N686FE

Part: SEAT — CRACKED (ZONE 200) · airframe 31,272 hrs · 17,951 cycles

APPEARS FRONT OF CAPTAINS SEAT IS LOOSE. ROCKS EXCESSIVELY. AMM 25-XX-XX-XX FOUND CAPT SEAT CRACKED AT BOTH FRONT ATTACH POINTS REF AMM 25-11-11-06. AMM: 25-11-11-04 REMOVED AND REPLACED CAPT SEAT REF AMM 25-11-11-04, OP'S CHECK GOOD

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 30,574 hrs · 17,521 cycles

FOUND A DENT AT RH O/B FLAP UPPER SURFACE I/B T/E. CUT OUT THE DAMAGE AREA AND REPAIR WITH EXTERNAL DOUBLER I.A.W EA NO:6-5750-T0370136 P1, SEQ NO:000767, TITLE:WING - FLIGHT SURFACES - RH OUTER FLAP TRAILING EDGE UPPER SKIN REPAIR BETWEEN RIBS 3A AND 3B & A300-600F SRM 57-50-00-201, PARA.4E, PAGE.217-220, FIG.205.

Part: NONE — WORN (ZONE 200) · airframe 30,574 hrs · 17,521 cycles

FR38.2/FR40 RH NO.3 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393 INCHES(1.0MM) LESS THAN 0.0846 INCHES(2.15MM).SLOT GAP ACTUAL VALUE 1.46MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR. REPAIR ACCOMPLISHED.

Part: SEAT TRACK — WORN (CABIN) · airframe 30,574 hrs · 17,521 cycles

FR54/FR54.2 RH NO.4 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393 INCHES(1.0MM) LESS THAN 0.0846 INCHES(2.15MM).SLOT GAP ACTUAL VALUE 1.4MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR. REPAIR ACCOMPLISHED.

Part: NONE — WORN (ZONE 200) · airframe 30,574 hrs · 17,521 cycles

FR38.2/FR40 LH NO.2 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393 INCHES(1.0MM) LESS THAN 0.0846 INCHES(2.15MM).SLOT GAP ACTUAL VALUE 1.15MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR. REPAIR ACCOMPLISHED.

Part: DUMMY RAIL — WORN (ZONE 200) · airframe 30,574 hrs · 17,521 cycles

FR54/FR54.2 RH NO.5 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393 INCHES(1.0MM) LESS THAN 0.0846 INCHES(2.15MM).SLOT GAP ACTUAL VALUE 1.5MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR. REPAIR ACCOMPLISHED.

Part: NONE — WORN (ZONE 200) · airframe 30,574 hrs · 17,521 cycles

FR54/FR54.2 RH NO.3 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393 INCHES(1.0MM) LESS THAN 0.0846 INCHES(2.15MM).SLOT GAP ACTUAL VALUE 1.15MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR. REPAIR ACCOMPLISHED.

Part: DUMMY RAIL — WORN (ZONE 200) · airframe 30,574 hrs · 17,521 cycles

FR54/FR54.2 LH NO.5 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393 INCHES(1.0MM) LESS THAN 0.0846 INCHES(2.15MM).SLOT GAP ACTUAL VALUE 1.5MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR. REPAIR ACCOMPLISHED.

Part: NONE — WORN (ZONE 200) · airframe 30,574 hrs · 17,521 cycles

FR38.2/FR40 RH NO.5 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393 INCHES(1.0MM) LESS THAN 0.0846 INCHES(2.15MM).SLOT GAP ACTUAL VALUE 1.12MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR. REPAIR ACCOMPLISHED.

Part: NONE — NONE (NONE) · airframe 30,574 hrs · 17,521 cycles

AIRCRAFT REPAIR ASSESSMENT:EXISTING SPLICE REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR57-57.2,Y450 POSITION. COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1,TITLE:A300/A310 RPR IDENT & SUPPLEMENTAL MX REQ(SMR)TRK,INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA:A300-600F SRM 53-10-16-201 PARA.4 FIG.201 PAGE 203~208,THIS REPAIR IS CLASSIFIED AS MAJOR CATEGORY A REPAIR WITH NO SUPPLEMENTAL INSPECTION REQUIREMENTS.

Part: NONE — NONE (NONE) · airframe 30,574 hrs · 17,521 cycles

AIRCRAFT REPAIR ASSESSMENT:EXISTING SPLICE REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR56~FR57.2,-Y450 POSITION. COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1,TITLE:A300/A310 RPR IDENT & SUPPLEMENTAL MX REQ(SMR)TRK,INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA:A300-600F SRM 53-10-16-201 PARA.4 FIG.201 PAGE 203~208,THIS REPAIR IS CLASSIFIED AS MAJOR CATEGORY A REPAIR WITH NO SUPPLEMENTAL INSPECTION REQUIREMENTS.

Part: NONE — NONE (NONE) · airframe 30,574 hrs · 17,521 cycles

AIRCRAFT REPAIR ASSESSMENT:EXISTING CROSSBEAM REPAIR FOUND ON MAIN DECK AT FR58,BTW -Y450~-Y953. COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1,TITLE:A300/A310 RPR IDENT & SUPPLEMENTAL MX REQ(SMR)TRK,INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA:A300-600F SRM 53-10-15-201 PARA.14 FIG.211 PAGE 385~392,THIS REPAIR IS CLASSIFIED AS MAJOR CATEGORY A REPAIR WITH NO SUPPLEMENTAL INSPRCTION REQUIREMENTS.

Part: RIB — CRACKED (ZONE 500) · airframe 30,574 hrs · 17,521 cycles

3EA CRACKS(MAX18MM) WERE FOUND AT L/H WING CENTER FLAP RIB 26 FWD AND AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE WORK WITH REPAIR ANGLES AND EXTERNAL DOUBLER I.A.W EA NO:6-5750- T0369804 P1, SEQ NO:000760, TITLE:WING-FLIGHT SURFACES-LH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIB26 AND 27 BETWEEN STRINGERS 2.5 AND 2.8-ALI 575306-01 & A300-600F SRM 57- 50-00-201, PARA.4A & 4E, PAGE.202-205 & 217-220, FIG.201 & 205

Part: RIB — CRACKED (ZONE 500) · airframe 30,574 hrs · 17,521 cycles

1EA CRACK(7MM) WAS FOUND AT L/H WING CENTER FLAP RIB 27 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE WORK WITH REPAIR ANGLE AND EXTERNAL DOUBLER I.A.W EA NO:6-5750- T0369804 P1, SEQ NO:000760, TITLE:WING-FLIGHT SURFACES-LH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIB26 AND 27 BETWEEN STRINGERS 2.5 AND 2.8-ALI 575306-01 & A300-600F SRM 57- 50-00-201, PARA.4A & 4E, PAGE.202-205 & 217-220, FIG.201 & 205, SEE NRC NO:N00290 JPF FOR MORE DETAIL INFORMATION

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 30,574 hrs · 17,521 cycles

FWD CARGO COMPT #131MG FLOOR PANEL WAS FOUND INSERT DAMAGED. REPLACED THE DAMAGED INSERTS WITH NEW PARTS I.A.W FEDEX DRAWING NO:SRZ-25-005

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 30,574 hrs · 17,521 cycles

FWD CARGO COMPT #131RG FLOOR PANEL WAS FOUND INSERT DAMAGED. REPLACED THE DAMAGED INSERTS WITH NEW PARTS I.A.W FEDEX DRAWING NO:SRZ-25-005

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 30,574 hrs · 17,521 cycles

MAIN DECK FLOOR LONGERON SUPPORT STRUCT UPR SURFACE FOUND CORROSION NEAR FR12A 2",Y 730 REMOVED SUPPORT STRUCT AND INSTALLED NEW SUPPORT STRUCT I.A.W A300-600F SRM 51-72- 10-001, PAGE2 AND 51-40-21-001, PARA 6 , PAGE7B - PAGE23.

Part: RIB — CRACKED (ZONE 600) · airframe 30,574 hrs · 17,521 cycles

1EA CRACK WAS FOUND AT RH WING CENTER FLAP RIB 25AFT AREA. ACCOMPLISHED THE WORK WITH REPAIR ANGLE AND EXTERNAL DOUBLER I.A.W EA NO:6-5750- T0369907 P1 ,SEQ NO:000761 ,TITLE:WING-FLIGHT SURFACES-RH CENTER FLAP ,CRACKS IN UPPER FLANGES OF RIBS 25,26 AND 27 BETWEEN STRINGERS 2.6 AND 2.8-ALI 575306-01 &A300- 600F SRM 57-50-00-201 ,PARA 4A&4E , PAGE202-205 &217-220 ,FIG201 &205.

Part: RIB — CRACKED (ZONE 600) · airframe 30,574 hrs · 17,521 cycles

2EA CRACKS WERE FOUND AT RH WING CENTER FLAP RIB 26AFT AREA. ACCOMPLISHED THE WORK WITH REPAIR ANGLE AND EXTERNAL DOUBLER I.A.W EA NO:6-5750- T0369907 P1 ,SEQ NO:000761 ,TITLE:WING-FLIGHT SURFACES-RH CENTER FLAP ,CRACKS IN UPPER FLANGES OF RIBS 25,26 AND 27 BETWEEN STRINGERS 2.6 AND 2.8-ALI 575306-01 &A300- 600F SRM 57-50-00-201 ,PARA 4A&4E , PAGE202-205 &217-220 ,FIG201 &205. SEE NRC NO:N00213 WO:83289 JPF FOR MORE DETAIL REPAIR INFORMATION.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 30,574 hrs · 17,521 cycles

MAIN DECK WAS FOUND SEAT TRACK CORROSION AT FR14C~ FR17,Y-450 REPLACED THE SEAT TRACK WITH NEW ONE I.A.W A300-600F SRM 51-72-10-001, PAGE.2

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 30,574 hrs · 17,521 cycles

MAIN DECK WAS FOUND SEAT TRACK CORROSION AT FR14 7"~ FR15B 9",Y 450 REPLACED THE SEAT TRACK WITH NEW ONE I.A.W A300-600F SRM 51-72-10-001, PAGE.2

Part: RIB — CRACKED (ZONE 600) · airframe 30,574 hrs · 17,521 cycles

1EA CRACK WAS FOUND AT RH WING CENTER FLAP RIB 27AFT AREA. ACCOMPLISHED THE WORK WITH REPAIR ANGLE AND EXTERNAL DOUBLER I.A.W EA NO:6-5750- T0369907 P1 ,SEQ NO:000761 ,TITLE:WING-FLIGHT SURFACES-RH CENTER FLAP ,CRACKS IN UPPER FLANGES OF RIBS 25,26 AND 27 BETWEEN STRINGERS 2.6 AND 2.8-ALI 575306-01 &A300- 600F SRM 57-50-00-201 ,PARA 4A&4E , PAGE202-205 &217-220 ,FIG201 &205. SEE NRC NO:N00213 WO:83289 JPF FOR MORE DETAIL REPAIR INFORMATION.

