N127UP

Part: SLIDE — RUPTURED (ZONE 800) · airframe 27,870 hrs · 17,211 cycles

WHILE WORKING D/D MEL-L1 DOOR SLIDE, FOUND DOOR DAMPER PRESS LOW, AND DIAPHRAGM RUPTURED. VERIFIED ALL LOCKOUT PINS REMOVED FROM DOOR DAMPNER AND ALL OPS CHECKS GOOD IAW AMM 52-10-14

Part: ARMING LEVER — FAULTED (ZONE 800) · airframe 27,854 hrs · 17,202 cycles

UNABLE TO ARM DOOR. DMP C/W.

Part: SLIDE — NO DISCREPANCY (ZONE 800) · airframe 27,781 hrs · 17,161 cycles

UNABLE TO ARM SLIDE AFTER CLOSING DOOR ADJUSTED GIRT BAR ASSEMBLY REF AMM 25-61-21. DOOR OPERATES CORRECTLY AT THIS TIME. DEFERRAL CLEARED PLACARDS REMOVED.

Part: FITTING — DIRTY (GIRT BAR) · airframe 27,645 hrs · 17,072 cycles

PILOT REPORTS L1 DOOR SLIDE WOULD NOT ARM AT DEPARTURE. INSPECTED DOOR, CLEANED GIRT BAR FLOOR ATTACHMENT POINTS, OPS CHECK GOOD W/ SLIDE INDICATION ON ECAM. AMM 52-10-11

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 27,244 hrs · 16,852 cycles

L1 DOOR SLIDE LOW PRESSURE. REVERSED DMP 52-11-01-2-3, REPLACED DOOR SLIDE ASSEMBLY IAW AMM 25-61-21-401 DEFERRAL CLEARED PLACARD REMOVED. ACCOMPLISHED RII STEPS PER GMM 04-02.

Part: RIB — CRACKED (LT TE FLAP) · airframe 26,863 hrs · 16,649 cycles

LH CENTER FLAP CRACK RIB 25 ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-90495-REQ1 AND VT-MAE EA 300-5750-27-A3607, REV. -. REVIEWED

Part: RIB — CRACKED (LT TE FLAP) · airframe 26,863 hrs · 16,649 cycles

LEFTCENTER FLAP CRACKED RIB 25.

Part: FITTING — CRACKED (ZONE 800) · airframe 26,863 hrs · 16,649 cycles

*SUPPLEMENTAL SDR* FAULT: FWD CREW DOOR AFT LOWER FITTING HAS A CRACK REMOVED AND REPLACED LOWER FITTING CRACK FWD CREW DOOR IAW AMM 52-10-31/401 P/N A5211038420401 BATCH 0004293554. REVIEWED

Part: STOP FITTING — CRACKED (FWD CREW DOOR) · airframe 26,863 hrs · 16,649 cycles

FWD CREW DOOR AFT LOWER FITTING STOP CRACKED. OPEN

Part: BULKHEAD — DAMAGED (APU BAY) · airframe 26,863 hrs · 16,649 cycles

8 HOLES ON REAR PRESSURE BULKHEAD APU BLEED AIR CUT OUT HAVE DAMAGE. CLEANED 3 EA HOLES IAW SRM 51-40-44 ON APU BLEED AIR CUT OUT. ROTO PERFORMED ON 1 HOLE AT BOTTOM OF THE APU BLEED AIR CUTOUT. NO INDICATIONS FOUND. IAW NTM 51-10-01.

Part: FRAME — CRACKED (FRM 40) · airframe 26,863 hrs · 16,649 cycles

DAMAGE FOUND IN TOP HOLE, & CRACK FOUND IN MIDDLE HOLE ON FR40 LH UPPER TENSION BOLTS. CLEANED HOLES TOP HOLE AND MIDDLE HOLE ON FR 40 UPPER TENSION BOLT LH SIDE I.A.W. A300-600 SRM 51-73-10.

Part: FRAME — DAMAGED (ZONE 200) · airframe 26,863 hrs · 16,649 cycles

DAMAGE FOUND IN HOLES (A, B, C, D, E, F, P) ON FR47 RH HORIZONTAL JUNCTION. AREAS MARKED IN RED. ACCOMPLISHED THE REPAIR PER UPS EO: EO-90872-REQ1 AND VT MAE FINAL EA 300-5710-27-A3621 REV. -.

Part: RIB — CRACKED (TE FLAP) · airframe 26,863 hrs · 16,649 cycles

THE R/H CENTER FLAP ASSY, HAS A CRACK (1EA) AT RIB LOCATION 26, AFT SIDE. INSTALLED DOUBLER. IAW A300-600 SRM 51-40-21 AND SRM 57-50-00 REVIEWED

Part: STRUCTURE — CRACKED (LT TE FLAP) · airframe 26,863 hrs · 16,649 cycles

THE L/H CENTER FLAP ASSY, HAS MULTIPLE CRACKS (2EA) AT RIB LOCATION 27, AFT SIDE. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-90495-REQ1 AND VT-MAE EA 300-5750-27-A3607, REV. -. JOB COMPLETE. VERIFIED. REVIEWED

Part: RIB — CRACKED (LT WING FLAP) · airframe 26,863 hrs · 16,649 cycles

THE L/H CENTER FLAP ASSY, HAS A CRACK (1EA) AT RIB LOCATION 26, AFT SIDE. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-90495-REQ1 AND VT-MAE EA 300-5750-27-A3607, REV. -. JOB COMPLETE. VERIFIED. REVIEWED

Part: RIB — CRACKED (LT WING FLAP) · airframe 26,863 hrs · 16,649 cycles

THE L/H CENTER FLAP ASSY, HAS A CRACK (1EA) AT RIB LOCATION 25, AFT SIDE. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-90495-REQ1 AND VT-MAE EA 300-5750-27-A3607, REV. -.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 26,863 hrs · 16,649 cycles

MDC DOOR AFT MIDDLE FUSELAGE SKIN WITH DAMAGE REMOVED NEGLIGIBLE SURFACE DISCREPANCY BY HAND WITH SCOTCH BRITE THAT WAS NOTED IN PAINT SURFACE ONLY IAW SRM 51-73-11 AND NO MATERIAL LOSS WAS NOTED. OK TO TREAT AND PRIME. RESTORED SURFACE PROTECTION IAW SRM 51-21-10 AND SRM 51-75-10. (P/N ALODINE1132, BATCH: 0004297395 PRIMER P/N 10P4-2NF, BATCH: 8473347012, PAINT P/N G6-W2-G2, BATCH: 4159202, PAINT CUP# 02-012-176). REVIEWED

Part: HINGE — DAMAGED · airframe 26,863 hrs · 16,649 cycles

DAMAGE FOUND IN HOLES ON MIDDLE HINGE. STEEL (14D) ALUMINIUM (12F, 13F, 15F). CLEANED HOLE (14D AND 15F) IAW SRM 51-73-10 AND REAMING HOLES (12F AND 13F) SIZE .281 IAW SRM 51-40-21. ROTO INSPECTION PERFORMED IAW NTM 51-10-01 PT 6. ALL HOLES ARE DEFECT FREE.

