

Part: HYDRAULIC SYSTEM — LOW (GREEN SYSTEM) · airframe 30,274 hrs · 11,679 cycles

REJECT T/O DUE TO ECAM: GREEN SYSTEM HYD QTY LOW. VERY COLD OUTSIDE AIR TEMP. PERFORMED VISUAL INSPECTION AND NO LEAKS FOUND. SERVICED GREEN HYD SYS PER SMP AND A310-300 AMM REF 12-12-29, SERVICED TWO QTS. A/C OK FOR SERVICE.

Part: SLIDE — LOW (ZONE 800) · airframe 29,273 hrs · 11,074 cycles

R1 DOOR ESCAPE SLIDE PRESSURE INDICATOR NOT IN GREEN BAND REMOVED AND REPLACED R1 DOOR ESCAPE SLIDE IAW A310-300 AMM 25-61-22-4-01 AND A310 - 300 AMM 52-10-00-3.

Part: FITTING — CORRODED (FUSELAGE) · airframe 29,000 hrs · 10,896 cycles

COMPLY WITH AGING 9-AGING-INSP, FOUND CORROSION AND WEAR LOCATED IN RT FITTING BETWEEN FS 16A/ FS 17 IN HOLE AT ATTACHMENT FITTING OF AFT DOOR.

Part: SKIN — DAMAGED (RT MLG DOOR) · airframe 29,000 hrs · 10,896 cycles

RT MLG-STRUT DOOR W/SKIN SURFACE DAMAGED AND REPAIR AT LOWER AREA THE STRUT DOOR WAS REPAIRED PER FEDEX EA 6-5280-99721 EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MINOR".

Part: DOOR — MISREPAIRED (APU) · airframe 29,000 hrs · 10,896 cycles

FOUND REPAIR LOCATED RT APU DOOR BETWEEN STA 4986/5003 FR 98. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO AN EXISTING SRM REPAIR . NEW REPAIR ACCOMPLISHED IN ACCORDANCE WITH FEDEX ENGENEERING AUTHORIZATION EA 6-5240-99732. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MINOR".

Part: NONE — NONE (NONE) · airframe 29,000 hrs · 10,896 cycles

NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR RT APU DOOR BETWEEN STA 4969/5001 FS 97/98. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND REPAIR ACCOMPLISHED USING FAA APPROVED DATA.

Part: SKIN — DAMAGED (RT MLG DOOR) · airframe 29,000 hrs · 10,896 cycles

FOUND REPAIR LOCATED MLG RT W/W DOOR AT INNER LOWER SKIN SURFACE AT OUTBD LOWER PART. REPAIR REQUIRE EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR W/W DOOR PER SRM 52-81-12. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 29,000 hrs · 10,896 cycles

FOUND REPAIR LOCATED RT ELEVATOR AT INNER LOWER SKIN STA 604/ER26 AND STA 566/ER 24. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 55-21-12 FIG 204. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: NONE — NONE (NONE) · airframe 29,000 hrs · 10,896 cycles

FOUND REPAIR LOCATED RT OUTB FLAP AT INNER LOWER SKIN SURFACE AT T/E OF INBD OF RIB 3. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.

Part: NONE — NONE (NONE) · airframe 29,000 hrs · 10,896 cycles

FOUND REPAIR LOCATED LT INBD FLAP AT T/E UPPER AND LOWER SKIN SURFACE BETWEEN RIB 5 AND RIB 8. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 29,000 hrs · 10,896 cycles

FOUND REPAIR LOCATED AT RT ELEVATOR AT INNER LOWER SKIN SURFACE STA 833/ER 38 AND STA 791/ ER36. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 55-21-12 FIG 204. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: NONE — NONE (NONE) · airframe 29,000 hrs · 10,896 cycles

NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. PREVIOUS REPAIR FOUND AT BULK COMP´T DOOR SKIN LOCATED AT BEAM 5. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR ACCOMPLISHED USING FAA DATA.

Part: NONE — NONE (NONE) · airframe 29,000 hrs · 10,896 cycles

NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT. FOUND REPAIR RT APU DOOR BETWEEN STA 4937/4969 FS 96/97 REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPROVED DATA.