Part: SEAT TRACK — NONE (ZONE 200) · airframe 30,574 hrs · 17,521 cycles

FOUND EXISTING SPLICE REPAIR ON MAIN DECK SEAT TRACK BTW FR61-65, Y450 POSITION NOT I.A.W SRM 53-10-16-201 PARA.4 FIG.201. REMOVED THE UNQUALIFIED EXISTING REPAIR & PERFORMED SEAT TRACK SPLICE REPAIR I.A.W A300-600F SRM 53-10-16-201 PARA.4 FIG.201 PAGE.203-208, THIS REPAIR IS CLASSFIED AS A MAJOR CATEGORY A REPAIR. "MAJOR REPAIR"

Part: SEAT TRACK — NONE (ZONE 200) · airframe 30,574 hrs · 17,521 cycles

FOUND EXISTING SPLICE REPAIR ON MAIN DECK SEAT TRACK BTW FR 36~37, -Y1456 POSITION NOT I.A.W SRM 53-10-16-201 PARA.4 FIG.201. REMOVED THE INCORRECT INSTALLED FASTENERS & REPAIRED PER A300-600F SRM 53-10-16-201 PARA.4 FIG.201 PAGE.203-208, THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY A REPAIR.

Part: SEAT TRACK — NONE (ZONE 200) · airframe 30,574 hrs · 17,521 cycles

FOUND EXISTING SPLICE REPAIR ON MAIN DECK SEAT TRACK BTW FR 52~53, -Y450 POSITION NOT I.A.W SRM 53-10-16-201 PARA.4 FIG.201. ACCOMPLISHED THE REPAIR I.A.W FEDEX EA NO:T6-5310-T0370079 P1,TITLE:FUSELAGE- MAINFRAME-EXISTING SEAT TRACK REPAIR BETWEEN FR52 AND FR53 AT -Y450, SEQ NO:000765 &A300-600F SRM 51-40-21-001, PARA.7, PAGE.24-50

Part: SEAT TRACK — NONE (ZONE 200) · airframe 30,574 hrs · 17,521 cycles

FOUND EXISTING SPLICE REPAIR ON MAIN DECK SEAT TRACK BTW FR 56~57.2, Y1456 POSITION NOT I.A.W SRM 53-10-16-201 PARA.4 FIG.201. ACCOMPLISHED THE REPAIR WORK I.A.W. A300-600F SRM 53-10-16-201 PARA.4 FIG.201 P.203-208.

Part: SKIN — UNKNOWN (ZONE 100) · airframe 30,574 hrs · 17,521 cycles

AIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER REPAIR FOUND ON FUSELAGE SKIN AT FR59A,BTWSTGR41R-43R. COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1,TITLE:A300/A310 RPR IDENT & SUPPLEMENTAL MX REQ(SMR)TRK,INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA:A300-600F SRM 53-17-12,CONFIG-2,PAGE 201~210,FIG.201(SHEET1),THIS REPAIR IS CLASSIFIED AS MAJOR CATEGORY B REPAIR.

Part: NONE — NONE (NONE) · airframe 30,574 hrs · 17,521 cycles

THIS NRC IS FOR REWORK, REF TO N00121 FOR REPAIR ASSESSMENT, FOUND EXISTING DOUBLER REPAIR BTW FR20-20A STGR 39R-42R NOT TO BE CURRENT WITH FAA APPROVED SRM DATA 53-13-12-201 PARA.5 PAGE.206-211 FIG.201(SHEET.1).

Part: EPSU — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,106 hrs · 17,247 cycles

MDIS 686 33-50 1477 14JAN22 BUR FACT U EMERGENCY LIGHTS FOR L1 AND L2 DOORS AND COURIER AREA INOP. R/I 14JAN22 15:14 BUR U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: AD-3214-30 POS: 3 SRL: 88700 TAG NBR: 423G32 ON MPN: AD-3214-31 CPN: 3310373 SRL: 243729 TAG NBR: 3H4836 FACT 14JAN22 15:14 BUR U REMOVED AND REPLACED EPSU (29WL1) BATTERY PACK LOCATED BY L1 DOOR PER M/M 33-51-14-04. SYSTEM OPS CHECKS NORMAL.

Part: SLIDE — DETACHED (R1 DOOR) · airframe 28,580 hrs · 16,298 cycles

FOUND R-1 DOOR ESCAPE SLIDE SEPARATED FROM DOOR ATTACH BRACKET. CREW ENTRY DOOR ESCAPE SLIDE R1- REMOVED. INSTALLED ESCAPE SLIDE ON R1 DOOR, IN REF TO AMM 25-61-21-04-0. A/C OK FOR SERVICE.

Part: SLIDE — DETACHED (R1 DOOR) · airframe 28,580 hrs · 16,298 cycles

FOUND R-1 DOOR ESCAPE SLIDE SEPARATED FROM DOOR ATTACH BRACKET. INSTALLED ESCAPE SLIDE ON R1 DOOR IN REF TO AMM 25-61-21-04-0. A/C OK FOR SERVICE.

Part: MODULE — INOPERATIVE (FIRE HANDLE) · airframe 27,999 hrs · 15,962 cycles

NR 2 ENGINE FIRE HANDLE UPPER ROW LIGHT DOES NOT ILLUMINATE DURING FIRE TEST AND LIGHT TEST. R & R THE NR 2 ENGINE FIRE CONTROL MODULE IAW AMM 26-12-20-04. OPS NORMAL.

Part: WIRE HARNESS — MALFUNCTIONED (FIRE LOOP) · airframe 27,912 hrs · 15,899 cycles

ON DESCENT INTO AFW AT 6000' AND 250 KTS, SMOOTH AIR, ENG #1 LOOP A FAULTED, COMPLIED WITH QRH. RELEASED FOR SERVICE PER MEL : 26-12-01-01-A CATEGORY : C EXPIRATION : 21JUN20 "MEL 26-12-01-01-A: ENG 1 LOOP A - INOP. FLIGHT CREW MUST PERFORM FUNCTIONAL TEST OF ENG FIRE WARNING SYSTEM PRIOR TO EACH DEPARTURE." WORKED IN CONJUNCTION WITH TSI 26-10/9894. REMOVED AND REPLACED BOTH LH AND RH UPPER TURBINE LOOPS AS PER A300 AMM 26-12-12-04-02. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.

Part: WIRE HARNESS — FAULTED (NR 2 FIRE LOOP) · airframe 27,912 hrs · 15,899 cycles

DURING CLIMB OUT, NUMEROUS BRIEF ECAM WARNINGS OF NR 2 ENG B LOOP FAULT. ONCE LEVEL AT CRUISE AND POWER REDUCED, WARNINGS STOPPED. CLOSED AND SECURED NR 2 ENGINE FAN, REVERSER AND CORE COWLS IAW MM 71-10-00, RAN NR 2 ENGINE IAW JRH FOR OVER 20 MINUTE'S AND RAN TO PRACTICAL POWER WITH NO FIRE LOOP ISSUE'S NOTED, OK FOR SERVICE. R & R THE WIRE HARNESS.

Part: FIRE LOOP — FAULTED (NR 1 ENGINE) · airframe 27,912 hrs · 15,899 cycles

ON DESCENT INTO AFW AT 6000' AND 250 KTS, SMOOTH AIR, ENG NR 1 LOOP A FAULTED, COMPLIED WITH QRH. RELEASED FOR SERVICE PER MEL : 26-12-01-01-A CATEGORY : C EXPIRATION : 21JUN20 "MEL 26-12-01-01-A: ENG 1 LOOP A - INOP. FLIGHT CREW MUST PERFORM FUNCTIONAL TEST OF ENG FIRE WARNING SYSTEM PRIOR TO EACH DEPARTURE.

Part: PITOT LINE — OBSTRUCTED (PITOT/STATIC SYS) · airframe 27,896 hrs · 15,883 cycles

ABORTED TAKEOFF AT 100KIAS ON CAPT'S PFD. FIRST OFFICERS AIRSPEED INDICATION READ 70KIAS. FLUSHED CAPT AND FIRST OFFICER`S PITOT PRESSURE LINES IAW AMM 34-10-00-03. FOUND DEBRIS (BURNT FLYING BUG NEST AND BUGS) PURGED FROM FIRST OFFICERS LINE FUNCTIONAL TEST OF ADC 1 & ADC 2 PITOT SYSTEM, GOOD IAW AMM 34-10-00-05. SYSTEM OK FOR SERVICE.