Part: HINGE — DAMAGED (NOT REPORTED) · airframe 26,863 hrs · 16,649 cycles

DAMAGE FOUND IN HOLES ON MIDDLE HINGE. STEEL (14D) ALUMINIUM (12F, 13F, 15F). OPEN

Part: WEB — CRACKED (FR 86-87) · airframe 26,863 hrs · 16,649 cycles

AGING ACFT INSP.- FRAME WEB BETWEEN FRAME 86L AND 87L IN AFT ACCESORY COMPT. ARE BENT AND CRACKED. DOT AA025. INSTALLED FRAME WEB BETWEEN FRAME 86 & 87 LH STGR 34 IAW SRM 51-40-21 P/N:CR3213-5-02, BTCH:0004070310. APPLIED CIC AT FRAME WEB BETWEEN FR 86 & 87 LH STGR34 IAW EO:M-5100-2780-L.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 26,863 hrs · 16,649 cycles

FAULT STR FUSELAGE RH SIDE BETWEEN (Y= -450 TO Y= -953 FR 51 CROOSBEAM BROKEN DOT 108-119. VERIFIED CROSSBEAM REPLACEMENT AND INSTALLATION PER IAW A300-600 SRM 51-40-21. REVIEWED

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 26,863 hrs · 16,649 cycles

FAULT STR FUSELAGE RH SIDE BETWEEN (Y= -450 TO Y= -953) FR 50 CROOSBEAM CROKED DOT 108-120. INSTALLED NEW CROSSBEAN IAW SRM 51-40-21 AND APPLIED CIC IAW EO NO:M-5100-2780-L. REVIEWED

Part: SPLICE — CRACKED · airframe 26,863 hrs · 16,649 cycles

DAMAGE FOUND IN HOLES (A, E, L, M, AND N) CRACK/DAMAGE FOUND IN HOLE (H) ON FR47 LH SPLICE FITTING. AREAS MARKED IN RED. ACCOMPLISHED THE REPAIR PER EO-90930-REQ1 AND EA 300-5315-27-A3616 REV. -. JOB COMPLETE. REVIEWED

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 26,863 hrs · 16,649 cycles

L/H WING ACCESS PANEL 577DT HAS A COMPOSITE CRACK ON THE INNER SIDE. DOT 110/01. REPAIRED CRACKED AREA IAW AMM A300 53-15-63/801 PARA C.2.A-F. 08-010 (EA 934) BATCH 4271892.

Part: STRUCTURE — CRACKED (FR 40) · airframe 26,863 hrs · 16,649 cycles

CRACKS/DAMAGE FOUND IN ALL 3 HOLES ON FR40 RH UPPER TENSION BOLTS. TOP HOLE (3 SMALL CRACKS IN 1ST LAYER) MIDDLE HOLE (PITTED CORROSION AT START OF HOLE) BOTTOM HOLE (CRACK AT START OF HOLE). ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-90914-REQ1 AND VT-MAE EA 300-5710-27-A3619, REV. -. JOB COMPLETE. REVIEWED

Part: FLOOR SUPPORT — CRACKED (FRM 54) · airframe 26,863 hrs · 16,649 cycles

AFT CARGO FLOOR SUPPORT R/H MIDDLE AT FR 54 IS CRACKED. APPLIED TOP COAT ON FLOOR SUPPORT I.A.W. SRM 51-75-10, AND INSTALLED FLOOR SUPPORT I.A.W. SRM 51-40-20. REVIEWED

Part: FLOOR SUPPORT — CRACKED (FRM 54 CARGO) · airframe 26,863 hrs · 16,649 cycles

AFT CARGO FR 54 L/H O/B HAS A CRACKED FLOOR SUPPORT BRACKET. INSTALLED FLOOR SUPPORT FR 54/LH IAW 51-40-21 A300-600. REVIEWED

Part: SEAL — TORN (ZONE 800) · airframe 26,863 hrs · 16,649 cycles

CREW ENTRY DOOR SEAL AFT MIDDLE AREA HAS TORN COVERING IN SEVERAL PLACES DOT47-03 REMOVED AND REPLACED MAIN ENTRY DOOR SEAL IAW AMM 52-10-18/401 T95749. P/N F521813562000. BATCH 0004290380. REVIEWED

Part: SEAL — TORN (CREW DOOR) · airframe 26,863 hrs · 16,649 cycles

**SDR FILED OPEN**FAULT CREW ENTRY DOOR SEAL AFT MIDDLE AREA HAS TORN COVERING IN SEVERAL PLACES DOT47-03

Part: NOSE COWL — CRACKED (NR 2 ENGINE) · airframe 26,863 hrs · 16,649 cycles

ENGINE #2 NOSE COWL FRON SIDE, LIP WITH CRACK IN POSITION 10 HRS, APROX 0,5 INCH DOT 108-110. INSTALLED DOUBLER AND FILLER ON AREA OF #2 NOSE COWL FRONT SIDE, I.A.W. PWA SRM 54-10-00, FIGURE 204.

Part: BULKHEAD — CORRODED (ZONE 100) · airframe 26,863 hrs · 16,649 cycles

FAULT FWD CARGO COMPT AFT BULKHEAD FR39 UPPER TOP AREAS HAS 3 AREAS OF EXFOLIATING CORROSION MARKED WITH RED TAPE DOT 47-01 ACCOMPLISHED PERMANENT REPAIR PER EO-90839-REQ1 AND EA 300-5315-27-A3601 REV. -. JOB COMPLETE. REVIEWED

Part: APU — INOPERATIVE (EMPENNAGE) · airframe 25,916 hrs · 16,095 cycles

INSPECTION TYPE:NA*DIVERSION* DURING CRUISE APU AUTO SHUTDOWN APU OIL QTY BELOW MIN INDICATED. DIVERT TO BIL DUE ENG 2 B SYSTEM IGN DIVERT 1205Z AND APU REQ PER MELFOUND LOOSE B NUT ON LINE FOM OIL PUMP OUTLET. TIGHTENED PER AMM 49-90-00. LINE NUT OPS CHECKED AND LEAK CHECK NORMAL. ACFT OK TO CONT SERVICE. SERVICED OIL TO FULL ON APU.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,291 hrs · 15,719 cycles

EMERGENCY "EXIT" SIGN HAS 3 EA LAMPS INOPRELAMPED & OPS NORMAL W/REF TO MM 33-51-00 PB 0501

Part: BRAKE ASSY — MALFUNCTIONED (MLG) · airframe 25,270 hrs · 15,701 cycles

BTB: 1250 PULSATING BRAKES AT VARIOUS TAXI SPEED. BRAKES HIGHER THAN NORMAL TEMPPILOTS NOTED BRAKES 5 AND 6 TEMP HIGH. INSPECTED BRAKES 5 AND 6. NO DISCREPANCIES NOTED WHEN JACKED AND OPS CHECKED FOIUND 040 FAULT ON BSCU. REMOVED AND REPLACED BSCU IAW A300 AMM 32-42-72. NO FAULTS NOTED AT THIS TIME.

Part: WARNING LIGHT — INOPERATIVE (CABIN) · airframe 25,053 hrs · 15,574 cycles

INSPECTION TYPE:NA*SUPPLEMENTAL SDR* EVACUATION SLIDE WARNING SYSTEM LIGHT INOP. DEFERRED WARNING LIGHT IAW MEL 52-73-01-1. PLACARD INSTALLED. NIL DMP. C/N M794640 ASSIGNED.R/R ASPSU OUTBD BATTERY & INBD BATTERY REF AMM 52-73-11 PB 0401. SYSTEM OPS NORMAL. THIS CLEARS M794640

Part: NONE — NONE (DOORS) · airframe 23,987 hrs · 14,957 cycles

INSPECTION TYPE:NACANNOT PREFLIGHT THE ESCAPE SLIDE, PRESSURE GAUGE IS NOT VISIBLE IN THE SLIDE PACK HOUSING WINDOW.R/R DOOR SLIDE PER MM 25-61-21-0401. THIS CLEARS M763622.

Part: NONE — NONE (CABIN) · airframe 23,920 hrs · 14,914 cycles

INSPECTION TYPE:NA** SUPPLEMENTAL SDR ** THE DOOR SLIDE DOES NOT SHOW ARMED ON ECAM WITH DOOR CLOSED AND SLIDE IN ARMED POSITION. DEFERED PER MEL 52-30-04, PLACARD INSTALLED.FOUND CONNECTOR 13WN-A UNPLUGGED. RECONNECTED PLUG OPS CHECK PER 52-73-00-0001 PARA8. PLACARD REMOVED THIS CLEARS M761761.

Part: FRAME — CRACKED (FR45 LH) · airframe 23,920 hrs · 14,914 cycles

INSPECTION TYPE:SEGFUSELAGE FRAME FOOTING AT LH SIDE FRAME 45, IS CRACKED AT AREA 1ACCOMPLISHED REPAIR PER APPENDIX J OF EO. A300-5310-46789-G

Part: FRAME — CRACKED (FR44 LH) · airframe 23,920 hrs · 14,914 cycles

INSPECTION TYPE:SEGFUSELAGE FRAME FOOT FITTING LH SIDE FRAME 44, IS CRACKED AT AREA 1.ACCOMPLISHED REPAIR PER APPENDIX J OF EO A300-5310-46789-G

Part: FRAME — CRACKED (FR46 RH) · airframe 23,920 hrs · 14,914 cycles

INSPECTION TYPE:SEGFUSELAGE FRAME FOOT FITTING AT LH SIDE FRAME 46 IS CRACKED AT AREA 1.ACCOMPLISHED REPAIR PER APPENDIX K OF EO. A600-5310-46789-G.

