N125UP

Part: SPCC — FAULTED (SLAT SYS) · airframe 29,102 hrs · 17,992 cycles

DURING APPROACH, RECEIVED SLAT SYS 1+2 FAULT. RAN QRH AND ECAM. INITIALLY PLANNED <15 SLAT WITH 40 FLAP LANDING. WHEN WE SELECTED FLAPS 30/40, SYS 1 SELF CORRECTED, SLATS DEPLOYED TO APPROX 30 THEN. REF T3F18E007Y8MD REMOVED AND REPLACED #2 SFCC PER AMM 27-51-18/401. OPS CHECK GOOD. NO FAULTS NOTED ON EITHER SFCC #1 OR #2. OPERATED FLAPS AND SLATS FULL TRAVEL SEVERAL TIMES, NO FAULTS NOTED.

Part: LIGHT — DETACHED (ZONE 800) · airframe 28,355 hrs · 17,540 cycles

PASSENGER/CREW DOOR WARNING LIGHT ASSY HANGING OUT OF DOOR LINER. SECURED PASSENGER/CREW DOOR WARNING LIGHT HOUSING IAW AMM 52-73-11. OPS CHECK GOOD.

Part: SUPPORT ANGLE — DEFORMED (ZONE 400) · airframe 28,285 hrs · 17,493 cycles

NR 2 PYLON FWD FAIRING LH AND RH SIDE SUPPORT ANGLES DEFORMED FWD OF RIB 4A. DOT# 110-99 JP-110. ACCOMPLISHED E.A.#: 300-5452-27-A3926, PRELIMINARY 6, STEP #38: INSTALLED IAW DRAWING A54612175 AND SRM 51-40-21.

Part: SKIN — DEFORMED (ZONE 400) · airframe 28,285 hrs · 17,493 cycles

NR 2 PYLON FWD FAIRING LH AND RH SIDE SUPPORT ANGLES (P/N A54612200200/201)DEFORMED FWD OF RIB J4. DOT# 110-99 JP-110

Part: SKIN — DEFORMED (ZONE 400) · airframe 28,285 hrs · 17,493 cycles

#2 PYLON FWD FAIRING LH AND RH SIDE SUPPORT ANGLES (P/N A54612232200/201)DEFORMED FWD OF RIB J4. DOT# 110-99 JP-110 VERIFIED REMOVAL OF 2 EA SUPPORT ANGLES IAW-A300-SRM-51-40-21

Part: SUPPORT ANGLE — DEFORMED (ZONE 400) · airframe 28,317 hrs · 17,509 cycles

NUMBER 2 PYLON FWD FAIRING LH AND RH SIDE SUPPORT ANGLES (P/N A54612232200/201)DEFORMED FWD OF RIB 4A. DOT# 110-99 JP-110 REFORMED AREA AT #2 PYLON FWD FAIRING L/H AND R/H SIDE SUPPORT ANGLES P/N A54612232200/201 FWD OF RIB 4A IAW SREO-41097-C. AND EA 3005452-27-A3926 STEP 37 PRELIM 6. ACCOMPLISHED EA 300-5452-27-A3926 STEP 39 PRELIM 6: INSTALL REFORMED 2 EACH SHEET METAL FOLDED P/N: A54612232200/201 PER AIRBUS DRAWING A54612175, A54612197 AND SRM 51-40-21.

Part: SKIN — WRINKLED (ZONE 400) · airframe 28,285 hrs · 17,493 cycles

#1 ENGINE NACELLE FORWARD SKIN PANEL WRINKLED AT RIB J1 VERIFIED ACCOMPLISHMENT OF EA #300-5452-27-A3925 PRELIMINARY 3 STEPS 20, 21 AND 22<BR>NO DISCREPANCIES NOTED AT THIS TIME.

Part: SKIN — WRINKLED (ZONE 400) · airframe 28,317 hrs · 17,509 cycles

NUMBER 2 ENGINE NACELLE FORWARD SKIN PANEL WRINKLED THE CURRENT CONFIGURATION OF AIRCRAFT AND PYLON: ENGINE REMOVED, DAMAGED SKIN REMOVED,DAMAGED LH AND RH SIDE SUPPORT ANGLES REMOVED (ITEM 170 ON SRM 54-52-11 FIG 1)ACCOMPLISHED STEP 5 OF EA: 300-5452-27-A3926.

Part: SKIN — WRINKLED (ZONE 400) · airframe 28,285 hrs · 17,493 cycles

#2 ENGINE NACELLE FORWARD SKIN PANEL WRINKLED VERIFIED ACCOMPLISHMENT OF STEP 17 PER EA: 300-5452-27-A3926 PRELIMINARY 3.<BR>VALIDATED DVI INSPECTION ON PYLON PRIMARY STRUCTURE, NO DAMAGE FOUND.

Part: SKIN — WRINKLED (ZONE 400) · airframe 28,320 hrs · 17,511 cycles

NR 1 ENGINE NACELLE FORWARD SKIN PANEL WRINKLED AT RIB J1 ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-93897-REQ1 AND VT-MAE EA 300-5452-27-A3925 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: SKIN — CRACKED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

TWO CRACKS FOUND INSIDE HOLE T ON FR47 RH HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93655-REQ1 REV. 2 AND EA 300-5710-27-A3905 REV. A. 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: SKIN — CRACKED (ZONE 100) · airframe 28,285 hrs · 17,493 cycles

CRACK FOUND IN FASTENER HOLE ON BULK CARGO DOOR SCUFF PLATE. AREA MARKED IN RED. ACCOMPLISHED E.A.#: 300-5317-27-A3915, PRELIMINARY 1, STEP# 2: "INCREMENTALLY REAM THE 1 EACH CRACKED HOLE IN STEPS OF 0.4 MM UNTIL DAMAGE FREE AND ROUND CONDITION ACHIEVED OR MAX DIAMETER 0.326 INCH. SEE FIGURE 1 FOR LOCATION". INCREMENT REAM, HOLE WAS REAMED: 0.279"

Part: SKIN — CRACKED (ZONE 100) · airframe 28,285 hrs · 17,493 cycles

CRACK FOUND IN HOLE T ON FR47 LH HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93642-REQ1 AND EA 300-5710-27-A3893 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: SKIN — CRACKED (ZONE 100) · airframe 28,285 hrs · 17,493 cycles

CRACK FOUND IN HOLE S ON RH FR47 HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93655-REQ1 REV. 2 AND EA 300-5710-27-A3905 REV. A. 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: SKIN — CRACKED (ZONE 100) · airframe 28,285 hrs · 17,493 cycles

CRACK FOUND IN HOLE G ON RH FR47 HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93655-REQ1 REV. 2 AND EA 300-5710-27-A3905 REV. A. 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: SKIN — CRACKED (ZONE 100) · airframe 28,285 hrs · 17,493 cycles

CRACK FOUND IN HOLE C ON RH FR47 HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93655-REQ1 REV. 2 AND EA 300-5710-27-A3905 REV. A. 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: BRACKET — CRACKED (ZONE 300) · airframe 28,285 hrs · 17,493 cycles

LH HORIZONTAL STAB LEADING EDGE APRON SUPPORT BRACKET P/N: A5517155120451 BROKEN. INSTALLATION OF NEW BRACKET P/N: A5517155120451, B/N:0004388210 IAW A300-600F SRM 51-40-21. FASTENERS USED: FOUR HI-LOKS P/N HL10VF6-6, BATCH #0004358134 AND FOUR COLLARS P/N NSA5075-6, BATCH #0004291986.

Part: SKIN — CRACKED (ZONE 100) · airframe 28,285 hrs · 17,493 cycles

TWO CRACKS FOUND IN HOLE A ON RH FR47 HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93655-REQ1 REV. 2 AND EA 300-5710-27-A3905 REV. A. 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: SKIN — CRACKED (ZONE 100) · airframe 28,285 hrs · 17,493 cycles

CRACK FOUND IN HOLE E ON RH FR47 HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93655-REQ1 REV. 2 AND EA 300-5710-27-A3905 REV. A. 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: DOOR FRAME — GOUGED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

CREW DOOR, AFT FRAME (FR16.1) MECHANISM LOCK FITTING HAS GOUGE.

Part: DOOR FRAME — GOUGED (ZONE 200) · airframe 28,317 hrs · 17,509 cycles

CREW DOOR, AFT FRAME (FR16.1) MECHANISM LOCK FITTING HAS GOUGE. DOT 103-62 (ATTACHED PHOTO) REMOVED MINOR GOUGE AT LOCK FITTING IAW SRM A300-600 51-73-11 MATERIAL THIKNESS IS 1.100" AND MATERIAL LOSS 0.003 AND REMAINING THIKNESS IS 1.197" THERE IS WHTIN IN LIMITS IAW SRM 51-73-11 T98826 C18-C02 AND RESTORE SURFACE PROTECTION.

Part: SUPPORT BRACKET — GOUGED (ZONE 800) · airframe 28,285 hrs · 17,493 cycles

CREW DOOR, INNER SURFACE, UPPER SIDE, BRACKET SUPPORT AT AFT LOCK HOLE HAS GOUGE.

Part: LOCK — DAMAGED (ZONE 800) · airframe 28,317 hrs · 17,509 cycles

CREW DOOR, INNER SURFACE, UPPER SIDE, BRACKET SUPPORT AT AFT LOCK HOLE HAS GOUGE. DOT 103-64 (ATTACHED PHOTO) REMOVED MINOR GAUGE IAW SRM A300-600 51-73-11 MATERIAL LOSS 0.002 WITHIN LIMITS IAW SRM 51-73-11. T988826 C18-C02 OK TO RESTORE SURFACE PROTECTION. APPLIED SURFACE PROTECTION AT BRACKET SUPPORT IAW SRM 51-21-10 PN ALODINE 1132 BATCH 0004333328 AND PRIMER PN 10-P4-2/2TU BATCH 0004341754 PAINT PN ECL-G-101 BATCH 4321170 AND PAINT CUP 02-012-C70.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

MDC FLOOR PANEL 231KJ IS DAMAGED AND BROKEN. FABRICATED MAIN DECK FLOOR PANEL 231KJ IAW SREO-16407-REQ001.

Part: BRACKET — GOUGED (ZONE 500) · airframe 28,285 hrs · 17,493 cycles

LH WING, UPPER SURFACE, ATTACHMENT WTB FAIRIG AREA, BRACKET SUPPORT HAS GOUGE (2EA). DOT 103-34 (ATTACHED PHOTO). NSTALLED NEW BRACKET IAW A300-600 SRM 51-40-21. RIVET P/N: CR3213-6-03 BATCH: 0004194656, HI-LOCK P/N: DAN5-6-6 BATCH: 0004178101, COLLAR P/N: NSA5075-6 BATCH: 0004291986, SEALANT P/N: 04-001-0109 BATCH: 0004371367. REVIEWED

Part: CROSSBEAM — BENT (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

MAIN DECK CROSSBEAM AT FR 48 BETWEEN -Y450 AND -Y953 BENT.DOT# 110-61 JP-110. INSTALLED NEW CROSSBEM I.A.W A300-600 SREO 75878-REQ001.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

MDC FLOOR STRUCTURE RH SIDE FR38.1 SUPPORT (DOG BONE) CRACKED. DOT 11-056 THE SPARE PART IS CONSUMABLE AND DOES NOT HAVE A UPS PARTS TAG. (SEE ATTACHMENT).

Part: FRAME — CRACKED · airframe 28,285 hrs · 17,493 cycles

CRACK FOUND IN HOLE G ON FR47 LH HORIZONTAL JUNCTION. COMPLIED WITH STEP 15 OF PRELIM 1 EA-300-5710-27-A3893.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

MDC FLOOR STRUCTURE RH SIDE FR38.2 SUPPORT (DOG BONE) CRACKED.

Part: CROSSBEAM — BENT (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

MAIN DECK CROSSBEAM AT FR 49 BETWEEN -Y450 AND -Y953 BENT. DOT# 110-62 JP-110. INSTALLED NEW CROSSBEM I.A.W A300-600 SREO 75878-REQ001. REVIEWED

Part: ADAPTER — CORRODED (ZON E200) · airframe 28,285 hrs · 17,493 cycles

MDC FLOOR STRUCTURE FR58/Y-0 UNDER FLOOR PANEL 251FM CLS ADAPTER CORRODED. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-93740-REQ1 AND VT-MAE EA 300-5316-27-A3909 REV. - .

