N668FE

Part: NONE — NONE (N/A) · airframe 34,354 hrs · 19,376 cycles

PDIS 668 29-02 4189 29DEC21 MEM OPEN U ON DECENT IN TO MEM, ECAM ALERTED GREEN SYSTEM QUANTITY LOW, COMPLIED AND TURNED BOTH GREEN PUMPS. FOLLOWED ECAM AND QRH, DECLARED EMERGENCY, CRANKED THE GEAR DOWN AND LANDED UNEVENTFULLY. ENT BY: 228808 RPT BY:228808 INFO 29DEC21 15:41 MEM R ********************MOCC UPDATE******************** PLEASE WORK IN CONJUNCTION WITH TSI: 29-01/4149 *************THANKS MOCC TECH SERVICES************* SHGN 30DEC21 00:59 MEM FOUND ELECTROHYDRAULIC VALVE(3GA) LEAKING IN CENTER WHEELWELL FACT 30DEC21 02:59 MEM REMOVED AND REPLACED PACKING ON PORT C OF LANDING GEAR SELECTOR VALVE IN REF WITH AMM 32-31-12-04. LEAK CHECKED GOOD AT THIS TIME. O-RING/ PACKING, PROPONENT, P/N NAS1612-16A, S/N N/A FOR PACKINGS.

Part: INDICATION SYS — MALFUNCTIONED (PAX DOOR) · airframe 33,716 hrs · 18,978 cycles

DOORS DONT SHOW ARMED ON ECAM WHEN HANDLE IS PLACED IN ARMED POSITIONS BOTH LEFT AND RIGHT CREW DOORS PART 18JUN21 23:05 MEM U IDENTIFIED PARTS EMER POWER SUPPLY BATTERY. RELEASED FOR SERVICE PER MEL : 52-30-04 CATEGORY : C EXPIRATION : 28JUN21 "MEL 52-30-04: ECAM SLIDE INDICATION SYSTEM FOR (IDENTIFY L1 OR R1) R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE." PERFORMED ASPSU OPS CHECK REF A300 M/M 52-73-00-5 AND L1 DOOR ARMED INDICATION AND RESIDUAL PRESSURE LIGHT AND WARNING CHECKED NORMAL. R1 DOOR ARMED INDICATION STILL REMAIN INOP, TRANSFERRED R1 ECAM SLIDE INDICATION TO MEL. A/C OK TO CONT. RAN TSM 52-70-00 FIG 103 AND CLOSED AND ARMED SEVERAL TIMES SYSTEM OP CK OK AT THIS TIME.

Part: VALVE — FAILED (MLG) · airframe 33,405 hrs · 18,776 cycles

PDIS 668 32-30 3276 20MAR21 GSO ON APPROACH TO KGSO THE GEAR DID NOT EXTEND IN SYS 2. THERE WAS NO ECAM MESSAGE. THE ONLY INDICATION WE RECEIVED WERE THREE UNLK LIGHTS ON THE LANDING GEAR PANEL AND OVERHEAD PANEL. THERE WAS NO NOISE INDICATING GEAR MOVEMENT. WE DISCONTINUED THE APPROACH. FOUND A SAFE AREA TO WORK THE PROBLEM. WE TRIED SYS 1 AND HAD SOME INDICATIONS. NEVER IN EITHER POSITION DID WE GET THE SOUND OF GEAR OR GEAR DOORS MOVING. WE DECLARED AN EMERGENCY WITH ATC. TALKED WITH MAINTENANCE , OPS & GOC. AFTER SEVERAL MINUTES THE ECAM DIRECTED US TO LANDING GEAR GRAVITY EXTENSION CHECKLIST. WE ACCOMPLISHED THIS AND LANDED. SHGN 21MAR21 05:14 GSO RMVD AND RPLD LANDING GEAR SELECTOR VALVE 3GA AS PER AMM 32-31-12-04. NEEDS LK CKED AND TESTED AS PER AMM 32-31-12-06. FACT 21MAR21 23:04 GSO COMPLIED WITH GEAR SWING IN BOTH POSTION 1 AND 2 PER MM 07-11-00-00 (JACKING OF AIRCRAFT) AND 32-31-00-05 ( NORMAL EXTENSION AND RETRACTION ) NO DEFECTS NOTED ALL INDICATIONS SATISFACTORY A/C OK FOR SERVICE.

Part: STRUCTURE — DAMAGED (RT ELEVATOR) · airframe 32,733 hrs · 18,391 cycles

RT ELEVATOR HAS AN IR INDICATION (POSSIBLE WATER) 33" FROM THE INBOARD EDGE OF ER 2 AND 13" FROM THE T/E. INDICATION HAS THE SAME IR SIGNATURE AS A NEARBY REPAIR. HOWEVER, THERE IS NO VISUAL INDICATION OF A REPAIR IN THE AREA OF THE INDICATION. REPAIRED RT ELEVATOR WATER INGRESS, IAW SRM 55-21-12 PAR 5 H. MAJOR REPAIR, CAT A.

Part: WEB — CRACKED (FRAME 47) · airframe 32,733 hrs · 18,391 cycles

DURING THE ACCOMPLISHMENT OF STEP (9)(C) OF EO 6-5710-E0342809 P5 (LT WING), A CRACK NDICATION WAS NOTED APPROXIMATELY .500" FROM THE BOTTOM OF HOLE G AT THE 7 O'LOCK POSITION. CRACK MEASURES APPROXIMATELY .500" IN LENGTH. COMPLIED WITH EA 6-5700-T0356307 P1, TITLE: WING-GENERAL-CENTER WING REPAIR-SB A300-57-6049 AND A300-57-6086 FR47 CRACK HOLE G LT. MAJOR REPAIR, CAT A.

Part: WEB — CRACKED (NR 2 NACELLE) · airframe 32,733 hrs · 18,391 cycles

NR 2 ENG PYLON UPPER FAIRING WEB BETWEEN RIB A11 AND RIB J08 CRACKED. REPAIRED CRACKED WEB BETEEN RIB 11 & 8 ON NR 2 ENG PYLON UPPER FAIRING, IAW SRM 54-52-11 FIG 201 SHEET 1. MAJOR REPAIR (CAT A).

Part: FLOOR PANEL — GOUGED (ZONE 200) · airframe 32,733 hrs · 18,391 cycles

ZONE 230 TOP OF FLOOR BOARD 231CF IS GOUGED. FABRICATED ZONE 230 FLOOR BOARD 231CF ON TRAVELER T20/1508545 IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 32,733 hrs · 18,391 cycles

ZONE 230 FLOOR BOARD 231LG IS BROKEN. FABRICATED ZONE 230 FLOOR BOARD 231LG ON TRAVELER T20/1508459 IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 32,733 hrs · 18,391 cycles

ZONE 230 FLOOR BOARD 232JG IS DELAMINTED. FABRICATED ZONE 230 FLOOR BOARD 232JG ON TRAVELER T20/1508455 IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 32,733 hrs · 18,391 cycles

ZONE 230 FLOOR BOARD 232NG EMBEDDED DEBRIS ON TOP OF BOARD. FABRICATED ZONE 230 FLOOR PANEL 232NG ON TRAVELER T20/1508460 IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 32,733 hrs · 18,391 cycles

ZONE 230 FLOOR BOARD 232LG IS BROKEN. FABRICATED ZONE 230 FLOOR BOARD 232LG ON TRAVELER T20/1508456 IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 32,733 hrs · 18,391 cycles

ZONE 260 FLOOR BOARD 262XF IS BROKEN. FABRICATED ZONE 260 FLOOR BOARD 262XF ON TRAVELER T20/1508458 IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 32,733 hrs · 18,391 cycles

ZONE 230 FLOOR BOARD 232YG BROKEN. FABRICATED ZONE 230 FLOOR BOARD 232YG ON TRAVELER T20/1508457 IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 32,733 hrs · 18,391 cycles

AFT PIT FLOOR PANEL 151RF IS DAMAGED. FABRICATED AFT PIT FLOOR PANEL 151RF ON VTMAE TRAVELER NR T20/1507606 PER DWG SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 32,733 hrs · 18,391 cycles

FWD PIT FLOOR PANEL 132LG IS BROKEN. FABRICATED FWD PIT FLOOR PANEL 132LG ON VTMAE TRAVELER # T20/1507567 PER DWG SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 32,733 hrs · 18,391 cycles

BULK CARGO COMPT. FLOOR PANEL 161JF IS DELAMINATED. FABRICATED BULK CARGO COMPT. FLOOR PANEL 161JF ON VTMAE TRAVELER # T20/1507615 PER DWG SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FWD CARGO BAY) · airframe 32,733 hrs · 18,391 cycles

FWD PIT FLOOR PANEL 131QG IS BROKEN. FABRICATED FWD PIT FLOOR PANEL 131QG ON VTMAE TRAVELER # T20/1507578 PER DWG SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (FWD CARGO BAY) · airframe 32,733 hrs · 18,391 cycles

FWD PIT FLOOR PANEL 132MG IS DELAMINATED. FABRICATED FWD PIT FLOOR PANEL 132MG ON VTMAE TRAVELER # T20/1507565 PER DWG SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (FWD CARGO BAY) · airframe 32,733 hrs · 18,391 cycles

FWD PIT FLOOR PANEL 131KG IS DAMAGED AND DELAMINATED. FABRICATED FWD PIT FLOOR PANEL 131KG ON VTMAE TRAVELER # T20/1507577 PER DWG SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 32,733 hrs · 18,391 cycles

BULK CARGO COMPT. FLOOR PANEL 161CF IS DELAMINATED. FABRICATED BULK CARGO COMPT. FLOOR PANEL 161CF ON VTMAE TRAVELER # T20/1507603 PER DWG SRZ-25-005. MAJOR REPAIR.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 32,556 hrs · 18,277 cycles

FUSELAGE, FIRST OFFICER'S WINDOW FRAME 4R GUSSET, REPAIR OF CRACKS FOUND DURING. COMPLY WITH EA 6-5310-T0354515 REV NR POS P1. ATTACHED TO WORK ORDER 00077674. COMPLIED WITH EA 6-5310-T0354515. INSTALLED NEW GUSSET.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 32,556 hrs · 18,277 cycles

FUSELAGE, CAPTAIN'S WINDOW FRAME 4L GUSSET. REPAIR OF CRACKS FOUND DURING WORK. COMPLY WITH EA 6-5310-T0354512 REV NR POS P1. ATTACHED TO WORK ORDER 00077674. COMPLIED WITH EA 6-5310-T0354512. INSTALLED NEW GUSSET.

Part: SERVO VALVE — FAILED (SPOILER) · airframe 32,533 hrs · 18,262 cycles

ON CLIMB OUT GOT 3&2 SPLR FAULT. COMPLIED WITH ECAM & QRH. LIGHT & FAULT CLEARED FOR REMAINDER OF FLIGHT UNTIL FLAPS 15 WAS SELECTED ON FINAL APPROACH. TRIED TO RESET, UNSUCCESSFUL AND NR 3 SPOILER SHOWED (AND CONFIRMED BY BUFFET AND ROLL) THAT IT WAS DEPLOYED OR UNLATCHED. RAN SPOILERS UP & DOWN SEVERAL TIMES. PERFORMED BITE TEST OF EFCU'S REF TSM 27-61-06. BOTH EFCU'S FAULTED 3L SERVO VALVE. REPLACED SPOILER 3L SERVO VALVE REF MM 27-64-12-04. NO LEAKS NOTED. OPS CKS NORMAL. NO FAULTS SHOWN ON ECAM/OVHD OR ON EFCU'S. A/C OK FOR SERVICE.