Part: SPAR — CRACKED (FRAME 47) · airframe 27,476 hrs · 15,641 cycles

INSPECTION OF CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE, RH SIDE, FOUND HOLE D WITH CRACK SIGNAL REPAIRED THE CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE, RH SIDE, CRACKED HOLE D PER EA: 6-5710-T0352050 P1. EA TITLE: WINGS - BASIC WING STRUCTURE - CRACK HOLES AT FR47 - SB57-6086 EMBODIMENT. MAJOR REPAIR IAW FEDEX GMM6-2-100

Part: ANGLE — CRACKED (FRAME 47) · airframe 27,476 hrs · 15,641 cycles

INSPECTION OF CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE, LH SIDE, FOUND HOLE G WITH CRACK SIGNAL REPAIRED THE CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE, LH SIDE, CRACKED HOLE G PER EA: 6-5710-T0352050 P1. EA TITLE: WINGS - BASIC WING STRUCTURE - CRACK HOLES AT FR47 - SB57-6086 EMBODIMENT. MAJOR REPAIR IAW FEDEX GMM6-2-100

Part: WEB — CRACKED (FRAME 47) · airframe 27,476 hrs · 15,641 cycles

MAIN DECK FR47 UNDERFLOOR WEB BETWEEN Y953 AND Y1456 CRACKED REPAIRED THE CRACKED WEB OF MAIN DECK FR47 UNDERFLOOR BETWEEN Y953 AND Y1456 PER A300-600F SRM53-15-15-C2-201 PARA.5. THE REPAIR WAS CATEGORY B AND IT MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI 53-15-15-2-002-00. INSPECTION THRESHOLD FROM REPAIR EMBODIMENT: 24000FC. SUBSEQUENT INSPECTION AT INTERVAL OF 3000FC UNTIL 42500FC. INSPECTION METHOD: DETAILED VISUAL. MAJOR REPAIR IAW FEDEX GMM6-2-100.

Part: WEB — CRACKED (FRAME 47) · airframe 27,476 hrs · 15,641 cycles

MAIN DECK FR47 UNDERFLOOR WEB BETWEEN Y0 AND Y450 CRACKED REPAIRED THE CRACKED WEB OF MAIN DECK FR47 UNDERFLOOR BETWEEN Y0 AND Y450 PER A300-600F SRM53-15-15-C2-201 PARA.5. THE REPAIR WAS CATEGORY B AND IT MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI 53-15-15-2-002-00. INSPECTION THRESHOLD FROM REPAIR EMBODIMENT: 24000FC. SUBSEQUENT INSPECTION AT INTERVAL OF 3000FC UNTIL 42500FC. INSPECTION METHOD: DETAILED VISUAL. MAJOR REPAIR IAW FEDEX GMM6-2-100.

Part: WEB — CRACKED (FRAME 47) · airframe 27,476 hrs · 15,641 cycles

MAIN DECK FR47 UNDERFLOOR WEB BETWEEN Y0 AND -Y450 CRACKED REPAIRED THE CRACKED WEB OF MAIN DECK FR47 UNDERFLOOR BETWEEN Y0 AND -Y450 PER A300-600F SRM53-15-15-C2-201 PARA.5. THE REPAIR WAS CATEGORY B AND IT MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI 53-15-15-2-002-00. INSPECTION THRESHOLD FROM REPAIR EMBODIMENT: 24000FC. SUBSEQUENT INSPECTION AT INTERVAL OF 3000FC UNTIL 42500FC. INSPECTION METHOD: DETAILED VISUAL. MAJOR REPAIR IAW FEDEX GMM6-2-100.

Part: FLOORBEAM — CRACKED (FRAME 31) · airframe 27,476 hrs · 15,641 cycles

MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR31, BETWEEN -Y450 AND -Y953 REPAIRED THE CRACKED CROSSBEAM OF MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE AT FR31 BETWEEN -Y450 AND -Y953 PER A300-600F SRM53-10-15 FIG212 AND EA: 6-5310-T0351820 P1. EA TITLE: FUSELAGE - MAINFRAME - CRACK ON FR31 CROSSBEAM, BETWEEN -Y450 AND -Y953. MAJOR REPAIR IAW FEDEX GMM6-2-100

Part: FLOORBEAM — CRACKED (FRAME 30) · airframe 27,476 hrs · 15,641 cycles

MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR30, BETWEEN -Y450 AND -Y953 REPAIRED THE CRACKED CROSSBEAM OF MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE AT FR30 BETWEEN -Y450 AND -Y953 PER A300-600F SRM53-10-15 FIG212 AND EA: 6-5310-T0351819 P1. EA TITLE: FUSELAGE - MAINFRAME - CRACK ON FR30 CROSSBEAM, BETWEEN -Y450 AND -Y953. MAJOR REPAIR IAW FEDEX GMM6-2-100

Part: FLOORBEAM — CRACKED (FRAME 57.3) · airframe 27,476 hrs · 15,641 cycles

MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR57.3, BETWEEN Y1456 AND Y1959 REPAIRED THE CRACKED CROSSBEAM OF MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE AT FR57.3 BETWEEN Y1456 AND Y1959 PER A300-600F SRM53-10-15 FIG211. MAJOR REPAIR IAW FEDEX GMM6-2-100

Part: FLOORBEAM — CRACKED (FRAME 64) · airframe 27,476 hrs · 15,641 cycles

MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR64, BETWEEN Y1456 AND Y1959 REPAIRED THE CRACKED CROSSBEAM OF MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE AT FR64 BETWEEN Y1456 AND Y1959 PER A300-600F SRM53-10-15 FIG211. MAJOR REPAIR IAW FEDEX GMM6-2-100

Part: FILTER — ODOR (COCKPIT) · airframe 27,078 hrs · 15,395 cycles

PDIS 686 21-50 9237 14SEP19 MEM FACT U LOGPAGES:3143852 AFTER TALE-OFF @ KSDF, FUMES/ODORS FROM A/C PACKS WITH ECON SELECTED ON OVHD PANEL, DESELECTED ECON FLOW BUT STILL LINGERING FUMES/ODORS. FACT 14SEP19 16:40 MEM U R/R FILTER FOR THE FLIGHT COMPARTMENT IAW AMM 21-21-16-04. A/C OK FOR SERVICE.

Part: SUPPORT — DAMAGED (MLG) · airframe 26,679 hrs · 15,073 cycles

GEAR WOUL NOT RETRACT ON T/O SYS1. SWITCHED TO SYS 2 AND GEAR WOULD NOT RETRACT. GEAR LEVER WOULD NOT MOVE PAST CENTER DETENT. TSM: 32-30-00 FIG.109 AND FOUND NO CONTINUITY BETWEEN PIN H AND PIN K, LANDING GEAR CONTROL LEVER TO BE REPLACED. LANDING GEAR CONTROL UNIT 2GA REPLACED AS REQUIRED GENERAL VISUAL INSPECTION OF LDG SENSOR CARRIED OUT FOR PRECAUTIONS DUE TO REPETITIVE ITEM (INSPECTION REF AMM 32 00-00-04). DURING INSPECTION FOUND LH MLG BOGIE BEAM PROX SNSR NOT IN CORRECT POSITION DUE TO BRACKET ASSEMBLY BROKEN. REF AMM 32-00-00-04 FIG 402 ITEM 36. NEW BRACKET INSTALLED, PERFORMED PROX SWITCHED 9GA AND 11GA ADJUSTMENT TEST AS PER AMM 32-00-00-04. PERFORMED LDG GEAR RETRACTION AND EXTENTION ON BOTH SYSTEM AS PER AMM 32-00-00-05. ALL TESTS PASSED.

Part: NONE — NONE · airframe 25,965 hrs · 14,555 cycles

MAIN CABIN UNDER FLOOR PANEL 232UG SEAT TRACK HAS A SPOT OF CORROSION ON THE SIDE JUST AFT OF THE SEAT TRACK SPLICE, FR26 TO 27, O/B TRACK REMOVED DAMAGE ABD EVALUATED DAMAGE AREA IAW A300-600 SRM 51-10-16. MAX RE-WORK DEPTH PER SRM IS .012", DEPTH ON AIRCRAFT IS .009", DAMAGE IS IN LIMITS PER A300-600 SRM 53-10-16. RESTORED PROTECTIVE FINISH IAW A300-600 SRM 51-75-10.

Part: GCU — DAMAGED (AVIONICS) · airframe 26,457 hrs · 14,865 cycles

MDIS 686 05-50 8095 28NOV18 CDG OPEN U REPEAT:FOUND WATER IN AVIONICS COMPARTMENT,CAUSES BOTH GENERATORS FAILURES .SEE MM 05-50-01-00 PDIS 686 24-20 8094 28NOV18 CDG OPEN LOGPAGES:3020421 BOTH GENS FAULTED AFTER BLOCK OUT. GCU#1 REPLACED, GCU#2 REPLACED AND PRECAUTIONARY REPLACED GCU APU. ENTRY AREA FLOOR PANELS RESEALED ACCOMPLISHED EA 6-0550-T0343806.

Part: GCU — DAMAGED (NR 1) · airframe 26,393 hrs · 14,812 cycles

NR 2 GENERATOR FAULT ILLUMINATED DURING TAKEOFF ROLL, NR 1 GENERATOR FAULT ILLUMINATED DURING CLIMB OUT OF 2000 FT WITH ECAM. PERFORMED QRH AND RECOVERED THE NR 1 GENERATOR. R & R NR 2 GCU IAW AMM 24-22-12-04, OPS CHECKED NORMAL, OK FOR SERVICE. RAN THE NR 2 ENGINE IAW JRH, GENERATOR CARRIED A LOAD. R & R THE NR 1 ENGINE GCU IAW AMM 24-22-12-04, OPS CHECKED NORMAL, OK FOR SERVICE. RAN THE NR 1 & 2 ENGINES IAW JRH. OPS CHECKED NORMAL, OK FOR SERVICE.

Part: GCU — MALFUNCTIONED (NR 1) · airframe 26,393 hrs · 14,812 cycles

NR 2 GENERATOR FAULT ILLUMINATED DURING TAKEOFF ROLL, AND THE NR 1 GENERATOR FAULT ILLUMINATED DURING CLIMB OUT OF 2000 FT WITH ECAM. PERFORMED QRH AND RECOVERED THE NR 1 GENERATOR. INSPECTED THE E & E ON A POST FLIGHT AND FOUND NO OBVIOUS WATER INTRUSION. PERFORMED A WATER ACCUMULATION CHECK IN THE E & E IAW AMM 05-50-01-00. E & E WAS DRY, FOUND SLIGHT SEEP JUST ABOVE GCU RACKS. DRAIN PAN AND DRAIN HOSE ABOVE GCUS WERE INSTALLED AND INTACT. PERFORMED A BITE OF GPCU IAW IAW AMM 24-41-00. LAST FLIGHT LEG FAULTS BOTH GCUS. R & R THE NR 1 GCU IAW AMM 24-22-12-04, OPS CHECKED NORMAL, OK FOR SERVICE. RAN THE NR 1 & 2 ENGINES IAW JRH. OPS CHECKED NORMAL. OK FOR SERVICE.

