N160UP

Part: SKIN — DAMAGED (ZONE 100) · airframe 25,309 hrs · 15,046 cycles

LIGHTNING STRIKE DAMAGE ON FUSELAGE BETWEEN FR 23 AND 24, 37 INCHES BELOW LWR FWD CARGO DOOR. BLENDED AREA WITHIN ALLOWABLE LIMITS AND RESTORED FINISHED TO THE REQUIREMENTS OF SRM 53-10-12 REPAIR 6.

Part: SKIN — DAMAGED (MLG DOOR) · airframe 25,305 hrs · 15,045 cycles

LIGHTNING STRIKE DAMAGE ON RIGHT NOSE GEAR DOOR 2€?AFT OF LE, 6€? OF OUTBD EDGE

Part: SKIN — DAMAGED (ZONE 100) · airframe 25,305 hrs · 15,045 cycles

LIGHTNING STRIKE DAMAGE ON FUSELAGE BETWEEN FR 23 AND 24, 37 INCHES BELOW LWR FWD CARGO DOOR.

Part: DOOR — DAMAGED (NLG) · airframe 25,309 hrs · 15,046 cycles

LIGHTNING STRIKE DAMAGE ON RIGHT NOSE GEAR DOOR 2€?AFT OF LE, 6€? OF OUTBD EDGE ADDRESSED AREA AS PER AMM 12-21-11.

Part: DOOR — DAMAGED (NLG) · airframe 25,309 hrs · 15,046 cycles

LIGHTNING STRIKE DAMAGE ON RIGHT NOSE GEAR DOOR 1€?FWD OF AFT EDGE, 10€? FROM OUTBD EDGE. REPAIRED IAW SRM 53-10-12.

Part: SKIN — DAMAGED (ZONE 100) · airframe 25,305 hrs · 15,045 cycles

LIGHTNING STRIKE DAMAGE ON FUSELAGE RT SIDE AT 2410 35€? BELOW WING.

Part: SKIN — DAMAGED (ZONE 100) · airframe 25,309 hrs · 15,046 cycles

LIGHTNING STRIKE DAMAGE ON FUSELAGE RT SIDE AT 2410 35€? BELOW WING. PERFORMED A DVI AT STATION 2410 35 INCHES BELOW WING RIGHT HAND SIDE. AT ORANGE TAPE THERE WAS A BLACK SPECK ON FUSELAGE. WIPED ENTIRE AREA DOWN WITH ACETONE. NO LIGHTNING STRIKE NOTED IN THE AREA. CLEANED IAW AMM 12-21-11.

Part: SKIN — DAMAGED (MLG DOOR) · airframe 25,305 hrs · 15,045 cycles

LIGHTNING STRIKE DAMAGE ON RIGHT NOSE GEAR DOOR 1€?FWD OF AFT EDGE, 10€? FROM OUTBD EDGE.

Part: ADC — FAULTED (ZONE 200) · airframe 24,700 hrs · 14,722 cycles

ECAM: NAV ADC FAULT 2 FAULT WAS INTERMITTENT EVERY 30 SECONDS / USE EMERGENCY CANCEL TO STOP AUDIO ALERT TROUBLESHOT PER TSM CH 34-10-00-101 FIGURE 103. PERFORMED BITE TEST OF ADC #2 BOX. NO FAULTS FOUND. PERFORMED BITE TEST OF ADC #2 SYSTEM PER AMM CH 34-10-00-501. NO FAULTS FOUND. AIRCRAFT OK FOR SERVICE. WORK PERFORMED BY CAT CERTIFIED MECHANIC

Part: HYDRAULIC SYSTEM — LEAKING · airframe 24,367 hrs · 14,541 cycles

**EMERGENCY DECLARED**ECAM GREEN HYD RES LO , FLUID QTY INDICATION LOSS OF FLUID. COMPLIED WITH ECAM / ARCH PROCEDURES SERVICED GREEN HYDRAULIC WITH 2 GALLONS REF AMM 12-12-29/0001

Part: ADAPTER — BROKEN (FRM 19) · airframe 24,177 hrs · 14,430 cycles

FOUND BROKEN "CLS" ADAPTOR , RH FR19 BETWEEN MCD FLOOR PANELS 222DG AND 232EF REMOVED AND REPLACED CLS ADAPTER IN R/H FR 19 IAW A300 SRM 51-40-21 PARAGRAPH 7. P/N: B5377413820200 S/N: TAG 02036446. INSTALLED MCD FLOOR PANELS 222DE AND 232EF. IAW AMM 53-10-23-0401.

Part: SUPPORT ANGLE — CRACKED (FRM 38) · airframe 24,177 hrs · 14,430 cycles

FAULT -A300 OPEN Z200 - RH FR 38.1 MAIN CARGO DECK SUPPORT ANGLE IS CRACKED. INSTALLED STIFFENER AT FRAME 38.1 R/H TO 38.2 R/H IAW SRM 51-40-21 P/N HL11VF6-3 BATCH #0004186230 P/N HL116-6 BATCH# 4279917 P/N 3D0006-3 BATCH# 0004273630 REVIEWED.

Part: SUPPORT ANGLE — CRACKED (FRM 37) · airframe 24,177 hrs · 14,430 cycles

FAULT -A300 OPEN Z200 - RH FR 37 MAIN CARGO DECK SUPPORT ANGLE IS CRACKED. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-40-21 P/N HL11VF6-3 BATCH# 0004186230 P/N 3D0006-3 BATCH# 0004273630 REVIEWED.

Part: SUPPORT ANGLE — CRACKED (FRM 38) · airframe 24,177 hrs · 14,430 cycles

RH FR 38.2 MAIN CARGO DECK SUPPORT ANGLE IS CRACKED TREATED AND PRIMED NEW CUSP WEB IAW A300 SRM 51-21-10 PRIMER PN: 10P4-2NF BATCH: 8473297014 ALODINE1132 BATCH: 1445846. APPLIED TOPCOAT IAW A300 SRM 51-75-10-201 P/N ECL-G-101

Part: CUSP WEB — BROKEN (FRM 38) · airframe 24,177 hrs · 14,430 cycles

BROKEN CUSP WEB AT MCD LH FR 38.2 TREATED AND PRIMED NEW CUSP WEB IAW A300 SRM 51-21-10 PRIMER PN: 10P4-2NF BATCH: 8473297014 ALODINE1132 BATCH: 1445846. APPLIED TOPCOAT IAW A300 SRM 51-75-10-201 P/N ECL-G-101 BATCH: 4266626

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 24,177 hrs · 14,430 cycles

FWD CARGO FLOOR PANEL 131AH IS DAMAGED REVIEWED.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 24,177 hrs · 14,430 cycles

FWD CARGO FLOOR PANEL 131RG IS DAMAGED APPROVED.