Part: SPOILER — DAMAGED (LT WING) · airframe 31,735 hrs · 17,768 cycles

ON POST FLIGHT WALK AROUND FOUND NUMBER FIVE (5) SPOILER DAMAGE, L/H WING BEGAN INSTALLATION OF SPOILER REF AMM 27-61-53-04 STEP C 1 THRU D (3) (C). COMPLETED INSTALLATION OF NR 5 LT SPOILER IAW AMM 27-61-53-04. OPS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (R1 DOOR) · airframe 30,917 hrs · 17,206 cycles

AFTER TAKEOFF THE R1 DOOR WAS RATTLING AND FLASHING RED LIGHT AND AURAL ALARM THE ENTIRE FLIGHT FROM MEM TO RSW. NO ECAM INDICATIONS UP FRONT. INSPECTED R1 DOOR PER MM 52-10-11-05-2 & VERIFIED NORMAL SMOOTH OPERATION & NORMAL COCKPIT INDICATIONS. UNABLE TO DUPLICATE. SUSPECT INSIDE DOOR HANDLE NOT FULLY PUSHED DOWN. A/C OK FOR SERVICE.

Part: HANDLE — OUT OF RIG (MAIN CARGO DOOR) · airframe 30,198 hrs · 16,583 cycles

ON LANDING, MAIN DECK CARGO DOOR ECAM ALERTED, MAIN DECK SWITCH FAULT, MAIN DECK NOT CLOSED. STAYED ON FOR REMAINDER OF TAXI IN. PERFORMED ADJUSTMENT/TEST OF MDC DOOR. FOUND INNER DOOR HANDLE OUT OF RIG AND PERFORMED ADJUSTMENT OF ROD 3 PER AMM 52-36-21-05. VERIFIED DOOR LOCKING MECHANISM NOW WITHIN RIG. HANDLE NOW HAS POSITIVE OVERCENTER AND TENSION PER AMM 52-36-21-05. NO OTHER DEFECTS NOTED. DOOR WARNING INDICATION SYSTEM OPS CHECKED NORMAL.

Part: FLOOR SUPPORT — CORRODED (FRAMES 11-18) · corrosion level 3 · airframe 30,053 hrs · 16,492 cycles

FWD MAIN DECK CARGO FLOOR SUPPORT UNDER LAV HAS CORRSION Y1456 FR11 TO FR14 REMOVED AND REPLACED MAIN DECK CARGO COMPT FLOOR SUPPORT FROM FR11 TO FR18 Y1456 IAW SRM 51-40-21 CORROSION FOUND OUT OF LIMITS IAW SRM 53-12-15. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (FRAME 78) · airframe 30,053 hrs · 16,492 cycles

MAIN DECK CARGO SEAT TRACK AND SCALLOP GOUGED, FRAME 78, Y0. REMOVED THE GOUGE AND FOUND OUT OF LIMITS IAW SRM 53-10-16, FIG 102. REMOVED THE SECTION OF THE SEAT TRACK IAW SRM 53-10-16. FABRICATED A REPAIR SECTION AND FOUR SPLICES IAW SRM 51-27-11. INSTALLED THE REPAIR SECTION IAW SRM 51-40-21 MAJOR REPAIR

Part: SHEAR PLATE — CRACKED (FRAMES 65-66) · airframe 30,053 hrs · 16,492 cycles

AFT CARGO LT SHEAR WEB CRACKED AT FRAMES 65 TO 66. REMOVED AND REPLACED THE SHEAR WEB IAW SRM 51-40-21, SRM 51-40-44, SRM 51-21-10. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 30,053 hrs · 16,492 cycles

FWD CARGO FLOOR PANEL 132PG EDGE DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 30,053 hrs · 16,492 cycles

FWD CARGO FLOOR PANEL 132SG CRACKED. FABRICATED A NEWFLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 30,053 hrs · 16,492 cycles

FWD CARGO FLOOR PANEL 131SG HAD EDGE DAMAGE. FABRICTED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 30,053 hrs · 16,492 cycles

AFT CARGO FLOOR PANEL 151TF EDGE DAMAGE. FABRICATED FLOOR PANEL 151TF ON T17/1317621 PER SRZ-25-005 CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 30,053 hrs · 16,492 cycles

AFT CARGO FLOOR PANEL 151UF EDGE DAMAGE. FABRICATED FLOOR PANEL 151UF ON T17/1317326 PER SRZ-25-005 CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 30,053 hrs · 16,492 cycles

FWD CARGO FLOOR PANEL 131RG HAD EDGE DAMAGE. FABRICATED A NEW FLOOR PANEL IAWSRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 30,053 hrs · 16,492 cycles

FWD CARGO FLOOR PANEL 131RG CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (FRAMES 13-18) · corrosion level 3 · airframe 30,053 hrs · 16,492 cycles

FWD MAIN DECK CARGO FLOOR SUPPORT UNDER LAV HAS CORROSION UPPER CHORD Y1959 FROM FR13 TO FR13B. REMOVED AND REPLACED MDCC FLOOR SUPPORT UPPER CHORD FROM Y1959 FR13 TO FR18 IAW SRM 51-40-21. CORROSION FOUND OUT OF LIMITS IAW SRM 53-12-15.

Part: FLOOR PANEL — PUNCTURED (FWD CARGO) · airframe 30,053 hrs · 16,492 cycles

FWD CARGO FLOOR PANEL 131MG PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 30,053 hrs · 16,492 cycles

MAIN DECK CARGO COMPT 241RJ FLOOR PANEL BROKEN. FABRICATED FLOOR PANEL 241RJ ON T17/1317474 PER DWG SRZ-25-005 CAT "A" MAJOR REPAIR.

Part: BRACKET — CORRODED (FRAMES 26-28) · corrosion level 3 · airframe 30,053 hrs · 16,492 cycles

FWD MDC PRESSURE DECK PLATE HAS CORROSION BETWEEN FRAMES 26 TO 28, -Y1456 TO -Y1959. REMOVED AND REPLACED THE TWO THRUST BRACKETS IAW SRM 51-40-21. FABRICATED THE THRUST BRACKETS IAW DWG A5378198 AND SRM 53-14-15. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 30,053 hrs · 16,492 cycles

AFT CARGO FLOOR PANEL 151SF EDGE DAMAGE FABRICATED FLOOR PANEL 151SF ON T17/1317256 PER SRZ-25-005 CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (MAIN CARGO) · airframe 30,053 hrs · 16,492 cycles

MAIN DECK CARGO FLOOR PANEL 231CF BROKEN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 30,053 hrs · 16,492 cycles

AFT CARGO FLOOR PANEL 152XF EDGE DAMAGE. FABRICATED FLOOR PANEL 152XF ON T17/1317235 PER SRZ-25-005 CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 30,053 hrs · 16,492 cycles

FWD CARGO FLOOR PANEL 131QG FOUND CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 30,053 hrs · 16,492 cycles

AFT CARGO FLOOR PANEL 152UF EDGE DAMAGE. FABRICATED FLOOR PANEL 152UF ON T17/1317334 PER SRZ-25-005 CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 30,053 hrs · 16,492 cycles

AFT CARGO FLOOR PANEL 151MF HAD EDGE DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (COURIER) · airframe 30,053 hrs · 16,492 cycles

COURIER FLOOR PANEL 221 HF PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DRAWING SRZ 25-005, REV M. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 30,053 hrs · 16,492 cycles

FWD CARGO FLOOR PANEL 131LG CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 30,053 hrs · 16,492 cycles

FWD CARGO FLOOR PANEL 132LG CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (FWD CARGO) · airframe 30,053 hrs · 16,492 cycles

FWD CARGO FLOOR PANEL 131KG PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 30,053 hrs · 16,492 cycles

AFT CARGO FLOOR PANEL 152PF WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (COURIER) · airframe 30,053 hrs · 16,492 cycles

COURIER FLOOR PANEL 221RF PUNCTURED AND HAD DAMAGED INSERTS. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005, REV M. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (COURIER) · airframe 30,053 hrs · 16,492 cycles

COURIER FLOOR PANEL 222NF PUNCTURED AND CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25- 005, REV M. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 30,053 hrs · 16,492 cycles

AFT CARGO FLOOR PANEL 151WF HAD EDGE DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAR.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 30,053 hrs · 16,492 cycles

FWD CARGO FLOOR PANEL 132NG CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (COURIER) · airframe 30,053 hrs · 16,492 cycles

COURIER FLOOR PANEL 222QF GOUGED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005, REV M. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 30,053 hrs · 16,492 cycles

COURIER FLOOR PANEL 221QF PUNCTURED AND HAD DAMAGED INSERTS. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005, REV M. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 30,053 hrs · 16,492 cycles

FWD CARGO FLOOR PANEL 131NG CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 30,053 hrs · 16,492 cycles

AFT CARGO FLOOR PANEL 152WF HAD EDGE DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 30,053 hrs · 16,492 cycles

FWD CARGO FLOOR PANEL 132QG CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (COURIER) · airframe 30,053 hrs · 16,492 cycles

COURIER FLOOR PANEL 221LF DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25- 005, REV M. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 30,053 hrs · 16,492 cycles

AFT CARGO FLOOR PANEL 152TF HAD EDGE DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (COURIER) · airframe 30,053 hrs · 16,492 cycles

COURIER FLOOR PANEL 221 MF PUNCTURED AND CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005, REV M. MAJOR REPAIR.

Part: TRANSFORMER — FAILED · airframe 28,526 hrs · 15,603 cycles

AT ROTATION, ACARS SHOWED ZERO OIL PRESSURE ON NR 2 ENGINE AND NR 2 PITCH TRIM KICKED OFF. AIRBORNE, ACARS SHOWED ADC 2 INOPERATIVE. MULTIPLE SPOILER FAULTS. NR 2 PITCH FAULT & NR 2 ANALOG GAUGE AS WELL. DECLARED EMERGENCY & LANDED. FOUND CIRCUIT BREAKER 6XN OPEN. UNIT MECHANICALLY WEAK & EASY TO OPEN. R & R THE CIRCUIT BREAKER & 18XN AUTO TRANSFORMER, PERFORMED SATISFACTORY PITCH TRIM, ADC 2, STBY AOA, & AFS/AUTOLAND TESTS. IAW ESPM 20-46-10, AMM 24-51-11-04, 22-27-00-05, 34-11-34-04, 22-27-39-04, 22-40-00-05, 25-11-13-04 & SSM 24-51-00, 24-58-24 & 24-57-00. PERFORMED NR 2 ENG RUN IAW JRH. BOTH ECAM & ANALOG OIL PRESSURE INDICATIONS NORMAL. OTHER PARAMATERS NORMAL. OPS CHECKED GOOD.

Part: SWITCH — DIRTY (NLG) · airframe 27,411 hrs · 14,948 cycles

ON GEAR EXTENSION AT 180 KTS, NOSE GEAR DOOR DID NOT CLOSE ON BOTH 1 & 2 SYS FACT 09 DEC 15 12:06. PIT U DOORS IN CLOSED POSITION UPON ARRIVAL. CYCLED NOSE GEAR DOORS & LIGHT EXTINGUISHED. CLEANED DOOR SWITCHES & TESTED NOSE GEAR DOOR SYS IAW MM 32-31-00-5 3 D B. SYS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 273 hrs · 14,926 cycles

DURING DEPARTURE, NR 2 PRESSURE REGULATOR FAILED SHORTLY FOLLOWED BY NR 1 REGULATOR FAILING. CABIN CLIMBED UNCONTROLLABLY, STOPPED CLIMB AT 10K OR BELOW. ECAM DISPLAYED AFT OUT FLOW VALVE FULLY OPEN. SELECTED OUTFLOW VALVE OFF, CABIN PRESSURIZED NORMALLY WITH NO SYS FAULTS. COMPLIED WITH ECAM & QRH PROCEDURES. IAW AMM 21-31-12-04 REPLACED AFT OUT FLOW VALVE. PERFORMED ALL REQUIRED TEST IN BOTH NR 1 & 2 SYSTEMS, NO FAULTS NOTED.

