N651FE

Part: FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 38,808 hrs · 21,537 cycles

LH RIB 5, MLG FWD PINTLE AIRFRAME ATTACH FITTING HAS CORROSION ON AFT SPOT FACE. REPAIRED PER AIRBUS INSTRUCTIONS R57240425

Part: FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 38,808 hrs · 21,537 cycles

LH RIB 5, MLG FWD PINTLE AIRFRAME ATTACH FITTING HAS CORROSION ON FWD SPOT FACE. REPAIRED PER AIRBUS INSTRUCTIONS R57240425

Part: FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 38,808 hrs · 21,537 cycles

L/H MLG AFT PINTLE FWD LUG HAS SIGN OF CORROSION. REPAIRED PER AIRBUS INSTRUCTIONS R57240425

Part: SKIN — UNKNOWN (ZONE 600) · airframe 38,277 hrs · 21,141 cycles

AGING AIRCRAFT ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP LWR SKIN BTW RIB 11~13 T/E-9". COMPLIED WITH ATTACHMENT B OF EO: E 6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA: EA#6-5710-149787, TITLE:WINGS-FLIGHT SURFACE-RH IB FLAP EXISTING AND NEW REPAIR EO 6- 5100-7-5000-RSC TRACKING, THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY A REPAIR. "MAJOR REPAIR"

Part: SKIN — UNKNOWN (ZONE 600) · airframe 38,277 hrs · 21,141 cycles

AGING AIRCRAFT ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP UPR SKIN BTW RIB 1C~5,STGR 2.1~2.2. COMPLIED WITH ATTACHMENT B OF EO: E 6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA: EA#6-5710-149787, TITLE:WINGS-FLIGHT SURFACE-RH IB FLAP EXISTING AND NEW REPAIR EO 6- 5100-7-5000-RSC TRACKING, THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY A REPAIR. "MAJOR REPAIR"

Part: SKIN — UNKNOWN (ZONE 600) · airframe 38,277 hrs · 21,141 cycles

AGING AIRCRAFT ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP LWR SKIN BTW RIB 11~13 T/E-9". COMPLIED WITH ATTACHMENT B OF EO: E 6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA: EA#6-5710-149787, TITLE:WINGS-FLIGHT SURFACE-RH IB FLAP EXISTING AND NEW REPAIR EO 6- 5100-7-5000-RSC TRACKING, THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY A REPAIR. "MAJOR REPAIR"

Part: SKIN — UNKNOWN (ZONE 600) · airframe 38,277 hrs · 21,141 cycles

EXISTING REPAIR ON RH WING #1 SLAT TAIL SECTION UPR SKIN, T/E-11.5" POSITION, BTW RIB 8~9, EVALUATE TO DETERMINE WHETHER IT IS ACCOMPLISHED BY APPROVED DATA DUE TO NO EXISTING DOCUMENTATION SUPPORTING THIS REPAIR, REMOVED THE EXISTING REPAIR AND PERFORMED NEW REPAIR TO THE AREA I.A.W. EA # 6-5750-T0373635, TITLE: WINGS- FLIGHT SURFACES-RH #1 SLAT- EXISTING REPAIRS ON TAIL SECTION TOP SKIN-DOUBLER REPAIR, THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY A REPAIR. "MAJOR REPAIR"

Part: SKIN — UNKNOWN (ZONE 600) · airframe 38,277 hrs · 21,141 cycles

EXISTING REPAIR ON RH WING #1 SLAT TAIL SECTION UPR SKIN, T/E-8.5" POSITION, BTW RIB 22~24, EVALUATE TO DETERMINE WHETHER IT IS ACCOMPLISHED BY APPROVED DATA DUE TO NO EXISTING DOCUMENTATION SUPPORTING THIS REPAIR, REMOVED THE EXISTING REPAIR AND PERFORMED NEW REPAIR TO THE AREA I.A.W. EA # 6-5750-T0373635, TITLE: WINGS- FLIGHT SURFACES-RH #1 SLAT- EXISTING REPAIRS ON TAIL SECTION TOP SKIN-DOUBLER REPAIR, THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY A REPAIR. "MAJOR REPAIR"

Part: SEAT TRACK — WORN (ZONE 200) · airframe 38,277 hrs · 21,141 cycles

FR54/FR54.2 RH NO.2 DUMMY SEAT TRACK GAP OVER 1.0MM. I.A.W A300-600 SRM 53-15-16 PARA 5A FIG.201 P201-P210 PERFORM REPAIR ACCOMPLISHED.

Part: SPOILER — DELAMINATED (ZONE 500) · airframe 38,277 hrs · 21,141 cycles

LH WING #6 SPOILER L/E CTR SECTION DELAMINATED. REMOVED L6 SPLR, REPAIRED THE DELAMINATION AREA, REINSTALLED, ADJUSTED, AND PFMED TEST OF L6 SPLR IAW A300-600 AMM 27-61-53-04 AND A300-600F SRM 57-72-11-201, PARA.12, PAGE.211-213, FIG.206. "MAJOR REPAIR"

Part: SKIN — DELAMINATED (ZONE 500) · airframe 38,277 hrs · 21,141 cycles

LH WING #6 SPOILER L/E CTR SECTION DELAMINATED REMOVED L6 SPLR, REPAIRED THE DELAMINATION AREA, REINSTALLED, ADJUSTED, AND PFMED TEST OF L6 SPLR IAW A300-600 AMM 27-61-53-04 AND A300-600F SRM 57-72-11-201, PARA.12, PAGE.211-213, FIG.206. "MAJOR REPAIR"

Part: SEAT TRACK — UNKNOWN (ZONE 200) · airframe 38,277 hrs · 21,141 cycles

N00123 AGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 67~68, -Y1456 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA:A300-600F SRM 53-10-16-201,PARA.4, FIG.201,PAGE203~208,THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY A REPAIR. "MAJOR REPAIR"

Part: SEAT TRACK — UNKNOWN (ZONE 200) · airframe 38,277 hrs · 21,141 cycles

N00120 AGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 55~56, -Y953 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA:A300-600F SRM 53-10-16-201,PARA.4, FIG.201,PAGE203~208,THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY A REPAIR. "MAJOR REPAIR"

Part: SEAT TRACK — UNKNOWN (ZONE 200) · airframe 38,277 hrs · 21,141 cycles

N00119 AGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 31~32, -Y1456 FOUND THE EXISTING SPLICE REPAIR UPPER FLANGE NOT COMPLIANCE WITH APPROVED DATA: A300-600F SRM 53-10-16-201, FIG.201, REMOVED HILOKS AND PERFORMED ROTOTEST INSPECTION, CHECKED NO DISCREPANCY WAS NOTED, INSTALLED CORRECT FASTENER TYPE (RIVET) TO THE UPPER FLANGE POSITION I.A.W. A300-600F SRM 53-10-16-201, FIG.201, PAGE.203- 208. "MAJOR REPAIR"

Part: SEAT TRACK — UNKNOWN (ZONE 200) · airframe 38,277 hrs · 21,141 cycles

N00124 AGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 67~68, -Y450 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA:A300-600F SRM 53-10-16-201,PARA.4, FIG.201,PAGE203~208,THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY A REPAIR. "MAJOR REPAIR"

Part: SEAT TRACK — UNKNOWN (ZONE 200) · airframe 38,277 hrs · 21,141 cycles

N00121 AGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 62~63, -Y953 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA:A300-600F SRM 53-10-16-201,PARA.4, FIG.201,PAGE203~208,THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY A REPAIR. "MAJOR REPAIR"

Part: SEAT TRACK — UNKNOWN (ZONE 200) · airframe 38,277 hrs · 21,141 cycles

N00122 AGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 65~69, Y0 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA:A300-600F SRM 53-10-16-201,PARA.4, FIG.201,PAGE203~208,THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY A REPAIR. "MAJOR REPAIR"

Part: SEAT TRACK — UNKNOWN (ZONE 200) · airframe 38,277 hrs · 21,141 cycles

N00125 AGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 69~70, Y450 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA:A300-600F SRM 53-10-16-201,PARA.4, FIG.201,PAGE203~208,THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY A REPAIR. "MAJOR REPAIR"

Part: SLAT — UNKNOWN (ZONE 600) · airframe 38,277 hrs · 21,141 cycles

AGING AIRCRAFT ASSESSMENT : EXISTING FLUSH DOUBLER REPAIR FOUND ON RH WING #3 SLAT NOSE SKIN O/B END. DUE TO NO APPROVED DOCUMENTATION TO SUPPORT THE REPAIR, REMOVED ALL REPAIR PARTS AND PERFORMED NEW REPAIR TO THE AREA I.A.W. EA# T6-5750-T0373565 P1, TITLE: WINGS- FLIGHT SURFACES-RH #3 SLAT- OUTER SKIN REPAIR AT THE OUTBOARD LEADING EDGE, THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY A REPAIR. "MAJOR REPAIR"

Part: SKIN — NONE (ZONE 600) · airframe 38,277 hrs · 21,141 cycles

EXISTING FLUSH DOUBLER REPAIR FOUND ON RH WING #3 SLAT NOSE SKIN O/B END. DUE TO NO APPROVED DOCUMENTATION TO SUPPORT THE REPAIR, REMOVED ALL REPAIR PARTS AND PERFORMED NEW REPAIR TO THE AREA I.A.W. EA# T6-5750-T0373565 P1, TITLE: WINGS- FLIGHT SURFACES-RH #3 SLAT- OUTER SKIN REPAIR AT THE OUTBOARD LEADING EDGE, THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY A REPAIR."MAJOR REPAIR"

Part: SPOILER — DELAMINATED (ZONE 500) · airframe 38,277 hrs · 21,141 cycles

1EA DELAMINATION WAS FOUND (2" X 1") AT LH SPOILER NO.5 UPPER SKIN. REMOVED L5 SPLR, REPAIRED THE DELAMINATION AREA, REINSTALLED, ADJUSTED, AND PFMED TEST OF L5 SPLR IAW A300-600 AMM 27-61-53-04 AND A300-600F SRM 57-72-11-201, PARA.12, P.211~213, FIG.206. "MAJOR REPAIR"

Part: SKIN — DELAMINATED (ZONE 500) · airframe 38,277 hrs · 21,141 cycles

1EA DELAMINATION WAS FOUND (2" X 1") AT LH SPOILER NO.5 UPPER SKIN REMOVED L5 SPLR, REPAIRED THE DELAMINATION AREA, REINSTALLED, ADJUSTED, AND PFMED TEST OF L5 SPLR IAW A300-600 AMM 27-61-53-04 AND A300-600F SRM 57-72-11-201, PARA.12, P.211~213, FIG.206. "MAJOR REPAIR"

Part: AILERON — DAMAGED (ZONE 500) · airframe 38,277 hrs · 21,141 cycles

LH WING AILERON UPPER SKIN DEFORMED AT RIB1 & REAR SPAR-17" ACCOMPLISHED THE DOUBLER REPAIR, THIS IS CAT.A REPAIR I.A.W A300-600F SRM 57-61-11-201, PARA.4D, PAGE.213-PAGE.216, FIG.204 MAJOR REPAIR

Part: SKIN — DAMAGED (UNKNOWN) · airframe 38,277 hrs · 21,141 cycles

EVALUATE PREVIOUS DENT AT LHS FUSELAGE LWR SKIN FR10 6", 8 O'CLOCK. ACCOMPLISHED THECAT B DOUBLER REPAIR IAW A300-600F SRM 53-12-12-201, CONFIG 2, PAR. 5A, PAGE 203-208, FIG.201 & SRI 53-12-12-201, IR 53-12-12-2-006-00, PARA. 3F, TABLE 207 "MAJOR REPAIR".

Part: CONTROL MODULE — UNKNOWN (N/A) · airframe 37,417 hrs · 20,549 cycles

MDIS 651 26-10 5623 18APR22 IND OPEN U #1 ENGINE AGENT #2 SQUIB INOP SHGN 18APR22 15:25 IND U WHEN TESTING #1 ENG SQUIB, AGENT 2 SQUIB LIGHT IS NOT ILLUMINATING. SQUIB LIGHT ILLUMINATES W/ ANNUN LT TEST. PER A300-600 TSM 26-21-00, FIG 114, INSTALLED SERVICEABLE FIRE CONTROL MODULE 39WD, NO HELP. REINSTALLED ORIGINAL. DISCONNECTED CONNECTOR 25WE AND FOUND NO VOLTAGE BETWEEN PIN B AND GROUND, THEREFORE CANNOT PLACE ON MEL. REQUIRES FURTHER T/S. SHGN 18APR22 17:05 IND U REMOVED AND REPLACED RELAY13WE REF TSM 26-21-01 WITH NO HELP FURTHER TROUBLESHOOTING NEEDED PER A300 MM 26-12-20-04 REMOVED AND REPLACED #1 ENGINE FIRE CONTROL MODULE OPS CHECK GOOD ACFT OK TO CONTINUE.

Part: LIGHT — INOPERATIVE (N/A) · airframe 37,367 hrs · 20,514 cycles

MDIS 651 33-50 5547 18MAR22 LRD FACT U LAVATORY AUXILIARY MIRROW EMERGENCY LIGHT OUT. FACT 18MAR22 14:45 LRD U RELAMPED LAV AUX MIRROW EMERGENCY, IAW AMM 33-51-21-04, OPS CKS NORMAL AT THIS TIME.

Part: POWER SUPPLY — UNKNOWN (ZONE 100) · airframe 37,333 hrs · 20,484 cycles

SLIDE DID NOT DISPLAY ON ECAM WHEN ARMING RIGHT CABIN DOOR. RELEASED FOR SERVICE PER MEL : 52- XX-XX CATEGORY : C EXP: 25MAR22 - (R1) DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE." AUTONOMOUS STANDBY UNIT MPN: 3214-91 CPN: 5210609 QTY: 1 REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: AD-3214-30 POS: 2 SRL: 104117 TAG NBR: 3174F2. ON MPN: AD-3214-31 CPN: 3310373 SRL: 256491 TAG NBR: 6210H6 FACT 16MAR22 12:25 AMM: 52-73-00-05-01 ADJ AND TEST WORKED AT BLOCK IN IAW AMM. TEST OF POWER SUPPLY SHOWED BATTERY NUMBER 2 BAD R&R BATTERY IAW AMM 52-73-18-04 OPS CHECKS GOOD AT THIS TIME NO FURTHER FAULTS NOTED

Part: CONTROLLER — INOPERATIVE (LE FLAPS) · airframe 36,820 hrs · 20,128 cycles

AFTER T/O ON SLAT RETRACTION HAD KRUEGER FAULT. RAN APPROPRIATE CHECKLISTS AND RTB. PERFORMED BITE DISPLAY OF BOTH SFCC'S AND FOUND ALL OF THE FAULT BALLS FOR THE NR 1 UNIT LIGHT. THAT FAULT CODE CORRESPONDS WITH BAD SFCC REF AMM 27-80-00. IND INSPECTED THE LT AND RT KRUGER FLAPS AND SWITCHES, ALSO OPERATED KRUGER FLAPS THRU SEVERAL CYCLES AND THE OPERATION WAS NORMAL. REPLACED THE NR 1 SFCC AND NR 2 SFCC PER M/M 27-51-18-04, OPS TEST WAS GOOD. ALSO PERFORMED AN LLM TEST PER M/M 22-40-00-05, TEST WAS GOOD.

Part: ACTUATOR — FAILED (NLG DOOR) · airframe 35,709 hrs · 19,424 cycles

CREW REPORT: DURING MANUAL GEAR EXTENSION GOT LOUD NOISE AND EXCESSIVE VIBRATION ABOVE NORMAL LEVELS. WOULD NOT RECYCLE, REMOVED AND REPLACED NLG DOOR ACTUATOR LT SIDE. REMOVED AND REPLACED NOSE GEAR SEQUENCE VALVE. REMOVED AND REPLACED NON RETURN VALVE. PERFORMED FUNCTIONAL TEST FOR FREE FALL EXT, TEST IS OK IAW AMM 32-31-16-04, AMM032-31-18-04, AMM 20-23-12-00, AMM 32-33-00-05.

Part: PIN — MISSING (ESCAPE SLIDE) · airframe 35,707 hrs · 19,423 cycles

MISSING PASSENGER CREW DOOR 831 INFLATE RESERVOIR SAFETY PIN ESCAPE SLIDE RAFT AT FWD GALLEY AREA (1EA). REPLACED PASSENGER CREW DOOR 831 ESCAPE SLIDE RAFT IAW AMM 25-61-21-04 AT FWD GALLEY AREA.

Part: BOLT — CORRODED (SLAT TRACK) · corrosion level 2 · airframe 35,707 hrs · 19,423 cycles

CORROSION BOLT ATTACHMENT SLAT TRACK 7 UPPER POSITION ON LH WING (1 EA) REPLACED BOLT ATTACHMENT SLAT TRACK 7 UPPER POSITION ON LH WING IAW AMM 27-80-14- 04.

Part: BOLT — CORRODED (NR 7 SLAT TRACK) · corrosion level 2 · airframe 35,707 hrs · 19,423 cycles

ONE CORRODED BOLT ATTACHMENT ON SLAT TRACK NR 7 LOWER POSITION OF THE LT WING. REPLACED THE BOLT IAW AMM 27-80-14-04.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,707 hrs · 19,423 cycles

DELAMINATED FLOOR PANEL 242LK. REPAIRED THE FLOOR PANEL IAW DWG SRZ 25-005 REV. R.

Part: FLOOR PANEL — CRACKED (PAX CABIN) · airframe 35,707 hrs · 19,423 cycles

CRACK FLOOR PANEL 232VH THIS NON ROUTINE CARD IS FOR PURPOSE RDR GENERATION IN PASSENGER CABIN (1 EA) MANUFACTURED FLOOR PANEL 232VH AS PER DWG SRZ-25-005 REV. R AUG-22-2019. THIS NON ROUTINE CARD IS FOR PURPOSE RDR, SDR GENERATION. THIS JOB IS DOCUMENTED IN NON ROUTINE CARD N00371. FLOOR PANEL IDENTIFIED WITH P/N: A30 B5327048401400 FDX AUG-11- 2020 AS PER GMM 7-0-1000,

Part: FLOOR PANEL — CRACKED (BS 1764-1870) · airframe 35,707 hrs · 19,423 cycles

CRACK FLOOR PANEL 232VH. THIS NON ROUTINE CARD IS FOR PURPOSE RDR GENERATION IN PASSENGER CABIN (1 EA). MANUFACTURED FLOOR PANEL 232VH, AS PER DWG SRZ-25-005 REV. R AUG-22-2019. FLOOR PANEL MARKED WITH P/N FX B5327048401400 FDX AUG-11-2020, AS PER GMM 7-0-1001, FOR TRACEABILITY MATERIAL PO: 2020-161569/001.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 35,707 hrs · 19,423 cycles

CRACK FLOOR PANEL 232VH THIS NON ROUTINE CARD IS FOR PURPOSE RDR GENERATION IN PASSENGER CABIN (1 EA) MANUFACTURED FLOOR PANEL 232VH AS PER DWG SRZ-25-005 REV.R AUG-22-2019 AND FLOOR PANEL MARKED WITH P/N: FX B5327048401400 FDX AUG-11-2020 AS PER GMM 7-0-1001, FOR TRACIBILITY MATERIAL PO: 2020-161569/001.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 35,707 hrs · 19,423 cycles

DELAMINATED FLOOR PANEL 231NG ON MAIN DECK AFT CARGO COMPARTMENT THIS TASK CARD IS GENERATED FPR RDR PURPOSE IN PASSENGER CABIN (1 EA) THE REPAIR IS DOCUMENTED ON NON ROUTINE CARD N00543,

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 35,707 hrs · 19,423 cycles

DELAMINATED FLOOR PANEL 231UG ON MAIN DECK AFT CARGO COMPARTMENT THIS TASK CARD IS GENERATED FOR RDR PURPOSE IN PASSENGER CABIN (1 EA) THE REPAIR IS DOCUMENTED ON NON ROUTINE CARD N00343,

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 35,707 hrs · 19,423 cycles

DELAMINATED TOP LAYER FLOOR PANEL (MAIN DECK) 241EF IN PASSENGER CABIN (1 EA) REPAIRED FLOOR PANEL 241EF ON MAIN DECK ASPER A300 SRM 53-10-20 PAGEBLOCK 201 PARA B TOOL USED CALIPER PN 500-197-30 S/N A18135089 DUE DATE JUL-11-2021 SCALE PN CL5000 S/N AE-39882 DUE DATE NOV-05-2020 MICROBONDER PN HCS8800 SN 01154420 DUE DATE AUG-09-2020

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 35,707 hrs · 19,423 cycles

DELAMINATED FLOOR PANEL 231ZG ON MAIN DECK AFT CARGO COMPARTMENT THIS TASK CARD IS GENERATED FOR RDR PURPOSE IN PASSENGER CABIN (1 EA) THE REPAIR IS DOCUMENTED ON NON ROUTINE CARD N00343, THIS SNRM, (N00653) IS GENERATED RDR PURPOSE

Part: BOLT — CORRODED (RT SLAT TRACK) · airframe 35,707 hrs · 19,423 cycles

CORROSION BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING REPLACED BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING IAW AMM 27- 80-12-04

Part: BOLT — CORRODED (LT WING STAT) · airframe 35,707 hrs · 19,423 cycles

CORROSION SLAT 2 SCREWJACK 4 BOLT ON LH WING REPLACED SLAT 2 SCREWJACK BOLT ON LH WING IAW AMM 27-84-22-04 STEP 2.D(5)(A)

Part: BOLT — CORRODED (RT SLAT TRACK) · airframe 35,707 hrs · 19,423 cycles

CORROSION BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING REPLACED BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING IAW AMM 27- 80-12-04

Part: BOLT — CORRODED (RT SLAT TRACK) · airframe 35,707 hrs · 19,423 cycles

CORROSION BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING REPLACED BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING IAW AMM 27- 80-12-04

Part: BOLT — CORRODED (RT WING) · airframe 35,707 hrs · 19,423 cycles

CORROSION BOLT ATTACHMENT SLAT TRACK 8 ECCENTRIC BOLT ON RT WING. REPLACED BOLT ATTACHMENT SLAT TRACK 8 ECCENTRIC BOLT ON RY WING IAW AMM 27-80-14-04.

