N676FE

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 35,305 hrs · 20,180 cycles

L1 DOOR EMERGENCY EXIT SPOT LIGHT DOES NOT ILLUMINATE. AMM: 33-51-13-04 SERVICED L1 DOOR EMERGENCY LIGHT OPS GOOD OK FOR SVC.

Part: SKIN — DELAMINATED (ZONE 500 SPOILER) · airframe 34,994 hrs · 19,996 cycles

LH WING #5 SPOILER CENTER I/B & O/B HINGE ARM UPR SKIN FOUND DELAMINATION. SIZE: (1)40MM*18MM, DEPTH: 2.40MM (2)83MM*40MM, DEPTH: 2.38MM COMPLIED WITH EA: 6-5750-T0383299 P1. TITLE: WING - FLIGHT SURFACES - LH #5 SPOILER TOP SKIN UPPER SURFACE DELAMINATION ABOVE CENTER HINGE ARM. REPAIRED THE LH WING #5 SPOILER CENTER I/B & O/B HINGE ARM UPR SKIN DELAMINATION. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100. SEE WRI 57504074 FOR WORK DETAILS.

Part: DOOR — CRACKED (ZONE 800) · airframe 34,994 hrs · 19,996 cycles

MAIN DECK CARGO DOOR UPR EDGE AT PT1 BETWEEN FR23 AND FR24 FOUND CRACK SIGNAL ON 3EA FASTENER HOLES COMPLIED WITH EA: 6-5230-T0383235 P1. TITLE: DOORS - CARGO DOOR/HYD SYS - CRACKED HOLES ON MAIN DECK CARGO DOOR UPPER LONGERON. REPAIRED THE MAIN DECK CARGO DOOR UPR EDGE 3EA CRACKED FASTENER HOLES AT PT1 BETWEEN FR23 AND FR24. THIS REPAIR IS CONSIDERED AS CATEGORY B REPAIR DUE TO AWAITING FURTHER DT APPROVAL. THIS REQUIREMENT WILL BE TRACKING BY ENMDS TO ABTAIN STAGE 2 AND/OR STAGE 3 APPROVAL WITHIN 6-MONTHS PER EA: 6-5230-T0383235. MAJOR REPAIR IAW FEDEX GMM6-2-100. SEE WRI 52304081 FOR WORK DETAILS.

Part: CROSSBEAM — UNKNOWN (ZONE 200) · airframe 34,994 hrs · 19,996 cycles

MAIN DECK CARGO COMPARTMENT - EXISTING CROSSBEAM REPAIR FROM Y1959 TO Y2462 BETWEEN FR54.1 AND FR54.2 REQUIRES EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF THE REPAIR CONFORMS TO FAA APPROVED DATA THE EXISTING CROSSBEAM REPAIR FROM Y1959 TO T2462 BETWEEN FR54.1 AND FR54.2 WAS EVALUATED AND FOUND IN CONFORMITY WITH DWG: A53813215 (ISSUE.A00). NO REPAIR RECORD WAS FOUND. EO: 6-5100-7-5000 D07 PART 1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300 / A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. THE REPAIR WAS CATEGORY "A" AND WAS CLASSIFIED AS MAJOR PER GMM 6-2-100

Part: CARGO TRACK — BROKEN (ZONE 200) · airframe 34,994 hrs · 19,996 cycles

MAIN DECK CARGO FR42-FR43 Y953 SEAT TRACK BROKEN REPLACED THE MAIN DECK CARGO BROKEN SEAT TRACK AT Y953 BETWEEN FR40 AND FR45 WITH A FABRICATED PART PER A300-600 SRM51-40-21 AND DWG A53832020(ISSUE: G). THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.

Part: SKIN — NO DISCREPANCY (ZONE 600 FLAP) · airframe 34,994 hrs · 19,996 cycles

EXISTING REPAIR ON RH WING CENTER FLAP LOWER SKIN RIB10-RIB12 BETWEEN S2.2 AND REAR SPAR REQUIRES EVALUATION FOR CONFORMITY. EXISTING REPAIR ON RH WING CENTER FLAP LOWER SKIN RIB10-RIB12 BETWEEN S2.2 AND REAR SPAR WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM57-50-00 FIG.205. REPAIRED PER EA 6-5750-T0383250. TITLE: WINGS - FLIGHT SURFACES - EXISTING REPAIRS ON RH CENTER FLAP LOWER SKIN. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR121.707. THE REPAIR WAS CATEGORY "A" AND WAS CLASSIFIED AS MAJOR PER GMM6-2-100. RSC TRACKING EA: 6-5750-T0383250 WAS ISSUED AND COMPLETED.

Part: SKIN — DAMAGED (ZONE 600 FLAP) · airframe 34,994 hrs · 19,996 cycles

EXISTING REPAIR ON RH WING CENTER FLAP LOWER SKIN RIB15-RIB18 BETWEEN S2.2 AND REAR SPAR REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON RH WING CENTER FLAP LOWER SKIN RIB15-RIB18 BETWEEN S2.2 AND REAR SPAR WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM57-50-00 FIG.205. REPAIRED PER EA 6-5750-T0383250. TITLE: WINGS - FLIGHT SURFACES - EXISTING REPAIRS ON RH CENTER FLAP LOWER SKIN. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR121.707. THE REPAIR WAS CATEGORY "A" AND WAS CLASSIFIED AS MAJOR PER GMM6-2-100.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 34,994 hrs · 19,996 cycles

MAIN DECK FR11-FR13A Y730 FLOOR SUPPORT CORRODED. REPLACED THE CORRODED FLOOR SUPPORT AT MAIN DECK FR11-FR13A Y730 WITH NEW PART PER A300-600F SRM51-40-21. THIS IS CATEGORY A REPAIR. MINOR REPAIR IAW FEDEX GMM6-2-100

Part: SKIN — NO DISCREPANCY (ZONE 600 FLAP) · airframe 34,994 hrs · 19,996 cycles

EXISTING REPAIR ON RH WING CENTER FLAP LOWER SKIN RIB16-RIB17 BETWEEN FRONT SPAR AND S2.3 REQUIRES EVALUATION FOR CONFORMITY. EXISTING REPAIR ON RH WING CENTER FLAP LOWER SKIN RIB16-RIB17 BETWEEN FRONT SPAR AND S2.3 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM57-50-00 FIG.205. REPAIRED PER EA 6-5750-T0383250. TITLE: WINGS - FLIGHT SURFACES - EXISTING REPAIRS ON RH CENTER FLAP LOWER SKIN. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR121.707. THE REPAIR WAS CATEGORY "A" AND WAS CLASSIFIED AS MAJOR PER GMM6-2-100.

Part: FLOOR SUPPORT — UNKNOWN (ZONE 200) · airframe 34,994 hrs · 19,996 cycles

EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR11 - FR13A FLOOR SUPPORT AT Y232 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR11-FR13A FLOOR SUPPORT AT Y232 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM 53-12-15-201-2 FIG.207. REPAIRED IT PER A300-600F SRM53-12-15-201-2 FIG.207. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. THE REPAIR WAS CATEGORY "B" AND WAS CLASSIFIED AS "MAJOR" PER GMM 6-2-100. THE FIRST INSPECTION THRESHOLD WAS 42500FC / 89000FH AFTER REPAIR EMBODIMENT. THE REPETITIVE INSPECTION INTERVAL AND METHOD WERE TBD PER A300-600F SRI 53-12-15-2-004-00.

Part: FITTING — CRACKED (ZONE 200) · airframe 34,994 hrs · 19,996 cycles

CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 LH SIDE, FASTENER "I" HOLE FOUND CRACK SIGNAL COMPLIED WITH EO 6-5710-E0342809 D P1. TITLE: WINGS - CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE. SBÏ¿½S A300-57-6049 R08, A300-57- 6086 R07, A300-57-6121 IR & 300-57-6050 R03. REPAIRED THE CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 LH SIDE CRACKED FASTENER "I" HOLE. THIS IS CATEGORY A REPAIR. MINOR REPAIR IAW FEDEX GMM6-2-100. SEE WRI 57103926 FOR WORK DETAILS.

Part: SEAT TRACK — BROKEN (ZONE 200) · airframe 34,994 hrs · 19,996 cycles

MAIN DECK FR33-FR34 -Y1959 SEAT TRACK BROKEN. REPAIRED THE MAIN DECK BROKEN SEAT TRACK AT -Y1959 BETWEEN FR33 AND FR34 PER A300- 600F SRM53-10-16-201 FIG.201. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2- 100

Part: BEARING — NOT REPORTED (ZONE 800) · airframe 34,994 hrs · 19,996 cycles

COMPLY WITH EO 6-5230-E0378588 B P5 FOR MAIN DECK CARGO DOOR ACTUATOR BEARING FITTINGS REPLACEMENT. COMPLIED WITH EO 6-5230-E0378588 B P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCC) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016-24. REPLACED THE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTINGS. THIS IS CATEGORY B REPAIR. FOLLOW-UP INSPECTION PER EO 6-5230- E0378588 B. MAJOR REPAIR IAW GMM6-2-100.

Part: HINGE ARM — DELAMINATED (ZONE 500 SPOILER) · airframe 34,994 hrs · 19,996 cycles

LH WING #3 SPOILER CENTER I/B & O/B HINGE ARM UPR SKIN FOUND DELAMINATION. SIZE: (1)14MM*7MM, DEPTH: 1.46MM (2)35MM*10MM, DEPTH: 1.56MM COMPLIED WITH EA: 6-5750-T0383024 P1. TITLE: WING - FLIGHT SURFACES - LH #3 SPOILER CENTER HINGE ARM AREA DELAMINATION. REPAIRED THE LH WING #3 SPOILER CENTER I/B & O/B HINGE ARM UPR SKIN DELAMINATION. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100. SEE WRI 57504064 FOR WORK DETAILS.

Part: HINGE ARM — DELAMINATED (ZONE 500 SPOILER) · airframe 34,994 hrs · 19,996 cycles

LH WING #3 SPOILER CENTER O/B HINGE ARM OUTSIDE SURFACE FOUND 2EA LOCATIONS DELAMINATION. SIZE: (1)25MM*25MM, DEPTH: 1.94MM (2)30MM*25MM, DEPTH: 1.51MM COMPLIED WITH EA: 6-5750-T0383024 P1. TITLE: WING - FLIGHT SURFACES - LH #3 SPOILER CENTER HINGE ARM AREA DELAMINATION. REPAIRED THE LH WING #3 SPOILER CENTER O/B HINGE ARM OUTSIDE SURFACE 2EA LOCATIONS DELAMINATION. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100. SEE WRI 57504064 FOR WORK DETAILS.

Part: FRAME — CRACKED (ZONE 200) · airframe 34,994 hrs · 19,996 cycles

CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE, FASTENER "I" HOLE FOUND CRACK SIGNAL COMPLIED WITH EO 6-5710-E0342809 D P2. TITLE: WINGS - CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE. SBÏ¿½S A300-57-6049 R08, A300-57- 6086 R07, A300-57-6121 IR & 300-57-6050 R03. REPAIRED THE CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE CRACKED FASTENER "I" HOLE. THIS IS CATEGORY A REPAIR. MINOR REPAIR IAW FEDEX GMM6-2-100. SEE WRI 57103894 FOR WORK DETAILS.