Part: TIRE — FAILED (MLG) · airframe 23,735 hrs · 14,796 cycles

DIVERSION, EMERG DECLARED, A/C LANDED WITHOUT INCIDENT*ON TAKE OFF, AT ROTATION THE AIRPLANE YAWED TO THE LEFT WITH AN AUDIBLE "BANG/POP". WE SUSPECTED A BLOWN TIRE AND FLEW GEAR DOWN TO PNS. ENGINE INDICATIONS WERE NORMAL.AFTER ARRIVAL INSPECTED LH&RH LANDING GEARS REF: A300 AMM 05-51-15. NO BLOWN NOR DAMAGED TIRES FOUND. PER TECH SUPPORT THE TELEMETRY REPORT SHOWED NO EVIDENCE OF A ENG STALL, ALL PERIMETERS WERE NORMAL ON #1&#2 ENG. FOUND EVIDENCE OF BIRD STRIKE ON #1 ENG AT 5 O'CLOCK INSPECTED REF: A300 AMM 05-51-1

Part: HANDLE — MISSING (DOOR ASSIST) · airframe 23,505 hrs · 14,652 cycles

ENTRY DOOR HANDLE UPPER PORTION MISSING. R & R DOOR ASSIST HANDLE, REF AMM 52-10-13-401.

Part: ARMING LEVER — BINDING (ESCAPE SLIDE) · airframe 22,621 hrs · 14,157 cycles

INSPECTION TYPE: NA ESCAPE SLIDE ARMING LEVER DIFFICULT TO MOVE IN EITHER DIRECTION. CLEANED AND LUBED GIRT BAR. CHECKED LEVER ARMING OK FOR SERVICE, PER AMM 05-61-20.

Part: SLIDE — BINDING (PAX DOOR) · airframe 22,581 hrs · 14,134 cycles

INSPECTION TYPE: N/A CREW ENTRY DOOR SLIDE DIFFICULT TO ARM RIGHT GREEN FLAG SLIGHTLY HIGH. LUBRICATED CREW ENTRY DOOR, IAW A300-600 MM 12-22-52 SLIDE ARM HANDLE. OPERATIONS CHECK NORMAL. GREEN FLAGS OPERATIONS CHECK NORMAL. NO FURTHER ACTION TAKEN AT THIS TIME.

Part: PLATE — BROKEN (RT WING TE FLAP) · airframe 21,976 hrs · 13,748 cycles

INSPECTION TYPE:SV, RIGHT WING INBD FLAP, INBD ROLLER PLATE WAS BROKEN IN TWO PLACES3 REMOVED AND REPLACED FLAP.

Part: BULKHEAD — CRACKED (NR INLET) · airframe 21,976 hrs · 13,748 cycles

NR 2 ENGINE INLET AFT BULKHEAD HAS CRACK ON RH SIDE. REPAIRED IAW PW SRM 54-10-00. REPAIR #14 PAG 201

Part: ADAPTER — CORRODED (CABIN) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:10YR MAIN CABIN FLOOR CLS ADAPTER HAS CORROSION AT FR 23 LT SIDE Y=0. ACCOMPLISHED BLEND OUT REPAIR ON MAIN CABIN FLOOR LT CLS ADAPTER AT FR 23 Y=0 PER EA# 300-5310-01-A7827 I/R AND EO 300-5310-73141-A.

Part: ADAPTER — CORRODED (CABIN) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:10YR MAIN CABIN FLOOR RT SIDE CLS ADAPTER HAS CORROSION AT FR 24 Y=0. ACCOMPLISHED BLEND OUT REPAIR ON MAIN CABIN FLOOR RT CLS ADAPTER AT FR 24 Y=0 PER EA# 300-5310-01-A7827 I/R AND EO A300-5310-73141-A.

Part: ADAPTER — CORRODED (CABIN) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:10YR MAIN CABIN CLS ADAPTER AT FR 23 RT SIDE HAS CORROSION. ACCOMPLISHED BLEND OUT REPAIR ON MAIN CABIN CLS ADAPTER AT FR 23 Y=0 PER EA#5310-01-A7827 I/R AND EO A300-5310-73141-A.

Part: SKIN — CORRODED (LT WINGLET) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:10YR LT WINGLET CORRODED AT CENTER STATIC WICK BASE. ACCOMPLISHED BLEND OUT REPAIR ON LT WINGLET SKIN AT CENTER STATIC WICK BASE PER EA# 300-5720-01-A7819 I/R AND EO A300-5720-73049-A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:10YR SUPERNUMARY AREA FLOORBEAM UNDER PANEL 221VF HAS CORROSION ON UPPER SURFACE. ACCOMPLISHED BLEND OUT REPAIR ON MAIN CABIN FLOOR SUPPORT AT FR 14 STA Y 953 PER EA# 300-5312-01-A7820 I/R AND EO A300-5310-73069-A.

Part: STIFFENER — CRACKED (KRUEGER FLAP) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12YR LT WING KRUEGER FLAP MOVABLE VANE COVE STIFFENER IS CRACKED. REMOVED AND REPLACED CRACKED LT WING KRUEGER FLAP MOVABLE VANE COVE STIFFENER IAW SRM 51-40-21. (MINOR)

Part: STRINGER — CRACKED (FUSELAGE) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12Y AFT FUSELAGE STR. #9 IS CRACKED BETWEEN FRAME 99 & 100. REPAIRED CRACKED STR #9 AND SKIN BETWEEN FRAME 99 & 100 IAW EA 300-5310-01-A7827 REV. I/R AND EO A300-5310-73176-A. (MAJOR)

Part: LUG — DAMAGED (THRUST REVERSER) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12YR #1 ENGINE O/B T/R UPPER TRACK LUG EXTERNAL SURFACE HAS A LARGE WEAR MARK ON UPPER SURFACE. REPAIRED DAMAGED #1 ENGINE O/B T/R UPPER LUG IAW EA 300-7830-01-A7828 REV. IR AND EO A300-7830-73162-A. (MAJOR)

Part: SKIN — CHAFED (NR 3 FAN COWL) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:3C#3 ENG OTBD FAN COWL FWD HINGE HAS CHAFFE DAMAGE.ACCOMPLISHED REPAIR ON #3 ENG RH OTBD FAN COWL FWD HINGE PER VT-SAA EA#011-7110-01-A7776 I/R AND UPS EO MD-11-7110-72653-A.

Part: BARRIER — CORRODED (MAIN CARGO BAY) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12Y MAIN CARGO COMPARTMENT L-RIGID CARGO BARRIER LONGITUDINAL WALL OUTBOARD SKIN SURFACE CORRODED AT Y1156. REMOVED CORROSION ON MAIN CARGO COMPARTMENT L-RIGID CARGO BARRIER LONGITUDINAL WALL OUTBOARD SKIN SURFACE IAW EA 300-5310-01-A7815 AND EO A300-5310-73132-A. (MINOR)

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 20,491 hrs · 12,893 cycles

FWD CARGO FLOOR PANEL 131DE WAS DAMAGED. FABRICATED AND REPLACED THE FLOOR PANEL IAW EO A300-5320-16407-E, APPX C. MAJOR.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 20,491 hrs · 12,893 cycles

MAIN CABIN FLOOR PANEL 231MJ HAS PUNCTURED SKIN.REMOVED, FABRICATED AND REPLACED THE FLOOR PANEL IAW EO A300-5320-16407, APPX B. MAJOR.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 20,491 hrs · 12,893 cycles

MAIN CABIN FLOOR PANEL 232KH LOWER SKIN WAS CRACKED. FABRICATED AND REPLACED THE FLOOR PANEL IAW EO A300-5320-40552-B, APPX B. MAJOR.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 20,491 hrs · 12,893 cycles

MAIN CABIN FLOOR PANEL 232FF WAS CRACKED AND DEBONDED. FABRICATED AND REPLACED THE FLOOR PANEL IAW EO A300-5320-40552-B, APPX B. MAJOR.