Part: GCU — FAULTED (NR 2) · airframe 26,118 hrs · 14,648 cycles

NR 2 ENGINE GENERATOR FAULTED DURING TAKEOFF ROLL AT 80 KTS. TAXIED TO THE RAMP. REMOVED AND REPLACED THE NR 2 GCU IAW AMM 24-22-12-04. PERFORMED AN ENGINE RUN IAW JRH AND AMM 24-22-12-04. THE NR 2 GCU HAD GOOD FREQUENCIES AND VOLTS IAW JRH.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 25,965 hrs · 14,555 cycles

PANEL 231YG HAS NUMEROUS AREAS OF EDGE DAMAGE. FABRICATED NEW PNL 231YG, LOCATED HOLES, INSTALLED INSERTS AND POTTED EDGES IAW DWG SRZ-25-005 REV N.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 25,965 hrs · 14,555 cycles

MAIN CABIN FLOOR PANEL 232YG HAS CRUSHED AREAS SEVERAL PLACES. FABRICATED NEW FLOORBOARD 232YG IAW DWG SRZ-25-005 REV M AND GMM 7-0-1000.

Part: FLOOR PANEL — PERFORATED (CABIN) · airframe 25,965 hrs · 14,555 cycles

MAIN CABIN FLOOR PANEL 232FG HAS LONG AREA OF PERFORATIONS JUST FWD OF DRAIN. FABRICATED NEW PANEL 232FG IAW DWG SRZ-25-005 REV M AND GMM 7-0-1000.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO BAY) · airframe 25,965 hrs · 14,555 cycles

MAIN CARGO FLOOR PANEL 221LF HAS A SMALL PUNCTURE DAMAGE, FWD SIDE. FABRICATED NEW PANEL 221LF IAW DWG SRZ-25-005 REV M AND GMM 7-0-1000.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 25,965 hrs · 14,555 cycles

MAIN CARGO COMPARTMENT FLOOR PANEL 231FF HAS DAMAGE TO UPPER SURFACE. FABRICATED NEW PANEL 231FF IAW DWG SRZ-25-005 REV M AND GMM 7-0-1000.

Part: FLOOR PANEL — PUNCTURED (ZONE 100) · airframe 25,965 hrs · 14,555 cycles

MAIN CABIN FLOOR PANEL 221QF HAS PUNCTURE DAMAGE. FABRICATED MAIN CABIN FLOOR PANEL 221QF IAW DWG SRZ-25-005 AND GMM 7-0-1000.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 25,965 hrs · 14,555 cycles

MAIN CABIN FLOOR PANEL 232WG IS CRACKED. FABRICATED NEW FLOORBOARD 232WG IAW DWG SRZ-25-005 REV M AND GMM 7-0-1000.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 25,965 hrs · 14,555 cycles

MAIN CABIN FLOOR PANEL 231FH HAS AREA THAT IS CRUSHED / DELAMINATED. FABRICATED PANEL 231FH IAW DWG SRZ-25-005 AND GMM 7-0-1000.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 25,965 hrs · 14,555 cycles

MAIN CABIN FLOOR PANEL 231YG HAS EDGE DAMAGE, INBOARD FWD END FABRICATED NEW PANEL 231YG IAW DWG SRZ-25-005 REV M AND GMM 7-0-1000.

Part: SEAT TRACK — CORRODED (N/A) · airframe 25,965 hrs · 14,555 cycles

MAIN CABIN UNDER FLOOR PANEL 232UG SEAT TRACK HAS A SPOT OF CORROSION ON THE SIDE JUST AFT OF THE SEAT TRACK SPLICE, FR26 TO 27, O/B TRACK REMOVED DAMAGE ABD EVALUATED DAMAGE AREA IAW A300-600 SRM 51-10-16. MAX RE-WORK DEPTH PER SRM IS .012", DEPTH ON AIRCRAFT IS .009", DAMAGE IS IN LIMITS PER A300-600 SRM 53-10-16. RESTORED PROTECTIVE FINISH IAW A300-600 SRM 51-75-10.

Part: FLOOR PANEL — CRUSHED (ZONE 200) · airframe 25,965 hrs · 14,555 cycles

MAIN CABIN FLOOR PANEL 232NG HAS CRUSHED AREAS SEVERAL PLACES. FABRICATED NEW FLOORBOARD 232NG IAW DWG SRZ-25-005 REV M AND GMM 7-0-1000.

Part: PANEL — CRACKED (ZONE 200) · airframe 25,965 hrs · 14,555 cycles

MAIN CABIN FLOOR PANEL 231LG IS CRACKED. FABRICATED NEW FLOORBOARD PANEL 231LG PER DWG SRZ-25-005 REV M AND GMM 7-0-1000.

Part: FLOOR PANEL — CRUSHED (CABIN) · airframe 25,965 hrs · 14,555 cycles

MAIN CABIN FLOOR PANEL 232TG HAS CRUSHED AREAS SEVERAL PLACES. FABRICATED PANEL 232TG IAW DWG SRZ-25-005 REV M AND GMM 7-0-1000.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 25,965 hrs · 14,555 cycles

MAIN CABIN FLOOR PANEL 232RG IS CRACKED AT AFT INBOARD END. FABRICATED NEW FLOORBOARD 232RG IAW DWG SRZ-25-005 REV M AND GMM 7-0-1000

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 25,965 hrs · 14,555 cycles

MAIN CABIN FLOOR PANEL 231RG IS CRACKED AND HAS SEVERAL AREAS OF DAMAGE. FABRICATED PANEL 231RG IAW SRZ-25-005 REV M AND GMM 7-0-1000.

Part: FLOOR PANEL — CRUSHED (ZONE 200) · airframe 25,965 hrs · 14,555 cycles

MAIN CABIN FLOOR PANEL HG HAS CRUSHED AREAS SEVERAL PLACES. FABRICATED NEW FLOORBOARD 232HG IAW DWG SRZ-25-005 REV M AND GMM 7-0-1000.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 25,965 hrs · 14,555 cycles

MAIN CABIN FLOOR PANEL 231NG IS CRACKED. FABRICATED NEW PANEL 231NG IAW DWG SRZ-25-005 REV M AND GMM 7-0-1000.

Part: SLAT TRACK — GOUGED (RT WING) · airframe 24,743 hrs · 13,813 cycles

RIGHT WING NR 1 SLAT LOWER SURFACE OTBD OF THE NR 3 TRACK GOUGED. COMPLED WITH EA 6-5750-T033381 PT1 STEPS 1-9. MAJOR REPAIR.

Part: BRACKET — CORRODED (FRAME 26) · corrosion level 3 · airframe 24,743 hrs · 13,813 cycles

MAIN DECK, FRAME26, Y37.52 TO Y17.72 HAS CORROSION ON THE PRESSURE DECK. REMOVED CORROSION ON THRUST BRACKET IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW SRM 53-13-15. NO ALLOWABLE LIMITS. FABRICATED A NEW THRUST BRACKET IAW SRM 51-40-21, AND DWG A53781984. INSTALLED A NEW THRUST BRACKET IAW SRM 51-40-21. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 24,743 hrs · 13,813 cycles

MDCC 252ZH FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL ON T17/1282709 IAW SRZ 25-005.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 24,743 hrs · 13,813 cycles

FLOOR PANEL 131MG FWD CARGO BAY IS DAMAGED. FABRICATED A NEW FLOOR PANEL ON T17/1282969. CAT A MAJOR REPAIR.

Part: STRINGER — CORRODED (FRAMES 38-39) · corrosion level 3 · airframe 24,743 hrs · 13,813 cycles

FWD CARGO RT SIDE BETWEEN FR38 - FR39 STR 45R HAS CORROSION. REPAIRED STR 45R FR39 IAW SRM 53-10-14 FIG 208 P/N DAN50-02 MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 24,743 hrs · 13,813 cycles

MDCC 252ZH FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL ON T17/1282709 IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 24,743 hrs · 13,813 cycles

MDCC 251WH FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL ON T17/1282711 IAW SRZ 25-005.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 24,743 hrs · 13,813 cycles

MDCC 242SF FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL ON T17/1282736 IAW SRZ 25-005.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 24,743 hrs · 13,813 cycles

MDCC 252BF FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL ON T17/1283165 IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 24,743 hrs · 13,813 cycles

FLOOR PANEL 152WF IS DAMAGED. FABRICATED NEW PANEL ON T17/1282934 CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 24,743 hrs · 13,813 cycles

FLOOR PANEL 131SG FWD CARGO BAY DAMAGED. FABRICATED A NEW FLOOR PANEL ON T17/1283162. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 24,743 hrs · 13,813 cycles

FLOOR PANEL 131PG FWD CARGO BAY IS DAMAGED. FABRICATED A NEW FLOOR PANEL ON T17/1282970 PANEL INSTALLED ON WORKCARD 130-FL-FIT. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 24,743 hrs · 13,813 cycles

MDCC 252UH FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL ON T17/1282710 IAW SRZ 25-005.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 24,743 hrs · 13,813 cycles

FLOOR PANEL 131RG FWD CARGO BAY IS DAMAGED. FABRICATED A NEW FLOOR PANEL ON T17/1283022 CAT REPAIR. PANEL INSTALLED ON WORKCARD. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 24,743 hrs · 13,813 cycles

MDCC 252PH FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL ON T17/1282705 IAW SRZ 25-005.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 24,743 hrs · 13,813 cycles

FLOOR PANEL 151PF AFT CARGO BAY IS DAMAGED. FABRICATED NEW FLOOR PANEL 151PF ON T17/1282932 CAT A MAJOR REPAIR IAW SRZ 25-00.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 24,743 hrs · 13,813 cycles

FLOOR PANEL 132NG FWD CARGO BAY IS DAMAGED. FABRICATED A NEW FLOOR PANEL ON T17/1282890 CAT MAJOR REPAIR. INSTALLED ON WORKCARD.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 24,743 hrs · 13,813 cycles