Part: FLOORBOARD — BROKEN (FWD CARGO) · airframe 24,177 hrs · 14,430 cycles

FWD CARGO FLOOR PANEL 131FE IS DAMAGED FABRICATED FWD CARGO FLOOR PANEL 131FE P/N B5327052700000 USING MATERIAL P/N 5024N400001SS-G BATCH:0004055277 I.A.W. SREO A300-5320-16407-E.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 24,177 hrs · 14,430 cycles

FWD CARGO FLOOR PANEL 131FE IS DAMAGED APPROVED.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 24,177 hrs · 14,430 cycles

FWD CARGO FLOOR PANEL 131AH IS DAMAGED.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 24,177 hrs · 14,430 cycles

- FWD CARGO FLOOR PANEL 131RG IS DAMAGED. COMPLETED SREO-16407-REQ002 ((APPX C). JOB IS NOW COMPLETE.

Part: REPAIR — DAMAGED (RT WING TE FLAP) · airframe 24,177 hrs · 14,430 cycles

RIGHT WING INNER FLAP HAS A DAMAGED EXISTING REPAIR DOUBLER. INSTALLED REPAIR DOUBLER AT INNER FLAP IAW SRM 57-50-00-201. APPLIED TOP COAT AT REPAIR DOUBLER ON INNER FLAP IAW SRM 51-23-10-001. ACCOMPLISH A PERMANENT REPAIR PER SRM REV. 40, 57-50-00-201 PARAGRAPH 4.E., FIGURE 205.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 24,177 hrs · 14,430 cycles

MAIN CARGO FLOOR PANEL 231LG HAS A CRACK UNDER PANEL.DOT 135/057 FABRICATED M.D.C. FLOOR PANEL 231LG PN: B5327073500000 USING MATERIAL PN:5024N400001SS-G BTCH: 0004055277 I.A.W. S.R.O.A300-5320-40552.

Part: REPAIR — DAMAGED (RT WING TE FLAP) · airframe 24,177 hrs · 14,430 cycles

OPEN, RW INNER FLAP HAS A DAMAGED EXISTING REPAIR DOUBLER AND FILLED OUT MEASUREMENTS

Part: FLOOR PANEL — BROKEN (MAIN CARGO) · airframe 24,177 hrs · 14,430 cycles

MAIN CARGO FLOOR PANEL 232WG FOUND TO BE CRACKED ON BOTTOM FABRICATED M.D.C. FLOOR PANEL 232WG PN: B5327074600400 USING MATERIAL PN:5024N400001SS-G BTCH: 0004055277 I.A.W. S.R.O.A300-5320-40552. INSTALLED FLOOR PANEL 232WG IAW A300 AMM 53-10-23-0401.

Part: SUPPORT ANGLE — CORRODED (FRM 54) · airframe 24,177 hrs · 14,430 cycles

FAULT - MXP-531535-01-1-151- AFT CARGO FR54 BLKHD RH UPPER ANGLE IS CORRODED DOT 5612-1 INSTALLED NEW AFT CARGO BLKH RIGHT UPPER ANGLE IAW SRM 51-40-21 REVIEWED

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 24,177 hrs · 14,430 cycles

AFT CARGO CEILING SUPPORT AT FR54.2 IS CORRODED. TREATED AND PRIMED NEW CEILING SUPPPORTS (2EA) IAW SRM 51-21-10. INSTALLED 2EA CEILING SUPPORTS IAW SRM 51-40-21.

Part: SUPPORT — CORRODED (CABIN) · airframe 24,177 hrs · 14,430 cycles

AFT CARGO CEILING SUPPORT AT FR62 IS CORRODED. TREATED AND PRIMED SUPPORT IAW SRM 51-21-10. INSTALLED CELING SUPPORT IAW SRM 51-40-21.

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 24,177 hrs · 14,430 cycles

AFT CARGO CEILING SUPPORT AT FR58 IS CORRODED. VERIFIED APPLICATION OF TOPCOAT ON CEILING SUPPORT AND OK TO INSTALL CEILING SUPPORT GIVEN INSP ONLY. INSTALLED CEILING SUPPORT IAW A300 SRM 51-40-21.

Part: SUPPORT — CORRODED (CABIN) · airframe 24,177 hrs · 14,430 cycles

AFT CARGO CEILING SUPPORT AT FR57 IS CORRODED. TREATED AND PRIMED SUPPORTS IAW A300 SRM 51-21-10. INSTALLED 2EA CEILING SUPPORTS IAW SRM 51-40-21.

Part: FLOOR PANEL — BROKEN (MAIN CARGO DECK) · airframe 24,177 hrs · 14,430 cycles

**SDR FILED OPEN** FAULT- MCD FLOOR PANEL 231WG IS BROKEN INSTALLED FLOOR PANEL 231WG IAW A300 AMM 53-10-23-0401.

Part: ANGLE — CRACKED (FRM 10) · airframe 24,177 hrs · 14,430 cycles

ACCESS AVIONICS AREA FRAME 10 Y-953 INTERCOASTAL HAS PREVIUOS REPAIR CRACKED 3 INCHS LONG IN THE CORNER NO DOT. INSTALLED 1EA. ANGLE P/N UPA53610270522 AND 1EA. WEB P/N UPA5361197720201 IAW SRM 51-40-21.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 24,177 hrs · 14,430 cycles

TWO CRACKS FOUND ON RIB FLANGE 11 RIGHT WING FLAP. COMPLIED WITH UPS EO-90101 AND VTMAE FINAL EA 300-5750-27-A3570 REV-.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 24,177 hrs · 14,430 cycles

ONE CRACK FOUND ON RIB FLANGE 17 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.

Part: SHROUD — GOUGED (LT WINGTIP) · airframe 24,177 hrs · 14,430 cycles

LEFT WINGTIP LE HAS A DENT FRONT INBD SIDE. APPLIED TREAT AND PRIMER IAW SRM 51-21-10 PARAGRAPH 2. INSTALLED NEW SHROUD ASSY IAW SRM 51-40-21, PARAGRAPH 13. INSTALLED STRIP IAW IAW SRM 51-40-21 PARAGRAPH 5. APPLIED TOP COAT IN AREA IAW SRM 51-75-10, PARAGRAPH 3.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 24,177 hrs · 14,430 cycles

TWO CRACKS FOUND ON RIB FLANGE 25 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 24,177 hrs · 14,430 cycles

ONE CRACK FOUND ON RIB FLANGE 12 RT WING FLAP. COMPLIED WITH UPS EO-90101 AND VTMAE FINAL EA 300-5750-27-A3570 REV-.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 24,177 hrs · 14,430 cycles

TWO CRACKS FOUND ON RIB FLANGE 18 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 24,177 hrs · 14,430 cycles

CRACK FOUND RIB FLANGE 27A LEFT FLAP TOP SKIN. ACCOMPLISH PERMANENT REPAIR PER EO-90102-REQ1 AND EA 300-5750-27-A3568 REV -.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 24,177 hrs · 14,430 cycles

TWO CRACKS FOUND ON RIB FLANGE 26 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV-.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 24,177 hrs · 14,430 cycles

TWO CRACKS FOUND ON RIB FLANGE 13 RT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 24,177 hrs · 14,430 cycles

ONE CRACK FOUND ON RIB FLANGE 15 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 24,177 hrs · 14,430 cycles

ONE CRACK FOUND ON RIB FLANGE 26 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 24,177 hrs · 14,430 cycles

TWO CRACKS FOUND ON RIB FLANGE 27 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 24,177 hrs · 14,430 cycles

CRACK FOUND ON RIB FLANGE 19 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 24,177 hrs · 14,430 cycles

**SDR FILED OPEN** FAULT: 1 CRACK FOUND ON RIB FLANGE 17A RIGHT WING FLAP. VERIFIED STEP # 31 COMPLETED .

Part: COVER PLATE — CRACKED (FRM 40) · airframe 24,177 hrs · 14,430 cycles

FAULT: CRACK FOUND ON FR40 R/W LOWER CORNER RADIUS AT 6 O'CLOCK POSITION FACING FORWARD. INSTALLEED REPAIR PARTS IAW DRAWING R53810798 REV C AND SRM 51-40-21 AND EO 64579-JIC004 REV 1. INSTALLED RIB AND INTERCOSTAL AT FR 40 L/E IAW SRM 51-40-21 AND EO 64579-JIC004 REV 1. REVIEWED.

