N138UP

Part: DOOR — BINDING (ZONE 800) · airframe 28,954 hrs · 17,497 cycles

CREW ENTRY DOOR DIFFICULT TO OPEN AND APPEARS TO BIND IN FANNIE HANDLE DOES NOT STAY UP IN ELEVATED POSITION. UNSURE OF WHERE IT IS CATCHING. INSTALLED L1 DOOR REF AMM 52-11-11/401 UP TO AND 2 F (8).

Part: ACTUATOR — FAULTED (YAW DAMPER) · airframe 28,809 hrs · 17,422 cycles

EMERGENCY DECLARED, YAW DAMPER KICKED OFF WOULD NOT RESET. REPLACED YAW DAMPER ACTUATOR IAW AMM 22-23-22/401 OPS AND LEAKS CHECKS GOOD OK FOR SERVICE. ALL WORK ACCOMPLISHED BY ALL CAT 3 QUALIFIED TECH.

Part: ACTUATOR — INOPERATIVE (YAW DAMPER) · airframe 28,812 hrs · 17,423 cycles

YAW DAMPER KICKED OFF WOULD NOT RESET. REPLACED YAW DAMPER ACTUATOR IAW AMM 22-23-22/401 OPS AND LEAKS CHECKS GOOD OK FOR SERVICE. ALL WORK ACCOMPLISHED BY ALL CAT 3 QUALIFIED TECH.

Part: SKIN — PUNCTURED (FLAP) · airframe 28,930 hrs · 17,482 cycles

MAJOR REPAIR, DURING CLEAN UP , PUNCTURED INNER FLAP LOWER SKIN INFO SENT TO ENGINEERING ALL STEPS OF EO-95467-REQ4 COMPLETED. THIS IS A PERMANENT REPAIR. THIS DEFERRAL IS NOW CLOSED.

Part: FITTING — CRACKED (ZONE 100) · airframe 28,457 hrs · 17,213 cycles

CRACK FOUND AT BASE FITTING FR44, RH SIDE. THIS JOB WAS PERFORMED IAW EO-46789-JIC008, REPAIR - BASE FRAME FITTING, FR 41 TO FR 46, RH SIDE (SB A300-57-6177).

Part: FITTING — CRACKED · airframe 28,457 hrs · 17,213 cycles

CRACK FOUND AT BASE FITTING FR45, RH SIDE.THIS JOB WAS PERFORMED IAW EO-46789-JIC008. (REPAIR - BASE FRAME FITTING, FR 41 TO FR 46, RH SIDE (SB A300-57-6177)) [T3F18E00711GE] STEPS 43 THROUGH 53

Part: FITTING — CRACKED · airframe 28,457 hrs · 17,213 cycles

CRACK FOUND AT BASE FITTING FR46, RIGHT SIDE.ACCOMPLISHED EO-46789-JIC008 REPAIR OF FR46 RH SIDE BASE FITTING COMPLETE.

Part: FASTENER — CORRODED (ZONE 800) · airframe 28,457 hrs · 17,213 cycles

ALL FASTENERS AROUND CREW DOOR EXTERNAL SURFACE CORRODED.

Part: DOOR — CORRODED (ZONE 800) · airframe 28,467 hrs · 17,216 cycles

*** SUPPLEMENTAL SDR *** FAULT: STR-ZONE 831- ALL FASTENERS AROUND CREW DOOR EXTERNAL SURFACE CORRODED. JP-110 REVIEWED

Part: SUPPORT — CORRODED (OZNE 200) · airframe 28,457 hrs · 17,213 cycles

FAULT- STR- ZONE 100- AFT CARGO FR 58 RH SLOPE STRUCTURE (P/N F539-71534-006-00) IS CORRODED IN 2EA PLACES. 91148554.REMOVED AFT CARGO FR 58 PROFILE BRACKET P/N F539-71534-006-00 IAW A300-600 SRM 51-40-21.RECEIVED NEW SECTION SUPPORT (01EA)P/N F5397153400600 BCH# 0004416281.INSTALLED 01 SECTION SUPPORT P/N F53971534-006-00, BCH# 0004416281 USING 02 HI-LOK P/N HL10VF6-5, BCH# 0004271003 AND 02 COLLAR P/N NSA5075-6, BCH# 0004291986

Part: ATTACH ANGLE — CRACKED (ZONE 400) · airframe 28,457 hrs · 17,213 cycles

NR 1 PYLON-INSIDE 475AL 4TH STIFFENER FROM AFT END ON I/B SIDE HAS UPPER ATTACH ANGLE BROKEN-109-VWV-91195430 VERIFIED INSTALLATION OF NEW ANGLE.

Part: SKIN — DAMAGED (ZONE 800) · airframe 28,457 hrs · 17,213 cycles

CREW DOOR UPPER INNER SKIN HAS BARE METAL EXPOSED.

Part: ANGLE — CRACKED (ZONE 400) · airframe 28,457 hrs · 17,213 cycles

FAULT: STR-ZONE 400-#1 PYLON-INSIDE 475AL O/B SIDE 7TH FRAME FROM FWD SIDE-LOWER PART OF FRAME BROKEN ANGLE-109-VWV-91195430.FAB BROKEN ANGLE LOCATED AND DRILLED IAW A300-600 SRM.APPLIED TREATED AND PRIMER TO NEW ANGLE WITH P/N#ALODINE1132 BTCH#4381945 QTY: 1EA P/N#02-013-8 BTCH#4331971 CUP: CCAS1M3 QTY: 0.10 OZ. REMOVED BROKEN ANGLE FROM #1 PYLON-INSIDE 475AL O/B SIDE 7TH FRAME FWD SIDE-LOWER IAW A300-600 SRM 51-40-21.INSTALLED NEW ANGLE ON 1 PYLON-INSIDE 475AL O/B SIDE 7TH FRAME FROM FWD SIDE-LOWER WITH P/N#CR3523-6-6 BTCH#4266798 QTY: 2 EA. P/N#CR3523-6-04 BTCH#4226398 QTY: 2 EA

Part: SUPPORT — CORRODED (ZONE 100) · airframe 28,457 hrs · 17,213 cycles

FAULT- STR- ZONE 100- FR 57 LH SLOPE STRUCTURE HAS CORROSION IN 1 PLACED MARKED IN RED. 91148554. REMOVED AFT CARGO FR 57 LH PROFILE BRACKET P/N F539-71534-006-00 IAW A300-600 SRM 51-40-21.RECEIVED NEW SECTION SUPPORT (01EA) P/N F5397153400600 BCH# 0004416282.INSTALLED 01 SECTION SUPPORT P/N F53971534-006-00, BCH# 0004416282 USING 02 HI-LOK P/N HL10VF6-5, BCH# 0004271003 AND 02 COLLAR P/N NSA5075-6, BCH# 0004291986

Part: SKIN — DAMAGED (ZONE 800) · airframe 28,467 hrs · 17,216 cycles

CREW DOOR UPPER INNER SKIN HAS BARE METAL EXPOSED. CLEANED AREA AND RESTORED SURFACE PROTECTION IAW A300-600 SRM 51-21-10, SRM 51-75-10 AND AMM 12-21-11.

Part: PANEL — CRACKED (ZONE 800) · airframe 28,457 hrs · 17,213 cycles

PANEL 831AZ HAS CRACK (.600 IN).

Part: SKIN — GOUGED (ZONE 100) · airframe 28,457 hrs · 17,213 cycles

FUSELAGE TAIL LOWER JACK SECTION, REINFORCE DOUBLER HAS MULTIPLE GOUGES (5EA) AND (1EA) DENT. INSTALLED FILLER, DOUBLER AND BALL AT FUSELAGE TAIL LOWER JACK SECTION IAW 53-10-12-201 PARA 13 FIGURE 210 REV 42 AND SRM 51-40-21.

Part: SIGHT GLASS — SCRATCHED (ZONE 800) · airframe 28,457 hrs · 17,213 cycles

L-1 CREW DOOR EMERGENCY SLIDE COVER LOOKING GLASS IS SCRATCHED AND UNABLE TO SEE THROUGH

Part: PANEL — CRACKED · airframe 28,467 hrs · 17,216 cycles

PANEL 831BZ HAS CRACK (.500 IN). 91148554 APPLIED ADHESIVE TO DAMAGE AREA OF PANEL 831BZ. P/N EC3532, B/N 0004408668. CURED AND SANDED. IAW AMM 25-00-00/801 PARA 4 REPAIR A STEP (B). RESTORED PROTECTIVE COATING AT REPAIRED AREA. P/N WS-3-BR227K1Q, B/N 0004319071. IAW AMM 25-00-00/801 PARA 4 REPAIR A STEP (D).

Part: PANEL — CRACKED (ZONE 800) · airframe 28,457 hrs · 17,213 cycles

PANEL 831BZ HAS CRACK (.500 IN).

Part: PANEL — CRACKED · airframe 28,467 hrs · 17,216 cycles

PANEL 831AZ HAS CRACK (.600 IN). 91148554 REPAIRED CRACK WITH 08-116, BATCH 4394542. IAW AMM A300-600 52-34-13/801 PARA 4.3.B.4-6. PAINTED REPAIRED AREA WITH .05 OZ OF 16-407, BATCH 4352735. CUP 02-012-176. IAW AMM A300-600 52-34-13/801 PARA 4.3.C.1.

Part: SIGHT GLASS — SCRATCHED (ZONE 800) · airframe 28,467 hrs · 17,216 cycles

L-1 CREW DOOR EMERGENCY SLIDE COVER LOOKING GLASS IS SCRATCHED AND UNABLE TO SEE THROUGH INSTALLED CREW DOOR EMERGENCY SLIDE COVER IAW A300 AMM 52-10-13/401.

Part: FRAME — BROKEN (ZONE 400) · airframe 28,457 hrs · 17,213 cycles

NUMBER 2 PYLON, INSIDE 485AL OTBD SIDE 5TH FRAME FWD FROM AFT END HAS BROKEN STIFFENER ON LOWER END. CLIP AND FRAME WAS INSTALLED IAW A300/600 SRM 51-40-21.

Part: ROLLER — GOUGED (ZONE 100) · airframe 28,457 hrs · 17,213 cycles

AFT CARGO COMPT ROLLER @ FRAME 57 LBL 30 DAMAGED. REMOVED AND REPLACED ROLLER BRAKING IAW AMM 25-58-34/0401.VERIFIED 1 EACH ROLLER REMOVED AND REPLACED. JOB COMPLETE.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 28,457 hrs · 17,213 cycles

MAJOR REPAIR, MDC FLOOR PANEL 231QH WITH CORNER BROKEN FABRICATED FLOOR PANEL 231QH IAW A300 SREO-16407-REQ001. PAINTED IAW AMM 25-00-00/801.

Part: FLOOR SUPPORT — BROKEN (ZONE 200) · airframe 28,457 hrs · 17,213 cycles

MDC FLOOR STRUCTURE REINFORCEMENT SUPPORT CRACKED BTWN FR 38 AND FR 38.1 AT -Y2127.5. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-21 WITH FASTENERS AND SEALANT.