Part: BARRIER — CORRODED (MAIN CARGO BAY) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12YR MAIN CARGO COMPARTMENT L-RIGID BARRIER AFT WALL FORWARD AND AFT SKIN SURFACES ARE CORRODED BETWEEN Y1156 AND Y2462. REMOVED CORROSION ON MAIN CARGO COMPARTMENT L-RIGID CARGO BARRIER AFT WALL, FORWARD AND AFT SKIN SURFACES BETWEEN T1156 AND Y2462 IAW EA 300-5310-01-A7810 AND EO A300-5310-73134-A

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 20,491 hrs · 12,893 cycles

MAIN CABIN FLOOR PANEL 232AH WAS DAMAGED ON THE LOWER SKIN. FABRICATED AND REPLACED THE FLOOR PANEL IAW EO A300-5320-16407-E, APPX B. MAJOR.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 20,491 hrs · 12,893 cycles

MAIN CABIN FLOOR PANEL 231TG LOWER SKIN WAS PUNCTURED. FABRICATED AND REPLACED THE FLOOR PANEL IAW EO A300-5320-40552-B, APPX B. MAJOR.

Part: FLOOR PANEL — PUNCTURED (MAIN CABIN) · airframe 20,491 hrs · 12,893 cycles

MAIN CABIN FLOOR PANEL 222DG LOWER SKIN PUNCTURED. FABRICATED AND REPLACED THE FLOOR PANEL IAW EO A300-5320-40552-B, APPX B. MAJOR.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12YR MAIN CABIN FWD RCB AFT LOWER SURFACE HAS CORROSION IN 2 PLACES ALONG BOTTOM AT FR 15. RERPAIRED CORRODED MAIN CABIN FWD RCB AFT LOWER SURFACE AT FR 15, -Y954 & -Y1791 IAW EA 300-5310-01-A7809 REV. IR AND EO A300-5310-73133-A. (MINOR)

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 20,491 hrs · 12,893 cycles

MAIN CABIN FLOOR PANEL 231NG LOWER SKIN WAS CRACKED. FABRICATED AND REPLACED THE FLOOR PANEL IAW EO A300-5320-40552-B, APPX B. MAJOR.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 20,491 hrs · 12,893 cycles

MAIN CABIN FLOOR PANEL 231VG SKIN CRACKED. FABRICATED AND REPLACED THE FLOOR PANEL 231VG IAW EO A300-5320-16407-E, APPX. B. MAJOR.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 20,491 hrs · 12,893 cycles

MAIN CABIN FLOOR PANEL 231RH LOWER SKIN WAS CRACKED. FABRICATED AND REPLACED THE FLOOR PANEL IAW EO A300-5320-40552-B, APPX. B. MAJOR.

Part: ADAPTER — CORRODED (MAIN DECK) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12Y CLS ADAPTER CORRODED AT FR20, -Y1959REMOVED, FABRICATED AND REPLACED CLS ADAPTER WITH ALTERNATE MATERIAL IAW EA 300-5310-01-A7806 REV I/R AND EO A300-5310-72958-A. (MAJOR)

Part: ADAPTER — CORRODED (CABIN) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12YR MAIN CABIN CLS ADAPTER AT FR 24 LEFT OF C/L HAS CORROSION. REPAIRED CORRODED MAIN CABIN CLS ADAPTER AT FR 24 LEFT OF C/L IAW EA 300-5310-01-A7827 REV. IR AND EO A300-5310-73141-A. (MINOR)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12Y MAIN CABIN SEAT TRACK IS CORRODED BETWEEN FRAME 80/82 AND Y=-450. REPAIRED CORRODED SEAT TRACK BETWEEN FRAME 80/82 AND Y=-450 IAW SRM 53-10-06 PARA. 4 FIG. 201. (MAJOR)

Part: FITTING — BROKEN (CABIN) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12YR MAIN CABIN FLOOR FITTING HAS A BROKEN LUG AT FR 50, -Y2462. REMOVED, FABRICATED AND REPLACED BROKEN MAIN CABIN FLOOR STRUCTURE EQUIPMENT FITTING ASSEMBLY AT FR 50, -Y2462 USING ALTERNATE MATERIAL IAW EA 3005320-01-A7822 REV. IR AND EO A300-5320-73161-A. (MAJOR)

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 20,491 hrs · 12,893 cycles

MAIN CABIN FLOOR PANEL 252LG IS DAMAGED. FABRICATED AND REPLACED THE FLOOR PANEL IAW EO A300-5320-40552-B APPX. B. MAJOR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12Y MAIN CABIN SEAT TRACK IS CORRODED BETWEEN FRAME 80/82 AND Y=450. REPAIRED CORRODED SEAT TRACK BETWEEN FRAME 80/82 AND Y=450 IAW SRM 53-10-06 PARA. 4 FIG. 201. (MAJOR)

Part: SKIN PANEL — DENTED (RT HORIZ STAB) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12YR RT HORIZONTAL STAB L/E PANEL 341DB HAS 6 DENTS ON UPPER SURFACE. REPAIRED DENTED RT HORIZONTAL STAB L/E PANEL 341DB UPPER SURFACE IAW EA 300-5510-01-A7817 REV. IR AND EO A300-5510-73086-A. (MINOR)

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 20,491 hrs · 12,893 cycles

MAIN CARGO FLOOR PANEL 251CN LOWER SKIN WAS PUNCTURED. FABRICATED AND REPLACED THE FLOOR PANEL IAW EO A300-5320-40552-B, APPX B. MAJOR.

Part: WEDGE — CHAFED (TE FLAP) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12YR RT WING I/B FLAP I/B T/E WEDGE IS CHAFED. REPAIRED CHAFED RT WING I/B FLAP I/B T/E WEDGE IAW EA 300-5750-01-A7826 REV. I/R AND EO A300-5750-73173-A. (MAJOR)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12Y MAIN CABIN SEAT TRACK IS CORRODED BETWEEN FRAME 80/82 AND Y=0. REPAIRED CORRODED SEAT TRACK BETWEEN FRAME 80/82 AND Y=0 IAW SRM 53-10-06 PARA. 4 FIG. 201. (MAJOR)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12Y MAIN CABIN SEAT TRACK IS CORRODED BETWEEN FRAME 80/80 AND Y=-1137.1. REPAIRED CORRODED SEAT TRACK BETWEEN FRAME 80/80 AND Y=-1137.1 IAW SRM 53-10-16 PARA. 4 FIG. 201. (MAJOR)

Part: SKIN PANEL — DENTED (TE FLAP) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12Y LT WING T/E UPPER SKIN PANEL HAS 10 DENTS. REPAIRED LT WING T/E UPPER SKIN PANEL IAW EA 300-5750-01-A7813 REV. I/R AND EO A300-5750-72999-A. (MINOR)

Part: FLAP — DENTED (RT WING) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12YR RT O/B FLAP L/E IS DENTED APPROX. 30" I/B OF #4 FLAP TRACK. REPAIRED DENTED RT O/B FLAP L/E 5" I/B OF RIB 19 AND 7" O/B OF RIB 18 IAW SRM 57-50-00 PAR. 4.H, FIGURE 208. (MAJOR)

Part: SUPPORT RIB — DAMAGED (NR 1 PYLON) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12YR #1 PYLON L/H FRAME SUPPORT AT RIB 20 HAS ELONGATED HOLE AT LOWER CASE DRAIN LINE.REPAIRED DAMAGED #1 PYLON L/H FRAME SUPPORT RIB 20 ELONGATED HOLE IAW EA 300-5450-01-A7808 REV. IR AND EO A300-5450-73000-A. (MINOR)

Part: PLATE — CRACKED (RT WING) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12YR RT WING CRACK ON UPPER SURFACE REINFORCING PLATE IN WING ISLAND O/B OF THE AILERON INSIDE ACCESS PANEL. REMOVED, FABRICATED AND REPLACED CRACKED REINFORCING PLATE ON RT WING ISLAND O'B OF THE AILERON ACCESS PANEL IAW DWG A57242294 AND SRM 51-40-23.

Part: SKIN — CORRODED (LT WING) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12YR LT WING O/B T/E HAS CORROSION UNDER O/B STATIC WICK BASE. REPAIRED CORRODED LT WING O/B T/E AT O/B STATIC WICK BASE IAW EA 300-5730-1-A7823 REV. IR AND EO A300-5720-73168-A. (MINOR)

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 20,491 hrs · 12,893 cycles

FWD CARGO FLOOR PANEL 132DF HAS MULTIPLE PUNCTURES ON THE LOWER SURFACE. FABRICATED AND REPLACED THE FLOOR PANEL 132DF IAW EO A300-5320-16407-E APPX. C. MAJOR.

