N126UP

Part: SKIN — GOUGED (ZONE 300) · airframe 28,301 hrs · 17,173 cycles

WHILE GIVING OK TO INSTALL RT VERTICAL ROOT PANEL 323AR, FOUND GOUGE ON FUSELAGE UNDER PANEL, ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-95674-REQ1 AND VT-MAE EA 300-5319-27-A4225 REV IR.

Part: SKIN — CORRODED (ZONE 500) · airframe 28,301 hrs · 17,173 cycles

LEFT WING HAS DISBOND PLY ON LOWER SURFACE OF THE OUTBOARD TRAILING EDGE COVERED BY SPEED TAPE. INSTALLED NEW EXTRUSION (SECTION PANEL TRAILING EDGE) AT LT WING O/B IAW SRM 51-40-21. REMOVED CORROSION AT ALUMINUM EXTRUSION IAW SRM 51-74-10. FOUND TO BE OUT LIMITS IAW SRM 57-51-12 PAR.(3)(H).

Part: SKIN — CORRODED (ZONE 600) · airframe 28,301 hrs · 17,173 cycles

RIGHT WING OTBD TRAILING EDGE HAS 3 PIECES OF SPEED TAPE. REMOVED CORROSION AT ALUMINUM EXTRUSION IAW SRM 51-74-10. FOUND TO BE OUT LIMITS IAW SRM 57-51-12 PAR.(3)(H). INSTALLED REPAIR PLATES (2EA) AND INSERTS (2EA) AT RT WING OTBD TRAILING EDGE IAW SRM 57-51-12 PAR. (L) 7(N) TO 7(P).

Part: BRACKET — BROKEN (ZONE 500 FLAP) · airframe 28,301 hrs · 17,173 cycles

LEFT WING CENTER FLAP OUTBD SIDE BRACKET IS BROKEN OFF. INSTALLED BRACKET IAW A300-600 SRM 51-40-21 P/N CR3223-4-2 BATCH# 0004423484 3EA.

Part: ANGLE — BROKEN (ZONE 200) · airframe 28,301 hrs · 17,173 cycles

MAIN CARGO FLOOR STRUCTURE "Z" ANGLE IS CRACKED AT -Y2127.5 BETWEEN FR73 AND FR74 DOT 1/038. INSTALLED "Z" ANGLE AT MAIN CARGO FLOOR STRUCTURE -Y2127.5 BETWEEN FR73 AND FR74 IAW A300-600 SRM 51-40-21.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 28,301 hrs · 17,173 cycles

MDC FLOOR PANEL 261JM BROKEN. DOT 21-08. FLOOR PANEL FABICATION IS COMPLETED IAW SREO-16407-REQ001 ((APPX B) MAIN DECK CARGO COMPARTMENT FLOOR PANEL FABRICATION (SREO)).

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 28,301 hrs · 17,173 cycles

MAIN CARGO FLOOR PANEL 262DM BROKEN ON FWD RH CORNER DOT 1/034. FLOOR PANEL FABICATION IS COMPLETED IAW SREO-16407-REQ001 ((APPX B) A300 MAIN CARGO DECK COMPARTMENT FLOOR PANEL FABRICATION (SREO)).

Part: ANGLE — BROKEN (ZONE 200) · airframe 28,301 hrs · 17,173 cycles

CRACK ON Z ANGLE FR 80/82 Y2127.5. INSTALLED "Z" ANGLE AT Z ANGLE FR 80/82 Y2127.5 IAW A300-600 SRM 51-40-21.

Part: SKIN — CRACKED (ZONE 600) · airframe 28,301 hrs · 17,173 cycles

RH WING, L/E, CUTOUT OF 613AB ACCESS, HAS A CRACK ON FWD O/B SCREW HOLE. INSTALLED REPAIR DOUBLERS 1 AND 3 ON RH WING LEADING EDGE CUTOUT FOR ACCESS PANEL 613AB IAW SRM 53-15-63 PARAGRAPH 2 (M,N).

Part: ANGLE — BROKEN (ZONE 200) · airframe 28,301 hrs · 17,173 cycles

MCD FLOOR STRUSCTURE WITH Z ANGLE CRACKED AT FR 80/82 L/H SIDE. Y1580.5. DOT 21-01. INSTALLED "Z" ANGLE AT MCD FLOOR STRUCTURE FR80 AND FR82 L/H SIDE Y1580.5 IAW A300-600 SRM 51-40-21.

Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 28,301 hrs · 17,173 cycles

MDC FLOOR PANEL 261DM BROKEN AT UPPER SURFACE. DOT 21-02. FLOOR PANEL FABICATION IS COMPLETED IAW SREO-16407-REQ001 ((APPX B) A300 MAIN DECK CARGO COMPARTMENT FLOOR PANEL FABRICATION (SREO)).