Part: BOLT — CORRODED (RT SLAT TRACK) · airframe 35,707 hrs · 19,423 cycles

CORROSION BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING REPLACED BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING IAW AMM 27- 80-12-04

Part: BOLT — CORRODED (LT SLAT TRACK) · airframe 35,707 hrs · 19,423 cycles

CORROSION BOLT ATTACHMENT SLAT TRACK 1 FWD UPPER POSITION ON LH WING REPLACED BOLT ATTACHMENT SLAT TRACK 1 FWD UPPER POSITION ON LH WING IAW AMM 27- 80-11-04

Part: FAILSAFE — CORRODED (LT SLAT TRACK) · airframe 35,707 hrs · 19,423 cycles

CORROSION BOLT ATTACHMENT SLAT TRACK 8 FWD LOWER POSITION ON LH WING REPLACED BOLT ATTACHMENT SLAT TRACK 8 FWD LOWE POSITION ON LH WING (1E/A) IAW AMM 27-80-12-04

Part: BOLT — CORRODED (RT SLAT TRACK) · airframe 35,707 hrs · 19,423 cycles

CORROSION BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING REPLACED BOLT ATTACHMENT SLAT TRACK 11 FWD LOWER POSITION ON RH WING IAW AMM 27- 80-12-04

Part: BOLT — CORRODED (RT WING) · airframe 35,707 hrs · 19,423 cycles

CORROSION BOLT ON SCREWJACK 2 FWD POSITION ON RH WING (1 EA) REPLACED BOLT ON SCREWJACK 2 FWD POSITION ON RH WING (1E/A) IAW AMM 27-84-22-04 STEP 2.D(5) LOCATION OF THE SCREWJACK 2 IS BETWEEN WING RIB 5 AND 6 IAW AMM 06-31-57- 00

Part: SPAR — CRACKED (CENTER FUEL TANK) · airframe 35,707 hrs · 19,423 cycles

CRACK INDICATION FOUND ON HOLE C ON REAR SPAR AND BOTTOM PANEL JUNCTION AREA RT SIDE AT CENTER FUEL TANK, CRACK DIRECTION IS 12 O'CLOCK, 1 E/A. ACCOMPLISHED REPAIR ON REAR SPAR AND BOTTOM PANEL JUNCTION AREA RT SIDE AT CENTER FUEL TANK, IAW EA NR 6-5710-T0355600 AND RDAS NR 70577882/042/2020. THIS REPAIR IS CAT B. FOR REQUIREMENTS INSPECTION SEE RDAS NR 70577882/042/2020.

Part: BRACKET — CRACKED (BS 1552-1605) · airframe 35,707 hrs · 19,423 cycles

MACHINE BRACKETS (2E/A) ITEM 4, IAW EA NR 6-5313-T0355604 P1 STEP 10 FIGURE 2. MACHINED BRACKETS (2E/A) ITEM 4, AS PER EA NR 6-5313-T0355404 P1 STEP 10, FIG 2 AND DWG 13A53774203.

Part: RIB — GOUGED (RT WING) · airframe 35,707 hrs · 19,423 cycles

WEAR RIB LOCATED AT OUTER WING REAR SPAR WI AX 21.90 BETWEEN RIB 6A AND RIB 7A ON RT WING (1 EA). PERFORMED PERMANENT REPAIR ON RIB LOCATED AT OUTER WING REAR SPAR WI AX 21.90 BETWEEN RIB 6A AND RIB 7A ON RT WING (1EA), IAW EA NR 6-5710-T0355668 P1 EA; TITLE: WING ATTACH FITTING RT WING TRAINING EDGE INTERMEDIATE RIB BETWEEN RIB 6A AND RIB 7A. GOUGE REPAIR.

Part: FRAME — GOUGED (FRM 73) · airframe 35,707 hrs · 19,423 cycles

GOUGE FRAME 73 RH AT LEVEL STR 21R ON UPPER FUSELAGE

Part: FRAME — GOUGED (FRM 73) · airframe 35,707 hrs · 19,423 cycles

GOUGE FRAME 73 RT AT LEVEL STR 21 ON UPPER FUSELAGE REPAIRED FRAME 73 RT AT LEVEL STR 21 ON UPPER FUSELAGE, IAW A300-600 SRM 53-10-13 PAR 5C FIG 202. THIS MUST BE INSPECTED AT DEFINED INTERVALS. THE INSPECTION INSTRUCTION REFERENCE IS 53-10-13-2-002-00 TABLE 202.

Part: MOUNT — CORRODED (RT NACELLE) · corrosion level 2 · airframe 35,707 hrs · 19,423 cycles

CORROSION FORWARD MOUNT RIB 1 ATTACHED FITTING (PYRAMID) ON RH PYLON PERFORMED REPAIR LOC. ON BASE PLATE AND 3EA HOLES OF THE BOLTS OF FWD MOUNT RIB 1 ATTACHED FITTING PYRAMID ON RH PYLON IAW EA NO T6-5450-167628 B P3, #2 PYLON FWD ENG MOUNT FITTING CORROSION REPAIR AND A300-600 SRM 54-51-81 CONFIG 2 PAR 5B. RECHECK REQUIRED FOR 2EA FRONT HOLES OF THE BOLTS I/B AND O/B POSITION SEE SNRM N00695 AND 1EA REAR HOLE OF THE BOLT I/B POSITION SEE SNRM N00704

Part: STRUCTURE — CRACKED (RUDDER) · airframe 35,707 hrs · 19,423 cycles

BROKEN RUDDER UPPER HOIST POINT AT LEVEL RIB 13 LH SIDE ON VERTICAL STABILIZER REPAIRED RUDDER HOIST POINT AT LEVEL RIB 13 LH SIDE ON VERTICAL STABILIZER AS PER A300 SRM 55-41-12 P.B. 201 PARA. 26. THIS REPAIR IS APPLICABLE TO THE INSPECTION PROGRAM DEFINED IN SRI AND FIRST INSPECTION AFTER REPAIR EMBODIMENT AT 42,500 FC AS PER SRI 55-41-12-2-009-00 TABLE 210; SUBSEQUENT INSPECTION AND INSPECTION METHOD TBD AND I.A.W EA # 6-5540-T0355297

Part: MOUNT — CORRODED (LT NACELLE) · corrosion level 2 · airframe 35,707 hrs · 19,423 cycles

CORROSION ENGINE MOUNT FWD PYRAMID ON LH PYLON PERFORMED REPAIR LOC ON BASE PLATE AND (2E/A) HOLES OF THE BOLTS OF FORWARD MOUNT RIB 1 ATTACHED FITTING PYRAMID ON LH PYLON IAW EA N. T6-5450-T0355859 P1, #1 ENGINELH FORWARD MOUNT BASE PLATE CORROSION REPAIR AND A300-600 SRM 54-51-81 CONFIG-2 PARAGRAPH 5B. RECHECK REQUIRED FOR (1E/A) FRONT HOLE OF BOLT INBOARD POSITION SEE SNRM N00694 AND (1E/A) REAR HOLE OF BOLT INBOARD POSITION SEE SNRM N00705

Part: BEAM — CRACKED (RT WING) · airframe 35,707 hrs · 19,423 cycles

CRACK TRAILING EDGE IN OVERWING PANEL BEAM 5 ON RT WING. PERFORMED PERMANENT REPAIR LOC. TRAILING EDGE IN OVERWING PANEL BEAM 5 ON RT WING, IAW EA 6-5720-T0355567 A WING. SECONDARY STRUCTURES TRAILING EDGE STRUCTURES OVER MLG BAY, INBOARD SHROUD, CRACK, PERMANENT REPAIR.

Part: FRAME — GOUGED (FRM 54) · airframe 35,707 hrs · 19,423 cycles

GOUGE FRAME FR-54 BETWEEN STR-12 LT TO 13 LT SIDE ON AFT FACE IN PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON FRAME 54 BETWEEN STR 12 LT TO 13 LT SIDE ON AFT FACE IN PASSENGER CABIN, IAW EA 6-5310-T0355414 A P1 EA TITTLE: FUSELAGE-MAINFRAME-MAIN DECK CARGO COMPARTMENT - CHAFE/WORN DAMAGE COMMON TO LH FRAME 54 BETWEEN STR-12 AND STR-13. PERMANENT REPAIR.

Part: ROLLER TRACK — CORRODED (FRAMES 32-38) · corrosion level 2 · airframe 35,707 hrs · 19,423 cycles

CORRODED ROLLER TRACK ASSY BETWEEN FRAMES 32 & 38.2, -Y450 TO -Y953 IN THE FWD CARGO COMPARTMENT. REPLACED THE ROLLER TRACK ASSY IAW SRM 51-72-10, AND DRAWING A25774009.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 35,707 hrs · 19,423 cycles

PUNCTURE ON FLOOR PANEL 212HF IN COCKPIT. REPAIRED FLOOR PANEL 212HF IN COCKPIT AS PER DRAWING SR30-53-005

Part: FRAME — CRACKED (FRM 26) · airframe 35,707 hrs · 19,423 cycles

CRACK FRAME 26 BETWEEN STRINGERS 13R TO 14R IN PASSENGER CABIN. REPLACED THE SECTION OF FRAME IAW DRAWING A53777450, SRM 51-40-21, AND SRM 51-72-10.

Part: FRAME — GOUGED (FRAME 31) · airframe 35,707 hrs · 19,423 cycles

GOUGE FRAME 31 AT LEVEL STR-17 LH SIDE ON AFT FACE INBOARD FLANGE IN PASSENGER CABIN REPAIRED FRAME 31 AT LEVEL STR 17 LH SIDE ON AFT FACE INBOARD FLANGE IN PASSENGER CABIN IAW SRM A300-600 53-10-13-201 THIS REPAIR MUST BE INSPECTED AT DEFINED INTERVALS THE INSPECTION INSTRUCTIONS REFERENCE IS 53-10-13-2-001-00

Part: ROLLER TRACK — CORRODED (FWD CARGO BAY) · corrosion level 2 · airframe 35,707 hrs · 19,423 cycles

CORROSION ROLLER TRACK ASSY BETWEEN FRAMES 32 TO 38.2, Y450 TO Y953 IN THE FWD CARGO COMPARTMENT. REPLACED THE ROLLER TRACK ASSY IAW SRM 51-72-10, AND DRAWING A25771363.

Part: FRAME — CRACKED (FRM 26) · airframe 35,707 hrs · 19,423 cycles

CRACKED FRAME 26, BETWEEN STRINGERS 13R TO 14R. REPLACED THE SECTION OF FRAME IAW DRAWING A53777450, SRM 51-40-21, AND SRM 51-72-10.

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 35,707 hrs · 19,423 cycles

CRACK FLOOR PANEL 252DH ZONA 250 IN AFT CARGO COMPARTMENT (1 EA) MANUFACTURED FLOOR PANEL 252DH AS PER DWG SRZ-25-005 REV. R

Part: ROLLER TRACK — CORRODED (FWD CARGO) · corrosion level 2 · airframe 35,707 hrs · 19,423 cycles

CORROSION ROLLER TRACK ASSY LOC. AT FR37 AND BTW Y0 TO -Y453 IN FWD CARGO COMPARTMENT REPLACED ROLLER TRACK ASSY IN FWD CARGO IAW SRM 51-72-10 AND DRAWING A25774009.

Part: FLOOR PANEL — DELAMINATED (E/E BAY) · airframe 35,707 hrs · 19,423 cycles

DELAMINATED PANEL 122DF IN FWD AVIONIC COMPARTMENT MANUFACTURED FLOOR PANEL 122DF IN FWD AVIONIC COMPARTMENT AS PER DWG SRZ-25- 005 REV. R AUG-22-2019. MARKED NEW FLOOR PANEL WITH P/N: A30 A5321024400000 FDX AUG- 11-2020 AS PER GMM 7-0-1000 FOR TRACIBILITY MATERIAL PO: 2020-161569/001

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 35,707 hrs · 19,423 cycles

CRACKED FLOOR PANEL 252DH ZONA 250 IN AFT CARGO COMPARTMENT (1 EA). MANUFACTURED FLOOR PANEL 252DH ZONE 250 IN AFT CARGO COMPARTMENT, AS PER DWG NO. SRZ-25-005 REV. R AUG-22-2019. MARKED NEW FLOOR PANEL WITH P/N: FX B5327036100600 FDX AUG-11-2020, AS PER GMM 7-0-1001, FOR TRACEABILITY MATERIAL P/O IS 2020-161569/001. TOOL USED CALIPER P/N:500-197-30 S/N:15242824 DUE DATE APR-21-2021.

Part: FLOOR PANEL — DELAMINATED (FWD E/E BAY) · airframe 35,707 hrs · 19,423 cycles

DELAMINATED PANEL 122DF IN FWD AVIONIC COMPARTMENT MANUFACTURED FLOOR PANEL 122DF IN FWD AVIONIC COMPARTMENT AS PER DWG NO. SRZ- 25-005. REV R. AUG-22-2019 MARKED NEW FLOOR PANEL WITH P/N FX A5321024400000FDX AUG- 11-2020. AS PER GMM 7-0-1001. FOR TRACIBILITY MATERIAL P/O IS 2020-161569/001 TOOL USED CALIPER P/N:500-197-30 S/N:15242824 DUE DATE APR-21-2021

Part: FRAME — GOUGED (FRM 31) · airframe 35,707 hrs · 19,423 cycles

GOUGE FRAME 31 AT LEVEL STR-17 LT SIDE ON AFT FACE INBOARD FLANGE IN PASSENGER CABIN. REPAIRED FRAME 31 AT LEVEL STR 17 LT SIDE ON AFT FACE INBOARD FLANGE IN PASSENGER CABIN, IAW SRM A300-600 53-10-13-201 PARA 5.C. THIS REPAIR MUST BE INSPECTED AT DEFINED INTERVALS. THE INSPECTION INSTRUCTIONS REFERENCE IS SRI 53-10-13-2-002-00 TABLE 203.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 35,707 hrs · 19,423 cycles

DELAMINATED PANEL 121TF IN FWD AVIONIC COMPARTMENT. REPAIRED PANEL 121TF IN FWD AVIONIC COMPARTMENT, AS PER DRAWING SRZ-25-005 REV R.

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 35,707 hrs · 19,423 cycles

CRACK FLOOR PANEL 252DH ZONA 250 IN AFT CARGO COMPARTMENT (1 EA) MANUFACTURED FLOOR PANEL 252DH AS PER DWG SRZ-25-005 REV. R AUG-22-2019. MARKED NEW FLOOR PANEL WITH P/N: A30 B5327036100600 FDX AUG-11-2020 AS PER GMM 7-0-1000, FOR TRACIBILITY MATERIAL PO: 2020-161569/001.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 35,707 hrs · 19,423 cycles

DELAMINATED FLOOR PANEL MAIN DECK AFT CARGO COMPARTMENT 231TG, 231UG,23 1NG,231ZG,232VH,232FG IN PAX CABIN (6 EA). REPAIRED FLOOR PANEL MAIN DECK AFT CARGO COMPARTMENT 231UG, 231TG, 231NG, 231ZG IN PASSENGER CABIN AS PER A300 SRM 53-10-20 PAGE BLOCK 201 PARA 3 AND IRM 9701 REV I. THE REPAIR PROCESS OF FLOOR PANEL 232FG AND 323VH WILL BE DOCUMENTED ON NON ROUTINE CARD: N00371. THE RDR TO FLOOR PANEL 231UG WAS GENERATED ON SNMR N00651. THE RDR TO FLOOR PANEL 231NG WAS GENERATED ON SNMR N00652. THE RDR TO FLOOR PANEL PANEL 231ZG WAS GENERATED ON SNMR N00653. THE RDR TO FLOOR PANEL 231TG WAS GENERATED ON THIS SNMR (N00343).

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 35,707 hrs · 19,423 cycles

CRACK FLOOR PANEL 252BH (MAIN DECK) IN PASSENGER CABIN (1 EA) MANUFACTURED FLOOR PANEL 252BH IN PASSENGER CABIN ASPER DWG NO. SRZ-25-005. REV R. AUG-22-2019, MARKED NEW FLOOR PANEL WITH P/N FX B5327028700100FDX AUG-11-2020 ASPER GMM 7-0-1001 FOR TRACIBILITY MATERIAL P/O: IS 2020-161569/001 TOOL USED CALIPER P/N:500-197-30 S/N:15242824 DUE DATE APR-21-2021.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 35,707 hrs · 19,423 cycles

CRACK FLOOR PANEL 232FG (MAIN DECK) IN PASSENGER CABIN (1 EA) MANUFACTURED FLOOR PANEL 232FG AS PER DRAWING SRZ 25-005 REV R.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 35,707 hrs · 19,423 cycles

CRACK FLOOR PANEL 232FG (MAIN DECK) IN PASSENGER CABIN MANUFACTURED FLOOR PANEL 232FG IN PASSENGER CABIN AS PER DWG SRZ-25-005 REV.R AUG-22-2019, MARKED FLOOR PANEL 232FG WITH P/N: FX B5327046000000 FDX DATE: AUG-11- 2020 AS PER GMM 7-0-1001, FOR TRACIBILITY MATERIAL PO: 2020-161569/001

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 35,707 hrs · 19,423 cycles

CRACK FLOOR PANEL 252BH (MAIN DECK) IN PASSENGER CABIN (1 EA) MANUFACTURED FLOOR PANEL 252BH AS PER DWG SRZ-25-005 REV. R,

Part: FLOOR PANEL — CRACKED (MAIN DECK) · airframe 35,707 hrs · 19,423 cycles

CRACK FLOOR PANEL 242GF (MAIN DECK) IN PASSENGER CABIN (1 EA) MANUFACTURED FLOOR PANEL 242GF AS PER DWG SRZ 25-005 REV. R AUG-22-2019. THIS JOB IS DOCUMENTED ON NON ROUTINE CARD N00346, FLOOR PANEL IDENTIFIED WITH P/N: A30 B5327048001700 FDX AUG-11-2020 AS PER GMM 7-0-1000, FOR TRACIBILITY MATERIAL PO: 2020- 161569/001. THIS NON ROUTINE CARD IS FOR RDR AND SDR GENERATION.

Part: FLOOR PANEL — CRACKED (PAX CABIN) · airframe 35,707 hrs · 19,423 cycles

CRACK FLOOR PANEL PLATE 242SF IN PASSENGER CABIN (1EA) MANUFACTURED FLOOR PANEL 242SF AS PER DWG SRZ 25-005 REV. R.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 35,707 hrs · 19,423 cycles

CRACK FLOOR PANEL PLATE 242SF IN PASSENGER CABIN (1EA) MANUFACTURED FLOOR PANEL 242SF IN PASSENGER CABIN AS PER DWG NO. SRZ-25-005 REV.R AUG-22-2019, MARKED NEW FLOOR PANEL WITH P/N: FX B5327061802100FDX AUG-11- 2020 AS PER GMM 7-0-1001, FOR TRACIBILITY MATERIAL P/O IS 2020-161569/001 TOOL USED CALIPER P/N: 500-197-30 S/N:15242824 DUE DATE APR-21-2021

Part: FLOOR SUPPORT — CORRODED (FRAMES 11-13) · airframe 35,707 hrs · 19,423 cycles

CORROSION SUPPORT FLOOR LOCATED BETWEEN FR 11 TO FR 13 AND BETWEEN Y450 TO Y953 AT FWD GALLEY AREA. REPLACED SUPPORT FLOOR LOCATED BETWEEN FR11 TO FR13 BETWEEN Y450 TO Y953, IAW A300-600 SRM 51- 72-10 AND DWG A53612214 MEASURES OF DAMAGE L=4.699", W=1.697".

Part: WEB — CRACKED (FRAME 47) · airframe 35,707 hrs · 19,423 cycles

CRACK ON WEB LOCATED AT FRAME 47, Y1203, HORIZONTAL PRESSURE DECK AREA LT SIDE PERFORMED PERMANENT REPAIR LOC. ON WEB IAW SRM 53-15-15, FIG 201, SHEET 2.

Part: SKIN — DELAMINATED (RUDDER) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON RUDDER LT SIDE PANEL HONEYCOMB CORE CELLS. LOCATED AROUND THE TRAILING EDGE FASTENER 31 ON VERTICAL STABILIZER (1EA) (L=4.5INCH W=3 INCH). REPAIRED RUDDER LT SIDE PANEL HONEYCOMB CORE CELLS LOCATED AROUND THE TRAILING EDGE FASTENER 31 ON VERTICAL STABILIZER, AS PER A300 SRM 55-41-12 PB 201 PAR 23. THIS INSPECTION IS APPLICABLE TO THE INSPECTION PROGRAM DEFINED IN SRI AND FIRST INSPECTION AFTER REPAIR EMBODIMENT AT 42500 FC AS PER SRI 55-41-12-2-006-00 TABLE 207. SUBSEQUENT INSPECTION AND INSPECTION METHOD TBD AND IAW EA 6-5540-T0355297.