Part: WEB — CRACKED (FRAME 21) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12YRFWD CARGO UNDER FLOOR L/H INTERCOSTAL WEB IS CRACKED AT FR 21 BELOW O/B ROLLER TRAY.REMOVED AND REPLACED CRACKED FWD CARGO UNDER FLOOR L/H INTERCOSTAL WEB AT FR 21 BELOW O/B ROLLER TRAY IAW SRM 51-40-21.

Part: SKIN — CORRODED (LT WING) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12YR LT WING UPPER SKIN CORROSION AT RIB 9 AND STRINGER 13. BLENDED CORROSION ON LT WING UPPER SKIN AT RIB 9 AND STRINGER 13 IAW EA 300-5730-01-A7818 I/R AND EO A300-5730-73178-A.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12Y RT ELEVATOR UPPER SKIN HAS 11 DENTS. REPAIRED RT ELEVATOR UPPER SKIN DENTS IAW EO A300-5500-43343-B. (MINOR)

Part: DOUBLER — DENTED (FUSELAGE) · airframe 20,491 hrs · 12,893 cycles

INSPECTION TYPE:12Y AFT FUSELAGE SKIN, DENT/BLEND ON REPAIR DOUBLER BETWEEN FRAME 84 & 86 AND STR. 43R.REPAIRED SAID AREA IAW EA 300-5319-01-A7811 REV. I/R AND EO A300-5330-73062-A. (MINOR)

Part: HANDLE — BROKEN (ENTRY DOOR) · airframe 20,175 hrs · 12,707 cycles

INSPECTION TYPE:N/A CREW ENTRY DOOR INTERIOR DOOR HANDLE BROKEN. REPLACED TOP SECTION OF DOOR INTERIOR ASSIST HANDLE AS REQ PER MM 52-10-13-0401.

Part: FLOOR PANEL — DAMAGED · airframe 19,977 hrs · 12,585 cycles

INSPECTION TYPE:N/A FLOOR PANEL 231KJ DAMAGED. FABRICATED FLOORBOARD IAW SREO A300-5320-40552-B AND DWG13-B53270727.

Part: COVER — DAMAGED (CREW ENTRY) · airframe 19,833 hrs · 12,508 cycles

CREW ENTRY DOOR INSIDE HANDLE MISSING A PIECE. INSTALLED A NEW COVER IAW MM 52-10-00.

Part: DUCT — DAMAGED (CARGO BAY) · airframe 19,170 hrs · 12,111 cycles

BULK CARGO VENTILATION TUBE ASSY (ELBOW) DAMAGED (CRACKED). LOCATED NEAR AFT OUTFLOW VALVE. VENTILATION TUBE P/N A2128091900200, REMOVED FOR EVALUATION. PVM0558935 05/16/18. C/W EO A300-2120-68535-A. NO OTHER DEFECTS NOTED. OK FOR SERVICE. REPLACED BULK CARGO COMPARTMENT VENTILATION DUCT PER EO A300-2120-68535-A & DRM PAGE701. OK FOR SERVICE.

Part: SEAL — LEAKING (PAX DOOR) · airframe 18,778 hrs · 11,901 cycles

DOOR SEAL LEAKING. R & R THE DOOR SEAL IAW AMM 52-10-18-0401.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 18,692 hrs · 11,852 cycles

WALL MOUNTED EMERGENCY LIGHT, FWD OF THE LAVATORY DOOR MISSING THE LENS. INSTALLED A NEW LENS IAW MM 33-51-17-0401.

Part: CONNECTOR — NOT SEATED (DOOR SLIDE) · airframe 17,890 hrs · 11,353 cycles

SLIDE WARNING LIGHT INOPERATIVE. RESEATED THE CONNECTOR ON ASPSU. OPS GOOD IAW AMM 52-73-00-0501.

Part: CONTROL BOX — LEAKING (L1 DOOR) · airframe 17,465 hrs · 11,067 cycles

CABIN ENTRY DOOR HAS A SQUEAL FROM LOWER LEFT CORNER WHEN PRESSURIZED. PRESSURIZED TO 3 PSI, SQUEAL STARTED AND WAS TRACED TO ENTRY DOOR HANDLE AT AFT HINGE POINT ON EXTERIOR HANDLE. R & R THE DOOR CONTROL BOX. PRESSURIZED ACFT NO LEAKS NOTED.

Part: GUIDE — OUT OF ADJUST (L1 DOOR) · airframe 17,463 hrs · 11,065 cycles

A LOUD WHISTLING NOISE COMING FROM CABIN ENTRY DOOR AREA DURING PRESSURIZED FLT. ADJUSTED ALL 4 DOOR GUIDE FITTINGS. PRESSURIZED ACFT. NO LEAKS NOTED IAW MM 52-10-11-0501, AND MM 05-53-00-0001.

Part: SKIN — PUNCTURED (LT WING TE FLAP) · airframe 17,189 hrs · 10,920 cycles

INSPECTION TYPE: C1, LT INBD FLAP LOWER SURFACE TRACK IS PUNCTURED, FOUND TO BE OUT OF SRM LIMITS. TRIMMED OUT DAMAGE AND INSTALLED AN EXTERNAL DOUBLER IAW EO A300-5750-62373-A.

Part: SWITCH — MALFUNCTIONED (CABIN) · airframe 17,047 hrs · 10,830 cycles

EMERGENCY EXIT LIGHTS WILL NOT DISARM, CYCLED EMERGENCY LIGHT SWITCH ON AND OFF VARIOUS TIMES. LIGHT DOES DISARM WHEN SWITCH IS OFF. OPS CHECK GOOD.

Part: FITTING — OUT OF ADJUST (GIRT BAR) · airframe 16,472 hrs · 10,425 cycles

UNABLE TO MOVE SLIDE, DISARM HANDLE ON CREW DOOR FULLY TO THE LEFT. PIN WILL NOT INSERT. ADJUSTED GIRT BAR FITTINGS IAW MM 52-10-11-05. INSTALLED DUAL ESCAPE SLIDE IAW AMM 25-61-21-04.

Part: DOUBLER — DAMAGED (FRAME 85) · airframe 16,161 hrs · 10,241 cycles

DAMAGE TO FUSELAGE SKIN DOUBLER LOCATED AT FR 85 BETWEEN S44L TO S44R, REF EO A300-5330-58946A FOR DETAILS REPLACED SKIN DOUBLER IAW EO A300-5330-58946A.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 15,865 hrs · 10,025 cycles

INSPECTION TYPE:5YR, RT WING INBD FLAP LOWER SURFACE APPROXIMATELY, RIB 15 IS DENTED & GOUGED, REPAIRED IAW EO.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 15,865 hrs · 10,025 cycles

INSPECTION TYPE:5YR, LT ENGINE INBD FLAP LOWER SURFACE APPROXIMATELY, RIB 14-14A IS DENTED AND GOUGED, REPAIRED IAW EO.

Part: FITTING — CRACKED (FRAME 61) · airframe 15,865 hrs · 10,025 cycles

INSPECTION TYPE:5YR, AFT CARGO DOOR FORK FITTING AT 61A CRACKED. R & R IAW SREO A300-5230-57988-A.

Part: FITTING — CRACKED (FRAME 61) · airframe 15,865 hrs · 10,025 cycles

INSPECTION TYPE: 5YR, AFT CARGO DOOR FORK FITTING AT FRAME 61 CRACKED. R & R IAW SREO A300-5230-57988-A.

Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 15,865 hrs · 10,025 cycles

INSPECTION TYPE: 5YR, AFT CABIN UNDERFLOOR CROSSBEAM LT FRAME 79 +Y1580 HAS A 2.25 INCH CRACK. REPAIRED IAW EO A300-5310-58004-A.

Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 15,865 hrs · 10,025 cycles

INSPECTION TYPE: 5YR, AFT CABIN UNDERFLOOR, RT FRAME 79 -Y1580 HAS A CRACK. REPAIRED IAW EO A300-5310-58004-A.