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

FAULT: STR-Z200 MDC FLOOR STRUCTURE UNDER FLOOR PANEL 262FM FR80/-Y794.3 SEAT TRACK CORRODED. DOT 11-024.REMOVED CORROSION ON SEAT TRACK AT FR 80/-Y953 IAW A300-600F SRM 51-74-10.REMOVED SEAT TRACK AT MDC FLOOR STRUCTURE UNDER FLOOR PANEL 262FM FR80/-Y794.3, IAW A300-600-SRM-53-10-16 FIG 201.FABRICATED NEW SEAT TRACK P/N R5307007120600, IAW A300-600 SRM 53-10-16-201 PAG 207/208. REQUEST OK TO LOCATE AND DRILL.INSTALLED SEAT TRACK SPLICE AT MDC FLOOR STRUCTURE UNDER FLOOR PANEL 262FM FR80/-Y794.3, IAW A300-600 SRM 53-10-16-201 PAG 207/208.INSTALLED SEAT TRACK AT MDC FLOOR STRUCTURE UNDER FLOOR PANEL 262FM FR80/-Y794.3, IAW A300-600 SRM 53-10-16-201 PAG 207/208.

Part: ADAPTER — CORRODED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

MDC ON PANEL 251 WG ADAPTER CLS WITH CORROSION.

Part: ADAPTER — CORRODED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

MDC FR57.1/Y-0 UNDER FLOOR PANEL 252LG CLS ADAPTER CORRODED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

MDC FLOOR, SEAT TRACK IN Y450 ON PANEL 251VF HAVE CORROSION DOT 07-116 VERIFIED INSTALLATION OF NEW SEAT TRACK SECTION IN Y450 BETWEEN FR63 AND FR66 IAW SRM 53-10-16 PARAGRAPH 4 FIGURE 201 PAGE 207/208 AND SRM 51-40-21 . OPEN

Part: ADAPTER — CORRODED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

MDC FLOOR PANEL 251WG FWD ADAPTER CLS WITH CORROSION .

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

MDC FLOOR STRUCTURE FR79/-Y450 UNDER FLOOR PANEL 262EM SEAT TRACK CORRODED. DOT 11-023. VERIFIED REMOVAL OF CORROSION ON SEAT TRACK IAW A300-600F SRM 51-74-10. ORIGINAL MATERIAL THICKNESS .535", MATERIAL LOSS .021", MATERIAL LEFT .514". THE LOSS IS IN LIMITS IAW A300-600F SRM53-10-16.

Part: PROFILE — CRACKED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

**SDR FILED OPEN**FAULT: STR-Z200 MDC FLOOR STRUCTURE FR79 RH SIDE FLOOR PANEL 262AH PROFILE CRACKED. DOT 11-026 VERIFIED INSTALLATION OF MDC FLOOR IN FR79 RH Z PROFILE IAW A300-600F SRM 51-40-21. MATERIALS USED: SEALANT P/N 04-001-0109, BATCH #0004371367, SOLID RIVETS 36 EACH P/N NAS1097AD5-8, BATCH # 0004367320.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

MDC FLOOR PANEL 251FM BROKEN. DOT 11-040 REVIEWED

Part: PROFILE — CRACKED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

**SDR FILED OPEN**FAULT-STR-Z200-MDC FLOOR IN C65 LH Z PROFILE HAVE A CRACK DOT 07-119 VERIFIED INSTALLATION OF MDC FLOOR IN C65 LH Z PROFILE IAW A300-600F SRM 51-40-21. MATERIALS USED: SEALANT P/N 04-001-0109, BATCH #0004371367, SOLID RIVETS 36 EACH P/N NAS1097AD5-8, BATCH # 0004367320.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

MDC FLOOR STRUCTURE FR79 RH SIDE FLOOR PANEL 262AH PROFILE CRACKED. DOT 11-026. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-93576-REQ1 AND VT-MAE EA 300-5318-27-A3917, REV. -.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

MDC FLOOR STRUCTURE FR79/Y0 UNDER FLOOR PANEL 261EM SEAT TRACK CORRODED.

Part: SUPPORT — CRACKED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

FLOOR STRUCTURE RH SIDE BETWEEN FR73/74 WEB SUPPORT UNDER SURFACE CRACKED. DOT 11-030.REMOVED SUPPORT UNDER MDC FLOOR STRUCTURE RH SIDE BETWEEN FR73/74 IAW A300-600 SRM 51-40-21.TREATED AND PRIMED NEW PART SHEAR WED IAW A300-600 SRM 51-21-10. APPLIED TOPCOAT NEW PART SHEAR WED IAW A300-600 SRM 51-23-10. INSTALLED WEB SUPPORT ON MDC FLOOR STRUCTURE BETWEEN FR 73-74 RH SIDE IAW SRM 51-40-21 AND A300-600F SRM 51-72-10.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

MDC COMPARTMENT AFT AREA FLOOR PANEL 261HM HAS A SUPPORT CRACKED. DOT 11-020. REMOVED AND REPLACED FLOOR SUPPORT ANGLE (PROFILE) FRAME 80 RH PNL 261 HM IAW A300-600 SRM 51-40-21. ANGLE P/N: A5398140120000 BATCH:0004390460. RIVETS P/N: MS20470AD5-5 .BATCH:0004379716.

Part: WEB — CRACKED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

MDC, BETWEEN FR74 AND FR73, LH SIDE, UNDER FLOOR STRUCTURE FRAME HAS A CRACK BETWEEN 2 RIVETS. DOT 23-003 VERIFIED INSTALL STEP 15

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

MDC, BETWEEN FR 78 AND FR 77, LH SIDE, FLOOR STRUCTURE FRAME HAS 2EA CRACKS. DOT 23-002. NEW WEB HAS BEEN INSTALLED IAW A300-600 SRM 51-40-21 AND ALSO THE INTERFAY SEALING HAVE BEEN RESTORED BETWEEN THE SURFACES IAW A300-600 SRM 51-76-10. MATERIALS USED: SEALING P/N:04-001-0109 BATCH# 0004371367 PROTUDING RIVET P/N: MS20470AD5-5 BATCH#0004369861 FLUSH RIVET P/N: MS20426D5-7 BATCH#0004361439. REQUEST OK TO RESTORE TOPCOAT ON THE RIVET'S HEADS. APPROVED

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

FAULT-INTERIORS-ZONE200-MAIN CABIN: FLOORBOARD 241ZH BROKEN. DOT NO. 17-27.FABRICATED MDC FLOOR PANEL 241ZH I.A.W. SREO-16407-REQ001, MATERIAL USED P/N: 5024N400001SS-G BTCH:0004055277, PAINT P/N:34655-526A-RS65 BTCH:0004326906.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

-MDC, BETWEEN FR 78 AND FR 77, LH SIDE, FLOOR STRUCTURE FRAME HAS 2EA CRACKS. DOT 23-002 SDR COMPLETED

Part: FRAME — CRACKED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

MDC, BETWEEN FR74 AND FR73, LH SIDE, UNDER FLOOR STRUCTURE FRAME HAS A CRACK BETWEEN 2 RIVETS. INSTALLED NEW SHEAR WEB I.A.W A300-600 SRM 51-40-21.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

FAULT-COMP-Z200-MDC FLOOR PANEL 261JM IS BROKEN. DOT 23-006. VERIFIED FABRICATION OF MDC FLOOR PANEL 261JM I.A.W. SREO-16407-REQ001, MATERIAL USED P/N: 5024N400001SS-G BTCH:0004055277, PAINT P/N: 34655-526A-RS65 BTCH: 0004326906, CUP#: 02-012-176, PLUG P/N:G2001B-3P BTCH:0004365510, INSERT P/N: G2002A-3S BTCH: 0004370926. REVIEWED

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 28,285 hrs · 17,493 cycles

**SDR FILED OPEN** MDC COMPARTMENT AFT AREA FLOOR PANEL 261HM HAS A SUPPORT CRACKED. DOT 11-020 VERIFIED REMOVAL/ REPLACEMENT OF FLOOR SUPPORT ANGLE (PROFILE) FRAME 80 RH PNL 261 HM

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

FAULT-STR-Z200-MDC FLOOR STRUCTURE, BETWEEN FR 79 AND FR 78, BEHIND PANEL 261AH, HAS A STRUCTURE DRILLED OUT. DOT 23-001.PERFORMED CUTOUT OF OUTBOARD FLANGE BETWEEN FR 78 AND FR 79 AT TRACK Y1580. MEASURES 1.90" WIDE BY .900" INBOARD IAW A300-600-SRM-53-10-16 FIG 202.LOCATED AND DRILLED REPAIR ANGLE AND FILLER IAW A300-600-SRM-51-40-44, TRIMED TO FIT REPAIR PARTS IAW A300-600-SRM-53-10-16 FIG 202.TREATED AND PRIMED REPAIR PARTS USING PRIMER P/N 10-P4-2/2TU B# 0004341753 IAW A300-600-SRM-51-21-10.INSTALLED ANGEL REPAIR AND FILLER REPAIR IAW A300-600-SRM-53-10-16 FIG 202.

Part: RIB — CRACKED (ZONE 600 FLAP) · airframe 28,285 hrs · 17,493 cycles

R/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 27A HAS (2) CRACK INDICATION AND HAS BEEN MARKED IN RED. INSTALLED NEW ANGLE FOR R/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 27 FLANGER REPAIR BETWEEN STRINGER 2.6 AND STRINGER 2.7 AND 2.8 AND REAR SPART IAW A300-600 SRM 57-50-00 (PARAGRAPH 4A OR 4B (FIGURE 201 RESPECTIVELY 202). E.A#: 300-5750-27-A3892, PRELIMINARY 1. FASTENER P/N: CR3212-4-02, BATCH# 0004373520, P/N: CR3213-4-02(20), BATCH# 0004388028,

Part: RIB — CRACKED (ZONE 600) · airframe 28,285 hrs · 17,493 cycles

SDR FILED OPEN. R/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 27F HAS (1) CRACK INDICATION AND HAS BEEN MARKED IN READ. VERIFIED SERVICE DIFFICULTY REPORT HAS BEEN INITIATED.COMPLIED WITH STEP 20 OF E.A 300-5750-27-A3892 PRELIMINRY 1.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

FLOOR SUPPORT AT Y1456, FR11 TO FR15A CORRODED AT MANY LOCATIONS DOT# 110-34 JP-110. INSTALLED NEW FLOOR SUPPORT PART NUMBER BAC1505-100590 IAW SRM 51-40-21, MATERIAL INFO: SEALANT PS870-B1/2, BATCH NUMBER 0004371367, HI-LOKS PART NUMBER EN6115K3-4,BATCH NUMBER 0004084645 QTY 10EA , RIVETS PART NUMBER MS20470AD6-10, BATCH NUMBER 0004201341, QTY 0.40LB.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

FLOOR SUPPORT AT Y953, FR11 TO FR15A CORRODED AT MANY LOCATIONS DOT# 110-33 JP-110 VERIFIED INSTALLATION OF NEW FLOOR SUPPORT PART NUMBER BAC1505-100590, BATCH NUMBER 0004389085 IAW SRM51-40-21, MATERIAL INFO: SEALANT PS870-B1/2, BATCH NUMBER 0004371367, COLLAR NSA5075-6, BATCH NUMBER 0004291986, QTY 200EA,, RIVETS PART NUMBER MS20470AD5-5, BATCH NUMBER 0004361891, QTY O.40LB, HI-LOKS PART NUMBER HL10VF6-6, QTY 30EA.

Part: RIB — CRACKED (ZONE 600) · airframe 28,285 hrs · 17,493 cycles

R/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 26A HAS (1) CRACK INDICATION AND HAS BEEN MARKED IN READ. VERIFIED SERVICE DIFFICULTY REPORT HAS BEEN INITIATED.COMPLIED WITH STEP 20 OF E.A 300-5750-27-A3892 PRELIMINRY 1. OPEN

Part: RIB — CRACKED (ZONE 600) · airframe 28,285 hrs · 17,493 cycles

R/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 27A HAS (2) CRACK INDICATION AND HAS BEEN MARKED IN RED. VERIFIED SERVICE DIFFICULTY REPORT HAS BEEN INITIATED.COMPLIED WITH STEP 20 OF E.A 300-5750-27-A3892 PRELIMINRY 1. OPEN

Part: RIB — CRACKED (ZONE 500 FLAP) · airframe 28,285 hrs · 17,493 cycles

**SUPPLEMENTAL SDR** FAULT: L/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 27A HAS (1) CRACK INDICATION AND HAS BEEN MARKED IN RED. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-93428-REQ1 AND VT-MAE EA 300-5750-27-A3891, REV. -. REVIEWED

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

FLOOR SUPPORT AT Y730, FR11 TO FR14 CORRODED AT MANY LOCATIONS

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

FLOOR SUPPORT AT Y1959, FR12A TO FR17 CORRODED AT MANY LOCATIONS DOT# 110-35 JP-110. NSTALLED NEW FLOOR SUPPORT PART NUMBER A53613033212, BATCH NUMBER 0004389085, SEALANT PART NUMBER PS870-B1/2, BATCH NUMBER 4371367, IAW SRM 51-40-21.