Part: FIRE SEAL — CRACKED (ZONE 400) · airframe 28,457 hrs · 17,213 cycles

RIGHT PYLON, LOWER MIDDLE FIRE SEAL HAS A CRACK. REMOVED AND REPLACED LOWER FIRE SEAL, IAW SRM 51-40-21.

Part: FITTING — CRACKED (ZONE 100) · airframe 28,457 hrs · 17,213 cycles

LEFT HAND HORIZONTAL JUCTION AREA AT FRAME 47 HOLE #A HAS CRACK AND DAMAGE INDICATIONS IN THE ALL LAYERS IN THE 9 O`CLOCK POSTION FACEING FORWARD. VERIFIED REPAIR HAS BEEN ACCOMPLISHED IAW EO-94545-REQ1 AND EA 300-5710-27-A4027 REV. -.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,457 hrs · 17,213 cycles

MAIN DECK FLOOR PANEL 231NG IS DAMAGED. FABRICATED FLOOR PANEL 231NG IAW A300 SREO-16407-REQ001, VERIFIED FABRICATION AND PAINT.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 28,457 hrs · 17,213 cycles

FWD CARGO CMPT, FLOOR PANEL 132MG; FR 27-32 RH IS DAMAGED. FABRICATED FLOOR PANEL 132MG IAW SREO-16407-REQ003 STEPS 1 - 19 .

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,457 hrs · 17,213 cycles

FWD CARGO CMPT, FLOOR PANEL 131MG; FR 27-32 LH IS DAMAGED. INSTALLED FABRICATED REPLACEMENT FLOOR PANEL FOR FWD PIT IAW SREO-16407-REQ002 ((APPX C)) JOB COMPLETE. REVIEWED

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 28,457 hrs · 17,213 cycles

FWD CARGO CMPT FR 38.2; UPPER FLOORBEAM, LOWER CHANNEL SUPPORT BRACKETS (3EA) ARE CRACKED.REMOVED SUPPORT BRACKETS (3EA) AT FRAME 38.2 UPPER FLOOR BEAM IAW A300/600 SRM 51-40-21.FABRICATED NEW BRACKETS (3EA) ON FWD CARGO CMPT FROM MAT. 2024-T3.032C BTCH#:0004355009 MAT.QUANTITI 10"X 7" IAW A300-600 AMM 09.08.01.01.INSTALLED NEW BRACKETS (3EA) FROM FWD CARGO CMPT FR38.2 UPPER BLOOR BEAM RIVET (6EA) P/N:HL10VF5-8 BTCH#:0004254757 COLLAR (6EA)P/N:NSA5075-5 BTCH#:0004178417 (9EA)P/N:MS20426AD5-7 BTCH#:0004372118, SEALANT P/N:04-001-0114 BTCH#:0004362800 QTY:1 IAW A300-600 SRM 51-40-21

Part: WEB — CRACKED (ZONE 200) · airframe 28,457 hrs · 17,213 cycles

MDC FLOOR BETWEEN C73 TO 74 Y2127.5 WEB WITH EVIDENCE OF CRACK IN THE LOWER SURFACE INSTALLED NEW WEB BTW FR73 AND FR74 AT 2127.5 IAW A300-600 SRM 51-40-21.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 28,457 hrs · 17,213 cycles

MAJOR REPAIR, FLOOR C73 TO C74 AND Y 852 SEAT TRACK WITH EVIDENCE OF CORROSION INSTALLED NEW SEAT TRACK SECCTION ON MDC FLOOR STRUCTURE C71 TO C74 AND Y 852 IAW SRM 53-10-16. RESTORED PROTECTIVE SURFACE ON SEAT TRACK REPAIRED IAW SRM 51 75 10.51 10 16.

Part: ADAPTER — CORRODED (SEAT TRACK) · airframe 28,481 hrs · 17,226 cycles

CORROSION FOUND ON SEAT TRACK (5 LOCATIONS, EACH ONE ON A FRAME) BTW FR21&FR27 -Y65.5 INSTALLED NEW SEAT TRACK ADAPTER, CLS (4E/A) AND NUTPLATES (10E/A) IAW A300-600 SRM 51-40-21.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 28,457 hrs · 17,213 cycles

MAJOR REPAIR, MAIN DECK CARGO FLOOR PANEL 232WG INSERT IS BROKEN (1 EA) FABRICATED FLOOR PANEL 232WG IAW A300 SREO-16407-REQ001. PAINTED IAW A300 AMM 25-00-00/801.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 28,457 hrs · 17,213 cycles

MAJOR REPAIR. MAIN DECK CARGO FLOOR PANEL 241LM BROKEN FABRICATED FLOOR PANEL 241LM IAW A300 SREO-16407-REQ001.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 28,467 hrs · 17,216 cycles

MAIN DECK FLOOR PANEL 232EF IS CRACKED. FABRICATED FLOOR PANEL 232EF IAW SREO-16407-REQ001. PAINTED IAW AMM 25-00-00/801.

Part: FITTING — CRACKED (ZONE 200) · airframe 28,467 hrs · 17,216 cycles

CRACK FOUND AT ANGLE-FITTING FR10 Y953 (PN A53612356200) INSTALLED 01 ANGLE FITTING P/N A5361235620000, BCH #0004410795, USING 11 SOLID RIVET IAW SRM 51-40-21 AND SRM 51-21-10

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 28,457 hrs · 17,213 cycles

MAIN DECK FLOOR PANEL 232EF IS CRACKED AUDIT COMPLETE

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 28,457 hrs · 17,213 cycles

MAIN DECK FLOOR PANEL 242LJ IS BROKEN. FABRICATED FLOOR PANEL 242LJ IAW A300 SREO-16407-REQ001.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 28,457 hrs · 17,213 cycles

MAIN DECK FLOOR PANEL 231PJ IS DAMAGED AUDIT COMPLETE

Part: RIB — CRACKED (ZONE 600) · airframe 28,467 hrs · 17,216 cycles

RH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACK INDICATION NOTED AT RIB 26. CIRCLED IN RED. VERIFIED REPAIR HAS BEEN ACCOMPLISHED IAW VT-MAE EA 300-5720-27-A4024 REV- AND EO-94347-REQ1.

Part: RIB — CRACKED (ZONE 600) · airframe 28,467 hrs · 17,216 cycles

RH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 CRACK INDICATION NOTED AT RIB 19. CIRCLED IN RED. VERIFIED REPAIR WAS ACCOMPLISHED IAW E0-94347-REQ1 AND EA 300-5750-27-A4024.

Part: PROFILE — CRACKED · airframe 28,457 hrs · 17,213 cycles

CRACK ON PROFILES-T AT FR80/82 LH Y1580.5/RH -Y1580.5 INSTALLED PROFILES-T AT FR80/82 LH Y1580.5/RH -Y1580.5 IAW SRM 51-40-21

Part: SKIN — CRACKED (ZONE 500 FLAP) · airframe 28,457 hrs · 17,213 cycles

MAJOR REPAIR, LH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACK INDICATION NOTED AT RIB 27. CIRCLED IN RED. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-94346-REQ1 AND VT-MAE EA 300-5750-27-A4023, REV. -. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUIREMENTS AND RII BUY - OFF WHICH MUST BE PERFORMED BY A PROPERLY TRAINED AND CURRENTLY AUTHORIZED INDIVIDUAL. TO DETERMINE RII AUTHORIZATION, REFER TO THE CURRENT RII AUTHORIZATION LIST, SEE CHAPTER 04 OF THE GMM.

Part: PROFILE — CRACKED (ZONE 200) · airframe 28,457 hrs · 17,213 cycles

CRACK AT FR74 HOLE ON PROFILE-Z RH BTW FR72 AND FR75. RT PROFILE-Z FR72-75 REMOVED DUE TO CRACK IAW SRM 51-40-21. FABRICATED NEW PROFILE Z IAW GMM 09.08.01.03 FOLLOWING 4 AND SRM 53-18-18 FIGURE 3 SHEET 2 ITEM 55. INSTALLED NEW PROFILE Z RH FOR STRUCTURE BTW FR72 AND FR75. VERIFIED STEP 12. NEW R/H PROFILE Z BTW FR72 AND FR75 INSTALLATION C/W. JOB COMPLETE.

Part: PROFILE — CRACKED (ZONE 200) · airframe 28,457 hrs · 17,213 cycles

CRACK AT FR74 HOLE ON PROFILE-Z LH BTW FR72 AND FR75 INSTALLED NEW PROFILE Z LH FOR STRUCTURE BTW FR72 AND FR75 IAW A300-600 SRM 51-40-21.

Part: ADAPTER — CORRODED (ZONE 200) · airframe 28,467 hrs · 17,216 cycles

FOUND CORROSION AT CLS ADAPTER FR77 -Y1580.5 REMOVE AND REPLACE THE FR 78 CLS ADAPTER (P/N: A53275455204) LOCATED BETWEEN -Y1221.2 AND -Y1580.5 PER AIRBUS DRAWING A53278756 REQUIREMENTS AND A300-600F SRM CHAPTER 51 REQUIREMENTS. UPS CONSIDERS THIS A MINOR REPAIR PER GMM 05.04.

Part: RIB — CRACKED (ZONE 600) · airframe 28,467 hrs · 17,216 cycles

MAJOR REPAIR, RH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACK INDICATION NOTED AT RIB 25. CIRCLED IN RED. VERIFIED PERMANENT REPAIR ACCOMPLISHED IAW EO-94347-REQ1 AND VT-MAE EA 300-5750-27-A4024, REV. -.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 28,457 hrs · 17,213 cycles

MAJOR REPAIR FOUND CORROSION AT SEAT TRACK BTW FR 79 AND FR80-82 Y0 ACOMPLISHED, REPAIR SEAT TRACK, P/N A53279239202, PER SRM 53-10-16-201 PARAGRAPH 4 FIGURE 201. REV. 42. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUIREMENTS AND RII BUY - OFF WHICH MUST BE PERFORMED BY A PROPERLY TRAINED AND CURRENTLY AUTHORIZED INDIVIDUAL. TO DETERMINE RII AUTHORIZATION, REFER TO THE CURRENT RII AUTHORIZATION LIST, SEE CHAPTER 04 OF THE GMM

Part: RIB — CRACKED (ZONE 600) · airframe 28,457 hrs · 17,213 cycles

RIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 CRACK INDICATION NOTED AT RIB 13. CIRCLED IN RED. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94347-REQ1 AND VT-MAE EA 300-5750-27-A4024, REV. -. REVIEWED.

Part: ADAPTER — CORRODED (ZONE 200) · airframe 28,457 hrs · 17,213 cycles

FOUND CORROSION AT CLS ADAPTER FR77 -Y1580.5. VERIFIED INSTALLATION.