Part: DAMPENER — INOPERATIVE (LANDING GEAR) · airframe 15,694 hrs · 9,920 cycles

LANDING GEAR RETRACT FAULT. ECAM. LEVER WOULD NOT GO PAST NEUTRAL IN POSITION 1 OR 2. R & R OF LT AND RT PITCH DAMPERS JACKED ACFT IAW AMM 07-11-00-0001. PERFORMED LANDING GEAR RETRACTION AND EXTENSION IN BOTH POS 1 AND 2. SYS OPS CK NORMAL. OK FOR CONTINUED SERVICE.

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 15,550 hrs · 9,813 cycles

CREW ENTRY DOOR WILL NOT OPEN. FOUND LOWER END OF COMPENSATOR MECHANISM LOOSE, ATTACHED MECHANISM, FOUND DOOR OUT OF ADJUSTMENT. ADJUSTED LOCKING DOOR MECHANISM IN HIGH POSITION IAW MM 52-10-20 PARA 3.3, 4. CLEANED AND LUBED MECHANISM. INSTALLED LINERS AND SECURED.

Part: FITTING — CRACKED (CENTER FUSELAGE) · airframe 14,914 hrs · 9,400 cycles

1C INSPECTION, AIR CONDITIONING BAY RT BASE FRAME FITTING IS CRACKED AT FRAME 45. R & R FITTING IAW EO A300-5310-46789-A, APPENDIX G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 14,914 hrs · 9,400 cycles

3C INSPECTION, BULK CARGO FLOOR PANEL 161JF IS BENT AND TORN. FABRICATED NEW FLOOR PANEL IAW EO A300-5320-16407-E.

Part: GIRT BAR — STUCK (PAX SLIDE)

COULD NOT DISARM SLIDE ON ARRIVAL. FOUND FWD END OF GIRT BAR NOT INSTALLED INTO SLIDER. REINSERTED SLIDER ARMS & DISARMS NORMALLY IAW AMM 25-61-21-04.

Part: GIRT BAR — MALFUNCTIONED (DOOR SLIDE)

SLIDE APPEARED TO DISARM BUT HANDLE WOULD NOT MOVE ENOUGH TO INSTALL PIN. INSERTED GIRT BAR SLIDER IAW AMM 25-61-21-04-01. OPS CHECKED DOOR SLIDE ARM LEVER MULTIPLE TIMES. OPS CHECKED NORMAL.

Part: SLIDE — DISLODGED (L1 DOOR)

MAIN CABIN DOOR ESCAPE SLIDE FELL OUT OF IT`S COVER. R & R MAIN ENTRY DOOR SLIDE PACK IAW AMM 25-61-21-0401, 25-61-20-0601 & 52-10-00-0301.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

DURING MX INSPECTION; LAVATORY EMERGENCY LIGHT BULB WAS FOUND TO BE INOPERATIVE. REPLACED BULB IAW AMM 33-51-21-401. OPS CHECKED GOOD.

Part: FLOOR PANEL — DELAMINATED · airframe 13,037 hrs · 8,160 cycles

FLOOR PANEL 231QH DELAMINATED & TORN. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 13,037 hrs · 8,160 cycles

INSPECTION TYPE:SV, MAIN CABIN FLOORBOARD 231SG HAS UPPER SKIN PUNCTURED AND WORN THRU. FABRICATED MAIN CABIN FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK CARGO) · airframe 13,037 hrs · 8,160 cycles

MAIN DECK CARGO FLOOR PANEL 231VG DELAMINATED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 13,037 hrs · 8,160 cycles

INSPECTION TYPE:SV, MAIN CABIN FLOORBOARD 231TG UPPER SKIN DETERIORATED. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B APPENDIX B.

Part: FLOOR PANEL — PUNCTURED · airframe 13,037 hrs · 8,160 cycles

FLOOR PANEL 232SG PUNCTURED. REPAIRED FLOOR PANEL EO A300-5320-42721-B, PARA 6A.

Part: FLOOR PANEL — PUNCTURED · airframe 13,037 hrs · 8,160 cycles

FLOOR PANEL 231LG PUNCTURED & TORN. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 13,037 hrs · 8,160 cycles

MAIN CABIN FLOORBOARD 231PJ HAS UPPER AND LOWER SKIN DELAMINATED. FABRICATED MAIN CABIN FLOORBOARD IAW EO A300-5320-40552-B.

Part: FLOOR PANEL — CRACKED (MAIN DECK CARGO) · airframe 13,037 hrs · 8,160 cycles

MAIN DECK CARGO FLOOR PANEL 231NJ CRACKED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOOR PANEL — PUNCTURED · airframe 13,037 hrs · 8,160 cycles

FLOOR PANEL 231KJ PUNCTURED & DELAMINATED. FABRICATED NEW FLOOR PANEL IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOOR PANEL — CRACKED (MAIN DECK CARGO) · airframe 13,037 hrs · 8,160 cycles

MAIN DECK CARGO FLOOR PANEL 222DG CRACKED AND HAS CORRODED INSERTS. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOOR PANEL — PUNCTURED · airframe 13,037 hrs · 8,160 cycles

FLOOR PANEL 231LJ PUNCTURED & CRACKED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOOR PANEL — PUNCTURED · airframe 13,037 hrs · 8,160 cycles

FLOOR PANEL 231PH PUNCTURED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOOR PANEL — PUNCTURED (MAIN CARGO) · airframe 13,037 hrs · 8,160 cycles

MAIN DECK CARGO FLOOR PANEL 232JF PUNCTURED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 12,275 hrs · 7,677 cycles

INSPECTION TYPE:1C, RT FUSELAGE SKIN 14.4" BELOW COCKPIT WINDOW AT FR7 DAMAGED. REPAIRED DAMAGE IAW SRM 53-11-12, FIG 202, PARA 5B.

Part: WARNING LIGHT — INOPERATIVE (COCKPIT)

EVACUATION SLIDE RELEASE WARNING SYSTEM LIGHT DOES NOT ILLUMINATE. DEFERRED PER MEL 52-73-01-1. ASSIGNED M461499. INSPECTED AND REPLACED INDICATION LIGHT. CHECKED OK IAW 52-73-11-06.

Part: SKIN — DAMAGED (FUSELAGE)

FUSE SKIN DOUBLER AND SKIN DAMAGED AT FRAME 85. REPAIRED IAW EO A300-5330-43693-B.

Part: POWER SUPPLY — UNSERVICEABLE (COCKPIT)

EMERGENCY LIGHTS REMAIN ON WHEN POWER IS REMOVED FROM ACFT. R & R POWER SUPPLY UNIT IAW AMM 33-51-14-04.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY)

DAMAGED BULK PIT FLOOR PANEL. REPAIRED IAW SRM 53-10-20, FIG 207.

Part: WINDOW — CRACKED (COCKPIT)

GOT RT WINDOW HT FAULT ON CLIMB OUT. COMPLIED WITH CHECKLIST. WINDOW WAS ARCING AND CRACKED. REMOVED RT WINDOW IAW MM 56-11-11-04 FROM STEPS 1A, THROUGH 8 B. REINSTALLED RT FRONT WINDOW MM 56-11-11-04.

Part: LIGHT — INOPERATIVE (CABIN)

INSP TYPE: ASN COURIER/SUPER NUMERARY AREA EMERGENCY LIGHT TEST FUNCTION INOP. C/W DMP + DEFERRED 33-51-05-2.

Part: LIGHT — INOPERATIVE (CABIN)

ASN COURIER/SUPER NUMERARY AREA EMERGENCY LIGHT TEST FUNCTION INOP M432421. RELAMPED DOOR EXIT SIGN WITH REF TO AMM 33-51-13-04. OPS TESTED, TEST FUNCTION IAW AMM 33-51-00-05. OPS CKS GOOD. STICKER REMOVED M-432421 CLEARED.

Part: FLOORBOARD — CRACKED (MAIN CARGO BAY) · airframe 10,955 hrs · 6,832 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 241LT CRACKED. REPAIRED MAIN CABIN FLOORBOARD 241LT IAW EO A300-5320-38221-B.

Part: FLOORBOARD — PUNCTURED (MAIN CARGO BAY) · airframe 10,955 hrs · 6,832 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 251AN HAS A PUNCTURE. REPAIRED MAIN CABIN FLOORBOARD 251AN IAW EO A300-5320-38221-B.