Part: RIB — CRACKED (ZONE 500 FLAP) · airframe 28,285 hrs · 17,493 cycles

L/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 26A HAS (1) CRACK INDICATION AND HAS BEEN MARKED IN RED. ACCOMPLISHED WHIT E.A 300-5750-27-A3891 PRELIMINRY 1 AND INSTALLED DOUBLER AT CENTER FLAP LH IN ACCORDANCE WHIT SRM 57-50-00 AND MATERIAL USED 2024T3 0.056 AND ALODINE 1132 BATCH 000433328 AND PRIMER PN 02-013-8 BATCH 4271767 AND PAINT CUP CCAS-LM3 AND RIVET USED PN CR3212-5-03 BATCH 0004318529 AND ACCORDANCE WHIT A300-600 SRM 51-40-21.

Part: RIB — CRACKED (ZONE 600 FLAP) · airframe 28,285 hrs · 17,493 cycles

R/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 26A HAS (1) CRACK INDICATION AND HAS BEEN MARKED IN READ. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-93431-REQ1 AND VT-MAE EA 300-5750-27-A3892, REV. -. REVIEWED

Part: RIB — CRACKED (ZONE 500) · airframe 28,285 hrs · 17,493 cycles

L/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 26A HAS (1) CRACK INDICATION AND HAS BEEN MARKED IN RED. VERIFIED SERVICE DIFFICULTY REPORT HAS BEEN INITIATED. COMPLIED WITH STEP 20 OF E.A 300-5750-27-A3891 PRELIMINRY 1. OPEN

Part: RIB — CRACKED (ZONE 500) · airframe 28,285 hrs · 17,493 cycles

L/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 27A HAS (1) CRACK INDICATION AND HAS BEEN MARKED IN RED. VERIFIED SERVICE DIFFICULTY REPORT HAS BEEN INITIATED. COMPLIED WITH STEP 20 OF E.A 300-5750-27-A3891 PRELIMINRY 1. OPEN

Part: STIFFENER — CORRODED (ZONE 400) · airframe 28,285 hrs · 17,493 cycles

#1 PYLON INTERNAL LOWER SPAR, LIGHT SURFACE CORROSION, AS SEEN THROUGH SIDE PANEL# 415AL

Part: CEILING PANEL — CRACKED (ZONE 200) · airframe 28,285 hrs · 17,493 cycles

*** SDR FILED OPEN *** FAULT-STR-ZONE 100-FWD CARGO 132LC HAS 3 DENTS AROUND 3 HOLES-DOT 109-94 VWV 5430 AUDIT COMPLETED

Part: WEB — CRACKED (ZONE 600 LE) · airframe 28,285 hrs · 17,493 cycles

RT WING INBD LEADING EDGE WEB CRACKED NEAR RIB 2.

Part: WARNING HORN — NO TEST (ZONE 700) · airframe 28,285 hrs · 17,493 cycles

NOSE LANDING GEAR HORN FAILS TO ACTIVATE WHEN PERFORMING OPS TEST OF OVERBOARD VALVE FAULT WARNING APPROVED.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 28,256 hrs · 17,481 cycles

LAVATORY EMERGENCY LIGHT INOPERATIVE RELAMPED OPERATING NORMALLY OK FOR SERVICE REF 33-51-00

Part: INDICATION SYS — MALFUNCTIONED (ENGINE OIL) · airframe 28,195 hrs · 17,446 cycles

*DIVERSION* ENG 2/ENGINE ADV LOW OIL PRESSURE (CONDITION BOTH OIL PRESSURE GAUGE AND ECAM NOT CONFIRMED BY OIL PRESSURE LOCAL WARNING, R/R ENGINE #2 PRESURE INDICATOR PER AMM 79-33-21 OPS CHECK GOOD

Part: DOOR — DAMAGED (ZONE 800) · airframe 28,033 hrs · 17,349 cycles

LOAD REPORTS BUG NET ON K LOADER MADE CONTACT WITH THE MAIN CARGO DOOR.. UPON INSPECTION FOUND 5 OF 8 INDICATOR FLAGS DAMAGED. (FWD TO AFT 1,2,4,7,8). REPLACED DAMAGED LOCKING INDICATORS REF AMM 52-36-23/401. OSD: 2/5/2025

Part: LIFE VEST — MISSING (ZONE 200) · airframe 27,997 hrs · 17,332 cycles

COCKPIT OBSERVER/JUMPSEAT LIFE VEST IS NOT FOUND IN COCKPIT (FOUND MISSING ON PSM CHECK) PLACED NEW LIFE VEST INTO COCKPIT PER LOCATION DESCRIPTION LISTED IN THE A 300 PSM CHECK. MXP-PSM-025000-01-1-999-JIC. (FOR MAINTENIX PURPOSES REMOVED PART INFORMATION FOR MISSING LIFE VEST WAS DOCUMENTED DUE TO A REMOVED P/N AND S/N NEEDING TO BE ACCOUNTED FOR, FOR SIGNOFF: HOWEVER, CONFIRMED THIS VEST WAS NOT PHYSICALLY INSTALLED IN AIRCRAFT)

Part: SLIDE — OUT OF POSITION (ZONE 800) · airframe 27,795 hrs · 17,225 cycles

SLIDE LEVER WOULD NOT DISARM AFTER SEVERAL ATTEMPTS. LEVER WOULD 3/4 OF THE WAY AND €ŒSTICK€? MECHANIC JUMPSEATER WAS ABLE TO MANIPULATE THE SLIDE ENOUGH TO GET THE LEVER TO €ŒDISARM€? CLEANED AND LUBRICATED GIRT BAR SLIDERS AND FLOOR FITTINGS REF AMM 52-10-30. NO RII REQUIREMENTS PER GMM 04-02.

Part: PLUG — MISSING (DOOR HANDLE) · airframe 27,084 hrs · 16,831 cycles

CREW ENTRY DOOR EXTERNAL HANDLE MISSING PLUG. INSTALLED PLUG IAW AMM 52-10-20

Part: BOTTLE — LOW PRESSURE (DOOR) · airframe 26,645 hrs · 16,544 cycles

DOOR EMG. ASSIST PRESSURE LOW SERVICED ENRTRY DOOR EMERGENCY OPERATION CYLINDER PER AMM 52-10-14-301.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 26,522 hrs · 16,465 cycles

CABIN DOOR ACTUATOR PRESSURE IS LOW. SERVICED CABIN DOOR ACTUATOR IAW AMM 52-10-14

Part: A/C PACK — ODOR · airframe 26,233 hrs · 16,258 cycles

INSPECTION TYPE:NAAFTER T/O WE NOTICED A BURNING SMELL LIKE OIL COMING FROM THE GASPER VENTS FROM PACK1 / PACK2 DEFERRED NO SMOKE JUST ODOR SMELL WENT AWAY AROUND 5000'ACCOMPLISHED @2 ENG RUN W/R/T AMM 71-00-00-0201. RAN #1 PACK W/R/T AMM 21-51-00-0501. OPS GOOD NO ODORS OR SMELLS OF BURNING NOTED OK TO CONTINUE

Part: MECHANISM — LACK OF LUBE (DOOR ARMING) · airframe 25,504 hrs · 15,793 cycles

AFTER PARKING, DOOR SLIDE WOULD NOT DISARM. REMOVED FWD DOOR LINING MM 52-10-13-401, LUBRICATED SLIDE ARM MECHANISM IAW MM 52-10-30-601 SLIDE ARMS AND DISARMS WITH NO BINDING MM 25-61-20-601 (4).

Part: MECHANISM — LACK OF LUBE (DOOR ARMING) · airframe 25,503 hrs · 15,792 cycles

INSPECTION TYPE:NAAFTER PARKING DOOR SLIDE WOULD NOT DISARM, SEE PAGE 477510 AND 477516. DEFERRED MAIN ENTRY DOOR SLIDE PER MEL 52-11-01-2-3. M797137 CREATED, PLACARD INSTALLED DMP C.W. REMOVED FWD DOOR LINING MM 52-10-13-401 LUBED SLIDE ARM MECHANISM PER MM 52-10-30-601 SLIDE ARMS AND DISARMS WITH NO BINDING MM 25-61-20-601 (4)

Part: MECHANISM — LACK OF LUBE (ARMING HANDLE) · airframe 25,503 hrs · 15,792 cycles

INSPECTION TYPE:NAAFTER PARKING SLIDE ARM HANDLE WOULD NOT MOVE TO DISARM POSITIONLUBED SLIDE ARM MECHANISM PER MM 12-22-52-0001 OPS CHECK GOOD PER MM 52-10-30-601

Part: SLIDE CHANNEL — FOD (MAIN DOOR) · airframe 25,488 hrs · 15,784 cycles

MAIN DOOR WON'T DISARM, CYCLED DISARM/ARM LEVEL SERVERAL TIMES FOUND DEBRIS STUCK ON ARM SLIDES UNDER DOOR FOR ILLEG CLEANED DEBRIS OUT AND OPS CHECK GOOD. REF AMM A300 52-10-30

Part: LEVER — BINDING (PAX DOOR) · airframe 25,470 hrs · 15,774 cycles

AFTER BLOCKING - DOOR SLIDE LEVER TOOK SEVERAL ATTEMPTS TO DISARM, COULD NOT DUPLICATE. NO HISTORY. CHECK SYS IAW MM 25-61-20-0501 ADJ/TEST OPS CK OK. RTS. HISTORY STARTED

Part: DOOR — BINDING (L1) · airframe 25,351 hrs · 15,707 cycles

MAIN CABIN CREW ENTRY DOOR DIFFICULT TO CLOSE FROM THE INSIDE. PERFORMED INSPECT/CHECK OF LH CREW ENTRY DOOR IAW AMM 52-00-00. OPS CHECK GOOD

Part: PANEL — CORRODED (NACELLE) · airframe 25,338 hrs · 15,697 cycles

INSPECTION TYPE:SEG, PANEL 414ER HAS CORROSION AROUND SCREW HOLES.CUT OUT DAMAGE INSTALLED FILLER AND DOUBLER IAW SRM 54-52-51-FIG 201.

Part: PANEL — WORN (NR 2 NACELLE) · airframe 25,338 hrs · 15,697 cycles

INSPECTION TYPE:SEG#2 PYLON PANEL 423CL 2EA FASTENER HOLE CUT OUT WORN2EA AREAS WAS CUTOUT FILLERS AND A DOUBLER WAS INSTALLED IAW SRM 54-52-51 FIG 201

Part: DOOR — CORRODED (LAV SERVICING) · airframe 25,338 hrs · 15,697 cycles

INSPECTION TYPE:SEG, LOWER FWD EXTERNAL FUSE TOILET SERVICE PANEL 121DL HAS CORROSION INNER AND OUTER SURFACE.DOOR/PANEL WAS FOUND TO BE OUT OF LIMITS DOOR WAS REMOVED AND REPLACED IAW SRM 51-40-21

Part: PANEL — WORN (NR 2 NACELLE) · airframe 25,338 hrs · 15,697 cycles

INSPECTION TYPE:SEG, #2 PYLON PANEL 424CR 2EA FASTENER HOLE CUT OUT WORN2EA AREAS WAS CUTOUT FILLERS AND DOUBLER WAS INSTALLED IAW SRM 54-52-51 FIG 201

Part: FLAP — VIBRATION (CABIN) · airframe 25,169 hrs · 15,597 cycles

INSPECTION TYPE:N/A** ATB ** EMERGENCY DECLARED ** LANDED SUCCESSFULLY ** DURING CLIMBOUT ACCELERATING THRU 280 KIAS, ACFT BEGAN CONTINOUS VIBRATION UNTIL SPEED BELOW 280 KIAS. ALL INDICATIONS NORMAL. ATTEMPTED CLIMB AGAIN VIBRATION RESUMED.PERFORMED TROUBLESHOOTING PER TSM 05-50-00 FIG 101. PERFORMED PRESSURIZATION CHECK AMM 21-31-00 FOR MAIN CARGO, LOWER CARGO, AND CREW ENTRY DOOR SEALS. SUSPECT SEAL MIGHT NOT HAVE BEEN SEALED CORRECTLY IN FRAME IN FLT. CLEANED SEALS. PERFORMED VISUAL INSPECTIONS OF ALL CONTROL SURFACES, LANDING GEAR

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,746 hrs · 15,352 cycles

ON PREFLIGHT SLIDE ARMED LIGHT DOES NOT ILLUMINATE BUZZER WORKS. RESET C/B'S ACCOMPLISHED LIGHT CHECK W/R/T AMM 52-73-00-0501. OPS CHECK GOOD.