Part: FLOORBEAM — CORRODED (FRAME 40) · corrosion level 2 · airframe 270 hrs · 14,709 cycles

MAIN DECK CARGO COMPARTMENT, FLOOR PANEL BEAM BRACKET AT FRAME 40 BETWEEN Y953 & Y1456 HAS CORROSION. REMOVED CORROSION ON FLOORBEAM CROSSBEAM IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW SRM 53-15-15 FIG 7. FABRICATED NEW CROSSBEAM ON T15 1151895 IAW SRM 53-15-15. R & R CROSSBEAM IAW SRM 51-40-21. MAJOR REPAIR.

Part: CARGO TRACK — CORRODED (FRAMES 41-45) · corrosion level 2 · airframe 270 hrs · 14,709 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT -Y1456, BETWEEN FRAME 41 & 45 HAS CORROSION IN 3 PLACES. R & R SEAT TRACK AT -Y1456, BETWEEN FRAME 41 & 45 IAW SRM 51-40-21. CLASSIFIED CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 252 HH, LT SIDE 1 EA FASTENER HOLE ELONGATED. FABRICATED NEW PANEL ON T15 1152421 IAW DWG SRZ-25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 270 hrs · 14,709 cycles

MAIN DECK FLOOR PANEL 252 XG DAMAGED. FABRICATED NEW PANEL ON T15 1151522 IAW DWG SRZ-25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 270 hrs · 14,709 cycles

MDCC FLOOR SUPPORT Y232, FRAME 11 TO 13, CORRODED AT 2 EACH LOCATIONS. R & R FLOOR SUPPORT PN A5361221420001, BATCH 2821031 IAW SRM 51-40-21 & SRM 51-40-44.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 261 AH HAS MISSING INSERT. FABRICATED NEW PANEL ON T15 1152422 IAW DWG SRZ-25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 251 BH TOP SURFACE HAS CRACK & 1 EACH INSERT DAMAGE. FABRICATED NEW PANEL ON T15 1151859 IAW DWG SRZ-25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 251 XG LT FWD EDGE CORNER HAS DAMAGE. FABRICATED NEW PANEL ON T15 1151857 IAW DWG SRZ-25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 252 LG 1 EACH FASTENER HOLE ELONGATED, FWD CORNER RT SIDE. FABRICATED NEW PANEL ON T15 1152417 IAW DWG SRZ-25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 262 PF HAS MISSING INSERT. FABRICATED NEW PANEL ON T15 1152423 IAW DWG SRZ-25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 251 RT TOP SURFACE HAS PUNCTURED. FABRICATED NEW PANEL ON T5 1152419 IAW DWG SRZ-25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 252 BF TOP SURFACE HAS CRACKS 2 PLACES. FABRICATED NEW PANEL ON T15 1152418 IAW DWG SRZ-25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 251 MG BOTTOM SURFACE HAS PUNCTURE. FABRICATED NEW PANEL ON T15 152416 IAW DWG SRZ-25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 251 DH, RT FWD CORNER FASTENER HOLE ELONGATED & EDGE CORNER HAS DAMAGE. FABRICATED NEW PANEL ON T15 1152420 IAW DWG SRZ-25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 270 hrs · 14,709 cycles

MAIN CABIN FLOOR PANEL 242ZH PUNCTURED. FABRICATED NEW PANEL ON T15 1151077 IAW DWG SRZ-25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 270 hrs · 14,709 cycles

MAIN CABIN FLOOR PANEL 252VF DAMAGED. FABRICATED NEW PANEL ON T15 1151521 IAW DWG SRZ-25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 270 hrs · 14,709 cycles

MAIN CABIN FLOOR PANEL 252PH DAMAGED. FABRICATED NEW PANEL ON T15 1151509 IAW DWG SRZ-25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 270 hrs · 14,709 cycles

MAIN CABIN FLOOR PANEL 252DH DAMAGED. FABRICATED NEW PANEL ON T15 115508 IAW DWG SRZ-25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 242MF, TOP SURFACE HAS PUNCTURED & EDGE CORNER DAMAGE. FABRICATED NEW PANEL ON T15 1151855 IAW DWG SRZ-25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 252 YG TOP SURFACE HAS CRACK. FABRICATED NEW PANEL ON T15 1151858 IAW DWG SRZ-25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 242SF TOP SURFACE HAS PUNCTURE & CRACK. FABRICATED NEW PANEL ON T15 1151507 IAW DWG SRZ-25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 270 hrs · 14,709 cycles

MDCC SEAT TRACK AT -Y1456 A BIT FWD OF FRAME 40 HAS CORROSION. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS D=0.046" L=3" W=1.125". REMOVED SEAT TRACK IAW 51-40-21. LOCATED & DRILLED HOLES AT NEW SEAT TRACK IAW SRM 51-40-44. INSTALL NEW SEAT TRACK IAW SRM 51-40-21. TOP COAT IAW SRM 51-75-10. CLASSIFIED AS CAT A MAJOR REPAIR.

Part: ADAPTER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 270 hrs · 14,709 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK FROM FRAME 35 - 36 AT -Y953 TO -Y450 HAS LIGHT SURFACE CORROSION. REMOVED 2 EACH LOCK FASTENERS FOR ACCESS TO CORROSION IAW SRM 51-40-21. REMOVED CORROSION IAW SRM 51-74-10, CHECKED LIMITS, MAT LOSS = 0.018", MAX ALLOWED 0.027". FOUND TO BE WITHIN LIMITS IAW SRM 53-10-15. REINSTALLED LOCK FASTENER AT FRAME 35 IAW SRM 51-40- 21. REMOVED CORROSION IAW SRM 51-74-10 AT FRAME 36 ADAPT. MAT LOSS = 0.030", MAX ALLOWED 0.027". FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15 FIG 101. REMOVED ADAPT IAW SRM 51-40-21, RECEIVED NEW ADAPT. PN A5378193720100 BA0002819812. INSTALLED NEW ADAPT IAW SRM 51-40-21. CLASSIFIED CAT A MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 241DF HAS CRACK & DAMAGE ON SEVERAL AREAS. FABRICATED NEW PANEL ON T15 1151505 IAW DWG SRZ-25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 270 hrs · 14,709 cycles

MAIN CABIN FLOOR PANEL 242EK CRACKED. FABRICATED NEW FLOOR PANEL ON T15 1151079 IAW DWG SRZ-25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 270 hrs · 14,709 cycles

MAIN CABIN FLOORBOARD 242 VG DAMAGED. FABRICATED NEW PANEL ON T15 1151523 IAW DWG SRZ-25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 241LJ, TOP SURFACE HAS PUNCTURE, DELAMINATION & MISSING INSERTS. FABRICATED NEW PANEL ON T15 1151852 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 270 hrs · 14,709 cycles

MAIN CABIN FLOOR PANEL 242UJ PUNCTURED. FABRICATED NEW PANEL ON T15 1151075 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 242 BF HAS BROKEN & MISSING WASHERS & INSERTS. FABRICATED NEW PANEL ON T15 1151506 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 270 hrs · 14,709 cycles

FORWARD CARGO FLOOR PANEL 132MG PUNCTURED. FABRICATED FLOOR PANEL 132MG ON T15 1150226 IAW DWG SRZ-25-005. CLASSIFIED AS CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 270 hrs · 14,709 cycles

FORWARD CARGO FLOOR PANEL 131KG DAMAGED & PUNCTURED. FABRICATED FLOOR PANEL 131KG ON T15 1150224 IAW DWG SRZ-25-005. CLASSIFIED AS CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 242BK EDGE CORNERS HAVE DAMAGE. FABRICATED NEW PANEL ON T15 1152395 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 242QF EDGE HAS CRACK, RT AFT. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 270 hrs · 14,709 cycles

MAIN CABIN FLOOR PANEL 242ZJ PUNCTURED. FABRICATED NEW PANEL ON T 15 1151076 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 242LK EDGE, CORNER HAS DAMAGE. FABRICATED NEW PANEL ON T15 1152397 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 270 hrs · 14,709 cycles

MAIN DECK CARGO FLOOR PANEL 241NJ CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 270 hrs · 14,709 cycles

FORWARD CARGO FLOOR PANEL 132KG PUNCTURED. FABRICATED PANEL 132KG ON T15 1150223 IAW DWG SRZ-25-0005. CLASSIFIED AS CAT A MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 242KJ, BOTTOM SURFACE HAS PUNCTURE. FABRICATED NEW PANEL ON T15 1152399 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 242LJ TOP SURFACE HAS PUNCTURES, 2 PLACES & EDGE CORNER DAMAGE. FABRICATED NEW PANEL ON T15 1151853 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 252 BH FWD EDGE & CUT OUT DAMAGED. FABRICATED NEW PANEL ON T5 1151860 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — CRACKED (FRAMES 51-54) · airframe 270 hrs · 14,709 cycles

MAIN CABIN FLOOR PANEL 241EK CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 241GJ TOP SURFACE HAS PUNCTURE & CRACKS. FABRICATED NEW PANEL ON T15 1152396 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 242QJ CRACKED & DAMAGED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 242FK EDGE CORNER HAS DAMAGE. FABRICATED NEW PANEL ON T15 1152415 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 241UH, TOP SURFACE HAS CRACKS & DELAMINATED 2 PLACES. FABRICATED NEW PANEL ON T15 1152400 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 270 hrs · 14,709 cycles

FORWARD CARGO COMPARTMENT, FLOOR PANEL 131PG CRACKED. FLOOR PANEL 131PG FABRICATED ON T15 1150257 IAW DWG SRZ-25-005. CLASSIFIED AS CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 270 hrs · 14,709 cycles

FORWARD CARGO FLOOR PANEL 131MG PUNCTURED. 131 MG FLOOR PANEL FABRICATED ON T15 1150225 IAW DWG SRZ-25-005. CLASSIFIED AS CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 241BF TOP SURFACE HAS PUNCTURE, 2 PLACES. FABRICATED NEW PANEL ON T15 1151851 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 270 hrs · 14,709 cycles

MAIN CABIN FLOOR PANEL 252VH DAMAGED. FABRICATED PANEL ON T15 1151510 IAW DWG SRZ-25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 242VH TOP SURFACE HAS CRACK. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 242TG, BOTTOM SURFACE HAS PUNCTURES IN 2 PLACES. FABRICATED NEW FLOOR PANEL ON T15 1152398 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN DECK) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 241AJ EDGES CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 241UJ TOP SURFACE CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 242AJ EDGE HAS CRACK AROUND THE FASTENER HOLE, FOUR PLACES. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 270 hrs · 14,709 cycles

MDCC FLOOR PANEL 241JF TOP SURFACE PUNCTURED & CRACKED 2 PLACES. FABRICATED NEW PANEL ON T15 1151854 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 270 hrs · 14,709 cycles

AFT CARGO FLOORBOARD 161GF DELAMINATED. FABRICATED FLOOR PANEL 161GF ON T15 1151323 IAW DWG SRZ 25-005 CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 270 hrs · 14,709 cycles

AFT CARGO FLOORBOARD 151UF DELAMINATED. R & R FLOOR PANEL 151UF IAW AMM 53-10-35-04. FABRICATED FLOOR PANEL 151UF ON T15 1151328 IAW SRZ 25-005 CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 270 hrs · 14,709 cycles