Part: SEAT TRACK — NO DISCREPANCY (ZONE 200) · airframe 34,994 hrs · 19,996 cycles

EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR20 - FR21 SEAT TRACK AT Y1959 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR20 - FR21 SEAT TRACK AT Y1959 WAS EVALUATED AND FOUND IN CONFORMITY WITH EA: 6-5313-102503 A. TITLE: FUSELAGE - SEAT TRACK AT FRAME 20 - 21 AND Y=1959 BENT - REPAIR. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. THE REPAIR WAS CATEGORY "A" AND WAS CLASSIFIED AS MAJOR PER GMM6-2-100.

Part: TRANSMITTER — FAILED (UNKNOWN) · airframe 33,642 hrs · 19,111 cycles

PDIS 676 29-01 2402 19AUG23 MEM OPEN U GREEN HYD RSVR LO LEVEL ECAM MESSAGE IN CRUISE. COMPLIED WITH ECAM AND QRH PROCEDURES. DIVERTED TO MEM. GREEN HYD QUANTITY GAUGE SHOWED APPROXIMATELY 2 NEEDLE WIDTHS LOW FROM HAT. GAP GREW TO 4 NEEDLE WIDTHS DURING DESCENT. INSPECTED HYD SYSTEM FOR LEAKS WITH NO LEAKS NOTED AT THIS TIME. FOUND THE GREEN HYD RESERVOUIR TO BE OVER SERVICED BY TWO GALLONS. REMOVED AND REPLACED THE GREEN HYD RESERVOIR QTY TRANSMITTER REF AMM 29-31-11-04. OPS AND LEAK CHECK GOOD. PERFORMED HYD RESERVOIR SYSTEM LEAKAGE TEST REF AMM 29-14-00-05. CHANGED RESERVOIR PRESSURIZATION FILTER HOUSING ASSY DUE TO SUSPECTED LEAK. NO LEAKS FOUND IN SYSTEM. LET THE AIRCRAFT SIT FOR 4 HOURS BEFORE AND AFTER, READINGS HAVE NOT CHANGED FOR GREEN SYSTEM RESERVOIR(6.5 GALLONS FOR RESIGREEN SYSTEM AND HOLDING AT 52 PSI ON THE GREEN SYSTEM). RAN THE #1 AND #2 ENGINES FOR 30 MINUTES ALONG WITH RUNNUNG THE FLIGHT CONTROLS THRU WITH NO FAULTS NOTED AND THE GREEN SYSTEM HAS NOT FLUCUATED OR CHANGED.

Part: HOSE — LEAKING (N/A) · airframe 33,600 hrs · 19,087 cycles

YELLOW HYD SYS LO PR ECAM CLIMBING THROUGH FL260. COMPLIED WITH ECAM AND QRH. YELLOW SYSTEM RESERVOIR QUANTITY INDICATOR FLUCTUATION IN YELLOW ABOVE AND BELOW RED DOT. ECAM QUANTITY INDICATES STEADY. COORDINATED WITH GOC AND MOC VIA ATLANTA RADIO AND ACARS. GOC/MOC RELAYED OK TO CONTINUE W/YELLOW HYD SYS OFF . - EMERGENCY DECLARED FOR LANDING - INSTALLED HOSE P/N A2714201300000, TAG NR 01612331, PER A300 AMM20-23-11-00-0. INSTALLED LACING TAPE FOR CHAFING PER A300 AMM 20-23-14-00-0. SERVICED YELLOW HYD SYSTEM PER AMM012-12-29-00-0.. CHECKED YELLOW HYD SYSTEM FILTER CLOGGING INDICATORS PER A300 AMM 29-00-00-03-0. YELLOW HYD SYSTEM IS SERVICEABLE AT THIS TIME.

Part: FITTING — CORRODED (UNKNOWN) · airframe 33,766 hrs · 19,196 cycles

CORROSION FOUND IN THE RIB 5 FITTING. REPAIR PER AIRBUS REPAIR INSTRUCTIONS R57240425

Part: CROSSBEAM — CRACKED (N/A) · airframe 33,135 hrs · 18,786 cycles

MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR28, BETWEEN -Y450 AND -Y953. COMPLIED WITH EA: 6-5310-T0372502 P1. MAJOR REPAIR IAW GMM6-2-100

Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 33,135 hrs · 18,786 cycles

MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR31, BETWEEN -Y450 AND -Y953. COMPLIED WITH EA: 6-5310-T0372501 P1. MAJOR REPAIR IAW GMM6-2-100

Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 33,135 hrs · 18,786 cycles

MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR64, BETWEEN Y1456 AND Y1959. REPAIRED THE CRACKED CROSSBEAM IN THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE AT FR64 BETWEEN Y1456 AND Y1959 PER A300-600F SRM53-10-15-201 PARA.14. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100

Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 33,135 hrs · 18,786 cycles

MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR61, BETWEEN -Y1456 AND -Y1959. REPAIRED THE CRACKED CROSSBEAM IN THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE AT FR61 BETWEEN -Y1456 AND -Y1959 PER A300-600F SRM53-10-15-201 PARA.14. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100

Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 33,135 hrs · 18,786 cycles

MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR32, BETWEEN -Y450 AND -Y953. COMPLIED WITH EA: 6-5310-T0372499 P1. MAJOR REPAIR IAW FEDEX GMM6-2-100

Part: UNKNOWN — UNKNOWN (N/A) · airframe 33,135 hrs · 18,786 cycles

EMERGENCY DECLARED: RECEIVED GREEN HYD LOW LVL. COMPLIED WITH ECAM AND QRH DECLARED EMERGENCY AND PERFORMED LANDING GEAR GRAVITY EXTEND. 1. PER AMM 29-21-00-03 PRESSURED THE GREEN HYD SYS AND CHECK THE LEAKAGE. RESULT: LEAKAGE FOUND AT THREE POSITIONS. (1)ELBOW OF GREEN HTD SYS HP MAINFOLD. (2)HYDRAULIC LINE OF AUTOMATIC SELECTOR. (3)RH LDG DOOR UPLOCK ASSY. 2. RECORDED THE GREEN SYS HYD QUANTITY RESULT: 5 GALLONS 3. PER AMM 29-11-12-04 & AMM 20-23-12-00 REPLACED THE PACKING AND BACKUP PACKING OF THE ELBOW OF GREEN HYD SYS HP MANIFOLD 4. PER AMM 29-00-00-03 CHECKED CLOGGING INDICATORS OF GREEN HYD SYS, CHECKED NORMAL 5. PER AMM 12-12-29-00 REPLENISHED THE GREEN HYD SYS 6. PER AMM 71-00-00-05 PERFORMED ENG IDLE TEST AND PRESSURE THE GREEN HYD SYS WITH EDPS THEN CHECK THE LEAKAGE, RECORD THE RESULT NO LEAKAGE 7. PER AMM 32-42-13-04 & AMM 20-23-12-00 REPLACED THE HYDRAULIC LINE OF AUTOMATIC SELECTOR (1300) 8. PER AMM 32-31-33-04 & AMM 20-23-12-00 REPLACED THE PACKING OF RH LDG DOOR UPLOCK ASSY 9. PER ASM 29-31-00 & AWM 29-31-03 MEASURED THE WIRES BETWEEN G RSVR HYD QTY XMTR(25GQ), FWC(1WW2) AND SDAC(1WV), CHECKED NORMAL 10. PER AMM 12-12-29-00 REPLENISHED THE GREEN HYD SYS TO THE RECORD QTY 6.3GALLONS NOTE: COMPLIED WITH WORK CARD 3233000-00-31. TITLE: LANDING GEAR FREE FALL CABLE TENSION - FNC. PERFORMED FREE FALL EXTENSION TEST. TEST RESULT: NORMAL

Part: TRANSMISSION — INOPERATIVE (N/A) · airframe 33,135 hrs · 18,786 cycles

EMERGENCY DECLARED RECEIVED GREEN HYD LOW LVL. COMPLIED WITH ECAM AND QRH DECLARED EMERGENCY AND PERFORMED LANDING GEAR GRAVITY EXTEND. PRESS'D THE GRN HYD SYS AND CK THE LEAKAGE. FOUND LEAK AT 3 POSITON.1) ELBOW OF GRN HYD SYS HP MAINFOLD.2) HYD LINE OF AUTO SEL 3) RH LDG DOOR UPLK ASSY 2. RCD THE GRN SYS HYD QTY. RESULT :5 GALS 3. PER AMM R/R THE PACKING & BACKUP PACKING OF ELBOW OF GRN HYD SYS HP MANIFOLD 4. CKED CLOGGING IND OF GRN HYD SYS.CK NORM 5. REPL THE GRN HYD SYS 6. PER AMM PERF ENG IDLE TEST & PRESS THE GRN HYD SYS WITH EDPS THEN CK THE LEAKAGE, RCD RESULT.CK NO LEAKAGE 7. R/R THE HYD LINE OF AUTO SEL 8. PER AMM R/R THE PACKING OF RH LDG DOOR UPLK ASSY 9. MSRD THE WIRES BETWEEN G RSVR HYD QTY XMTR, FWC & SDAC. CHECK NORM 10. REPD THE GRN HYD SYS TO THE RCD QTY. 6.3 GALS 11. BLEED YEL SYS 12. BLD GRN SYS 13. DRAIN OF GRN HYD RSVR 14. R/R THE GRN RSVR HYD QTY TRMTR .NO LEAKAGE 16. PERFORMED GRN HYD FLUID LVL IND TEST. TEST NORM 17. PERF A FUNCT TEST OF MAX PRESS DELIVERED TO THE BRAKES TEST NORM 18. PERF TEST OF BRAKING SUPPLIED WITH ACCUM PRESS TEST NORM 19. ALT BRAKING SYS OP TEST, NORM 20. PERF THE LDG NORM RET/EXT TEST, NORM. NO FAULT MESS WERE FOUND 21. PERF ENG IDLE TEST AND MONITOR THE GRN SYS LO LVL.CHECKED NORM 22. CKED GRN RSRV HYD FLUID LEVEL.CK NORM 23. CK'D THAT GRN RSVR PRESS IS NORM.