Part: WEB — CRACKED (FRAME 47) · airframe 35,707 hrs · 19,423 cycles

CRACK ON WEB LOCATED FRAME 47 -Y225 HORIZONTAL PRESSURE DECK RH SIDE PERFORMED REPAIR ON WEB LOCATED FRAME 47 -Y225 HORIZONTAL PRESSURE DECK RH SIDE IAW A300-600 SRM 53-15-15 FIG 201. INSPECTION THRESHOLD FROM REPAIR EMBODIMENT AT 24000 FC/FH NOT RELEVANT, SUBSEQUENT INSPECTION AT INTERVALS OF 3000 FC/FH NOT RELEVANT, INSPECTION METHOD DVI IAW SRI 53-15-15-2-002-00 PAR. 3B TABLE 203

Part: WEB — CRACKED (FRAME 43) · airframe 35,707 hrs · 19,423 cycles

CRACKED WEB LOCATED FRAME 43 -Y1203 HORIZONTAL PRESSURE DECK RH SIDE PERFORMED PERMANENT REPAIR EXACTLY LOCATION ON WEB ON FR 47 ON -Y1203 HORIZONTAL PRESSURE DECK AREA RH SIDE IAW SRM 53-15-15, FIG 201, SHEET 2 .

Part: WEB — CRACKED (FRAME 47) · airframe 35,707 hrs · 19,423 cycles

CRACK ON WEB LOCATED FRAME 47 Y225 HORIZONTAL STABILIZER PRESSURE DECK L/H SIDE PERFORMED PERMANENT REPAIR ON WEB LOCATED FR 47 AND Y225 HORIZONTAL PRESSURE DECK LH SIDE AS PER A300-600 SRM 53-15-15 FIGURE 201 (SHEET 2). FOR INSPECTION THRESHOLD FROM REPAIR EMBODIMENT 24000 FC/FH NOT RELEVANT, SUBSEQUENT INSPECTION AT INTERVAL OF 3000 FC/FH NOT RELEVANT, INSPECTION METHOD DETAIL VISUAL AS PER SRI 53-15-15-2-002-00 TABLE 203

Part: SKIN — DELAMINATED (RUDDER) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON RUDDER LH SIDE PANEL HONEYCOMB CORE CELLS. LOCATED AROUND THE TRAILING EDGE FASTENER N. 31 ON VERTICAL STABILIZER (1EA) (L=4.5INCH W=3 INCH) REPAIRED RUDDER LH SIDE PANEL HONEYCOMB CORE CELLS LOCATED AROUND THE TRAILING EDGE FASTENER 31 ON VERTICAL STABILIZER AS PER A300 SRM 55-41-12 PB 201 PAR 23. THIS INSPECTION IS APPLICABLE TO THE INSPECTION PROGRAM DEFINED IN SRI AND FIRST INSPECTION AFTER REPAIR EMBODIMENT AT 42500 FC AS PER SRI 55-41-12-2-006-00 TABLE 207 SUBSEQUENT INSPECTION AND INSPECTION METHOD TBD AND IAW EA 6-5540-T0355297

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 35,707 hrs · 19,423 cycles

DEBONDED ACCESS PANEL 121CF IN FWD AVIONIC COMPARTMENT. MANUFACTURED ACCESS PANEL 121CF IN FWD AVIONIC COMPARTMENT, AS PER DWG NO. SRZ-25-005 REV. R. AUG-22-2019. MARKED NEW ACCESS PANEL WITH P/N: FX A5321024200000 FDX AUG-11-2020, AS PER GMM 7-0-1001 FOR TRACEABILITY MATERIAL P/O IS 2020-161569/001. TOOL USED CALIPER P/N:500-197-30 S/N:15242824 DUE DATE APR-21-2021. MAJOR REPAIR.

Part: FRAME — DAMAGED (FRM 54) · airframe 35,707 hrs · 19,423 cycles

WEAR ON FRAME 54 AT LEVEL STR 16 RT SIDE ON UPPER FUSELAGE. PERFORMED PERMANENT REPAIR ON FRAME 54 AT LEVEL STR 16 RT SIDE ON UPPER FUSELAGE, IAW EA 6-5310-T0355376 P1 EA TITLE: FUSELAGE - MAINFRAME - MAIN DECK CARGO COMPARTMENT - CHAFE/WORN DAMAGE COMMON TO RT FRAME 54 BETWEEN STR-15 AND STR- 16. PERMANENT REPAIR.

Part: ACCESS PANEL — DEBONDED (E/E BAY) · airframe 35,707 hrs · 19,423 cycles

DEBONDED ACCESS PANEL 121CF IN FWD AVIONIC COMPARTMENT MANUFACTURED ACCESS PANEL 121CF AS PER DWG SRZ 25-005 REV. R

Part: FLOOR PANEL — DELAMINATED (E/E BAY) · airframe 35,707 hrs · 19,423 cycles

DEBONDED ACCESS PANEL 121CF IN FWD AVIONIC COMPARTMENT MANUFACTURED ACCESS PANEL 121CF AS PER DWG SRZ 25-005 REV. R AUG-22-2019. MARKED NEW ACCESS PANEL WITH P/N: A30 A5321024200000 FDX AUG-11-2020 AS PER GMM 7-0-1000 FOR TRACIBILITY MATERIAL, PO: 2020-161569/001.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 35,707 hrs · 19,423 cycles

IMPROPERLY ACCESS PANEL 121PF DUE TO MISSING INSERT IN FWD AVIONIC COMPARTMENT (1EA) INSTALLED NEW INSERT 1 EA ON FLOOR PANEL 121PF IN FWD AVIONIC COMPARTMENT ASPER DWG NO SRZ-25-005 REV. R AUG/22/2019 ITEM 8 TO15

Part: WEB — CRACKED (FRAME 47) · airframe 35,707 hrs · 19,423 cycles

CRACK ON WEB LOCATED FRAME 47 -Y1203 HORIZONTAL PRESSURE DECK RH SIDE PERFORMED PERMANENT REPAIR EXACTLY LOCATION ON WEB ON FR47 ON -Y1203 HORIZONTAL PRESSURE DECK AREA RH SIDE IAW A300-600 SRM 53-15-15, FIG 201-C2 (SHEET 2) RECHECK REQUIRED INSPECTION THRESHOLD FROM REPAIR EMBODIMENT 24000FC/FH NOT RELEVANT, SUBSEQUENT INSPECTION AT INTERVALS OF 3000 FC/FH NOT RELEVANT INSPECTION METHOD DETAILED VISUAL INSPECTION IAW A300-600 SRI 53-15-15-2-002-00 TABLE 203

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 35,707 hrs · 19,423 cycles

IMPROPERLY ACCESS PANEL 121YF DUE TO MISSING INSERT IN FWD AVIONIC COMPARTMENT (1EA) INSTALLED NEW INSERT 1 EA ON FLOOR PANEL 121YF IN FWD AVIONIC COMPARTMENT ASPER DWG NO SRZ-25-005 REV . R AUG/22/2019 ITEM 8 TO 15

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 9 INCH INBOARD FROM RIB 5 AND 13 INCH FROM TRALING EDGE. ADDITIONALLY, A DISBONDED AREA WAS FOUND WITHIN THIS SPOT, ON LT HORIZONTAL STABILIZER (1 EA) (L=3 INCH. W=2.3 INCH.). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEY COMB CORE CELL LOCATED AT 9.5 INCH FROM ERIB 5 AND 12.5 INCH FROM T/E ON LT HORIZONTAL STABILIZER, AS PER SRM A300 55-21-12 PAGE BLOCK 201 PARAGRAPH 5.J. EXACT LOCATION IS BETWEEN STA 274 AND STA 327, AS PER AMM 06-31-55-00 AND EA 6-5520-T0355929 (P1). THIS REPAIR IS CAT A.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON THE LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 27 INCHES OUTBOARD FROM RIB 13 AND 26 INCHED FROM TRAILING EDGE. REPAIRED THE LT ELEVATOR UPPER SKIN PANEL IAW SRM 55-21-12, PAGE BLOCK 201, PARAGRAPH 5.J.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 9 INCH OUTBOARD FROM RIB 7 AND 25 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=4.5 INCH. W=4 INCH). REPAIRED ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELL AT LEVEL 9'' FROM O/B ERIB 7 AND 24.5'' FROM T/E ON HORIZONTAL STABILIZER LT AS PER A300 SRM 55-21-12 PB 201 PARA 5 B. THIS REPAIR IS APPLICABLE TO THE INSPECTION PROGRAM DEFINED IN SRI AND FIRST INSPECTION AFTER A/C FIRST FLIGHT AT 42500FC/89000FH, AS PER SRI 55-21-12-2-001-00 TABLE 202. SUBSEQUENT INSPECTION AND INSPECTION METHOD TBD AND EA 6-5520-T0355929 (P1). THIS REPAIR IS CAT-B AND TRACKING IS ON EA.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON THE LEFT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE C ELLS. LOCATED AT 6 INCH. INBOARD FROM RIB 10 AND 15.5 INCH. FROM TRAILING EDGE. REPAIRED THE ELEVATOR UPPER SKIN IAW SRM 55-21-12, PB 201, PARA 5.B.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 4 INCH OUTBOARD FROM RIB 16 AND 17 INCH FROM TRAILING EDGE ON LT HORIZ STAB (1EA) (L=2 INCH. W=1.75 INCH). DUE TO THE DISTANCE BETWEEN DAMAGE AREA REPORTED ON NON ROUTINE CARD N00151, N00153, AND N00154 IS LESS THAN THE MINIMUM DISTANCE. THIS DAMAGE MUST BE ENVELOPED TOGETHER AND THE AREA MUST BE CONSIDERED AS ONE DAMAGE AREA. THE TOTAL AREA OF ENVELOPE TOGETHER IS: 18.49 SQ INCH AND EVALUATED AREA AND FOUND WITHIN LIMITS TO REPAIR, AS PER A300 SRM 55-20-00 PAGE BLOCK 101 PAR 8 FIG 104. THIS SDR IS DUPLICATED, REFER TO SDR 20-1806 ON NON ROUTINE CARD N00153 AND WORK WAS DOCUMENTED ON NON ROUTINE CARD N00153 AND EA 6-5520-T0355929 (P1). THIS REPAIR IS CAT-A.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON THE LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED 9 INCHES INBOARD FROM RIB 5 AND 13 INCHES FROM TRALING EDGE. REPAIRED THE SKIN IAW SRM 55-21-12, PAGE BLOCK 201, PARAGRAPH 5.J.

Part: FLOOR SUPPORT — CORRODED (FRAMES 14-16A) · airframe 35,707 hrs · 19,423 cycles

CORROSION FLOOR STRUCTURE Y1959 LOC. BTW FR14 TO FR16A AT FWD GALLEY AREA REPLACED FLOOR BEAM Y1959 AND FASTENERS LOC BTW FR14 TO FR16 AT FWD GALLEY AREA IAW SRM 51-73-10, 51-40-21 AND DWG A53612311 ISSUE M,

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON THE LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED 27 INCHES OUTBOARD FROM RIB 13, AND 7 INCHES FROM TRAILING EDGE. REPAIRED THE LT ELEVATOR UPPER SKIN IAW SRM 55-21-12, PAGE BLOCK 201, PARAGRAPH 5.J.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 8 INCH OUTBOARD FROM RIB 16 AND 8 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=2 INCH. W=1.8 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEY COMB CORE CELL LOCATED BETWEEN ERIB 16 AND ERIB 17 AT 7.9 INCHES FROM ERIB 16 AND 7.25 INCHES FROM T/E ON LT HORIZONTAL STABILIZER, AS PER A300 SRM 55-21-12 PAGE BLOCK 201 PARAGRAPH 5.J. EXACT LOCATION IS STATION 757 AND STATION 833, AS PER AMM 06-31-55-00 AND EA 6-5520-T0355929 (P1). THIS REPAIR IS CAT-A.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. 10 INCHED INBOARD FROM RIB 16 AND 15 INCHES FROM TRAILING EDGE. REPAIRED THE ELEVATOR UPPER SKIN IAW SRM 55-21-12, PAGE BLOCK 201, PARAGRAPH 5.J.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. 8 INCHED OUTBOARD FROM RIB 16 AND 8 INCHED FROM TRAILING EDGE. REPAIRED THE LT ELEVATOR UPPER SKIN IAW SRM 55-21-12, BLOCK 201, PARAGRAPH 5.J.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON LEFT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 19 INCH. INBOARD FROM RIB 16 AND 9 INCH. FROM TRAILING EDGE. REPAIRED THE ELEVATOR UPPER SKIN IAW SRM 55-21-12 PB 201 PARA. 5.B .

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED ONE INCH INBOARD FROM RIB 13 AND 14 INCHES FROM TRAILING EDGE. REPAIRED THE LT ELEVATOR UPPER SKIN IAW SRM 55-21-12, PAGE BLOCK 201, PARAGRAPH 5.J.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 20 INCH OUTBOARD FROM RIB 13 AND 18 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=2.5 INCH. W=2 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEY COMB CORE CELL LOCATED AT 19 INCH FROM O/B ERIB 13 AND 18.25 INCH FROM T/E ON LT HORIZONTAL STABILIZER, AS PER SRM A300 55-21-12 PAGE BLOCK 201 PARAGRAPH 5.J. EXACT LOCATION IS BETWEEN STA 576 AND STA 633, AS PER A300 AMM 06-31-55-00 AND EA NO 6-5520-T0355929 (P1). THIS REPAIR IS CAT A.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 10 INCH INBOARD FROM RIB 16 AND 15 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=3.5 INCH. W=2.25 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANNEL HONEYCOMB CORE CELLS LOCATED BETWEEN ERIB 17 AND RIB 18 AT 1.35 INCH FROM ERIB 17 AND 15.28 INCH FROM T/E ON LT HORIZONTAL STABILIZER, AS PER A300 SRM 55-21-12 PAGE BLOCK 201 PARAGRAPH 5.J. EXACT LOCATION IS BETWEEN STA 800 AND STA 833, AS PER A300 AMM 06-31-55-00 AND EA NO 6-5520-T0355929 P(1). THIS REPAIR IS CAT. A.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 7 INCH INBOARD FROM RIB 7 AND 16 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1 EA) (L=2 INCH W=1.5 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELL LOCATED AT 7.5 INCH FROM ERIB 7 AND 16 INCH FROM T/E ON LT HORIZONTAL STABILIZER, AS PER SRM A300 55-21-12 PAGE BLOCK 201 PARAGRAPH 5.J. EXACT LOCATION IS BETWEEN STA 327 AND STA 379, AS PER A300 AMM 06-31-55-00 AND EA 6-5520-T0355929 (P1). THIS REPAIR IS CAT-A.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 9 INCH. OUTBOARD FROM RIB 7 AND 25 INCH. FROM TRAILING EDGE. REPAIRED THE ELEVATOR UPPER SKIN IAW SRM 55-21-12, PB 201, PARA 5.B.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 27 INCH OUTBOARD FROM RIB 13 AND 26 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=1.75 INCH. W=1.5 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEY COMB CORE CELL LOCATED AT 26 INCH FROM OUTBOARD ERIB 13 AND 26 INCH FROM T/E ON LT HORIZONTAL STABILIZER, AS PER A300 SRM 55-- 21-12 PAGE BLOCK 201 PARAGRAPH 5.J. EXACT LOCATION IS BETWEEN STA 576 AND STA 633, AS PER A300 AMM 06-31-55-00 AND EA NO 6-5520-T0355929 P(1) THIS REPAIR IS CAT. A.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON THE LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED 17 INCHES OUTBOARD FROM RIB 2 AND 5.5 INCHES FROM TRAILING EDGE. REPAIRED IAW SRM 55-21-12, PAGE BLOCK 201, PARAGRAPH 5.J.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS LOCATED AT 1 INCH. OUTBOARD FROM RIB 5 AND 4 INCH. FROM TRAILING EDGE ON RH HORIZONTAL STABILIZER (1 EA) (L=6 INCH. W=1.5 INCH) REPAIRED RH ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELL LOCATED AT 3.52 INCHES FROM ERIB 7 AND 6.22 INCHES FROM T/E ON RH HORIZONTAL STABILIZER AS PER A300- 600 SRM 55-21-12 PAGEBLOCK 201 PARAGRAPH 5.J. EXACTLY LOCATION IS BETWEEN STA 327 AND STA 379 AS PER A300 AMM 06-31-55-00 AND EA 6-5520-T0355916 (P1). THIS REPAIR IS CAT-A.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED 4 INCHEC. OUTBOARD FROM RIB 16 AND 17 INCH. FROM TRAILING EDGE. REPAIRED THE LT ELEVATOR UPPER SKIN IAW SRM A-300 55-21-12 PAGE BLOCK 201 PARAGRAPH 5.J.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON THE LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED 10 INCHES INBOARD FROM RIB 16 AND 8 INCHES FROM TRAILING EDGE. REPAIRED THE LT ELEVATOR UPPER SKIN PANEL IAW SRM 55-21-12, PAGE BLOCK 201, PARAGRAPH 5.J.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON THE LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED 3 INCHES OUTBOARD FROM RIB 13 AND 19 INCHES FROM TRAILING EDGE. REPAIRED THE LT ELEVATOR UPPER SKIN PANEL IAW SRM 55-21-12, PAGE BLOCK 201, PARAGRAPH 5.J.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 12 INCH OUTBOARD FROM RIB 7 AND 16 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=7.5 INCH. W=3 INCH). REPAIRED ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS AT LEVEL 12 INCHES FROM O/B ERIB 7 AND 16 INCHES FROM T/E ON HORIZONTAL STABILIZER, IAW A300 SRM 55-21-12 P.B. 201 PARA 5.B. THIS REPAIR IS APPLICABLE TO THE INSPECTION PROGRAM DEFINED IN SRI AND FIRST INSPECTION AFTER A/C FIRST FLIGHT AT 42500FC/89000FH, IAW SRI 55-21-12-2-001-00 TABLE 202. SUBSEQUENT INSPECTION AND INSPECTION METHOD TBD. EXACT LOCATION IS BTW STA 379 AND STA 402, AS PER A300 AMM 06-31-55-00 AND EA 6-5520-T0355929 (P1). REPAIR CAT-B AND TRACKING IS ON EA.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON THE LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED 7 INCHES INBOARD FROM RIB 7, AND 16 INCHES FROM TRAILING EDGE. REPAIRED THE LT ELEVATOR UPPER SKIN IAW SRM 55-21-12, PAGE BLOCK 201, PARAGRAPH 5.J.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON THE LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED 20 INCHES OUTBOARD FROM RIB 13 AND 18 INCHES FROM TRAILING EDGE. REPAIRED THE LT ELEVATOR UPPER SKIN PANEL IAW SRM 55-21-12, PAGE BLOCK 201PARAGRAPH 5.J.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE C ELLS. LOCATED AT 19 INCH. INBOARD FROM RIB 16 AND 9 INCH. FROM TRAILING EDGE ON LH HORIZONTAL STABILIZER (1EA) (L=4.25 INCH. W=2.25 INCH) REPAIRED ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELL AT LEVEL BTW ERIB 14 AND ERIB 15 AT 10.50'' FROM ERIB 15 AND 8.70'' FROM TRAILING EDGE ON HORIZONTAL STABILIZER LH AS PER A300 SRM 55-21-12 PB 201 PARA. 5.B THIS REPAIR IS APPLICABLE TO THE INSPECTION PROGRAM DEFINED IN SRI AND FIRST INSPECTION AFTER A/C FIRST FLIGHT AT 42500FC/89000FH AS PER SRI 55-21-12-2-001-00 TABLE 202. SUBSEQUENT INSPECTION AND INSPECTION METHOD TBD AND EA 6-5520-T0355929 (P1)

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON THE RT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS, LOCATED 1 INCH OUTBOARD FROM RIB 5, AND 4 INCHES FROM TRAILING EDGE. REPAIRED IAW SRM 55-21-12, PAGE BLOCK 201, PARAGRAPH 5.J.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 4 INCH. OUTBOARD FROM RIB 16 AND 17 INCH FROM TRAILING EDGE ON LT HORIZ STAB (1EA) (L=2 INCH. W=1.75 INCH). DUE TO THE DISTANCE BETWEEN DAMAGE AREA REPORTED ON NON ROUTINE CARD N00151, N00153, AND N00154 IS LESS THAN THE MINIMUM DISTANCE. THIS DAMAGE MUST BE ENVELOPED TOGETHER AND THE AREA MUST BE CONSIDERED AS ONE DAMAGE AREA. THE TOTAL AREA OF ENVELOPE TOGETHER IS: 18.49 SQ INCH AND EVALUATED AREA AND FOUND WITHIN LIMITS TO REPAIR, AS PER A300 SRM 55-20-00 PAGE BLOCK 101 PAR 8 FIG 104. THIS SDR IS DUPLICATED, REFER TO SDR 20-1806 ON NON ROUTINE CARD N00153 AND WORK WAS DOCUMENTED ON NON ROUTINE CARD N00153 AND EA 6-5520-T0355929 (P1) THIS REPAIR IS CAT-A.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 17 INCH OUTBOARD FROM RIB 2 AND 5.5 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1 EA) (L=3 INCH. AND W=1 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEY COMB CELLS LOCATED AT 14.75 INCHES FROM ERIB 2 AND 4.5 INCHES FROM T/E ON LT HORIZONTAL STABILIZER, AS PER SRM A300-600 55-21-12 PAGE BLOCK 201 PARAGRAPH 5.J. EXACT LOCATION BETWEEN STA 168 AND STA 221, AS PER A300 AMM 06-31-55-00 AND EA 6-5520-T0355929 (P1). THIS REPAIR IS CAT-A.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 10 INCH INBOARD FROM RIB 16 AND 8 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=2.75 INCH. W=2.25 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEY COMB CORE CELL LOCATED BETWEEN ERIB 15 AND 16 AT 3.90 INCHES FROM ERIB 16 AND 8.20 INCHES FROM T/E ON LT HORIZONTAL STABILIZER, AS PER SRM A300 55-21-12 PAGE BLOCK 201 PARAGRAPH 5.J. EXACT LOCATION IS BETWEEN STA 689 AND STA 757, AS PER A300 AMM 06-31-55-00 AND EA NO 6-5520-T0355929 P(1). THIS REPAIR IS CAT-A.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 27 INCH OUTBOARD FROM RIB 13 AND 7 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=2.25 INCH. W=1.5 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS LOCATED AT 27 INCHES OUTBOARD ERIB 13 AND 7.5 INCHES FROM T/E ON LT HORIZONTAL STABILIZER, AS PER SRM A300 55-21-12 PAGE BLOCK 201 PARAGRAPH 5.J. EXACT LOCATION IS BETWEEN STA 576 AND STA 633, AS PER A300 AMM 06-31-55-00 AND EA NO 6-5520-T0355929 P(1). THIS REPAIR IS CAT-A.