BULK CARGO FLOORBOARD 162HF HAS HOLES IN IT, METAL. R & R FLOOR PANEL 162HF IAW AMM 53-10-35-04. FABRICATED FLOOR PANEL 162HF ON T15 1151322 IAW SRZ 25-005 CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 270 hrs · 14,709 cycles

AFT CARGO FLOORBOARD 162EF DELAMINATED. R & R FLOOR PANEL 162EF IAW AMM 53-10-35-04. FABRICATED FLOOR PANEL 162EF ON T15 1151324 IAW SRZ 25-005 CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 270 hrs · 14,709 cycles

AFT CARGO FLOORBOARD 161BF DELAMINATED. FABRICATED FLOOR PANEL 161BF ON T15 1151326 IAW DWG SRZ 25-005 CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 270 hrs · 14,709 cycles

AFT CARGO FLOORBOARD 151WF DELAMINATED. FABRICATED FLOOR PANEL 151WF ON T15 1151327 IAW DWG SRZ 25-005 CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 270 hrs · 14,709 cycles

AFT CARGO FLOORBOARD 151VF DELAMINATED. FABRICATED FLOOR PANEL 151VF ON T15 1151329 IAW DWG SRZ-25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 270 hrs · 14,709 cycles

AFT CARGO FLOORBOARD 161AF DELAMINATED. FABRICATED FLOOR PANEL 161AF ON T15 1151325 IAW DWG SRZ-25-005. CAT A MAJOR REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 270 hrs · 14,709 cycles

RIGHT SIDE UPPER FUSELAGE SKIN HAS A PIN HOLE, FRAME 10 TO 10A, 23 " FROM CTR. REAMED LIGHTNING STRIKE PIN HOLE TO .128 IAW SRM 53-10-12 FIG 203. ROTO PROBED IAW NTM 51-10-01, NO DEFECT NOTED. INSTALLED REPAIR WASHED & FASTENER IAW SRM 53-10-12 FIG 203. PAINTED IAW SRM 51-75-10.

Part: SKIN — DENTED (FUSELAGE) · airframe 270 hrs · 14,709 cycles

PRIOR TO START OF LOADING, AMJ ON DOLLY STRUCK THE ACFT AT AREA APPROX 1 FOOT ABOVE & SLIGHTLY AHEAD OF LT STATIC PORT RED OUTLINE. NO RESTRICTION IAW 53-10-12 DENT WAS FOUND 1 FOOT ABOVE THE LT STATIC PORT RED OUTLINED AREA & IS WITHIN LIMITS IAW SRM 53-10-12 DIAGRAM 103 SHEET 1 FLAG NOTE 2 IAW ER 13-07745, EXTERNAL DVI USING 10X MAG GLASS CARRIED OUT OF DENT LOCATION WITH NO CRACKS FOUND, NO SKIN GOUGES, DENT AREA COVERED WITH SPEED TAPE FOR PROTECTION. REPAIRED DAMAGED SKIN IAW SRM 53-10-12 FIGURE 207 SHEET 5. REPAIRED DAMAGED SKIN IAW SRM 53-10-12 FIG 202 SH 5.

Part: HYDRAULIC SYSTEM — CONTAMINATED · airframe 26,133 hrs · 14,230 cycles

ON TAXI OUT DID A FLIGHT CONTROL CHECK & ECAM DISPLAYED BRIEFLY A GREEN HYD PUMP 1 & 2 LOW PRESS. DID A FULL RECHECK OF FLIGHT CONTROLS WITH NO ECAM. ON TAKEOFF ROLL AROUND 60KTS RECEIVED A GREEN HYD PUMP 1 & 2 LOW PRESS WARNING AGAIN ON ECAM. REJECTED TAKEOFF & RAN CHECKLIST IAW QRH. THIS INDICATES AIR IS STILL TRAPPED IN SYS. PERFORMED SATISFACTORY TEST OF HYD QTY INDICATION SYS IAW AMM 29-32-00-05. ENGS WERE RUN AT POWER & AILERONS WERE ROLLED CONTINUOUSLY UNTIL LOW PRESS INDICATION WOULD NO LONGER DISPLAY. NOTED HYD QTY DECREASED DUE AIR PURGE, NO EVIDENCE OF FLUID LOSS AROUND ACFT. SERVICED GREEN SYS HYD FLUID TO UPPER MIDDLE OF HAT, 6.0 GALS, IAW AMM 12-12-29-0. ACFT OK FOR SERVICE.

Part: SUPPORT CHANNEL — CRACKED (ZONE 100) · airframe 24,450 hrs · 13,342 cycles

CRACKED LANDING ANGLE FWD HOLD LT AFT FRAME 38.2 SLOPING SIDEWALL. REPAIRED IAW EA 6-5314-T0302440.

Part: SUPPORT CHANNEL — CRACKED (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

CEILING PANEL SUPPORT CHANNEL AT FRAME 21, CRACKED AT ANCHOR NUT ADJACENT TO LT AIR CONDITIONER DIFFUSER PANEL. SUPPORT CHANNEL REPLACED IAW SRM 51-40-21.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 24,450 hrs · 13,342 cycles

FWD CARGO BAY LEFT AFT LANDING ANGLE CRACKED AT FRAME 38.2. REPAIRED IAW INSTRUCTION OF EA 6-5314-T0302440.

Part: STRUCTURE — GOUGED (WING TIP) · airframe 24,450 hrs · 13,342 cycles

GOUGE DAMAGE TO RT WING TIP FWD OF WINGLET. REPAIR CARRIED OUT IAW EA 6-5700-T0207148.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 24,450 hrs · 13,342 cycles

CENTER FLOOR TRACK Y0, 100MM, AFT OF FRAME 30 ON MAIN CARGO DECK FOUND TO HAVE SURFACE DETERIORATION CENTER FLOOR TRACK Y0, 100MM. AFT OF FRAME 30 ON MAIN CARGO DECK ACCESS AND FOUND TO BE OUT OF LIMITS. SPLICE REPAIR CARRIED OUT IAW SRM 53-10-16 FIG 201 AND SRM 51-40-21. ITEMS 1-8 FOR RECTIFICATION DETAILS, REPAIR CLASSED AS MAJOR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 24,450 hrs · 13,342 cycles

SEAT TRACK THIRD IN FROM LT OTBD SIDE HAS SIGNS OF COROSION IN CENTER RAIL BETWEEN FRAMES 52-54. SEAT TRACK REPLACED IAW DWG NR A53812914 AND SRM 51-40-21 REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 24,450 hrs · 13,342 cycles

SEAT TRACK ON CENTER LINE HAS SIGNS OF CORROSION IN CENTER OF TRACK BETWEEN FRAMES 47-48. SEAT TRACK REPLACED IAW SRM 51-40-21.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

SEAT TRACK AT FRAMES 11-14, Y1456 HAS AREA OF CORROSION ON TOP SECTION. SEAT TRACK REPLACED IAW SRM 51-40-21 DUE FOUND OUT OF LIMITS.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 24,450 hrs · 13,342 cycles

SEAT TRACK SECOND IN FROM LT OTBD SIDE HAS SIGNS OF CORROSION IN CENTER OF TRACK BETWEEN FRAME 40-41. SEAT TRACK REPLACED IAW SRM 51-40-21.

Part: ROLLER TRACK — CORRODED (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

FWD CARGO BAY LT ROLLER TRACK ASSY CORROSION EVIDENT ON RAIL Y805 BETWEEN FR 34-35 ROLLER TRACK ASSY AT Y805 BETWEEN FR32-FR38.2. REPLACED IAW SRM 51-40-21.

Part: RIB — CRACKED (NLG WW) · airframe 24,450 hrs · 13,342 cycles

NLG WELL RT SIDE LATERAL MACHINED PANEL RIB FOUND CRACKED BETWEEN FRAMES 12A TO 13 AND 12 INCHES FROM BOTTOM OF PANEL. NLG WELL RT SIDE PANEL RIB REPAIRED IAW EA 6-5310-T0301990 P1.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

FLOOR SUPPORT FOUND CRACKED AT CORNER AT LOCATION FRAME 12A Y-1959. FLOOR SUPPORT REPLACED IAW SRM 51-40-21. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

FLOORBEAM AT FRAME 48 BETWEEN -Y1456 AND -Y1956 CRACKED. REPLACED FLOORBEAM IAW SRM 51-40-21.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

SIGNS OF CORROSION ON FLOOR SUPPORT AT FR 42. FLOOR SUPPORT REPLACED IAW SRM 51-40-21.

Part: SKIN — DAMAGED (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

FWD CARGO BAY RT SIDE FRAMES 38.0 TO 38.1, AREA BETWEEN STRINGERS 29-30R ABOVE NOTCH FLAP STRUCTURE REPLACED SOLID RIVET HAS A LARGE ELONGATED HOLE. CARGO BAY RT SIDE FR38.0-FR38.1 AREA STRINGERS 29-30 ABOVE NOTCH FLAP REPAIRED IAW EA 6-5310-T0207146.

Part: SUPPORT — CRACKED (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

SUPPORT PLATE CRACKED BETWEEN SKIN AND OTBD RT SEAT TRACK BETWEEN 38.1-38.2. SUPPORT PLATE SKIN AND OTBD RT SEAT TRACK BETWEEN FR 38.1 -FR 38.2. REPLACED IAW SRM 51-40-21.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

SEAT TRACK FR 14-17 AT STA -Y953 HAS EVIDENCE OF SURFACE DETERIORATION. SEAT TRACK REPLACED IAW SRM 51-40-21. MAJOR REPAIR.

Part: CARGO TRACK — WORN (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

CARGO TRACK WORN FR 58-59 AT STA -1456 BETWEEN FLOOR PANELS 252RH AND 252QH MCD. CARGO TRACK REPLACED IAW SRM 53-10-16, FIG 201.

Part: FLOOR SUPPORT — DAMAGED (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

CABIN FLOOR STRUCTURE, SEAT TRACK FR 14-17 AT Y450 HAS EVIDENCE OF SURFACE DETERIORATION SEAT TRACK AT FR 14-17, STA Y450. REPLACED IAW SRM 51-40-21. REPAIR CLASSED AS MAJOR.

Part: FLOOR SUPPORT — DAMAGED (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

CABIN FLOOR SUPPORT STRUCTURE FR 14-17 AT STA -Y1959, EVIDENCE OF SURFACE DETERIORATION AND DAMAGE AROUND FASTENER HOLES -Y1959 CABIN FLOOR TOP CAP SUPPORT STRUCTURE REPLACED IAW SRM 51-40-21 AND SRM 51-72-10 AT FR 14-17 AT STA -Y1959. REPAIR CLASSED AS MAJOR.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

SEAT TRACK AT FWD CABIN LT SIDE FR12-17, Y1959 HAS EVIDENCE OF CORROSION. SEAT TRACK AT FWD CABIN LT SIDE FR12-17, Y1959 REPLACED IAW SRM 51-40-44.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

CABIN FLOOR SUPPORT STRUCTURE, FR11-16, Y953 HAS VARIOUS AREAS OF SURFACE DETERIORATION AND BARE METAL. CABIN FLOOR STRUCTURE FROM FR11-16, Y953 REPLACED IAW SRM 51-72-10 AND DWG A53612550.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

SEAT TRACK FR15-17 Y-450 HAS EVIDENCE OF SURFACE DETERIORATION. REPLACED IAW SRM 51-72-10.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

CABIN FLOOR SUPPORT STRUCTURE FR11-14 Y730 FOUND HEAVILY CORRODED. CABIN FLOOR SUPPORT STRUCTURE FR11-14 LT Y730 REPLACED IAW SRM 53-12-15 AND DWG A53612214.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

SEAT TRACK Y-1959 FR45-54 HAS SIGNS OF CORROSION ON OTBD FLANGE BETWEEN FR50-51. FABRICATED SEAT TRACK Y-1959 FR45-54 INSTALLED IAW SRM 51-72-10.