Part: COVER PLATE — CRACKED (FRM 40) · airframe 24,177 hrs · 14,430 cycles

FAULT: MULTIPLE CRACKS FOUND ON F40 L/W LOWER RADIUS HOLE AROUND 9-11 O'CLOCK FACING FOWARD. INSTALLED REPAIR PARTS IAW DRAWING R53810798 REV C AND SRM 51-40-21 AND EO 64579-JIC003 REV 1. RE-INSTALLED RIB AND INTERCOSTAL AT FR 40 L/E IAW SRM 51-40-21 AND EO 64579-JIC003 REV 1. REVIEWED.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 24,177 hrs · 14,430 cycles

**SDR FILED OPEN**FAULT - LH OUTBOARD FLAP HAS DENT IN LEADING EDGE VERIFIED TOP COAT APPLICATION STEP 49.

Part: DOOR — INOPERATIVE (UNKNOWN) · airframe 23,319 hrs · 13,932 cycles

CREW ENTRY DOOR TOP COVER MISSING AFT UPPER BOLT/WASHER.RE-ATTATCHED SHIMS ON BOTH SIDES OF UPPER HOLES ON PANEL. REPLACED BOTH BOLTS AND WASHERS AND INSTALLED MOVEABLE UPPER PANEL. OPS CHECK GOOD. PANEL MOVES FREELY W/O RESTRICTION MM 52-10-00.

Part: EVAS UNIT — INOPERATIVE (CABIN) · airframe 23,069 hrs · 13,778 cycles

INSPECTION TYPE:N/AEVAS ON CAPT'S SIDE SEPERATED FROM MOUNTEVAS JUST LOOSED ON MOUNT TIGHTENED EVAS BASE MOUNT SCREWS IAW AMM 25-60-00. OK FOR SERVICES

Part: ARM — INOPERATIVE (DOOR SLIDE) · airframe 21,682 hrs · 12,969 cycles

ENTRY DOOR SLIDE ARM TETHERED BROKEN WITH PIN ATTACHED. REMOVED DAMAGE PIN/LANYARD INSTALLED NEW PIN IAW A300 25-61-20 CHECKS GOOD.

Part: NONE — BROKEN (DOOR) · airframe 21,079 hrs · 12,638 cycles

INSPECTION TYPE:N/A** SDR FILED OPEN**CABIN DOOR SLIDE ARM SAFETY PIN CABLE IS BROKEN. DEFERRED MAIN ENTRY DOOR EVAC SLIDE ARMING HANDLE SAFETY PIN LANYARD AS DAMAGED PER NEF LIST REF # 25-70-52-10-08.CONTROL # M-764663 ASSIGNED.PIN IS FUNCTIONAL.

Part: ANGLE — CRACKED (RT K FLAP) · airframe 20,842 hrs · 12,499 cycles

INSPECTION TYPE:CRH KRUEGER FLAP CAVITY SUPPORT ANGLE IS CRACKED.REMOVED AND REPLACED ANGLE IAW SRM 51-40-21.

Part: ANGLE — CRACKED (RT K FLAP) · airframe 20,842 hrs · 12,499 cycles

INSPECTION TYPE:C, CRACKED FRAME CLIP AT RH KRUGER FLAP CAVITY FWD O/B AREA. REMOVED AND REPLACED ANGLE CLIP IAW SRM 51-40-21.

Part: FLT CONTROLS — MALFUNCTIONED · airframe 19,995 hrs · 11,995 cycles

INSPECTION TYPE:NA**ATB -EMERGENCY DECLARED - NO EMERG EQUIP USED - LANDED W/OUT INCIDENT - AC TAKEN OOS** DUE OT EXTREMELY LOUD POPPING SOUNDS UNDER FLOOR. ONCE AIRBORNE THE AIRCRAFT WANTED TO MOVE SIDE TO SIDE. WE DID EXPERIENCE SOME HANDLING ISSUES. TREMENDOUS LOUD SOUNDS COMING UNDER THE FLOOR. ON APP MORE DIFF THAN NORMAL TO MAINTAIN AIRSPEED.R/R'D PCMCIA CARD FOR DATA REC PER MM 31-31-90. ACCOMP COLD WXR MX OF LWR FUSELAGE DRAINS, FOUND STANDING WATER IN AFT CARGO FWD COMP UNDER FLOOR. RMVD FLOOR PNL, REMOVED WATER & REINSTALLED FLOOR PANEL PER MM 12-31-51 & 53-10-33. OK FOR SVC.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 19,554 hrs · 11,764 cycles

INSPECTION TYPE: N/A LT WING INBOARD FLAP UPPER SKIN DAMAGE. REPAIRED PER EO A300-5750-78068-B.

Part: CARRIAGE — OBSTRUCTED (TE FLAP) · airframe 18,708 hrs · 11,272 cycles

INSPECTION TYPE:NA**SUPPLEMENTAL SDR** ** EMERGENCY DECLARED ** LANDED WITHOUT INCIDENT ** TRAILING EDGE FLAPS JAMMED IN THE STOWED 0 POSITION. DEFERRED DISCEPANCY PER FERRY PERMIT NO 9001 C/W ENGINEERING MAINTENANCE ACTIONS PER FORM 52-19-014A.FOUND FOD LODGED IN #2 FLAP CARRIAGE. REMOVED FOD. NO DEFECTS NOTED. FLAPS OPS CHECKED GOOD PER AMM 27-50-00-0301. D705396 CLOSED.

Part: HANDLE — CRACKED (L1 DOOR) · airframe 18,707 hrs · 11,271 cycles

INSPECTION TYPE:N/AINNER CREW DOOR UPPER HANDLE ASSY CRACKEDREPLACED REPLACED CREW DOOR INNER UPPER HANDLE ASSY IAW AMM 52-10-13. ESR: A300 IPC 52-11-11-03C

Part: COALESCER BAG — ODOR (AC BAY) · airframe 18,628 hrs · 11,222 cycles

INSPECTION TYPE:N/AINFLIGHT #1 PAC HAS BURNING RUBBER SMELL.R&R # PAC COALESCER BAG I.A.W. AMM 21-51-16-0301. OPERATED PACK FOR 30 MINUTES, NO UNUSUAL ODORS NOTED. EFF SOURCE REF: IPC 21-54-01-01A

Part: LINK — BROKEN (L1 DOOR HANDLE) · airframe 18,126 hrs · 10,949 cycles

L1 DOOR WILL NOT CLOSE AND LOCK WITH EXTERIOR HANDLE, BROKEN PARTS REMOVED AND INSTALLED NEW HANDLE CONNECTING LINKS. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (LOWER SKIN) · airframe 17,911 hrs · 10,835 cycles

INSPECTION TYPE:N/ART INBD MAIN FLAP LWR SKIN AND STRINGER DAMAGED.REMOVED DAMAGE. HFEC FOR CRACKS. PERFORMED STRINGER REPAIR. INSTALLED FILLER AND DOUBLER. COMPLETED EO A300-5750-74381A.