FLOOR PANEL 132SG FWD CARGO BAY IS DAMAGED. FABRICATED A NEW FLOOR PANEL ON CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 24,743 hrs · 13,813 cycles

MDCC 252VF FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL P/N B5327028000800 IAW SRZ 25-005 ON T17 / 1283169. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 24,743 hrs · 13,813 cycles

MDCC 232CF FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL ON T17/1282734 IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 24,743 hrs · 13,813 cycles

FLOOR PANEL 151UF AFT PIT IS DAMAGED. FABRICATED NEW PANEL 151UF ON T17/`282947 CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 24,743 hrs · 13,813 cycles

FLOOR PANEL 132QG FWD CARGO BAY IS DAMAGED. FABRICATED A NEW FLOOR PANEL ON T17/1283021 CAT REPAIR. INSTALLED PANEL ON WORKCARD, MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 24,743 hrs · 13,813 cycles

MDCC 252GF FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL P/N B5327027300000 IAW SRZ 25-005 ON T17/1283170. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 24,743 hrs · 13,813 cycles

FLOOR PANEL 132LG FWD CARGO BAY IS DAMAGED. FABRICATED A NEW FLOOR PANEL ON T17/1283164. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 24,743 hrs · 13,813 cycles

FLOOR PANEL 152QF AFT CARGO BAY IS DAMAGED. FABRICATED A NEW FLOOR PANEL IAW T17-1282936. CAT A MAJOR REPAIR.

Part: DECK PLATE — CORRODED (FRAME 25) · corrosion level 2 · airframe 24,743 hrs · 13,813 cycles

MAIN CARGO DECK, JUST AFT OF FRAME 25 & BETWEEN Y 0 & -Y450, FLOOR PRESSURE DECK PLATE HAS CORROSION. REMOVED AND REPLACED PRESSURE DECK PLATE IAW SRM 51-40-21.

Part: CONTROL PANEL — NO TEST (FIRE DETECTION) · airframe 24,394 hrs · 13,594 cycles

NR 2 ENGINE OVERHEAD FIRE CONTROL PANEL, AGENT 2 SQUIB LIGHT WILL NOT TEST. REMOVED AND REPLACED NR 2 ENGINE FIRE CONTROL MODULE AND TESTED IAW AMM 26-12-20. OPS CHECKED GOOD.

Part: INDICATION SYS — MALFUNCTIONED (FUEL QTY) · airframe 24,259 hrs · 13,499 cycles

TRIM TANK ISOLATION VALVE NOT OPEN, ACCOMPANIED BY ALL X'S ON ECAM FUEL PAGE, TOTAL FUEL INDICATION, AND CG/GW INDICATIONS. ALSO,RT INNER AND RT OUTER INDICATIONS ON BACK-UP FUEL INDICATORS WERE BLANK. DIAGNOSED AS AN FQI FAULT. TRIPPED AND RESET CIRCUIT BREAKERS P60 AND P61 ON 132VU PANEL, THE FAULT CLEARED. PREFORMED AN OPERATIONAL (BITE) TEST IAW AMM 28-42-00-05-02, ONLY FAULT CODE 631, ACTUATOR 1 NOT INSTALLED. SYSTEM OPS NORMAL, ACFT OK TO CONTINUE.

Part: SKIN — DENTED (RT WING SLAT) · airframe 24,085 hrs · 13,404 cycles

NR 1 RT WING SLAT LEADING EDGE SKIN DENTED. REPAIRED THE NR 1 SLAT IAW SRM 57-42-11 FIG 203.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 23,636 hrs · 13,104 cycles

LANDING GEAR WOULD NOT RETRACT. GEAR HANDLE DID MOVE PAST INTERLOCK TO UP POSITION, BUT GEAR DID NOT RETRACT. NO ABNORMAL GEAR POSITION INDICATIONS SHOWN. INSTALLED THREE EACH GEAR PINS. JACKED ACFT IAW MM 07-11-00-00 & RETRACTED GEAR SEVERAL TIMES IAW AMM 32-31- 00-05 ON SYS 1 & 2 WITH NO FAULTS INDICATED. NO PROBLEMS FOUND ON PITCH DAMPERS, BUTTONS WERE NOT POPPED & NO FAULT LIGHTS OR CODES ON THE PROXIMITY BOX. ACFT OK FOR SERVICE.

Part: SEAT TRACK — WORN (FRAMES 60-61) · airframe 221 hrs · 12,212 cycles

MDCC FRAMES 60 - 61, Y1456 SEAT TRACK WORN. REPAIRED THE SEAT TRACK IAW SRM 53-10-16 FIGURE 201. THIS REPAIR IS CATEGORY A. AND LOADING SYS TEST OK. MAJOR REPAIR IAW GMM 6-2-100.

Part: SKIN — PUNCTURED (RT WING TE FLAP) · airframe 221 hrs · 12,212 cycles

RIGHT WING INBD FLAP LOWER SKIN BETWEEN RIB 12 - 13 FOUND ONE EACH PUNCTURE. REPAIRED IAW SRM 57-50-00 PARA. 4E. MAJOR REPAIR IAW GMM 6-2-100.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 221 hrs · 12,212 cycles

FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STRINGER 24 - 26 LT, INSPECTION FOUND FASTENER HOLE L WITH CRACK SIGNAL. COMPLIED WITH EA 6-5310-T0315451 PT1. REPAIRED FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STGR24-26 LT, FASTENER HOLE "L". THIS REPAIR IS CATEGORY B. MAJOR REPAIR IAW GMM 6-2-100

Part: SPLICE — CRACKED (FUSELAGE) · airframe 221 hrs · 12,212 cycles

FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STRINGER 24 - 26 LT, INSPECTION FOUND FASTENER HOLE B WITH CRACK SIGNAL. COMPLIED WITH EA 6-5310-T0315451 PT1. REPAIRED FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STGR24-26 LT, FASTENER HOLE "B". THIS REPAIR IS CATEGORY B. MAJOR REPAIR IAW GMM 6-2-100

Part: SPLICE — CRACKED (FUSELAGE) · airframe 221 hrs · 12,212 cycles

FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STRINGER 24 - 26 LT, INSPECTION FOUND FASTENER HOLE A WITH CRACK SIGNAL. REPAIRED FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STR 24-26 LT, FASTENER HOLE "A". THIS REPAIR IS CATEGORY B. MAJOR REPAIR IAW GMM 6-2-100

Part: STRUCTURE — CRACKED (WING) · airframe 221 hrs · 12,212 cycles

FRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION INSPECTION, RT MID BOLT HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0315522 PT 1. REPAIR FRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, RT MID BOLT HOLE. THIS REPAIR IS CATEGORY C. MAJOR REPAIR IAW GMM 6-2-100.

Part: STRUCTURE — CRACKED (WING) · airframe 221 hrs · 12,212 cycles

FRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION INSPECTION, RT LOWER BOLT HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0315522 PT 1. REPAIR FRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, RT LOWER BOLT HOLE. THIS REPAIR IS CATEGORY C. MAJOR REPAIR IAW GMM 6-2-100.

Part: ADC — FAULTY (NR 1) · airframe 21,136 hrs · 11,677 cycles

REPEAT, CAPTAIN`S ALTIMETER FAULTED WHEN PULLED TO STANDARD. UNABLE TO SILENCE THE CONTINUAL CHIME & WARNING SEQUENCE UNTIL RETURNED TO BARO POSITION, ECAM WARNINGS INCLUDED. AFTER LANDING IN BARO POSITION, THE WARNING REPEATED THEN CLEARED AS WE SLOWED BELOW 40 KIAS ON ROLL OUT. R & R CAPTAIN`S ALTIMETER IAW MM CHAPT 4-12-21-04. OPERATIONS CHECKED IAW MM CHAPT 34-10-00-5, ALSO R & R NR 1 ADC IAW MM CHAPT 34-11-34-04. WHILE PERFORMING INPUTS & BITE CHECK OF THE EFIS SYS NOTICED INPUT FAULT CONTROL PANEL NR 1. R & R NR 1 EFIS CONTROL PANEL IAW MM CHAPT 34-73-11-04. OPERATIONS CHECKED IAW MM CHAPT 34-71-00 P501. INSPECTED STATIC DRAINS FOR CONTAMINATION NONE FOUND. ALL TEST PASSED, ACFT OK FOR SERVICE.

Part: PROXIMITY SENSOR — INOPERATIVE (LANDING GEAR) · airframe 21,136 hrs · 11,676 cycles

CAPTAINS ALTIMETER FAULTED WHEN PULLED TO STANDARD. UNABLE TO SILENCE THE CONTINUAL CHIME & WARNING SEQUENCE UNTIL RETURNED TO BARO POSITION. INCLUDED ECAM WARNINGS. AFTER LANDING IN BARO POSITION THE WARNING REPEATED. R & R PROXIMITY DETECTOR UNIT IAW MM 32-31-71-04. ALL OPERATIONS CHECKED NORMAL. ACFT OK FOR SERVICE. ALSO BITE TEST CAPTAIN`S ALT IAW 34-10-00-05, ALL OPERATIONS CHECKED GOOD.

Part: VALVE — FAILED (NR 1 ENGINE) · airframe 20,688 hrs · 11,425 cycles

AFTER TAKEOFF AT APPROXIMATELY 2000 FT, RECEIVED ECAM WARNING, NR 1 ENG RUN, BLEED, TEMPERTURE KEPT RISING UNTIL NR 1 PACK TRIPPED, RECEIVED A AVIONICS SMOKE & MIN EQUIPMENT WARNINGS, ALONG WITH ASSOCIATED AURAL WARNINGS. REPEATED SEVERAL TIMES. NR 1 PNUEMATIC CONTROLLER SHOWS NR 1 ENGINE FAN AIR VALVE FAULT. REMOVED NR 1 FAN AIR VALVE IAW MM 36-11-16-04-02.