Part: SKIN — DELAMINATED (RUDDER) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 6 INCH INBOARD FROM RIB 10 AND 15.5 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=3 INCH. W=2.25 INCH). REPAIRED ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS AT LEVEL 6.5'' FROM I/B ERIB 10 AND 15.5'' FROM T/E ON HORIZONTAL STABILIZER LT, AS PER A300 SRM 55-21-12 PB 201 PARA 5.B. THIS REPAIR IS APPLICABLE TO THE INSPECTION PROGRAM DEFINED IN SRI AND FIRST INSPECTION AFTER A/C FIRST FLIGHT AT 42500FC/89000FH, AS PER SRI 55-21-12-2-001-00 TABLE 202. SUBSEQUENT INSPECTION AND INSPECTION METHOD TBD AND EA 6-5520-T0355929 (P1). REPAIR IS CAT B AND TRACKING IS ON EA.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 1 INCH INBOARD FROM RIB 13 AND 14 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=5.5 INCH. W=4.5 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS LOCATED AT 1 INCH FROM INBOARD ERIB 13 AND 15 INCHES FROM T/E ON LT HORIZONTAL STABILIZER, AS PER SRM A300 55-21-12 PAGE BLOCK 201 PARAGRAPH 5.J. EXACT LOCATION IS BETWEEN STA 633 AND STA 689, AS PER A300 AMM 06-31-55-00 AND EA 6-5520-T0355929 (P1). THIS REPAIR IS CAT-A.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 35,707 hrs · 19,423 cycles

TRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN PANEL HONEYCOMB CORE CELLS. LOCATED AT 3 INCH OUTBOARD FROM RIB 13 AND 19 INCH FROM TRAILING EDGE ON LT HORIZONTAL STABILIZER (1EA) (L=2 INCH. W=1.5 INCH). REPAIRED LT ELEVATOR UPPER SKIN PANEL HONEY COMB CORE CELL LOCATED AT 3 INCHES FROM ERIB 13 AND 19.25 INCHES FROM T/E ON LT HORIZONTAL STABILIZER, AS PER SRM A300 55-21-12 PAGE BLOCK 201 PARAGRAPH 5.J. EXACT LOCATION IS BETWEEN STA 576 AND STA 633, AS PER AMM 06-31-55-00 AND EA 6-5520-T0355929 (P1). THIS REPAIR IS CAT-A.

Part: SUPPORT — CRACKED (BS 1552-1605) · airframe 35,707 hrs · 19,423 cycles

CRACK INDICATION ON INTERNAL STRUCTURE IN OPEN FASTENERS HOLES 4 E/A ON DOOR ACTUATOR SUPPORT BEAM IN FWD CARGO COMPARTMENT. CRACK LOCATION ARE: CRACK HOLE 1 LOC FR 22 MORE 3 INCH; CRACK HOLE 2 LOC FR 22 MORE 8 INCH; CRACK HOLE 3 LOC FR 22 MORE 14 INCH; CRACK HOLE 4 LOC FR 22 MORE 19 INCH. PERFORMED REPLACED ON ACTUATOR FITTING FWD CARGO DOOR, IAW EA N 6-5313-T0355404 TITLE: FUSELAGE, FWD SECTION: FR22-FR23, FWD CARGO DOOR ACTUATOR SUPPORT BEAM, CRACKS AT DRAIN HOLES, PERMANENT REPAIR.

Part: SKIN — DENTED (FRAME 24) · airframe 35,707 hrs · 19,423 cycles

DENT EXTERNAL SKIN FR24 PLUS 12INCH STR51R LOWER FUSELAGE PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN FR 24 PLUS 12 INCH STR 51R LOWER FUSELAGE TITLE: FUSELAGE, PLATES AND SKIN: SKIN BETWEEN FR 24-FR 25, S51R, DENT, PERMANENT REPAIR EA # 6-5330-T0355526 "MINOR REPAIR"

Part: SUPPORT — CRACKED (FRAMES 61-62) · airframe 35,707 hrs · 19,423 cycles

CRACK INDICATION ON INTERNAL STRUCTURE IN OPEN FASTENERS HOLE 2 EA ON DOOR ACTUATOR SUPPORT BEAM BETWEEN FR 61 TO FR 62 IN AFT CARGO COMPARTMENT. CRACK LOCATIONS ARE: CRACK HOLE 1 LOC FR 61 MORE 7 INCH; CRACK HOLE 2 LOC FR 61 MORE 18 INCH. PERFORMED PERMANENT REPAIR ON ACTUATOR FITTING AFT CARGO DOOR, IAW EA NR 6-5317-T0355170 TITLE: FUSELAGE AFT INTERMEDIATE SECTION FR61-FR62 AFT CARGO DOOR ACTUATOR SUPPORT BEAM, CRACKS AT DRAIN HOLES PERMANENT REPAIR CHECK REQUIRED FIRST INSPECTION AT 10,000 FC.

Part: FITTING — CRACKED (BS 863) · airframe 35,707 hrs · 19,423 cycles

CRACK INDICATION ON FRAME 4 LOC. ON WINDSHIELD LOWER FRAME (CLOSING PANEL) RH SIDE HOLE NUMBER 10, CRACK DIRECTION IS 3 AND 7 O CLOCK IN COCKPIT (1 EA) REPLACED FITTING (GUSSET) LOCATED ON FRAME 4 ON WINDSHIELD LOWER FRAME 4 (CLOSING PANEL) RH SIDE IN COCKPIT IAW SRM A300-600 51-40-21 AND DWG A53613223

Part: IDG — LEAKING (NR 2 ENGINE) · airframe 34,652 hrs · 18,742 cycles

PDIS 651 24-20 2816 10JUL19 EWR OPEN U LOGPAGES:3138907 LOW IDG OIL PRESSURE WARNING, FOLLOWED BY LOSS OF #2 GENERATOR ON INITIAL TAKEOFF ROLL. REJECTED TAKEOFF @ < 60 KTS. COMPLIED W/PROCEDURES AND DECIDED TO REMAN FOR BRAKE COOLING. LOTS OF OIL COMING OUT OF ENGINE ON RETURN. MEL 10JUL19 22:02 EWR U RELEASED FOR SERVICE PER MEL : 24-11-01-B CATEGORY : B EXPIRATION : 13JUL19 "MEL 24-11-01-B: GEN (IDENTIFY 1 OR 2) 2 - INOP. APU GEN MUST BE USED TO POWER AFFECTED BUS THROUGHOUT FLIGHT. VERIFY AND RECORD IN AML/EAML THAT OIL QTY OF IDG IN DISCONNECT MODE, REMAINING OPERATIVE IDG, AND APU ARE CHECKED ONCE EACH FLIGHT DAY." AT A/C ARRIVAL BACK TO THE GATE, VERIFIED OIL COMING OUT OF #2 IDG THROUGH DRAIN MAST. SERVICED #2 IDG PER AMM 12-13-24-00-02. PART 11JUL19 02:09 MC1 U IDENTIFIED PARTS (W/KIT) INTEGRATED DRIVE MPN: 735874D CPN: 2410587 QTY: 1.

Part: FAIRING — FAILED (KRUEGER FLAP) · airframe 34,170 hrs · 18,461 cycles

KRUGER FLAPS DID NOT DEPLOY AT 3000/210 KTS. RAN QRH. AFTER TWO MINS KRUGER FLAPS DEPLOYED. REPLACED RH FOLDING FAIRING AND SPRING ROD FOR KRUGER FLAP. IAW 27-87-14-04. INSTALLED RT KRUEGER FLAP ACTUATOR IAW AMM 27-88-11-04. RIG, LEAK AND OPS CHECKED NORMAL. COMPLETED MECHANISM INSTALL AND OPS CHECK IAW AMM 27-87-14-04. FIT CHECK AND OPS CHECK OF RT KRUEGER FLAP IAW AMM 27-87-11-04. ALL OPS CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (R1 DOOR) · airframe 33,693 hrs · 18,154 cycles

MAIN CABIN DOOR R1 (COPILOT SIDE) WILL NOT ARM SLIDE. RELEASED FOR SERVICE PER MEL 52-XX ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE. PENDING T/S OF MEL ITEM, SDR IS OPEN.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 33,598 hrs · 18,101 cycles

MAIN CARGO COMPARTMENT FLOOR BOARD 232CF CRACKED. FABRICATED A NEW REPLACEMENT BOARD FOLLOWING DWG SRZ-25-005 REV N GUIDE LINES.

Part: BRACKET — CORRODED (FRAMES 26-27) · corrosion level 2 · airframe 33,598 hrs · 18,101 cycles

CORROSION FOUND ON THE MAIN CARGO BAY THRUST BRACKET, BETWEEN FRAMES 26 AND 27, -Y1456 TO -Y1959. REMOVED AND REPLACED THE THRUST BRACKET IAW SRM 53-14-15, AND DWG A537819700000.

Part: BRACKET — CORRODED (FRAMES 27-28) · corrosion level 2 · airframe 33,598 hrs · 18,101 cycles

CORROSION ON MAIN CARGO BAY THRUST BRACKET, BETWEEN FRAMES 27 AND 28, -Y1456 TO -Y1959. REMOVED AND REPLACED THRUST BRACKET IAW SRM 53-14-15, AND DWG A537819700000.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,598 hrs · 18,101 cycles

CORROSION ON MAIN CARGO COMPARTMENT SEAT TRACK FR28 AT LBL Y953. REMOVED AND REPLACED SEAT TRACK SECTION IAW SRM 53-10-16 FIGURE 201.

Part: BRACKET — CORRODED (FRAMES 26-27) · corrosion level 2 · airframe 33,598 hrs · 18,101 cycles

CORROSION ON MAIN CARGO BAY THRUST BRACKET, BETWEEN FRAMES 26 AND 27, -Y1959 TO -Y2462. REMOVED & REPLACED THRUST BRACKET IAW SRM 51-40-21 AND 51-42-11 AND DWG 53781941, ISSUE D.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,598 hrs · 18,101 cycles

CORROSION ON MAIN CARGO COMPARTMENT SEAT TRACK BETWEEN FR26 AND FR28 AT RBL Y2462. REMOVED AND REPLACED SEAT TRACK PER SRM 53-10-16 AND DWG A53781970 ISSUE D.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,598 hrs · 18,101 cycles

CORROSION ON MAIN CARGO COMPARTMENT SEAT TRACK BETWEEN FRAME 26 AND FR28 AT Y1959. REMOVED AND REPLACED SEAT TRACK SECTION PER SRM 53-10-16 AND DWG A53781970 ISSUE D.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,598 hrs · 18,101 cycles

CORROSION ON MAIN CARGO COMPARTMENT SEAT TRACK BETWEEN FRAME 26 AND FR28 AT Y953. REMOVED AND REPLACED SEAT TRACK SECTION IAW SRM 53-10-16 FIGURE 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,598 hrs · 18,101 cycles

CORROSION ON MAIN CARGO COMPARTMENT SEAT TRACK BETWEEN FRAME 26.5 AND FR27.5 AT Y1456. REMOVED AND REPLACED SEAT TRACK SECTION IAW SRM 53-10-16 FIGURE 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,598 hrs · 18,101 cycles

CORROSION ON MAIN CARGO COMPARTMENT SEAT TRACK, FRAME 26 Y2462. REMOVED AND REPLACED SEAT TRACK SECTION IAW EA 6-5310-T0341529.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,598 hrs · 18,101 cycles

CORROSION ON MAIN CARGO COMPARTMENT SEAT TRACK BETWEEN FRAME 26 AND FR28 AT Y450. REMOVED & REPLACED SEAT TRACK PER SRM 53-10-16 AND DWG A53781970 ISSUE D.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,598 hrs · 18,101 cycles

CORROSION ON MAIN CARGO COMPARTMENT SEAT TRACK BETWEEN FRAME 26 AND FR28 AT Y1959. REMOVED AND REPLACED SEAT TRACK SECTION IAW SRM 53-10-16 FIGURE 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,598 hrs · 18,101 cycles

CORROSION ON MAIN CARGO COMPARTMENT SEAT TRACK BETWEEN FRAME 26 AND FR28 AT Y1456. REMOVED AND REPLACED SEAT TRACK SECTION IAW SRM 53-10-16 FIGURE 201.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 33,598 hrs · 18,101 cycles

MAIN CARGO COMPARMENT FLOOR PANEL 231GG HAS IMPACT DAMAGE. FABRICATED NEW FLOOR PANEL IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 33,598 hrs · 18,101 cycles

MAIN CARGO COMPARMENT FLOOR PANEL 231NG HAS IMPACT DAMAGE. FABRICATED NEW FLOOR PANEL IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 33,598 hrs · 18,101 cycles

MAIN CARGO COMPARMENT FLOOR PANEL 231KG HAS IMPACT DAMAGE. FABRICATED NEW FLOOR PANEL IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 33,598 hrs · 18,101 cycles

MAIN CARGO COMPARMENT FLOOR PANEL 231PG HAS IMPACT DAMAGE. FABRICATED NEW FLOOR PANEL IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 33,598 hrs · 18,101 cycles

MAIN CARGO COMPARMENT FLOOR PANEL 231DH HAS IMPACT DAMAGE. FABRICATED NEW FLOOR PANEL IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 33,598 hrs · 18,101 cycles

MAIN CARGO COMPARMENT FLOOR PANEL 231EH HAS IMPACT DAMAGE. FABRICATED NEW FLOOR PANEL IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 33,598 hrs · 18,101 cycles

MAIN CARGO COMPARMENT FLOOR PANEL 231CF HAS IMPACT DAMAGE. FABRICATED NEW FLOOR PANEL IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 33,598 hrs · 18,101 cycles

MAIN CARGO COMPARMENT FLOOR PANEL 231EF HAS IMPACT DAMAGE. FABRICATED NEW FLOOR PANEL IAW DWG SRZ-25-005 REV N AND GMM 07-0-1000.

Part: RELAY — FAILED (FIRE DETECTION) · airframe 33,080 hrs · 17,781 cycles

PASSING 30K FEET CLIMBING TO FL 340, A NR 1 ENGINE FIRE INDICATION, ENGINE INDICATIONS WERE NORMAL. FOLLOWED ECAMS AND SECURED THE NR 1 ENGINE. FIRE INDICATION REMAINED AFTER AGENT FIRED. FIRED THE NR 2 AGENT AND THE FIRE INDICATION DEACTIVED. RETURNED TO DEPARTURE. REPLACED THE RELAY 9WD IAW ESPM 20-46-50. PERFORMED A NR 1 FIRE DETECTION TEST IAW 26-12-00-05-02. NO DEFECTS NOTED.

Part: CONTROL MODULE — MALFUNCTIONED (FIRE DETECTION) · airframe 33,054 hrs · 17,752 cycles

APPROACHING THE TOP OF DESCENT, RECEIVED SEVERAL 1 - 2 SECONDS NR 1 ENGINE FIRE ECAM INDICATIONS. ONLY THE LOOP A WAS ILLUNMINATED. TROUBLESHOT AND FOUND THE NR 1 ENGINE FIRE CONTROL MODULE HAS NOT YET BEEN REPLACED, R & R THE NR 1 FIRE CONTROL MODULE IAW AMM 26-12-20-04, UNIT OPS CHECKED GOOD. R & R THE NR 1 ENGINE FIRE DETECTION CONTROL UNIT IAW AMM 26-12-11-04, UNIT BITE CHECKED GOOD IAW AMM 26-12-00-5.

Part: DUCT — LOOSE (BLEED AIR) · airframe 33,050 hrs · 17,750 cycles

VERY SHORTLY AFTER LEVEL OFF, AT FL330, THE NR 1 ENGINE FIRE WARNING DISPLAYED. BEFORE INITIATING PROCEDURES, THE WARNING DISAPPEARED WITHIN A SHORT PERIOD, LESS THAN 10 SECONDS, THE WARNING DISPLAYED AGAIN AND REMAINED ILLUMINATED. COMPLIED WITH THE PROPER PROCEDURES AND DIVERTED TO LAND. FOUND THE NR 1 ENGINE LT UPPER HP RECOUP DUCT UPPER COUPLING LEAK DETECTING FOIL BLOWN OFF, ALSO FOUND PRESSURE REGULATOR VALVE LEAKING USING APU AIR. FOILED THE RECOUP TUBE COUPLING AND 7TH STAGE TURBINE COOLING TUBE FLEXABLE COUPLINGS. BLEEDS OPERATED NORMAL, NO FIRE DETECTION INDICATION, OPENED COWLINGS FOUND ALL TUBEING LEAK DETECT FOIL NOT BLOWN, NO LEAKS IAW MOCC. REMOVED AND REPLACED THE LEFT UPPER FIRE DETECTOR RAIL ASSY IAW MM 26-12-12-04-02, OPS TESTED GOOD IAW MM 26-12-00-05-02.

Part: DETECTION SYS — FALSE ACTIVATION (NR 1 ENGINE) · airframe 33,037 hrs · 17,742 cycles

NR 1 ENGINE FIRE INDICATION. SHUTDOWN THE ENGINE, PULLED FIRE HANDLE, DISCHARGED THE FIRE AGENT 1. FIRE INDICATION WENT AWAY AFTER AGENT DISCHARGED. FOIL WRAPPED TWO COUPLING DUCTS FOR LTP DUCT THAT HAD FOIL BLOWN OUT. RAN THE NR 1 ENGINE IAW JRH, TESTED NR 1 ENGINE FIRE LOOP TEST NO FAULTS, RAN THE NR 1 ENGINE TO 80%, FOR 5 MINUTES, THEN IDLE, 70% FOR 5 MINUTES, THEN BACK TO IDLE, 50% FOR 10 MINUTES AND BACK TO IDLE, NO FAULTS, AND ALL FOIL ON CONNECTIONS CHECKED GOOD. OHMED OUT BOTH FIRE LOOPS A AND B FOR NR 1 ENGINE, IAW TSM 26-12-00, FIG 108, ALL LOOPS OHM GOOD. CHECKED WIRING FROM FDCU TO ENGINE FIRE LOOPS, NO OPENS. CHANGING OUT THE NR 1 ENGINE FDCU AS A PERCAUTION IAW AMM 26-12-11-04. AIRCRAFT OK FOR SERVICE.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 33,034 hrs · 17,738 cycles

RIGHT WING, CENTER FLAP INTERNAL RIB 27 CRACKED AT 6 FASTENERS FWD OF REAR SPAR. REMOVED THE DAMAGED FLANGE OF THE RIB IAW SRM 57-50-00, REPAIRED IAW SRM 57-50-00 WITH REPAIR ANGLE, CLASSIFIED AS CAT A AND MAJOR REPAIR.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 33,034 hrs · 17,738 cycles

R/H WING CENTER FLAP RIB 26 CRACKED FWD OF REAR SPAR. REMOVED THE DAMAGED FLANGE OF THE RIB IAW SRM 57-50-00, REPAIRED IAW SRM 57-50-00, FIG. 201 WITH A REPAIR ANGLE. CLASSIFIED AS CAT A AND MAJOR REPAIR.

Part: NONE — NONE (NONE) · airframe 33,034 hrs · 17,738 cycles

NEED TO ACCOMPLISH SKIN REPAIR ON L/H CENTER FLAP ADJACENT TO RIB #12 FOR ACCESS TO RIB REPAIR. REPAIR PER SRM 57-50-00, FIG 205, DOUBLER INSTALLED ON L/H CENTER FLAP BETWEEN RIBS 11 AND 12 AND BETWEEN THE REAR SPAR AND STRINGER 2.1, BOTTOM SKIN IAW SRM 51-40-21, CLASSIFIED AS CAT "A" AND MAJOR REPAIR.

Part: RIB — CRACKED (LT WING TE FLAP) · airframe 33,034 hrs · 17,738 cycles

LEFT WING, CENTER FLAP INTERNAL RIB #12 CRACKED 6 FASTENERS FWD OF REAR SPAR. REMOVED DAMAGE ON L/H WING CENTER FLAP RIB #12 IAW SRM 57-50-00, FIG. 201, FABRICATED REPAIR ANGLE IAW SRM 57-50-00, FIG 20, INSTALLED REPAIR ANGLE IAW SRM 51-40-21, CLASSIFED AS "A" AND MAJOR REPAIR.

Part: NONE — NONE (NONE) · airframe 33,034 hrs · 17,738 cycles

NEED TO ACCOMPLISH SKIN REPAIR ON R/H CENTER FLAP ADJACENT TO RIB #25 FOR ACCESS TO RIB REPAIR. REMOVED FASTENERS FOR REPAIR DOUBLER ON CENTER FLAP AT RIB #25 R/H, FABRICATED DOUBLER REPAIR IAW A300-600 SRM 57-50-00 PAGE 217, LOCATED AND DRILLED DOUBLER IAW SRM 51-40-44, INSTALLED REPAIR DOUBLER ON CENTER FLAP AT RIB #25 R/H IAW A300-600 SRM 51-40-21, CLASSIFIED AS CAT "A" AND MAJOR REPAIR.