Part: BRACKET — CRACKED (ZONE 600 FLAP) · airframe 28,301 hrs · 17,173 cycles

RIGHT WING CENTER FLAP OUTBD SIDE BRACKET IS BROKEN OFF. INSTALLED BRACKET IAW SRM 51-40-21.

Part: ANGLE — BROKEN (ZONE 200) · airframe 28,301 hrs · 17,173 cycles

MCD FLOOR STRUSCTURE "Z" ANGLE IS CRACKED AT 2EA LOCATIONS BTWN FR 74 AND FR 75 AT L/H SIDE. Y2127.5. DOT 21-07. INSTALLED "Z" ANGLE AT MAIN CARGO FLOOR STRUCTURE Y2127.5 BETWEEN FR 74 AND FR 75 AT L/H SIDE. Y2127.5 IAW A300-600 SRM 51-40-21.

Part: PANEL — CRACKED (ZONE 600 K FLAP) · airframe 28,301 hrs · 17,173 cycles

RIGHT WING, L/E, KRUGER FLAP BOX AREA, BY RIB2, PANEL STR HAS A CRACK ON A CORNER. REMOVED OTBD ZEE ANGLE P/N: A5724228220547, INBD ZEE ANGLE P/N: A57242282203, AND THREE STIFFENERS (UPPER, MIDDLE, LOWER) FROM PANEL P/N: A57242282001 TO FOM IAW SRM 51-40-21. INSTALLED THE OTBD ZEE ANGLE, INBD ZEE ANGLE, AND THREE STIFFENERS (UPPER, MIDDLE, LOWER) ON THE PANEL P/N: A57242282001 IAW SRM 51-40-21.

Part: FAIRING — CRACKED (ZONE 400) · airframe 28,301 hrs · 17,173 cycles

AFT FAIRING 485AL HAS A CRACK AT AFT I/B SIDE. PERFORMED WELDING AT CRACKED AREA AT AFT FAIRING 485AL AT AFT I/B SIDE. IAW SRM 54-55-51 AMS 4921 RED. VERIFIED PERFORED WELDING AT CRACKED AREA AT AFT FAIRING 485AL AT AFT I/B SIDE. IAW SRM 54-55-51 AMS 4921.

Part: INTERCOSTAL — BROKEN (ZONE 600) · airframe 28,301 hrs · 17,173 cycles

RIGHT WING TRAILIN EDGE STA 1196 RIB17 INTERCOSTAL IS BROKEN . INSTALLED INTERCOSTALL AND FITTING AT R/H WING T/E STA 1196 RIB 17. IAW SRM 51-40-21-001.

Part: RIB — CRACKED (ZONE 600) · airframe 28,301 hrs · 17,173 cycles

FAULT: RH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 EA CRACK INDICATION NOTED AT RIB 11. CIRCLED IN RED. ++PERFORM RIB 11 REPAIR IN ACCORDANCE WITH FIGURE 5, TAKING EXISTING FASTENER PATTERN INTO ACCOUNT INSTALLING SOLID RIVETS PER DRAWING REQUIREMENTS AT THE UPPER SKIN/RIB INTERFACE.

Part: BULB — INOPERATIVE (ZONE 200) · airframe 27,560 hrs · 16,782 cycles

L1 DOOR EMERGENCY SIGN PATHWAY LIGHT INOP REMOVED AND REPLACED BULB. REF AMM 33-51-13. OPS CHECK OK

Part: TRANSFER SYS — FAULTED (FUEL SYSTEM) · airframe 27,013 hrs · 16,516 cycles

ECAM- TRIM TANK AFT XFR NOT AVAILABLE. PERFORMED FUEL SYSTEM TRANSFER CONTROL SYSTEM TEST REF AMM 28-26-00 NO DEFECTS NOTED AT THIS TIME. REMOVED AND REPLACED TRIM TANK COMPENSATOR I.A.W. UPS A300 AMM 28-42-51-401. COMPLETED INSTALLATION OF TAIL TANK COMPENSATOR REF MM 28-42-51-401, STEP B -5(B) TILL END. TESTS NORMAL REF MM 28-42-00/501.

Part: SHEAR TIE — CRACKED (FRAME BASE 45R) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:1CFRAME 45R FRAME FEET CRACKED IN AREA 1.REMOVED AND REPLACED IAW EO A300-5310-46789-G APPENDIX G.