Part: BLOCKER DOOR — CORRODED (ZONE 400) · airframe 28,457 hrs · 17,213 cycles

EVIDENCE OF CORROSION AT THE ENG#2 I/B T/R BLOCKER DOOR #5 UPPER TO LOWER. INSTALLED ENG#2 I/B T/R BLOCKER DOOR #5 IAW-300-AMM 78-32-13/401. #2 ENGINE I/B T/R WAS REPLACED AT TC T3F18E006YV81 BEFORE COMPLETE PNEUMATIC OPS CHECK, MANUAL OPERATION WAS COMPLETED IAW A300-600 AMM 78-32-13/401 BEFORE T/R REPLACEMENT.

Part: SKIN — DAMAGED (ZONE 500) · airframe 28,467 hrs · 17,216 cycles

LH WING-ZONE500: LH WINGTIP LWR AFT CORNER DAMAGED. VERIFIED REPAIR ACCOMPLISHED IAW EO-94606-REQ1 AND VT-MAE EA 300-5730-27-A4061, REV.-.

Part: HOUSING — CRACKED (ZONE 800) · airframe 28,068 hrs · 16,992 cycles

MAJOR REPAIR, FWD LOWER CARGO DOOR, AT LOCK HANDLE CUTOUT, IS DEFLECTED AND CRACKED METAL USED IN REPAIR .080 2024 T3 PO NUMBER SP1451826 .071 2024 T3 SNR LOT 02051639. COMPLETED REPAIR REF EO-92402-REQ3. CAT B REPAIR INSTALLED.

Part: BUFFER — OUT OF ADJUST (MAIN DOOR) · airframe 26,890 hrs · 16,352 cycles

MAIN CABIN DOOR WILL NOT LOCK INTO OPEN POSITION. ADJUSTED DOOR BUFFER PER AMM 52-10-11/501. TWO EACH SHIMS REMOVED. NO DMP TO REVERSE. DMP 52-11-01-2-4 IS ONLY FOR VISUAL INSPECTION. NO RII REQUIRED FOR DOOR BUFFER.

Part: DUCT — LOOSE (HEAT EXCHANGER) · airframe 26,743 hrs · 16,248 cycles

EMERGENCY DECLARED, BTB. AFTER BOTH ENGINES STARTED AND AFTER TURNING LEFT PACK ON AND RIGHT PACK OFF - MASTER CAUTION WARNING ILLUMINATED ALONG WITH MAIN DECK CARGO SMOKE MID 1, RED SMOKE, LOOP A & B AMBER, ALSO CLAMP SECURING THE SLEEVE BETWEEN THE HEAT EXCHANGER AND DUCTING FOUND TO BE LOOSE, ALLOWING HOT AIR TO ESCAPE. OPEN

Part: SMOKE WARNING — ILLUMINATED (MAIN DECK CARGO) · airframe 26,747 hrs · 16,251 cycles

EMERGENCY DECLARED, AFTER BOTH ENGINES STARTED AND AFTER TURNING LEFT PACK ON AND RIGHT PACK OFF - MASTER CAUTION WARNING ILLUMINATED ALONG WITH MAIN DECK CARGO SMOKE MID 1, RED SMOKE, LOOP A & B AMBER, ALSO INSPECTED SLEEVE AND CLAMPS FOUND LOOSE ON #2 PACK HEAT EXCHANGER, NO DEFECTS WERE NOTED. REPOSITIONED SLEEVE AND SECURED WITH EXISTING CLAMPS PER AMM 21-51-32/401. INSPECTED BOTH PACKS FOR ANY OTHER DEFECTS, NONE NOTED. CLEANED ANY RESIDUAL HYDRAULIC FLUID FOUND INSIDE PACK BAY AND MAIN WHEEL WELL. REMOVED #2 PACK WATER SEPARATOR COALESCER, INSPECTED AND FOUND NO SIGNS OF CONTAMINATION, REPLACED PER AMM 21-51-16/301 FOR PREVENTIVE MAINTENANCE. LEAK CHECK BOTH PACKS WITH APU BLEED, NO LEAKS OR DEFECTS NOTED. PERFORMED BOTH ENGINES IDLE RUN FOR OVER 15 MIN SWITCHING FROM APU TO ENGINE PNUEMATICS (HOT AND COLD), WITH ALL HYDRAULICS SYSTEMS RUNNING. NO WARNING OR CAUTION LIGHTS, NO SIGNS OF SMOKE OR SMELL AND BOTH PACKS RUNNING AS REQUIRED PER AMM 21-51-00/501. OK FOR SERVICE.

Part: HYDRAULIC LINE — LEAKING (YELLOW SYSTEM) · airframe 26,733 hrs · 16,241 cycles

APPROACHING TOP OF CLIMB, HYD YELOW RSVR LO LEVEL ECAM. LOCAL INDICATIONS AGREE. A FEW MOMENTS LATER YELLOW PUMP LO PRESSURE ECAM. VERIFIED INDICATIONS AND COMPLIED W/ ECAM REMOVED AND REPLACED RH AILERON PRESSURE HOSE PER AMM 20-23-12/001. REQUIRES LACING CORD AND LEAK CHECK TO COMPLETE. INSTALLED LACING CORD AND LEAK CHECKED REF EO NO A300-2910-60058-C. NO LEAKS DETECTED.

Part: SWITCH — INTERMITTENT (SLIDE) · airframe 26,519 hrs · 16,103 cycles

SLIDE BUZZER AND LIGHT ARE ON DURING CLIMB CLEANED AND LUBED SLIDE GIRT BAR ASSY, OPERATED ESCAPE SLIDE RELEASE MECHANISM, SEVERAL TIMES, NO BINDING OR FAULTS NOTED.SLIDE GIRT BAR ENGAGES AND RELEASES NORMALLY PER AMM REF 52-73-00. THIS CLEARS M2808358. DMP REVERSED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 26,469 hrs · 16,076 cycles

CRACK IN #1 ENG AFT LOWER PYLON FAIRING. ALL STEPS COMPLETED PER SREO 32659-REQ001 APEND A

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 26,132 hrs · 15,880 cycles

SLIDE ARM WARNING LT ILLUMINATED IN FLT ACCOMPLISHED ESCAPE SLIDE WARNING TEST W/REF TO TSM 52-73-00, NO FAULTS NOTED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 26,124 hrs · 15,876 cycles

*** SDR FILED OPEN *** SLIDE ARM WARNING LT ILLUMINATED IN FLT ACCOMPLISHED ESCAPE SLIDE WARNING TEST W/REF TO TSM 52-73-00, NO FAULTS NOTED

Part: DOOR — INOPERATIVE (DOORS) · airframe 25,657 hrs · 15,570 cycles

INSPECTION TYPE:N/AMAIN ENTRY DOOR WILL NOT LOCK IN OPEN POSITIONCLEANED AND LUBED DOOR LATCH & HOOK RELEASE SSY OPS GOOD IAW AMM 52-10-00

Part: ARM — WARNING LIGHT (DOORS) · airframe 25,616 hrs · 15,541 cycles

CLIMBING PAST FL250 SLIDE ARM WARNING LT AND BUZZER CAME ON. NO DOOR WARNING INDICATIONS, NO PRESSURIZATION PROBLEMS AT CRUISE DP 8.2 ON DESCENT PASSING FL 265 P 7.0 LIGHT AND BUZZER WENT OUT. DEFERRED PER MEL 52-11-01-23 M806500 ASSIGNEDPERFORMED TEST OF DOOR WARNING SYSTEM PER TSM 52-73-00 AND GMM 52-73-00 FIG 501. OPS CHECK GOOD.

Part: PAD — INOPERATIVE (POWERPLANT) · airframe 25,520 hrs · 15,483 cycles

INSPECTION TYPE:NA#1 ENGINE MANUAL CRANK PAD COVER CRACKEDREMOVED AND REPLACED #1 ENG MANUAL CRANKPAD COVER AS PER A300 AMM 72-00-00. MS 5064809 03/04/23. CRANK PAD COVER OIL LEAK PENDING. LEAK CHECK C/W 72-61-00 ITEM 90

Part: BRACKET — CRACKED (AFT CRGO) · airframe 25,390 hrs · 15,399 cycles

INSPECTION TYPE:CAFT CARGO COMPARTMENT FWD BULKHEAD UPPER AREA UNDER PARTITION PANEL 152DW THE CHANNEL HAS 1 CRACK. *NOT REPORTABLE*REMOVED AND REPLACED CHANNEL IAW SRM 51-40-21

Part: BRACKET — CRACKED (AFT CARGO) · airframe 25,390 hrs · 15,399 cycles

INSPECTION TYPE:CAFT CARGO COMPARTMENT FWD BULKHEAD UPPER AREA UNDER PARTITION PANEL 151DW THE CHANNEL HAS 1 CRACKREMOVED, FABRICATED, AND REPLACED CHANNEL IAW SRM 51-26-00 AND SRM 51-40-21

Part: WEB — CRACKED (NACELLE) · airframe 25,390 hrs · 15,399 cycles

INSPECTION TYPE:1C, PYLON PANEL 413BL INTERNAL WEB CRACKED AT CORNER. FABRICATED DOUBLER IAW SRM 54-52-51 AND INSTALLED IAW SRM 51-40-21.

Part: BRACKET — CRACKED (AFT CARGO) · airframe 25,390 hrs · 15,399 cycles

INSPECTION TYPE:CAFT CARGO COMPARTMENT FWD BULKHEAD UPPER AREA UNDER PARTITION PANEL 151BW THE CHANNEL HAS 1 CRACKREMOVED AND REPLACED CHANNEL IAW SRM 51-40-21

Part: SHEAR TIE — DAMAGED (NR 2 NACELLE) · airframe 23,412 hrs · 14,336 cycles

INSPECTION TYPE:N/A#2 PYLON AFT PYLON O/B SIDE SKIN ATTACHMENT LUG IS DAMAGEDREPAIRED AREA IAW EO A300-5450-81319-F AND COMPLETED INSTALLATION PER AIRBUS DWG R5460328

Part: GIRT BAR — FOD (L1 DOOR SLIDE) · airframe 22,486 hrs · 13,802 cycles

EMERGENCY SLIDE WILL NOT ARM. DEFERRED L-1 DOOR SLIDE W/REF TO MEL 52-11-01-4. C/N M734800 ASSIGNED.DISCOVERED DEBRIS IN THE GIRT BAR ANCHORS IN THE FLOOR. CLEANED AND RELUBRICATED ANCHORS AND BAR. OPERATIONAL CHECK NORMAL. GOOD ECAM INDICATION REF AMM 52-10-00. M734800 CLOSED. PLACARD REMOVED.

Part: TEST PANEL — NO TEST (L1 DOOR SLIDE) · airframe 22,394 hrs · 13,745 cycles

INSPECTION TYPE: NA, SUPPLEMENTAL SDR. ON PREFLIGHT RED L1 DOOR SLIDE WARNING LIGHT WILL NOT TEST. LIGHT DEFFERRED PER MEL52-73-01-1, M-732086 ASSIGNED PLACARD INSTALLED. REMOVED, CLEANED & RE-INSTALLED CONNECTGOR TO AUTONOMOUS STANDBY POWER SUPPLY UNIT (ASPSU). PERFORMED CREW ENTRY DOOR SLIDE WARNING TEST, PER AMM 52-73-00-10-0501. OPERATIONS CHECKED GOOD. M732086 CLOSED. PLACARD REMOVED. EFF SOURCE REF WDM 52-73-01 SHEET 1.