Part: RIB — CRACKED (LT WING TE FLAP) · airframe 33,034 hrs · 17,738 cycles

LEFT WING, CENTER FLAP INTERNAL RIB # 26 CRACKED 6 FASTENERS FWD OF REAR SPAR. REPAIRED RIB #26 WITH 3 EA. FLANGES IAW A300 SRM 57-50-00, FIG. 201. CLASSIFED AS CAT "A" AND MAJOR REPAIR.

Part: NONE — NONE (NONE) · airframe 33,034 hrs · 17,738 cycles

NEED TO ACCOMPLISH SKIN REPAIR ON L/H CENTER FLAP BETWEEN RIB #26 AND #27 FOR ACCESS TO RIB REPAIR. REPAIRED PER SRM 57-50-00, FIG 205, DOUBLER INSTALLED ON L/H CENTER FLAP BETWEEN RIBS 26 AND RIB 27, BETWEEN THE REAR SPAR AND STRINGER 2.3 BOTTOM SKIN IAW SRM 51- 40-21 AND SRM 57-50-00, CLASSIFIED AS CAT "A" AND MAJOR REPAIR.

Part: NONE — NONE (NONE) · airframe 33,034 hrs · 17,738 cycles

NEED TO ACCOMPLISH SKIN REPAIR ON R/H CENTER FLAP ADJACENT TO RIB #19 FOR ACCESS TO RIB REPAIR. REMOVED FASTENERS FOR REPAIR DOUBLER ON RIGHT WING CENTER FLAP RIB #19, FABRICATED REPAIR DOUBLER IAW SRM 57-50-00, INSTALLED REPAIR DOUBLER IAW SRM 51-40- 21, REPAIR CLASSIFIED AS CAT "A" AND MAJOR REPAIR.

Part: COUPLING — BENT (FRAME 23) · airframe 33,034 hrs · 17,738 cycles

MAIN DECK RH SIDE AT FRAME 23 BETWEEN STR 8 AND STR9 FRAME SPLICE HAS BENT. REMOVED DAMAGE COUPLING IAW A300 SRM 51-40-21, FABRICATED NEW COUPLING P/N FX- A53770903210 ON VT MAE TRAVELER T17/132376 IAW SRM 53-13-13, INSTALLATION NEW COUPLING IAW SRM A300 SRM 51-40-44 AND SRM 51-40-21. REPAIR CLASSIFIED AS CAT. 'A' AND MAJOR REPAIR.

Part: ANGLE — CRACKED (RT WING TE FLAP) · airframe 33,034 hrs · 17,738 cycles

RIGHT WING, CENTER FLAP INTERNAL RIB #19 CRACKED 6 FASTENERS FWD OF REAR SPAR. REMOVED CRACKED RIB #19 IAW SRM 57-50-00 FIG 201, REPAIR CRACKED RIB #19 RIGHT WING CENTER FLAP IAW SR 57-50-00 FIG 201 WITH REPAIR ANGLE. CLASSIFIED AS "A" AND MAJOR REPAIR.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 33,034 hrs · 17,738 cycles

RIGHT WING CENTER FLAP INTERNAL RIB #25 CRACKED 6 FASTENERS FWD OF REAR SPAR. REMOVED CRACKED RIB #25 IAW SRM 57-50-00, REPAIRED CRACK RIB #25 ON R/H WING CENTER WING FLAP IAW SRM 57-50-00 WITH REPAIR ANGLE, REPAIR CLASSIFIED AS CAT "A" AND MAJOR REPAIR.

Part: RIB — CRACKED (LT WING TE FLAP) · airframe 33,034 hrs · 17,738 cycles

LEFT WING, CENTER FLAP INTERNAL RIB NR 27 CRACKED FWD OF REAR SPAR. REPAIRED THE RIB IAW SRM 57-50-00, FIG 201 AND 202, CLASSIFIED AS A CAT "A' AND MAJOR REPAIR.

Part: COUPLING — BENT (FRAME 22) · airframe 33,034 hrs · 17,738 cycles

MAIN DECK RH SIDE AT FRAME 22 STR8 AND STR9 FRAME AND SPLICE HAS BENT. REMOVED DAMAGE COUPLING IAW A300-600 SRM 51-40-21, FABRICATED NEW COUPLING P/ FX- A53770903210 ON VTMAE TRAVELER T17/1312426 IAW SRM 53-13-13, INSTALLATION COUPLING IAW A300 SRM 51-40-44 AND SRM 51-40-21. REPAIR IS CLASSIFED AS CAT "A" AND MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 33,034 hrs · 17,738 cycles

MDCC 241LK FLOOR PANEL BROKEN. FABRICATED FLOOR PANEL 241LK ON VTMAE TRAVELER #17/1311725 IAW SRZ 25-005, CLASSIFED AS CAT. 'A' AND MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (MAIN DECK) · airframe 33,034 hrs · 17,738 cycles

MDCC 252BF FLOOR PANEL BROKEN FABRICATED FLOOR PANEL 252BF ON VTMAE TRAVELER #17/1311729 IAW SRZ 25-005, CLSSIFED AS CAT. "A" AND MAJOR REPAIR.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 32,737 hrs · 17,551 cycles

ON CLIMBOUT FROM KMEM NOTICED YELLOW HYD SYSTEM FLUID DECREASING. WITHIN A COUPLE MINUTES THE ECAM ALERTED US TO LOW PRESSURE. WE FOLLWED ECAM PROCEDURES AND QRH PROCEDURES. THERE WAS A LITTLE FLUID LEFT UPON SHUTTING DOWN THE YELLOW PUMP. RTB UNEVENTFULL. WHILE WORKING WRI 29-02/0701 MECHANICS FOUND NR 5 SPOILER ACTUATOR MOUNT BOLTS BROKEN. INSPECTED A/C FOUND RT WING NR 5 SPOILER ACCUATOR O/B PRESSURE LINE LEAKING AT SWEDGE NEAR B-NUT. HYDRAULIC LINE REPLACED. INSTALLED MISSING BLOCK CLAMP ASSY. CHECKED LINES FOR SECURITY AND TORQUE. PRESSURIZED AND OPERATED SPOILER SEVERAL CYCLES WITH NO LEAKS NOTED. CLOSED LOWER TRAILING EDGE PANEL. ACOMPLISHED HUYDRAULIC BLEED PRO0CEDURE WITH ENGINES RUNNING FOR YELLOW SYSTEM.

Part: ENGINE — FAILED (NR 1) · airframe 32,241 hrs · 17,267 cycles

FLYING FROM SJC TO IND AT LEVEL OFF THE OIL BUGS WERE SET AT 16QTS ON EACH GAGE TO MATCH THE CORRECT OIL QUANTITY READING. APPROXIMATELY 15-20 MINS LATER, NR 1 ENG OIL QUANTITY DECREASED TO 13 QTS, THEN 5-10MIN LATER WENT TO 12.5 QTS. FO WENT TO THE CABIN ARE AND NOTICED VISUAL INDICATION OF SIGNIFICANT FUMES. DIVERTED TO SLC, OIL QTY CONTINUED TO DECREASE TO 12 QTS WHICH WAS THE LAST INDICATION THAT WE NOTICED BEFORE LANDING. INSTALLED NR 1 ENGINE PER AIRCRAFT MAINTENANCE WORK CARD 64T0100-1.

Part: LIMITER — LEAKING (TE FLAP) · airframe 30,996 hrs · 16,508 cycles

BOTH FLAP SYS 1 & 2 FAILED ON APPROACH. INTERROGATED SFCC 1 & 2. BOTH SHOWED JAM. RESET & DID BITE CHECK, BOTH PASSED. CHECKED LT & RT FLAP TORQUE LIMITERS. LT FLAP TORQUE LIMITER WAS POPPED IAW MM 27-51-00-05. WILL OPS CHECK FLAPS WHEN DONE UNLOADING. DURING BACKLASH CHECK IAW TSM 27-50-02 FIG 106, FOUND LT TORQUE LIMITER LEAKING & BAD. R & R LT FLAP TORQUE LIMITER 5294 IAW AMM 27-54-12-04. PASSED BACKLASH CHECK IAW TSM 27-50-02. STILL REQUIRES OPERATIONS CHECK AFTER TROUBLESHOOTING FLAP FAULT. FAILED OPERATIONS CHECK OF FLAPS IAW MM 27-54-00-05. FOUND LT FLAP TORQUE LIMITER POPPED. BACKLASH CHECKED ON 1 & 2 FLAP JACKSCREWS IAW TSM 27-50-02 FIG 101 BLOCK 11. STARTED ON BLOCK 12 OF TSM 27-50-02 FIG 101. NO MOVEMENT BETWEEN SCREW JACK 2 & 3. NEED TO CHECK BETWEEN 3 & 4 FLAP SCREW JACK NEXT.

Part: BATTERY — DISCHARGED (R1 DOOR) · airframe 30,981 hrs · 16,497 cycles

R1 DOOR SLIDE WOULD NOT ARM. RELEASED FOR SERVICE IAW MEL 52-30-04 CATEGORY C EXPIRATION 16 APR1 16. ECAM SLIDE INDICATION SYS FOR R1 DOOR INOPERATIVE. DOOR ESCAPE SLIDE ARMING SYS IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE. TROUBLE SHOT IAW TSM 52-73-00 & ASM 52-73-00. R & R BATT 2 ON ASPSU 70WN IAW MM 52-73-18. SLIDE ARM NORMAL. R & R POWER SUPPLY UNIT AUTONOMOUS STANDBY 70WN IAW MM CH 52-73-18.

Part: INDICATION SYS — FAULTY (FUEL SYSTEM) · airframe 301 hrs · 16,013 cycles

ON CLIMB OUT PASSING FL 230 GOT ECAM FUEL ADVISORY, LT INNER WAS READING 16.5 & RT INNER READING APPROX 10.5, WITHIN 2 MINUTES WENT DOWN TO MATCH RT INNER, THEN WENT 4.0 BELOW RT INNER. RELEASED FOR SERVICE IAW MEL 28-42-01-05 CATEGORY C, EXPIRATION 02 SEPT 15. LT INNER TANK INDICATIONS INOPERATIVE. EITHER FUEL TO KNOWN QTY OR, AFTER REFUELING VERIFY TANK QTY WITH MAG LEVEL INDICATORS & ROD INCREMENT READINGS ARE RECORDED IN AML & EAML. FOUND INTERMITTENT CODES 331, 022, 502 & 960. CODE 7.07 WAS CONTINUOUS. PLACED LT INNER FQI SYS ON MEL 28-42-01-05.

Part: THRUST REVERSER — DAMAGED (NR 1) · airframe 299 hrs · 15,899 cycles

NUMBER 1 OTBD THRUST REVERSER AFT HINGE LUG DAMAGED EXHAUST SYS. THRUST REVERSER BLEND REPAIR OF HINGE BEAM REPAIRED IAW EA 6-7830-T0318435. THIS REPAIR IS CLASSIFIED AS A CATEGORY B MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 299 hrs · 15,899 cycles

152 RF HAS 1 TORN OUT FASTENER HOLE & CRACKED ON BACKSIDE CORNER. FABRICATED NEW PANEL 15 2RF ON T15 1145409.

Part: WINDOW FRAME — GOUGED (FUSELAGE) · airframe 299 hrs · 15,899 cycles

LEFT SLIDING WINDOW PANEL FWD FRAME CHAFED. ACCOMPLISHED FINAL EA 6-5610-T0318226 P 1 LT SLIDING WINDOW FWD FRAME GOUGED.

Part: WINDOW FRAME — GOUGED (COCKPIT) · airframe 299 hrs · 15,899 cycles

RIGHT SLIDING WINDOW PANEL FWD FRAME HAS CHAFED MARKS. ACCOMPLISHED FINAL EA 6-5610-T0318208 PT 1. RT SLIDING WINDOW FWD FRAME GOUGED.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 299 hrs · 15,899 cycles

FORWARD CARGO COMPARTMENT FLOOR PANEL 132 NG HAS SEVERAL DENTS, CRACKS, DAMAGED INSERT & HONEY COMB EDGES. FABRICATED FLOOR PANEL 132 NG ON T15 1144765 IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 299 hrs · 15,899 cycles

FORWARD CARGO COMPARTMENT PANEL 131 MG HAS MULTIPLE DENTS, PUNCTURED & DAMAGED EDGES & HONEY COMB. FABRICATED FLOOR PANEL 131 MG ON T15 1146570 IAW SRZ 25-005. THIS REPAIR IS CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 299 hrs · 15,899 cycles

BULK CARGO FLOOR PANEL 162 HF, PROTECTIVE COATING CHIPPED OFF SHOWING SIGNS OF CORROSION ON SOME AREAS. FABRICATED FLOOR PANEL 162 HF ON T15 1145638 IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 299 hrs · 15,899 cycles

BULK PIT FRAME 65 TO 66 AT -Y1949 FLOOR SUPPORT IS CRACKED FWD END. R & R FLOOR SUPPORT IAW SRM 51-40-21. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 299 hrs · 15,899 cycles

BULK CARGO FLOOR LEVEL AT FRAME 66, LT SIDE FLOORBEAM HAS CORROSION. R & R FRAME 66 FLOORBEAM BULK CARGO FLOOR IAW SRM 51-40-21 DUE TO CORROSION OUT OF LIMITS IAW SRM 51-74-10 & SRM 51-10-10. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 299 hrs · 15,899 cycles

FORWARD CARGO COMPARTMENT, FLOOR PANEL 131 SG HAS MULTIPLE DENTS, CRACKS, DAMAGED EDGES, HONEY COMB & SEALANT. FABRICATED FLOOR PANEL 131SG ON 15 1145640 IAW DWG SRZ 25-005. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 299 hrs · 15,899 cycles

FORWARD CARGO COMPARTMENT, FLOOR PANEL 131 NG DAMAGED. FABRICATED FLOOR PANEL 131 NG ON T15 1144769 IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 299 hrs · 15,899 cycles

FORWARD CARGO COMPARTMENT FLOOR PANEL 131 PG HAS MULTIPLE DENTS, CRACKS, DAMAGED INSERTS & EDGES, HONEY COMB & SEALANT. FABRICATED FLOOR PANEL 131 PG ON T15 1146574 IAW DWG SRZ 25-005. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 299 hrs · 15,899 cycles

BULK CARGO FLOOR PANEL 161HF HAS DENTS ALL OVER & SIGNS OF CORROSION. FABRICATED FLOOR PANEL 161HF ON T15 1146575 IAW DWG SRZ25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 299 hrs · 15,899 cycles

FORWARD CARGO COMPARTMENT, FLOOR PANEL 132 SG HAS SEVERAL DENTS, CRACKS, DAMAGED EDGES, HONEY COMB & MISSING SEALANT. FABRICATED FLOOR PANEL 132 SG ON T15 1145781 IAW DWG SRZ 25-005. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 299 hrs · 15,899 cycles

FORWARD CARGO COMPARTMENT FLOOR PANEL 131 KG HAS SEVERAL DENTS & DAMAGED INSERTS. FABRICATED FLOOR PANEL 131 KG ON T15 1146564 PER DWG SRZ 25-005. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 299 hrs · 15,899 cycles

FORWARD CARGO COMPARTMENT FLOOR PANEL 132 PG HAS SEVERAL DENTS, PUNCTURED & DAMAGED EDGE. FABRICATED FLOOR PANEL 132 PG ON T15 1146568 IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 299 hrs · 15,899 cycles

162 EF HAS REPAIRED DENTS WITH REPAIRS DELAMINATED PEALING UP & BROKEN OFF CORNER. FABRICATED FLOOR PANEL 162 EF ON T15 1146587 IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 299 hrs · 15,899 cycles

DURING ACCOMPLISHMENT OF SEAT TRACK & DUMMY SEAT TRACK ATTACHMENT FITTING EO 6-5310-7-3322 B2 PT 1, FOUND SEAT TRACK AT FRAME 54 - 54.2, RT NR 5 GAP VALUE TO BE OUT OF LIMITS. REPAIRED SEAT TRACK IAW SRM 53-15-16 FIG 201. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 299 hrs · 15,899 cycles

FORWARD CARGO COMPARTMENT FLOOR PANEL 131 QG HAS MULTIPLE DENTS, DAMAGED & MISSING INSERTS, HONEY COMB & MISSING SEALANT. FABRICATED FLOOR PANEL 131 QG ON T15 1144770 IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 299 hrs · 15,899 cycles

152 QF PANEL, CRACKED IN SEVERAL PLACES. FABRICATED FLOOR PANEL 152 QF ON T15 1145787 IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 299 hrs · 15,899 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 152 WF DAMAGED. FABRICATED FLOOR PANEL 152 WF ON T15 11446592 IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 299 hrs · 15,899 cycles

FORWARD CARGO COMPARTMENT FLOOR PANEL 132 KG HAS SEVERAL DENTS, CRACKS, DAMAGED INSERT & HONEY COMB EDGES. FABRICATED FLOOR PANEL 132 KG ON T15 1146572 IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DENTED (ZONE 100) · airframe 299 hrs · 15,899 cycles

BULK CARGO FLOOR PANEL 161 AF HAS DENTS. FABRICATED FLOOR PANEL 161 AF ON T15 1145639 IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · corrosion level 2 · airframe 299 hrs · 15,899 cycles

BULK CARGO FLOOR PANEL 161 CF HAS DENTS, PUNCTURED & CORROSIONS AT THE BACK. FABRICATED FLOOR PANEL 161 CF ON T15 1145406 IAW DWG SRZ 25-005. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.

Part: RIB — CHAFED (LT WING) · airframe 299 hrs · 15,899 cycles

LEFT WING AFT OF REAR SPAR HYD SUCTION LINE CLAMP BLOCK ATTACHMENT BOLT CHAFING ON RIB 7A. CUT OUT EDGE COMPLIED WITH EA 6-5710-T0318026 ON LT RIB 7A OTBD EDGE DUE TO MATERIAL REMOVED FROM RIB EXCEEDED SRM LIMITS IAW SRM 57-20-19. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 299 hrs · 15,899 cycles

152 SF HAS NUMEROUS CRACKS IN BOTTOM SKIN. FABRICATED FLOOR PANEL 152 SF ON T15 1145410 IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DENTED (CARGO BAY) · airframe 299 hrs · 15,899 cycles

FORWARD CARGO COMPARTMENT FLOOR PANEL 132 RG HAS SEVERAL DENTS. DAMAGED INSERT & EDGES, HONEY COMB & SEALANT. FABRICATED FLOOR PANEL 132 RG ON T15 1146558 IAW DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 299 hrs · 15,899 cycles

FORWARD CARGO COMPARTMENT FLOOR PANEL 132 MG HAS SEVERAL DENTS, DAMAGED INSERT, EDGES, HONEYCOMB & SEALANT. FABRICATED FLOOR PANEL 132 MG ON T15 1146559 IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 299 hrs · 15,899 cycles

152TF HAS NUMEROUS PUNCTURES ON SKIN UNDERSIDE. FABRICATED FLOOR PANEL 152 TF ON T15 1145786 IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 299 hrs · 15,899 cycles

WHEEL WELL FLOOR PANEL 147EF HAS EDGE DAMAGE & IS FLUID SOAKED. FABRICATED FLOOR PANEL 147EF ON T15 1144767 IAW DWG SRZ25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 299 hrs · 15,899 cycles

FORWARD CARGO COMPARTMENT FLOOR PANEL 132 LG HAS SEVERAL DENTS, MISSING & DAMAGED INSERT, DAMAGED EDGES, HONEYCOMB & MISSING SEALANT. FABRICATED FLOOR PANEL 132 LG ON T15 1145782 IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOOR SUPPORT BEAM AT FRAME 14 - 16A, BL -Y1959 CORRODED. REMOVED CORROSION IAW SRM 51-74-10. ORIGINAL MATERIAL .070, LOST MATERIAL .017, FOUND OUT OF LIMITS IAW SRM 53-12-15. REMOVED FLOOR SUPPORT BEAM IAW SRM 51-40-21. LOCATED & DRILLED IAW SRM 51-40-44. TREATED & PRIMED IAW SRM 51-21-10. TOP COATED IAW SRM 51-75-10. INSTALLED FLOOR SUPPORT IAW SRM 51-40-21. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 299 hrs · 15,899 cycles

171BF HAS DELAMINATION & CRACK IN PREVIOUS REPAIR. FABRICATED PANEL 171BF ON T15 1145784 IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 299 hrs · 15,899 cycles

151 RF HAS 2 EA BLOWN OUT FASTENER HOLES & GOUGES. FABRICATED FLOOR PANEL 151 RF ON T15 1145409 IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 299 hrs · 15,899 cycles

FORWARD CARGO COMPARTMENT FLOOR PANEL 131 LG DAMAGED. FABRICATED FLOOR PANEL 131 LG ON T15 1145783 IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 299 hrs · 15,899 cycles

LEFT SIDE EXTERNAL FUSELAGE SKIN HAS DENT OUT ON FRAME 79, STRINGER 29L - 30L. EVALUATED DENT IAW SRM 53-18-12 & SRM 53-10-12 FIG 102 DIAGRAM 103 D, 0.020" A:0.00 DENT IS OUT OF LIMITS. REPAIRED SKIN SECTION IAW SRM 53-10-12 FIG 208. CLASSIFIED AS MAJOR CAT B REPAIR.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 299 hrs · 15,899 cycles

FORWARD CARGO COMPARTMENT FLOOR PANEL 132 QG HAS MULTIPLE PUNCTURED & DAMAGED INSERT HOLES. FABRICATED FLOOR PANEL 132 QG ON T15 1144768 IAW DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 299 hrs · 15,899 cycles

151 UF HAS PULLED THROUGH INSERT. FABRICATED FLOOR PANEL 151 UF ON T15 1145408 IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 299 hrs · 15,899 cycles

FORWARD CARGO COMPARTMENT FLOOR PANEL 131 RG HAS MULTIPLE DENTS, CRACKS, DAMAGED EDGES, HONEYCOMB & MISSING SEALANT. FABRICATED FLOOR PANEL 131 RG ON T15 1146557 IAW DWG SRZ 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MLG WELL FLOOR PANEL 143DF DELAMINATED, PANEL RACK. FABRICATED FLOOR PANEL 143DF ON 15 1145405 IAW DWG SRZ25-005. CAT A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 299 hrs · 15,899 cycles

CABIN SEAT TRACK -Y1456 RT, FRAME 40 - 45 HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-10. CHECKED LIMITS, MATERIAL REMOVED L 2.0 W 0.450" D .050, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16-101. R & R SEAT TRACK SECTION PN A5383202020400 BATCH 0002806689 IAW SRM 51-40-21.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 299 hrs · 15,899 cycles

162CF HAS CRACK IN OUTER SKIN & NUMEROUS DENTS. FABRICATED FLOOR PANEL 162CF ON T15 1145407 IAW SRZ 25-005 DWG. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MDCC FLOOR PANEL 241 PJ FWD LT SECTION BROKEN & WITH DENTS. FABRICATED FLOOR PANEL 241 PJ ON T15 1144954 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 299 hrs · 15,899 cycles

FLOORBOARD PANEL 242 QJ PREVIOUS REPAIR CRACKED & SEVERAL HONEYCOMB EDGES ERODED. FABRICATED FLOOR PANEL 242 QJ ON T15 1144624 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MDCC FLOOR PANEL 242 WH UPPER SURFACE HAS DENT & PUNCTURED SECTION. FABRICATED FLOOR PANEL 242 WH ON T15 1149766 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 299 hrs · 15,899 cycles

FLOORBOARD PANEL 241 AJ TWO EACH INSERTS MISSING & TORN & SEVERAL UPPER SURFACE PUNCTURED. FABRICATED FLOOR PANEL 241 AJ ON T15 1144623 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOOR PANEL 251 BH CRACKED. FABRICATED FLOOR PANEL 251 BH ON T15 1143902 IAW SRZ DWG 25-005 CAT A MAJOR REPAIR.