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 20,685 hrs · 11,422 cycles

AT FL 350, CAPTAIN`S FRONT WINDSHIELD BEGAN TO ARC. TURN SWITCH OFF TO SECURE WINDOW. R & R WINDOW IAW AMM 56-11-11-04. OPS CHECKED TEMP CONTROL UNIT PER AMM 30-42-00,P BLOCK 501. TESTED GOOD. OPS CHECKED WINDOW HEAT PROTECTION UNIT PER AMM 30-42-00 P BLOCK 501 CHECKED GOOD.WINDOW CHECKED GOOD DURING WINDSHIELD PANEL ANTI-ICING AND DE-FOGGING OPS TEST PER 30-42-00,P BLOCK 501. ACFT OK FOR SERVICE.

Part: FRAME — DAMAGED (ZONE 600) · airframe 18,830 hrs · 10,372 cycles

DURING SB A300-57-6086 ACCOMPLISHMENT, DAMAGE FOUND IN HOLE "P" AT FRAME 47 RT SIDE. DAMAGE WAS NOTED IN THE TEE AND SPAR. REMOVED NOMINAL FASTENER FROM HOLE "P" AT FRAME 47 RT SIDE, VERIFIED DAMAGE IN UPPER 2 LAYERS (TEE AND SPAR), OVERSIZED ALL FIVE LAYERS OF HOLE "P" TO 20.345MM. NDT VERIFIED NO DAMAGE REMAINING IN HOLE IAW NTM 51-10-01. FABRICATED ONE SHOULDERED, ONE COUNTERSUNK, AND THREE STRAIGHT BUSHINGS. INSTALLED FIVE BUSHINGS IN HOLE "P", COUNTERDRILLED ALL FIVE BUSHINGS TO 14.275MM AND INSTALLED ONE NOMINAL FASTENER IN TRANSITION FIT. ALL STEPS IAW EA 6-5710-157874. COMPLIED WITH EA 6-5710-157874 PT 1 WINGS AD 2005-23-08.

Part: WEB — DAMAGED (LT MLG WW) · airframe 18,830 hrs · 10,372 cycles

MLG WHEEL WELL, LT SIDE VERTICAL KEEL BEAM WEB HAS PUNCTURE DAMAGE, APPROX 1.0 X 1.7 ADJACENT TO MLG DOOR FWD HINGE FITTING. REPAIRED DAMAGED AREA IAW EA6-5310-7-160189 FUSELAGE LT KEEL BEAM WEB AT MLG DOOR FWD HINGE REPAIR. OPS CHECK/ADJUSTMENT OF LT MLG DOOR GOOD IAW AMM 32-12-11-05, GEAR NORMAL EXTENSION RETRACTION CHECKED GOOD IAW AMM 32-31-00-05. REF WRI 53100923

Part: ATTACH ANGLE — CRACKED (ZONE 300) · airframe 18,830 hrs · 10,372 cycles

ATTACH ANGLE FOR THE TRAILING EDGE PANEL ATTACHMENT RIB "RT" IS CRACKED .400", OFF ACFT PART. R & R UPPER ATTACH ANGLE ON RT SIDE OF HORIZONTAL STAB REAR SPAR AT RIB 5 8" IAW SRM 51-40-21. FABRICATED ATTACH ANGLE IAW SRM 55-13-11 AND DWG A55177134. LOCATED AND DRILLED ATTACH ANGLE IAW SRM 51-40-40 AND 51-72-10.

Part: SKIN — DENTED (RT AILERON) · airframe 18,830 hrs · 10,372 cycles

RT AILERON LOWER SURFACE T/E SKIN HAS A 18.0" X 0.500" X 0.130" DEEP DENT. DENT FOUND TO BE OUT OF LIMITS IAW SRM 57-61-11, PB 201, PARA E. REPAIRED DENT IAW SRM 51-77-12, PARA 4 D. AND 4 A. (5). RESTORED PROTECTIVE COATING IAW SRM 51-75-10 PARA 3 A.

Part: SKIN — DENTED (RT AILERON) · airframe 18,830 hrs · 10,372 cycles

RT WING AILERON HAS TWO DENTS ON LOWER SURFACE. DENTS MEASURED 0.500 X 0.500 X 0.023 DEEP AND 1.00 X 1.00 X 0.019 DEEP. ONE DENT FOUND TO BE OUT OF LIMITS IAW SRM 57-61-11 PB 201, PARA E. REPAIRED BOTH DENTS IAW SRM 51-77-12 PAR 4.D. AND 4.A.(5) PAGES 292 AND 274. RESTORED PROTECTIVE COATING IAW SRM 51-75-10, PARA 3.A.

Part: ANGLE — CRACKED (LT WING) · airframe 18,830 hrs · 10,372 cycles

LEFT WING KREUGER FLAP WELL IN WING LE IB UPPER RIB JUST OB OF KREUGER ACTUATOR CRACKED 2.5 IN. IN THE RADIUS. REMOVED AND REPLACED REINFORCING ANGLE IAW SRM 51-40-21

Part: CROSSBEAM — DENTED (K FLAP) · airframe 18,830 hrs · 10,372 cycles

UPON REMOVAL OF LT WING KRUGER FLAP 1 EA DENTED AREA APPROX 2 IN LONG WAS NOTED ON SUPPORT WEB JUST ABOVE KRUGER FLAP ACTUATOR ZONE 510. REMOVED AND REPLACED LT WING KREUGER FLAP CROSSBEAM IAW SRM 51-72-10 PG 1-3

Part: LINK ASSY — CRACKED (ZONE 200) · airframe 18,830 hrs · 10,372 cycles

MAIN DECK CARGO FRAME 48L BELOW SEAT TRACK 4L SUPPORT STRUCTURE ATTACHMENT LUG CRACKED ONE INCH LONG, STR 27-28. R & R DAMAGED LINK ASSY IAW SRM 51-40-21, PG 7, PARA 5.

Part: ANGLE — CRACKED (ZONE 600) · airframe 18,830 hrs · 10,372 cycles

RIGHT WING LOWER L/E RIB 1 VERTICAL WEB STIFFENER ANGLE HAS 3 INCH CRACK. R & R RT WING L/E RIB 1 VERTICAL WEB STIFFENER IAW FSRM 51-72-10, PG 2-3.

Part: FLOORBOARD — GOUGED (ZONE 200) · airframe 18,830 hrs · 10,372 cycles

MAIN DECK CARGO FLOORBOARD 242VG UPPER SURFACE GOUGED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 18,830 hrs · 10,372 cycles

MAIN DECK CARGO FLOORBOARD 232YG HAS IMPACT DAMAGE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 18,830 hrs · 10,372 cycles

FLOORBOARD 232HG OUTER PLY CRUSHED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — DELAMINATED (ZONE 300) · airframe 18,830 hrs · 10,372 cycles

AFT ACCESSORY BAY FLOOR PANEL 312BF IS DELAMINATED ON UPPER SURFACE, AFT INBD CORNER. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 18,830 hrs · 10,372 cycles

MAIN DECK CARGO FR 48 BELOW SEAT TRACK 4R SUPPORT STRUCTURE ATTACHMENT LUG CRACKED 1.5" LONG. REMOVED AND REPLACED ATTACHMENT LUG PER SRM 51-72-10.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 18,830 hrs · 10,372 cycles

MAIN DECK CARGO FLOORBOARD 231EF BETWEEN FR 18 AND FR21 SEAT TRACK , 4L & 5L HAS 6"X 1" AREA OF DAMAGE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 18,830 hrs · 10,372 cycles

MAIN DECK CARGO SEAT TRACK 4R AT FRAME 37 HAS 1 EA ELONGATED SCALLOP. REMOVED DAMAGE SEAT TRACK 4R FR 36 TO 39 IAW SRM 53-10-16 PG 207 AND 208. LOCATED TRIMMED AND DRILLED SEAT TRACK SECTION AND 2 EA REPAIR SPLICES IAW SRM 53-10-16 PG 207 AND 208. INSTALLED REPAIR PARTS AT FR 36 TO 39 4R SEAT TRACK IAW SRM 53-10-16 PG 207 AND 208 FIG 201 REPROTECTED AREA IAW SRM 51-75-10

Part: ADAPTER — CRACKED (ZONE 200) · airframe 18,830 hrs · 10,372 cycles

CLEVIS ADAPTER AT FR21 BETWEEN SEAT TRACKS 3L AND 4L HAS .25 IN CRACK ON FWD FLANGE AND 1". CRACK ON AFT FLANGE. REMOVED CLEVIS ADAPTER IAW FSRM 51-72-10, PARA 5. LOCATED, DRILLED, AND INSTALLED NEW CLEVIS ADAPTER AT FR21 BETWEEN SEAT TRACKS 3L AND 4L IAW FSRM 51-72-10, PARA 6.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 18,830 hrs · 10,372 cycles

MAIN DECK CARGO FLOORBOARD 242UJ CRACKED. FABRICATED FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 18,830 hrs · 10,372 cycles

MAIN DECK CARGO FLOORBOARD 242EK DEFORMED & CRACKED, 4 INCHES LONG. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: WEB — CRACKED (ZONE 200) · airframe 18,830 hrs · 10,372 cycles

MAIN DECK CARGO FLOOR WEB AT FR 79 RT OTBD OF FLOOR RAIL HAS .25" CRACK EXTENDING FROM LIGHTENING HOLE. R & R WEB IAW SRM 51-72-10, P1.

Part: FLOORBOARD — DAMAGED (ZONE 100) · airframe 18,830 hrs · 10,372 cycles

FLOORBOARD 132QG CRACKED ON LOWER SURFACE AND SIDES. FABRICATED FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: WEB — CRACKED (ZONE 200) · airframe 18,830 hrs · 10,372 cycles

MAIN DECK CARGO FLOOR WEB AT FR 79, OTBD OF FLOOR RAIL HAS 1.5 IN. CRACK FROM EDGE TO LIGHTENING HOLE. R & R FLOOR WEB AFT OF FR 79 STR 26 LT IAW SRM 51-40-21, PARA 7 AND SRM 51-72-10, PG 2.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 18,830 hrs · 10,372 cycles

MAIN DECK CARGO FLOORBOARD 241TH IS DEFORMED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 18,830 hrs · 10,372 cycles

FLOORBOARD 242GF HAS THREE AREAS OF CRUSHED AND COMPRESSION DAMAGE AROUND CLEVIS ADAPTER CUT-OUTS. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 18,830 hrs · 10,372 cycles

MAIN DECK CARGO FLOORBOARD 242ZJ DEFORMED & CRACKED 5 INCHES LONG. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 18,830 hrs · 10,372 cycles

MAIN DECK CARGO FLOORBOARD 242RH IS CRACKED. FABRICATED FLOORBOARD IAW 25-005, REV J.