Part: WARNING HORN — FALSE ACTIVATION (SLIDE WARNING) · airframe 22,372 hrs · 13,733 cycles

INSPECTION TYPE: NA EVACUATION SLIDE WARING HORN RUNS CONTINOUSLY IN THE ARMED POSITION DURING CLIMB THRU FL200 AND REMAINED ON UNTIL DESCENDING THRU FL190. PERFORMED OPERATIONS CHECK OF SLIDE, PER AMM 52-73-00-0501. TEST PASSED CLEANED CONNECTOR FOR THE ASPSU.

Part: HEAT SHIELD — CRACKED (NR 2 NACELLE) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 NR 2 PYLON SHIELD ASSEMBLYY HAS FLANGE BENT AND CRACKED, AS MARKED. COMPLIED WITH EA 300-6741-27-A2517 & UPS EO A300-5740-78436-A.

Part: LINK — GOUGED (LT WING TE FLAP) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 LT MID FLAP OUTBOARD LINK CUTOUT HAS A DEEP GOUGE. REPAIRED AREA IAW EA 300-5753-27-A2514/UPS EO A300-5750-78403.

Part: FRAME — CRACKED (FRM 63) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 DURING ACCOMPLISHMENT OF STEP (2) OF TC523208-01-1-812, THE AFT LOWER HOLE OF FR 63 WAS FOUND TO HAVE A CRACK INDICATION AT THE 6 O'CLOCK POSITION AND APPROXIMATELY 1" IN LENGTH. REMOVED DAMAGE & REPAIRED, IAW EA30-5230-27-2511, UPS EO A300-5230-78289-A.

Part: FLOOR PANEL — PUNCTURED (FLIGHT DECK) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 SDR FILED OPEN. FLOOR PANEL 212EP PUNCTURED, REMOVE & REPAIR, IAW SREO. REPLACED FLOOR PANEL 212 EP, IAW MM 53-10-21-0401.

Part: FLOOR PANEL — BROKEN (MDC) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 MDC FLOOR PANEL 231KJ IS BROKEN. SREO A300-5320-40552-B.

Part: SEAT TRACK — CORRODED (FRAME 80) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 MCD SEAT TRACK AT FR 80 -Y450 HAS CORROSION. REMOVED DAMAGED SECTION & REPAIRED, IAW SRM 53-10-16 FIG 201.

Part: SEAT TRACK — CORRODED (AFT CABIN) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 AFT CABIN FLOOR SEAT TRACK HAS CORROSION LOCATED 2 IN FWD OF FR 80, Y1137. REMOVED DAMAGED SECTION & REPAIRED, IAW SRM 53-10-16 FIG 201.

Part: SEAT TRACK — CORRODED (FRAME 80) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 MCD SEAT TRACK AT FR 80 -Y794.3 HAS CORROSION. REMOVED DAMAGED SECTION & REPAIRED, IAW SRM 53-10-16 FIG 201.

Part: FLOOR PANEL — PUNCTURED (MAIN CARGO) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 MAIN CARGO COMPARTMENT FLOOR PANEL 252YJ HAS PUNCTURE. REPAIRED PER SREO A300-5520-42722.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 MAIN DECK FLOOR PANEL 251DN IS DAMAGED. REPAIRED PER SREO A300-5320-42722.

Part: FLOOR PANEL — BROKEN (AFT CARGO) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 AFT CARGO COMPARTMENT FLOOR PANEL 152NG CORNER BROKENS REO A300-5320-42722.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 FWD CARGO COMPARTMENT FLOOR PANEL 131GE CRACKED. REPAIRED PER SREO A300-5520-42722.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 FWD CARGO COMPARTMENT FLOOR PANEL 131DE CRACKED. REPAIRED PER SREO A300-5520-42722.

Part: FLOOR PANEL — PUNCTURED (MAIN CARGO) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 MAIN CARGO COMPARTMENT FLOOR PANEL 252WN HAS PUNCTURE. REPAIRED PER SREO A300-5520-42722.

Part: DEFLECTOR — CHAFED (THRUST REVERSER) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 NR 2 ENGINE RT T/R-LOWER FWD LATCH ACCESS DOOR HAS CHAFED AREA ON INNER SURFACE. REMOVED & REPLACED DEFLECTOR ASSEMBLY, IAW SRM 51-40-21.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 AVIONICS COMPARTMENT PANEL 121JF CORNER CRACKED. REPAIRED BY SREO A300-5320-42722.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 CABIN FLOOR PANEL 221EG CORNER CRACKED. REPAIRED PER SREO A300-5320-42722.

Part: WEB — CRACKED (FRAMES 12-17) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 UPON REMOVED OF LAV SUPPORT Y1959 FR 12-FR 17 FOUND WEB AT FR 12A TO FR 14 CRACKED. REMOVED & REPLACED WEB, IAW SRM 51-40-21.

Part: STRUCTURE — GOUGED (RT WING TE) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 RT WING FIXED TRAILING EDGE FWD OF NR 2 SPOILER OUTBOARD SIDE PANEL SUPPORT STRUCTURE HAS GOUGE/WEAR MARKS. REMOVED & REPLACED RIB ATTACHMENT, IAW SRM 51-40-21.

Part: BRACKET — GOUGED (FRAME 52) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 LT WING TOP SURFACE INBOARD AREA UNDER WING TO BODY PANEL 577DT STRUCTURE ANGLE HAS GOUGE. REMOVED & REPLACED BRACKET, IAW SRM 51-40-21.

Part: FLOOR PANEL — BROKEN (BULK CARGO) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 BULK CARGO FLOOR BROKEN, AS MARKED. SREO A300-5520-42722.

Part: FLOOR PANEL — BROKEN (MDC) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: CMDC FLOOR PANEL 232EF IS BROKEN. FABBED PER SREO 40552-B.

Part: FLOOR SUPPORT — CORRODED (FRAMES 14-16) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: CMDCC AT MAIN ENTRY DOOR AREA BETWEEN FR 14 AND FR 16 TO Y1959 FLOOR SUPPORT STRUCTURE HAS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT, IAW SRM 51-40-21.

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: CMCD FLOOR PANEL 231RG IS DAMAGE. FABBED PER SREO 40552-B.

Part: BRACKET — CRACKED (LT WING) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: C LT WING FIXED TRAILING EDGE LOWER SURFACE DOUBLER PLATE CRACK AROUND THE FASTENER HOLES 1 EA FWD OF NR 3 SPOILER INBOARD HINGE. REMOVED BRACKET, IAW SRM 51-40-21 FABRICATED REPLACEMENT BRACKET, IAW SRM 51-72-10 TRAVELER T20/1521649. INSTALLED REPLACEMENT BRACKET, IAW SRM 51-40-21.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: C CABIN FLOOR PANEL 221EG CRACKED. REO A300-5320-42722.

Part: FLOORBEAM — CRACKED (FRAME 51) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 MCD FLOOR SUPPORT OF FR 51 BETWEEN -Y450 AND -Y953 HAS CRACK. REMOVED & REPLACED MCD FLOOR SUPPORT AT FR 51 -Y450 TO -Y153, IAW SRM 51-40-21.

Part: WEB — CRACKED (FRAMES 38-39) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 FUSELAGE INTERNAL UPPER HALF RT SIDE CORNER BETWEEN FR C38.1 AND FR 39 SUPPORT WEB CRACKED. REMOVED & REPLACED IAW A300 SRM 51-40-21.

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: C AFT CARGO FLOOR PANEL 152KG CRACKED. SREO A300-5520-42722.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: C CABIN FLOOR PANEL 232NN CRACKED. SREO A300-5320-42722.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 2ND ROW AFT FROM FRONT FASTENERS 6, 7, 8 NR 2 ENGINE OUTBOARD LOWER PYLON FAIRING SKIN CRACK REPAIR ACCOMPLISH PERMANENT REPAIR. REMOVED & REPLACE NR 2 PYLON FAIRING OUTBOARD SKIN, IAW SRM 51-40-21.

Part: FLOOR PANEL — BROKEN (MAIN DECK CARGO) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: C MDC FLOOR PANEL 222DG IS BROKEN FABBED, PER SREO 40552-B.

Part: FLOOR PANEL — PUNCTURED (MAIN CARGO) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: C MAIN CARGO COMPARTMENT FLOOR PANEL 251XS HAS PUNCTURE ON UPPER SIDE A300-5520-42722.

Part: FLOOR PANEL — BROKEN (MAIN CARGO) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: C MAIN CARGO COMPARTMENT FLOOR PANEL 262SF HAS BROKEN CORNERS REO A300-5520-42722.

Part: FLOOR PANEL — CRACKED (E&E BAY) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: CE&E FLOOR PANEL 172AF IS CRACKED, AS MARKED. SREO A300-5520-42722.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: C MAIN CARGO COMPARTMENT FLOOR PANEL 251WJ HAS DAMAGE ON UPPER LEFT AREAS REO A300-5520-42722.

Part: WEB — CRACKED (FRAMES 38 & 39) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: C FUSELAGE UPPER HALF LT SIDE CORNER BETWEEN FR C38.1 AND FR 39 SUPPORT WEB CRACKED. REMOVED AND REPLACED, IAW A300 SRM 51-40-21.

Part: SEAT TRACK — CORRODED (FRAMES 78-80) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 AFT CABIN SEAT TRACK BEAM HAS CORROSION LOCATED 4 IN FWD OF F.80Y0. REPARIED SEAT TRACK FROM FR 78-5 TO F.80, IAW SRM 53-10-16 FIG 201.

Part: DOUBLER — GOUGED (LT WING TE FLAP) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: CL/H INBOARD FLAP GOUGE IN PREVIOUSLY EXISTING REPAIR DOUBLER ON UPPER SKIN. COMPLIED WITH EA A300-5750-78240-A.

Part: RUB STRIP — WORN (LT WING TE FLAP) · airframe 22,170 hrs · 13,625 cycles

INSPECTION TYPE: A300 LT WING INBOARD FLAP LEADING EDGE TOP SURFACE SEVERAL RUB PLATE 7 EA HAS WORN MASK. REMOVED AND REPLACED 7 EA RUBSTRIPS, IAW SRM 51-40-21.

Part: FAULT LIGHT — ILLUMINATED (SMOKE DETECTOR) · airframe 21,942 hrs · 13,487 cycles

INSPECTION TYPE:N/A**DIVERTED** EMERGENCY DECLARED ** LANDED UNEVENTFULLY CRASH FIRE & RESCUE INSPECTED THE JET FOR FIRE, DAMAGE & SMOKE. THE FIRE CRASH TEAM RELEASED CREW TO RAMP**. MAIN DECK CARGO SMOKE DETECTION MID 2 LOOP A FAULT LIGHT DISPLAYED ON ECAM. SMOKE LIGHT WOULD NOT ILLUMINATE WITH LOOP A OFF.REPLACED MID UPPER CARGO SMOKE DET CTRL UNIT IAW AMM 26-19-34 PB 401.