Part: HYDRAULIC SYSTEM — MALFUNCTIONED · airframe 33,065 hrs · 18,751 cycles

AT BEGINNING OF DESCENT, RECEIVED ECAM GREEN HYD LOW LEVEL. INDICATION WAS ON THE RED. AFTER MANUALLY LOWERING MLG, GREEN QTY RETURNED TO NORMAL. EMERGENCY DECLARED. AMM 12-12-29-00, AMM 29-10-00-03, AMM: 27-00-00-05, AMM 12-14-29-00, AND JRH CH5. IN FLIGHT, FLUID FLUCTUATION BELIEVED CAUSED BY TRAPPED AIR FROM RECENT GREEN SYS REPAIRS. DEPRESSURIZED GREEN SYS & RESEVOIR. SERVICED GREEN SYS ACCUMULATOR TO FULL, & VERIFED BLADDER NOT RUPTURED. SERVICED GREEN SYS RESEVOIR WITH NITROGEN & HYD FLUID. PERFORMED HYD BLEEDING. RAN ENGINES & OPS ALL FLT CNTLS & MLG DOORS FOR 15 MINS. FLUID QTY STABILIZED. PRESSURIZED MLG ON GROUND. NO QTY FLUCUTATIONS, LO PRESS OR AIR LIGHTS DURING PROCEDURE. OK FOR SERVICE

Part: SKIN — NOT REPORTED (FRMS 72-78) · airframe 32,971 hrs · 18,699 cycles

CENTER SKIN SECTION NEEDS REMOVED FROM FR78.5 TO FR72 STRINGER 52L TO 52R REPLACED CENTER SKIN SECTION FROM FR72 TO FR80 STRINGER 51L TO 51R IAW E.A. 6-5330- T0370451 PART 2 STEPS 11 AND 12. THIS IS A MAJOR REPAIR. SEE JPF FOR WORK STEPS. SEE N95 FOR INSTALLATION OF SHEAR TIES AT FR76 AND SEE N96 FOR SHEAR TIE INSTALLATION AT FR77 STRINGERS 52L TO 52R ON BOTH CARDS.

Part: FRAME — DENTED (FRM 77 S47-48R) · airframe 32,971 hrs · 18,699 cycles

FR77 CENTER FRAME AT STRINGER 47R AND 48R IS DEFORMED 0000433443 : PATE, ROBERT L - 05-NOV-2022 06:14 REMOVED AND REPLACED LEFT-HAND STUB FRAME, RIGHT-HAND STUB FRAME AND CENTER MILLED FRAME SECTION AT FR77 IAW EA 6-5330-T0370451 PART 2 STEP 17 AND A300-600 SRM 51-40-21. THIS IS A MAJOR REPAIR PLEASE SEE JPF FOR COMPLETED WORK STEPS.

Part: SKIN — DEFORMED (FRM 77 S47R) · airframe 32,971 hrs · 18,699 cycles

SKIN DEFORMATION AT FR 77 AT STR 47R (MEASURED 0.142? TO 0.172?) REPAIRED SKIN DEFORMATION AT FR76 AND FR77 STRINGER 47R IAW EA 6-5330-T0370451 PART 2 STEPS 13 AND STEP14. THIS IS A MAJOR REPAIR.

Part: SKIN — DEFORMED (FRM 77 S47L) · airframe 32,971 hrs · 18,699 cycles

SKIN DEFORMATION AT FR 77 AT STR 47L (MEASURED 0.082? TO 0.087?) REPAIRED SKIN DEFORMATION AT FRAME 76.5 TO FR77.5 STRINGER 47L TO 51L IAW EA 6-5330- T0370451 PART 2 STEPS 15,10 REF FIGURE 3 OF 3 FOUND IN STEPS 3. SEE N109 FOR EDGE SEALING AND PAINT SEE JPF THIS IS A MAJOR REPAIR.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 32,921 hrs · 18,673 cycles

MDIS 676 33-50 1687 17AUG22 BUR FACT U COURIER AREA EMERGERNCY LIGHTING WILL NOT TEST OR TURN ON R/I 17AUG22 19:12 BUR U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: AD-3214-30 POS: 3 SRL: 59192 ON MPN: AD-3214-31 CPN: 3310373 SRL: 279535 TAG NBR: 35H905 FACT 17AUG22 19:12 BUR U REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY 29WL1 REF AMM 33-51-14-04. OPS CHECKS GOOD.

Part: NONE — NONE (N/A) · airframe 31,826 hrs · 18,048 cycles

PDIS 676 73-35 0791 18OCT21 OKC OPEN U IN CRUISE FLIGHT AT FL340 ABOUT AN HOUR AFTER TAKEOFF WE GOT ECAM WARNING OF ENG #1 FUEL FILTER CLOG. WE ALSO GOT THE FUEL CLOG LITE FOR THE #1 ENGINE. WE FOLLOWED THE QRH PROCEDURE AND REDUCED THE #1 THROTTLE TO IDLE BUT THE CLOG LIGHT AND ECAM WARNINGS DID NOT GO AWAY. WE DIVERTED TO LAND AND LANDED APPROX 30 MINUTES AFTER THE INITIAL WARNING. THE ECAM WARNING AND FUEL CLOG LITE BOTH REMAINED ON UNTIL ENGINE WAS SHUT DOWN. WE DID NOT NOTICE ANY UNUSUAL FUEL FLOW OR ENGINE INDICATIONS. FACT 18OCT21 20:56 OKC REPLACED #1 ENG FUEL FILTER, (WHICH DID NOT APPEAR TO BE CLOGGED AT ALL) REF AMM 73-12-02-04-0-F AND REPLACED FUEL FILTER DIFF PRESSURE SW AS WELL , REF AMM 73-34-11-04. OPS AND LEAK CHECKS GOOD. RAN ENG REF JRH CH6, AND AMM 71-00-00-5 OPS NORMAL WITH NO FUEL CLOG LIGHT. ACFT OK FOR SVC.

Part: HANDLE — FAILED (MLG) · airframe 31,711 hrs · 17,976 cycles

PDIS 676 32-30 0707 14SEP21 AFW OPEN U GEAR WOULD NOT RETRACT AFTER TAKEOFF (GEAR HANDLE STOPPED IN MIDDLE POSITION) - TRIED POS 1 AND 2 WITH NO DIFFERENCE. PLACED GEAR HANDLE DOWN AND LANDED. SHGN 14SEP21 10:30 AFW U PERFORMED GVI OF BOTH MAIN LANDING GEARS NO OBVIOUS DEFECTS NOTED. BOTH PITCH DAMPERS ARE WITH IN SERVICE LIMITS, RED DPI NOT EXTENDED. INTERROGATED PROX BOX UNIT (54GB) FOUND ONE FAULT OF "BR" (BOGIE RIGHT FAIL). NO OTHER FAULTS FOUND. MEL 14SEP21 11:35 AFW U RELEASED FOR SERVICE PER MEL : 32-30-01-B CATEGORY : C EXPIRATION : 24SEP21 "MEL 32-30-01-B: LANDING GEAR RETRACTION SYSTEM - INOP. MAX SPEED 255 KIAS / 0.65 M. DO NOT USE FMS PROFILE MODE." MEL C/728600

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 30,279 hrs · 17,126 cycles

AFT CARGO FLOOR PANEL 152PF CRACKED AND DELAMINATED.(PANEL RACK) FABRICATED NEW FLOOR PANEL 152PF ON VTMAE TRAVELER # T20/1503455 IAW FEDEX DWG SRZ-25-005R, MAJOR REPAIR.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 30,279 hrs · 17,126 cycles

FOUND RH CENTER FLAP CRACKED AT RIB 17 APPROX 5" AFT OF FRONT SPAR LOWER SKIN. AFTER FURTHER INVESTIGATIONI OF X-RAY FILM AND BORESCOPE OF THE SUSPECTED AREA AREA, NO CRACK WAS NOTED ON RIB 17 OF THE RH FLAP. CUT LOWER SKIN 6" X 3" FOR ACCESS IAW SRM 57-50-00. AFTER VERIFICATION OF NO CRACK ON RIB, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-40-40, SRM 57-50-00 FIG 205, AND SRM 51-40-21. MAJOR REPAIR

Part: FLOOR PANEL — CRACKED (FRAMES 54-54.2) · airframe 30,279 hrs · 17,126 cycles

FLOOR PANEL 151PF CRACKED, FABRICATED FLOOR PANEL 151PF FROM TRAVELER TD/000437 IAW DWG SRZ-25-005R, CATEGORY "A" AND MAJOR REPAIR.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 30,279 hrs · 17,126 cycles

RIGHT ELEVATOR HAD WATER ENTRAPMENT ON THE LT EDGE OF ER13 APPROIMATELY 12 3/4 INCHES FROM THE TRAILING EDGE AND MEASURES 1 5/8 INCHES X 2 INCHES IN SIZE. REPAIRED THE RT ELEVATOR IAW SRM 55-21-12 PARA 5H, FIG 212. MAJOR REPAIR.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 30,279 hrs · 17,126 cycles

LEFT ELEVATOR HAD WATER ENTRAPMENT 19 1/2 INCHES FROM THE OUTBD EDGE OF ER2, APPROXIMATELY 21 3/8 INCHES FROM THE TRAILING EDGE AND MEASURES 5/8 X 3/4 INCH IN SIZE. REPAIRED THE LT ELEVATOR IAW SRM 55-21-12, PARA 5H. MAJOR REPAIR.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 30,279 hrs · 17,126 cycles

LEFT ELEVATOR HAD WATER ENTRAPMENT 30 7/8 INCHES FROM THE OTBD EDGE OF ER13, APPROXIMATELY 21 INCHES FROM THE TRALING EDGE AND MEASURES 1 X 1 INCH IN SIZE. REPAIRED THE LT ELEVATOR IAW SRM 55-21-12, PARA 5H. MAJOR REPAIR.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 30,279 hrs · 17,126 cycles

LEFT ELEVATOR HAD WATER ENTRAPMENT 12 INCHES FROM THE OUTBD EDGE OF ER2, APPROXIMATELY 21 1/4 INCHES FROM THE TRALING EDGE AND MEASURES 1 1/4 X 1 3/8 INCHES IN SIZE. REPAIRED THE LT ELEVATOR IAW SRM 55-21-12, PARA 5H, MAJOR REPAIR.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 30,279 hrs · 17,126 cycles

FOUND A CRACK ON THE RT CENTER FLAP AT RIB 11, LOCATED APPROX 5 INCHES FWD OF REAR SPAR IN THE UPPER SKIN. ACCESSED AND REPAIRED THE DAMAGE IAW SRM 57-50-00, FIG 201. INSTALLED A DOUBLER ON LOWER THE SKIN IAW SRM 57-50-00, FIG 205, AND SRM 51-40-21. CATAGORY -A- MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 30,279 hrs · 17,126 cycles

FLOOR PANEL 131SG DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R. CATAGORY -A- MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (BULK CARGO) · airframe 30,279 hrs · 17,126 cycles

BULK CARGO FLOOR PANEL 161GF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 30,279 hrs · 17,126 cycles

FLOOR PANEL 131KG DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R. CATAGORY -A- MAJOR REPAIR.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 30,279 hrs · 17,126 cycles

FOUND A CRACK ON THE RT CENTER FLAP AT RIB 12, APPROX 5.1 INCHES FWD OF REAR SPAR, ON UPPER SKIN. ACCESSED AND REPAIRED THE DAMAGE IAW SRM 57-50-00, FIG 201. INSTALLED A DOUBLER ON THE LOWER SKIN IAW SRM 57-50-00, FIG 205, AND SRM 51-40-21. CATAGORY -A- MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 30,279 hrs · 17,126 cycles