Part: FLOORBOARD — DAMAGED (ZONE 100) · airframe 18,830 hrs · 10,372 cycles

FLOORBOARD 131NG CRACKED ON LOWER SURFACE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 18,830 hrs · 10,372 cycles

FLOORBOARD 232NG TOP SKIN HAS IMPACT DAMAGE. FABRICATED FLOORBOARD IAW SRZ 25-005, REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 18,830 hrs · 10,372 cycles

MAIN DECK CARGO FLOOR PANEL 252 BF UPPER SURFACE GOUGED AT 3 EA AFT CLEVIS ADAPTER CUTOUTS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — GOUGED (ZONE 200) · airframe 18,830 hrs · 10,372 cycles

MAIN DECK CARGO FLOOR PANEL 252GF UPPER SURFACE GOUGED AT 3EA AFT CLEVIS ADAPTER CUTOUTS. MEASURED 10 SQ IN, 10 SQ IN, AND 5 SQ IN, FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV. J.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 18,830 hrs · 10,372 cycles

MAIN DECK CARGO FLOORBOARD 251PH IS DEFORMED AND HAS PUNCTURES. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: WEB — BENT (ZONE 300) · airframe 18,830 hrs · 10,372 cycles

THS COMPARTMENT BETWEEN FR 86 AND FR 87 S33R WEB UPPER STIFFNER IS DEFORMED /BENT. REMOVED AND INSTALLED NEW WEB AND STIFFNER IN THS COMPARTMENT BETWEEN FR 86 AND FR 87 AT STGR 33R IAW SRM 51-40-21 PAR 6 AND 7.

Part: FLOORBOARD — DAMAGED (MAIN CARGO) · airframe 18,830 hrs · 10,372 cycles

MAIN DECK CARGO FLOORBOARD 251RG IS DEFORMED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 18,830 hrs · 10,372 cycles

MAIN DECK CARGO FLOORBOARD 242RG IS CRUSHED AT CLEVIS CUTOUT BETWEEN FR 54 AND FR 54.2 AND SEAT TRACKS 2R AND 3R. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — CRACKED (ZONE 100) · airframe 18,830 hrs · 10,372 cycles

FLOORBOARD 131SG CRACKED ON LOWER SURFACE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 18,830 hrs · 10,372 cycles

MAIN DECK CARGO FLOORBOARD 251DF CRACKED, FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — GOUGED (ZONE 200) · airframe 18,830 hrs · 10,372 cycles

FLOORBOARD 252UH UPPER SURFACE GOUGED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: FLOORBOARD — DAMAGED (ZONE 100) · airframe 18,830 hrs · 10,372 cycles

FLOORBOARD 151TF HAS TWO AREAS DAMAGED UPPER AND LOWER SKIN PLYS WITH CRUSHED CORE. THE LARGEST AREA IS 8" BY 3". FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 18,830 hrs · 10,372 cycles

LEFT WING OUTER FLAP INBD SIDE L/E CHAFED MARK APPROX LENGTH IS 1 INCH AND WIDTH IS 0.50 REF AMM 27-00-00-06, ZONE 580. REPAIRED WING OUTER FLAP IAW A300-600 FSRM 57-50-00 PARA 4.H. PG 231 THRU 233 AND FIG 208 AND EA 6-5750-160186 PT. 1.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 18,830 hrs · 10,372 cycles

MAIN CARGO DECK FLOORBEAM AT FR 61 BETWEEN SEAT TRACK 4R AND 5R CRACKED ABOUT 0.125" ON THE AFT FACE EXTRUSION REF AMM 53-10-15-06-02, ZONE 250. BLENDED FLOORBEAM IAW SRM 53- 10-15- PG 14. CUT OUT CRACKED AREA OF FLOORBEAM IAW SRM 53-10-15 FIG 211 PG 386. NDT VERIFIED NO CRACK INDICATION AFTER CUT OUT IAW NTM 51-10-08. FABRICATED REPAIR CHANNEL IAW SRM 53-10-15 PAR 14, LOCATED AND DRILLED AND INSTALLED REPAIR CHANNEL IAW SRM 53-10-15 PG 385-390. REPROTECTICTED FR 61 AND REPAIR ANGLE IAW SRM 51-75-10 AND SRM 51-23-00.

Part: HEATER — ARCED (WINDSHIELD) · airframe 17,667 hrs · 9,707 cycles

L1 WINDOW HEAT ARCHING THEN CRACKED AT FLIGHT LEVEL 350. FOLLOWED QRH AND TURNED OFF WINDOW HEAT AND DESCENDED TO 250, DIVERTED. REMOVED AND REPLACED LEFT WINDSHIELD PANEL PER AMM 56-11-11-04.

Part: CARRIAGE — MISALIGNED (ZONE 500) · airframe 16,328 hrs · 9,003 cycles

LT WING T/E NR 3 TRACK CARRIAGE UPPER BRIDGE INBD SHIM GOT MIGRATION. EA 6-2750-141636 REPAIR ACCOMPLISHED. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: CARRIAGE — MISALIGNED (ZONE 600) · airframe 16,328 hrs · 9,003 cycles

RT WING T/E FLAP NR3 FRONT CARRIAGE UPPER BRIDGE WAS FOUND SHIM MIGRATION. EA 6-2750-141636 REPAIR ACCOMPLISHED. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: CARRIAGE — MISALIGNED (ZONE 600) · airframe 16,328 hrs · 9,003 cycles

RT WING T/E FLAP NR6 REAR CARRIAGE LEVER MOUNTING YOKE INBD SHIM MIGRATED. EA 6-2750-414636 REPAIR ACCOMPLISHED. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SHIM — MISALIGNED (LT WING) · airframe 16,328 hrs · 9,003 cycles

LT WING T/E NR 5 TRACK CARRIAGE UPPER BRIDGE INBD SHIM GOT MIGRATION. EA 6-2750-141636 REPAIR ACCOMPLISHED. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: CARRIAGE — MISALIGNED (ZONE 600) · airframe 16,328 hrs · 9,003 cycles

RT WING T/E FLAP NR 5 FRONT CARRIAGE UPPER BRIDGE WAS FOUND SHIM MIGRATION. EA 6-2750-141636 REPAIR ACCOMPLISHED. GMM 6-2-100 REPAIR CLASSIFIED AS MINOR.

Part: CARRIAGE — MISALIGNED (ZONE 600) · airframe 16,328 hrs · 9,003 cycles

RT WING T/E FLAP NR 6 FRONT CARRIAGE UPPER BRIDGE WAS FOUND SHIM MIGRATION. EA 6-2750-141636 REPAIR ACCOMPLISHED. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: CARRIAGE — MISALIGNED (ZONE 600) · airframe 16,328 hrs · 9,003 cycles

RT WING T/E FLAP NR4 FRONT CARRIAGE UPPER BRIDGE WAS FOUND SHIM MIGRATION. EA 6-2750-141636 REPAIR ACCOMPLISHED THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 16,328 hrs · 9,003 cycles

LT WING T/E UPPER SKIN SUPPORT WEB CRACKED AT NR 4 SPOILER OTBD HINGE NEARBY. FABRICATED LT SUPPORT SKIN I.AW AB6F DWG NR A57240194 (PN A57240194200). INSTALLED THE SUPPORT SKIN WITH FASTENER IAW AB6F SRM 51-40-21. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: RIB — CRACKED (ZONE 500) · airframe 16,328 hrs · 9,003 cycles

FASTENER HOLES WERE FOUND CRACKED AT RIB25A OF LEFT WING INBD FLAP IAW EO E6-5750-7-5003, PT1. THE REPAIR CLASSIFIED AS MINOR GMM 6-2-100.

Part: DOOR — CRACKED (ZONE 700) · airframe 16,328 hrs · 9,003 cycles

LT MLG DOOR OTBD EDGE GOT IMPACT DAMAGED AT CTR AREA. DAMAGE EDGE AREA REPAIRED IAW EA NR 6-5280-141635 . THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 16,328 hrs · 9,003 cycles

LT WING T/E UPPER SKIN SUPPORT WEB GOT CRACK AT NR 3 SPOILER INBD HINGE NEARBY. FABRICATED LT SUPPORT SKIN IAW AB6F DWG NR A57240194 (PN A57240194201). INSTALLED THE SUPPORT SKIN WITH FASTENER IAW AB6F SRM 51-41-21. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: GEARBOX — LEAKING (TE FLAPS) · airframe 15,432 hrs · 8,517 cycles

AFTER T/O FLAPS WOULD NOT RETRACT. OVERHEAD PANEL INDICATED FLAP SYS 2 FAULT & WHEN HANDLE RAISED THE FLAPS STAYED AT 20 DEG AND FLAP SYS 1 FAULT CAME ON. THERE WAS NOT A FLAPS LIGHT ON SPFI PANEL AT ANY TIME. RECYCLED FLAP HANDLE IAW QRH & GOT SAME RESULTS & INDICATIONS EACH TIME NORMAL LANDING ACCOMPLISHED WITH FLAPS IN 15/20 SETTING. R&R NR 6 LT DOWNDRIVE FLAP TRACK GEARBOX IAW AMM 27-54-15-4. R & R LT FLAP NR 2 SCREWJACK IAW AMM LT FLAP NR 2 SCREWJACK IAW AMM 27-54-22. PPU 3CN AND PPU 27CV ON FLAP DRIVE UNIT REPLACED IAW MM 27-55-12-4 AND 27-51-19-4. NOTE THE NR 6 GEARBOX WAS CAUSE OF DISCREPANCY OTHER ITEMS CHANGED FOUND DURING TROUBLESHOOTING ITEM OR CAUSE BY TROUBLESHOOTING ITEM .