Part: WARNING LIGHT — INOPERATIVE (CARGO DOOR) · airframe 21,385 hrs · 13,171 cycles

INSPECTION TYPE:N/A** SUPPLEMENTAL SDR ** SLIDE LIGHT WARNING INOP ON MAIN CARGO DOOR. DEFERRED PER MEL 52 73 01 1COULD NOT DUPLICATE DISCREPANCY FOR TROUBLESHOOTING. REPLACED LIGHT IAW AMM 52 73 00 0501 & AMM 52 73 11 0401, SYSTEM OPS CK NORMAL AT THIS TIME. DMP SN PLACARD REMOVED THIS CLEARS M 703424 EFF 52 73 01 03C.

Part: SHROUD — GOUGED (THRUST REVERSER) · airframe 18,902 hrs · 11,727 cycles

INSPECTION TYPE:1C, NR 1 ENG O/B T/R UPPER COOLING VALVE SHROUD IS GOUGED AND DAMAGED. REMOVED AND REPLACED SHROUD PER SRM 54-04-01.

Part: SUPPORT BRACKET — BENT (NR 1 PYLON) · airframe 18,902 hrs · 11,727 cycles

INSPECTION TYPE:1C, NR 1 PYLON AFT UPPER O/B PANEL SUPPORT BRACKET IS BENT (STREAMER ATTACHED)REPAIRED AREA IAW SREO M-5100-41097-B.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 18,902 hrs · 11,727 cycles

INSPECTION TYPE:1C, FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT AT STA 38.2 LBL 41 CLIP CRACKED. REMOVED AND REPLACED IAW SRM 51-40-21.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 18,902 hrs · 11,727 cycles

INSPECTION TYPE:1C, AFT CARGO COMPARTMENT, FWD RT WALL ATTACH BRACKET CRACKED. REMOVE AND REPLACE IAW SRM 51-40-21.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 18,902 hrs · 11,727 cycles

INSPECTION TYPE:1C, FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT AT STA 38.2 RBL 22 CLIP CRACKED. REMOVED AND REPLACED IAW SRM 51-40-21.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 18,902 hrs · 11,727 cycles

INSPECTION TYPE:1C, FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT STA 38.2 RBL 41 CLIP CRACKED. REMOVED AND REPLACED IAW SRM 51-40-21.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 18,902 hrs · 11,727 cycles

INSPECTION TYPE:1C, FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT AT STA 38.2 LBL22 CLIP. CRACKED REMOVED AND REPLACED CLIP PER SRM 51-40-21.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 18,902 hrs · 11,727 cycles

INSPECTION TYPE:1C, AFT CARGO COMPARTMENT FWD BULKHEAD UPPER PANEL SUPPORT BRACKET AT FR54 LBL36 CRACKED. REMOVED AND REPLACED NEW SUPPORT BRACKET IAW SRM 51-40-21

Part: BRACKET — CRACKED (FUSELAGE) · airframe 18,902 hrs · 11,727 cycles

INSPECTION TYPE:1C, AFT CARGO COMPARTMENT FWD BULKHEAD UPPER PANEL SUPPORT BRACKET FR54 LBL40 CRACKED. REMOVED AND REPLACED NEW SUPPORT BRACKET IAW SRM 51-40-21.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 18,902 hrs · 11,727 cycles

INSPECTION TYPE:1C, AFT CARGO COMPARTMENT FWD BULKHEAD UPPER PANEL SUPPORT BRACKET AT FR54 RBL 36 CRACKED. REMOVED AND REPLACED NEW SUPPORT BRACKET IAW SRM 51-40-21.

Part: WARNING HORN — FALSE ACTIVATION (MAIN CABIN) · airframe 18,136 hrs · 11,321 cycles

MAIN CABIN WARNING HORN SOUNDS CONTINUOSLY IN FLT, BEGAN CLIMBING THROUGH FL300. RESET THE CIRCUIT BREAKER E22, OPS CHECKED SLIDE HORN & BITE CHECKED AUTONOMUS SUPPLY UNIT 70WN. OPS CHECKED GOOD

Part: RELAY — INOPERATIVE (CABIN) · airframe 17,926 hrs · 11,193 cycles

T/S EXIT SIGN FUNCTION USING EXIT SWITCH. C/W T/S PER AWM 33-51-12 AND DETERMINED RELAY 69WL AT FAULT. REQUIRES REPLACEMENT. R&R RELAY 69WL PER ESPM 20-46-50-0101-02 OPS TEST GOOD IAW MM 33-50-00-5.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,090 hrs · 10,662 cycles

CREW ENTRY DOOR EXIT SIGN HAS INOPERATIVE LAMPS. REPLACED THE LAMPS IAW AMM A300-33-51-13-0401. OPS CHECKED GOOD.

Part: CONNECTOR — MELTED (DC BUSS) · airframe 16,495 hrs · 10,310 cycles

EMERGENCY DECLARED. RECEIVED DC NORM BUSS OFF MESSAGE RESULTING IN LOSS OF ACARS, VHF AND SLATS & FLAPS. NO FLAP & NO SLAT APPROACH. THERMAL CONNETOR MELTING. R & R NR 1 T/R IAW MM 24- 32-11-401. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,108 hrs · 10,038 cycles

ON OVERHEAD PANEL EMERGENCY EXIT LT BULBS INOPERATIVE. REPLACED THE LAMP EMERGENCY EXIT LIGHT ON OVERHEAD PANEL IAW STANDARD PRACTICES 20-45-44. OPS CHECKED NORMAL.

Part: ATTACH ANGLE — CRACKED (FRAME 79) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE: 1C, 2C, MAIN CABIN AT FWD SIDE OF RT FRAME 79 SEAT TRACK ATTACH ANGLE IS CRACKED. FABRICATED AND INSTALLED NEW ANGLE IAW EO A300-5310-59655-A AND DWG A300-53-006.

Part: FLOORBOARD — DAMAGED (FWD CARGO) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE:5YR, FWD CARGO FLOORBOARD 132-SG HAS EDGE DAMAGE. REPAIRED THE DAMAGE IAW EO A3005320-427722-E.

Part: CEILING PANEL — DAMAGED (AFT CARGO) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE:5YR, AFT CARGO CEILING PANEL NR 152QC HAS MINOR DAMAGE AT FASTENER HOLE REPAIR IAW EO A300-2550-29554-C.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE:5 YR, MAIN CABIN FLOOR PANEL 231MJ HAS A BROKEN CORNER. REPAIRED FLOOR PANEL IAW SREO A300-5320-42721-F.

Part: WEB — PUNCTURED (FWD CARGO) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE:123C FWD CARGO BALL MAT 131 QE HAS PUNCTURE THROUGH METAL SKIN ON BOTTOM SIDE, REPAIRED IAW SREO M-2550-11648-K.

Part: SIDEWALL PANEL — DELAMINATED (FWD CARGO) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE: 5YR, FWD CARGO LT SIDEWALL PANEL 131SW HAS DELAMINATION AT CORNER TO SURFACE. REPAIRED IAW SRM 51-77-10 AND 51-77-11.

Part: BRACKET — CRACKED (AFT CARGO) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE:5YR, AFT PIT FWD BULKHEAD UPPER PANEL VENT ATTACH BRACKET AT THE C/L CRACKED. R & R BRACKET IAW SRM 51-40-21.

Part: SHEAR TIE — CRACKED (FRAME 79) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE: 1C, 2C, MAIN CABIN SHEAR PLATE AT FRAME 29, S26R IS CRACKED. REMOVED SHEAR PLATE AND REPLACED WITH ANGLE BRACKET IAW 5310-58168-A.

Part: SIDEWALL PANEL — PUNCTURED (FWD CARGO) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE:5 YR, FWD SIDE WALL PANEL LT NR 131SW HAS PUNCTURE ON BACK SIDE OF BLOW OUT PANEL. REPAIR IAW SRM 51-77-10, 51-77-11.

Part: BRACKET — CRACKED (AFT CARGO BAY) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE: 5YR, AFT CARGO FWD BULKHEAD UPPER PANEL VENT ATTACH BRACKET 39 IN LEFT C/L CRACKED. R & R BRACKET IAW SRM 51-40-21.

Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE:123C, MAIN CABIN FLOOR PANEL 231PH BROKEN. REPAIR MAIN CABIN FLOOR PANEL 231PH IAW SRM 51-77-10, 51-77-11.

Part: FLOORBOARD — DENTED (CARGO BAY) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE:1C , 2C, BULK CARGO FLOORBOARD 161LF IS DENTED ON TOP SURFACE. REPAIRED IAW SRM 51-77-10 AND 51-77-11.

Part: FLOOR PANEL — DENTED (BULK CARGO) · airframe 15,874 hrs · 9,892 cycles

BULK CARGO PANEL 161CW DENTED ON TOP SURFACE REPAIRED PANEL 161CW IAW SRM 51-77-10, 51-77-11.

Part: FLOOR PANEL — DENTED (AFT CARGO) · airframe 15,874 hrs · 9,892 cycles

AFT CARGO RT PANEL 162CW DENTED ON TOP SURFACE REPAIRED DENTS IAW SRM 51-77-10 AND 51-77-11.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE:C1. MAIN CABIN FLOOR PANEL 232QH CRACKED. REPAIR IAW EO A300-5320-42722-E AND SRM 5310-20, SRM 51-77-10, 51-77-11.

Part: SIDEWALL PANEL — PUNCTURED (BULK CARGO) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE:5YR, BULK CARGO PANEL 161LW DENTED 2 PLACES AND PUNCTURED ON TOP SURFACE REPAIRED BULK CARGO PANEL 161LW IAW SRM 51-77-11, 51-77-10.

Part: FLOORBOARD — DENTED (BULK CARGO) · airframe 15,874 hrs · 9,892 cycles

BULK CARGO FLOORBOARD 161MF DENTED ON TOP SURFACE REPAIRED DENT IAW SRM 51-77-10 AND 51-77-11.

Part: FLOOR PANEL — DENTED (BULK CARGO) · airframe 15,874 hrs · 9,892 cycles

BULK CARGO PANEL NR 161MW DENTED ON TOP SURFACE REPAIR DENT IAW SRM 51-77-10 AND 51-77-11.

Part: ADAPTER — CRACKED (SEAT TRACK) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE: C1, MAIN CABIN SEAT TRACK ADAPTER AT FR 35 LT IS CRACKED. R & R ADAPTER IAW DWG B53774136 AND SRM 51-40-21.

Part: PARTITION — PUNCTURED (MAIN CARGO) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE:5YR, CABIN PANEL 626CY HAS PUNCTURES ON TOP SURFACE. REPAIRED THE PARTITION IAW SRM 51-77-10, SRM 51-77-11.