Part: CROSSBEAM — DAMAGED (ZONE 100) · airframe 24,450 hrs · 13,342 cycles

FWD CARGO BAY, LT SIDE CROSSBEAM AT FR38, INBD OF SEAT RAIL Y953, EVIDENCE OF DAMAGE ON THE FWD FACE FWD CARGO BAY, LT SIDE CROSS BEAM AT FR38, INBD OF SEAT RAIL Y953 FWD FACE BLENDED IAW SRM 51-75-00 AND EA 6-5314-T0302193 P1, SURFACE REPROTECTED IAW SRM 53-10-15.

Part: SPAR — CRACKED (RT WING) · airframe 24,450 hrs · 13,342 cycles

RT WING FRAME 47, VERTICAL HOLE G, REF EO 6-5710-7-3305PT4 HAS CRACK INDICATION HOLE DIA 0.515". REPAIRED IAW EA 6-5710-T0301726.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,450 hrs · 13,342 cycles

-Y953, FRAMES 51-54 SEAT TRACK HAS TWO AREAS OF CORROSION. REMOVED CORROSION IAW SRM 51-22-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. SEAT TRACK REPLACED IAW SRM 51-40-21 AND SRM 51-72-10. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 24,450 hrs · 13,342 cycles

SEAT TRACK -Y953 FRAMES 45-46 HAD SIGNS OF CORROSION. CORROSION BLENDED IAW SRM 53-10-16 AND FOUND OUT OF LIMITS. SEAT TRACK REPLACED.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 24,450 hrs · 13,342 cycles

SEAT TRACK -Y953 FRAMES 47-48, HAD SIGNS OF CORROSION, BLENDED IAW SRM 53-10-16 AND FOUND OUT OF LIMITS. SEAT TRACK REPLACED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,450 hrs · 13,342 cycles

SEAT TRACK -Y953, FRAMES 50-51 HAS SIGNS OF CORROSION IN CENTER OF TRACK. BLENDED IAW SRM 53-10-16 AND FOUND OUT OF LIMITS. SEAT TRACK REPLACED.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 24,450 hrs · 13,342 cycles

RIGHT INBD FLAP UPPER SURFACE HAS TWO GOUGES FOUND APPROX 85 INCHES FROM OTBD EDGE. GOUGES ASSESSED IAW SRM 57-50-00, SHT 5, FIG 101 TO 105 AND FOUND TO BE OUT OF SRM LIMITS. REPAIRED IAW EA 6-5700-T0301962. MAJOR REPAIR.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

SEAT TRACK FITTING SHEARED AT FR 61. REPLACED IAW SRM 51-72-10 REF DWG A53278288203, MAJOR REPAIR CAT A REPLACMENT.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

LATERAL SEAT TRACK FITTING SHEARED AT FR 61. REPLACED IAW SRM 51-72-10 REF AIB DWG A53278288203, MAJOR REPAIR CAT A REPLACMENT.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

SEAT TRACK WORN FR 60, REPLACED.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

SEAT TRACK WORN FR 58. REPLACED IAW SRM 51-72-10 IAW DWG A53278286 MAJOR REPAIR CAT A REPLACMENT.

Part: FLOOR SUPPORT — DAMAGED (MAIN DECK) · airframe 24,450 hrs · 13,342 cycles

MAIN DECK FLOOR SUPPORT ANGLE AT FR 62, DAMAGED MAIN DECK FLOOR SUPPORT ANGLE REPLACED IAW SRM 51-40-21 AND DWG A53275411.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

SEAT TRACK AT FR 32 BETWEEN STA Y1456 AND Y1959 DAMAGED. REPLACED SEAT TRACK IAW SRM 51-40-21.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

FLOORBEAM AT FR 49 BETWEEN SEAT TRACK 3RD AND 4TH IN FROM RT OTBD SIDE (-Y1456 AND -Y1959) IS CRACKED. REPLACED IAW SRM 51-40-21.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 24,450 hrs · 13,342 cycles

LATERAL SEAT TRACK AT FR 30 BETWEEN STA Y450 AND Y953 DAMAGED LATERAL SEAT TRACK AT FR 30 BETWEEN STA Y450 AND Y953 REPLACED IAW SRM 51-40-21.

Part: GCU — FAILED (NR 2 GENERATOR) · airframe 23,744 hrs · 12,958 cycles

DURING TAKEOFF ROLL, RECEIVED GEN 2 FAULT AND OBVIOUS POWER TRANSFER. ABORTED TAKEOFF. ATTEMPTED ONE RESET IAW CHECKLIST. CSD OIL LEVEL OK DPI OK R & R GCU MM REF 24-22-12. RAN ENGINE IAW JRH, POWER TRANSFER OK VOLTS/FREQS GOOD.

Part: INDICATOR — MALFUNCTIONED (ENGINE N1) · airframe 22,664 hrs · 12,323 cycles

NR 1 N1 ANALOG NEEDLE WOULD NOT INCREASE ABOVE 45 PERCENT ON TAKEOFF. R& R NR1 ENG N1 GAUGE REF MM 77-11-21-04; OPS CHECKS GOOD. OK FOR SERVICE.

Part: RIB — WORN (ZONE 600) · airframe 21,643 hrs · 11,758 cycles

RT WING RIB 5 FITTING HAS 2 EA SECOND OVERSIZE LOCK FASTENER INSTALLED IN HOLES 47/54. REAMED AND COUNTERSUNK HOLES 47 AND 54 TO THIRD OVERSIZE INTERFERENCE FIT 0.8095 IAW EA 6-5710-136750 AND REPAIR DWG R57150117 ISSUE B INSTALLED OVERSIZE FASTENERS IAW SRM 51-40-21, PARA 7 AND TORQUED IAW SRM 51-40-00, TABLE 9. TITLE: WINGS AD 2010-23-26-EO6-5710-7-3325, SBA300-57-6110. MLG RIB 5 SPOTFACE ON THE BOTTOM FLANGE.

Part: SKIN — WORN (ZONE 500) · airframe 21,643 hrs · 11,758 cycles

LT WING RIB 5 FITTING HAS 2 EA TAPERLOKS INSTALLED AT HOLES 47/54 REWORKED SPOTFACE AND INSTALLED NEW TAPERLOKS AT HOLES 47/54 IAW EA 6-5710-136750 TITLE WINGS- AD2010-23-26-EO6-5710-7-3325-SB A300-57-6110-MLG RIB 5 SPOTFACE ON THE BOTTOM FLANGE.

Part: FLOOR PANEL — BROKEN (CARGO BAY) · airframe 21,643 hrs · 11,758 cycles

AFT CARGO PIT FLOOR PANEL 152 XF IS BROKEN.

Part: FLOOR PANEL — BROKEN (CARGO BAY) · airframe 21,643 hrs · 11,758 cycles

AFT CARGO PIT FLOOR PANEL 152 WF IS BROKEN.

Part: SKIN — CRACKED (ZONE 500) · airframe 21,643 hrs · 11,758 cycles

FOUND A CRACK ON THE LEFT WING LOWER SKIN IN HOLE "Q" AT THE 8 0'CLOCK POSITION. REAMED HOLE "Q" TO .639 IAW SRM 51-40-44. PERFORMED BHEC OF HOLE "Q" PER NDTM PT6 51-10-01. NO CRACKS NOTED. FASTENER INSTALLED ON CARD 6-5710-7-3305, PT 3.

Part: SKIN — CRACKED (ZONE 600) · airframe 21,643 hrs · 11,758 cycles

WHILE ACCOMPLISHING EO 6-5710-7-5013, PT5 FOUND CRACKS IN HOLE "G" (REF FIG 2, ITEM 21). IAW STEP 6-D. "IF ANY CRACKS ARE FOUND REFER TO EO PART 1. (ISB A300-57- 6029)". REPAIRED PER EA 6-5730-136749.

Part: SKIN — CRACKED (ZONE 600) · airframe 21,643 hrs · 11,758 cycles

FOUND A CRACK ON THE RT WING LOWER SKIN IN HOLE "G" AT THE 5 O'CLOCK POSITION. REAMED HOLE "G" TO .511 IAW A300-600 SRM 51-40-44. ACCOMPLISHED BHEC OF HOLE "G" PER NDTM PT6 51-10-01. NO CRACKS NOTED. FASTENER INSTALLED ON CARD 6-5710-7-3305, PT 4.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 21,643 hrs · 11,758 cycles

SEAT TRACK IN UPPER MAIN CABIN DECK AT FRAME 32 & 69 IS WORN & GOUGED. REMOVED AND REPLACED ADAPTER IAW SRM 51-40-21, PG 24 AND SRM 53-10-16, FIG 101.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 21,643 hrs · 11,758 cycles

RT NR 6 HALF TRACK FROM FRAME 54 TO FRAME 54.2 EXCEEDS WEAR LIMITS IAW EO 6-5310-7-3322 PT1, STEP 15. REMOVED 6 CLIPS FROM THE DAMAGED TRACK IAW SRM 51-40-21, PG 24. DRILLED & TRANSFERED HOLES ON NEW TRACK IAW SRM 51-72-10, PG 2. INSTALLED 6 CLIPS TO NEW TRACK IAW SRM 51-40-21, PG 24. TRACK WILL BE INSTALLED ON WORK CARD E 6-5310-7-3322 PT1.

Part: SKIN — CRACKED (ZONE 500) · airframe 21,643 hrs · 11,758 cycles

FOUND A CRACK ON THE LT WING LOWER SKIN IN HOLE "S" AT THE 2 O'CLOCK AND 11 O'CLOCK POSITIONS. REAMED HOLE "S" TO .639 IAW SRM 51-40-44. PERFORMED BHEC OF HOLE "S" PER NDTM PT6 51-10-01. NO CRACKS NOTED. FASTENER INSTALLED ON CARD 6-5710-7-3305, PT 3.

Part: SKIN — CRACKED (ZONE 500) · airframe 21,643 hrs · 11,758 cycles

WHILE ACCOMPLISHING EO 6-5710-7-5013, FOUND CRACKED HOLE "G". REPAIRED PER FEDEX EA 6-5730-136749.

Part: SKIN — CRACKED (ZONE 600) · airframe 21,643 hrs · 11,758 cycles

FOUND A CRACK ON THE RIGHT WING LOWER SKIN IN HOLE "C" AT THE 2 0'CLOCK POSITION. REAMED HOLE "C" TO .526 IAW SRM 51-40-44. PERFORMED BHEC HOLE "C" PER NDTM PT6 51-10-01. CRACK INDICATORS ARE AT SHIM LOCATION LAYER NR 3. NO FURTHER ACTION REQUIRED. FASTENER INSTALLED ON CARD 6-5710-7-3305, PT 4.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,643 hrs · 11,758 cycles

MAIN CABIN COMPARTMENT FLOOR PANEL 232 FG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232 FG IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 21,643 hrs · 11,758 cycles

TAIL COMPARTMENT AFT OF THE PRESSURE BULKHEAD; FWD LT FLOOR PANEL HAS A PUNCTURE HOLE. FABRICATED NEW FLOOR PANEL AFT TAIL TAIL COMPARTMENT IAW FEDEX DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,643 hrs · 11,758 cycles

MAIN CABIN COMPARTMENT FLOOR PANEL 252 ZF IS DAMAGED. FABRICATED NEW FLOOR PANEL 252 ZF IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,643 hrs · 11,758 cycles

MAIN CABIN COMPARTMENT FLOOR PANEL 251 PG IS DAMAGED. FABRICATED NEW FLOOR PANEL 251 PG IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,643 hrs · 11,758 cycles

MAIN CABIN COMPARTMENT FLOOR PANEL 251 GF IS DAMAGED. FABRICATED NEW FLOOR PANEL 251 GF IAW DWG SRZ 25-005, REV "H".