BULK CARGO FLOOR PANEL 161GF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005R. CATAGORY -A- MAJOR REPAIR.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 30,279 hrs · 17,126 cycles

FOUND A CRACK ON THE RT CENTER FLAP, AT RIB 16 APPROX 4.8 INCHES FWD OF REAR SPAR UPPER SKIN. CUT THE SKIN ON LOWER SURFACE FOR ACCESS AND REPAIRED THE CRACK IAW SRM 57-50-00, FIG 201. INSTALLED A DOUBLER IAW SRM 57-50-00, FIG 205. CATAGORY -A- MAJOR REPAIR.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 30,279 hrs · 17,126 cycles

FOUND A CRACK ON THE RT CENTER FLAP AT RIB 18, APPROX 5 INCHES FWD OF REAR SPAR ON UPPER SKIN. CUT THE SKIN ON LOWER SURFACE FOR ACCESS AND REPAIRED THE CRACK IAW SRM 57-50-00, FIG 201. INSTALLED A DOUBLER IAW SRM 57-50-00, FIG 205. CATAGORY A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 30,279 hrs · 17,126 cycles

BULK CARGO FLOOR PANEL 162HF HAS A PULLED THROUGH INSERT, MISSING. FABRICATED A FLOOR PANEL IAW DWG SRZ-25-005R. CATAGORY -A- MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 30,279 hrs · 17,126 cycles

FLOOR PANEL 132KG BROKEN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R. CATAGORY -A- MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 30,279 hrs · 17,126 cycles

FLOOR PANEL 132QG WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R, CATAGORY -A- MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 30,279 hrs · 17,126 cycles

FLOOR PANEL 131NG BROKEN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R, CATAGORY -A- MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 30,279 hrs · 17,126 cycles

FLOOR PANEL 152QF WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R. CATAGORY -A- MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 30,279 hrs · 17,126 cycles

FLOOR PANEL 132SG WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R. A CATAGORY -A- MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 30,279 hrs · 17,126 cycles

BULK CARGO FLOOR PANEL 161AF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R. CATAGOY -A- MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 30,279 hrs · 17,126 cycles

FLOOR PANEL 151MF CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R, CAT A MAJOR REPAIR.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 30,279 hrs · 17,126 cycles

FOUND CRACK ON RT CTR FLAP AT RIB 27 APPROX. 4.8" FWD OF REAR SPAR UPPER SKIN. REPAIRED RIB FLANGE IAW SRM 57-50-00, FIG. 205, CAT A MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 30,279 hrs · 17,126 cycles

FLOOR PANEL 152TF CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R, CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 30,279 hrs · 17,126 cycles

BULK CARGO FLOOR PANEL 161CF DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R, CATEGORY -A- MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 30,279 hrs · 17,126 cycles

FLOOR PANEL 152PF CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R, CATEGORY -A- MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 30,279 hrs · 17,126 cycles

MAIN DECK FLOOR PANEL 241MJ BROKEN. FABRICATED MAIN DECK FLOOR PANEL 241MJ ON TD/000425 PER DRAWING SRZ-25-005R, CLASS CAT "A" AND MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 30,279 hrs · 17,126 cycles

MAIN DECK FLOOR PANEL 252NG BROKEN. FABRICATED MAIN DECK FLOOR PANEL 252NG ON TD/000414 PER DRAWING SRZ-25-005R, CAT "A" AND MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 30,279 hrs · 17,126 cycles

MAIN DECK FLOOR PANEL 241NJ IS BROKEN. FABRICATED MAIN DECK FLOOR PANEL 241NJ ON TD/000429 PER DRAWING SRZ-25-005R, CLASS CAT "A" AND MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 30,279 hrs · 17,126 cycles

MAIN DECK FLOOR PANEL 251QH IS BROKEN. FABRICATED MAIN DECK FLOOR PANEL 251QH ON TD/000428 PER DRAWING SRZ-25-005R, CLASSIFIED CAT "A" AND MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 30,279 hrs · 17,126 cycles

MAIN DECK FLOOR PANEL 231RG IS BROKEN. FABRICATED MAIN DECK FLOOR PANEL 231RG ON TD/000427 PER DRAWING SRZ-25-005R, CLASSIFIED CAT "A" AND MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 30,279 hrs · 17,126 cycles

MAIN DECK FLOOR PANEL 251DF IS BROKEN. FABRICATED MAIN DECK FLOOR PANEL 251DF ON TD/000415 PER DRAWING SRZ-25-005R, CLASS CAT "A" AND MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 30,279 hrs · 17,126 cycles

MAIN DECK FLOOR PANEL 231JG IS BROKEN. FABRICATED MAIN DECK FLOOR PANEL 231JG ON TD/000426 PER DRAWING SRZ-25-005R, CLASS CAT "A" AND MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 30,279 hrs · 17,126 cycles

MAIN DECK FLOOR PANEL 231HG IS BROKEN. FABRICATED MAIN DECK FLOOR PANEL 231HG ON TD/000406 PER DRAWING SRZ-25-005R, CLASS CAT "A" AND MAJOR REPAIR.

Part: COMPUTER — FAULTED (FUEL SYSTEM) · airframe 29,399 hrs · 16,565 cycles

PDIS 676 28-40 8572 24SEP19 ELP FACT U LOGPAGES:3167557 CLIMBING THROUGH FL 200, ECAM MEMO PAGE SHOWED ALL XX'S ON GROSS WT CG, AND TOTAL FUEL INDICATION. ECAM FUEL PAGE SHOWED ALL XX'S ON ALL TANKS. THE FUEL PANEL ON THE OVERHEAD SHOWED QUANTITIES FOR THE LEFT OUTER, LEFT INNER AND CTR/TT, BUT THE RIGHT INNER AND RT OUTER WERE BLANK. AT LEVEL OFF, ALL QUANTITIES DISPALYED FOR ABOUT 30 SECONDS, THEN WENT BACK TO INDICATIONS I JUST DESCRIBED. SHGN 24SEP19 04:28 ELP U PERFORMED FUEL SYSTEM BITE REF TSM 28-42-00, OVERHEAD READINGS ARE 7.06 ( REF TSM 28-42-00 REPLACE FQIC ). CYCLED FQI CONTROL BREAKERS AND ALL INDICATIONS RETURNED TO NORMAL. CGCC LAST FLIGHT LEG SHOWS FQIS FAULT. REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: SIC5077-4 POS: ONL SRL: 0400 TAG NR: 19F893 ON MPN: SIC5077-4 CPN: 2810225 SRL: 0296 TAG NR: 3268E8 SHGN 24SEP19 13:46 DUE TO HARD FAULT CODE 706, REMOVED AND REPLACED FQIC 15QT IAW 28-42-38-04. OPS CHECK SATISFACTORY. BITE MEMORY CLEARED. FACT 24SEP19 13:47 ELP U REPLACED FUEL QUANTITY COMPUTER BECAUSE OF FAILED BITE TEST WITH HARD FAULT CODE 706 AND PERFORMED A SUCCESSFUL OPERATIONAL TEST PER AMM 28-42-38. THE FUEL QUANTITY COMPUTER IS QUALIFIED FOR FURTHER SERVICE.

Part: POWER SUPPLY — MALFUNCTIONED (DOOR ARMING) · airframe 28,856 hrs · 16,159 cycles

RIGHT CABIN DOOR WILL NOT ARM NO SLIDE INDICATION ON ECAM AUTONOMOUS STANDBY POWER SUPPLY UNIT C/B RESET. AFTER RESET,DOOR ARMED AND INDICATION OPS SATIS ON ECAM

Part: POWER UNIT — INOPERATIVE (DOOR) · airframe 28,602 hrs · 15,918 cycles

L1 AND R1 DOORS ESCAPE SLIDES RELEASE WARNING LIGHT INOPERATIVE. REMOVED & REPLACED THE AUTONOMOUS STANDBY SUPPLY UNIT, 70 WN IAW AMM 52-73-18-04 AND THE BOTH EMERGENCY POWER SUPPLY BATTERY IAW AMM 33-51-14-04. PERFORMED AN OPS TEST IAW AMM 52-73-00-05-02, PASSED. ACFT OK FOR SERVICE.

Part: INDICATION SYS — INOPERATIVE (R1 DOOR) · airframe 28,600 hrs · 15,915 cycles

R1 ENTRY DOOR ECAM SLIDE INDICATION SYSTEM INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE. UNABLE TO HAVE BOTH L1 AND R1 DOOR ESCAPE SLIDE INDICATION WARNING LIGHT ILLUMINATED AND R1 SLIDE. ECAM INDICATION WHEN DOOR ARMED. NO POWER OUT OF PIN "R" OF 70WN ASPSU WITH BUTT BUS NR 2 OR WITH INTERNAL BATTERIES. UNABLE TO TEST ASPSU WITH TEST BUTTON, NO RESPONSE. SUGGEST TO REPLACE ASPSU 70WN ALONG WITH TWO EMERGENCY BATTERIES PRECAUTIONARY. REMOVED & REPLACED THE AUTONOMOUS STANDBY SUPPLY UNIT (70 WN) PER AMM 52-73-18-04 AND THE BOTH EMERG POWER SUPPLY BATT PER AMM 33-51-14-04. PERFORMED THE TEST PER AMM 52-73-00-05-02 ALL PASSED. A/C OK FOR SERVICE.

Part: O-RING — TORN (HYDRAULIC SYS) · airframe 27,856 hrs · 15,419 cycles

AT CRUISE OVER KTYS FL310 ECAM GRN HYD SYS LOW PSI, SPOILER NR 6 FAULT, THEN ECAM GRN HYD SYS LOW RSVR. GRN SYS HYD QUANTITY GAUGE ON OVERHEAD PANEL AT RED DOT. GRN SYS HYD QUANTITY INDICATOR ON ECAM IN AMBER. AFTER MANUAL GEAR EXTENSION, GRN SYS HYD QUANTITIES ON OVERHEAD PANEL AND ECAM READ NORMAL. FOUND LEAK COMING FROM GREEN/BLUE PTU, AT THE GREEN PRESSURE LINE UNION. REMOVED AND REPLACED "O' RING. REINSTALLED UNION AND PRESSURE LINE. LEAKS CKED GOOD. REFERENCE AMM 29-22-11-04 AND SMP. SERVICE GREEN SYSTEM TO TOP HAT, REFERENCE AMM 12-12-29-00-0. PERFORMED RESTORATION LANDING GEAR ACTUATING TO NORMAL OPERATING CONDITION AFTER FREE FALL EXTENSION, REFERENCE AMM 32-33-00-02-0. RAN NR 1 AND NR 2 ENGINES REFERENCE JRH, AND EXTEN/RETRACT FLAPS, AND RUN ALL FLT CONTROLS. A/C OK FOR SERVICE.

Part: BRACKET — CRACKED (FRAME 47) · airframe 27,734 hrs · 15,343 cycles

ANGLE BRACKET CRACKED, INBD OF SEAT TRACK -Y953, FRAME 47, REMOVED THE ANGLE BRACKET IAW SRM 51-40-21, FABRICATED NEW BRACKET IAW EA 6-5340-T0337966, AND INSTALLED IAW SRM 51-40-21, REPAIR CLASSIFED AS MAJOR.