Part: HANDLE — INOPERATIVE (MLG) · airframe 23,906 hrs · 14,899 cycles

AIR TURNBACK ON DEPARTURE THE LANDING GEAR HANDLE WOULD ONLY MOVE TO THE UNLOCK POSITION. GEAR WOULD NOT RETRACT. WE RAN THE CHECKLIST AND PUT THE GEAR BACK IN THE DOWN POSITION. NO OTHER INDICATIONS THE #1 PITCH TRIM PADDLE ALSO KICKED OFF. WOULD NOTFOUND C/B 2GB-L/G PROX DET & RELAY SYS 1-BREAKER POPPED. SHORT TO GROUND OCCURING SOMEWHERE IN 104VU CENTER RELAY BOX. REMOVED ALL ASSOCIATED RELAYS TO TERMINAL BLOCK 158VT AND BREAKER STILL POPS, REQUIRES FURTHER T/S. PERF SHORT TO GROUND TEST REF ESPM 20-52-21 F. PERF LANDING GEAR EXT & RETRACTION IAW AMM 32-31-00-0501. OPS CK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (PAX DOOR) · airframe 23,612 hrs · 14,725 cycles

INSPECTION TYPE:NACABIN DOOR OPEN AND DOOR WARNING HORN ECOM INDICATION COME ON DURING CLIMB - NO PRESSURE LOSSPERFORMED TEST PER AMM 52-10-11-0501. DOS OPERATES SMOOTHLY AND DOOR EICAM MESSAGE. OPS CK GOOD. OK TO CONTINUE NO RECENT HISTORY

Part: SEAL — LEAKING (BLUE HYD PUMP) · airframe 22,977 hrs · 14,353 cycles

INSPECTION TYPE: NA, EMERGENCY DECLARED, NO EQUIPMENT USED. LANDING UNEVENTFUL. ON APPROACH, FLAPS 15/0 ECAM HYD BLUE RSVR LOW AIR PRESS, BLUE RSVR LOW LEVEL. BLUE QTY INDICATION LOW. REPLACED NR 1 ENGINE BLUE SYS HYD PUMP REAR DRIVE SEAL, PER AMM 72-65-07-0401. REPLACED BLUE SYSTEM ENGINE PUMP PRESS SWITCH AMM 29-12-62-401. REPLACED NR 1 ENGINE BLUE SYS HYD PUMP, PER AMM. LEAK & OPERATIONS CHECK NORMAL, AMM REF FOR PUMP 29-11-32-0401. IPC REF PW 29-11-01.

Part: WARNING LIGHT — INOPERATIVE (DOORS) · airframe 22,931 hrs · 14,326 cycles

INSPECTION TYPE: NA SDR FILED OPEN. CREW ENTRY DOOR WARNING LIGHT INOPERABLE. BUZZER WORKS. DEFERRED CREW ENTRY N DOOR WARNING LIGHT, IAW MEL 52-73-01-1. PLACARD INSTALLED, A/C OK TO CONTINUE.

Part: WARNING MESSAGE — FALSE ACTIVATION (E/E BAY) · airframe 22,483 hrs · 14,067 cycles

INSPECTION TYPE: N/A SMOKE, AVIONICS SMOKE WARNING CAME ON/OFF ABOUT 6 TIMES. THE LAST TIME IT STAYED ON EVEN AFTER SHUTDOWN. CREW C/W SNIFFER TEST, WHICH WAS NEGATIVE. WENT INTO AVIONICS COMPARTMENT, NO SMELL OF SMOKE. BITE SYSTEM TEST ON FIRE MODULE PASSED, PER AMM 26-15-00-0501. ADJ TESTS IN POSITION ELECT BAY, MAIN AND EQUIPMENT BAY PASSED. OK FOR DISPATCH.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 22,254 hrs · 13,932 cycles

FWD CARGO FWD FLOOR PANEL 131MG WAS DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO A300-5320-16407-E.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 22,254 hrs · 13,932 cycles

AFT CARGO FLOOR PANEL 151RF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO A300-5320-16407-E.

Part: FLOOR PANEL — DAMAGED (MAIN DECK CARGO) · airframe 22,254 hrs · 13,932 cycles

FLOOR BOARD 242BJ DAMAGED. REPAIRED IAW SREO A300-5320-42722-F.

Part: BULKHEAD WEB — WORN (NR 1 INLET) · airframe 22,254 hrs · 13,932 cycles

NR 1 ENGINE INLET COWL, OTBD SESE LINE BULKHEAD FITTING HOLE IN WEB WAS WORN, AND ENLARGED. REMOVED & REPLACED THE WEB IAW SRM 54-10-00, FIG 201.

Part: FAIRING — DAMAGED (NR 1 NACELLE) · airframe 22,254 hrs · 13,932 cycles

NR 1 ENGINE AFT LOWER FAIRING 475AL, LT UPPER EDGE HAD FOUR ENLONGATED SCREW HOLES BETWEEN FWD TO AFT EDGES. REMOVED & REPLACED IAW SRM 51-40-21.

Part: ANGLE — DAMAGED (THRUST REVERSER) · airframe 22,254 hrs · 13,932 cycles

NR 1 ENGINE INBD THRUST REVERSER COWL AFT UPPER FWD CUTOUT CORNER METAL SUPPORT DAMAGED. INSTALLED A NEW WEAR ANGLE IAW SRM 51-40-20.

Part: SUPPORT — CORRODED (AFT CARGO CEILIN) · airframe 22,254 hrs · 13,932 cycles

AFT CARGO BAY CEILING PANEL SUPPORT STRUCTURE CORRODED AT 2 LOCATIONS BETWEEN Y750-Y1100. REMOVED & REPLACED IAW SRM 51-40-21.

Part: PLATE — DAMAGED (NR 1 NAC FAIRING) · airframe 22,254 hrs · 13,932 cycles

NR 1 ENGINE AFT LOWER FAIRING 475AL LT UPPER EDGE FOUR ENLONGATED SCREW HOLES BETWEEN FWD TO AFT EDGES.REMOVE & REPLACE IAW SRM 51-40-21.

Part: PLATE — DAMAGED (NR 1 NAC FAIRING) · airframe 22,254 hrs · 13,932 cycles

NR 1 ENGINE AFT LOWER FAIRING 475AL, RT UPPER EDGE HAD 10 ENLONGATED SCREW HOLES BETWEEN FWD TO AFT EDGES. REMOVED & REPLACED IAW SRM 51-40-21.

Part: DOUBLER — GOUGED (THRUST REVERSER) · airframe 22,254 hrs · 13,932 cycles

NR 1 ENGINE INBD THRUST REVERSER COWL AFT UPPER FWD CUTOUT DOUBLER. REPAIRED HAS DEEP GOUGE. INSTALL NEW DOUBLER IAW SRM 51-40-21.

Part: SUPPORT — GOUGED (VERTICAL STAB) · airframe 22,254 hrs · 13,932 cycles

VERTICAL STAB L/E ACCESS PANEL 32213L UPPER RT STRUCTURAL SUPPORT FASTENER HOLE WAS GOUGED. REPAIRED IAW A300-5530-77397, AND EA#300-5532-27-A2787

Part: SUPPORT — DAMAGED (NR 1 NAC FAIRING) · airframe 22,254 hrs · 13,932 cycles

NR 1 ENG AFT LOWER FAIRING 475AL, RT UPPER EDGE HAD 10 ENLONGATED SCREW HOLES BETWEEN FWD TO AFT EDGES. REMOVED & REPLACED IAW SRM 51-40-21.

Part: SEAT TRACK — CORRODED (FRAME 80) · airframe 22,254 hrs · 13,932 cycles

INSPECTION TYPE:SEG, MCD SEAT TRACK HAS CORROSION FRAME 80 TRACK Y794. REPAIRED PER SRM 53-18-16.

Part: CARGO TRACK — CORRODED (FRAME 80) · airframe 22,254 hrs · 13,932 cycles

INSPECTION TYPE:SEGMAIN CARGO SEAT TRACK HAS CORROSION CROSSBEAM 80 TRACK Y1137REPAR IAW A300-600 SRM 53-10-16 FIG 201

Part: ADAPTER — CORRODED (FRAME 62) · airframe 22,254 hrs · 13,932 cycles

INSPECTION TYPE:SEG, MAIN CARGO CORROSION ON CARGO TRACK ADAPTER CROSSBEAM 62. REMOVED & REPLACED THE CLS ADAPTER IAW SRM 51-40-21

Part: CARGO TRACK — CORRODED (FRAME 80) · airframe 22,254 hrs · 13,932 cycles

INSPECTION TYPE:SEG, MAIN CARGO SEAT TRACK HAS CORROSION CROSSBEAM 80 TRACK -Y1137. REPAIRED IAW SRM 53-18-16.

Part: FLOORBOARD — DAMAGED (NOT REPORTED) · airframe 22,254 hrs · 13,932 cycles

FLOORBOARD 231MJ DAMAGED. FABRICATED A NEW FLOORBOARD IAW SREO A300-5320-40552-B.

Part: SEAT TRACK — CORRODED (MAIN CARGO) · airframe 22,254 hrs · 13,932 cycles

MAIN CARGO SEAT TRACK WAS CORRODED. REPAIRED IAW SRM 53-10-16, FIG 201.

Part: SEAT TRACK — CORRODED (FRAME 80) · airframe 22,254 hrs · 13,932 cycles

MAIN CARGO SEAT TRACK WAS CORRODED FRAME 80. REPAIRED THE SEAT TRACK IAW SRM 53-10-16, FIG 201.

Part: SKIN — CRACKED (NR 1 NACELLE) · airframe 22,254 hrs · 13,932 cycles

NR 1 PYLON PANEL 413BL CRACKED. REPAIRED IAW SRM 54-52-51

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 22,254 hrs · 13,932 cycles

AFT CARGO FLOOR PANEL 152MG DAMAGED. REPAIRED IAW SREO A300-53200-42722-F.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 22,254 hrs · 13,932 cycles

AFT CARGO FLOOR PANEL 152TF DAMAGED. REPAIRED IAW SREO A300-5320-42722-F

Part: THRUST REVERSER — GOUGED (NR 2 ENGINE) · airframe 22,254 hrs · 13,932 cycles

NR 2 ENGINE I/B THRUST REVERSER FWD EDGE LOWER SIDE GOUGED. FABRICATED A FILLER IAW SRM 51-4-21.

Part: FLOOR PANEL — DAMAGED (FWD CARGO BAY) · airframe 22,254 hrs · 13,932 cycles

FWD CARGO BAY FLOOR PANEL 132DH WAS DAMAGED. REPAIRED IAW SREO A300-5320-42722-F.

Part: FLOORBOARD — DAMAGED (NOT REPORTED) · airframe 22,254 hrs · 13,932 cycles

FLOORBOARD 232SG DAMAGED. FABRICATED A NEW FLOORBOARD IAW SREO A300-5320-40552-B.

Part: FLOORBOARD — DAMAGED (NOT REPORTED) · airframe 22,254 hrs · 13,932 cycles

FLOORBOARD 261AH DAMAGED. FABRICATED A NEW FLOORBOARD IAW SREO A300-5320-40552-B.

Part: FLOORBOARD — DAMAGED (NOT REPORTED) · airframe 22,254 hrs · 13,932 cycles

FLOORBOARD 221CG DAMAGED. FABRICATED A NEW FLOORBOARD IAW SREO A300-5320-40552-B.

Part: FLOORBOARD — DAMAGED (NOT REPORTED) · airframe 22,254 hrs · 13,932 cycles

FLOORBOARD 242AJ DAMAGED. FABRICATED A NEW FLOORBOARD IAW SREO A300-5320-40552-B.

Part: BUTTON — DAMAGED (EMERGENCY LIGHTS) · airframe 22,254 hrs · 13,932 cycles

OVERHEAD PANEL EMERGENCY EXIT DISARM LIGHT DAMAGED. REMOVED AND REPLACED OVER HEAD PANEL EMERGENCY EXIT DISARM LIGHT PUSH BUTTON HEAD.

Part: FLOORBOARD — DAMAGED (NOT REPORTED) · airframe 22,254 hrs · 13,932 cycles

FLOORBOARD 242ZH DAMAGED. FABRICATED A NEW FLOORBOARD IAW SREO A300-5320-40552-B.

Part: PLATE — WORN (THRUST REVERSER) · airframe 22,254 hrs · 13,932 cycles

INSPECTION TYPE:A300ENG #2 O/B TR INNER BARREL UPPER BIFURCATION UPPER EDGE AFT SIDE METAL PLATE WORN & TORNREMOVED & REPLACED RUB STRIP & WEAR ANGLE IAW SRM 51-70-21, 54-30-00

Part: FITTING — CRACKED (FRAME 40) · airframe 22,254 hrs · 13,932 cycles

RIGHT FRAME 40 FITTING HOLE HAS CRACK INDICATION AT 4 O'CLOCK.COMPLIED WITH EO#A300-5710-64579-D

Part: FITTING — CRACKED (FRAME 40) · airframe 22,254 hrs · 13,932 cycles

LEFT FRAME 40 FWD FITTING HOLE 7 O'CLOCK APPROX .61" FIRST LAYER TO EXTEND ON THE SURFACE APPROX 1.2" CRACKED. COMPLIED WITH EO A300-571-64579-D.

Part: HINGE FITTING — GOUGED (NR 1 NACELLE) · airframe 22,254 hrs · 13,932 cycles

NR 1 O/B FAN COWL AFT HINGE FITTING FAN COWL SIE IS GOUGED. REMOVED & REPLACED FITTING IAW AMMM 71-13-08.