Part: PCU — FAILED (TE FLAPS) · airframe 15,432 hrs · 8,516 cycles

AFTER T/O FLAPS WOULD NOT RETRACT- FOLLOWED QRH -RECYCLED NO HELP - RETURNED TO DEPARTURE. REPLACED LT FLAP PCU HIGH SPEED VALVE IAW MM 27-54-33-4. OPS CKD FLAP SEVERAL TIMES. OPS CKD GOOD. INSPECTED BOTH FSCC'S. NO FAULTS NOTED. CLOSED TDR RESULTS= CONFIRMED EXTERNAL LEAKS.

Part: UNKNOWN — UNKNOWN · airframe 13,979 hrs · 7,705 cycles

LEVEL CRUISE AT FL 250, ENG 2 FUEL CLOG LIGHT CAME ON WITH ASSOCIATED ECAM ALERT. REDUCED ENG 2 POWER TO IDLE IAW ECAM. STARTED RETURN TO MEM. AFTER 7-8 MINS AT IDLE, LIGHT WENT OUT AND STAYED OUT THROUGHOUT APPROACH AND LANDING USING NORMAL POWER. REPEAT WRITE UP, ORIGINAL FUEL FILTER FOUND TO HAVE NO CONTAMINATION. REPLACED FUEL FILTER REF AMM 73-12-0 2-4, LEAK CHECK OK. REMOVED AND REPLACED NR 2 ENG FUEL PRESS SWITCH IAW AMM 73-34-11-4 05 OPS NORMAL NO LEAKS NOTED. RAN NR 2 ENGINE PER JRH CLOG LIGHT REMAINED EXTINGUISHED.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 13,436 hrs · 7,380 cycles

MAIN CARGO DECK LT SIDE NR 4 SEAT TRACK BETWEEN FR 57 AND FR 57.1 HAS 2 EA ELONGATED SCALLOPS. REMOVED DAMAGED SECTION OF TRACK AND INSTALLED SEAT TRACK SPLICE REPAIR AT TRACK NR 4 LT BETWEEN FR 57 AND FR 57.1 IAW SRM 53-10-16, FIG 201, PG 207/208.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 13,436 hrs · 7,380 cycles

RT WING CENTER FLAP UPPER SURFACE APPROX RIB 16, 7 EA WEAR MARKS FROM BUTTON HEAD RIVETS CHAFING REMOVED DAMAGED SECTION AND INSTALLED FLAP SKIN PATCH REPAIR IAW SRM 57-50-00, FIG 205, PG 219.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 13,436 hrs · 7,380 cycles

MAIN DECK LT SIDE SEAT TRACK 4L AT FRAME 20 HAS 3 ELONGATED SCALLOPS. REMOVED AND REPLACED SEAT TRACK 4L FROM FRAMES 18 TO 26 IAW A300-600 SRM 51-72-10 AND 51-40-21.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 13,436 hrs · 7,380 cycles

MAIN DECK LEFT SIDE SEAT TRACK 4 AT FRAME 54 HAS 2 ELONGATED SCALLOPS. REMOVED DAMAGED TRACK FROM FRAMES 54 TO 54.2 AND INSTALLED NEW TRACK IAW A300-600 SRM 51-72-10 AND 51-40-21. RESTORED PROTECTIVE COATING IAW A300-600 SRM 51-75-10.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 13,436 hrs · 7,380 cycles

MAIN CARGO DECK LT SIDE NR 4 SEAT TRACK BETWEEN FR 60 AND FR 61 HAS 3 EA ELONGATED SCALLOPS. REMOVED DAMAGED TRACK SECTION AND INSTALLED SEAT TRACK SPLICE. REPAIR AT LT TRACK NR 4 BETWEEN FR 60 AND FR 61 IAW A300-600 SRM 53-10-16, FIG 201, PG207/208.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 13,436 hrs · 7,380 cycles

MAIN DECK LT SIDE SEAT TRACK NR 2 AT FRAME 52 HAS 1 ELONGATED SCALLOP REMOVED DAMAGED SECTION AND INSTALLED REPAIR ON NR 2 LT SEAT TRACK AT FRAMES 52-54 IAW SRM 53-10-16 FIG 203 SHEET 5.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 12,791 hrs · 6,998 cycles

APPROXIMATELY ONE HOUR IN FLIGHT, ECAM WARNING: GREEN PUMP 2 LO PR" FOLLOWED BY "GREEN PUMP 1 LO PR". OBSERVED GREEN RESERVOIR OVERHEAT LIGHT ON. COMPLIED WITH ECAM AND QRH AND TURNED OFF BOTH GREEN PUMPS. ON APPROACH AND LANDING. ON SHORT FINAL, GREEN NR 2 LO PR LIGHT ILLUMINATED. LEAK FOUND BY GROUND CREW. REMOVED AND REPLACED NR 1 ENG GREEN SYS HYD PUMP PER MM 29-11-32-4 AND REMOVED AND REPLACED BOTH CASE DRAIN FILTERS PER MM 29-11-36-4. STILL NEEDS LEAK CK AND SAFETY WIRE. SLIGHT DISCOLORATION BUT LOOKED NORMAL. REMOVED ENG NR 2 GREEN SYS HYD PUMP AND COULD NOT ROTATE PUMP AND FOUND THE PRESSURE SIDE HYD FLUID HAD THE SAME SLIGHT DISCOLORATION BUT LOOK NORMAL WHEN REMOVED SUCTION HOSE FOUND A VERY BAD BURNT SMELL.

Part: UNKNOWN — UNKNOWN (COCKPIT) · airframe 11,217 hrs · 6,112 cycles

CALLED OUT A/C AFTER AN ABORTED T/O FOR A LOUD SQUEAL ON FLIGHTDECK AT 80 KTS. REQUESTED FLIGHT CREW UNPLUG PERSONAL HEADSET AND PLUG IN COMPANY HEADSET. CREW REQUESTED ANOTHER T/O ATTEMPT, A/C DEPARTED KIND.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 8,801 hrs · 4,764 cycles

DURING APPROACH WHEN LANDING GEAR LOWERED, LANDING GEAR INDICATIONS ON FORWARD PANEL INDICATED 3 DOWN GREEN WITH 3 RED UNLOCKED INDICATION, POSITION DETECTION SYSTEM WAS SELECTED TO SYS 1. ECAM DIRECTED SWITCH TO POSITION DETECTOR SYS 2. SWITCHED TO SYSTEM 2 FORWARD INDICATION SYSTEM REMAINED THE SAME 3 GREEN, 3 RED OVERHEAD LANDING GEAR INDICATORS INDICATED 3 GREEN, RECYCLED LANDING GEAR USING SYS 1 DETECTOR AND RECEIVED NORMAL INDICATIONS 3 GREEN, NO RED UNLOCKED. INSPECTED AND PERFORMED PROX BOX UNIT TEST IAW AMM 32-00-00-501 PROX UNIT TESTED GOOD NO FAULTS LOGGED OR SHOWING. ALL COCKPIT LANDING GEAR INDICATION SYS TEST GOOD. COULD NOT DUPLICATE, OK TO CONTINUE.

Part: LIMIT SWITCH — FAILED (THRUST REVERSER) · airframe 8,242 hrs · 4,494 cycles

ON T/O AFTER BRK REL AND STANDARD POWER SET APPROX 50 KTS HAD AMBER ECAM 1 THR REV UNLOCK WITH AMBER REV UNLOCK ON PANEL ABOVE ENG INSTRUMENTS. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C. ENGINE 1 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION. LOCKED OUT 1 T/R IN ACCORDANCE WITH MEL 78-30-01-A. DURING TAKEOFF SUSPECT BAD RT ELECTRICAL LIMIT SWITCH. DEACTIVATED 1 T/R PER MEL 78-30-01-A. REMOVED AND REPLACED 1 ENGINE RIGHT REVERSER FEEDBACK TRANSDUCER PER MM 78-31-07. RAN ENGINE PER JRH AND OPERATED 1 REVERSER WITH NO DEFECTS NOTED. ITEM CLEARED.

Part: THRUST REVERSER — INOPERATIVE (NR 1 ENGINE) · airframe 8,229 hrs · 4,484 cycles

NR 1 REVERSER PRESSURIZED ECAM ALERT ON INITIAL TAKEOFF. NR 1 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION.

Part: RESERVOIR — LOW (HYD SYSTEM) · airframe 7,389 hrs · 4,012 cycles

DURING CRUISE FLIGHT AT FL 330 .80 MACH ECAM ALERTED-INDICATING LOSS OF BLUE HYD SYSTEM (HYD RSVR LO LEVEL) - ECAM SYSTEM PAGE SHOWED BLUE HYD SYSTEM RESEVIOR WAS LOW. ECAM PROCEDURE FOR HYD RSVR LO LEVEL ACCOMPLISHED. REMAINING HYD SYSTEMS NORMAL. FOUND BLUE HYD SYS PSI TRANS CRACKED. REMOVED AND REPLACED BLUE HYD SYS PSI TRANS. OPS AND LK CK OK. REF A300MM 29-32-13-4. ENT BY: 446285 RPT BY: 446285 R/I 22JUL04 11:26 MEM R R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 64250-005-2, POS P1, SRL 12051, TAG 611495 ON MFG 64250-005-2 SRL 11564, TAG 609018.

Part: WARNING LIGHT — ILLUMINATED (NR 2 ENGINE T/R) · airframe 1,995 hrs · 967 cycles

DURING T/O ROLL, RECEIVED ECAM WARNING NR 2 ENG REVERSER PRESSURIZED. AC RELEASED FOR SERVICE PER MEL 78-1.

Part: UNKNOWN — ODOR (CABIN) · airframe 1,464 hrs · 709 cycles

STRONG ODOR OF NATURAL GAS OR PROPANE AT CR. ALL FREIGHT REMOVED AND INSP, NONE FOUND. AN OPS CK OF TR1, & TR2, & ESS TR WAS DONE DUE TO TR POPPING C/B.