Part: LATCH — DIRTY (CREW DOOR) · airframe 17,633 hrs · 10,676 cycles

CREW ENTRY DOOR WILL NOT LATCH FROM OUTSIDE. CLEANED AND LUBED EXTERNAL HANDLE LINKAGE, OPERATED L1 DOOR WITH EXTERNAL HANDLE SEVERAL TIMES, DOOR OPERATES NORMAL IAW 52-10-00.

Part: ACCESS PANEL — CRACKED (NR 1 PYLON) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:12YR #1 PYLON UPPER THE PRE-COOLER COVER ACCESS PANEL 413BL HAS A CRACK ON THE INSIDE RUNNING ALONG THE FASTENER FLANGE APPROX. 12 TO 14 INCHES LONG. REPAIRED PART IAW SRM 54-52-51.

Part: SHROUD — GOUGED (RT WING) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:123C, RT WING OTBD FIXED WING L/E FWD CORNER WAS GOUGED AFT OF THE NR 3 SLAT OTBD END. REPLACED THE SHROUD IAW SRM 51-40-21, AND DWG A57244218.

Part: WEB — CRACKED (FRAME 47) · airframe 17,508 hrs · 10,599 cycles

FRAME 47, Y450 WEB FOUND CRACKED AT DRAIN HOLE. REPAIRED PER SRM 53-15 PB 201.

Part: WEB — CRACKED (FRAME 47) · airframe 17,508 hrs · 10,599 cycles

FRAME 47 TO-Y450 WEB IS CRACKED AT DRAIN HOLE. REPAIRED PER SRM 53-15-15 PB 201.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:123C, PANEL 132QG CRACKED ON UPPER SURFACEFAB'D NEW PANEL IAW UPS EO A300-5320-16407

Part: SUPPORT BRACKET — CRACKED (AFT CARGO) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:12YRAFT CARGO FR54 PRESSURE BULKHEAD LH INBD SUPPORT BRACKET (2EA) IS CRACKED. DOT H902 & H903REMOVED & REPLACED.

Part: BRACKET — CRACKED (FRAME 54) · airframe 17,508 hrs · 10,599 cycles

AFT CARGO FR-54 PRESSURE BULKHEAD RH OUTBD SUPPORT BRACKET (1EA) IS CRACKED.REMOVED AND REPLACED

Part: SUPPORT BRACKET — CRACKED (AFT CARGO) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:12YR AFT CARGO FR54 PRESSURE BULKHEAD LH INBD SUPPORT BRACKET (2EA) IS CRACKED. DOT H902 & H903.REMOVED & REPLACED.

Part: SUPPORT BRACKET — CRACKED (FRAME 54) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:12YRAFT CARGO FR54 PRESSURE BULKHEAD RH OUTBD SUPPORT BRACKET (1EA) IS CRACKED.REMOVED & REPLACED.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:12YR INSIDE CENTER WING BOX RT FR47 DOUBLER HAS 7 EA GOUGES. REPAIR PER EO #A300-5710-73067-A.

Part: BULKHEAD WEB — CRACKED (NR 2 INLET) · airframe 17,508 hrs · 10,599 cycles

NR 2 ENG INLET COWL AFT BULKHEAD WEB CRACKED 3 O'CLOCK POSITION AT SENSE LINE FITTINGREPAIR PER PW SRM 54-10-00 REPAIR #14

Part: BULKHEAD WEB — CRACKED (NR 2 INLET) · airframe 17,508 hrs · 10,599 cycles

NR 2 ENG INLET COWL AFT BULKHEAD WEB CRACKED 9 O'CLOCK POSITION AT SENSE LINE FITTINGREPAIR PER PW SRM 54-10-00 REPAIR #14

Part: SKIN — CORRODED (FUSELAGE) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:12YRBULK PIT DOOR CUTOUT IS CORRODED AT AFT LOWER CORNER.REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW A300 SRM 51-74-10. RESTORED SURFACE IAW A300-600 SRM 51-21-10 AND 51-75-10.

Part: SUPPORT BRACKET — CRACKED (FRAME 54) · airframe 17,508 hrs · 10,599 cycles

AFT CARGO FR54 PRESSURE BULKHEAD LH OUTBD SUPPORT BRACKET 1EA IS CRACKEDREMOVE AND REPLACE SUPPORT BRACKET IAW 51-40-21

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:123C APU AFT BULKHEAD AFT SIDE HAS CRACK R/H SIDE AT EXHAUST NOZZLE ATTACH BRACKET.REPAIRED IAW EO A300-5310-73116-A.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:123CMAIN CABIN FLOOR PANEL 241FK IS CRACKED.FABRICATED NEW PANEL.

Part: SUPPORT BRACKET — CRACKED (FR54 BULKHEAD) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:12YRAFT CARGO FR54 PRESSURE BULKHEAD CENTER SUPPORT BRACKET 1EA IS CRACKED.REMOVED AND REPLACED IAW A300-600 SRM 51-40-21.

Part: WEB — BENT (FRAMES 86-87) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:123C, ONE INTERCOSTAL RH FRAMES 86 TO 87 IS BENT THRU 312AR. REMOVED AND REPLACE IAW SRM 51-40-21

Part: STRUCTURE — GOUGED (CARGO DOOR FRAME) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:12YRLOWER CARGO DOOR SURROUND AFT MIDDLE SEALING SECTION IS GOUGED AT MULTIPLE AREAS.REMOVED AND REPLACED IAW A300-600 SRM 51-40-21.

Part: STRUCTURE — GOUGED (FWD CARGO DOOR) · airframe 17,508 hrs · 10,599 cycles

LOWER FWD CARGO DOOR SURROUNDING FWD UPPER SEALING SECTION IS GOUGED AND BENT.REMOVED AND REPLACED SEALING SECTION IAW 51-40-21.

Part: SKIN — CRACKED (FRAME 20) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:12YRFWD LOWER CARGO DOOR SURROUNDING HAS GOUGE ON EDGE OF FUSELAGE SKIN FR20 APPROX. STGR 40RH.BLENDED DAMAGE, FOUND TO BE WITHIN LIMITS AND RESTORE SURFACE IAW A300-600 SRM 53-13-12.

Part: STRUCTURE — GOUGED (CARGO DOOR FRAME) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:12YRLOWER CARGO DOOR SURROUND AFT LOWER SEALING SECTION IS GOUGED AT MULTIPLE AREAS.REMOVED AND REPLACED IAW A300-600 SRM 51-40-21.