Part: RUB STRIP — WORN (THRUST REVERSER) · airframe 22,254 hrs · 13,932 cycles

NR 2 ENGINE INBD INNER 6011EL UPPER BIFUNCTION UPPER OFF METAL EDGE WORN & TORN. REMOVED & REPLACED THE RUB STRIP & WEAR ANGLE IAW SRM 51-42-21

Part: RIB — CRACKED (LT WING) · airframe 22,254 hrs · 13,932 cycles

LEFT WING T/E UPPER FIXED PANEL SUPPORT BRACKET BELOW THE INBD END OF THE NR 3 SPOILER WAS CRACKED. REMOVED & REPLACED THE RIB.

Part: RIB — CRACKED (LT WING) · airframe 22,254 hrs · 13,932 cycles

LEFT WING T/E UPPER FIXED PANEL SUPPORT BRACKET ABOVE THE NR 4 FLAP TRACK WAS CRACKED. REMOVED & REPLACED THE RIB IAW SRM 51-40-21.

Part: FAIRING — CRACKED (NR 2 PYLON) · airframe 22,254 hrs · 13,932 cycles

NR 2 PYLON O/B SIDE FIXED FAIRING HAS POSSIBLE CRACK ON LOWER AREA AROUND FASTENER. FABRICATED & INSTALLED REPAIR DOUBLER IAW SRM 54-53-10 FIG 201.

Part: STRIP — WORN (THRUST REVERSER) · airframe 22,254 hrs · 13,932 cycles

INSPECTION TYPE:A300 NR 1 ENGINE I/B TR COWL UPPER LANDING AFT METAL STRIP WORN OUT. REMOVED & REPLACED IAW SRM 51-40-21.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,254 hrs · 13,932 cycles

INSPECTION TYPE:A300 COCKPIT FLOOR STRUCTURE CROSSBEAM 10/Y-953 HAS INTERCOSTAL ANGLE CRACKED. REMOVED & REPLACED IAW SRM 51-40-21.

Part: PLATE — CRACKED (RT WING TE FLAP) · airframe 22,254 hrs · 13,932 cycles

RIGHT WING OTBD FLAP R:61 ANGLE PLATE CRACKED, REMOVED & REPLACED

Part: WARNING SYSTEM — MALFUNCTIONED (L1 DOOR) · airframe 22,216 hrs · 13,913 cycles

ON PREFLT TESTED L1 DOOR SLIDE WARNING SYSTEM BUZZER DID NOT WORK LIGHT WAS NORMAL. OPS CHECKED EVACUATION SLIDE WARNING HORN IAW AMM 52-73-12-0401. NO DEFECTS NOTED.

Part: WARNING SYSTEM — MALFUNCTIONED (DOOR) · airframe 21,845 hrs · 13,687 cycles

INSPECTION TYPE:N/A** SUPPLEMENTAL SDR ** EVACUATION SLIDE BUZZER WARNING INOP.TRANSFERED TO M702615 REF MEL 52-73-01-2 PLACARDS INSTALLED.RESET AUTONOMOUS POWER SUPPLY AND BUZZER UNIT IAW AMM 52-73-11-0401, OPS CK OK, DI REMOVED.

Part: TEST BUTTON — DIRTY (COCKPIT) · airframe 20,376 hrs · 12,875 cycles

INSPECTION TYPE:SDR WITH SLIDE IN DISARMED POSITION, BUZZER AND HORN ARE BOTH SOUNDING. CLEANED EMERGENCY ARM AND DISARM TEST BUTTON OPS CK GOOD PER 52-10-00 AQMM OK TO CONTINUE.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 20,091 hrs · 12,713 cycles

INSPECTION TYPE:NAL1 DOOR DAMPER/EMERGENCY CYLINDER PRESS LOWSERVICED L1 DOOR DAMPER/EMERGENCY CYLINDER TO PROPER LEVEL PER MM 52-10-14-301

Part: POWER SUPPLY — INOPERATIVE (SLIDE ARMING LT) · airframe 20,030 hrs · 12,674 cycles

INSPECTION TYPE:SDRL1 DOOR SLIDE ARMING LIGHT WOULD NOT ILLUMINATEREMOVED AN REPLACED INBD POWER SUPPLY UNIT, IAW AMM 52-73-18 PAGE BLOCK 0401, OPS CHECK GOOD AUTONOMOUS STAND POWER UNIT .

Part: BATTERY — INOPERATIVE (DOOR SLIDE LIGHT) · airframe 20,030 hrs · 12,674 cycles

CABIN ENTRY DOOR SLIDE RED LIGHT BAR DOES NOT ILLUMINATE WHEN TEST BUTTON PRESSED. ITEM DEFERRED PER MEL 52-73-01-1. OK FOR SERVICE. INBD BAT R/R'D. OPS CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 19,741 hrs · 12,512 cycles

CREW ENTRANCE DOOR OPENING PRESSURE WAS LOW. SERVICED L1 DOOR BOTTLE IAW AMM 52-10-14. OK FOR SERVICE.

Part: BRACKET — BROKEN (VERTICAL STAB) · airframe 19,676 hrs · 12,472 cycles

FWD VERTICAL STABILIZER SIDE FAIRING PANEL 323AL HAD A BROKEN BRACKET, ATTACHED TO THE FUSELAGE. REMOVED AND REPLACED THE BRACKET IAW SRM 51-40-21.

Part: FLOOR PANEL — DELAMINATED (FWD CARGO) · airframe 19,676 hrs · 12,472 cycles

INSPECTION TYPE: 4C, THE FWD CARGO COMPARTMENT FLOOR PANEL 132MG WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO A300-5320-16407-E.

Part: SEAL DEPRESSOR — CRACKED (AFT CARGO) · airframe 19,676 hrs · 12,472 cycles

INSPECTION TYPE: 1C, AFT CARGO DOOR FRAME AFT UPPER SEAL DEPRESSOR, FR65 WAS CRACKED. REMOVED & REPLACED THE SEAL DEPRESSOR IAW SRM 51-40-21.

Part: SUPPORT BRACKET — CRACKED (FRAME 54) · airframe 19,676 hrs · 12,472 cycles

AFT CARGO COMPARTMENT FWD BULKHEAD UPPER PANEL SUPPORT BRACKET AT FRAME 54, LBL 40 WAS CRACKED. REMOVED AND REPLACED SUPPORT BRACKETIAW SRM 51-40-21.

Part: SUPPORT BRACKET — CRACKED (FRAME 54) · airframe 19,676 hrs · 12,472 cycles

AFT CARGO COMPARTMENT FWD BULKHEAD UPPER SUPPORT BRACKET AT FRAME 54, LBL 77 WAS CRACKED. REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-40-21.

Part: CLOSEOUT PANEL — CRACKED (FWD CARGO DOOR) · airframe 19,676 hrs · 12,472 cycles

INSPECTION TYPE: 1-4C, FWD CARGO DOOR CUTOUT FWD CLOSEOUT PANEL WAS PUNCTURED. REMOVED AND REPLACED THE CLOSEOUT PANEL.

Part: FLOORBEAM — CRACKED (FRAME 10) · airframe 19,675 hrs · 12,471 cycles

INSPECTION TYPE: 1C, AVIONICS COMPARTMENT FLOORBEAM ANGLE, FRAME 10, LBL 37 WAS CRACKED. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-40-21.

Part: SUPPORT ANGLE — CRACKED (FRAME 38.2) · airframe 19,675 hrs · 12,471 cycles

FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT FRM 38.2, LBL 60 ANGLE CRACKED. REMOVED AND REPLACED IAW SRM 51-40-21.

Part: SUPPORT BRACKET — CRACKED (FRAME 54) · airframe 19,675 hrs · 12,471 cycles

AFT CARGO COMPARTMENT FWD BULKHEAD UPPER PANEL SUPPORT BRACKET AT FRAME 54, BL 0. REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-40-21.

Part: SUPPORT ANGLE — CRACKED (FRAME 38.2) · airframe 19,675 hrs · 12,471 cycles

FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT FRAME 38.2, RBL 22 ANGLE WAS CRACKED. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-40-21.

Part: DOOR FRAME — DAMAGED (FRM 20) · airframe 19,675 hrs · 12,471 cycles

FWD CARGO DOOR FRAME UPPER RT CORNER, FRAME 20 DAMAGED. REMOVED AND REPLACED IAW SRM 51-40-21.

Part: SUPPORT ANGLE — CRACKED (FRAME 38.2) · airframe 19,675 hrs · 12,471 cycles

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

Part: SUPPORT FRAME — CRACKED (FRAME 38.2) · airframe 19,675 hrs · 12,471 cycles

FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT AT FRAME 38.2, RBL 41 WAS FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-40-21.

Part: SUPPORT — CRACKED (FRAME 38.2) · airframe 19,675 hrs · 12,471 cycles

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

Part: CYLINDER — LOW PRESSURE (CREW ENTRY) · airframe 19,597 hrs · 12,435 cycles

CREW ENTRY DOOR OPENING MECHANISM PRESSURE WAS LOW. SERVICED THE MAIN ENTRY DOOR OPEN CYLINDER IAW AMM 52-10-14-0301.

Part: ROD — NOT REPORTED (FAN COWL) · airframe 19,521 hrs · 12,386 cycles

NR 2 ENGINE FAN COWL SUPPORT ROD. R & R THE SUPPORT ROD IAW AMM 71-13-04-0401, OPS NORMAL.

Part: CYLINDER — LOW PRESSURE (PAX DOOR) · airframe 18,281 hrs · 11,699 cycles

ENTERY DOOR DAMPER CYLINDER PRESSURE IS LOW. SERVICED THE CYLINDER IAW MM 52-10-14.

Part: LAMP — INOPERATIVE (LAV MIRROR LIGHT) · airframe 17,920 hrs · 11,465 cycles

LAVATORY AVX MIRROR LIGHTS INOPERATIVE. REPLACED THE LAMPS IAWAMM 33-41-21-0402. OPS CHECKED GOOD

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 17,767 hrs · 11,371 cycles

EMERGENCY LIGHT LENS AT COCKPIT ENTRANCE MISSING. REPLACED THE LENS.

Part: SUPPORT RIB — DAMAGED (LT COWLING) · airframe 17,707 hrs · 11,330 cycles

WHILE PERFORMING TC545028-01-1-435 FOUND DAMAGE TO NR 1 ENG RT FAN COWL AFT HINGE CONSISTING OF CHAFING ON FWD SUPPORT RIB MEASURING .750 LONG X .062 DEEP. AFT SUPPORT RIB MEASURING .250 LONG X .0625 DEEP. ACCOMPLISHED INTERIM REPAIR IAW EO -7110-64275-A.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,631 hrs · 11,275 cycles

THREE BULBS NOT ILLUMINATED IN DOOR EXIT SIGN MODULE ABOVE L1 DOOR. REPLACED THE BULBS FOR DOOR EXIT SIGN MODULE 21WL IAW AMM 33-51-13-04. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,631 hrs · 11,275 cycles

THREE BULBS NOT ILLUMINATED IN THE EXIT SIGN MODULE ABOVE L1 DOOR. REPLACED THE BULBS IAW AMM 33-51-13-04. OPS CHECKED GOOD.

Part: PANEL — CRACKED (NR 2 PYLON) · airframe 16,812 hrs · 10,743 cycles

INSPECTION TYPE:1C, NR 2 PYLON PANEL 423BL HAS A CRACK ON INSIDE EDGE. REPAIRED IAW SRM 54-52-51, FIG 204.

Part: ACCESS DOOR — CRACKED (THRUST REVERSER) · airframe 16,812 hrs · 10,743 cycles

INSPECTION TYPE:1C, NR 2 ENGINE OTBD T/R FWD LOWER LATCH ACCESS DOOR CRACKED AT FWD HINGE. R & R ACCESS DOOR IAW SRM 54-04-02.

Part: WEB — CRACKED (NR 2 COWLING) · airframe 16,812 hrs · 10,743 cycles

INSPECTION TYPE:C-1, NR 2 ENGINE INLET COWL, AFT WEB CRACKED ABOVE ACCESS PLATE AT TUBING CONNECTION. REPAIRED IAW PW SRM 54-10-00.

Part: TRANSMITTER — LEAKING (HYD PRESSURE) · airframe 16,676 hrs · 10,665 cycles

EMERGENCY DECLARED, DESENDING THROUGH 18000' THE GREEN HYDRAULIC QTY INDICATED AT THE RED DOT LEVEL AND THE GREEN HYDRAULIC PRESSURE INDICATED ZERO. ACCOMPLISHED HYDRAULIC SYS LO PR CHECKLIST. R & R GREEN RESERVOIR HYD QTY TRANSMITTER IAW 29-31-11-0401. R & R PRESSURE SWITCH FOR GREEN SYSTEM IAW AMM 29-11-62-0401. ALL OPS CHECKED GOOD. REF LOG PAGE 251899, ITEM 3, REPLACED NON RETURN VALVE; GREEN HYDRAULIC SYS IAW AMM 29-11-65-0401. REPLACED GREEN HYD MANIFOLD. NO LEAKS NOTED.