Part: CEILING PANEL — DENTED (AFT CARGO) · airframe 15,874 hrs · 9,892 cycles

AFT CARGO RT PANEL 162DW HAS DENTS ON TOP SURFACE REPAIRED PANEL 162DW IAW SRM 51-77-11, 51-77-10.

Part: FLOORBOARD — PUNCTURED (CARGO BAY) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE:5YR BULK CARGO PIT FLOORBOARD 172BF HAS PUNCTURE ON BACK SIDE REPAIRED PUNCTURE IAW SRM 51-77-11 AND 51-77-10.

Part: FLOORBOARD — PUNCTURED (MAIN CARGO) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE: 5YR, MAIN CABIN FLOORBOARD 232JF HAS PUNCTURE. REPAIRED THE FLOORBOARD IAW EO A300-5320-42722-E.

Part: FLOORBOARD — PUNCTURED (FWD CARGO) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE:1C, 2C, FWD CARGO FLOORBOARD 132MG IS PUNCTURED ON BACK SIDE. REPAIRED FLOORBOARD IAW SRM 51-77-10, 51-77-11.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE:123C, FWD CARGO FLOORBOARD 132SG IS CRACKED. FABRICATED NEW FWD CARGO FLOORBOARD PANEL 132SG IAW SREO A300-5320-16407.

Part: CEILING PANEL — DAMAGED (FWD CARGO) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE:5YR, FWD CARGO CEILING PANEL 132WC HAS EDGE DAMAGE REPAIRED FWD CARGO CEILING PANEL 132WC IAW SRM 51-77-10, 51-77-11.

Part: SIDEWALL PANEL — PUNCTURED (FWD CARGO) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE:5YR, FWD CARGO PANEL 132UW HAS PUNCTURES ON TOP SIDE REPAIRED FWD CARGO PANEL 132UW IAW SRM 51-77-10, 51-77-11.

Part: SIDEWALL PANEL — PUNCTURED (AFT CARGO) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE:1C,2C, AFT CARGO SIDEWALL PANEL 151MX HAS PUNCTURES ON TOP AND BOTTOM SIDES. REPAIRED IAW SRM 51-77-10, SRM 51-77-11.

Part: SIDEWALL PANEL — PUNCTURED (FWD CARGO) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE:5YR, FWD CARGO 131TW HAS PUNCTURE ON BACK SIDE REPAIRED FWD CARGO 131TW PANEL IAW SRM 51-77-11.

Part: FLOOR PANEL — PUNCTURED (AFT CARGO) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE: 1C, 2C, AFT CARGO FLOOR PANEL 151GX HAS SMALL PUNCTURE ON TOP SIDE. REPAIRED THE FLOOR PANEL IAW SRM 51-77-10, 51-77-11.

Part: SIDEWALL PANEL — PUNCTURED (AFT CARGO) · airframe 15,874 hrs · 9,892 cycles

INSPECTION TYPE:1C,2C, AFT CARGO SIDEWALL PANEL 151JX HAS PUNCTURES ON TOP AND BOTTOM SIDES. REPAIRED THE PANEL IAW SRM 51-77-10, 57-77-11.

Part: PARTITION — DAMAGED (FWD CARGO) · airframe 15,873 hrs · 9,891 cycles

INSPECTION TYPE:5YR, FWD PIT/ AVIONICS COMPARTMENT PARTITION PANEL 132CW HAS EDGE DAMAGE. REPAIR PANEL 132CW IAW SRM 51-77-10, 51-77-11.

Part: CEILING PANEL — PUNCTURED (FWD CARGO) · airframe 15,873 hrs · 9,891 cycles

INSPECTION TYPE:5YR, FWD PIT CEILING PANEL 132LL HAS PUNCTURE FASTENER HOLE. REPAIRED DAMAGE IAW SRM 51-77-10, SRM 51-77-11.

Part: SIDEWALL PANEL — DAMAGED (AFT CARGO) · airframe 15,873 hrs · 9,891 cycles

INSPECTION TYPE:5YR, AFT PIT RT SIDEWALL PANEL 152CX HAS DAMAGE ON BACK. REPAIRED DAMAGE IAW SRM 51-77-10, SRM 51-77-11.

Part: SKIN — WORN (LT ELEVATOR) · airframe 15,873 hrs · 9,891 cycles

INSPECTION TYPE:5YR, TRAPPED WATER INDICATION FOUND LT ELEVATOR UPPER SURFACE 2" X 3", 4" FWD OF THE 18" OTBD OF ER10. EVALUATED /REPAIRED IAW SERO A300-5500-43303-B.

Part: SKIN — WORN (LT ELEVATOR) · airframe 15,873 hrs · 9,891 cycles

INSPECTION TYPE:5YR, TRAPPED WATER INDICATION FOUND LT ELEVATOR UPPER SURFACE JUST OTBD OF ER2 MARKED 1.5" X 2" 37" FWD OF T/E. REPAIRED /EVALUATED AREA IAW SERO A300-5500-43303-B.

Part: CEILING PANEL — PUNCTURED (MAIN CARGO) · airframe 15,873 hrs · 9,891 cycles

INSPECTION TYPE:5YR, MAIN CABIN PANEL 231NY HAS PUNCTURE ON TOP SIDE. REPAIRED PANEL IAW SRM 51-77-10, SRM 51-77-11.

Part: SIDEWALL PANEL — PUNCTURED (AFT CARGO) · airframe 15,873 hrs · 9,891 cycles

INSPECTION TYPE:5YR, AFT CARGO PANEL 151FX HAS PUNCTURES ON TOP SIDE. REPAIRED PANEL IAW SRM 51-77-10 AND SRM 51-77-11.

Part: FLOOR PANEL — PUNCTURED (FWD CARGO) · airframe 15,873 hrs · 9,891 cycles

INSPECTION TYPE:5YR, CARGO FLOOR PANEL NR 132RG HAS PUNCTURE ON BACK SIDE. REPAIR IAW EO NR A300-5320-42722-E AND SRM 53-10-20, SRM 51-77-10 AND 51-77-11.

Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 15,873 hrs · 9,891 cycles

INSPECTION TYPE: 1C, 2C, MAIN CABIN FLOORBEAM RT FRAME 79, 1580 IS CRACKED. REPAIRED IAW EO A300-5310-59505-B.

Part: CEILING PANEL — PUNCTURED (AFT CARGO) · airframe 15,873 hrs · 9,891 cycles

INSPECTION TYPE:5YR, AFT CARGO CEILING PANEL 152QC HAS PUNCTURE AROUND FASTENER HOLE. REPAIRED PANEL IAW SRM 51-77-10, SRM 51-77-11.

Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 15,873 hrs · 9,891 cycles

INSPECTION TYPE: 1C,2C, MAIN CABIN FLOOR CROSSBEAM LT FRAME 79 AT Y1580 IS CRACKED. REPAIRED IAW EO A300-5310-59505-1.

Part: CEILING PANEL — DAMAGED (FWD CARGO) · airframe 15,873 hrs · 9,891 cycles

INSPECTION TYPE:5YR, FWD PIT CEILING PANEL 132LL HAS DAMAGE ON BACK SIDE. REPAIRED DAMAGE IAW SRM 51-77-10, SRM 51-77-11.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 15,873 hrs · 9,891 cycles

INSPECTION TYPE:1C2C, LT WING INBD FLAP UPPER SURFACE CHAFED 20 INCHES FROM L/E, 80 INCHES FROM INBD EDGE AT RIB 12 STR 2.1 TO STR 2.2. REPAIRED DAMAGED AREA IAW SRM 57-50-00, PARA 4E.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

MAIN ENTRY DOOR EMERGENCY LIGHTS WILL NOT TEST. REPLACED EMERGENCY POWER SUPPLY UNIT 29WL. OPS CHECKED NORMAL IAW AMM 33-51-14-0401.

Part: ESCAPE ROPE — LOOSE (COCKPIT)

ESCAPE ROPE ON CAPTAIN`S SIDE LOOSE. STOWED CAPTAIN'S ESCAPE ROPE IAW AMM 25 10 00.

Part: HANDLE — BINDING (ESCAPE SLIDE)

EMERGENCY ESCAPE SLIDE HANDLE IS BINDING. OPERATED EMERGENCY ESCAPE SLIDE CONTROL HANDLE REPEATEDLY WITH NO BINDING OR DEFECTS OBSERVED. GIRT BAR AND PADS FREE FROM OBSTRUCTION. NO HISTORY ON SYS. EMERGENCY ESCAPE SLIDE, OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (MULTIPLE)

NUMEROUS FLIGHT DECK FAULTS. MASTER CAUTION ILLUMINATED WITH ECAM MESSAGE. PERFORMED OPS TEST OF CABIN NR 1 PRESSURE SYSTEM IAW AMM 21-30-00-05. FOUND SATISFACTORY, PERFORMED OPS TEST OF NR 1 PITCH TRIM IAW AMM 22-27-00-05. PERFORMED AFTS TEST IAW AMM 22-40-00-05. TEST FOUND SATISFACTORY. PERFORMED PROBE HEAT TEST IAW AMM 30-31-00-05.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 12,489 hrs · 7,637 cycles

INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 232WG IS CRACKED AT LOWER SURFACE. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOOR PANEL — PUNCTURED (MAIN CARGO) · airframe 12,489 hrs · 7,637 cycles

INSPECTION TYPE: SV, MAIN DECK CARGO FLOOR PANEL 231WG PUNCTURED/CRACKED. REPAIRED FLOOR PANEL IAW EO A300-5320-40552-B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 12,489 hrs · 7,637 cycles

INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 221EG IS CRACKED AT LOWER SURFACE. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 12,489 hrs · 7,637 cycles

INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 232KG IS PUNCTURED IN 2 PLACES ON UPPER AND LOWER SURFACE. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 10,883 hrs · 6,670 cycles

INSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT FLOORBOARD NR 262JM IS CRACKED. REPAIRED MAIN CABIN FLOORBOARD NR 262JM IAW EO A300-5320-38221-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 10,883 hrs · 6,670 cycles

INSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT FLOORBOARD NR 232KG IS CRACKED. REPAIRED MAIN CABIN FLOORBOARD NR 232KGIAW EO A300-5320-38221-B, PARA, 6A 1.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 10,883 hrs · 6,670 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 222EG IS CRACKED. REPAIRED MAIN CABIN FLOORBOARD NR 222EG IAW EO A300-5320-38221-B, PARA 6A 1.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 10,883 hrs · 6,670 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD N221UF IS PUNCTURED AND DELAMINATED AT LOWER SURFACE. REPAIRED MAIN CABIN FLOORBOARD NR 221UF IAW EO A300-5320-38221-B, PARA 6A 1.