Part: NONE — NONE (NONE) · airframe 29,000 hrs · 10,896 cycles

NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED LT APU DOOR BETWEEN STA 5033/5045 FS 99/99. REPAIR REQUIRES EVALUATION FOR MAJOR/ MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPROVED DATA.

Part: NONE — NONE (NONE) · airframe 29,000 hrs · 10,896 cycles

NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED LT FS4715/4760, FS 89/90, STRG 33/38 NEXT TO APU INLET. REPAIR REQUIRED EVALUATION FOR MAJOR/ MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.

Part: NONE — NONE (NONE) · airframe 29,000 hrs · 10,896 cycles

NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. PREVIOUS REPAIR FOUND AT FUSELAGE SKIN LOCATED BETWEEN FS 66/68 AND BETWEEN STRG 48/54 RT . REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR ACCOMPLISHED USING FAA DATA.

Part: NONE — NONE (NONE) · airframe 29,000 hrs · 10,896 cycles

COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED AT RT ELEVATOR AT INNER LOWER SKIN SURFACE STA 833/ ER 38 AND STA 791/ ER36. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.

Part: NONE — NONE (NONE) · airframe 29,000 hrs · 10,896 cycles

COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED MLG RT W/W DOOR AT INNER LOWER SKIN SURFACE AT OUTB LOWER PART. REPAIR REQUIRE EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.

Part: NONE — NONE (NONE) · airframe 29,000 hrs · 10,896 cycles

COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, FOUND REPAIR LOCATED RT INB FLAP AT INNER LOWER AND UPPER SKIN SURFACE AT T/E OF FLAP RIB 19. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 29,000 hrs · 10,896 cycles

PREVIOUS REPAIR FOUND AT BULK COMP´T DOOR SKIN LOCATED AT BEAM 5. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR ACCOMPLISHED USING FAA DATA EXISTING REPAIR COVERED BY RAS REF:RAS/DAHAM/4014519/2001. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: DOOR — MISREPAIRED (APU) · airframe 29,000 hrs · 10,896 cycles

FOUND REPAIR RT APU DOOR BETWEEN STA 4969/5001 FS 97/98. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR. 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 EA 6-5240-99732. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MINOR".

Part: SKIN — DAMAGED (T/E FLAP) · airframe 29,000 hrs · 10,896 cycles

FOUND REPAIR LOCATED RT INB FLAP AT INNER LOWER AND UPPER SKIN SURFACE AT T/E OF FLAP RIB 19. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR CONFORMS TO EXISTING FEDEX ENGINEERING AUTHORIZATION PER EA 6-5710-99724. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: SKIN — DAMAGED (T/E FLAP) · airframe 29,000 hrs · 10,896 cycles

FOUND REPAIR LOCATED RT OUTBD FLAP AT INNER LOWER SKIN SURFACE AND UPPER SKIN SURFACE OF T/E RIB 11/RIB 12. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 57-53-12 FIG 207. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MINOR".

Part: NONE — NONE (NONE) · airframe 29,000 hrs · 10,896 cycles

NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED RT APU DOOR BETWEEN STA 4986/5003 FR 98. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPROVED DATA.

Part: DOOR — MISREPAIRED (APU) · airframe 29,000 hrs · 10,896 cycles

FOUND REPAIR RT APU DOOR BETWEEN STA 4937/4969 FR 96/97 REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR. 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 EA 6-5240-99732 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MINOR".

Part: NONE — NONE (NONE) · airframe 29,000 hrs · 10,896 cycles

FOUND REPAIR LOCATED ON RT WING T/E WS 1625, RIB 26-27 BETWEEN OB FLAP AND WING TIP. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.

Part: NONE — NONE (NONE) · airframe 29,000 hrs · 10,896 cycles

COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED RT ELEVATOR AT INNER LOWER SKIN STA 604/ER26 AND STA 566/ER 24. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.