Part: FLOORBOARD — DAMAGED (FWD CARGO BAY) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE: 5YR, FWD CARGO FLOORBOARD 132MG DAMAGE ON BOTTOM SIDE. REPAIRED FWD CARGO FLOORBOARD IAW SRM 51-77-10, SRM 51-77-11.

Part: PANEL — DENTED (CARGO BAY) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE:5YR, BULK CARGO PANEL 161GW DENTED. REPAIRED BULK CARGO PANEL IAW SRM 51-77-10, & SRM 51-77-11.

Part: WEB — DENTED (FRAME 69) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE:5YR, BULK CARGO BAY LT SIDE FRAME 69 VERTICAL WEB HAS MULTIPLE DENTS. REMOVED DAMAGED WEB AND REPLACED WITH NEW WEB.

Part: PANEL — DELAMINATED (MAIN WHEEL WELL) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE:5YR, MAIN WHEEL WELL CAT WALK PANEL 147EF LOWER SURFACE DELAMINATED. REPAIRED PANEL 147EF IAW SRM 51-77-10, SRM 51-77-11.

Part: FLOORBOARD — DAMAGED (AFT CARGO BAY) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE:5YR, AFT PIT FLOORBOARD 161KF DAMAGED ON BACK SIDE. REPAIRED THE FLOORBOARD IAW SRM 51-57-10, SRM 51-77-11.

Part: FLOORBOARD — DAMAGED (AFT CARGO BAY) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE:5YR, AFT CARGO FLOORBOARD 162MF DAMAGED CORNER. REPAIRED FLOORBOARD IAW SRM 51-77-10, SRM 51-77-11.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE: 5YR, AFT CARGO BALL MATERIAL PANEL 151GG CORRODED LOWER CORNER BOTTOM PANEL. REPLACED CORRODED BALL MATERIAL WITH NEW BALL MATERIAL.

Part: BRACKET — CRACKED (FWD BULKHEAD) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE:5YR, AFT CARGO FWD BULKHEAD 5 EA ANGLES CRACKED. R & R 5 EA ANGLES IAW SRM 51-40-22, NOTE: ADDITIONAL PN'S A5341076521800, A5341076522300, A5341076522100, A5341076521900.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE:5YR, MAIN CABIN FLOORBOARD 231LB HAS EDGE DAMAGE. REPAIRED IAW EO A300-5320-42741-F.

Part: MOUNT — CORRODED · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE:5YR, AFT LOWER EXTERNAL FUSELAGE, AFT RADIO ALTIMETER CAN CORRODED ON MOUNTING FLANGE INNER MATTING SURFACE. R & R CAN IAW SRM 51-40-21.

Part: SEAT TRACK — CORRODED (FRAMES 61-62) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE: 5YR, MAIN CABIN SEAT TRACK CORRODED BL 0, FRAMES 61 - 62. REMOVED CORROSION AND FOUND WITHIN LIMITS. TREATED AREA IAW SRM 53-10-16.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE: 5YR, FLOOR SUPPORT UNDER LAV HAS ELONGATED HOLES. REPAIRED AREA IAW EO A300-5310-58897-A.

Part: ANGLE — CRACKED (FRAME 80) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE:5YR, MAIN CABIN ANGLE AT FR 80 RT -Y1137.1 IS CRACKED. R & R ANGLE IAW SRM 51-40-21.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE: 5YR, RT ELEVATOR SKIN DELAMINATED. REPAIRED UPPER SURFACE OF RT ELEVATOR SKIN IAW SRM 55-21-12, PARA 5A, FIG 201, CATEGORY "B" REPAIR.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE: 5YR, RT ELEVATOR SKIN DELAMINATED. REPAIRED UPPER SURFACE OF RT ELEVATOR SKIN IAW SRM 55-21-12, PARA 5A, FIG 201, CATEGORY "B" REPAIR.

Part: SKIN — DELAMINATED (ELEVATOR) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE:5YR, SURFACE OF ELEVATOR SKIN DELAMINATED. REPAIRED UPPER SURFACE OF ELEVATOR SKIN IAW SRM 55-21-12, PAR 5A, FIG 201, CATEGORY "B" REPAIR.

Part: ANGLE — CRACKED (FRAMES 80-82) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE: 5YR, MAIN CABIN ANGLE AT FR 80-82, LT Y1137.1 IS CRACKED. FABRICATED NEW ANGLE IAW DWG A53981401 AND INSTALLED IAW SRM 51-40-21.

Part: SEAT TRACK — CORRODED (FRAME 80) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE: 5YR, MAIN DECK SEAT TRACK AT FRAME 80, Y450 HAS CORROSION. REMOVED CORROSION FOUND TO BE WITHIN LIMITS AND TREATED IAW SRM 53-10-16.

Part: WEB — DENTED (CARGO BULKHEAD) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE:5YR, BULK CARGO PIT RT SIDE FRAME-69 VERTICAL WEB, SHEET NR A53974225240 HAS MULTIPLE DENTS. REMOVED THE DENTED SHEET AND REPLACED WITH A NEW SHEET.

Part: SEAT TRACK — CORRODED (FRAME 80) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE: 5YR, MAIN CABIN SEAT TRACK AT FRAME 80, Y 0 HAS CORROSION. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS AND TREATED IAW SRM 53-10-16.

Part: SEAT TRACK — CORRODED (FRAME 80) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE: 5YR, MAIN DECK SEAT TRACK AT FRAME 80 -Y1137.1 HAS CORROSION. REMOVED CORROSION, FOUND WITHIN LIMITS AND PRIMED IAW SRM 53-10-16.

Part: SEAT TRACK — CORRODED (FRAME 80) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE: 5YR, MAIN DECK SEAT TRACK AT FRAME 80, -Y794.3 HAS CORROSION. REMOVED CORROSION FOUND TO BE WITHIN LIMITS AND TREATED IAW SRM 53-10-16.

Part: SEAT TRACK — CORRODED (FRAME 80) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE: 5YR, MAIN DECK SEAT TRACK AT FRAME 80, Y794.3 HAS CORROSION. REMOVED CORROSION FOUND TO BE WITHIN LIMITS AND TREATED IAW SRM 53-10-16.

Part: SEAT TRACK — CORRODED (FRAME 80) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE: 5YR, MAIN DECK SEAT TRACK AT FRAME 80, Y1137.1 HAS CORROSION. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS AND TREATED IAW SRM 53-10-16.

Part: CROSSBEAM — CRACKED (FRAME 79) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE:5YR, MAIN CABIN CROSSBEAM RT FR 79 -Y1580 CRACKED. REPAIRED CROSSBEAM IAW EO A300-5310-58800-A.

Part: CROSSBEAM — CRACKED (FRAME 79) · airframe 15,965 hrs · 10,222 cycles

INSPECTION TYPE: 5YR, MAIN CABIN FRAME 79 CROSSBEAM LT Y1580 CRACKED. REPAIRED IAW EO A300-5310-58800-A.

Part: FRAME — CRACKED (CARGO DOOR) · airframe 15,962 hrs · 10,219 cycles

INSPECTION TYPE:5YR, AFT CARGO DOOR FORK FRAME 61 CRACKED. REPLACED FRAME IAW EO A300-5230-57988-C.

Part: FLOORBOARD — DENTED (AFT CARGO BAY) · airframe 15,962 hrs · 10,219 cycles

INSPECTION TYPE: 5YR, AFT CARGO BAY FLOORBOARD 161MF DENTED. REPAIRED THE FLOORBOARD IAW SRM 51-77-11.

Part: FLOORBOARD — DENTED (AFT CARGO) · airframe 15,962 hrs · 10,219 cycles

INSPECTION TYPE: 5YR, AFT CARGO BAY FLOORBOARD 161LF HAS DENTS ON TOP SIDE. REPLACED THE FLOORBOARD IAW SRM 51-77-11.

Part: FORK — CRACKED (AFT CARGO DOOR) · airframe 15,962 hrs · 10,219 cycles

INSPECTION TYPE: 5YR, AFT CARGO DOOR FORK FRAME 61A CRACKED. REPLACED FRAME IAW EO A300-5230-57988-C.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 15,889 hrs · 10,164 cycles

EMERGENCY EXIT LIGHTS FAILED ON PASSING FL240. R & R EPSU. OPS CHECKED GOOD IAW AMM 33-51-14-0401.

Part: CONNECTOR — UNKNOWN (EMERGENCY LIGHTS) · airframe 15,885 hrs · 10,161 cycles

INSPECTION TYPE: IN, EMERGENCY EXIT LIGHTS REMAIN ON CONTINUALLY. SWITCH HAS NO EFFECT. REMOVED & RECONNECTED CONNECTOR FROM 436 VU IAW WDM 33-51-03. OPS CHECK GOOD.

Part: SWITCH — FAULTY (PITCH TRIM) · airframe 15,732 hrs · 10,054 cycles

ATB - NR 1 PITCH TRIM DISCONNECTED, WOULD NOT RESET. R & R F/O'S PITCH TRIM SWITCH IAW MM 22-27-12-0401.

Part: SKIN — CRACKED (LT WING TE FLAP)

75" CRACK LT WING INBD FLAP LOWER SKIN 60" FROM INBD END AND 12.5" FROM T/E REPAIRED IAW EO A300-5750-55531-A.

Part: WARNING LIGHT — INOPERATIVE (EMERGENCY LIGHTS)

DURING EMERGENCY LIGHT TEST, WARNING LIGHT FAILED TO ILLUMINATED AND DOOR EXIT LIGHTS REMAINED ON. ACCOMPLISHED ADJUSTMENT TEST OF EMERGENCY LIGHTS, NO FAULTS NOTED IAW AMM 33-55-00.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 14,429 hrs · 9,170 cycles

INSPECTION TYPE:1C, RT CENTER FLAP UPPER SURFACE REPAIR DOUBLER CHAFED BETWEEN RIB 13-15 AND STGR 2.6-2.8. REPAIRED RT CENTER FLAP UPPER SURFACE BETWEEN RIB 13-15 AND STGR 2.6-2.8 IAW STASA EA300-5750-01-A5057-IR AND A300-5750-53353-A.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 14,429 hrs · 9,170 cycles

INSPECTION TYPE:1C, RT WING INNER FLAP UPPER SKIN REPAIR DOUBLER BETWEEN RIBS 11-14 AND STGR 2.1-2.2 CHAFED. REPAIRED RT WING INNER FLAP UPPER SKIN BETWEEN RIBS 11-14 AND STGR 2.1-2.2 IAW STASA EA 300-5750-01-A5059-IR AND EO A300-5750-533352-A.

Part: RIB — CHAFED (RT WING) · airframe 14,429 hrs · 9,170 cycles

INSPECTION TYPE:3C, RT WING FIXED L/E JACK NR 1 INNER RIB AT STA-239.6 IS CHAFED. ACCOMPLISHED REPAIR ON RT WING FIXED L/E, JACK NR 1 INNER RIB AT STA -239.6 IAW EO A300-5720-53354-A, PARA 6A.

Part: SKIN — DAMAGED (FUSELAGE)

DAMAGE FOUND SKIN FRAME 58 STRINGER 25L REF D502476, REPAIRED IAW EO A300-5330-52462-A.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

DURING MX INSPECTION; LAVATORY EMERGENCY LIGHT HAD ONE BULB INOPERATIVE. REPLACED BULB IAW MM33-51-21-04; OPS CHECKED NORMAL.

Part: FLOOR PANEL — PUNCTURED · airframe 12,941 hrs · 8,183 cycles

INSPECTION TYPE: SV, FLOOR PANEL 232WG PUNCTURED/DELAMINATED. FABRICATED NEW FLOOR PANEL IAW EO A300-5320-40552-B.

Part: FLOOR PANEL — DELAMINATED · airframe 12,941 hrs · 8,183 cycles

INSPECTION TYPE: SV, FLOOR PANEL 231LH DELAMINATED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 12,941 hrs · 8,183 cycles

INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 222DG HAS LWR SKIN CRACKED AND HAS CORRODED INSERTS. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOOR PANEL — DAMAGED · airframe 12,941 hrs · 8,183 cycles

INSPECTION TYPE: SV, FLOOR PANEL 222AG HAS DRILLED OFF SCREWS IN INSERTS AND LOWER SKIN HAS NUT JAMMED INTO HONEYCOMB. FABRICATED NEW FLOOR PANEL IAW EO A300-5320-40552-B.

Part: FLOOR PANEL — CRACKED · airframe 12,941 hrs · 8,183 cycles

INSPECTION TYPE: SV FLOOR PANEL 221EG CRACKED. FABRICATED NEW FLOOR PANEL IAW EO A300-5320-40552-B.