Part: FLOOR PANEL — CRACKED (MAIN CARGO BAY) · airframe 10,955 hrs · 6,832 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 251BN HAS A CRACK. REPAIRED MAIN CABIN FLOORBOARD 251BN IAW EO A300-5320-38221-B.

Part: FLOOR PANEL — PUNCTURED (MAIN CARGO BAY) · airframe 10,955 hrs · 6,832 cycles

INSPECTION TYPE:10YR, MAIN DECK CARGO COMPT FLOOR PANEL 242TN IS PUNCTURED. REPAIRED MAIN DECK FLOOR PANEL 242TN IAW EO A300-5320-38221-B.

Part: FLOOR PANEL — CRACKED (MAIN CARGO BAY) · airframe 10,955 hrs · 6,832 cycles

INSPECTION TYPE:10YR, MAIN DECK CARGO COMPT FLOOR PANEL 241BQ IS CRACKED. REPAIRED MAIN DECK FLOOR PANEL 241BQ IAW EO A300-5320-38221-B.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO BAY) · airframe 10,955 hrs · 6,832 cycles

INSPECTION TYPE:10YR, RUSTED INSERTS/BROKEN OFF SCREW ON MAIN CABIN FLOOR PANEL 222BG. REPAIRED MAIN CABIN FLOOR PANEL 222BG IAW EO A300-5320-38221-B.

Part: FLOOR PANEL — PUNCTURED (MAIN CARGO BAY) · airframe 10,955 hrs · 6,832 cycles

INSPECTION TYPE:10YR, FLOORBOARD 252DF IN MAIN CABIN HAS A PUNCTURE. REPAIRED MAIN CABIN FLOORBOARD 252DF IAW EO A300-5320-38221-B.

Part: FLOORBOARD — DEBONDED (MAIN CARGO BAY) · airframe 10,955 hrs · 6,832 cycles

INSPECTION TYPE:10YR, FLOORBOARD NR 242LJ IS DISBONDED AT FWD END AT MAIN DECK CARGO FLOOR. ACCOMPLISHED REPAIR ON MAIN DECK FLOORBOARD NR 242LJ IAW EO A300-5320-38221-B.

Part: FLOORBOARD — PUNCTURED (MAIN CARGO BAY) · airframe 10,955 hrs · 6,832 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 252RG HAS A PUNCTURE. REPAIRED MAIN CABIN FLOORBOARD 252RG IAW EO A300-5320-38221-B.

Part: FLOORBOARD — PUNCTURED (CARGO BAY) · airframe 10,955 hrs · 6,832 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 252MG HAS A PUNCTURE. REPAIRED MAIN CABIN FLOORBOARD 252MG IAW EO A300-5320-38221-B.

Part: FLOORBOARD — CRACKED (FWD CARGO BAY) · airframe 10,955 hrs · 6,832 cycles

INSPECTION TYPE:10YR, FWD CARGO FLOORBOARD 132FE IS CRACKED ON THE BOTTOM. REPAIRED FWD CARGO FLOORBOARD 132FE IAW EO A300-5320-38221-B.

Part: FLOORBOARD — CRACKED (FWD CARGO BAY) · airframe 10,955 hrs · 6,832 cycles

INSPECTION TYPE:10YR, FWD CARGO FLOORBOARD 132QG IS CRACKED ON THE BOTTOM SIDE. REPAIRED FWD CARGO FLOORBOARD 132QG IAW EO A300-5320-38221-B.

Part: FLOORBOARD — CRACKED (FWD CARGO BAY) · airframe 10,955 hrs · 6,832 cycles

INSPECTION TYPE:10YR, FWD CARGO FLOORBOARD 132SG IS CRACKED ON THE BOTTOM SIDE. REPAIRED FWD CARGO FLOORBOARD 132SG IAW EO A300-5320-38221-B.

Part: FLOORBOARD — CRACKED (AFT CARGO BAY) · airframe 10,955 hrs · 6,832 cycles

INSPECTION TYPE:10YR, AFT CARGO FLOORBOARD 151SF HAS CRACKED EDGE. REPAIRED AFT CARGO FLOORBOARD 151SF IAW EO A300-5320-38221-B.

Part: FLOORBOARD — CRACKED (FWD CARGO BAY) · airframe 10,955 hrs · 6,832 cycles

INSPECTION TYPE:10YR, FWD CARGO FLOORBOARD 131SG IS CRACKED ON BOTTOM SIDE. REPAIRED FWD CARGO FLOORBOARD 131SG IAW EO A300-5320-38221-B.

Part: FLOORBOARD — CRACKED (FWD CARGO BAY) · airframe 10,955 hrs · 6,832 cycles

INSPECTION TYPE:10YR, FWD CARGO FLOORBOARD 131AH IS CRACKED ON THE BOTTOM SIDE. REPAIRED FWD CARGO FLOORBOARD 131AH IAW EO A300-5320-38221-B.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 10,955 hrs · 6,832 cycles

INSPECTION TYPE:10YR, AFT CARGO FLOOR PANEL NR 151NG IS DELAMINATED ON BOTTOM SIDE FABRICATED AFT CARGO FLOOR PANEL NR 151NG IAW EO A300-5320-16407-D, APPENDIX C.

Part: FLOORBOARD — CRACKED (FWD CARGO BAY) · airframe 10,955 hrs · 6,832 cycles

INSPECTION TYPE:10YR, FWD CARGO FLOORBOARD 131RG IS CRACKED ON THE BOTTOM SIDE. REPAIRED FWD CARGO FLOORBOARD 131RG IAW EO A300-5320-38221-B.

Part: FLOOR PANEL — CRACKED (AFT CARGO BAY) · airframe 9,771 hrs · 6,082 cycles

INSPECTION TYPE:4C AFT CARGO FLOOR PANEL 152TF IS CRACKED AT CORNER. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-C, APPX C.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 9,771 hrs · 6,082 cycles

INSPECTION TYPE:4C BULK PIT FLOOR PANEL 162HF REQUIRES REPLACEMENT IAW EO A300-5100-33666 -A. FABBED FLOOR PANEL 162HF IAW UPS EO A300-5320-16407-C, APPX D.

Part: DOUBLER — GOUGED (TE FLAP) · airframe 9,771 hrs · 6,082 cycles

INSPECTION TYPE:4C REPAIR SURVEY SEQUENCE 127-W3-02 REPAIR DOUBLER IS GOUGED. REMOVED, FABRICATED AND INSTALLED NEW REPAIR DOUBLER PER EA 300-5753-0 1-A1902.

Part: DOUBLER — GOUGED (TE FLAP) · airframe 9,771 hrs · 6,082 cycles

INSPECTION TYPE:4C REPAIR SURVEY SEQUENCE 127-W3-01 REPAIR DOUBLER IS GOUGED. REMOVED, FABRICATED AND INSTALLED NEW REPAIR DOUBLER PER A300-600 SRM 57-50-00 FIG 205 PARA 4E.

Part: DOUBLER — GOUGED (TE FLAP) · airframe 9,771 hrs · 6,082 cycles

INSPECTION TYPE:4C REPAIR SURVEY SEQ 127-W3-01 REPAIR DOUBLER IS GOUGED. REMOVED, FABBED, AND INSTALLED REPAIR DOUBLER IAW A300-SRM 57-50-00 FIG 205, PARAGRAPH 4E.

Part: FLOORBOARD — GOUGED (CARGO BAY) · airframe 9,771 hrs · 6,082 cycles

INSPECTION TYPE:4C FLOORBOARD PANEL 131MG HAS SEVERAL EDGE GOUGES AS MARKED. FABRICATED FLOORBOARD PER EO A300-5320-16407-C, APPX C.

Part: THRUST REVERSER — CRACKED (NR 2 ENGINE) · airframe 9,771 hrs · 6,082 cycles

INSPECTION TYPE:4C NR 2 ENGINE INBOARD T/R TRANSLATING SLEEVE AT 6:00 POSITION HAS CRACKED LWR CLOSURE AT LWR END. REPAIRED IAW UPS EO A300-7830-34175-A, SAA EA 300-7830-01-A1899, & R CD 368227.

Part: THRUST REVERSER — CRACKED (NR 1 ENGINE) · airframe 9,771 hrs · 6,082 cycles

INSPECTION TYPE:4C NR 1 ENG INBOARD TRANSLATING SLEEVE LWR EDGE ANGLE IS CRACKED AT 6:00 POSITION. REMOVED CLOSURE ANGLE, FABRICATED ANGLE AND FILLER, AND INSTALLED PER EO A300-7830-34175-A.