Part: SKIN — DAMAGED (T/E FLAP) · airframe 29,000 hrs · 10,896 cycles

FOUND REPAIR LOCATED INBD FLAP LT AT LOWER SURFACE AT RIB 8/ RIB 10. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR COVERED BY RAS REF : RAS /DA/BRE/1642/97, REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: STRUCTURE — UNKNOWN (RT WING) · airframe 29,000 hrs · 10,896 cycles

FOUND REPAIR LOCATED ON RT WING T/E WS 1625, RIB 26-27 BETWEEN OUTB FLAP AND WING TIP. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. THIS REPAIR WAS REMOVED AND REPLACED A NEW TRAILING EDGE PER SRM 51-72-10 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MINOR".

Part: NONE — NONE (NONE) · airframe 29,000 hrs · 10,896 cycles

NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED RT APU DOOR BETWEEN STA 5055/5065 FS 100/100. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPROVED DATA.

Part: NONE — NONE (NONE) · airframe 29,000 hrs · 10,896 cycles

COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED ON LT NR 2 SLAT SKIN SURFACE OF L/E BETWEEN RIB 44/45 (NEXT JACK RIB 4). REPAIR REQUIRES EVALUATION FOR MAJOR/ MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.

Part: SKIN — DAMAGED (T/E FLAP) · airframe 29,000 hrs · 10,896 cycles

FOUND REPAIR LOCATED LT INB FLAP AT T/E UPPER AND LOWER SKIN SURFACE BETWEEN RIB 5 AND RIB 8. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIR ACCOMPLISHED PER FEDEX ENG AUTH 6-5710-99724. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: NONE — NONE (NONE) · airframe 29,000 hrs · 10,896 cycles

NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. PREVIOUS REPAIR FOUND AT AFT COMP´T DOOR FRAME BETWEEN FS 63/64 AND STRINGER BETWEEN 40/44 RT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR ACCOMPLISHED USING FAA DATA.

Part: DOOR — MISREPAIRED (APU) · airframe 29,000 hrs · 10,896 cycles

FOUND REPAIR LOCATED LT APU DOOR BETWEEN STA 5033/5045 FS 99/99. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIR ACCOMPLISHED PER SRM 52-41-11 FIG 201. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MINOR".

Part: DOOR — MISREPAIRED (APU) · airframe 29,000 hrs · 10,896 cycles

FOUND REPAIR LOCATED RT APU DOOR BETWEEN STA 5055/5065 FS 100/100. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR 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 EA 6-5240-99732. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MINOR".

Part: NONE — NONE (NONE) · airframe 29,000 hrs · 10,896 cycles

COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED INBD FLAP LT AT LOWER SURFACE AT RIB 8/ RIB 10. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.

Part: SKIN — DAMAGED (T/E FLAP) · airframe 29,000 hrs · 10,896 cycles

FOUND REPAIR LOCATED RT OUTB FLAP AT INNER LOWER SKIN SURFACE AT T/E OF INDB OF RIB 3. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR 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 207. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MINOR".

Part: NONE — NONE (NONE) · airframe 29,000 hrs · 10,896 cycles

NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. PREVIOUS REPAIR FOUND AT FUSELAGE SKIN LOCATED BETWEEN FS 64/67 AND BETWEEN STRG 33/40 RT . REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR ACCOMPLISHED USING FAA DATA.

Part: SKIN — DAMAGED (L/E SLAT) · airframe 29,000 hrs · 10,896 cycles

FOUND REPAIR LOCATED ON LT NR 2 SLAT SKIN SURFACE OF L/E BETWEEN RIB 44/45 (NEXT JACK RIB 4). REPAIR REQUIRES EVALUATION FOR MAJOR/ MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR, DISCREPANCY REPORT 43000001-391 (010) REPAIR EVALUATED PER GMM 6-20-100 AND CLASSIFIED AS "MAJOR".

Part: NONE — NONE (NONE) · airframe 29,000 hrs · 10,896 cycles

COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED RT OUTB FLAP AT INNER LOWER SKIN SURFACE AND UPPER SKIN SURFACE OF T/E RIB 11/RIB 12. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.