Part: FLOOR PANEL — DELAMINATED · airframe 12,941 hrs · 8,183 cycles

INSPECTION TYPE :SV, FLOOR PANEL 222NG DELAMINATED. FABRICATED NEW FLOOR PANEL IAW EO A300-5320-40552-B.

Part: FLOOR PANEL — CRACKED · airframe 12,941 hrs · 8,183 cycles

INSPECTION TYPE: SV, FLOOR PANEL 232RH UPPER SKIN CRACKED. FABRICATED NEW FLOOR PANEL IAW EO NR A300-5320-40552-B.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 12,941 hrs · 8,183 cycles

INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 231LG LOWER SKIN IS TORN DELAMINATED AND PUNCTURED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOOR PANEL — PUNCTURED · airframe 12,941 hrs · 8,183 cycles

INSPECTION TYPE: SV, FLOOR PANEL 221BG PUNCTURED. REPAIRED MDCC FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOOR PANEL — PUNCTURED · airframe 12,941 hrs · 8,183 cycles

INSPECTION TYPE: SV, FLOOR PANEL 232NJ PUNCTURED. FABRICATED NEW FLOOR PANEL 232NJ EO A300-5320-40552-B.

Part: DOOR — FAILED (RT MLG)

RT GEAR DOOR WOULD NOT CLOSE AFTER TAKEOFF. FOLLOWED ECAM PROCEDURE A AND QRH PROCEDURE. RETURNED TO DEPARTURE, GEAR EXTENDED NORMAL UPON THEIR RETURN. DEFERRED IAW 32-30-01. (SDR OPEN)

Part: UPLOCK — INOPERATIVE (RT MLG DOOR)

RIGHT GEAR DOOR WOULD NOT CLOSE AFTER TAKEOFF. FOLLOWED ECAM PROCEDURE A AND QRH PROCEDURE. RETURNED TO DEPARTURE, GEAR EXTENDED NORMAL UPON THE RETURN. DEFERRED IAW 32-30-01. R & R RT MLG DOOR UPLOCK ASSY IAW MM 32-31-33-04. PERFORMED A GEAR SWING TO VERIFY NORMAL GEAR INDICATION. NO DEFECTS NOTED IAW MM 07-11-00-00. THIS CLEARS M462809. PLACARD REMOVED, DMP REVERSED.

Part: SIGN — INOPERATIVE (COCKPIT)

DOOR EXIT SIGN AUTO FEATURE INOPERATIVE. PERFORMED OPS TEST OF SUPER NUMERARY LIGHTS/SIGNS IAW AMM 33-26-00. OPS CHECKED GOOD. PLACARD REMOVED.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 11,990 hrs · 7,588 cycles

INSPECTION TYPE:1C RT INBD FLAP T/E UPPER SURFACE BETWEEN RIBS 9A AND 9 IS DENTED. REPAIRED RT INBD FLAP T/E UPPER SURFACE BETWEEN RIBS 9A AND 9 IAW STA-SA EA 300-5753-01-A3440, REV I/R AND EO A300-5750-44256-A REF: CONTROL NR 486137.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, MAIN DECK FLOOR PANEL 231NJ HAS MATERIAL MISSING AT BOTTOM EDGE. REPAIRED MAIN DECK FLOOR PANEL 231NJ IAW EO A300-5320-38221-B.

Part: FLOORBOARD — BROKEN (MAIN CABIN) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, MAIN CABIN COMPARTMENT FLOORBOARD NR241MN HAS A BROKEN CORNER AT FWD INBD SIDE AND ONE DENT ON UPPER SKIN. FABRICATED MAIN CABIN FLOORBOARD NR241MN IAW EO A300-5320-16407-E, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 241HN HAS A CRACK AT CORNER. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 241HN IAW EO A300-5320-38221-B PARA 6A.

Part: FLOOR PANEL — PUNCTURED (MAIN CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, MAIN CARGO COMPT FLOOR PANEL 252VF IS PUNCTURED. REPAIRED MAIN CARGO COMPT FLOOR PANEL 252VF IAW EO A300-5320-38221-B.

Part: FLOORBOARD — CRACKED (MAIN CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, MAIN CARGO FLOORBOARD NR 242ZF HAS A CRACK ACCOMPLISHED REPAIR ON MAIN CARGO FLOORBOARD NR 242ZF IAW EO A300-5320-38221-B PARA 6A.

Part: FLOORBOARD — PUNCTURED (MAIN CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 252BN HAS 2 EA PUNCTURED ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 252BN IAW EO A300-5320-38221-B PARA 6A.

Part: FLOORBOARD — DELAMINATED (MAIN CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT ZONE 231, NR 231PJ. FLOORBOARD HAS DELAMINATED AREA AT UPPER SKIN. FABRICATED MAIN CABIN FLOORBOARD NR 231PJ IAW EO A300-5320-16407-E, APPENDIX B.

Part: FLOORBOARD — PUNCTURED (MAIN CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR252XG HAS A PUNCTURE ACOMPLISHED REPAIR ON MAIN CARGO FLOORBOARD NR252XG IAW EO A300-5320-38221-B PARA 6A.

Part: FLOORBOARD — DELAMINATED (MAIN CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT FLOORBOARD NR 241TK IS DELAMINATED AT FWD LOWER AREA. ACCOMPLISHED REPAIR IAW EO A300-5320-38221-B, PARA 6A.

Part: FLOOR PANEL — CRACKED (MAIN CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, MAIN CARGO COMPT FLOOR PANEL 241LJ CORNER IS BROKEN OFF. FABRICATED NEW MAIN CARGO FLOOR PANEL 241LJ IAW EO A300-5320-16407-E APPENDIX A/B.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 11,099 hrs · 6,409 cycles

INSPECTION TYPE:10YR, RT CTR FLAP UPPER SKIN REPAIR DOUBLER IS GOUGED IN 5 PLACES. ACCOMPLISHED REPAIR IAW EO A300-5750-39854-A PARA. 6A.

Part: FLOORBOARD — BROKEN (MAIN CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT FLOORBOARD NR231SG IS BROKEN OFF AT FWD INBD CORNER. FABRICATED MAIN CARGO FLOORBOARD NR231SG IAW EO A300-5320-16407-E, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR231NJ IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR231NJ IAW EO A300-5320-38221-B PARA A.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, RT INBD FLAP UPPER SKIN REPAIR DOUBLER HAS 4 SMALL GOUGES AND LOOSE RIVET AT FWD UPPER CORNER. REPAIRED RT INBD FLAP UPPER SKIN BETWEEN RIBS 11-14, STGR 2.1-2.2 IAW EO A300-5750-39726-A AND STA-SA EA 300-5750-01-A2670 I/R.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR MAIN CARGO COMPT FLOOR PANEL 251WG IS DELAMINATED. FABRICATED NEW MAIN CARGO COMPT FLOOR PANEL 251WG PER IPXA EO A300-5320-16407-E APPENDIX A/B.

Part: FLOORBOARD — CRACKED (MAIN CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT FLOORBOARD NR252UJ IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CARGO FLOORBOARD NR252UJ IAW EO A300-5320-38221-B PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT FLOORBOARD NR 252NG IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CARGO FLOORBOARD NR 252NG IAW EO A300-5320-38221-B PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD NR261RF IS CRACKED. ACCOMPLISHED REPAIR ON MAIN DECK CARGO FLOORBOARD NR261RF IAW EO A300-5320-38221-B PARA 6A.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR LEFT WING CENTER FLAP UPPER SURFACE PREVIOUS REPAIR IS GOUGED. ACCOMPLISHED REPAIR IAW EO A300-5750-39715-A, PARA 6A.

Part: FLOORBOARD — BROKEN (MAIN CABIN) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, MDC FLOORBOARD NR 251VF CORNER IS BROKEN OFF FABRICATED MAIN CABIN FLOORBOARD NR 251VF IAW EO A300-5320-16407-E, APPX B.

Part: FLOORBOARD — BROKEN (MAIN CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR MAIN DECK FLOORBOARD NR252TJ IS BROKEN AT MOUNTING SCREW HOLE. ACCOMPLISHED REPAIR ON MAIN CARGO FLOORBOARD NR252TJ IAW UPS EO A300-5320-38221-B PARA 6A.

Part: FLOOR PANEL — CRACKED (MAIN CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, MAIN CARGO COMPT FLOOR PANEL 251EN IS CRACKED. REPAIRED MAIN CARGO FLOOR PANEL 251EN IAW EO A300-5320-38221-B.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR MAIN CARGO FLOOR PANEL NR252GF IS DELAMINATED. ACCOMPLISHED REPAIR ON MAIN CARGO FLOOR PANEL NR252GF IAW EO A300-5320-38221-B, PARA A.

Part: FLOORBOARD — CRACKED (MAIN CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, MAIN DECK CARGO COMPARTMENT FLOOR PANEL NR262GH IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CARGO FLOORBOARD NR 262GH IAW UPS EO A300-5320-38221-B PARA 6A.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK CORRODED AT FR 80, Y450. REPAIRED MAIN CABIN SEAT TRACK IAW SRM 53-10-16, PB 201, PARA 4, FIG 201.

Part: FLOORBOARD — CRACKED (FWD CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, FWD CARGO FLOORBOARD NR 132QG HAS SEVERAL PRY BAR MARKS. FABRICATED FWD CARGO FLOORBOARD NR 132QG IAW EO A300-5320-16407-E APPENDIX C.

Part: FLOORBOARD — PUNCTURED (FWD CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, FWD CARGO FLOORBOARD NR 131BH HAS NUMEROUS PRY BAR MARKS. ACOMPLISHED REPAIR ON FLOORBOARD 131BH IAW EO A300-5320-38221-B PARA 6A.

Part: FLOORBOARD — CRUSHED (FWD CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, FWD CARGO FLOORBOARD NR 132FE THE HONEYCOMB SIDE IS CRUSHED AND BROKEN. FABRICATED FWD CARGO FLOORBOARD NR 132FE IAW EO A300-5320-16407-E, APPENDIX C.

Part: FLOORBOARD — CRACKED (FWD CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, FWD CARGO FLOORBOARD NR 132AH HAS A 3 IN. CRACK ACCOMPLISHED REPAIR ON FWD CARGO FLOORBOARD NR 132AH IAW EO A300-5320-38221-B PARA 6A.

Part: FLOORBOARD — PUNCTURED (FWD CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR FWD CARGO FLOORBOARD NR 131DE IS PUNCTURED ACCOMPLISHED REPAIR ON FWD CARGO FLOORBOARD NR 131DE IAW EO A300-5320-38221-B PARA.6A.

Part: FLOORBOARD — CRACKED (AFT CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, AFT CARGO COMPARTMENT FLOORBOARD NR 152LG IS CRACKED AT LOWER SURFACE. ACCOMPLISHED REPAIR ON AFT CARGO FLOORBOARD NR 152LG IAW EO A300-5320-38221-B PARA 6A.

Part: FLOORBOARD — CRACKED (AFT CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, AFT CARGO COMPARTMENT FLOORBOARD NR 151TF HAS SEVERAL CRACKS AT LOWER SURFACE AND EDGE ACCOMPLISHED REPAIR ON AFT CARGO FLOORBOARD NR 151TF IAW EO A300-5320-38221-B PARA 6A0.

Part: FLOORBOARD — CRACKED (AFT CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, AFT CARGO COMPARTMENT FLOORBOARD NR151QF IS CRACKED AT LOWER SURFACE. ACCOMPLISHED REPAIR ON AFT CARGO FLOORBOARD NR 151QF EO A300-5320-38221-B PARA 6A.

Part: FLOORBOARD — CRACKED (AFT CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, AFT CARGO COMPARTMENT FLOORBOARD NR 152RF HAS SEVERAL CRACKS AND PUNCTURES ON LOWER SURFACE. FABRICATED AFT CARGO FLOORBOARD NR 152RF IAW EO A300-5320-16407-E APPENDIX C.

Part: FLOORBOARD — CRACKED (AFT CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, AFT CARGO COMPARTMENT FLOORBOARD NR 151KG HAS SEVERAL CRACKS ON LOWER SURFACE. ACCOMPLISHED REPAIR ON FLOOBOARD NR 151KG IAW EO A300-5320-38221-B PARA 6A.

Part: FLOORBOARD — CRACKED (AFT CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, AFT CARGO COMPARTMENT FLOORBOARD NR 151RF HAS SEVERAL CRACKS ON LOWER SURFACE. ACCOMPLISHED REPAIR ON AFT CARGO FLOORBOARD NR 151RF IAW EO A300-5320-38221-B PARA 6A.

Part: FLOOR PANEL — CRACKED (AFT CARGO BAY) · airframe 11,099 hrs · 6,994 cycles

INSPECTION TYPE:10YR, AFT CARGO COMPT FLOOR PANEL 151VF IS CRACKED. FABRICATED NEW AFT CARGO COMPT FLOOR PANEL 151VF IAW EO A300-5320-16407-E APPENDIX C.