Part: JACKSCREW — INOPERATIVE (TE FLAP) · airframe 21,643 hrs · 11,758 cycles

DURING FLAP RETRACTION FLAPS STUCK AT 20 DEGS WITH FLAPS FAULT SYS 1 & 2 LIGHT ON OVERHEAD. FOLLOWED ECAM/QRCH FLAPS REMAINSED AT 20 DEGS AT 20 DEGS. ON APPROACH SELECTED AND GOT FLAPS 40. AFTER LANDING FLAPS RETRACTED NORMALLY-REPEAT. REMOVED AND REPLACED L/H #3 AND LT 5 FLAP SCREWJACK ASSY IAW AMM 27-54-24-04 AND 27-54-23-04.OPERATIONAL AND LEAK CK NORMAL..

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,643 hrs · 11,758 cycles

MAIN CABIN COMPARTMENT FLOOR PANEL 251 WG IS DAMAGED. FABRICATED NEW FLOOR PANEL 251 WG IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,643 hrs · 11,758 cycles

MAIN CABIN COMPARTMENT FLOOR PANEL 252 VF IS DAMAGED. FABRICATED NEW FLOOR PANEL 252 VF IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 21,643 hrs · 11,758 cycles

MAIN CABIN COMPARTMENT FLOOR PANEL 251 QH IS DAMAGED. FABRICATED NEW FLOOR PANEL 251 QH IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,643 hrs · 11,758 cycles

MAIN CABIN COMPARTMENT FLOOR PANEL 231 QG IS DAMAGED. FABRICATED NEW FLOOR PANEL 231 QG IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,643 hrs · 11,758 cycles

MAIN CABIN COMPARTMENT FLOOR PANEL 241 AJ IS DAMAGED. FABRICATED NEW FLOOR PANEL 241 AJ IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 21,643 hrs · 11,758 cycles

MAIN CABIN COMPARTMENT FLOOR PANEL 252 NH IS DAMAGED. FABRICATED NEW FLOOR PANEL 252 NH IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,643 hrs · 11,758 cycles

MAIN CABIN COMPARTMENT FLOOR PANEL 252 YG IS DAMAGED. FABRICATED NEW FLOOR PANEL 252 YG IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,643 hrs · 11,758 cycles

MAIN CABIN COMPARTMENT FLOOR PANEL 231 EF IS DAMAGED. FABRICATED NEW FLOOR PANEL 231 EF IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,643 hrs · 11,758 cycles

MAIN CABIN COMPARTMENT FLOOR PANEL 232 HG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232 HG IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,643 hrs · 11,758 cycles

MAIN CABIN COMPARTMENT FLOOR PANEL 232 TG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232 TG IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,643 hrs · 11,758 cycles

MAIN CABIN COMPARTMENT FLOOR PANEL 231 TG IS DAMAGED. FABRICATED NEW FLOOR PANEL 231 TG IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 21,643 hrs · 11,758 cycles

MAIN CABIN COMPARTMENT FLOOR PANEL 252 PG IS DAMAGED. FABRICATED NEW FLOOR PANEL 252 PG IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,643 hrs · 11,758 cycles

MAIN CABIN COMPARTMENT FLOOR PANEL 232 NG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232 NG IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,643 hrs · 11,758 cycles

MAIN CABIN COMPARTMENT FLOOR PANEL 231 VG IS DAMAGED. FABRICATED NEW FLOOR PANEL 231 VG IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,643 hrs · 11,758 cycles

MAIN CABIN COMPARTMENT FLOOR PANEL 261 AH IS DAMAGED. FABRICATED NEW FLOOR PANEL 261 AH IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 21,643 hrs · 11,758 cycles

MAIN CABIN COMPARTMENT FLOOR PANEL 251 BH IS DAMAGED. FABRICATED NEW FLOOR PANEL 251 BH IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,643 hrs · 11,758 cycles

MAIN CABIN COMPARTMENT FLOOR PANEL 252 TH IS DAMAGED. FABRICATED NEW FLOOR PANEL 252 TH IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,643 hrs · 11,758 cycles

MAIN CABIN COMPARTMENT FLOOR PANEL 242 ZJ IS DAMAGED. FABRICATED NEW FLOOR PANEL 242 ZJ IAW DWG SRZ 25-005, REV "H".

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,643 hrs · 11,758 cycles

MAIN CABIN COMPARTMENT FLOOR PANEL 232 YG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232 YG IAW DWG SRZ 25-005, REV "H".

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 21,643 hrs · 11,758 cycles

AFT MAIN CABIN LT SIDE BETWEEN FRAME 79 & FRAME 80/82 AT FLOOR LEVEL; INTERCOSTAL WEB STRUCTURE IS CRACKED, STRINGER 26L-STRINGER 26L. REMOVED CRACKED WEB INTERCOSTAL IAW SRM 51-40-21, PARA 7. RECEIVED NEW WEB IAW DWG 18A53981113, ISSUE "A", PO 686125.1. LOCATED AND DRILLED NEW WEB IAW SRM 51-40-44. INSTALLED WEB IAW SRM 51-40-21, PARA 7 AND DWG 18A53981113, ISSUE "A".

Part: FRAME — CRACKED (FUSELAGE) · airframe 21,643 hrs · 11,758 cycles

FWD CARGO COMPARTMENT OVERHEAD FLOORBEAM; FWD SIDE OF FRAME 30 & LBL 27 IS CRACKED.

Part: JACKSCREW — FAILED (TE FLAPS) · airframe 21,640 hrs · 11,755 cycles

DURING FLAP RETRACTION FLAPS STUCK AT 20 DEGS WITH FLAPS FAULT SYS 1 & 2 LIGHT ON OVERHEAD. FOLLOWED ECAM/QRCH FLAPS REMAINED AT 20 DEGS AT 20 DEGS. ON APPROACH SELECTED AND GOT FLAPS 40. AFTER LANDING FLAPS RETRACTED NORMALLY-REPEAT. REMOVED AND REPLACED LT NR 3 AND LT NR 5 FLAP SCREWJACK ASSY IAW AMM 27-54-24-04 AND 27-54-23-04.OPERATIONAL AND LEAK CK NORMAL..

Part: JACKSCREW — STUCK (TE FLAPS) · airframe 21,637 hrs · 11,752 cycles

ON TAKEOFF, WHEN FLAP HANDLE WAS RAISED, ECAM SHOWED FLAPS 1 AND 2 FAULT WITH FAULT LIGHTS ON OVERHEAD PANEL AS WELL. FLAPS STUCK AT 20 DEGREES, CYCLED HANDLE AND STILL HAD FLAPS STUCK AT 20 DEGREES. RETURNED TO LANDING, NORMAL. INSPECTED THE NR 3 LT FLAP JACK SCREW AND FOUND THE RIG PIN HOLE SLIGHTLY MISALIGNED AND THE CLOSED DIMENSION TO BE OFF BY 1/8 IN, AT THIS TIME. DUE TO THE AIR TURN BACK AND THE PREVIOUS HISTORY OF THE AIRCRAFT, REPLACED THE NR 3 LT FLAP JACKSCREW ASSY REF MM 27- 54-23-04. OPERATED FLAPS AND THE NR 3 JACKSCREW OPERATES SMOOTHLY. PERFORMED ADJ/TEST OF FLAPS PER MM 27-50-00-05, ADJUSTED NR 6 FLAP PER MM 27-50-00-05 4A. ALL RIG ADJUSTMENTS CHECKED GOOD, OP'S OF FLAPS CHECKED GOOD. ACFT OK TO CONTINUE.

Part: JACKSCREW — INOPERATIVE (TE FLAPS) · airframe 21,560 hrs · 11,711 cycles

FLAP SYSTEM 1, 2, FAULT ON OVERHEAD PANEL ON ECAM. ATTEMPTED TO CYCLE FLAP HANDLE BUT PROBLEM REMAINED. FOLLOWED QRH RETURNED TO DEPARTURE. HAPPENED WHEN FLAPS 15 SELECTED. FLAPS APPEARED STUCK APPROX 13-14 DEG, WOULD NOT MOVE PAST THAT. ACFT BELOW MAX LANDING WEIGHT. CHECKED SFCC'S FOR FAULTS. BOTH 1 AND 2 SFCC SHOWED FAULT, BALLS CONSISTENT WITH "FLAPS JAMMED". FOUND LT SYS TORQUE LIMITER INDICATOR POPPED. NR 2 LT SHAFT AND JACKSCREW. DRAINED OIL AND FOUND OIL VERY BLACK (OPAQUE) WITH SOME METAL SHAVINGS, REF TSM 27-50-02. REPLACING NR2 JACKSCREW. CHECKED REMAINING JACKSCREWS .

Part: LIMITER — MALFUNCTIONED (TE FLAP SYSTEM) · airframe 21,443 hrs · 11,642 cycles

FLAPS FAULT 1 & 2 STUCK AT 20. SFCC 1 AND 2 INDICATES SLAT 00001 / FLAP 011111. (LT EXTEND SWITCH KRUGER / NOTCH) AND (FLAP JAM) REF TO SFCC BITE CHECK TSM 27-50-00. FOUND LT TORQUE LIMITER POPPED (INDICATING ACTIVATED).

Part: INDICATION SYS — MALFUNCTIONED (EGPWS) · airframe 20,010 hrs · 10,759 cycles

APPROACHING ON CAT III APP GOT EGPWS TERRAIN WARNING-ACCOMPLISHED EGPWS ESCAPE MANEUVER AT APPROX 400 FT AGL WITH FIREWALL POWER, HOWEVER, EXCEEDENCE INDICATORS DID NOT EXCEED. OP CHECKED EGPWS 4 TIMES IAW AMM 34-48-01-5, COULD NOT DUPLICATE DISCREPANCY ON THE GROUND. SYS OP CHECKED GOOD IAW 34-48-01-5. ACFT OK TO CONTINUE.

Part: INDICATION SYS — MALFUNCTIONED (EGPWS) · airframe 20,010 hrs · 10,759 cycles

ON CAT III APP GOT EGPWS TERRAIN WARNING-ACCOMPLISHED EGPWS ESCAPE MANUVER AT APPROX 400 FT AGL WITH FIREWALL POWER, HOWEVER EXCEEDENCE INDICATORS DID NOT EXCEED. OP CHECKED EGPWS 4 TIMES IAW AMM 34-48-01-5. COULD NOT DUPLICATE DISCREPANCY ON THE GROUND. SYS OPS CHECKED GOOD IAW 34-48-01-5. ACFT OK TO CONTINUE.

Part: VALVE — LEAKING · airframe 19,551 hrs · 10,489 cycles

SUSPECT MAJOR FUEL LEAK RT INNER TANK. ALSO IT MAY SOME HOW TRANSFERRED FUEL TO LEFT INNER FOB MINUS FBO ARE VERY CLOSE TO TAKEOFF FUEL. TRANSFERRED FUEL FROM LT TO RT TANK AND DETERMINED THAT FUEL HAD INDEED MIGRATED TO THE LT TANK. BALANCED FUEL LOADS AND LT PUMPS ON FOR AN EXTENDED PERIOD OF TIME WITH NO DUPLICATION OF DISCREPENCY IAW MOC REMOVED AND REPLACED LI REFUEL/DEFUEL VALVE REF. AMM 28-25-12-4 OPS AND LEAK CHECK GOOD REFER TO WRI FOR 05-50/1692 FOR LANDING INSP R/I 15MAY09 05:56 MEM R&R FROM FACT PREMATURE REMOVAL/INSTALLATION OFF .