Part: FLOORBOARD — GOUGED (MAIN CARGO) · airframe 10,883 hrs · 6,670 cycles

INSPECTION TYPE:10YR, MAIN CARGO FLOORBOARD NR 231KG IS GOUGED. REPAIRED MAIN DECK FLOORBOARD NR 231KG IAW EO A300-5320-38221-B, PARA 6 A1.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 10,883 hrs · 6,670 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 221TF IS PUNCTURED AT LOWER SURFACE. REPAIRED MAIN CABIN FLOORBOARD NR 221TF IAW EO A300-5320-38221-B, PARA 6A 1.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 10,883 hrs · 6,670 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 241MN IS PUNCTURED AT LOWER SURFACE, REPAIRED MAIN CABIN FLOORBOARD NR 241MN IAW EO A300-5320-38221-B PARA. 6A 1.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 10,883 hrs · 6,670 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 251BN IS CRACKED AT BOTTOM SIDE. REPAIRED MAIN CABIN FLOORBOARD NR 251BN IAW EO A300-5320-38221-B PARA 6A 1.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 10,883 hrs · 6,670 cycles

INSPECTION TYPE:10YR, MAIN CARGO FLOORBOARD NR 232QG LOWER SURFACE IS PUCTURED IN 3 PLACES. REPAIRED MAIN CABIN FLOORBOARD NR 232QG IAW EO A300-5320-38221-B, PARA. 6A 1

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 10,883 hrs · 6,670 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 262GH IS DELAMINATED AT LOWER SURFACE. REPAIRED MAIN CABIN FLOORBOARD NR 262GH IAW EO A300-5320-38221-B, PARA. 6A 1.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 10,883 hrs · 6,670 cycles

INSPECTION TYPE:10YR, MAIN DECK FLOORBOARD NR 262BH IS DELAMINATED AT LOWER SURFACE. REPAIRED MAIN CABIN FLOORBOARD NR 262BH IAW EO A300-5320-38221-B, PARA 6A 1.

Part: FLOOR PANEL — CRACKED (MAIN DECK) · airframe 10,883 hrs · 6,670 cycles

INSPECTION TYPE:10YR, FLOOR PANEL, 252NM CRACKED. REPAIRED FLOOR PANEL 252NM IAW EO A300-5320-38221-B, PARA 6 (1).

Part: FLOORBOARD — BROKEN (MAIN CABIN) · airframe 10,883 hrs · 6,670 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 252YJ LOWER SURFACE IS BROKEN. REPAIRED MAIN CABIN FLOORBOARD NR 252YJ IAW EO A300-5320-38221-B, PARA. 6A 1.

Part: FLOOR PANEL — CRACKED (CARGO DECK) · airframe 10,883 hrs · 6,670 cycles

INSPECTION TYPE:10YR, MAIN DECK CARGO PANEL 252WJ IS CRACKED AND DELAMINATED. REPAIRED MAIN CABIN FLOOR PANEL NR 252WJ IAW EO A300-5320-38221-B, PARA 6A 1.

Part: SEAT TRACK — CORRODED (MAIN DECK) · airframe 10,883 hrs · 6,670 cycles

INSPECTION TYPE:10YR, FR79 Y450 SEAT TRACK CORRODED. REPAIRED FR79, Y450 SEAT TRACK IAW SRM 53-10-16, PARA 4, FIG 201.

Part: SEAT TRACK — CORRODED (CARGO BAY) · airframe 10,883 hrs · 6,670 cycles

INSPECTION TYPE:10YR, CORROSION FOUND AT SEAT TRACK -Y1137.1 FR 80 AT MAIN CARGO COMPT. ACCOMPLISHED REPAIR ON MAIN CABIN SEAT TRACK AT FR -1137.1 FR 80 IAW SRM 53-10-16, FIG 201, PB 201, PARA 4.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 10,883 hrs · 6,670 cycles

INSPECTION TYPE:10YR, REPAIR SURVEY SEQUENCE NR 138-W3-01, REPAIR DOUBLER IS GOUGED AT RIB 13 TO RIB 15, STGR 2.6 TO 2.8 LT WING CTR FLAP. ACCOMPLISHED REPAIR ON LT WING CTR FLAP RIB 13 TO RIB 15, STGR 2.6 TO 2.8 IAW SRM 57-50-00, PARA 4F, FIG 206 AND EO A300-5750-35931-C, APPENDIX A.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 10,883 hrs · 6,670 cycles

INSP TYPE:10YR, REPAIR SURVEY SEQUENCE NR138-W3-02, REPAIR DOUBLER HAS LOOSE RIVETS AT LT INBD FLAP UPPER SURFACE RIB3 TO RIB 4, STR 2.1 TO 2.2 AND DOES NOT CORRELATE TO THE SRM. ACCOMPLISHED REPAIR ON LT INBD FLAP UPPER SURFACE IAW SRM 57-50-00, PB 201, PARA 4E AND FIG 205.

Part: FLOORBOARD — DELAMINATED (FWD CARGO BAY) · airframe 10,883 hrs · 6,670 cycles

INSPECTION TYPE:10YR, FWD CARGO PIT FLOORBOARD NR 132FE IS DELAMINATING AT CORNER AND SKIN IS GOUGED. FABRICATED FWD CARGO FLOORBOARD NR 132FE IAW EO A300-5320-16407-E, APPENDIX C.

Part: BULLNOSE — CHAFED (RT WING TE FLAP) · airframe 10,883 hrs · 6,670 cycles

INSPECTION TYPE:10YR, RT WING OTBD FLAP INBD BULLNOSE IS CHAFED. ACCOMPLISHED REPAIR ON RT WING OTBD FLAP INBD BULLNOSE IAW SRM 57-50-00, PB 201, PARA 4H FIG 208.

Part: SKIN — GOUGED (THRUST REVERSER) · airframe 10,883 hrs · 6,670 cycles

INSPECTION TYPE:10YR, NR 1 ENG INBD T/R UPPER LONGERON SKIN GOUGED AT 12:00 POSITION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW EO A300- 7830-40521-B AND EA 300-7830-01-A2949.

Part: SKIN — DAMAGED (FUSELAGE)

REF LOG PAGE 434115 ITEM 1, REF D412751 FUSELAGE EXTERNAL REPAIR DOUBLER DMG ADJACENT TO FR85 AND L45. REPAIRED IAW EO A300-5330-35623D.

Part: SKIN — DAMAGED (FUSELAGE)

FUSELAGE SKIN DAMAGED FR 85. REPAIRED IAW EO A300-5330-35623-C.

Part: SOLENOID VALVE — INOPERATIVE (SLAT SYS 2)

ON TAKEOFF, SLAT SYS 2 FAULT LIGHT ECAM SLAT SYS 2 FAULT ILLUMINATED OVERHEAD PANEL. R & R SOLENOID VALVE ON VALVE BLOCK 26CV REF MM 27-84-33-04. FOLLOWED FIM 27-80-05, STEP 1 TO A2-6-13. ENABLE SOLENOID VALVE HAD RESISTANCE VALVE OF 69 OHMS. OPS CK OF SYS 2 SLATS OPS NORMAL. REF AMM 27- 84-00-05.

Part: SKIN — DENTED (RT WING TE FLAP)

RT INBD FLAP DENTED WITH GOUGE. REPAIRED IAW EO A300-5750-35971-C.

Part: WARNING LIGHT — FALSE ACTIVATION (ESCAPE SLIDE)

WHILE PASSING THROUGH FL210 ON CLIMB OUT GOT SLIDE WARNING ON CREW DOOR (AURAL AND LIGHT) WARNING WENT OUT ON DESCENT PASSING THROUGH 13,500 AT 305 KTS AND 410 PSI. PERFORMED OPS TEST OF EMER ESCAPE SLIDE RELEASE IAW MM 52-73-00-05. AURAL AND LIGHT CHECKS GOOD.

Part: SLIDE — INOPERATIVE (L1 DOOR)

L1 DOOR SLIDE INOP. REMOVED AND REPLACED L1 DOOR SLIDE ASSY IAW MM 25-61-21-04. OPS CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (ESCAPE SLIDE)

MAIN CREW DOOR SLIDE BOTTLE PRESSURE LOW. PLACED ON MEL 52-11-01-3. M414400 ASSIGNED. CREW DOOR EVAC SLIDE INOP. REMOVED AND REPLACED L1 DOOR SLIDE ASSY IAW MM 35-61-21-04. OPS CHECK GOOD. M414400 CLEARED.

Part: JACKSCREW — MALFUNCTIONED (NR 3)

INSPECTION TYPE:N/A NEITHER SLAT EXTENDED FOR LANDING. RECYCLED, NO SLATS/FLAPS 40. T/S IAW TSM 27-80-02 FOUND RT TQ LIMITER POPPED AND RT NR 3 JACKSCREW LOCKOUT TRIPPED. TOPPED OFF RT NR 3 JACKSCREW WITH 70CC IAW AMM 12-13-27. GREASED BALL NUT IAW AMM 12-22-27. FUNCTIONAL CHECK OK IAW AMM 27-80-00 -05. OK FOR SERVICE.

Part: CONNECTOR — NOT SEATED (WARNING SYSTEM)

INSPECTION TYPE:N/A EVAC SLIDE OR SLIDE RAFT RELEASE WARNING SYS LIGHT INOP. BUZZER OK. DEFERRED PER MEL 52-73-01-1 M395381. RESEATED ASPSU CONNECTOR PERFORMED TEST OF POWER SUPPLY UNIT IAW MM 52-73-00. SYSTEM OPS CHECK GOOD. THIS CLEARS M395381.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 7,797 hrs · 4,877 cycles

INSPECTION TYPE:C1 MAIN CARGO FLOOR BOARD PANEL 252WJ HAS A FIELD REPAIR. REPAIRED MAIN CARGO FLOOR PANEL 252WJ REF SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 7,797 hrs · 4,877 cycles

INSPECTION TYPE:C1 MAIN CARGO FLOOR PANEL 251MJ FWD HAS FIELD REPAIR. REPAIRED MAIN CARGO FLOOR PANEL 251MJ REF SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 7,797 hrs · 4,877 cycles

INSPECTION TYPE:1C MAIN CARGO FLOOR PNL 252SJ HAS FIELD REPAIRS. REPAIRED MAIN CARGO FLOOR PNL 252SJ REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 7,797 hrs · 4,877 cycles

INSPECTION TYPE:C1 MAIN CARGO FLOOR PNL 251XJ AFT HAS FIELD REPAIRS. REPAIRED MAIN CARGO FLOOR PNL 251XJ REF A300-600 SRM 51-10-20 TABLE 201 PARA 8A.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 7,797 hrs · 4,877 cycles

INSPECTION TYPE:C1 MAIN CARGO FLOOR PANEL 251SJ HAS FIELD REPAIR. REPAIRED MAIN CARGO FLOOR PANEL 251SJ REF SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 7,797 hrs · 4,877 cycles

INSPECTION TYPE:1C MAIN CARGO FLOOR PANEL 252OJ HAS A FIELD REPAIR. REPAIRED MAIN CARGO FLOOR PANEL 252OJ REF SRM 53-10-20 TABLE 201 PARA 8A.