Part: BATTERY PACK — DISCHARGED (ESCAPE SLIDE)

MAIN DOOR SLIDE VOLTAGE INOP, DEFERRED M432151. TESTED BATTERY VOLTAGE IAW MC256120-02-1-L. MINIMUM VOLTAGE REQUIRED IS 8.7 VDC, WITHIN LIMITS. THIS CLEARS M432151.

Part: SMOKE DETECTOR — INOPERATIVE (MID 1 CARGO BAY)

ATB - PASSING THROUGH 15000 RECEIVED NUMEROUS MOMENTARY ECAM FAULTS FOLLOWED BY A CONSTANT MAIN DECK CARGO LOOP FAULT MID 1 MAIN DECK LOOP FAULT AFTER IT REMAINED STEADY. PERFORMED QRH PROCEDURE FOR MAIN DECK CARGO LOOP FAULT. R & R ALL MID 1 CARGO COMPARTMENT SMOKE DETECTORS FOR LOOPS A&B IAW 26-19-12-04. PERFORMED OPS CHECK OF MAIN COMPARTMENT DETECTION SYS IAW 26-19-00-05. R & R MAIN CARGO SMOKE DETECTION CONTROL UNIT 50WU1 IAW 26-19-34-04. ALL SMOKE DETECTOR ON/OFF CGDU2000-00. S/NS ON/OFF 21WU 3811/2729, 22WU 3677/11.

Part: CONTROL UNIT — FALSE INDICATION (SMOKE DETECTION)

RECEIVED CARGO SMOKE ALERT MSG. "AFTER ECAM ITEMS" STATUS BECAME LAND ASAP. MEM WAS CLOSE. LANDED MEM. DEFERRED MAIN DECK SMOKE DETECTOR SYSTEM MID1/ LOOP B IAW MEL 26-17-01 01-1, CONTROL NR M421063 ASSIGNED, PLACARD INSTALLED. T/S WITH REFERENCE TO TSM 26-14-00 PG 103. REPLACED MAIN DECK DETECTION CONTROL UNIT (50WU1) PRECAUTIONARY WITH REFERNCE TO MM 26-19-34-04. OPS CHECK OK. CLEARED M421063 AND REMOVED PLACARD.

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A FLOOR PANEL 132PG DAMAGED. REPAIRED PER EO A300-5320-16407-C.

Part: FLOORBOARD — MISREPAIRED (CARGO BAY) · airframe 9,637 hrs · 6,105 cycles

INSPECTION TYPE:4C REPAIR TO FLOORBOARD EFN 12520051005 CANNOT BE CORRELATED TO THE SRM. FLOORBOARD 161JF MUST BE REPLACED PER EO A300-5320-16407. REMOVED, FABRICATED, AND INSTALLED FLOORBOARD 161JF PER EO A300-5320-16 407C APP D.

Part: SKIN — GOUGED (TE FLAP) · airframe 9,637 hrs · 6,105 cycles

INSPECTION TYPE-4/C REPAIR SURVEY SEQUENCE NR 125-W3-02 ON MIDDLE FLAP UPPER SURFACE IS GOUGED. REPLACED DOUBLER IAW SRM 57-50-00 PARG. 4E, AND FIG. 205 REF UPS RCD NR 358682.

Part: SKIN — GOUGED (TE FLAP) · airframe 9,637 hrs · 6,105 cycles

INSPECTION TYPE-4/C REPAIR SURVEY SEQ. NR 125-W4-01 ON RT INBD FLAP UPPER SURFACE IS GOUGED. REPLACE DOUBLER IAW SRM 57-50-00, PARA. 4E, FIG 205 REF. RCD NR 358679.

Part: STRUCTURE — MISREPAIRED (RUDDER) · airframe 9,637 hrs · 6,105 cycles

INSPECTION TYPE:4C REPAIJR SURVEY SEQ NR 125-S4-01 ON UPPER RT SIDE OF THE RUDDER DOES NOT CORRELATE TO SRM. FAB AND INSTALL REPAIR DOUBLER IAW SRM 55-41-12, PARA. 13, FIG. 209 REF. RCD NR 358680.

Part: SKIN — MISREPAIRED (TE FLAP) · airframe 9,637 hrs · 6,105 cycles

INSPECTION TYPE-4/C REPAIR SURVEY SEQ NR 125-W4-03 ON RT MIDDLE FLAP LEADING EDGE DOES NOT CORRELATE WITH SRM. REMOVED AND REPLACED REPAIR DOUBLER IAW EO A300-5750-33755-A AND EA NR 300-5753-01-A1801, REF RCD NR 358681.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 9,637 hrs · 6,105 cycles

INSPECTION TYPE:4C BULK CARGO FLOOR PANEL 162HF IS DENTED AND PUNCTURED. REMOVED, FABRICATED AND INSTALLED FLOOR PANEL 162HF PER EO A300-5320 -16407C APP D.

Part: FLOORBOARD — DENTED (CARGO BAY) · airframe 9,637 hrs · 6,105 cycles

INSPECTION TYPE:4C BULK CARGO FLOOR PANEL 161GF IS HEAVILY DENTED. REMOVED, FABRICATED AND INSTALLED FLOOR PANEL 161GF PER EO A300-5320-16407-C, APPX D.

Part: ADAPTER — DAMAGED (CABIN) · airframe 9,637 hrs · 6,105 cycles

INSPECTION TYPE-4/C ROB SEAT TRACK ADAPTER AT LT FR 36 MAIN CABIN FOR ACFT. ACCOMPLISHED REPAIR OF SEAT TRACK ADAPTER IAW EO NR A300-5310-33718- A AND RCD NR 358564.

Part: DOUBLER — GOUGED (RT FLAP) · airframe 9,637 hrs · 6,105 cycles

INSPECTION TYPE-4/C 4 GOUGED AREAS CENTER OF BACKSIDE OF RT MID FLAP APPX. 7 INCHES FROM INBD END. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-50-00, PAGE 220, FIG. 205, AND SRM 57-50-00, PARA. 4 E.,FIG 205 REF SAA EA 300-7530-01-A1817 AND UPS EO NR A300-5750-33760-A.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 9,637 hrs · 6,105 cycles

INSPECTION TYPE:4C BULK CARGO FLOOR PANEL 161HF HAS SEVERAL FIELD REPAIRS, DENTS AND PUNCTURES. REMOVED, FABRICATED & INSTALLED FLOOR PANEL 161HF PER PER A300-5320-16407 APPX D.

Part: PITOT SYSTEM — CONTAMINATED (CAPTAINS)

INSPECTION TYPE:N/A RTO (X2) SPLIT BETWEEN CAPTAIN AND STANDBY AIRSPEED AFTER 1ST RTO. MX ACCOMPLISHED ADC TEST ON BOTH ADC'S & PITOT CK ON BOTH PITOT SYS PER AMM. DRIED WATER FOUND IN CAPT'S PITOT DRAIN. BOTH SYS CHECK NORMAL SPLIT WAS AT 100 & 80 KTS, A/C OOS FOR T/S AFTER 2ND RTO. ACCOMPLISHED ADC TEST ON NR 1 & 2 ADC'S PER M/M 34 18 00 00 BOTH CKS NORMAL. T/S TO WATER & CAPT PITOT DRAIN. DRIED WATER, ACCOMPLISHED PITOT CHECK ON BOTH NR 1 & 2 PITOT SYSTEMS PER M/M 34-10-00-05. BOTH WENT UP AND DOWN TOGETHER IN AIRSPEED. ACCOMP PITOT LEAK TEST AT 310 KTS PER M/M 34 10 00 05. NO LEAKS NOTED. ACCOMP AFS LAND TEST NO FAULT.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A GLARESHIELD EMERGENCY LIGHT CAPTAIN'S PANEL INOP. RELAMPED EMERGENCY LIGHT, CHECKS OK IAW TC 050000-01-1.

Part: MECHANISM — OBSTRUCTED (COCKPIT)

DURING FINAL APPROACH, CREW DECLARED AND EMERGENCY DUE TO THE SLATS/FLAPS WERE STUCK IN THE 15/0 POSITION. CREW EXECUTED A NO FLAP LANDING AND WAS ABLE TO LAND WITHOUT FURTHER INCIDENT. REMOVED DEBRIS FROM SLAT/FLAP CONTROL HANDLE LEVER MECHANISM. ACCOMPLISHED SLAT/FLAP BITE TEST PER AMM 27-51-00-05. OPERATIONAL TEST NORMAL.

Part: GAUGE — NOT SEATED (EVAC SLIDE)

INSPECTION TYPE:N/A PRESSURE GAUGE IN SLIDE HARD TO READ. RESEATED THE GAUGE IAW 25-60-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

FWD ENTRY DOOR EXIT SIGN MODULE LOWER 2 BULBS ARE INOP. BULBS REPLACED. OP TEST PERFORMED IAW 33-51-13-04. TEST OK.

Part: SWITCH — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LTS WILL NOT DISARM USING SWITCH. INSTALLED NEW 22WL TOGGLE SWITCH IAW A300 ESPM 20-45-21. TESTS GOOD IAW A300 AMM 33-51-00-05.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHT SWITCH INTERMITTENT IN DISARM POSITION, DISARM ANNUNCIATOR DID NOT ILLUMINATE, BUT EMERGENCY LIGHT DID ILLUMINATE IN BOTH "DISARM" AND "ARM" POSITIONS OF SWITCH . REMOVED AND REPLACED POWER SUPPLY EPSU UNIT PER MM 33-51-14-4. ALSO REFER TO LOG PAGE 315311.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE)

FOUND ESCAPE SLIDE PRESSURE GAUGE NOT VISIBLE FOR PREFLIGHT. REPOSITIONED GAUGE AS NEEDED.

Part: LIGHT — INOPERATIVE (LAVATORY)

LAV EMERG LIGHT INOP. RELAMPED WORKED OK.

Part: PIN — DEACTIVATED (ESCAPE SLIDE)

DURING INSTALLATION OF ENTRY DOOR ESCA PE SLIDE LOCKOUT PIN FOUND DEACTIVATION PIN INSTALLED. REMOVED INSTALLED PIN AND ROUTED TO QC SDF.

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 5,395 hrs · 3,425 cycles

NR 2 PYLON LOWER AFT DOUBLER ANGLE CRACKED. REMOVED AND REPLACED LOWER AFT DOUBLER ANGLE ON NR 2 PYLON IAW A300 SRM 51-40-00.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 5,395 hrs · 3,425 cycles

NR 1 PYLON LOWER AFT DOUBLER ANGLE CRACKED INBD SIDE. REMOVED AND REPLACED LOWER AFT DOUBLER ANGLE ON THE NR 1 PYLON IAW A300 SRM 51-40-00.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 5,395 hrs · 3,425 cycles

RT INBD FLAP TOP MID FWD CHAFING. REPAIRED FLAP IAW A300 SRM 57-50-00 FIG 205 AND 51-25-00.

Part: WINDSHIELD — FAILED (COCKPIT)

INSPECTION TYPE:N/A CAPTS WINDSHIELD OUTER PANE SHATTERED. REMOVED AND REPLACED CAPT WINDSHIELD SRT 56-11-11-4.

Part: BRAKE — FIRE (MAIN BRAKE SYS)

DURING BLOCK IN NR 4 BRAKE WAS SEEN TO BE ON FIRE. SMALL AREA OFF BRAKE ONLY. WHEEL ASSY AND GEAR AREA NOT AFFECTED. REMOVED AND REPLACED NR 4 BRAKE UNIT IAW MM 32-42-27-4.

Part: POWER SUPPLY — MALFUNCTIONED (CABIN)

INSPECTION TYPE:PFLT DOOR CABIN ESCAPE SLIDE WARNING LIGHT DID NOT TEST DURING PREFLIGHT. RESET AUTONOMOUS STANDBY POWER SUPPLY UNIT, WARNING LIGHT TESTS NORMALLY.

Part: SLIDE — MALFUNCTIONED (COCKPIT)

INSPECTION TYPE:N/A DOOR SLIDE DIFFICULT TO ARM ON LAST 2 LEGS. CHECKED ESCAPE SLIDE ARM IAW MM 25-61-20-5, FOUND SATISFACTORY. LUBRICATED TELESCOPIC UNIT IAW MM 12-22-52, CHECKED OK.

Part: FUSIBLE PLUG — OVERTEMP (NR 5 BRAKE)

NR 5 BRAKE OVERTEMP CAUSING NR 5 TIRE FUSE PLUG TO BLOW. *** OPEN ***

Part: LIGHT — INOPERATIVE (EVACUATION SLIDE)

EVACUATION SLIDE WARNING LIGHT INOP. RESET POWER TO ADJUST POWER AND TESTED LIGHT IAW AMM 5273-11-4. THIS CLEARS M260785 - PLACARD REMOVED.