Part: LINER — CRACKED (BULK CARGO DOOR) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:12RYLOWER BULK CARGO DOOR LINER CRACKED IN MULTIPLE LOCATIONSREPAIRED PER UPS SREO #A300-2550-43367-B

Part: LINER — CRACKED (CARGO DOOR) · airframe 17,508 hrs · 10,599 cycles

LOWER FWD CARGO DOOR LINER PNL 811-AZ IS CRACKED AT MULTIPLE AREAS AS MARKED.REPLACED LINER WITH NEW.

Part: COVER — CRACKED (FRAME 20) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:5YR FWD LOWER CARGO COMPARTMENT DR 20 CORNER COVER PN A25576510200 REQUIRES FABRICATION DUE TO NO PART AVAILABLEFABRICATED NEW CORNER COVER IAW DWG A25576545. INSTALLED NEW CORNER COVER IAW SRM 51-40-21

Part: LINER — CRACKED (CARGO DOOR) · airframe 17,508 hrs · 10,599 cycles

LOWER AFT CARGO DOOR LINER PNL 812-BZ IS CRACKED AT MULTIPLE AREAS AS MARKED.REPAIRED AREAS IAW UPS EO NO. A300-2550-43367-B.

Part: FLOORBOARD — CRACKED (AFT CARGO) · airframe 17,508 hrs · 10,599 cycles

CRACKED LOWER FLOORBOARD SKIN. FABRICATED NEW FLOORBOARD IAW EO #A300-5320-16407-E REV.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 17,508 hrs · 10,599 cycles

MAIN CABIN FLOOR PANEL IS DAMAGED AT FASTENER HOLE. REPAIRED PER SREO A300-5320-42722-F.

Part: FLOOR PANEL — DAMAGED (FRAMES 47-51) · airframe 17,508 hrs · 10,599 cycles

MAIN CABIN FLOOR PANEL IS DELAMINATED. FABRICATED AND REPLACED FLOOR PANEL PER UPS SREO A300-5320-40552-B.

Part: FLOOR PANEL — CRACKED (FR22-27) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:123CMAIN CABIN FLOOR PANEL IS CRACKEDFABRICATED AND REPLACED PANEL PER UPS SREO# A300-5320-40552

Part: TUBE — CRACKED (SMOKE DETECTOR) · airframe 17,508 hrs · 10,599 cycles

MAIN CABIN FR46-42 SMOKE DETECTOR TUBE IS CRACKEDREPAIRED PER DUCT REPAIR MANUAL DRM

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:123C, MAIN CABIN FLOOR PANEL IS CRACKED. FABRICATED AND REPLACED PANEL PER SREO# A300-5320-40552.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:12YMAIN CABIN FLOOR PANEL 251DG HAS EDGE DAMAGEREPAIRED PER UPS REO A300-5320-42722-F.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:123C, MAIN CABIN FLOOR PANEL IS CRACKED, FABRICATED AND REPLACED PANEL PER UPS SREO# A300-5320-40552.

Part: SHEAR PLATE — CRACKED (FRAME 79) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:12YRFR79 STRG 26R SHEAR PLATE CRACKEDREMOVED AND REPLACED PER UPS SREO #A300-5310-58168-A

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:123C, MAIN CABIN FLOOR PANEL HAS EDGE DAMAGE. REPAIRED PER SREO# A300-5320-42722-F.

Part: BRACKET — CRACKED (RT WING K FLAP) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:123CR/W I/B KREUGER FLAP FWD IWR CLOSE OUT WELL I/B BRACKET CRACKEDREMOVED AND REPLACED BRACKET PER A300-600 SRM 51-40-21

Part: BRACKET — CRACKED (RT WING K FLAP) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:123CR/W I/B KREUGER FLAP AFT CLOSE OUT WELL I/B BRACKET CRACKEDREMOVED AND REPLACED BRACKET PER A300-600 SRM 51-40-21

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:12YRR/W I/B FLAP UPPER SURFACE PREVIOUS DOUBLER GOUGEDREMAKE REPAIR DOUBLER PER A300-600 SRM 57-50-00 PARA 4E

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:123C, MAIN CABIN FLOOR PANEL HAS EDGE DAMAGE.REPAIRED PER UPS EO# A300-5320-42721-F.

Part: SKIN — CRACKED (WING) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:123C, PANEL 423CL HAS MULTIPLE CRACKS. REPLACED THE PANEL PER A300-600 SRM 51-40-21.

Part: SEAT TRACK — CRACKED (FRAME 79) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:12YR FR79, Y1589.5 SEAT TRACK ANGLE IS CRACKEDREMOVED AND REPLACED PER SRM 51-40-21 AND A300-600 DWG A53278757 ISSUE C

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:123C, MAIN CABIN FLOOR PANEL 251CH IS DELAMINATED. FABRICATED AND REPLACED FLOOR PANEL PER SREO A300-5320-40552-B

Part: SHEAR PLATE — CRACKED (FRAME 79) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:12YRFR79 STGR 26L SHEAR PLATE CRACKEDREMOVED AND REPLACED PER UPS SREO #A300-5310-58168-A

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:123CMAIN CABIN FLOOR PANEL HAS DAMAGE BY FASTENER HOLE.REPAIRED PER UPS EO# A300-5320-42722-F.

Part: SEAT TRACK — CRACKED (FRAME 79) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:12YR FR79, -Y1589.5 SEAT TRACK ANGLE IS CRACKEDREPLACED DISCREPANT ANGLE PER UPS EO #A300-5310-72852-A

Part: PANEL — DAMAGED (NR 2 PYLON) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:12YR #2 PYLON PANEL #481AL HAS COMPOSITE DAMAGE. REPAIRED PER EO A300-5450-72982-A.

Part: FLOORBOARD — DELAMINATED (FWD CARGO) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:12YREDGE OF PANEL WAS CRACKED AND DEELAMINATED IN SEVERAL PLACESFABRICATED NEW PANEL IAW UPS EO A300-5320-16407-E

Part: FAIRING — CORRODED (TE FLAP) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:123C LT WING, AFT FLAP FAIRING 533BB CORRODED AT STATIC WICK BASE AREA. REPLACED STATIC WICK BASE & EARTHPLATE IAW EO NO. A300-5750-28259A.

Part: FLOORBOARD — CRACKED (FWD CARGO) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:12YREDGE OF PANEL WAS CRACKED AND DELAMINATED IN SEVERAL PLACESFABRICATED NEW PANEL IAW UPS EO A300-5320-16407-E

Part: LIFE VEST — MISSING (SUPERNUMERARY) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:123C, SUPERNUMERARY AREA MIDDLE SEAT MISSING LIFE VESTINSTALLED NEW LIFE VEST P/N P01074-201C S/N 18080430010 IAW A300-600 AMM 25-60-00

Part: SUPPORT — CRACKED (NR 2 NACELLE) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:123C, NR 2 PYLON ACCESS PANEL 424CR SUPPORT STRUCTURE, FORWARD UPPER CORNER REENFORCING CLIP WAS CRACKED. REMOVED AND REPLACED THE FISHPLATE PER SRM 51-40-21, AND DWG A54612371.