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 19,353 hrs · 10,379 cycles

ON TAKEOFF, AFTER TOGA WAS SET, NOSE OF ACFT VEERED RIGHT. TILER WAS INEFFECTIVE IN STRAIGHTENING OUT. SUSPECTED DRAGGING RIGHT BRAKES. ABORTED TAKEOFF AND HAD SAN RAMP LOOK OVER WHEELS AND BRAKES. EVERYTHING CHECKED GOOD. TAXIED OUT AND TAKEOFF REST OF FLIGHT UNEVENTFUL. SAN MAINTENANCE INSPECTED ACFT ON REMOTE RAMP AND NO FAULTS FOUND, ACFT DEPARTED. ACFT ARRIVED WITH NORMAL BRAKE TEMPS ON BOTH GEARS. OPS CK'D SYS PER MM 32-42-00-5 PAR 1D AND 2, NO DEFECTS NOTED ALSO PER FLIGHT CREW THERE WERE NO ADDITIONAL PROBLEMS. ACFT OK FOR SERVICE. SECOND LEG UNEVENTFUL AS WELL. (MEM-LBB)

Part: WIRE — DISCONNECTED (FUEL QTY) · airframe 19,064 hrs · 10,228 cycles

DURING CLIMB-OUT, ABOUT 10,000, LT OUTER FUEL QTY BEGAN TO DECREASE. CENTER TANKS (BOTH) FAULTED EVEN THOUGH 400 LBS PRESENT OR INDICATED. LT OUTER DECREASED TO BELOW 1,000 LBS. DURING DESCENT, LT OUTER FUEL QTY INDICATION BEGAN TO INCREASE RISING TO 3,400 LBS BY 10,000 FT. LT OUTER TANKS INDICATED NEAR FULL BY SHORT APPROACH. TOTAL FUEL QTY REFLECTED FLUCTUATING LT OUTER INDICATIONS. BOTH ECAM & OVHD PANEL PRODUCED ACCOMPLISHED FQIC BITE TEST. AFTER BITE TEST, RESET FQIC. PERFORMED LT OUTER INDIVIDUAL PROBE CAPACITANCE & RESISTANCE CHECK IN REF TO AMM28-42-00-5. ALL PROBE CAP AND RESISTANCES WITHIN LIMITS. MEGGED WIRING FROM 563VCA TO FQIC ALL WIRING CHECKED GOOD. CONDUCTOR (-W OF 563VCA). DEPINNED SHIELDED WIRE PIN -W FOR INSPECTION & 2 SHIELD WIRES THAT WERE PIGGY-BACKED TO IT PULLED OUT OF THE SOLDER SLEEVE. WIRE 2842-5100-W. RETERMINATED SOCKET FOR CENTER CONDUCTOR (-W) AND REASSEMBLED SOLDER SLEEVE FOR SHIELD & TWO PIGGY-BACKED WIRES. OPENED & VENTED LT OUTER TANK. PERFORMED DETAILED VISUAL INSPECTION OF TANK INTERNAL PROBE WIRING, SECURED CLAMP ON PROBE NR 11. FUELED ACFT AND TESTED GOOD.

Part: INDICATION SYS — MALFUNCTIONED (FUEL QTY) · airframe 19,057 hrs · 10,222 cycles

DURING CLIMB, THRU APPROX 18K, NOTICED LT OUTER FUEL QTY DECREASING AT APPROX 500-1000 LBS MIN, THIS WAS ON THE ECAM AND OVHD PANEL. REF QRH UNDER "POSSIBLE FUEL LEAK" PULLED FQI CHAN SUPPLY 1 2 C/B'S. WHEN FUEL INDICATIONS RETURNED LT OUTER RESUMED IT'S STEADY DECREASE. AFTER LANDING (30K UNDER MAX LNG WT) ALL FUEL IND'S RETURNED TO NORMAL (IE FUEL IND IN OUTERS). T/S INFO MTSI 28-40/1374, PER MOCC REQUEST COMPLIED WITH STEP A: DURING BITE CHECK FOUND FAULTS 312 AND 322 ON FQI. COMPLIED WITH TSM 28-42-00 FAULT CODE TROUBLESHOOTING PAGE 127, NO DEFECTS FOUND. STEP B: LEFT OUTER TANK CAPACITANCE AND RESISTANCE CHECKS OK PER MM 28-42-00-5. STEP C: VERIFIED WIRING AND PINS FROM CONNECTORS 56VC AND 5073VC PER AWM 28-42-02. PERFORMED CAPACITANCE AND RESISTANCE CHECKS ON LEFT OUTER TANK, ALL CHECKS NORMAL PER MM 28-42-00-5.

Part: WIRE — DAMAGED (FUEL SYSTEM) · airframe 19,049 hrs · 10,220 cycles

DURING CLIMB THRU 18K, LOW FUEL QTY DECREASING AT APPX 500-1000 LBS/MIN, THIS WAS ON THE ECAM & OVHD PANEL. REF QRH, "POSSIBLE FUEL LEAK" PULLED FQI CHAN SUPPLY 1 2 C/B'S. WHEN FQI RETURNED LOW RESUMED IT'S STEADY DECREASE. AFTER LANDING, ALL FUEL IND'S RETURNED TO NORMAL. ACFT RELEASED FOR SERVICE PER MEL/CDL: 28-42-01-01 RELEASED FOR SERVICE. BITE TEST OF CGCC & FUEL QTY COMPUTER NORMAL. DEPINNED SHIELDED WIRE PIN -W FOR INSPECTION & TWO SHIELD WIRES THAT WERE PIGGY-BACKED TO IT PULLED OUT OF THE SOLDER. RETERMINATED SOCKET FOR CENTER CONDUCTOR AND REASSEMBLED SOLDER SLEEVE FOR SHIELD & TWO PIGGY-BACKED WIRES.

Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 18,889 hrs · 10,140 cycles

GUIDE BROKE AT POS 9L WITH FLOOR DAMAGE REMOVED DAMAGED SECTION AT FLOORBEAM FRAME 64 BETWEEN SEAT TRACK NR 3 LT AND NR 4 LT AND REPAIRED IAW FEDEX EA 6-5310-117443, RELEASE DATE 11/14/07.

Part: FRAME — CRACKED (THRUST REVERSER) · airframe 18,889 hrs · 10,140 cycles

NR 1 ENG OTBD T/R FWD FLANGE FOR MOUNTING RING LATCH ASSY HAS 2.25 IN CRACK AT 12 O'CLOCK POS REMOVED CRACK AND REPAIRED NR 1 OTBD T/R FWD FLANGE IAW FEDEX EA 6-7830-124134, RELEASE DATE 8 OCTOBER, 2008.

Part: FRAME — CRACKED (THRUST REVERSER) · airframe 18,889 hrs · 10,140 cycles

NR 1 ENG INBD T/R FWD FLANGE FOR MOUNTING RING LATCH ASSY HAS 2 INCH CRACK AT 12 O'CLOCK POS REMOVED CRACK AND REPAIRED NR 1 ENG INBD T/R FWD FLANGE IAW FEDEX EA 6-7830-124133, RELEASE DATE 8 OCTOBER, 2008.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 18,889 hrs · 10,140 cycles

FUSELAGE AUXILIARY STRUCTURES, 2 WORN LOBES ON SEAT TRACK Y2462 RT AT FRAME 20. REMOVED DAMAGED SEAT TRACK SECTION FROM BETWEEN FRAMES 18/19 TO BETWEEN FRAME 27/28 AND REPLACED IAW SRM 53-13-16 CONFIG 2 ITEM 40 AND EA6-5320-105302C PT3.

Part: TRACK — DAMAGED (ZONE 200) · airframe 18,889 hrs · 10,140 cycles

RT NR 5 (-Y1959) AFT DUMMY TRACK AT FRAME 54.1 HAS 6 FASTENERS IMPROPERLY INSTALLED AND 1 HOLE IS ELONGATED ON INBD AFT FLANGE OF DUMMY TRACK. REPAIRED RT NR 5 (-Y1959) AFT DUMMY TRACK AT FRAME 54.1 IAW A300-600 FREIGHTER SRM 53-10-16 FIG 202.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 18,889 hrs · 10,140 cycles

MDCC SEAT TRACK (Y1959) LT NR 5 AT FRAME 30 HAS 1 ELONGATED SCALLOP. REPAIRED SEAT TRACK (Y1959) LT NR 5 AT FRAME 30 BY USING SPLICE FROM FRAME 27 TO BETWEEN FR 32 AND 33 IAW A300-600 FREIGHTER SRM 53-10-16 FIG 201A PGS 203-208.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 18,889 hrs · 10,140 cycles

FWD CARGO COMPT FR 31 BETWEEN SEAT TRACK NR 4 LT AND TRACK NR 5 LT FLOORBEAM HAS .25 INCH CRACK. REMOVED CRACK AND INSTALLED CROSSBEAM REPAIR AT CRACKED STIFFENER AT FR 31, BETWEEN SEAT TRACK NR 4 LT AND NR 5 LT IAW SRM 53-10-15, FIG 212, PAGE 397/398.

Part: FRAME — CRACKED (THRUST REVERSER) · airframe 18,889 hrs · 10,140 cycles

NR 2 ENG OTBD T/R FWD FLANGE FOR MOUNTING RING LATCH ASSY HAS 2.750 INCH CRACK AT 12 O'CLOCK POSITION. REPAIRED CRACK ON NR 2 OTBD T/R FLANGE IAW FEDEX EA 6-7830-124135, RELEASE DATE 8 OCTOBER, 2008.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 18,889 hrs · 10,140 cycles

MAIN DECK CARGO COMPT FLOORBEAM CRACKED AT FR 64, BETWEEN SEAT TRACK NR 3 RT AND NR 4 RT, .25 INCH LONG. CUT OUT DAMAGED AREA AND INSTALLED CROSSBEAM REPAIR AT FR 64, BETWEEN SEAT TRACKS NR 3 RT AND NR 4 RT IAW SRM 53-10-15, FIG 211, PAGE 389/390.

Part: FRAME — CRACKED (THRUST REVERSER) · airframe 18,889 hrs · 10,140 cycles

NR 2 ENG INBD THRUST REVERSER HAS A CRACK .225 INCH LONG ON UPPER FWD END FRAME ROUTED CRACK ON NR 2 ENG INBD T/R TORQUE BOX FWD FRAME AND REPAIRED IAW FEDEX EA 6-7830-124136, RELEASE DATE 8 OCTOBER, 2008.

Part: BRACKET — FAILED (MLG) · airframe 18,490 hrs · 9,930 cycles

REPEAT WRITE-UP- DURING FINAL APPROACH PHASE, LEFT LANDING GEAR WOULD NOT INDICATE DOWN AND LOCKED AFTER GEAR SELECTED DOWN. RECYCLED GEAR HANDLE WITH SAME RESULT, COMPLIED WITH ALL ECAM AND QRH ITEMS. TRIED SIDE SLIPS AFTER MANUALLY LOWERING GEAR. NO HELP AFTER 20 MIN IN PATTERN TRYING TO TROUBLESHOOT INDICATION CHANGED TO DOWN AND LOCKED ON ITS OWN. ORDERED DOWN LOCK (SIDE BRACE ACTUATOR) DUE TO FAT STARTED AFTER CHANGING FOR LEAKING ACTUATOR. REMOVED AND REPLACED LT GEAR BRACE STRUT CYLINDER IAW A300 AMM 32-31-55-4. OPS AND LEAK CHECKS GOOD. PERFORMED EXT AND RETRACTION IAW A300 AMM 32-31-00. OPS CHECKS GOOD PERFORMED MANUAL EXT AND RETRACTION. OPS CHECKS GOOD RESET MANUAL EXT IAW.