Part: FLAP — GOUGED (RIGHT) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:CRH IB FLAP OB TOP BOUBLER HAS GOUGESREPLACED DOUBLER WITH A NEW DOUBLE IAW UPS EO A300-5750-87370-A

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:CSEAT TRACK AT Y1959 BETWEEN FR 30 AND 32 IS CORRODEDREPAIRED SEAT TRACK IAW SRM53-10-16-201

Part: FLAP — CRACKED (RW CENTER) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:CRH WING CENTER FLAP HAS 1EA CRACK ON FLANGE 13REPAIRED FLANG IAW SRM 57-50-00-201

Part: FLAP — CRACKED (RW CENTER FLAP) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:CRH WING CENTER FLAP HAS 1EA CRACK ON FLANGE 21REPAIRED FLANG IAW SRM 57-50-00-201

Part: FLAP — CRACKED (RW CENTER) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:C, RT WING CENTER FLAP HAS 1EA CRACK ON RIB 26REPAIER IAW UPS EO A300-5750-87448 REV A

Part: FLAP — CRACKED (RW CENTER) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:CRH WING CENTER FLAP HAS 1EA CRACK ON RIB 17REPAIER IAW UPS EO A300-5750-87448 REV A

Part: FLAP — CRACKED (RW CENTER) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:CRH WING CENTER FLAP HAS 1EA CRACK ON RIB 27REPAIER IAW UPS EO A300-5750-87448 REV A

Part: FLAP — CRACKED (RW CENTER) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:CRH WING CENTER FLAP HAS 1EA CRAK ON RIB 25REPAIER IAW UPS EO A300-5750-87448 REV A

Part: DOUBLER — CRACKED (PYLON) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:1CPYLON PRECOOLER PANEL 413BL HAS A CRACK ON THE LOWER SIDE.FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 54-52-51 AND 51-40-21.

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:1CPANEL 231RG DAMAGEDFABBED PNL IAW SREO A300-5320-40552-B.

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:1CPANEL 232SG DAMAGEDFABBED PNL IAW SREO A300-5320-40552-B

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:1CPANEL 231WG IS DAMAGEDFABBED PNL IAW SREO A300-5320-40552-B

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:1CPANEL 221FG DAMAGEDFABBED PNL IAW SREO A300-5320-40552-B

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:1CPANEL 231BH BROKENFABBED PNL IAW SREO A300-5320-40552-B

Part: SEAT TRACK — CORRODED (MCD) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:1C*MAJOR REPAIR* AFT CABIN SEAT TRACK AT Y1580.5 AT FRAME 79 IS CORRODED.REMOVED, FABRICATED, AND INSTALLED IAW RCD 293484 AND SRM 53-10-16-201.

Part: SEAT TRACK — CORRODED (MCD) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:IC*MAJOR REPAIR* AFT CABIN SEAT TRACK AT -Y450 AT FRAME 78 IS CORRODED.REMOVED, FABRICATED, AND INSTALLED IAW RCD 293485 AND SRM 53-10-16-201.

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:IC2CPANEL DAMAGEDFABBED PNL IAW SREO A300-5320-40552-B

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:1CPANEL 231NJ DAMAGEDFABBED PNL IAW SREO A300-5320-40552-B.

Part: ADAPTER — BROKEN (MCD) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:1CMAIN DECK CARGO FLOOR SEAT ADAPTER AT FR 34 L/H BETWEEN Y1959 AND Y2462 BROKEN.REMOVED AND REPLACED IAW SRM 51-40-21.

Part: BRACKET — CRACKED (AFT CARGO) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE: 1C AFT CARGO FR 54 BRACKET AT Y953 LH CRACKED.REMOVED AND REPLACED IAW SRM 51-40-21.

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:1CPANEL 232XG IS DAMAGEDFABBED PNL IAW SREO A300-5320-40552-B

Part: SEAT TRACK — CORRODED (MCD) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:1C*MAJOR REPAIR* AFT CABIN SEAT TRACK AT Y1137.1 AT FRAME 80 IS CORRODED.REMOVED, FABRICATED, AND INSTALLED IAW RCD 293318 AND SRM 53-10-16-201.

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:1CPANEL 232NJ DAMAGEDFABBED PNL IAW SREO A300-5320-40552-B

Part: BRACKET — BROKEN (333AT) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:1CTHREE EACH SUPPORTS FOR APRON 333AT ARE BROKEN.REMOVED AND REPLACED IAW SRM 51-40-21.

Part: BRACKET — BROKEN (333AT) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:1CTHREE EACH SUPPORTS FOR APRON 333AT ARE BROKENREMOVED AND REPLACED IAW SRM 51-40-21.

Part: BRACKET — BROKEN (333AT) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:1CTHREE EACH SUPPORTS FOR APRON 333AT ARE BROKEN.REMOVED AND REPLACED IAW SRM 51-40-21.

Part: SPAR — CRACKED (#1 INLET COWL) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:1CENGINE 1 I/B SIDE INLET COWL REAR SPAR HAS 1 EA CRACK AT 3 O'CLOCK POSITION.FABRICATED WEB SPAR AND REPLACED IAW SRM 51-40-21 AND P&W SRM 54-10-00.