Part: FLOORBOARD — PUNCTURED (ZONE 200) · airframe 299 hrs · 15,899 cycles

FLOORBOARD 242GJ HAS TWO PUNCTURED DENTS. FABRICATED A NEW FLOOR PANE IAW DWG 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOOR PANEL 241 QH HAS TWO EACH PUNCTURED. FABRICATED FLOOR PANEL 241 QH ON T15 144655 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 299 hrs · 15,899 cycles

FLOORBOARD PANEL 242 ZJ UPPER SURFACE HAS CRACKED & DEFORMED & ONE EACH INSERT TORN. FABRICATED FLOOR PANEL 242 ZJ ON T15 1145454 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FRAMES 40-41) · corrosion level 2 · airframe 299 hrs · 15,899 cycles

MAIN DECK SEAT TRACK Y1456 CORRODED BETWEEN FRAMES 40 & 41. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-21. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 299 hrs · 15,899 cycles

CABIN FLOORBOARD 242 BF UPPER SURFACE HAS CRACKED. FABRICATED FLOOR PANEL 242 BF ON T15 1144627 IAW DWG SRZ 25-005 CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MDCC FLOOR PANEL 241BF MID & INBD EDGE HAS DENT. FABRICATED FLOOR PANEL 241BF ON T15 1144660 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MDCC FLOOR PANEL 241 KF UPPER SURFACE AFT & MID-SECTION HAS DENT WITH DELAMINATION. FABRICATED FLOOR PANEL 241 KF ON T15 1144721 IAW DWG SRZ 25-005 CAT A MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOOR PANEL 241CK HAS PUNCTURE. FABRICATED FLOOR PANEL 241CK ON T15 1144656 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MDCC FLOOR PANEL 241NJ UPPER SURFACE HAS GOUGE & DENT. FABRICATED FLOOR PANEL 241NJ ON T15 1144659 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 299 hrs · 15,899 cycles

CABIN FLOORBOARD 242KJ HAS A CRACKED. FABRICATED FLOOR PANEL 242KJ ON T15 1144728 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 299 hrs · 15,899 cycles

FLOORBOARD 241LK, HAD TWO POINTS TORN & HONEYCOMB EDGE ERODED. FABRICATED A NEW FLOORBOARD IAW DWG 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOOR PANEL 251VH CRACKED. FABRICATED FLOOR PANEL 251VH ON T15 1143904 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MDCC FLOOR PANEL 241BF MID & INBD EDGE HAS DENT. FABRICATED FLOOR PANEL 241BF ON T15 1144660 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MDCC FLOOR PANEL 241DF UPPER SURFACE HAS CRACKS & DENTS IN SEVERAL AREAS. FABRICATED FLOOR PANEL 241DF ON T15 1144658 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOOR PANEL 242MF WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MAIN DECK CARGO COMPARTMENT FLOOR PANEL 241FJ, ONE EACH HOLE INSERT MISSING & DELAMINATED. FABRICATED FLOOR PANEL 241FJ ON T15 1145453 IAW DWG SRZ 25-005 CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 299 hrs · 15,899 cycles

FLOORBOARD PANEL 242AJ, ONE EACH INSERT MISSING & ONE EACH CORNER EDGE ERODED. FABRICATED FLOOR PANEL 242AJ ON T15 1145458 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOOR PANEL 251QH CRACKED. FABRICATED FLOOR PANEL 251QH ON T15 1143906 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MDCC FLOOR PANEL 241BF MID & INBD EDGE HAS DENT. FABRICATED FLOOR PANEL 241BF ON T15 1144660 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 299 hrs · 15,899 cycles

CABIN FLOORBOARD 241 KJ UPPER SURFACE HAS CRACKS ON 2 LOCATIONS & BROKEN FROM SEAL. FABRICATED FLOOR PANEL 241 KJ ON T15 1144727 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MDCC FLOOR PANEL 241HF UPPER SURFACE WAS DENTED IN SEVERAL LOCATIONS. FABRICATED A NEW FLOOR PANEL IAW DWG 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MDCC FLOOR PANEL 241GK UPPER SURFACE PUNCTURE. FABRICATED FLOOR PANEL 241GK ON T15 1144764 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOOR PANEL 241 MH HAS PUNCTURE. FABRICATED FLOOR PANEL 241MH ON T15 1144653 IAW DWG SRZ 25-005 CAT A MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOOR PANEL 241HJ HAS PUNCTURED ON BOTTOM SURFACE. FABRICATED FLOOR PANEL 241HJ ON T15 1144726 IAW SRZ DWG 25-005, CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 299 hrs · 15,899 cycles

FLOORBOARD PANEL 241GJ, SEVERAL HONEYCOMB EDGES ERODED. FABRICATED FLOOR PANEL 241GJ ON T15 1144729 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOOR PANEL 252VH CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MDCC FLOOR PANEL 241VG, ONE EACH CORNER DAMAGED. FABRICATED FLOOR PANEL 241VG ON T15 1145460 IAW SRZ DWG 25-005, CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MDCC FLOOR PANEL 241LH UPPER SURFACE HAS DENT IN SEVERAL LOCATIONS. FABRICATED FLOOR PANEL 241LH ON T15 1144763 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MDCC FLOOR PANEL 242EJ HAS SEVERAL RUSTY INSERTS & SEVERAL MISSING. FABRICATED FLOOR PANEL 242EJ ON T15 1144955 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DEFORMED (ZONE 200) · airframe 299 hrs · 15,899 cycles

FLOORBOARD PANEL 242UJ, UPPER SURFACE SEVERAL AREAS DEFORMED. FABRICATED FLOOR PANEL 242UJ ON T15 1144625 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 299 hrs · 15,899 cycles

FLOORBOARD PANEL 241QF, TWO EACH CORNER INSERTS MISSING & ERODED. FABRICATED FLOOR PANEL 241QF ON T15 1144952 IAW DWG SRZ 25-005 CAT A MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 299 hrs · 15,899 cycles

FLOORBOARD PANEL 242EK UPPER & LOWER SURFACES HAS CRACKED. FABRICATED FLOOR PANEL 242EK ON T15 1144626 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN DECK) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOOR PANEL 241PF HAS PUNCTURED. FABRICATED FLOOR PANEL 241PF ON T15 1144654 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MDCC FLOOR PANEL 241BF MID & INBD EDGE HAS DENT. FABRICATED FLOOR PANEL 241BF ON T15 1144660 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 299 hrs · 15,899 cycles

FLOORBOARD PANEL 241UJ, SEVERAL HONEYCOMB EDGES MISSING & ERODED. FABRICATED FLOOR PANEL 241UJ ON T15 1144621 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MDCC FLOOR PANEL 241 EF HAS DELAMINATION, DAMAGED EDGE & PUNCTURED AT MID-SECTION. FABRICATED FLOOR PANEL 241EF ON T15 1144657 IAW DWG SRZ 25-005 CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 299 hrs · 15,899 cycles

FLOORBOARD PANEL 242HK, SEVERAL HONEYCOMB EDGES ERODED. FABRICATED FLOOR PANEL 242HK ON T15 1144730 IAW SRZ DWG 25-005. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 299 hrs · 15,899 cycles

FLOORBOARD PANEL 241 WH HONEY COMB EDGE MISSING & CRACKED. FABRICATED FLOOR PANEL 241 WH ON T15 1144622 IAW DWG SRZ 25-005 CAT A MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOOR PANEL 252 PH CRACKED. FABRICATED NEW FLOOR PANEL 252 PH ON T15 1144097 IAW DWG SRZ-25-005 REV L CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 299 hrs · 15,899 cycles

MAIN CABIN DECK FLOOR PANEL 252 VF CRACKED. FABRICATED NEW FLOOR PANEL 252 VF ON T15 1145461 IAW DWG SRZ-25-005 REV L CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOOR PANEL 251 GF HAS SEVERAL DAMAGED SCREW INSERTS. FABRICATED NEW FLOOR PANEL 252GF ON T15 1143907 IAW DWG SRZ-25-005, REV L CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOOR PANEL 252 YG CRACKED. FABRICATED NEW FLOOR PANEL 252 YG ON T15 11433903 IAW DWG SRZ-25-005 REV L CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOOR PANEL 252 GF CRACKED. FABRICATED NEW FLOOR PANEL 252 GF ON T15 1143908 IAW DWG SRZ-25-005 REV L CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 299 hrs · 15,899 cycles

COURIER AREA FLOOR PANEL 222NF HAS GOUGES & PUNCTURES. FABRICATED COURIER AREA FLOOR PANEL FX-R532B135700000 IAW DWG SRZ-25-005 ON TR 15 1143520 CATEGORY A MAJOR REPAIR.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOORBOARD 232WG UPPER SURFACE CRACKED. FABRICATED A NEW FLOORBOARD IAW DWG SRZ 25-005.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOORBOARD 232TG UPPER SURFACE FOUND CRACKED. A NEW FLOORBOARD WAS FABRICATED IAW DWG SRZ 25-005.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 299 hrs · 15,899 cycles

COURIER AREA FLOORBOARD 221 HF HAS GOUGES & PUNCTURES. FABRICATED COURIER AREA FLOOR PANEL 221 HF RX-R532B134900000 IAW SRZ 25-005 ON TRAVELER T15 1143541 CAT A MAJOR REPAIR.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOORBOARD 231HH HAS EDGE DAMAGE. FABRICATED NEW FLOORBOARD IAW DWG SRZ 25-005 REV L CLASSIFIED AS MAJOR CAT"A" REPAIR.

Part: FLOORBOARD — CRACKED (MAIN DECK) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOORBOARD 231YG UPPER SURFACE IS CRACKED. FABRICATED A NEW FLOORBOARD IAW DWG SRZ 25-00- REV L CLASIFIED AS CATAGORY "A" MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN DECK) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOOR PANEL 232NG CRACKED & DELAMINATING. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005 REV L.

Part: SEAT TRACK — CORRODED (MAIN DECK) · corrosion level 2 · airframe 299 hrs · 15,899 cycles

MAIN DECK SEAT TRACK Y2462 CORRODED FROM FRAME 18 TO SPLICE BETWEEN FRAME 20 & 21. R & R WITH A NEW SEAT TRACK IAW SRM 53-10-16.

Part: SEAT TRACK — CORRODED (MAIN DECK) · corrosion level 2 · airframe 299 hrs · 15,899 cycles

MAIN DECK SEAT TRACK FLANGES & WEBS BETWEEN Y1959 & Y2462, FRAMES 28 - 30, HAVE AREAS OF CORROSION. REPAIRED THE SEAT TRACK IAW SRM 53-10-16 FIG 201.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOORBOARD 231JG HAS EDGE DAMAGE. FABRICATED ANEW FLOORBOARD IAW DWG SRZ 25-005 REV L.

Part: FLOOR PANEL — PUNCTURED (MAIN DECK) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOOR PANEL 232HG PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005 REV L.

Part: SEAT TRACK — CORRODED (FRAMES 28-30) · corrosion level 2 · airframe 299 hrs · 15,899 cycles

MAIN DECK SEAT TRACK FLANGES BETWEEN Y1959 & Y1456, FRAMES 28 - 30 HAVE AREAS OF CORROSION. REPAIRED THE SEAT TRACK IAW SRM 53-10-16 FIG 201.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOORBOARD 231 AH UPPER SURFACE CRACKED. FABRICATED ON TRAVELER T15 1143759 IAW DWG SRZ 25-005. CLASSIFIED AS CAT A MAJOR REPAIR.

Part: FLOORBOARD — CRACKED (MAIN DECK) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOORBOARD 231VG FOUND CRACKED. FABRICATED A NEW FLOORBOARD IAW DWG SRZ 25-005.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOORBOARD 232UG HAS A DAMAGED FASTENER HOLE.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOOR PANEL 231 FH HAS EDGE DAMAGE. FABRICATED ON TRAVELER T15 1144091 IAW DWG SRZ 25-005. CLASSIFIED AS CAT A MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOOR PANEL 262 VF CRACKED. FABRICATED NEW FLOOR PANEL 262 VF ON TRAVELER T15 1143901 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN DECK) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOOR PANEL 232YG UPPER SURFACE FOUND CRACKED. A NEW FLOOR PANEL WAS FABRICATED IAW DWG SRZ 25-005.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOOR PANEL 231GH PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 299 hrs · 15,899 cycles

MAIN DECK FLOOR PANEL 232QG FOUND PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005.

Part: SEAT TRACK — DAMAGED (FRAME 54) · airframe 299 hrs · 15,899 cycles

MAIN DECK SEAT TRACK Y1959 SCALLOPS DAMAGED FR54.2 REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-21.

Part: SEAT TRACK — CORRODED (FRAMES 26-27) · corrosion level 2 · airframe 299 hrs · 15,899 cycles

CORROSION ON SEAT TRACK BETWEEN FRAMES 26 - 27 Y953. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM-53-10-16 FIG. 101, REMOVED AND REPLACED THE SEAT TRACK IAW SRM-53-10-16 PG. 207, FIG. 201. CAT"A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FRAMES 11-14) · airframe 299 hrs · 15,899 cycles

COURIER AREA FLOOR PANEL 221LF GOUGED AND PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW-DWG SRZ-25-005, CATAGORY "A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FRAMES 16-19) · airframe 299 hrs · 15,899 cycles

COURIER AREA FLOOR PANEL 222RF GOUGED AND PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005 CAT"A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FRAMES 14-15) · airframe 299 hrs · 15,899 cycles

COURIER AREA FLOOR PANEL 221 PF GOUGED AND PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005 CATAGORY "A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FRAME 13) · airframe 299 hrs · 15,899 cycles

FLOOR PANEL AT FRAME 13A AND BETWEEN FLOORBEAMS YE AND YD HAS EDGE DAMAGE. FABRICATED A NEW FLOOR PANEL IAW-DWG SRZ-25-005 CATEGORY "A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FRAMES 14-16) · airframe 299 hrs · 15,899 cycles

COURIER AREA FLOOR PANEL 222QF GOUGED AND PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005 CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FRAMES 16-19) · airframe 299 hrs · 15,899 cycles

COURIER AREA FLOOR PANEL 221RF GOUGED AND PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005 CATAGORY "A" MAJOR REPAIR.

Part: PROCESSING UNIT — FAILED · airframe 297 hrs · 15,747 cycles

AFTER TAKEOFF CAPTAIN ADC FAILED. AFTER TAKEOFF & AFTER SLAT RETRACTION 15/0 TAKEOFF GOT A SYS 1 FLAP FAULT. CYCLED THE SLATS & FLAPS 15. BOTH MOVED BUT FLAPS WERE SLOW. ON APPROACH PS 20 BOTH FLAP SYS 1 & 2 FAULTED & A FLAP 20 LANDING WAS MADE. PERFORMED ADJUSTMENT TEST ON CAPTAINS ADC NR 1. OPERATIONS CHECKED NORMAL. CHECK ADC NR 1 IAW TSM 31-10-00. . OPERATIONS NORMAL IAW MM 34-10-00-5. PERFORMED AFS & LAND TEST. ALL OPERATIONS NORMAL IAW MM 22-40-00-05. OK FOR SERVICE. BOTH SFCC REPLACED ALONG WITH THE FEEDBACK PPU. SYS OPERATIONS CHECKED NORMAL.

Part: GIMBAL JOINT — CONTAMINATED (TE FLAP) · airframe 28,900 hrs · 15,267 cycles

ON FINAL SELECTED FLAPS 20 & IMMEDIATELY GOT 2 FLAP SYS 1 & 2 FAULT LIGHTS. ELECTED TO GO AROUND & FOLLOWED ECAM & QRH PROCEDURES. AFTER LANDING, FLAP HANDLE SELECTED UP & THEY RETRACTED NORMALLY. FOUND TRACK 1 AND 2 GIMBLES ON BOTH WINGS WITH WATER UNDER HARD GREASE. PUMPED UNTIL CLEAN GREASE NOTED. SUSPECT WATER IN GIMBLE ASSY'S FREEZING IN FLIGHT. RAN SYSTEM AGAIN WITH NO DEFECTS NOTED AND NO FAULTS ON SFCC'S. A/C OK FOR CONTINUED SERVICE AT THIS TIME.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 28,872 hrs · 15,248 cycles

LEFT RIB 5 FWD LUG HAS CORROSION IN BORE & AFT SPOT FACE REPAIRED LT RIB 5 FWD LUG IAW DWG R57240425 ISSUE C & EA 6-5710-T0309453.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 28,872 hrs · 15,248 cycles

RIGHT RIB 5 FWD LUG HAS CORROSION IN BORE & IN FWD & AFT SPOT FACES. COMPLIED WITH EA 6-5710-T0309480 P-1 WING BASIC WING STRUCTURE RT RIB 5 FWD LUG CORROSION.

Part: TRANSMITTER — LEAKING (HYDRAULIC SYS) · airframe 28,814 hrs · 15,209 cycles

HYDRAULIC SYS BLUE LO PRESS IN FLT, COMPLIED WITH QRH. FOUND HYDRO FLUID LEAKING FROM AFT LT WW AREA. TROUBLESHOOTING IN PROGRESS TO ISOLATE. CREW REPORTED BLUE PUMP WAS TURNED OFF 30 SECONDS AFTER LOW PRESS INDICATION. BLUE HYD QTY IS JUST INSIDE THE BOTTOM OF THE GREEN BAND BY ABOUT 1/8". LEAK IS COMING FROM A PRESS TRANSMITTER MOUNTED ON THE PRIORITY VLV MANF ASSEMBLY FIN 2064. REPLACED PRESS TRANSMITTER 12WV IAW AMM 29-32-13-04. OPERATIONS & LEAK CHECKED GOOD. RAN ENGS & PERFORMED BLEED PROCEDURE IAW AMM 29-00-00-04. BLUE SYS FAILS STEP 2 B 2. NEEDLE IS NOT SUPPOSED TO MOVE MORE THE .40 GAL & WE ARE GETTING 1 GALLON PLUS. ACCOMPLISHED BLEED PROCEDURE SEVERAL MORE TIMES IAW AMM 29-00-00-04. ALL INDICATIONS NORMAL.

Part: SPRING — FAILED (DOOR UPLOCK) · airframe 28,338 hrs · 14,941 cycles

AFTER TAKEOFF, NOSE GEAR DOOR DID NOT CLOSE. BOTH SYSTEMS SHOWED DOOR UNSAFE, FOLLOWED ECAM. FOUND DOOR UPLOCK HOOK RETURN SPRINGS FOR LT NLG MAIN DOOR BOTH FAILED. R & R LT UP LOCK ASSEMBLY IAW MM 32-31-14-04. ACFT OK FOR SERVICE.

Part: SPRING — FAILED (DOOR UPLOCK) · airframe 28,338 hrs · 14,941 cycles

AFTER TAKEOFF, NOSE GEAR DOOR DID NOT CLOSE. BOTH SYSTEMS SHOWED DOOR UNSAFE, FOLLOWED ECAM. FOUND DOOR UPLOCK HOOK RETURN SPRINGS FOR LT NLG MAIN DOOR FAILED. R & R LT UPLOCK ASSEMBLY IAW MM 32-31-14-04.

Part: SPAR — CRACKED (ZONE 600) · airframe 27,585 hrs · 14,522 cycles

DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION IAW EO 6-5710-7-3305, PART 4, STEP 11 OF HOLE 'C' AT RT WING REAR SPAR FOUND CRACK INDICATION AT 6 O'CLOCK TOWARDS AFT. REPAIRED IAW EA 6-5710-T0300640 REV A, P1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.