Part: SEAT TRACK — BROKEN (FRAME 57) · airframe 27,734 hrs · 15,343 cycles

SEAT TRACK SCALOP BROKEN IN MDC BETWEEN FRAMES 57.1 AND 57.2, -Y450. FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-1--16, FIG 102. FABRICATED A NEW SEAT TRACK IAW SRM 53-10-16 FIG. 201 AND INSTALLED IAW SRM 53-10-16 FIG 201, MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,734 hrs · 15,343 cycles

MAIN CABIN FLOOR PANEL 241JF BROKEN. FABRCATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR

Part: FLOOR PANEL — BROKEN (MAIN DECK) · airframe 27,734 hrs · 15,343 cycles

MAIN DECK FLOOR PANEL 252CH BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (MAIN DECK) · airframe 27,734 hrs · 15,343 cycles

MAIN DECK FLOOR PANEL 241GJ BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (MAIN DECK) · airframe 27,734 hrs · 15,343 cycles

MAIN DECK FLOOR PANEL 252NH BROKEN. FABRICAED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 20) · airframe 27,734 hrs · 15,343 cycles

MAIN DECK FLOOR PANEL 241LH DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 27,734 hrs · 15,343 cycles

MAIN DECK FLOOR PANEL 241RJ BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (FRAME 69) · corrosion level 3 · airframe 27,734 hrs · 15,343 cycles

CORROSION ON SEAT TRACK FLANGES UPPER AND LOWER SURFACES AT FRAME 69, Y0. CORROSION FOUND OUT OF LIMITS IAW SRM 53-10-16. REMOVED AND REPLACED THE SECTION IAW SRM 51- 27-11, AND SRM 51-40-44. INSTALLED THE SPLICES IAW SRM 53-10-16, FIG 201B, AND SRM 51-40-21. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (MAIN DECK) · airframe 27,734 hrs · 15,343 cycles

MAIN DECK FLOOR PANEL 252QH BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (FRAME 57) · airframe 27,734 hrs · 15,343 cycles

SEAT TRACK SCALOPS GOUGED BETWEEN FRAMES 57 AND 57.1, Y950. CUT OUT DAMAGED SEAT TRACK SECTION IAW SRM 53-10-16, FIG 201. FABRICATED A NEW SEAT TRACK IAW SRM 53-10-16, FIG 201. INSTALLED IAW SRM 51-40-21. MAJOR REPAIR.

Part: DOUBLER — WORN (TE FLAP) · airframe 24,918 hrs · 13,694 cycles

AGING INSPECTION - EXISTING REPAIR ON LT INBD FLAP MAIN SECTION UPPER SKIN RIB 11A- RIB 14A STG 2.1-STG 2.2. WORN DAMAGE WAS FOUND ON THE EXTERNAL DOUBLE. REMOVED THE DAMAGED DOUBLER AND REPAIRED AGAIN PER A300-600F SRM 57-50-00 FIG 205 AND COMPLETED, TRACKING EA 6-5750-T0321134 P1 WAS ISSUED AND COMPLETED, WING-FLIGHT SURFACES-EO 6-5100-7-5000-SRM REPAIR ON LT INBD FLAP TOP SKIN BETWEEN RIB 11-12, STG 2.1-STG 2.2 - RSC TRACKING.EO 6-5100-7-5000 D1 PT1 WAS COMPLETED. CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 129.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 249 hrs · 13,694 cycles

MDCC HORIZONTAL PRESSURE DECK FRAME 47, Y0 - -Y450, WEB CRACKED APPROX 0.5 INCH IN LENGTH. NDT FOUND THE LENGTH OF THE CRACK WAS OUT OF LIMITS IAW SRM 53-15-15-201 C2 & NTM 51-10-07, L=30 MM. FABRICATED THE NEW WEB IAW DWG A53832100 ISSUE G. PERFORMED THE REPAIR ON THE WEB WITH REPLACEMENT OF THE WEB IAW SRM 51-40-21. THE REPAIR WAS CATEGORY A & WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 129.

Part: FRAME — CRACKED (FUSELAGE) · airframe 249 hrs · 13,694 cycles

CENTER WING, JOINT AT FRAME 40 LT UPPER HOLE HAS CRACK SIGNAL. PERFORMED THE REPAIR IAW EA 6-5710-T0320754 PT 1. THIS REPAIR WAS CATEGORY B & WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 129.

Part: FRAME — CRACKED (FRAME 40) · airframe 249 hrs · 13,694 cycles

CENTER WING, JOINT AT FRAME 40 LT LOWER HOLE HAS CRACK SIGNAL. PERFORMED THE REPAIR IAW EA 6-5710-T0320754 PT 1. THIS REPAIR WAS CATEGORY B & WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 129.

Part: FRAME — CRACKED (FUSELAGE) · airframe 249 hrs · 13,694 cycles

CENTER WING, JOINT AT FRAME 40 RT UPPER HOLE HAS CRACK SIGNAL. PERFORMED THE REPAIR IAW EA 6-5710-T0320754 PT 1. THIS REPAIR WAS CATEGORY B & WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 129.

Part: CROSSBEAM — CRACKED (FRAME 58) · airframe 249 hrs · 13,694 cycles

MDCC CROSSBEAM CRACKED AT FRAME 58, Y1700. IAW SRM 53-10-15 FIGURE 211 REWORK THE STIFFENER & CUT OUT THE CRACK. PERFORM HFEC INSPECTION TO THE CUT OUT & REWORKED AREA IAW NTM 51-10-08 & NO CRACK FOUND. MANUFACTURED THE REPAIR ANGLE & DRILL THE FASTENER HOLES IAW SRM 53-10-15 FIGURE 211. INSTALL THE REPAIR ANGLE IAW SRM 53-10-15 FIGURE 211. THIS REPAIR CATEGORY IS A, MAJOR REPAIR IAW GMM 6-2-100.

Part: PACKING — DAMAGED (HYDRAULIC SYS) · airframe 249 hrs · 13,692 cycles

GREEN HYD QTY IN YELLOW BAND DURING CRUISE. FOUND BLEEDER PLUG ON SIDE OF GREEN MANIFOLD LEAKING. REPLACED PACKING ON BLEEDER PLUG, LEAK & OPERATIONS CHECKED GOOD IAW AMM 29-10-00-03 & 29-10-00-03.

Part: COALESCER BAG — DIRTY (LT & RT) · airframe 22,577 hrs · 12,398 cycles

SMOKE APPEARED IN COCKPIT WITH NO ECAM INDICATIONS, DIVERTED. DURING TOUCHDOWN ECAM DISPLAYED AVIONICS SMOKE THEN EXTINGUISHED. FOUND EXCESSIVE DE-ICE FLUID IN MAIN WHEEL WHEEL WHILE ACCESSING AIR CONDITION PACK BAY AND CLEANED. INSPECTED BOTH LT & RT PACK COALESCER BAGS, FOUND BOTH TO BE VERY DIRTY. REPLACED COALESCER BAGS IAW MM 21-51-16. RAN BOTH ENGINES WITH BOTH PACKS OPERATING FOR 35 MINUTES IAW MM 21-51-00-03, NO NOTICABLE FUMES OR ODORS NOTED AT THIS TIME. ACCOMPLISHED AVIONICS SMOKE DETECTION SYSTEM IAW MM 26-15-00-05, CHECKED NORMAL.

Part: FITTING — CORRODED (RT MLG) · corrosion level 2 · airframe 22,269 hrs · 12,248 cycles

RT MLG NR 5 RIB FWD LUG FITTING CORRODED REPAIR THE LUG FITTING IAW DWG:R57240425 AND EA:6-5710-T0302748.

Part: FITTING — CORRODED (ZONE 500) · corrosion level 2 · airframe 22,269 hrs · 12,248 cycles

LT MLG NR 5 RIB FWD LUG FITTING CORRODED REPAIR THE LUG FITTING IAW DWG:R57240425 AND EA 6-5710-T0302747.

Part: PITOT TUBE — OBSTRUCTED · airframe 22,050 hrs · 12,125 cycles

RTO AT 90 KTS AIRSPEED SPLIT ON TAKEOFF ROLL. F/O AND STBY AIRSPEED MATCHED AT 90 KTS, CAPTAIN`S AIRSPEED AT 50 KTS. REMOVED AND REPLACED CAPTAIN'S PITOT PROBE IAW MM 34-11-15-04. PITOT TUBE THAT WAS REMOVED HAD SMALL BLACK DEBRIS COME OUT OF IT.

Part: COMPUTER — FAILED (ZONE 100) · airframe 21,620 hrs · 11,888 cycles

AVIONICS SMOKE DURING CLIMBOUT, WARNING WAS ACCOMPANIED BY ODOR. NO VISUAL SMOKE ONLY FUMES. FUMES WAS PHENOLIC BURNING ODOR. FLC SYS NR 2 CIRCUIT BREAKER WAS TRIPPED AND DISCOVERED BY MX AFTER BLOCK IN. R & R FLC NR 2 IAW AMM 27-23-26-04. OPS CHECKED GOOD.

Part: BUSHING — WORN (RUDDER) · airframe 21,611 hrs · 11,879 cycles

ACFT SHOOK IN SMOOTH AIR DURING DESCENT FROM LOWER 20`S THROUGH UPPER TEENS. ENGINE PAGE SHOWED NO VIBRATION ANOMOLIES. EXPERIMNTATION, DEMONSTRATED THAT VIBRATION WAS INDEPENDENT OF ENGINE RPM, BUT VARIED WITH SPEED AND COULD BE ALLEVIATED WITH A SLIGHT RUDDER DEFLECTION IN EITHER DIRECTION. COMPLIED WITH EA 6-3220-167712, REV NR POS P2. JACKED NOSE OF ACFT REF AMM 07-11-00-00. PERFORMED GEAR SWING OF NOSE GEAR REF AMM 32-31-00-05 AND FOUND THAT WHEN GEAR HANDLE WAS IN THE UP POSITION, NOSE DOORS FAIRED WELL. WHEN HANDLE PUT IN NEUTRAL, RT AFT NOSE GEAR DOOR DROOPED AND HAD SIGNIFICANT PLAY. INSTALLED NEW BUSHING IN THE DOOR SIDE OF THE ROTATING ROD REF IPC 52-82-13-01. PERFORMED GEAR SWING AGAIN, SAME REF, AND FOUND BOTH DOORS TIGHT AND WELL FAIRED. ACFT OK FOR SERVICE.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 21,602 hrs · 11,870 cycles

ON ARRIVAL AT THE ACFT GREEN HYD QTY WAS LOW, JUST ABOVE YELLOW RANGE MX SERVICED THE GREEN HYD BACK INTO TOP HAT MINIMUM. THEY STATED THERE WAS NO INDICATION OF A LEAK. DURING DESCENT WE HAD A LOW GREEN HYD QTY ALERT. THE OVHD QTY POINTER WAS AT RED DOT. WE TURNED OFF THE GREEN PUMPS AND LANDED W/O INCIDENT. AFTER MANUAL GEAR EXTENSION THE GREEN HYD QTY GAUGE INDICATOR MOVED TO THE 12 O'CLOCK POSITION. BY RETURN TO GATE IT DECREASED BACK ALMOST TO YELLOW AGAIN. REPAIRED CASE DRAIN HYD LINE IAW AMM 20-23-11. LEAK CHECKED GOOD.