Part: FAIRING — CORRODED (TE FLAP) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:123C LT WING, AFT FLAP FAIRING 535BB CORRODED AT STATIC WICK BASE AREA. REPLACED STATIC WICK EARTHPLATE AND BASE IAW EO NO A300-5750-28259-A.

Part: SUPPORT — CRACKED (NR 2 PYLON) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:12YR #2 PYLON SUPPORT STRUCTURE FOR ACCESS PNL 423EL CRACKED. REMOVED AND REPLACED WEB PER DWG #A546114022000 AND SRM 51-40-21.

Part: LATCH — CORRODED (#2 COWLING) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:12YR #2 ENG O/B AND I/B FAN COWLS LATCHING PLATES HAS FRETTING CORROSION. REMOVED AND REPLACED PER PW CMM 71-13-07.

Part: SKIN — GOUGED (FRAMES 19-20) · airframe 17,508 hrs · 10,599 cycles

EXTERIOR FUSELAGE SKIN JUST AFT OF POWER RECEPTACLE GOUGED. MARKED IN REDFOUND GOUGE TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-12. ORIG MAT'L THK .071" REMOVED .039"; REMAINING .032" REPAIR IAW SRM 51-40-50 AND 53-10-12, FIGURE 207, SHT 3.

Part: COVER — DENTED (FWD CARGO) · airframe 17,508 hrs · 10,599 cycles

INSPECTION TYPE:5YR FWD LWR CARGO COMPARTMENT CEILING COVER PROFILE DENT REPAIRREMOVED AND REPLACE COVER PROFILE IAW A300-600 SRM 51-40-21

Part: EPSU — FAILED (CABIN) · airframe 16,348 hrs · 9,939 cycles

REPLACED ENG PWR SUPPLY UNIT (EPSU) BATTERY SYSTEM FAILS TEST PER AMM 33-51-14-0401 F. RELAMPED SW 25WL OP CKS NORMAL PER AMM 33-51-14-0401.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 16,022 hrs · 9,766 cycles

DAMAGE TO DOUBLER BETWEEN FR 85-86 S544R & 543R. REPAIRED PER EO A300-5330-68428-B.

Part: WARNING BUZZER — MALFUNCTIONED (DOOR SLIDE) · airframe 15,978 hrs · 9,740 cycles

FORWARD DOOR ESCAPE SLIDE WARNING HORN WAS INTERMITTENT. REPLACED L1 EVAC SLIDE RELEASE WARNING BUZZER IAW MM 52-73-12-0401, OPS CHECKED NORMAL.

Part: PUMP — LOW PRESSURE (HYD SYSTEM) · airframe 13,678 hrs · 8,404 cycles

AFTER TAKE OFF, RECEIVED INDICATIONS OF BOTH GREEN SYSTEM HYDRAULIC PUMPS WERE PRODUCING LOW PRESSURE. DECLARED EMERGENCY AND RETURNED TO DEPARTURE. ACCOMPLISHED GEAR RETRACTION AND EXTENSION TEST IAW MM 32-31-00-501 AND MLG AND NLG INDICATING AND WARNING TEST IAW MM 32-61-00-501. ALL SYSTEMS OPS CK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,409 hrs · 8,243 cycles

ENTRY DOOR EXIT LIGHT HAS NUMEROUS BULBS INOPERATIVE, RELAMPED. OPS CK NORMAL, REF AMM 33-51-13.

Part: STOWAGE BOX — NO TEST (COCKPIT OXYGEN) · airframe 12,181 hrs · 7,453 cycles

F/O OXYGEN BOX WILL NOT TEST PROPERLY. R & R F/O OXYGEN STORAGE BOX AMM 35-12-51-0401.

Part: INDICATION SYS — MALFUNCTIONED (FUEL QTY)

LOST ALL RT SIDE FUEL QTY AND RT SIDE ECAM FUEL INDICATIONS. R & R FUEL QTY COMPUTER REF MM 28-42-38, TESTED REF MM 28-42-38, TESTS GOOD. INSPECTED NOSE EXTERIOR NLG WHEEL WELL AREA, AND AVIONICS BAY FOR DAMAGE OR ABNORMALITIES. NONE NOTED. ACFT OK FOR SERVICE.

Part: SPACER — MISINSTALLED (L1 GIRTBAR)

DOOR SLIDE WOULD NOT DISARM, R & R BOTH GIRT BAR SLIDERS, FOUND SPACER FOR SLIDER LINKAGE GUIDE IMPROPERLY INSTALLED. INSTALLED SPACER ON PROPER SIDE IAW IPC 52-11-11-18A-180. DOOR AND ARMING HANDLE TEST GOOD REF AMM 52-10-30-0501.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHT IS INOPERATIVE. REPLACED THE LAMPS AND TESTED IAW AMM 33-61-11-0401. OPS CHECKED NORMAL.

Part: FITTING — CRACKED (MAIN CABIN) · airframe 11,215 hrs · 6,833 cycles

MAIN CABIN FLOOR SUPPORT FRAME 12A FITTING IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOOR RT FR 12A FITTING IAW EO A300-5310--23539-G.

Part: SEAT TRACK — CORRODED (FRAME 62) · airframe 11,215 hrs · 6,833 cycles

MAIN CABIN SEAT TRACK IS CORRODED FRAME 62 Y953, REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201.

Part: SEAT TRACK — CORRODED (FRAME 62) · airframe 11,215 hrs · 6,833 cycles

MAIN CABIN SEAT TRACK CORRODED FRAME 62, -Y953. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201.

Part: SEAT TRACK — CORRODED (FRAME 67) · airframe 11,215 hrs · 6,833 cycles

MAIN CABIN SEAT TRACK CORRODED AT FRAME 67, Y0. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201.

Part: FLOORBOARD — DAMAGED (AFT CARGO) · airframe 11,215 hrs · 6,833 cycles

AFT CARGO FLOORBOARD NR 162HF IS ERODED. FABRICATED NEW FLOORBOARD IAW EO A300-5320-16407-E APPENDIX C.

Part: FLOORBOARD — CRACKED (FWD CARGO) · airframe 11,215 hrs · 6,833 cycles

FWD CARGO FLOORBOARD NR 131BH IS CRACKED ALONG CENTER OF PANEL. FABRICATED NEW FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX C.

Part: FLOORBOARD — DENTED (CARGO BAY) · airframe 11,215 hrs · 6,833 cycles

BULK CARGO FLOORBOARD 161JF L/E IS DENTED. FABRICATED NEW FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX D.

Part: SEAT TRACK — CORRODED (FRAMES 80-82) · airframe 11,215 hrs · 6,833 cycles

MAIN CABIN SEAT TRACK IS CORRODED FRAMES 80-82, -Y794.3. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201.

Part: SEAT TRACK — CORRODED (FRAMES 80-82) · airframe 11,215 hrs · 6,833 cycles

MAIN CABIN SEAT TRACK IS CORRODED AT FRAMES 80-82, -Y1137.1. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201.

Part: SEAT TRACK — CORRODED (FRAMES 80-82) · airframe 11,215 hrs · 6,833 cycles

MAIN CABIN SEAT TRACK CORRODED AT FRAMES 80-82, Y1137. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201.

Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 11,215 hrs · 6,833 cycles

MAIN CABIN FLOORBEAM IS CRACKED AT FRAME 79 -Y1580. REPAIRED FLOORBEAM IAW EA 300-5310-01-A5323 I/R AND EO A300-5310-54515-A.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 11,215 hrs · 6,833 cycles

RIGHT INBD FLAP UPPER SURFACE SKIN CHAFED. REPAIRED IAW SRM 57-50-00, PARA 4E, FIG 205.

Part: SEAT TRACK — CORRODED (FRAMES 80-82) · airframe 11,215 hrs · 6,833 cycles

MAIN CABIN SEAT TRACK IS CORRODED AT FRAMES 80-82, -Y450. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201.

Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 11,215 hrs · 6,833 cycles

MAIN CABIN FLOORBEAM IS CRACKED AT FRAME 79, Y1580.5. REPAIRED FLOORBEAM IAW EA 300-5310-01-A5323 I/R AND EO A300-5310-54515-A PARA 6A.

Part: SEAT TRACK — CORRODED (FRAMES 80-82) · airframe 11,215 hrs · 6,833 cycles

MAIN CABIN SEAT TRACK CORRODED AT FRAMES 80-82, Y794.3. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201.

Part: SEAT TRACK — CORRODED (FRAMES 80-82) · airframe 11,215 hrs · 6,833 cycles

MAIN CABIN SEAT TRACK CORRODED FRAMES 80-82, Y0. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201.

Part: SEAT TRACK — CORRODED (FRAMES 80-82) · airframe 11,215 hrs · 6,833 cycles

MAIN CABIN SEAT TRACK IS CORRODED AT FRAMES 80-82, Y450. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201.

Part: EPSU — INOPERATIVE (CABIN)

CABIN EPSU WILL NOT TEST. R & R EPSU IAW AMM 33-51-14-0401. OPS CHECKED NORMAL.

Part: SWITCH — FAILED (EMERGENCY LIGHTS)

EMERGENCY LIGHT STAYS ON IN THE DISARM POSITION. R & R LIGHT SWITCH, PERFORMED OPS AND ADJUSTMENT TEST, OPS NORMAL.

Part: LAMP — INOPERATIVE (LAVATORY)

LAVATORY MIRROR LIGHT OUT. LAMPED AND OPS CHECKED GOOD IAW AMM 33-51-21-0401.

Part: PANEL — FAULTY (RUDDER)

UNCOMMANDED RUDDER TRIM FOUND RUDDER/AIL TRIM PANEL FAULTY, UNABLE TO STOP RUDDER FROM TRIMMING. R & R RUDDER AIL TRIM PANEL IAW MM 27-12-31. OPS GOOD.

Part: STRUCTURE — CHAFED (LT WING FLAP) · airframe 8,543 hrs · 5,223 cycles

INSPECTION TYPE:3C, LT WING OTBD FLAP INBD BULLNOSE CHAFED. REPAIRED LT WING OTBD FLAP INBD BULLNOSE BETWEEN RIB 1 AND 2 REF EA 300-5750-01-A3574 AND EO A300-5750-44874-A.

Part: FLAP SYSTEM — FAULTED (TE FLAPS)

ATB DUE TO FLAP SYS 1 & 2 FAULT.RAN ECAM AND QRH PROCEDURES RETURNED TO DEPARTURE. FOUND JAM IND ON BOTH SFCC 1&2 ONE BLACK FOLLOWED BY 4 YELLOW BALLS AND OVER TQ IND POPPED IN RT W/W. PERFORMED TSM 27-50-02 AND AMM 12-13-27, AND MM 12-22-27.

Part: SKIN — DAMAGED (FUSELAGE)

SKIN DAMAGED. REPAIRED IAW EO A300-5330-37219-B.

Part: WEB — DAMAGED (FUSELAGE)

SHEAR WEB DAMAGED. REPAIRED IAW EO A300-5310-37837-A.

Part: SLIDE — MALFUNCTIONED (ENTRY DOOR)

SLIDE WOULD NOT DISARM FROM INSIDE. IT HAD TO BE UNLOCKED FROM OUTSIDE. FOUND FWD GIRT BAR ATTACHMENT BINDING ON FLOOR MOUNT BRACKET. LUBED SLIDING MECHANISM AND CYCLED ARM LEVER SEVERAL TIMES. DOOR NOW OPERATES NORMALLY IAW AMM 52-10-30-05.

Part: GIRT BAR — BENT (PAX DOOR)

EXIT SLIDE IS DIFFICULT TO DISARM, LEVER BINDS. REMOVED BENT GIRT BAR FROM DOOR SLIDE ASSEMBLY. REPLACED GIRT BAR PER MM 25 61 21. THIS CLEARS DEFERRAL.

Part: MECHANISM — LACK OF LUBE (ENTRY DOOR)

INSPECTION TYPE:N/A SLIDE ARMING LEVER ON CREW ENTRY DOOR IS HARD TO MOVE BETWEEN ARM AND DISARM. LUBRICATED SLIDE ARMING MECHANISM AND GIRT BAR PAWLS & ATTACH POINTS IAW A300 MM 12-31-00. OPS CHECK NORMAL.

Part: GIRT BAR — DETACHED (EVAC SLIDE)

INSPECTION TYPE:N/A EMERGENCY EXIT SLIDE WILL NOT DISARM. MECHANICALLY LATCHED IN ARMED POSITION. RE-ATTACHED GIRT BAR SLIDER TO DOOR PER MM 25-61-21-4. OPERATED DOOR SEVERAL TIMES. OK FOR SERVICE.

Part: SLIDE — INOPERATIVE (CREW ENTRY DOOR)

INSPECTION TYPE:N/A CREW ENTRY DOOR SLIDE INOP. CLEAN AND LUBED CREW ENTRY DOOR EMERGENCY HANDLE MECH & LINKAGE CYCLE SEVERAL TIMES. OPS CHECK NORMAL. REF MM 52-10-30-05. CLEAR M403007 PLACARD REMOVED.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 5,649 hrs · 3,454 cycles

5YR MAIN CABIN CARGO COMPARTMENT FLOORBOARD 251BN IS CRACKED FABRICATED FLOORBOARD 251BN IAW EO A300-5320-16407-C APPENDIX B.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 5,649 hrs · 3,454 cycles

INSPECTION TYPE-5YR FWD CARGO COMP FLOORBOARD 132RG IS CRACKED AT LOWER SURFACE. FABRICATED FLOORBOARD 132RG IAW EO A300-5320-16407-C APPENDIX C.