Part: FRAME — MISREPAIRED (ZONE 100) · airframe 27,585 hrs · 14,522 cycles

FORWARD CARGO COMPARTMENT DOOR CUT OUT AT FRAME 20A BETWEEN STRINGER 37 AND 41 RT MISREPAIRED. REPAIRED IAW DWG 13 R53706085, ISSUE C. REPAIR CLASSIFIED MAJOR IAW GMM6-2-100, REV 116.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 27,585 hrs · 14,522 cycles

RT WING T/E CENTER FLAP UPPER SURFACE BETWEEN RIB 12 AND RIB 13 MISREPAIRED. REPAIRED IAW EA 6-5750-167168. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 27,585 hrs · 14,522 cycles

MAIN DECK FWD UTILITY AREA LT DOORWAY FLOOR PANEL 221QF FOUND DELAMINATED. FLOOR PANEL FABRICATED IAW DWG SRZ-25-005 REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM6-2-100, REV 116. FLOOR PANEL R & R AMM 53-10-25, REV 55.2.

Part: MOUNT — CORRODED (NR 2 ENGINE) · airframe 27,585 hrs · 14,522 cycles

NR 2 ENGINE PYLON FWD ENGINE MOUNT FITTING MATING SURFACE FOUND RUST. REWORKED IAW SRM 54-51-81, CONFIG 2, FIGURE 104, REV 23. REPAIR ACCOMPLISHED IAW EA 6-5450-167628 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 116.

Part: MOUNT — CORRODED (NR 2 ENGINE) · airframe 27,585 hrs · 14,522 cycles

NR 2 ENGINE PYLON FWD ENGINE MOUNT FITTING AFT INBD BOLT HOLE SPOT FACE FOUND RUST. REWORKED IAW SRM 54-51-81 CONFIG 2, FIG 104, REV 23. REPAIR ACCOMPLISHED IAW EA 6-5450-167628, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 116.

Part: MOUNT — CORRODED (NR 2 ENGINE) · airframe 27,585 hrs · 14,522 cycles

NR 2 ENGINE PYLON FORWARD ENGINE MOUNT FITTING AFT OTBD BOLT HOLE SPOT FACE FOUND RUST. REWORKED AND FOUND WITH LIMITS IAW SRM 54-51-81, CONFIG 2, FIG 104, REV 23. REPAIR ACCOMPLISHED IAW EA NR 6-5450-167628, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 27,585 hrs · 14,522 cycles

AIR CONDITIONING COMPARTMENT FWD LT FLOOR PANEL FOUND DELAMINATED. REMOVED FLOOR PANEL AND INSTALLED IAW AMM 20-21-12, REV 55.2 , NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005 REVISION J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116 .

Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 27,585 hrs · 14,522 cycles

MAIN DECK CARGO COMPARTMENT CROSSBEAM FOUND CRACKED AT STATION FRAME 31 BETWEEN SEAT TRACK Y1456 AND Y1959. CRACKED CROSSBEAM REPAIRED IAW SRM 53-10-15, FIG 212, REV 23 AND EA 6-5310-T0300636. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: SEAT TRACK — MISREPAIRED (ZONE 200) · airframe 27,585 hrs · 14,522 cycles

SEAT TRACK AT MAIN DECK BETWEEN FRAME 29 AND FRAME 30, Y =0 MISREPAIRED. REPAIRED IAW SRM 51-40-21, REV 23 & SRM 53-10-16, FIG 201, REV 23. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: SEAT TRACK — MISREPAIRED (ZONE 200) · airframe 27,585 hrs · 14,522 cycles

MAIN DECK CARGO TRACK -Y450, BETWEEN FRAME 32 AND 33 MISREPAIRED. REPAIRED IAW SRM 53-10-16, FIG 201, REV 23. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 27,585 hrs · 14,522 cycles

MAIN DECK CARGO BAY CROSSBEAM FOUND CRACKED AT STATION FRAME 30 BETWEEN SEAT TRACK Y1456 AND Y1959. ACCOMPLISHED REPAIR AS IAW SRM 53-10-15, FIG 212 AND EA 6-5310-T0 300636 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: CARGO TRACK — CORRODED (ZONE 200) · airframe 27,585 hrs · 14,522 cycles

MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT Y1456, BETWEEN FRAME 53 AND FRAME 54, FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-10, REV 23. FOUND OUT OF LIMIT IAW SRM 53-10-16, FIG 102, REV 23. DAMAGED CARGO TRACK REMOVED IAW SRM 51-40-21, REV 23. NEW CARGO INSTALLED IAW SRM 51-40-21, REV 23. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: CARGO TRACK — CORRODED (ZONE 200) · airframe 27,585 hrs · 14,522 cycles

MAIN DECK CARGO TRACK AT Y450, BETWEEN FRAME 52 AND FRAME 53, FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT IAW SRM 53-10-16, FIG 102, REV 23. R & R IAW SRM 51-40-21, REV 23. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: SEAT TRACK — MISREPAIRED (ZONE 200) · airframe 27,585 hrs · 14,522 cycles

MAIN DECK CARGO SEAT TRACK BETWEEN FRAME 32 AND 33, -Y953 MISREPAIRED. REPAIRED IAW SRM 53-10-16, FIG 202, REV 23. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: CROSSBEAM — MISREPAIRED (ZONE 200) · airframe 27,585 hrs · 14,522 cycles

MAIN DECK CARGO COMPARTMENT CROSSBEAM, FRAME 30 BETWEEN -Y450 AND -Y953 MISREPAIRED. REPAIR CARRIED OUT IAW EA 6-5310-167620. REPAIR CLASSIFIED AS MAJOR GMM 6-2-100, REV 116.

Part: CROSSBEAM — MISREPAIRED (ZONE 200) · airframe 27,585 hrs · 14,522 cycles

MAIN DECK CARGO CROSSBEAM, FRAME 30 BETWEEN Y450 AND Y953 MISREPAIRED. REPAIRED IAW SRM 53-10-15, FIG 212, REV 23. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116. EO 6-5100-7-5000D, PART 1.

Part: CROSSBEAM — MISREPAIRED (ZONE 200) · airframe 27,585 hrs · 14,522 cycles

MAIN DECK CARGO COMPARTMENT CROSSBEAM, FRAME 27 BETWEEN -Y450 AND -Y953 MISREPAIRED. REPAIR CARRIED OUT IAW EA 6-5310-167620. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: SEAT TRACK — MISREPAIRED (ZONE 200) · airframe 27,585 hrs · 14,522 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN FRAME 33 AND FRAME 34, -Y953 MISREPAIRED. REPAIRED IAW SRM 53-10-16, FIG 202, REV 23. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: CROSSBEAM — MISREPAIRED (ZONE 200) · airframe 27,585 hrs · 14,522 cycles

MAIN DECK CARGO COMPARTMENT CROSSBEAM, FRAME 29 BETWEEN -Y450 AND -Y953 MISREPAIRED. REPAIR CARRIED OUT IAW EA 6-5310-167620. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: CROSSBEAM — MISREPAIRED (ZONE 100) · airframe 27,585 hrs · 14,522 cycles

MAIN DECK CARGO COMPARTMENT CROSSBEAM 28 BETWEEN-Y450 AND-Y953 MISREPAIRED. CARRIED OUT REPAIR IAW EA NR 6-5310-167620.

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 27,585 hrs · 14,522 cycles

FUSELAGE SKIN FRAME 85 TO FRAME 86, BETWEEN STRINGER 13-15R. REPAIRED IAW SRM 53-10-12, FIG 208 AND 51-40-44, REV 23. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116. EO 6-5100-7-5000D PART 1.

Part: SEAT TRACK — MISREPAIRED (ZONE 200) · airframe 27,585 hrs · 14,522 cycles

SEAT TRACK BETWEEN FRAME 74 AND FRAME 76, Y =0 MISREPAIRED. REPAIRED IAW SRM 53-10-16, FIG 201, REV 23. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 27,585 hrs · 14,522 cycles

FUSELAGE SKIN FRAME 77 TO FRAME 78, BETWEEN STRINGER 39 - 43R MISREPAIRED. REPAIRED IAW SRM 53-10-12, FIG 208, SHEET 1, REV 23. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116. EO 6-5100-7-5000D, PART 1,

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 26,668 hrs · 14,038 cycles

MAIN DECK CARGO FLOORBOARD 231DH BETWEEN FR 19 & FR 21 SEAT TRACK 3 L & 4L HAS 15 " X1' AREA OF DAMAGE ON UPPER SURFACE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.

Part: OUTFLOW VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 24,924 hrs · 13,032 cycles

DURING CLIMBOUT PASSING 10,000 FT, CABIN PRESS REG 1 FAULTED, COMPLIED WITH ECAM AND TURNED IT OFF. 1 MINUTE LATER, CABIN PRESS REG 2 FAULTED AND WE WERE IN MAN PRESSURE. IT APPEARED THAT THE AFT OUTFLOW VALVE WAS NOT PROGRAMMING PROPERLY.

Part: SKIN — CRACKED (ZONE 600) · airframe 24,781 hrs · 12,953 cycles

RT WING LOWER SKIN JUST IN FRONT AND OTBD EDGE OF ACCESS DOOR NR 675FB FOUND INTERIOR SUPPORT STIFFENER CRACKED. REPAIRED AS PER E.A. 6-5710-143870 PART 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 112.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 24,781 hrs · 12,953 cycles

RT WING INBD FLAP, T/E OF RIB 25A, 02 EA HOLES FOUND CRACKED INDICATION DURING HIGH FREQUENCY EDDY CURRENT INSP. CRACKED RIB 25A AT RT WING INBD FLAP R & R IAW SRM 51-40-21, REV 19. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 112.

Part: RIB — CRACKED (LT WING TE FLAP) · airframe 24,781 hrs · 12,953 cycles

LT WING INBD FLAP, T/E OF RIB 25A, 03 EA HOLES FOUND CRACKED INDICATION DURING HIGH FREQUENCY EDDY CURRENT INSP. CRACKED RIB 25A AT LT WING INBD FLAP R & R IAW SRM 51-40-21, REV 19. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 112.

Part: CROSSBEAM — DAMAGED (ZONE 100) · airframe 24,781 hrs · 12,953 cycles

FORWARD CARGO COMPARTMENT AT FRAME 32 CROSS BEAM BETWEEN LONGERON 3 AND 4 FOUND 04 FASTENERS MISSING. FASTENERS INSTALLED AS PER E.A. 6-5310-92946, PART 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 111.

Part: SKIN — CRACKED (ZONE 600) · airframe 24,781 hrs · 12,953 cycles

RT WING FIXED L/E SKIN UPPER CUTOUT FOR NR 2 SLAT INBD JACKSCREW, FOUND CRACKED. REPAIRED AS PER SRM 57-41-12 FIGURE 203, REVISION 19. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 112. REPAIR CLASSIFIED CATEGORY B. TO PERFORMED DETAILED VISUAL INSPECTION. INITIAL INSPECTION AT 12,000 FLIGHT CYCLES AND SUBSEQUENT INSPECTIONS AT INTERVALS OF 4,000 FLIGHT CYCLES AS PER SRM 57-41-12 TABLE 202, REVISION, 19 AND SRI 57-41-12 TABLE 203, REVISION 19.

Part: SKIN — CRACKED (LT WING) · airframe 24,781 hrs · 12,953 cycles

LT WING LOWER SKIN PANEL INBD OF RIB 9 OF REAR SPAR NEAR ACCESS PANEL 575FE FOUND CRACKED APPROX 0.375 IN LONG DURING HIGH FREQUENCY EDDY CURRENT INSP. REPAIRED AS PER EA 6-5710-143871 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 112.

Part: SKIN — CRACKED (ZONE 600) · airframe 24,781 hrs · 12,953 cycles

RT WING LOWER SKIN PANEL INBD OF RIB 9 OF REAR SPAR NEAR ACCESS PANEL 675FE FOUND CRACKED, APPROX 0.250 INCH LONG DURING HIGH FREQUENCY EDDY CURRENT INSPECTION. REPAIRED AS PER EA 6-5710-143870 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 112.

Part: FRAME — CRACKED (ZONE 200) · airframe 24,781 hrs · 12,953 cycles

CABIN RT SIDE FRAME 42 HOLE "B" FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP THROUGH WORK CARD E6-5310-7-5006A2, PT2. REPAIR CARRIED IAW EO NR E6 -5310 -7- 5006A2, PT2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: ATTACH FITTING — CRACKED (ZONE 100) · airframe 24,781 hrs · 12,953 cycles

AFT CARGO COMPARTMENT DOOR ACTUATOR ATTACH FITTING AT FRAME 61A FOUND APPROX 1.2 IN LENGTH CRACKED DURING HIGH FREQUENCY EDDY CURRENT INSP. R & R IAW SRM 51-40-21, REV 19. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: PROXIMITY SENSOR — MALFUNCTIONED (MLG) · airframe 23,986 hrs · 12,505 cycles

LANDING GEAR HANDLE WOULD NOT RAISE BEYOND NEUTRAL ON POSITION DETECTOR SYSTEM 2. SYSTEM 1 WAS DEFERRED. RETURN TO LAND ACCOMPLISHED. R & R 55GB PROX SENSOR IAW 32-00-00-4. NO HELP. OHMD WIRES FROM PDU TO 55GB. ALL WIRES CHECKED GOOD. SWAPPED 55GB AND 82GB PROX SENSORS CONNECTORS. NOW GEAR WOULD SWING IN EITHER 1 OR 2 POSITION. RE INSTALLED IN ORG POSITION. PER TSM CHECKED RIG BETWEEN PROX SENSOR 55GB, 82GB AND TARGETS. RIG WAS WITHIN MM LIMITS AT THE HIGH END OF THE RANGE. REF: MM 32-00-00-04. AS NO OTHER FAULTS FOUND, RE-RIGGED PROX SENSORS 55GB AND 82GB TO THE MIDDLE OF THE LIMIT IN THE MM. PREFORMED A GEAR SWING IAW 32-31-00. SYS 1 AND 2 OP CK'D NORMAL.

Part: ENGINE — FAILED (APU) · airframe 22,614 hrs · 11,766 cycles

APU AUTO SHUTDOWN IN FLIGHT. APU OIL QUANTITY SHOWS "0". NR 2 IDG WAS ON MEL AT THE TIME APU FAILED. SERVICED APU OIL IAW MM 12-13-49-0. OPS CHECKED APU IAW JRH. OPS CHECKED NORMAL.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,511 hrs · 11,152 cycles

MDCC SEAT TRACK NR 1 HAS 3 AREAS OF CORROSION BETWEEN FR 74 AND 8 IN AFT OF FR 76 REMOVED LEVEL 1 CORROSION FROM NR 1. REMOVED DAMAGED SECTION OF SEAT TRACK AND INSTALLED SEAT TRACK SPLICE REPAIR BETWEEN FR 74 AND FR 77 IAW A300-600 SRM 53-10-16, FIG 208, PAGE 247/248.

Part: SMOKE DETECTOR — MALFUNCTIONED (E/E BAY) · airframe 19,542 hrs · 10,113 cycles

CLIMB-OUT APPROACHING 2000' , CRC ECAM FLASHED FOR MIN EQUIP BAY SMOKE. SMOKE LIGHT CAME ON AND LIGHT EXTINGUISHED IN A FEW SECONDS. MIN EQUIP BAY SNIFFER CHECK, NEGATIVE. PASSED 11,000' SAME HAPPENED AGAIN, LIGHT STAYED ON. SNIFFER CHECK WAS NEGATIVE. DECLARED EMERG, RAN CHKLISTS AND CAME BACK. LIGHT EXTINGUISHED AGAIN, DON'T KNOW WHEN. REMOVED AND REPLACED SMOKE DETECTOR 12WA; OPS CK OK. PREMATURE REMOVAL/INSTALLATION OFF MFG CG7G0-11, POS AV2 SRL AB1227,TAG 390B62, ON MFG CG7G0-11, SRL 144, TAG 6565A4. REMOVED AND REPLACED LEFT AND RIGHT COALESCER BAGS PRECAUTIONARY.

Part: SKIN — DENTED (T/E FLAP) · airframe 18,338 hrs · 9,423 cycles

LEFT WING INBOARD FLAP UPPER SURFACE HAS CHAFED AND DENTS (THREE AREAS).

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,338 hrs · 9,423 cycles

FOUND MAIN CARGO DECK SEAT TRACK CORRODED AT FRAME 28 LBL97 AFT OF CARGO DOOR.

Part: FRAME — DENTED (FUSELAGE) · airframe 18,338 hrs · 9,423 cycles

FOUND FRAME 22 RT DENTED AT STRINGER 15R.

Part: FRAME — DENTED (FUSELAGE) · airframe 18,338 hrs · 9,423 cycles

FOUND FRAME 24RH DENTED AT STRINGER 15R.

Part: SKIN PANEL — DENTED (T/E FLAP) · airframe 18,338 hrs · 9,423 cycles

FOUND LEFT WING INBOARD FLAP LOWER SURFACE HAS SEVERAL DENTS (TRAILING EDGE).

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 18,338 hrs · 9,423 cycles

FOUND RIGHT LOWER ELEVATOR O/B AREA HAS A CRACK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,338 hrs · 9,423 cycles

MAIN CARGO DECK SEAT TRACK CORRODED BETWEEN FRAME 50-51, BL 0.

Part: SEAT TRACK — OUT OF LIMITS (FUSELAGE) · airframe 18,338 hrs · 9,423 cycles

FOUND MAIN DECK CARGO SEAT TRACK CORRODED FR 50 RBL17.

Part: REGULATOR — OBSTRUCTED (LT AILERONS) · airframe 18,200 hrs · 9,345 cycles

AFTER TAKEOFF COULD NOT TURN AIRCRAFT TO LEFT MANUALLY WITH YOKE. TURN RIGHT NORMALLY, ENGAGED AUTOPILOT WITH 15 DEGREE BANK AND AIRCRAFT TURNED WHAT SEEMED TO BE NORMAL TO LEFT WITH AUTOPILOT ON. AFTER LANDING CONTROL STILL JAMMED TO LEFT. NOTE NORMAL FLIGHT CONTROL CHECK PRIOR TO FLIGHT. PERFORMED DETAILED VISUAL INSPECTION OF LEFT HAND AILERON TENSION REGULATOR AND SURROUNDING AREAS. FOUND AND REMOVED SMALL BOLT HAD LODGED IN THE LEFT HAND AILERON TENSION REGULATOR.

Part: SOCKET — LEAKING (HYD SOLENOID CON) · airframe 17,387 hrs · 8,908 cycles

EN ROUTE AT FL330 RECEIVED ECAM FOR GREEN SYSTEM HYDRAULIC RESV LO. COMPLIED WITH ECAM AND DESELECTED GREEN PUMPS. AFTER NR 1 GREEN PUMP DESELECTED, ENGINE NR 1 GREEN PUMP C/B POPPED AND WOULD NOT ALLOW NR 1 GREEN PUMP TO BE DESELECTED. REFERENCE A300-600 AMM 29-00-00-3 GREEN HYDRAULIC QUANTITY WAS 4 GALS IN WHEEL WELL AT RESERVOIR. PERFORMED INSPECTION OF GREEN SYSTEM. PERFORMED TEST IAW A300-600 AMM 29-11-32, P. BLOCK 401. FOUND NR 1 ENGINE DEPRESS SOLENOID CONNECTOR SOCKET LOOSE ON SOLENOID ASSY. REMOVED AND REPLACED DEPRESSURIZING VALVE IAW MM SUP 29-11-32-4. OP'S CHECKS NORMAL AT THIS TIME. NO LEAKS NOTED, SEE 29-10/9080.

Part: PROXIMITY SENSOR — MALFUNCTIONED (PITCH TRIM) · airframe 17,313 hrs · 8,868 cycles

ON DEPARTURE KMEM GEAR WOULD NOT RETRACK IN SYSTEM 2 PITCH TRIM TRIPPED OFF, ATS TRIPPED OFF BOTH WOULD NOT RESET. FLIGHT DIRECTOR INOP, A/P INOP, RETURN TO MEM. NOSE GEAR TORQUE LINK PROX DETECTOR 55GB HAD IMPACT DAMAGE REMOVED AND TEMP INSTALLED THE DETECTOR, THE W/U WAS FOR THE NR 2 SYS 55GB IS NR 1 SYS. NO DEF 82 GB INSTALLED 55GB SENSOR, ALSO REMOVED AND REPLACED 82GB FOR SYS NR 2. BOTH W/I LIMITS, NO ADJUSTMENT MADE, REF A300-600 M/M 32-00-0 0-4. SWUNG NOSE GEAR SEVERAL TIMES WITH NO FAULTS IN PROX BOX.