Part: PITOT TUBE — OBSTRUCTED (FIRST OFFICER'S) · airframe 21,017 hrs · 11,557 cycles

ON TAKEOFF AT 80KTS - F/O'S PFD SHOWED "0" AIRSPEED, CAPTAIN'S PFD AND BOTH STBY AIRSPEED INDICATORS SHOWED 80KTS. FOUND F/O'S PITOT TUBE PARTIALLY BLOCKED. CLEANED BLOCKAGE, REF MM 34-11-15-04 , PERFORMED PRESSURE TEST ON PITOT SYS. OPS CHECK NORMAL. ACFT REMAINS RVSM REF GMM 6-5-490, ACFT OK FOR SERVICE.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 20,963 hrs · 11,524 cycles

ON DEPARTURE GEAR RETRACTION NORMAL. WHEN HANDLE MOVED TO CENTER POSITION GEAR CAME DOWN ECAM READ "L/G RETRACTION FAULT" DOORS SHOWED RED UNLOCKED. PUT GEAR HANDLE DOWN GEAR SHOWED LOCKED. NO FURTHER ATTEMPT TO RAISE GEAR. MEM U IAW VERBAL FROM CAPT. GOT A L/G RETRACTION INOP MESSAGE NOT A L/G RETRATION FAULT MESSAGE. R & R LANDING GEAR SELECTOR VALVE (3GA) IAW AMM.

Part: CONTROL SWITCH — MALFUNCTIONED (MLG) · airframe 20,963 hrs · 11,524 cycles

AFTER TAKEOFF LANDING GEAR RETRACTED NORMALLY, BUT WHEN GEAR HANDLE WAS PLACED IN THE NEUTRAL POSITION GEAR EXTENDED. INDICATIONS WERE 3 GREEN PLUS 3 UNLOCK LIGHTS. HANDLE RETURNED TO THE UP POSITION AND GEAR RETRACTED NORMALLY. HANDLE RETURNED TO NEUTRAL WITH NORMAL INDICATIONS REMINDER OF FLIGHT. GEAR EXTENDED NORMALLY FOR LANDING. NO LIMITATIONS WERE EXCEEDED. BITE TEST OF THE PROXIMITY BOX REF AMM 32-61-00, FOUND NO HARD FAULTS. WHILE ACCOMPLISHING THE TEST, FAULTS 24 & 64 WITH THE BOX LIGHT ON. SWUNG GEAR SEVERAL TIMES, NO DEFECTS NOTED, REF MM 32-31-00. AS A PRECAUTION, R & R LANDING GEAR CONTROL HANDLE IAW MM 32-31-11-04. PERFORMED OPS CHECK OF LANDING GEAR CONTROL SWITCHING UNIT IAW MM 32-31-11-04.

Part: PLUG — LEAKING (HYD SYSTEM) · airframe 20,881 hrs · 11,465 cycles

YELLOW HYD SYSTEM FAILED IN FLT. HYD QTY LOW. FOUND TWO PLUGS ON ACTUATOR BODY LEAKING AND NOT SAFETIED. TORQUED BOTH PLUGS REF. AMM 20-21-12-00 AND SAFETIED. SERVICED YELLOW SYSTEM REF. AMM 12-12-29-00. PRESSURIZED ALL THREE SYSTEMS WITH ELECTRIC PUMPS AND CYCLED RUDDER. OPS AND LEAK CHECKED GOOD.

Part: PROXIMITY SENSOR — FAILED (MLG) · airframe 20,467 hrs · 11,222 cycles

AFTER TAKEOFF, COULD NOT RAISE SYS 2 GEAR HANDLE, USED SYS 1. LOST F/O PITOT HEAT & TAT PROBES. LOST PITCH TRIM NR 2 & NR 2 CABIN PRESSURE REGULATOR. WOULD NOT RESET IN AIR & ALL SYSTEMS RETURNED TO NORMAL ON LANDING. PSU SHOWS FAULT 14, RT MLG SYS 2 PROXIMITY DETECTOR 62GB FAULTED IAW AMM 32-00-00-04. FOUND SENSOR 62GB CONNECTOR LOOSE AFTER REMOVING HEAT SHRINK. CLEANED CONNECTOR & REPLACED HEAT SHRINK. REPLACED PROXIMITY BOX IAW MM 32-31-71-04-0 & OPS CHECKED OK. OPS CHECKED PITOT HEAT & TAT OK IAW MM 30-31-00-05-0, PITCH TRIM OK IWA MM 22-27-00-05, CABIN PRESSURE OK IAW MM 21-31-00-05-0.

Part: FAIRING — MISSING (LT WING) · airframe 19,180 hrs · 10,480 cycles

AFTER FLIGHT, A FAIRING WAS DISCOVERED MISSING ON LT WING, UNDERSIDE, OTBD OF AFT PART OF THE ENGINE PYLON. NEW FAIRING INSTALLED AS PER AMM 57-20-35 REV 52.0. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112

Part: SEAT TRACK — WORN (ZONE 200) · airframe 19,178 hrs · 10,478 cycles

MAIN DECK SEAT TRACK AT FRAME 38.2, NR 3 LEFT FOUND EXCEEDED LIMITS VALUE 0.043 INCH PER 6-5310-7-3322 P1 ITEM 11(I) MAIN DECK SEAT TRACK AT CABIN FRAME 38.2, RIGHT HAND NO.: 3 REPAIRED PER E.O. 6-5310-7-3322B PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV 112.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 19,178 hrs · 10,478 cycles

MAIN DECK SEAT TRACK AT CABIN FRAME 38.2, NR.:4 LT FOUND WORN, EXCEEDED LIMITS VALUE 0.050 INCH IAW EO 6-5310-3322, P1 ITEM 11 (I). MAIN DECK SEAT TRACK AT CABIN FRAME 38.2, NT.:4 LT REPAIRED IAW "EO 6-5310-7-3322B, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 19,178 hrs · 10,478 cycles

MAIN DECK SEAT TRACK AT FRAME 54.2, NR 5 LT, FOUND WORN EXCEEDED LIMITS, VALUE 0.020" IAW EO 6-5310-7-3322 P1 ITEM 11(I). MAIN DECK SEAT TRACK AT CABIN FRAME 54.2, NR 5 LT REPAIRED IAW EO 6-5310-7-3322B PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 19,178 hrs · 10,478 cycles

MAIN DECK SEAT TRACK AT FRAME 38.2, LT FOUND WORN EXCEEDED LIMITS VALUE 0.034 INCH IAW EO 6-5310-7-3322 P1 ITEM 11 (I). MAIN DECK SEAT TRACK AT CABIN FRAME 38.2, LT NR 5 REPAIRED IAW EO 6-5310-7-3322B, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 19,178 hrs · 10,478 cycles

MAIN DECK SEAT TRACK AT FRAME 38.2 NO.: 1 FOUND WORN EXCEEDED LIMITS VALUE 0.025 INCH PER EO 6-5310-7-3322 P1 ITEM 11 (I) MAIN DECK SEAT TRACK AT CABIN FRAME 38.2, REPAIRED PER E.O. 6-5310-7-3322B PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV 112.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 19,178 hrs · 10,478 cycles

MAIN DECK SEAT TRACK AT FRAME 54.2, NR 4 LEFT FOUND EXCEEDED LIMITS VALUE 0.023 INCH PER EO 6-5310-73322 P1 ITEM 11 (I) MAIN DECK SEAT TRACK AT CABIN FRAME 54.2, LEFT NR 4 REPAIRED PER E.O. 6-5310-7-3322B PART 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV 112.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 19,178 hrs · 10,478 cycles

CABIN SEAT TRACK AT FRAME 38.2, RIGHT HAND NO.: 3 FOUND 0.027 INCH WORN EXCEEDED LIMITS PER EO 6-5310-7-3322 ITEM 11(I), MAIN DECK SEAT TRACK AT CABIN FRAME 38.2, RIGHT HAND NO.: 3 REPAIRED PER EO 6-5310-7-3322B PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV 112.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 19,178 hrs · 10,478 cycles

MAIN DECK SEAT TRACK AT FRAME 38.2 LEFT FOUND EXCEEDED LIMITS VALUE 0.033 INCH PER EO 6-5310-7-3322 P1 ITEM 11 (I) MAIN DECK SEAT TRACK AT CABIN FRAME 38.2, LEFT REPAIRED PER E.O. 6-5310-7-3322B PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV 112.

Part: ACCESS PANEL — DELAMINATED (ZONE 100) · airframe 19,178 hrs · 10,478 cycles

LEFT HAND AIRCON COMPARTMENT ACCESS PANEL 147DZ FOUND DELAMINATED MORE THAN 70%. LEFT AIR CON COMPARTMENT ACCESS PANEL 1487DZ REMOVED AND REPLACED PER AMM 25-72-41-04 REV 52.0. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: ATTACH FITTING — CRACKED (CARGO DOOR) · airframe 19,178 hrs · 10,478 cycles

DURING HFEC INSP, CRACK APPROX 0.7 INCH, FOUND ON FWD CARGO DOOR. (FRAME 22A) ACTUATOR ATTACH FITTING. REMOVED AND REPLACED PER SRM 52-31-00, FIGURE 204 REV 20. ACCOMPLISHED E.A. 6-5230-150306. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.

Part: RIB — CRACKED (LT WING) · airframe 19,178 hrs · 10,478 cycles

LT WING INBD FLAP RIB 25A HORIZ UPPER FLANGE FOUND APPROX (1) INCH CRACKED. REMOVED AND REPLACED PER DRAWINGS: A5796000, 27A57960110 AND 57A5796005. ACCOMPLISHED FEDEX E.A. 6-5750-143558. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.

Part: RIB — CRACKED (RT WING) · airframe 19,178 hrs · 10,478 cycles

RT WING INBD FLAP RIB 25A HORIZ UPPER FLANGE FOUND APPROX (2) INCH CRACKED. REMOVED AND REPLACED PER DRAWINGS: A5796000, 27A57960110 AND 57A5796005. ACCOMPLISHED E.A. 6-5750-143559. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV 112.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 15,926 hrs · 8,625 cycles

MAIN CARGO FLOOR BOARD NR 242 AJ IS CRACKED AT FRAMES 50 - 54. MATERIAL ID FOR THE FLOOR PANEL IAW DWG SRZ 25-005, REV "G" AND ENGINEERING REPORT 91-019 QPL. MATERIAL P/N 402H35039-003, PO 626008.1. FABRICATED A NEW FLOOR PANEL PER DWG SRZ 25-005; REV "G". PAINT IAW AMM 51-23-20-0.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 15,926 hrs · 8,625 cycles

THE ADAPTER TRACK AT FRAME 61 RIGHT SIDE BUTT LINE 1456 HAS SCALLOPS BROKEN OFF. REMOVED FLOOR PANEL 252 UH TO GAIN ACCESS IAW AMM 53-10-25-4. RECEIVED A NEW ADAPTER TRACK PO 592553.5. LOCATED AND DRILLED THE NEW ADAPTER TRACK IAW SRM 51-40-40. INSTALLED THE NEW ADAPTER TRACK REF DWG A53278288; REV "A" AND SRM 51-40-21, PARA 7. INSTALLED FLOOR PANEL 252 UH REF AMM 53-10-25-4.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 15,926 hrs · 8,625 cycles

MAIN CABIN SEAT TRACK AT FRAME 57.1, Y 45.0 IS WORN AT THE TANG. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-10-16.