Part: SEQUENCE VALVE — FAILED (MLG) · airframe 18,488 hrs · 9,929 cycles

ON FINAL APPROCH DURING LANDING GEAR EXTENSION, LEFT MAIN GEAR WOULD NOT EXTEND. RED GEAR NOT DOWN INDICATION ON BOTH POSITION 1 AND 2 AND OVERHEAD PANEL. PROCEEDED WITH LANDING GEAR GRAVITY EXTENSION PROCEDURE. ALL GEAR DOORS OPENED BUT LEFT MAIN GEAR STILL NOT DOWN AND LOCKED. A STEADY STATE SIDE LOAD WAS APPLIED AND LEFT MAIN GEAR EXTENDED AND INDICATED GREEN LIGHT. ALL HYDRAULIC INDICATIONS NORMAL. SEQUENCING VALVE APPEARED TO BE BYPASSING. REMOVED AND REPLACED MLG LT SEQUENCING VALVE IAW A300 MM 32-31-37-4. CYCLED MLG 25 TIMES. OPS AND LEAK CK GOOD.

Part: UNKNOWN — UNKNOWN (THRUST REVERSER) · airframe 16,582 hrs · 8,904 cycles

ON T/O ROLL ECAM SHOWED NR 2 ENGINE REVERSER PRESSURIZED. CYCLED REVERSER WITH NO HELP. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 18FEB07 "MEL 78-30-01-A: ENGINE NR 2 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION." MXP AND FADEC CK, PLEASE WORK IN CONJUNCTION WITH TSI: 78-30 9440.

Part: THRUST REVERSER — INOPERATIVE (NR 2 ENGINE) · airframe 16,531 hrs · 8,873 cycles

AT 75 KNOTS, THE NR 2 ENG REV PRESSURE LIGHT CAME ON. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 10FEB07 "MEL 78-30-01-A: ENGINE (IDENTIFY 1 OR 2) NR 2 THRUST REVERSER, INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION." REMOVED AND REPLACED NR 2 RT REVERSER CTR DRIVE UNIT IN REFERENCE TO A300-600 M/M 78-31-01-4-05.OP CHECKED GOOD.

Part: LINE — RUPTURED (HYD SYSTEM) · airframe 16,377 hrs · 8,788 cycles

AFTER TAKEOFF, WHEN GEAR UP WAS SELECTED THE NOSE GEAR RETRACTING WAS EXCESSIVELY NOISY. SHORTLY THEREAFTER, ALL GREEN HYD QUANTITY WENT TO ZERO, WITH ECAM. ECAM AND OVERHEAD DISPLAYED ZERO QUANTITY. GREEN PRESSURE 3200 PSI FOR 3 MINUTES. QRH DIRECTED PUMPS OFF AND LANDING GEAR GRAVITY EXTENSION. NORMAL LANDING CHECKED QUANTITY ON RESV, MANUAL GAUGE AGREES WITH ECAM AND OVERHEAD IN COCKPIT. GAUGE SHOWS LITTLE OVER 3 GALS IN RESV SERVICED. FOUND LT INBD GREEN SYSTEM AILERON ACTUATOR PRESSURE FLEX LINE RUPTURED. REPLACED FLEX LINE. PERFORMED GEAR SWING. NO DEFECTS NOTED WITH NO ABNORMAL SOUNDS ON NLG.

Part: UNKNOWN — CONTAMINATED · airframe 16,303 hrs · 8,746 cycles

LANDED ON ORD RW09R WITH CONTAMINATED RW. STOPPED WITH LEFT MAIN GEAR OFF THE LEFT SIDE OF THE RW. RT GEAR STILL ON THE RW. NOSE SLIGHTLY OFF THE LEFT. PSC COMPLIED INSPECTION IAW AMM 05-51-24-0. AIRCRAFT FOUND TO BE AIRWORTHY.

Part: LINE — FAILED (THRUST REVERSER) · airframe 15,013 hrs · 8,068 cycles

SLOWING TO 250 KNTS FOR DESCENT, NOTICED AN INCREASED VIBRATION THAT FELT LIKE IT WAS ENGINE. FOUND T/R -Y- CHECK VALVE NR 1 ENGINE LOWER SUPPLY LINE BLOWN APART. REMOVED LINE AND ORDERED PARTS. UPON FURTHER INVESTIGATION ON WHY THE T/R V AIR TUBE CAME APART, FOUND THE FOWARD LINK ASSEMBLY ON THE T/R ACTUATION RGLTR SHUTOFF VALVE BROKEN. THE BROKEN LINK ASSEMBLY CAME TO REST ON AND DAMAGE A 1ST STAGE IGV VANE ACTN ARM ASSY. DUE TO THE UNKNOWN AND VIBS ALONG WITH THE IVGV LEVER BROKEN, APPROVED THIS ENGINE FOR CHANGE.

Part: LINE — FAILED (TR CHECK VALVE) · airframe 15,010 hrs · 8,067 cycles

SLOWING TO 250 KNTS FOR DESCENT NOTICED AN INCREASED VIBRATION THAT FELT LIKE IT WAS ENGINE. NORMAL LANDING KMHT (NOT A DIVERSION). FOUND T/R -Y- CHK VALVE NR 1 ENGINE LOWER SUPPLY LINE BLOWN APART. REMOVED LINE AND ORDERED PARTS. UPON FURTHER INVESTIGATION ON WHY THE T/R V AIR TUBE CAME APART, FOUND THE FOWARD LINK ASSEMBLY ON THE T/R ACTUATION RGLTR SHUTOFF VALVE BROKEN. THE BROKEN LINK ASSEMBLY CAME TO REST ON AND DAMAGED 1ST STAGE IGV VANE ACTN ARM ASSY. DUE TO THE UNKNOWN AND VIBS ALONG WITH THE IVGV LEVER BROKEN, APPROVED THIS ENGINE FOR CHANGE.

Part: INDICATOR — MALFUNCTIONED (BRAKE SYSTEM) · airframe 14,681 hrs · 7,876 cycles

FL320, THE RT BRAKE PRESS GAUGE INCREASED O TO 2000 PSI. AFTER 12 MIN IT DECREASED TO 1500 PSI. AFT 30 MIN IT DECREASED TO 400 PSI. BRAKE A/S SELECTOR WAS IN THE NORMAL ON POS. ALL WHEEL BRAKES SHOWED REL ON ECAM. PARKING BRAKE WAS VERIFIED OFF. LATER IN THE FLIGHT FROM OAK, THE PROBLEM REPEATED. DURING DESCENT RT BRAKE PRESSURE DECREASED TO ZERO. NORMAL LNDG. PERF OPS TEST OF ALT BRAKING SYS PER MM 32-43-00. OPS CK OK. PERF OPS TEST OF PARKING BRAKE SYS PER MM 32-45-00. OPS CK OK. REMOVED AND REPLACED BRAKE YELLOW PRESS TRIPLE IND MM 32-44-19-4 PRECAUTIONARY. REMOVED AND REPLACED YEL BRAKE SYS PRESS TRANSMITTER 72GG.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 13,617 hrs · 7,279 cycles

FO'S WINDSHIELD SHATTERED. DECLARED EMERGENCY. NO OVERWEIGHT LANDING. MEM R CHECK RESISTANCE VALUES ON NEW WINDSHIELD AND ALL CHECK GOOD PER AIRBUS TSM 30-42-00. REMOVED AND REPLACED F/O'S_WINDSHIELD IN REFERENCE T TO A300 AMM 56-11-11-4. OPS CHECKED GOOD AT THIS TIME. SEALANT APPLIED 19:25. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG NP175201-4, POS ONL SRL 98071H9632, TAG 3A0236 ON MFG NP175201-6 SRL 04261H6378, TAG 662105.

Part: THROTTLE — OBSTRUCTED (NR 2) · airframe 12,984 hrs · 6,911 cycles

RTO DUE TO LOW POWER NR 2, ENG NR 2 THROTTLE WOULD NOT ADVANCE PAST REF. POINT 30 AND N1 ADVANCED TO 93 PERCENT VS 108 PERCENT REQUIRED. RTO OCCURRED AT 90 KTS. ENT BY: 273927 RPT BY: 096714 SHGN 11SEP04 02:40 GDL U IN WORK, ENT BY: 273927 RPT BY: 273927 FACT 11SEP04 03:37 GDL U FOUND DSUZ SCREW BLOCKING NR 2 THROTTLE MECHANISM. INSPECTED SAME AND NO DAMAGE FOUND ON IT. TESTED FADEC NO FAULTS IN MEMORY. REF. TSM 76-00-30 AND AMM 73-38-00-5-F. OK FOR SERVICE. ENT BY: 273927 RPT BY: 273927

Part: FIRE LOOP — OUT OF POSITION (NR 1 ENGINE) · airframe 10,322 hrs · 5,386 cycles

ON CLIMB OUT NR 1 FIRE WARN/BELL WARN LT RET'D THROTTLE AND WARN STOPPED. COMPLETED FIRE S/D CKLIST AND RTO TO MEM FOR LD. LT & BELL EXT WHEN THROTTLE RTO, BUT ACTIVATED WHEN THROTTLE ADVANCED. INSP FIRE LOOPS NR 1 ENG FOUND LOOP MAKING PHYSICAL CONTACT WITH PNEUMATIC DUCT. FOUND HYD RESERVOIR HOSE CHAFED, CONTACT WITH LOOP SECT DH4. REPOSITIONED DH4 LOOP, REPLACED HYD RESERVOIR PRESS LINE IAW A300 MM 20-23-12-0. NO ENG RUN, CLOSED COWLS PER IAW A300 MM 71-13-00-3F. RAN ENG PER IAW JRH6-10 POWER ASSURANCE RUN FOR 5 MINS & 73 PERCENT WITH HP OPEN FOR 5 MINS & TAXI TO HIGH POWER RUN PAD, CND, OK FOR SERVICE.

Part: BLEED VALVE — MALFUNCTIONED (NR 2) · airframe 7,281 hrs · 3,667 cycles

00-354 NR 2 HP BLEED VALVE ON ECAM, NR 1 HP ECAM NOT CLOSED WARNING. DUAL HP VLV FAULTS. ** S/D ** COMING

Part: SENSOR — FAILED (LANDING GEAR)

99-195 - GEAR WOULD NOT RAISE WITH INTERLOCK WARNING SWITCH TO SYS 2, GEAR RAISED, LOST NR 1 PITCH TRIM, AUTO THROTTLES, AUTOPILOT, NR 1 PRESS REG. REMOVED AND REPLACED 64GB SENSOR, 32-00-00-4 AND OPS CK 32-00-00-5 AFS LAND TEST PASSED, 22-00-00-5.

Part: PILOT VALVE — MALFUNCTIONED (NR 1 TR UNIT)

ON POWER APPLICATION, NR 1 REV PRESS LIGHT CAME ON AND THEN WENT OUT, ON THE ECAM AT APPROX 200-300 FT AGL WARNING CAME BACK ON. REMOVED AND REPLACED NR 1 THRUST REVERSER DIRECTIONAL PILOT VALVE. OPS CHECK GOOD.