Part: SKIN — GOUGED (FUSELAGE) · airframe 7,797 hrs · 4,877 cycles

INSPECTION TYPE:1C GOUGE 24 INCHES FWD AND 18 INCHES LEFT OF TAIL STAND BALL. FABRICATED & INSTALLED PERMANENT REPAIR IN FUSELAGE SKIN 24 INCHES FWD & 18 INCHES LEFT OF TAIL STAND BALL REF SRM 53-10-12 FIG 216, SRM 53-19-12 FIG 2, EO A300-5100-20876-B AND EO M-5100-21238-B.

Part: LINER — LOOSE (DOOR)

CREW ENTRY DOOR SLIDE WARNING SOUNDING IN FLIGHT. FOUND GUIDE ARM LINING LOOSE AND MISSING HARDWARE. LINING WAS INTERFERING WITH DOOR CLOSING. INSTALLED HARDWARE AND LINING IAW 52-10-13-04. PRESS A/C IAW 21-31-00-5. NO DEFECTS NOTED. PERFORMED TEST OF MAIN ENTRY DOOR WARNING HORN IAW 52-43-12-04. NO DEFECTS NOTED.

Part: DOOR — UNSECURE (CREW ENTRY)

ATB - CREW ENTRY DOOR ECAM MESSAGE. A/C WAS SLOWLY LOSING PRESSURIZATION AND CREW WAS HEARING A LOUD SQUEAL. FLIGHT LANDED WITH NO FURTHER INCIDENT. PERFORMED MAINTENANCE CHECK PER AMM A300-05-53-00-00. NO FAULTS NOTED.

Part: SEAT — DEFECTIVE (COCKPIT)

INSPECTION TYPE:N/A DURING TAKEOFF ROLL IN MIAMI, CAPTS SEAT UNLATCHED AND SLID TO REAR STOP. REJECTED TAKEOFF SPEED LESS THAN 50 KTS. REMOVED AND REPLACED CAPT'S SEAT ASSY IAW A300 MM 25-11-11-04-01.

Part: LIGHT — INOPERATIVE (EVAC SLIDE)

INSPECTION TYPE:N/A EVACUATION SLIDE WARNING SYSTEM LIGHTS DO NOT ILLUMINATE WHEN TESTED M361512. FOUND ASPSU IN MAINTENANCE CYCLE. RESET ASPSU CB 3WN AND TESTED ASPSU IAW MM 52-73-00-05. RESIDUAL PRESSURE WARNING SYSTEM ALL TESTED NORMAL. THIS CLEARS M361512. PLACARD REMOVED.

Part: WIRE HARNESS — UNKNOWN (OIL PRESSURE)

INSPECTION TYPE:N/A ATB - IFSD - NR 2 ENGINE SHUT DOWN TO LOW OIL PRESSURE. *S/D* REMOVED AND REPLACED OIL PRESSURE TRANSMITTER HARNESS, WIRES 072057, 072056, 072055 FROM CONNECTOR DT583 & D4952P REF P&W CMM 71-51-01. REF LP 651061 REMOVED AND REPLACED NR 2 OIL PRESSURE REGULATOR VALVE IAW MM 79-21-04-04.

Part: INDICATOR — FLUCTUATES (COCKPIT)

INSPECTION TYPE:N/A DURING CLIMBOUT RIGHT ENGINE OIL PRESSURE INDICATION WENT TO XX ON BOTH ECAM & GAUGE, AFTER A COUPLE OF MINUTES INDICATION CAME BACK BUT WAS FLUCUATING, CREW REDUCED ENGINE POWER BUT DID NOT SHUTDOWN ENGINE, ON DESCENT EVERYTHING RETURNED TO NORMAL. VERIFIED INTEGRITY OF WIRING FROM XMTR TO IND. REMOVED AND REPLACED PRESS XMTR IAW 79-33-11-04. REMOVED AND REPLACED COCKPIT IND IAW 79-33-21-04 ON TECH SERVICE RECOMMENDATION PRECAUTIONARY. RAN ENG AT VARIOUS PWR SETTINGS. OIL PRESSURE IND ON DUAL INDICTOR & ECAM NORMAL. OK FOR CONTINUED SERVICE.

Part: FLOOR PANEL — PUNCTURED (MAIN CARGO BAY)

INSPECTION TYPE:N/A MAIN CARGO DECK FLOOR PANEL BETWEEN 10R AT 11R PUNCTURED 1 INCH. ACCOMPLISHED PERMANENT REPAIR PER SRM 53-10-20. OPS CHECK OK.

Part: SMOKE DETECTOR — INOPERATIVE

TURNING BASE, LEG TO BUD AIRPORT, RW31L MASTER CAUTION AND ECAM SMOKE, AVIONICS IND ILLUMINATED, A/C LANDED ASAP. AVIONICS SMOKE PROCEDURE ACCOMPLISHED. INDICATION CONTINUES INTERMITTENTLY. EMERGENCY DECLARED T/S PERFORMED IAW TSM 26-15-00 PG 101 FIG 102. COCKPIT DUCT SMOKE DETECTOR 13WA REPLACED IAW AMM 26-15-12-04 PG 1-4, TEST PERF IAW 26-15-00-05 PG 1-2, FOUND OK, P/N ON: CGDU2000-00, S/N ON: 1347.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

FOUND LAV EMERG LIGHT INOP. RELAMPED WORKED OK.

Part: CONNECTOR — NOT SEATED (ESCAPE SLIDE)

RED WARNINGS LIGHT ON ESCAPE SLIDE DOES NOT ILLUMINATE WHEN TEST BUTTON IS DEPRESSED. RESEATED CONNECTOR ON THE ASPSU. WARNING LIGHT AND BUZZER OP CKS GOOD. OK FOR CONTINUED SERVICE

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 4,879 hrs · 2,986 cycles

INSPECTION TYPE:5YR, NR 1 ENG STRINGER FAIRING, 2ND STIFFENER FWD FROM TRAILING EDGE, OUTBD SIDE IS CRACKED THROUGH RIVET AT BOTTOM END. REMOVED & REPLACED STIFFENER PER A300 SRM 51-40-00.

Part: BRACKET — CRACKED (BS 3354 BL0) · airframe 4,879 hrs · 2,986 cycles

AFT CARGO FWD BULKHEAD SUPPORT BRACKET CRACKED STA 3354 CTR. REMOVED AND REPLACED BRACKET PER A300 SRM 51-40-00.

Part: BRACKET — CRACKED (BS 3354 LBL40) · airframe 4,879 hrs · 2,986 cycles

AFT CARGO FWD BULKHEAD SUPPORT BRACKET CRACKED STA 3354. REMOVED AND REPLACED BRACKET PER A300 SRM 51-40-00.

Part: SUPPORT ANGLE — CRACKED (NR 2 PYLON) · airframe 4,879 hrs · 2,986 cycles

INSPECTION TYPE:5YR, NR 2 PYLON LOWER AFT OTBD SUPPORT ANGLE CRACKED AT JOGGLE INTERIOR SIDE. REMOVED AND REPLACED SUPPORT ANGLE PER A300 SRM 51-40-21.

Part: STRUCTURE — CRACKED (NR 1 PYLON) · airframe 4,879 hrs · 2,986 cycles

INSPECTION TYPE:5YR, NR 1 ENG AFT LOWER PYLON MEMBER SECTION IS CRACKED AT THRU HOLE FOR PNEUMATIC LINE. REMOVED AND REPLACED MEMBER SECTION PER A300 SRM 51-40-21.

Part: SUPPORT ANGLE — CRACKED (NR 2 PYLON) · airframe 4,879 hrs · 2,986 cycles

INSPECTION TYPE:5YR, NR 2 PYLON LOWER AFT INBD SUPPORT ANGLE CRACKED AT JOGGLE INTERIOR SIDE. REMOVED AND REPLACED SUPPORT ANGLE PER A300 SRM 51-40-21.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 4,879 hrs · 2,986 cycles

INSPECTION TYPE:5YR, NR 1 ENG AFT PYLON OTBD MEMBER SECTION ANGLE IS CRACKED AT JOGGLE. REMOVED AND REPLACED ANGLE PER A300 SRM 51-40-21.

Part: SUPPORT — CRACKED (NR 2 PYLON) · airframe 4,879 hrs · 2,986 cycles

INSPECTION TYPE:5YR, NR 2 PYLON LOWER AFT END SUPPORT MEMBER CRACKED AT INBD SIDE JUST ABOVE GANG DRAIN EXIT OF PYLON. REMOVED AND REPLACED MEMBER PER A300 SRM 51-40-21 AND 51-40-00.

Part: RIB — CRACKED (LT WING) · airframe 4,879 hrs · 2,986 cycles

INSPECTION TYPE:5YR LT WING KRUEGER BOX AREA CURVED DOUBLER ON 2ND RIB FROM FUSELAGE HAS A CRACK. REMOVED AND REPLACED DOUBLER PER A300 SRM 51-40-00.

Part: RIB — CRACKED (KRUEGER FLAP) · airframe 4,879 hrs · 2,986 cycles

RT WING KRUEGER FLAP WELL HAS RIB CRACKED APPROX 1.5" IN LOWER RADIUS. REMOVED AND REPLACED RIB PER A300 SRM 51-40-00.

Part: SHEAR PLATE — CRACKED (FR79 LBL64 STR25) · airframe 4,879 hrs · 2,986 cycles

LT AFT MAIN CARGO COMPT FS 79 LBL64.00 SHEAR PLATE CRACKED 1.5"L AT FWD INBD AREA AT LIGHTENING HOLE AT STR 25. REMOVED AND REPLACED SHEAR PLATE PER A300 SRM 51-40-21.

Part: SHEAR PLATE — CRACKED (FR79 RBL64 STR25) · airframe 4,879 hrs · 2,986 cycles

INSPECTION TYPE:5YR RT AFT MAIN CARGO COMPT FS 79 RBL64.00 SHEAR PLATE CRACKED 1.5" LONG AT INBD FWD AREA AT LIGHTENING HOLE AT STR 25R. REMOVED AND REPLACED SHEAR PLATE PER A300 SRM 51-40-21.

Part: SMOKE DETECTOR — INTERMITTENT (E/E BAY)

INSPECTION TYPE:N/A AVIONICS SMOKE INTERMITTENTLY. REMOVED AND REPLACED MAIN BAY SMOKE DETECTOR 11 IAW 26-15-124, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS, DISARM LIGHT INOP. REPLACED DISARM LIGHT ASSY IAW ESPM 20-45-11. OPS CHECK GOOD.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 1,999 hrs · 1,278 cycles

INSPECTION TYPE: C1, LT WING INBD FLAP TOP SURFACE IS GOUGED OUTBOARD END, BLENDED AREA IAW A300 SRM 57-50-00. ORIGINAL THICKNESS OF .032 REMAINING MATERIAL .025 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE IAW A300 SRM 51-50-00 INSTALLED REPAIR DOUBLER IAW A300 SRM 51-21-00 & 51-40-40.