Part: ADAPTER — GOUGED (ZONE 200) · airframe 15,926 hrs · 8,625 cycles

MAIN DECK CARGO COMPARTMENT CROSS TRACK AT FRAME 32; LBL 54. DAMAGE TO ADAPTER IS BEYOND LIMITS IAW SRM 53-10-15. REMOVED DAMAGED ADAPTER IAW SRM 51-40-21. LOCATED, DRILLED & INSTALLED THE NEW ADAPTER IAW DWG 10A53791837 & SRM 51-40-21.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 15,926 hrs · 8,625 cycles

LEFT WING INBD FLAP TOP SKIN IS CHAFED AT APPROX 13 INCHES AFT OF THE FRONT SPAR AND 79 INCHES FROM THE INBD EDGE. BLENDED CHAFED AREA REF SRM SRM 51-73-10. ORIGINAL MATERIAL THICKNESS 0.031 REF SRM 57-52-12. REMOVED MATERIAL 0.003. MATERIAL REMAINING 0.028, FOUND TO BE BEYOND LIMITS REF SRM 57-50-00. CUT OUT DAMAGED SKIN REF SRM 57-50-00; FIG 205. FABRICATED A REPAIR DOUBLER REF SRM 57-50-00; FIG 205. ALODINED REPAIR DOUBLER REF SRM 51-21-10. PRIMED REPAIR DOUBLER REF SRM 51-23-10. INSTALLED REPAIR DOUBLER REF SRM 57-50-00; FIG 205. PAINTED REPAIR DOUBLER REF SRM 51-23-10.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,926 hrs · 8,625 cycles

MAIN DECK CARGO COMPARTMENT FLOORBOARD IS TORN BETWEEN FRAME 43 AND FRAME 47; LBL 57 AND LBL 77. NR 241 WH FABRICATED FLOORBOARD IAW FEDEX DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000.

Part: SKIN PANEL — DAMAGED (ZONE 200) · airframe 15,926 hrs · 8,625 cycles

EXTERNAL FUSELAGE SKIN HAS EVIDENCE OF LIGHTNING STRIKE AT FRAME 13 A; STRINGERS 20 R TO 21 R, (JUST FWD OF THE L-1 DOOR). COMPLIED WITH THE PERMANENT LIGHTNING STRIKE REPAIR PAE SRM 53-10-12; FIG 203; SHEET 1.

Part: FLOORBOARD — TORN (ZONE 200) · airframe 15,926 hrs · 8,625 cycles

MAIN DECK CARGO COMPARTMENT FLOORBOARD IS TORN BETWEEN FRAME 34 AND FRAME 37; RBL 17 AND RBL 37. NR 242 GF FABRICATED FLOORBOARD IAW DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000.

Part: FLOORBOARD — TORN (ZONE 200) · airframe 15,926 hrs · 8,625 cycles

MAIN DECK CARGO COMPARTMENT FLOORBOARD IS TORN BETWEEN FRAME 37 AND FRAME 38.2; RBL 17 AND RBL 34. NR 242 MF FABRICATED FLOORBOARD IAW DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000.

Part: FLOORBOARD — TORN (ZONE 200) · airframe 15,926 hrs · 8,625 cycles

MAIN CABIN FLOOR BOARD IS TORN BETWEEN FRAME 58 AND FRAME 60, RBL 18 AND RBL 37. FABRICATED A NEW PANEL IAW DWG SRZ 25-005; REV "G". PART MARKED IAW GMM 7-0-1000.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 15,926 hrs · 8,625 cycles

AVIONICS COMPARTMENT FLOOR PANEL 121 JF HAS EDGE DAMAGE. FABBED A NEW PANEL IAW DWG SRZ 25-005; REV "G".

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 15,926 hrs · 8,625 cycles

BULK CARGO PIT FLOOR PANEL 161 GF HAS NUMEROUS AREAS OF DELAMINATION AND DENTS. FABBED NEW FLOOR PANEL IAW DWG SRZ 25-005; REV "G". MATERIAL ID A402H35039-003 IAW DWG SRZ 25-005; REV "G". PART MARKED IAW GMM 7-0-1000.

Part: FLOORBOARD — TORN (ZONE 200) · airframe 15,926 hrs · 8,625 cycles

MAIN DECK CARGO COMPARTMENT FLOORBOARD IS TORN BETWEEN FRAME 40 AND FRAME 43; LBL 57 AND LBL 77. NR 241 TH FABRICATED FLOORBOARD IAW DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000.

Part: FLOORBOARD — TORN (ZONE 200) · airframe 15,926 hrs · 8,625 cycles

MAIN DECK CARGO COMPARTMENT FLOORBOARD IS TORN BETWEEN FRAME 34 AND FRAME 37; RBL 17 AND RBL 37. FABRICATED FLOORBOARD IAW DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 15,926 hrs · 8,625 cycles

MAIN DECK CARGO COMPARTMENT FLOORBOARD 262 AH IS TORN BETWEEN FRAME 77 AND FRAME 80, RBL 57 AND RBL 70. FABRICATED FLOORBOARD IAW DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 15,926 hrs · 8,625 cycles

MAIN DECK CARGO COMPARTMENT FLOORBOARD IS CRACKED BETWEEN FRAME 77 AND FRAME 88; RBL 30 AND RBL 45. FABRICATED FLOORBOARD IAW DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000.

Part: FLOOR PANEL — CONTAMINATED (ZONE 100) · airframe 15,926 hrs · 8,625 cycles

MAIN WHEEL WELL FLOOR PANEL 147 AF IS DELAMINATED AND SOAKED WITH HYDRAULIC FLUID. FABRICATED A NEW PANEL IAW DWG SRZ 25-005; REV "G". PART MARKED IAW GMM 7- 0-1000.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 15,926 hrs · 8,625 cycles

CABIN FLOOR BOARD 251 RG IS CRACKED BETWEEN FRAME 57.1 & FRAME 58; LBL 57 & LBL 77. FABBED NEW FLOOR PANEL IAW DWG SRZ 25-005, REV "G". PART MARKED IAW GMM 7-0-1000.

Part: FLOORBOARD — TORN (ZONE 200) · airframe 15,926 hrs · 8,625 cycles

MAIN DECK CARGO COMPARTMENT FLOORBOARD IS TORN BETWEEN FRAME 60 AND FRAME 62, RBL 18 AND RBL 37. 242 QJ FABRICATED FLOORBOARD IAW DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000.

Part: FLOORBOARD — TORN (ZONE 200) · airframe 15,926 hrs · 8,625 cycles

MAIN DECK CARGO COMPARTMENT FLOORBOARD 252 NH HAS A TORN CORNER BETWEEN FRAME 58 AND FRAME 60; RBL 0 AND RBL 18. FABBED A NEW PANEL IAW DWG SRZ 25-005; REV "G". PART MARKED IAW GMM 7-0-1000.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 15,926 hrs · 8,625 cycles

FWD LOWER CARGO COMPARTMENT FLOOR PANEL 132 MG IS BROKEN AND PUNCTURED. FABBED NEW PANEL 132 MG IAW DWG SRZ 25-005; REV "G". PART MARKED IAW GMM 7-0-1000.

Part: FLOORBOARD — TORN (ZONE 600) · airframe 15,926 hrs · 8,625 cycles

MAIN DECK CARGO COMPARTMENT FLOOR BOARD 252 GF IS TORN BETWEEN FRAME 57.1 AND FRAME 58, RBL 18 AND RBL 37. FABRICATED A NEW PANEL IAW DWG SRZ 25-005; REV "G". PART MARKED IAW GMM 7- 0-1000.

Part: FLOORBOARD — TORN (ZONE 200) · airframe 15,926 hrs · 8,625 cycles

MAIN DECK CARGO COMPARTMENT FLOORBOARD IS TORN BETWEEN FRAME 60 AND FRAME 62, RBL 18 AND RBL 37. FABBED A NEW PANEL IAW DWG SRZ 25-005, REV "G". PART MARKED IAW GMM 7- 0-1000.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 15,926 hrs · 8,625 cycles

AVIONICS COMPARTMENT FLOOR PANEL 122 JF HAS EDGE DAMAGE. FABBED A NEW PANEL IAW PANEL IAW DWG SRZ 25-005 "G". PART MARKED IAW GMM 7-0-1001.

Part: FITTING — CRACKED (RT FUEL TANK) · airframe 15,926 hrs · 8,625 cycles

RIGHT THS INTERNAL FUEL TANK HOIST POINT FITTING IS CRACKED AT THE FWD SPAR, ACCESS 343 BB. WORK ACCOMPLISHED ON EA 6-5510-7-5001.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 15,926 hrs · 8,625 cycles

THERE ARE TOOL MARKS ON THE FLOOR CAPS IN THE MAIN CABIN AT FRAME 11, LBL 20 TO RBL 10. REMOVED DAMAGE. MATERIAL ID FOR REPAIR. FABRICATED AND INSTALLED REPAIR IAW SRM 51-70-10. ALODINED AND PRIMED IAW AMM 51-75-10-8.

Part: FLOOR SUPPORT — GOUGED (ZONE 200) · airframe 15,926 hrs · 8,625 cycles

DAMAGED FLOOR CAP AT FRAME 13 AND FWD; BL 0. REPAIRED DAMAGED FLOOR CAP IN REF TO SRM 51-71-50 & DWG A53612213.0

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 15,926 hrs · 8,625 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK IS GOUGED BETWEEN FRAME 63 AND FRAME 64, RBL 18. BLENDED AREA AND FOUND THE REMAINING MATERIAL TO BE BEYOND ALLOWABLE LIMITS IAW A300-600 SRM 53-10-16, FIG 102, TOOL NR T8878G. REPAIRED THE SEAT TRACK IAW A300-600 SRM 53-10-16, PGS 207/208. REMOVED AND RE-INSTALLED ELECTRICAL BRACKETS AND GROUND WIRES AS REQUIRED IAW A300-600 SRM 51-40-21; PARA 5.

Part: FITTING — CRACKED (RT FUEL TANK) · airframe 15,926 hrs · 8,625 cycles

RIGHT THS INTERNAL FUEL TANK HOIST POINT FITTING IS CRACKED AT THE FWD SPAR, ACCESS 343 EB. WORK ACCOMPLISHED ON E.A. 6-5510-7-5001.