Part: FASTENER — MISSING (AILERON TRIM) · airframe 17,151 hrs · 8,778 cycles

PASSING 5500FT MSL AND LEVELING AT 6000 FT, HAND FLYING USING AUTO THROTTLES, ATTEMPTED TO TRIM AIRCRAFT MANUALLY WITH TRIM BUTTON ON YOKE. DURING TRIM A VIBRATION WAS FELT ON THE A/C. NEEDED MORE TRIM TO LEVEL, AGAIN VIBRATION OCCURRED DURING TRIMMING, 250 KTS, 6000 FT MSL, CG 27.8 PERCENT, AUTOTHROTTLES ON & ENGINES NEAR IDLE. INSPECTED TRIMMABLE HORIZONTAL STABILIZER. ON STABILIZER APRON, FOUND ON BOTH SIDES BOTTOM HALF SEVERAL FINGER SKIRTS MISSING RIVETS (55-10/8938). FOUND MANY PIECES OF PAPER WEDGE IN AND AROUND PITCH TRIM CONTROL WHEEL CHAIN. REMOVED ALL DEBRIS. PERFORMED ADJ/TEST PER MM 22-27-00-5 OP'S

Part: WARNING LIGHT — ILLUMINATED (SMOKE ALERT) · airframe 16,113 hrs · 8,214 cycles

TOOK OFF OUT OF KMEM AND AT 1800 FT, A MIN EQUIP SMOKE ALERT WARNING ECAM INDICATION. REQUESTED TO LAND ASAP ALERT WAS CONFIRMED, QRH COMPLIED, NO EVIDENCE OF SMOKE ALERT STAYED UNTIL SHORT FINAL FOR RWY 18L ON SHORT FINAL ALERT WENT AWAY FOLLOWED BY SLATS/FLAPS FAULT LIGHT. LANDED WITH SLATS/FLAPS 15/20. REMOVED AND REPLACED AVIONICS MIN. EQUIPMENT SMOKE DETECTOR IAW A-300 MM26-15-12-4.OP'S TEST GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MDCC 4TH SEAT TRACK RT SIDE FROM CENTER LINE AT FR 27 HAS 1 EA AREA OF CORROSION. REMOVED AND REPLACED DAMAGED SECTION IAW A300-600 SRM 53-10-16 FIG 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

3RD SEAT TRACK FROM CENTERLINE JUST FWD OF FR 27 ONE EA AREA OF SURFACE CORROSION UPPER SURFACE. REPAIRED SEAT TRACK 3 LT FR 26-27 TO FR 27-28 AE PER A300-600 FREIGHTER SRM 53-10-16 PARA 4 FIG 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

4TH SEAT TRACK RT SIDE FROM CENTER LINE AT FR 27 HAS 1 EA AREA OF CORROSION. REMOVED AND REPLACED DAMAGED SECTION IAW A300-600 SRM 53-10-16 FIG 201

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

N01236 MDCC LT SIDE BETWEEN SEAT TRACK 3 AND 4 FROM CENTER LINE AT FR 27 FLOOR PANEL HAS 2 EA AREAS OF CORROSION UPPER SURFACE. REMOVED AND REPLACED THRUST BRACKET IAW A300-600 SRM 51-72-10

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MDCC 5TH SEAT TRACK FROM CENTERLINE RT SIDE BETWEEN FR 26 AND FR 27 1 EA AREA OF CORROSION CLEANED OUT CORROSION, FOUND TO BE OUT OF LIMITS, AND REPAIRED SEAT TRACK IAW A300-600 SRM 53-10-16

Part: BRACKET — CORRODED (FUSELAGE) · airframe 15,305 hrs · 7,731 cycles

FLOOR PAN PANEL BETWEEN RT SIDE OF 3 AND 4 SEAT TRACK AT FR 27 HAS FOUR EACH AREAS OF CORROSION UPPER SURFACE CLEANED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THRUST PLATE IAW A300-600 SRM 51-72-10

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MDCC FLOOR PAN PANEL BETWEEN SEAT TRACKS 1 AND 2 RT OF CENTERLINE FR 25 HAS CORROSION. REMOVED AND REPLACED THRUST BRACKET IAW A300-600 SRM 51-72-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MDCC LT SIDE NR 4 SEAT TRACK FROM CENTER LINE JUST FWD OF FR 27, 2 EA AREAS OF CORROSION, UPPER SURFACE. REPAIRED SEAT TRACK NR 4 LEFT FROM FR 26-27 TO FR 27-28 IAW A300-600 FREIGHTER SRM 53-10-16 FIG 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MDCC 5TH SEAT TRACK FROM CENTERLINE RT SIDE BETWEEN FR 26 AND FR 27 1 EA AREA OF CORROSION. CLEANED OUT CORROSION, FOUND TO BE OUT OF LIMITS, AND REPAIRED SEAT TRACK IAW A300-600 SRM 53-10-16.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

N01279 MDCC FLOOR PAN PANEL BETWEEN SEAT TRACKS 1 AND 2 RT OF CENTERLINE FR 25 HAS CORROSION. REMOVED AND REPLACED THRUST BRACKET IAW A300-600 SRM 51-72-10

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MAIN CABIN FR 41 UP TO FR 44, NR 4 RT SEAT TRACK NOTED CORROSIONS ON FOUR AREAS AS MARKED REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 51-72-10 AND 51-40-21

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MDCC FLOOR PAN PANEL BETWEEN RT SIDE OF 3 AND 4 SEAT TRACK AT FR 27 HAS FOUR EACH AREAS OF CORROSION UPPER SURFACE. CLEANED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THRUST PLATE IAW A300-600 SRM 51-72-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MAIN CABIN FR 41 UP TO FR 44, NR 4 RIGHT SEAT TRACK NOTED CORROSIONS ON FOUR AREAS AS MARKED. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 51-72-10 AND 51-40-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MDCC 3RD SEAT TRACK FROM CENTERLINE JUST FWD OF FR 27 ONE EA AREA OF SURFACE CORROSION UPPER SURFACE. REPAIRED SEAT TRACK 3 LEFT FR 26-27 TO FR 27-28 AE PER A300-600 FREIGHTER SRM 53-10-16 PARA 4 FIG 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MAIN DECK CARGO COMPARTMENT, LT SIDE BETWEEN SEAT TRACK 3 AND 4 FROM CENTERLINE AT FR 27 FLOOR PAN PANEL HAS 2 EA AREAS OF CORROSION UPPER SURFACE. REMOVED AND REPLACED THRUST BRACKET IAW A300-600 SRM 51-72-10.

Part: SEAT TRACK — CORRODED (FUSEAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MDCC LT SIDE NR 4 SEAT TRACK FROM CENTER LINE JUST FWD OF FR 27, 2 EA AREAS OF CORROSION, UPPER SURFACE. REPAIRED SEAT TRACK NR 4 LT FROM FR 26-27 TO FR 27-28 IAW A300-600 FREIGHTER SRM 53- 10-16 FIG 201

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MDCC FLOOR PAN PANEL BETWEEN 3 AND SEAT TRACK 4 AT FR 26 RT SIDE HAS 3 EA AREAS OF CORROSION UPPER SURFACE. REMOVED AND REPLACED THRUST PLATE IAW A300-600 SRM 51-72-10.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

N01291 MDCC FLOOR PAN PANEL BETWEEN 3 AND SEAT TRACK 4 AT FR 26 RT SIDE HAS 3 EA AREAS OF CORROSION UPPER SURFACE. REMOVED AND REPLACED THRUST PLATE IAW A300-600 SRM 51-72-10

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 15,305 hrs · 7,731 cycles

A 2 INCH CRACK ON INBOARD FLANGE LEFT NR 2 SEAT TRACK FWD OF FRAME 30, MAIN CABIN. REMOVED DAMAGED SECTION OF SEAT TRACK IAW A300-600 SRM 53-10-16. LOCATED AND DRILLED NEW SEAT TRACK SECTION IAW A300-600 SRM 53-10-16. ALODINE, PRIMED AND TOP COATED NEW SEAT TRACK SECTION IAW A300-600 SRM 51-20-23. INSTALLED NEW SEAT TRACK SECTION IAW A300-600 SRM 53-10-16. TOP COATED FASTENERS IAW A300-600 SRM 51-20-23.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

TWO AREAS OF CORROSION ON SUBFLOOR AFT OF FRAME 28 BETWEEN SEAT TRACKS 3L AND 4L, MAIN CABIN. REMOVED AND REPLACED THRUST BRACKET IAW A300-600 SRM 51-72-10.

Part: BRACKET — CORRODED (SUBFLOOR) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

TWO AREAS OF CORROSION ON SUBFLOOR AFT OF FRAME 28 BETWEEN SEAT TRACKS 3L AND 4L, MAIN CABIN. REMOVED AND REPLACED THRUST BRACAKET IAW A300-600 SRM 51-72-10.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 15,305 hrs · 7,731 cycles

A 2 INCH CRACK ON INBOARD FLANGE LEFT NR 2 SEAT TRACK FWD OF FRAME 30, MAIN CABIN. REMOVED DAMAGED SECTION OF SEAT TRACK IAW A300-600 SRM 53-10-16. LOCATED AND DRILLED NEW SEAT TRACK SECTION IAW A300-600 SRM 53-10-16. ALODINED, PRIMED AND TOP COATED NEW SEAT TRACK SECTION IAW A300-600 SRM 51-20-23. INSTALLED NEW SEAT TRACK SECTION IAW A300-600 SRM 53-10-16. TOP COATED FASTENERS IAW A300-600 SRM 51-20-23.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MDCC FLOOR PAN BETWEEN TRACKS 2 & 3 RT FR 27 HAS 2 EA AREAS OF CORROSION. REMOVED AND REPLACED THRUST BRACKET IAW A300-600 SRM 51-72-10 AND 51-40-21.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MDCC FLOOR PAN BETWEEN TRACKS 2 & 3 RT FR 26 HAS 1 AREA OF CORROSION. REMOVED AND REPLACED THRUST BRACKET IAW A300-600 SRM 51-72-10 AND 51-40-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

FIVE AREAS OF CORROSION ON SEAT TRACK FLANGE SEAT TRACK 1L BETWEEN FRAMES 26-28. REPAIRED SEAT TRACK IAW A300-600 FREIGHTER SRM 53-10-16 FIG 201 WITH SPLICE REPAIR BETWEEN FRAMES 26.5 TO 29.5.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MAIN CARGO DECK LEFT TRACK 5 HAS 8 EA AREAS OF CORROSION, 8 INCHES AFT OF FR 48, FR 49, 6 INCHES FWD OF FR 50, JUST FWD OF FR 51, JUST AFT OF FR 51, FWD OF FR 52, FR 53, FR 54. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IN AREAS 1-4. REMOVED AND REPLACED SEAT TRACK SECTION IAW A300-600 SRM 53-10-16 BETWEEN FRAMES 48-51, BURNISHED AND TREATED DISCREPANCIES IN OTHER NOTED AREAS.

Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

METAL PNL AT NR 4 LEFT AND 5 LEFT SEAT TRACK BETWEEN C30 AND 31 HAS 4EA AREA'S OF CORROSION. REMOVED ANGLE FROM OLD THRUST PLATE AND INSTALLED ON NEW THRUST PLATE IAW A300-600 SRM 51-72-10 AND 51-40-30 AND INSTALLED NEW THRUST PLATE IAW A300-600 SRM 51-72-10 AND 51-40-21.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MAIN DECK CARGO COMP BETWEEN 3 AND 4 SEAT TRACK FROM CENTER LINE, FLOOR PLATE PANEL HAS 3EA AREA OF CORROSION BETWEEN FR25 AND FR26. BLENDED OUT COROSION FOUND TO BE OUT OF LIMITS IWA A300-600 SRM 51-74-10 AND 53-10-00. REMOVED THRUST PLATE AND REINSTALLED OLD ANGLE FROM PLATE AND RE-INSTALLED ON NEW PLATE IAW A300-600 SRM 51-72-10 AND 51-40-21, AND INSTALLED NEW THRUST PLATE IAW A300-600 SRM 51-72-10 ABD 51-40-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MAIN DECK CARGO COMP, 1ST SEAT TRACK FROM CENTER LINE RT SIDE BETWEEN FRAME 74 AND 75, 2 AREAS OF CORROSION UPPER SURFACE. CLEANED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED SEAT TRACK SECTION PER A300-600 SRM 53-10-16 AND 51-40-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MAIN CABIN FR 40 TO 42 NR 3 RIGHT SEAT TRACK SPOT OF CORROSION ON TWO AREAS AS MARKED. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 51-72-10 AND 51-40-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

SEAT TRACK AT C31 BETWEEN RIGHT NR 1 AND NR 2 SEAT TWO AREAS OF CORROSION. REMOVED DISCREPANT CLS ADAPTER AND REPLACED WITH NEW CLS ADAPTER IAW A300-600 SRM 51-72-10.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MAIN DECK CARGO COMP 3RD CARGO TRACK RT SIDE FROM CENTER LINE AT FR 29 ONE EA AREA OF CORROSION. REPAIRED CORRODED AREA AS PER A300-600 SRM 53-10-16.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MAIN DECK CARGO COMP FLOOR, CENTER SEAT TRACK BETWEEN FRAME 66 AND 68, TWO EACH AREAS OF CORROSION. CLEANED CORROSION AND FOUND TO BE OUT OF LIMITS. SPLICED IN NEW SECTION OF SEAT TRACK BETWEEN FRAMES 65.5 AND 68.5 IAW A300-600 SRM 53-10-16.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MAIN DECK CARGO COMP 2ND SEAT TRACK FROM CENTER RT SIDE BETWEEN FRAMES 74 AND 75, 1 EA AREA OF CORROSION. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. CUT AND FABRICATED NEW SEAT TRACK SECTION IAW A300 SRM 53-10-16 FIG 208. LOCATED AND DRILLED NEW SPLICES, INSTALLED SEAT TRACK AND SPLICES IAW A300 SRM 53-10-16 FIG 208.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MAIN DECK CARGO COMP 2ND CARGO TRACK FROM CENTER RT SIDE BETWEEN FRAMES 77 AND 78, 2 EA AREAS OF CORROSION, UPPER SURFACE. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. CUT AND REMOVED DAMAGED SECTION OF CARGO TRACK, FABRICATED NEW SECTION OF CARGO TRACK, LOCATED AND DRILLED NEW SPLICES, INSTALLED CARGO TRACK AND SPLICES IAW A300-600 SRM 53-10-16 FIG 208.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

SEAT TRACK -0- [C/L] BETWEEN FRAMES 29-30 HAS CORROSION ON FLANGE NEAR FASTENER HOLE, MAIN CABIN FLOOR. REPAIRED SEAT TRACK AS PER A300-600 SRM 53-10-16 PG 210 FIG 202.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MAIN DECK CARGO COMP RT SIDE NR 5 SEAT TRACK BETWEEN FR 24 AND 25 HAS TWO AREAS OF CORROSION UPPER SURFACE. REPAIRED SEAT TRACK IAW A300-600 SRM 53-10-16 PG 210 FIG 202, TREATED AREA AS PER A300-600 SRM 51-75-10.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MAIN DECK CARGO LEFT SIDE FRAME 39 BETWEEN L3 AND L4, TWO HOLES CORRODED BOTTOM SIDE. REMOVED DISCREPANT CROSS BEAM AND INSTALLED NEW CROSS BEAM IAW A300-600 SRM 51-72-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MAIN CARGO COMP 1ST SEAT TRACK LT SIDE FROM CENTER AT FRAME 70 JUST AFT HAS MILD CORROSION UPPER SURFACE. CLEANED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-16. FABRICATED AND INSTALLED SEAT TRACK SECTION PER SRM 53-10-16 AND 51-40-21.

Part: SEAT TRACK — GOUGED (ZONE 200) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MAIN CABIN SMALL SIDE TRACK BETWEEN R4 AND R3 AT FRAME 61 HAS DEEP GOUGE. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 51-40-21.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MAIN DECK CARGO COMP CENTER SEAT AT CENTER LINE BETWEEN FRAME 74 TO 76, THREE EACH AREAS OF CORROSION ON UPPER SURFACE. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-10-16. CUT OUT SECTION OF SEAT TRACK .125 INCH LONG, FABRICATED AND INSTALLED REPLACEMENT SECTION PER SRM 53-10-16 AND 51-40-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

SEAT TRACK AT C33 RIGHT NR 1 AND 2 SEAT TRACKS THREE AREAS OF CORROSION, MAIN CARGO COMPT. REMOVED DISCREPANT CLS ADAPTER AND REPLACED WITH NEW CLS ADAPTER IAW A300-600 SRM 51-72-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

SECOND SEAT TRACK FROM CENTER LEFT BETWEEN FRAMES F77 & F78, 2 EA AREAS OF CORROSION UPPER SURFACE, MAIN CARGO COMPT. REMOVED CORROSION IAW A300-600 SRM 51-74-10. REMOVAL OF CORROSION WAS VISUALLY OUT OF LIMITS IAW A300-600 SRM 51-74-10. LOCATED, DRILLED, AND INSTALLED NEW SEAT TRACK SECTION IAW A300-600 SRM 53-10-16. TOP COATED FASTENERS IAW A300-600 SRM 51-75-10.

Part: CARGO TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,305 hrs · 7,731 cycles

MAIN DECK CARGO COMPARTMENT CENTER CARGO TRACK AT CENTER LINE RT SIDE BETWEEN FRAME 77 AND 78, 2 EA AREAS OF CORROSION. CUT OUT DAMAGED SECTION OF CARGO TRACK AND INSTALLED NEW SECTION IAW SRM 53-10-16.

Part: WIRE HARNESS — FAULTY (NLG) · airframe 14,270 hrs · 7,101 cycles

AFTER TO/ECAM LAND GEAR RETR FAULT BOTH PITCH TRIM LEVERS FAULTED-TRIPPED OFF & WOULD NOT RESET ATS LEVER TRIPPED OFF-WOULD NOT RESET-HAD NO ELECTRIC TRIM ON GEAR EXTENSION, RED INTRANSIT LIGHT ON NOSE GEAR DID NOT ILLUMINATE, GEAR EXTENDED. REMOVED AND REPLACED THE FOLLOWING LOOMS NLG UPPER RIGHT HAND ELECTRICAL HARNESS AND NLG UPPER LEFT HAND ELECTRICAL HARNESS, NLG STRUT ELECTRICAL HARNESS. PERFORMED FULL JACKING AS PER MM CHAPTER 7-11-00-0. ALSO PERFORMED NORMAL EXTENSION AND RETRACTION TEST OF GEARS AS PER MM CHAPTER 32-31-00-5. CYCLED LANDING GEAR 5 TIMES IN THE NR 1 IND POS AND 5 TIMES IN THE NR 2 IND POS. ALL CYCLES NORMAL AND INDICATIONS NORMAL.

Part: RELAY — FAILED (NLG) · airframe 14,270 hrs · 7,100 cycles

AFTER GEAR RETRACTION GOT ECAM WARNING- GEAR FAILED TO RETRACT, GEAR INDICATOR PANEL SHOWED NO LIGHTS. MOMENTS LATER GOT BOTH YAW DAMPERS BOTH PITCH TRIM AND ATS FAILURE. UNABLE TO RESET. RETURNED FOR LANDING. ALSO BOTH FD FAILED. UPDT 10JUN03 15:27 FLL R REMOVED AND REPLACED NLG SHOCK ABS RELAY 94GB DUE TO PROX FAULTING SHOCK ABS NOSE FAIL (SN CODE) & MTP FAULTING NOSE RELAY FAIL. OPS CHECKED NORMAL PER A300 M/M 32-31-7 1-4. FACT 10JUN03 16:27 FLL R PERF AFS LAND TEST TO CHECK YAW DAMP, ATS, PITCH TRIM & F/D'S. OPS CHECKS GOOD PER A-300 TSM 22-00-00.

Part: WIRE — BROKEN (MLG) · airframe 14,270 hrs · 7,100 cycles

AFTER GEAR RETRACTION, GOT LANDING GEAR RETRACT INOP ON ECAM. DURING RETRACTION NEVER GOT RED UPLOCK LIGHT IN NOSE INDICATOR LIGHT. TRIED POSITION INDICATION SYSTEM 2, SAME WARNING ON ECAM. AFTER RETRACTION ALL GEAR LIGHTS EXTINGUISHED. REPEAT WRITE-UP. T/S FOUND BROKEN WIRES ON 39GBA C/P FACT 11JUN03 18:28 FLL R FOUND BROKEN WIRE TO PIN 'E' AT C/P 39GBA (NLG UPLOCK SYS1 MICROSWITCH). REMOVED AND REPLACED C/P IAW SWP'S. C/W NOSE GEAR TEST (SWING) IAW AMMSUPP 32-31-00-5 PAR 6. ALL NOSE GEAR & DOOR INDICATIONS CHK NORMAL.

Part: HYDRAULIC SYSTEM — FAULTY · airframe 11,515 hrs · 5,545 cycles

01-288 LOST GREEN HYD SYS ON DECENT. COMPLIED WITH ECAM & QRH PROC. ** S/D ** COMING

Part: ENGINE — VIBRATION (NR 1)

00-23 - REPEAT OF PREV VIB WRITEUP FOR NR 1 ENGINE AT FL 210 W/CRUISE PWR 320 KNOTS AFT 1 MIN IN LVL FLT NR 1 ENG BEGAN SHAKING.

Part: ENGINE — VIBRATION (NR 1)

00-20 AT CR FLT AC BEGAN TO SHAKE ENG NR 1 N1 VIB = 6.0 N2 VIB = 2.2 VIB ABATED WHEN NR 1 THROTTLE PULL TO IDLE.

Part: COALESCER BAG — DIRTY (CABIN)

99-193 - AFT T/O, BURN SMELL PRESENT FOR 1 MIN WITH VENTS OPEN. REMOVED AND REPLACED WATER SEPARATOR IN BOTH PACKS PER MM 21-51-11-3. RAN ENG AT HI-PWR PER JRH. OPS CK GOOD. NO SMELL OR FUMES. OK FOR SERVICE.

Part: VALVE — INOP (NR 2 ENGINE)

AT T/O ROLL JUST AFT TOGA ACTIVATED ECAM ALERT NR 2 ENGINE REVERSE PRESSURIZED APPEARED. MASTER CAUTION ILLUM. *S/D* REMOVED AND REPLACED NR 2 ENG PILOT VALVE PER MM 78-10-01, OPS CK NORMAL.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO COMPT)

MID 1 MAIN DECK CARGO SMOKE WARNING WITH NO VISUAL INDICATION OR ODORS IN FLIGHT. AN EMERGENCY WAS DECLARED ON APPROACH INTO MSP. REMOVED AND REPLACED RALTU AND REPROGRAMMED. PERFORMED DISPLAY AND INPUTS BITE TEST ON ECAM. WARNING WENT AWAY AND SYSTEM WORKED NORMALLY.

Part: FUEL FILTER — CONTAMINATED (NR 1 ENGINE)

ON TAKEOFF, NR 1 ENG FUEL CLOG LIGHT WITH AMBER WARNING ILLUMINATED, ENGINE ANTI-ICE WAS ON. REMOVED AND REPLACED NR 1 ENG FUEL FILTER. SUSPECT WATER AND ICE IN SYSTEM. LEAK CHECK GOOD, OK FOR SERVICE.