Part: SWITCH — DEFECTIVE (CABIN)

INSPECTION TYPE:N/A EMERGENCY TEST SWITCH ON PANEL 818VU, INOP. FOUND PUSH BUTTON SWITCH BAD. NEW SWITCH ATTACHED TO CONNECTOR. THE 818VU PANEL REMOVED FROM BULKHEAD. REMOVED AND REPLACED 818VU PANEL. OPS CHECK PER M/M 33-51-00-5.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

EVAC SLIDE DOOR LIGHT INOP. DEFERRED IAW MEL 392753. OPEN

Part: WARNING LIGHT — INOPERATIVE (FLIGHT DECK)

EVAC SLIDE WARNING LIGHT INOP, BUZZER OK. PLACED ON MEL 52-73-01-1. CONTROL NR M373730. RESET ELEC. CONNECTOR ON ASPSU (7OWN) WITH REF TO AMM 52-73-18-04 PARA C(6). TESTED ASPSU IAW AMM 52-73-00-05. NO FAULTS NOTED. TESTED EVAC SLIDE WARNING LIGHT WITH REF TO AMM 52-73-11-04 PARA 1. OPS CK GOOD. THIS CLEARS M 373730.

Part: FITTING — OBSTRUCTED (GIRT BAR)

INSPECTION TYPE:N/A SLIDE ARMING LEVEL ON DOOR IS VERY STIFF & HARD TO DISARM. REMOVED DEBRIS FROM GIRT BAR FLOOR FITTINGS. OPS CHECK GOOD.

Part: CONNECTOR — MALFUNCTIONED (WARNING SYS)

INSPECTION TYPE:N/A ESCAPE SLIDE WARNING LIGHT FOUND INOP ON PREFLIGHT. DEFER PER MEL 52-73-01-1. *SUPPLEMENTAL SDR* RESET CONNECTOR ON ASPSU. PERFORMED SUCCESSFUL OPERATIONAL TEST IAW AMM 52-73-00-05. THIS CLEARS DEFERRAL M354613. PLACARD REMOVED.

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A IN BULK COMPARTMENT LOAD CREW REPORTED SMALL HOLE IN FLOOR FOUND TO BE DENT 1.75 INCH WITH .75 INCH TEAR AT BOTTOM LOCATED 31.5 INCHES IN FROM BULK DOOR AND 3.5 INCHES FROM TIE DOWN FITTING FOR NET. PERFORMED TEMP REPAIR TO DAMAGE W/ REF TO SRM 53-10-20 FIG 110. ITEM TO BE PERMANENTLY REPAIRED WITHIN 350 FLIGHT HOURS ASSIGNED ON DEFERRAL D-354335.

Part: FLOORBOARD — PUNCTURED (FUSELAGE)

INSPECTION TYPE: N/A (2) PUNCTURES IN FLOOR BOARD AS POSITION 1. REPAIRED (2) HOLES IAW SRM 53-10-20.

Part: LEVER — STIFF (SLIDE ARM)

SLIDE ARMING LEVER ON ENTRY DOOR IS EXTREMELY HARD TO ARM/DISARM. IT WILL NOT MOVE TO ARMED UNLESS WITH A LOT OF EFFORT. ABOVE NORMAL FORCE REQUIRED. CLEANED GIRT BAR ATTACH FITTINGS. OPS CK NORMAL PER MM 25-61-20-06 PARAGRAPH 4.

Part: WINDOW — CRACKED (COCKPIT)

ECAM WARNING RT WINDOW FAULT. FOLLOWED ECAM AND AOM PROCEDURES, WHICH SECURED RT WINDOW HEATS, 2 MINUTES LATER RT WINDOW CRACKED. FOLLOWED A AOM PROCEDURES, DECLARED AN EMERGENCY. ACCOMPLISH STEPS 1-6 PER 56-11-11-04 PER F/O'S WINDOW NEEDS TORQUED. TORQUED BOLTS AND COMPLETED WINDSHIELD INSTALLATION PER MM 56-11-11-04, OPS CK WINDSHIELD ANTI-ICE AND DEFOG PER MM 30-42-00-5, OK FOR SERVICE.

Part: WINDOW — FAILED (COCKPIT)

CAPTAIN'S WINDOW SEVERELY CRACKED. AT 330 WINDOW CRACKED. REMOVED CAPTAIN'S SIDE WINDSHIELD PANEL REF MM 56-11-11-4 STEPS 1B & C COMPLETED. COMPLETED R & R OF CAPTAIN'S WINDSHIELD PER MM 56-11- 11-4. SYSTEMS TESTS NORMAL PER MM 30-42-00-5.

Part: INDICATOR — ILLUMINATED (NR 2 FIRE LOOP)

ENGINE NR 2 "A" LOOP LIGHT ILLUMINATED. DEFERRED NR 2 ENG LOOP "A" INOP PER MEL 26-12-01-1, PLACARD INSTALLED.

Part: LIGHT — NO TEST (CABIN)

EMERGENCY LIGHT DOESN'T TEST PROPERLY. ALL 18 LTS ARE WORKING AND VISUALLY INSPECTED 11 18 PART NUMBERS (OM 0557802) REPLACED PSU OPS CK NORMAL PER 33-51-14-4.

Part: BULB — INOPERATIVE (EMERG EXIT SIGN)

INSPECTION TYPE:N/A EXIT SIGN ABOVE CREW ENTRY DOOR HAS AN INOP BULB. REMOVED AND REPLACED INOP BULB ON CREW ENTRY DOOR EXIT LIGHT MODULE PER MM 33-51-13-4.

Part: HANDLE — STUCK (ESCAPE SLIDE)

UNABLE TO DISARM SLIDE. LUBRICATED ARMING HANDLE, ARMED & DISARMED SLIDE SEVERAL TIMES. CHECKED ESCAPE SLIDE IAW MM 25-61-20-6, FOUND SATISFACTORY.

Part: LIMIT SWITCH — INOPERATIVE (EVAC SLIDE)

ESCAPE SLIDE DOES NOT ARM ONLY AFTER NUMEROUS TRIES. REMOVED AND REPLACED LIMIT SWITCH 13WN IAW MM 52-73-13-4, OPS CK.

Part: SWITCH — DEFECTIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT DISARM WILL NOT COME ON, LIGHT TEST OK. REMOVED PANEL 436 VU, REPLACED EMERGENCY EXIT LIGHT SWITCH, INSTALLED PANEL 436 VU. OPS CHECK OF ALL SWITCHES AND LIGHTS ON PANEL 436 VU OK.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT)

CAPTAINS OXYGEN MASK INOPERATIVE. REMOVED AND REPLACED CAPTAINS OXYGEN MASK STOWAGE BOX IAW MM 35-12-51-4.

Part: POWER SUPPLY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS STAY ON IN THE ARMED POSITION THROUGH FLIGHT. REPLACED EMERGENCY LIGHT POWER SUPPLY UNIT PER M/M 33-51-14-4, SYSTEM TEST OK P/N 324-54-10, S/N OFF 2804, S/N ON 3215.

Part: BATTERY — DISCHARGED (E/E BAY)

INSPECTION TYPE:IN EVACUATION SLIDE WARNING LIGHT AND BUZZER INOP, NO SLIDE ARM INDICATION ON ECAM EITHER. REMOVED AND REPLACED NR 2 MAIN SHIP BATTERY PER MM 24-31-11 SYSTEM OPS.

Part: BATTERY — DISCHARGED (E/E BAY)

INSPECTION TYPE: N/A AT DEPARTURE, FLT CREW REPORTED THAT THE EMERGENCY ESCAPE SLIDE WARNING LIGHT AND HORN WOULD NOT TEST. DURING TROUBLESHOOTING FOUND THAT NR 2 SHIP BATTERY DISCHARGED WITH ONLY 1V. REMOVED AND REPLACED BATTERY. SYSTEM OPERATION CHECKED NORMAL.

Part: OXYGEN BOTTLE — DISCHARGED (CABIN)

INSPECTION TYPE:N/A PILOT REPORTS CREW O2 BOTTLE EMPTY ****SUPPLEMENTAL MRR*** SERVICED BOTTLE