Part: DOUBLER — GOUGED (TE FLAP) · airframe 5,649 hrs · 3,454 cycles

5 YR REPAIR-SURVEY SEQUENCE NR 160-W4-01 HAS DAMAGE TO PREVIOUS REPAIR GOUGED. REMOVED OLD REPAIR, FABRICATED AND INSTALLED NEW DOUBLER IAW A300-600F 57-50-00 PARA 4E FIG. 205.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO BAY) · airframe 5,649 hrs · 3,454 cycles

5YR MAIN CARGO COMPARTMENT RT FLOOR PANEL 242ZH HOLE DAMAGE, PREVIOUSLY REPAIRED IAW A300-MM, A300 MM NOT APPROVED FOR STRUCTURAL REPAIRS IAW EO A300-5320-16407-C. FABBED FLOOR PANEL IAW EO NRA300-5320-16407-C, APPX. B

Part: FLOORBOARD — MISREPAIRED (CABIN) · airframe 5,649 hrs · 3,454 cycles

INSPECTION TYPE:5YR MAIN CARGO COMPARTMENT FLOORBOARD 242SH DAMAGED, PREVIOUSLY REPAIRED IAW MM, REPAIRED IAW EO A300-5320-16407-C APPENDIX B. FABRICATED FLOOR PANEL 242SH IAW EO A300-5320-16407-C APPENDIX B

Part: FLOORBOARD — MISREPAIRED (CARGO BAY) · airframe 5,649 hrs · 3,454 cycles

INSPECTION TYPE-5YR, AFT BULK CARGO PIT HAS ONE PUNCTURE ON THE FLOOR PANEL 161GF, PREVIOUSLY REPAIRED IAW AMM, NOT APPROVED FOR STRUCTURAL REPAIRS, REPAIR IAW EO A300-5320-16407-C APP D. FABRICATED FLOOR PANEL 161GF IAW EO A300-5320-16407-C APP D.

Part: STRUCTURE — CRACKED (THRUST REVERSER) · airframe 5,649 hrs · 3,454 cycles

INSPECTION TYPE:5 YR NR 2 ENG INBOARD T/R LWR AFT CLOSURE IS CRACKED AT LWR END. REMOVED, FABRICATED AND INSTALLED REPAIR ANGLES, AND FILLER IAW IPXA EO A300-7830-33879-A AND SAA EA 300-7830-A1839.

Part: FLOOR PANEL — DENTED (CARGO BAY) · airframe 5,649 hrs · 3,454 cycles

INSPECTION TYPE: 5YR BULK CARGO FLOOR PANEL 162HF HAS DENTS AND SEVERAL FIELD REPAIRS. FABRICATED FLOOR PANEL 162HF IAW EO A300-5320-16407-C APPENDIX D.

Part: FLOOR PANEL — DENTED (CARGO BAY) · airframe 5,649 hrs · 3,454 cycles

5YR BULK CARGO FLOOR PANEL 161HF HAS FIELD REPAIRS AND LARGE AREA DENTS. FABRICATED FLOORBOARD 161HF IAW EO A300-5320-16407-C, APPENDIX D.

Part: SKIN — GOUGED (FUSELAGE)

INSPECTION TYPE:N/A AFT CARGO DOOR CUTOUT, AFT EDGE HAS GOUGE OUT OF SRM LIMITS. BLENDED DAMAGE AND FOUND TO BE OUT OF LIMITS PER SRM 53-17-12 FIG 102. REPAIRED AS REQUIRED PER EO A300-5330-33063. C/W HFEC TO OPEN HOLE, NO CRACKS NOTED. REF A300-600-NTM 51-10-01. REPAIR IS PERMANENT.

Part: CONTROL BOX — FAILED (SMOKE DETECTION)

INSPECTION TYPE:N/A ATB - CLIMB APPROX PAST 4000FT ECAM MASTER CAUTION CARGO LOOP 1 FAULT INDICATED. INDICATION WENT AWAY BEFORE CKLIST ACCOMPLISHED, APPROX 5 SECS LATER ECAM MASTER WARNING INDICATED SMOKE. CREW DONNED O2 MASK & GOGGLES PER CKLIST; INDICATION WENT AWAY. FOLLOWED BY CARGO LOOP FAULT INDICATION. ACCOMPLISHED BITE TEST OF SMOKE DET CNTRL BOX-50WU2-R&R ON LOG PG 042140 DUE TO FAILED TEST. ACCOMPLISHED ADJ/TEST ON MAIN SMOKE DET SYSTEM PER MM 26-19-00-05. NO DEFECTS NOTED. SUSPECT SNOW ON CANS AND DE-ICING FLUID.

Part: LIGHT — INOPERATIVE (CREW DOOR)

INSPECTION TYPE:N/A LAMP INOP IN CREW DOOR EMERGENCY EXIT LIGHT SIGN. RELAMPED, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A LAMP INOP IN GLARESHIELD EMERGENCY LIGHT. RELAMPED EMERGENCY, OPS CHECK GOOD.

Part: SWITCH — INOPERATIVE (COCKPIT)

EMERGENCY LIGHTS WILL NOT SHUTOFF IN "SHUT OFF" POSITION. REMOVED AND REPLACED EMERGENCY LIGHT TOGGLE S/W E0062 PER CH 20. OPS CKS OK.

Part: JACKSCREW — OVERTORQUED (L/E SLAT)

SLATS WOULD NOT DEPLOY FOR LANDING. CHECKLIST PROCEDURES DID NOT RESOLVE THE PROBLEM. CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. FOUND RT INBOARD SLAT SCREWJACK OVERTORQUED. REMOVED AND REPLACED INBOARD SLAT SCREWJACK IAW MM 27-84-22-04. L/E AND T/E FLAPS SYSTEMS CHECKS GOOD, REF MM 27-54-00-5 AND 27-51-00-5.

Part: GASKET — FAILED (HYDRAULIC SYSTEM)

EMERGENCY DECLARED INTO SJU DUE TO GREEN HYDRAULIC SYSTEM FAILURE. A/C LANDED SAFELY AND WAS TOWED TO RAMP. FOUND PRESSURE SW GASKET BROKEN AT GREEN MANIFOLD HP REPLACED AS REQD PER AMM 29-00-00- AND 31-53-03. REMOVED AND REPLACED BOTH GREEN ENGINE DRIVEN PUMPS IAW AMM 29-11-32-04 AND REPLACED BOTH ENGINE CASE ELEMENT FILTERS AS A PRECAUTION. ACCOMPLISHED LEAK CHECK AND OPS CHECK.

Part: LIGHT — INOPERATIVE (LAVATORY)

LAV LIGHT INOP. RELAMPED WITH A SERVICEABLE LAMP IAW A300-600 AMM 33-51-21-4.

Part: SLIDE — MALFUNCTIONED (COCKPIT)

CABIN DOOR OPENED FROM OUTSIDE WITH SLIDE ARMED. SLIDE DISARMED AND PIN INSTALLED. A/C OK FOR SERVICE AT THIS TIME.

Part: LIGHT — INOPERATIVE (LAVATORY)

LAV EMERG EXIT LIGHT INOP. RELAMPED.

Part: ENGINE — CRACKED (NR 1)

NR 1 ENGINE INLET SKIN CRACKS. R&R LT ENGINE NOSE COWL IAW A300 MM THRU STEP 3B (10). INSTALLED LT NOSE COWL LEAK CHECK GOOD REF MM. THIS CLEARS D296652 INSPECTION.

Part: LIGHT — INOPERATIVE (MAIN ENTRY)

MAIN ENTRY DOOR SLIDE LT CENTER LIGHT SEGMENT OUT. RELAMPED CK GOOD, 52-73-11-4.