Part: WEB — CRACKED (FUSELAGE) · airframe 15,926 hrs · 8,625 cycles

CABIN RIGHT SIDE FLOOR WEB IS CRACKED AT FRAME 77; RBL 75. REMOVED THE CRACKED FLOOR WEB IAW SRM 51-40-21. LOCATED & DRILLED THE NEW WEB IAW DRAWING 18A53980389. INSTALLED WEB IAW SRM 53-18-18.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 15,926 hrs · 8,625 cycles

THE FWD LOWER CARGO DOOR INTERNAL SKIN IS CHAFFED AT DOOR FRAMES 7 AND 9. BLENDED IAW A300-600 SRM 51-74-10. UPON FURTHER INVESTIGATION MATERIAL REMAINING 0.050. FOUND TO BE WITHIN LIMITS IAW A300-600 52-30-00. ALODINED IAW A300-600 SRM 1-21-10; PARA 5-C. PRIMED AND PAINTED IAW A300-600 SRM 51-23-10, PARA 3-C.

Part: STRUCTURE — CORRODED (T/E FLAP) · airframe 12,631 hrs · 6,919 cycles

RIGHT WING TRAILING EDGE O/B FLAP AFT O/B CORNER UNDER STATIC WICK BASE IS CORRODED. COMPLIED WITH EA 6-5750-102894 & N00182 WITH JPF ATTACHED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 12,631 hrs · 6,919 cycles

KEEL BEAM BOX ANGLE CRACKED FROM RIVET TO RIVET ON AFT SIDE OF FR44 LT FWD SIDE OF BOX. CUT HORIZONTAL FLANGE OF RIB 44, FABRICATED AND INSTALLED REPAIR ANGLE AND SHIM PER FEDEX EA 6-5310-102893.

Part: ADAPTER — CORRODED (FUSELAGE) · airframe 12,631 hrs · 6,919 cycles

MDCC, ZONE, CLS ADAPTOR IS CORRODED AT FRAME 69 BETWEEN SEAT TRACKS 3L AND 4L. REMOVED CORROSION ON CLS ADAPTOR IAW A300-600 SRM 51-74-10 AND EA 6-5321-102474.

Part: SEAT TRACK — OUT OF POSITION (FUSELAGE) · airframe 12,631 hrs · 6,919 cycles

SEAT TRACK PULLED AWAY FROM FRAME BETWEEN FR 20 AND 21 (SEAT TRACK 5L). REPAIRED IAW EA 6-5313-102503 AND A300-600 SRM 51-40-21.

Part: PANEL — CORRODED (FUSELAGE) · airframe 12,631 hrs · 6,919 cycles

MDC FRAME 27 TO 28 BETWEEN SEAT TRACK 4L AND 5L THRUST PANEL IS CORRODED. REMOVED CORROSION IAW A300-600 SRM 51-74-10.

Part: PANEL — CORRODED (FUSELAGE) · airframe 12,631 hrs · 6,919 cycles

CORROSION MDC THRUST PANEL AT FRAME 26-27 SEAT TRACK 1L (1EA AREA). REMOVED CORROSION IAW A300-600 SRM 51-74-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,631 hrs · 6,919 cycles

CORROSION MDC THRUST PANEL AT FRAME 27- 28 SEAT TRACK 2L-3L 2EA AREAS OF CORROSION. REMOVED CORROSION IAW A300-600 SRM 51-74-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,631 hrs · 6,919 cycles

CORROSION MDC THRUST PANEL AT FRAME 25-26 SEAT TRACK 1L SEAT TRACK HAS IEA AREA OF CORROSION. REMOVED AND REPLACED THRUST PANEL IAW A300-600 SRM 51-40-21.

Part: ADAPTER — CORRODED (FUSELAGE) · airframe 12,631 hrs · 6,919 cycles

MDCC, ZONE 250, CLS ADAPTOR BETWEEN SEAT TRACK 4R AND 5R AT FRAME 58 HAS AREA OF CORROSION. REMOVED CORROSION IAW A300-600 SRM 51-74-10 AND EA 6-5321-102474.

Part: PANEL — CORRODED (FUSELAGE) · airframe 12,631 hrs · 6,919 cycles

CORROSION ON MDC THRUST PANEL AT FRAME 27-28 SEAT TRACK 3R-4R 3EA AREAS. REMOVED CORROSION IAW A300-600 SRM 51-74-10.

Part: ADAPTER — CORRODED (FUSELAGE) · airframe 12,631 hrs · 6,919 cycles

MDCC, ZONE 250, CLS ADAPTOR BETWEEN SEAT TRACKS 1R AND 2R AT FR 56 HAS CORROSION INSIDE TRACK. REMOVED CORROSION IAW A300-600 SRM 51-74-10 AND EA 6-5321-102474.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,631 hrs · 6,919 cycles

MDCC, ZONE 240, FLOORBEAM CRACKED BETWEEN SEAT TRACKS 3R AND 4R AT FRAME 35. REPAIRED FLOORBEAM IAW A300-600 FREIGHTER SRM 53-10-15 FIG 207 SECTION A-A.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,631 hrs · 6,919 cycles

MDCC FLOORBEAM IS CRACKED FR 38 BETWEEN SEAT TRACKS 4L AND 5L. REPAIRED FLOORBEAM IAW A300-600 SRM 51-75-10.

Part: ADAPTER — CORRODED (FUSELAGE) · airframe 12,631 hrs · 6,919 cycles

MDCC, ZONE 250, CLS ADAPTOR BETWEEN SEAT TRACKS 1R AND 2R AT FRAME 57 IS CORRODED. REMOVED CORROSION IAW A300-600SRM 51-74-10 AND EA 6-5321-102474.

Part: SEAT TRACK — TOOL DAMAGE · airframe 12,631 hrs · 6,919 cycles

NRC NR N00156, MDCC, ZONE 260, SEAT TRACK L-1 AT FRAME 80 HAS TOOLING MARKS INSIDE TRACK. REPAIRED SEAT TRACK IAW A300-600 SRM 53-10-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,631 hrs · 6,919 cycles

CORROSION MDC THRUST PANEL AT FRAME 25-26 SEAT TRACK 2L-3L (2EA SPOTS). REMOVED AND REPLACED PANEL IAW A300-600 SRM 51-40-21.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,631 hrs · 6,919 cycles

MDCC, ZONE 260, FLOORBEAM CRACKED BETWEEN SEAT TRACK 0 AND 1R AT FR 75. REPAIRED FLOORBEAM IAW A300-600 SRM 53-10-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,631 hrs · 6,919 cycles

CORROSION MDCC THRUST PANELS AT FRAME 27-28 SEAT TRACK 3L-4L REF N00429. REMOVED CORROSION IAW A300-600 SRM 51-74-10, FOUND TO BE WITHIN LIMITS IAW A300-600 SRM 53-10-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,631 hrs · 6,919 cycles

CORROSION MDC THRUST PANEL AT FR 26-27 SEAT TRACK 3L- 4L (2EA SPOTS). REMOVED AND REPLACED PANEL IAW A300-600 SRM 51-40-21.

Part: BRAKE — MALFUNCTIONED (LANDING GEAR) · airframe 12,201 hrs · 6,669 cycles

AFTER LANDING DURING ROLL AT SLOW SPEED AUTOBRAKES CYCLED. A/C BEGINS TO YAW LEFT. TOOK OVER MANUAL CONTROL BRAKES INEFFECTIVE. A/C LEFT SIDE OF RUNWAY. C/B'S PULLED. MX, CVR C/B PULLED TRANSFERED TO NEW WRI CHP 23. PERFORMED BITE CHECK OF BSCU IAW A300-600 AMM 32-42-00-5, NO FAULTS FOUND WITH BRAKE SYSTEM CONTROL. NO OTHER ATA'S OR MECHANICAL PROBLEMS WERE DETERMINED AT THIS TIME

Part: APU — LEAKING (APU BAY) · airframe 7,244 hrs · 3,886 cycles

DURING TAKEOFF APPROX 600 FT, CAPT SMELLED SMOKE BY MAIN DECK CARGO, SMOKE DET RT MID 2 SMOKE LOOP FOLLOWED BY LT MID 2 LOOP. DURING PROCEDURES ON DOWNWIND BOTH LIGHTS WENT OUT. ON FINAL BOTH MID 2 LOOPS ILLUM'D AND ON TOUCHDOWN MID 1 LEFT & RIGHT LOOPS ILLUMINATED. DURING GROUND EVACUATION R-1 WAS USED, DOOR OPENED BUT SLIDE DID NOT INFLATE. SMOKE RELATED ISSUE HAS BEEN ISOLATED TO APU LOAD COMPRESSOR BYPASS OIL LEAK REF: DISC 49-50/3233.

Part: WARNING LIGHT — FALSE INDICATION (CABIN) · airframe 6,970 hrs · 3,723 cycles

AFT AND BULK SMOKE LIGHT CAME ON DURING LANDING APPROACH AT 1000 FT AGL. FIRED AGENT 1. LIGHT WENT OUT AFTER A SHORT DELAY. FIRE PERSONNEL REPORTED NO EXTERIOR INDICATION OF SMOKE OR FIRE AFTER LANDING. FIRST OFFICER REPORTED MUSTY ODOR PRIOR TO DONNING OXYGEN MASK. AIRCRAFT RELEASED FOR SERVICE IAW MEL/CDL: 26-16-02-B FACT 06FEB03 12:46 REPLACED NR 1 LOWER DECK FIRE EXT BOTTLE. M/M REF. 26-23-11-4-02. ALL CHECKS OK.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 6,375 hrs · 3,370 cycles

TWO INCHES FROM FWD EDGE OF HANDLE OF BULK CARGO DOOR HANDLE CUTOUT GOUGED.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 4,961 hrs · 2,558 cycles

DURING CLIMBOUT, SEVERE COMPRESSOR STALL NR 2 ENG.

Part: PLATE — MISSING (LT MLG) · airframe 3,309 hrs · 1,681 cycles

FWD TRUNNION NUT ON LEFT HAND MAIN LAND GEAR LOOSE. LOCK PLATE MISSING.

Part: TRUNNION — LOOSE (LT MLG) · airframe 3,309 hrs · 1,681 cycles

FWD TRUNNION NUT ON LEFT HAND MAIN LAND GEAR LOOSE. LOCK PLATE MISSING. REF A300-600 IPC 32-11-05-02 FIG 2, PG 1 ITEM 150.

Part: FMC — INOP (E & E COMPT)

RTO IN DEN DUE TO MASTER CAUTION LIGHT ILLUM AND AUTO PILOT DISCONNECT AT 80 KNOTS. NO FAIL NOTED, CREW TOOK THE ACTIVE AGAIN. RTO NR 2 AUTOTHROTTLE DID NOT ENGAGE WHEN TOGA WAS SELECTED. MAINTENANCE PERFORMED GROUND SCAN, SHOW NO FAULTS. AUTOTHROTTLE CK OK, NO FAULTS PER AMM 22-30-00. AFS/LAND TEST SHOW NO FAULT. RESET FMC'S, ALL SYS OK.