Part: BRACKET — CRACKED (AFT CARGO) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:1CAFT CARGO FR 54 BRACKET AT-Y953 LH CRACKED.REMOVED AND REPLACED IAW SRM 51-40-21.

Part: BRACKET — CRACKED (AFT CARGO) · airframe 25,944 hrs · 15,848 cycles

INSPECTION TYPE:1CAFT CARGO FR 54 BRACKET AT - Y953 RH CRACKED.REMOVED AND REPLACED IAW SRM 51-40-21.

Part: DOOR — NONE (DOOR) · airframe 24,467 hrs · 14,978 cycles

INSPECTION TYPE:NALOCKING PIN MISSING FOR MAIN CREW ENTRY DOORREPLACED MISSING PIN WRT A300 AMM 52-73-00

Part: NONE — NONE (DOOR) · airframe 24,286 hrs · 14,861 cycles

INSPECTION TYPE:NA**SUPPLEMENTAL SDR **SLIDE PRESSURE NOT IN GREEEN BAND. DEFERRED L1 DOOR SLIDE IAW MEL 52-11-01-2-3REPLACED DOOR SLIDE AS PER AMM 25-61-21-0401 EMERGENCY OP CYL AND DOOR WARNING SYSTEM ARMED/CHECKED. DMP WAS NOT APPLICABLE AS PER 52-11-01-2-3. SLIDE WAS NOT REMOVED.

Part: INTERPHONE — FAILED (EMPENNAGE) · airframe 23,631 hrs · 14,469 cycles

ATB* EMERG DECL'D*HAZMAT INFO WAS SENT* A/C LANDED WITHOUT INCIDENT*A/C OOS* - WITH GEN #2 DEFFERED. APU FAILED AT 100 FT ON TAKEOFF. EMERGENCY DECLARED TO KMCO. R/R IDG & INTERPHONE BOX.TROUBLESHOT PER AMM 49-62-00 SCH 1 PG 101. THIS CLEARS M752897

Part: GIRT BAR — DIRTY (DOOR SLIDE) · airframe 23,586 hrs · 14,441 cycles

INSPECTION TYPE:NACREW REPORTED DIFFICULITY IN DISARMING DOOR SLIDE.CLEANED AND LUBED GIRT BAR AND ALL ASSOCIATED LINKAGES PER AMM 12-22-52-0001. OPS CHECK GOOD PER AMM 25-61-21-0401

Part: STIFFENER — CRACKED (LH WING LE KRUE) · airframe 23,526 hrs · 14,404 cycles

INSPECTION TYPE:CLH WING LE KRUEGER FLAP STIFFENER I/B CUTOUT IS DAMAGED.REMOVED AND REPLACED STIFFENER PER SRM 51-40-21.

Part: FORMER — CRACKED (LH WING LE KRUEG) · airframe 23,526 hrs · 14,404 cycles

INSPECTION TYPE:CLH WING LE KRUEGER FLAP FORMER I/B CUTOUT IS DAMAGED.REMOVED AND REPLACED FORMER PER SRM 51-40-21.

Part: FITTING — CRACKED (FRM 45 S36L) · airframe 23,526 hrs · 14,404 cycles

INSPECTION TYPE:A300CENTER FUSELAGE FRAME BASE FITTING STR. 36 FR45 L/H CRACKED.REPAIR IAW A300-5310-46789-G APPENDIX J.

Part: FRAME — CRACKED (FRM 40) · airframe 23,526 hrs · 14,404 cycles

INSPECTION TYPE:CFRAME 40 L/H UPPER JUNCTION TOP HOLE HAS CRACK INDICATION FOUND DURING ROTARY PROBE 2 O'CLOCK POSITIONREPAIRED IAW EA 300-5710-A2622 STEPS 1-35

Part: FRAME — CRACKED (FRM 40) · airframe 23,526 hrs · 14,404 cycles

INSPECTION TYPE:CFRAME 40 UPPER UNCTION BOTTOM HOLE HAS CRACK INDICATION FOUND DURING ROTARY PROBE 6 O'CLOCK POSITIONREPAIRED IAW EA 300-5710-A2622 STEPS 1-35

Part: FRAME — CRACKED (FRM 40) · airframe 23,526 hrs · 14,404 cycles

INSPECTION TYPE:CLH FR 40 UPPER JUNCTION MIDDLE FASTENER HOLE CRACKS 2 O'CLOCK POSITIONREPAIR HOLE PER EA 300-5710-27-A2622 STEPS 1-35

Part: FRAME — CRACKED (FRM 40) · airframe 23,526 hrs · 14,404 cycles

INSPECTION TYPE:A300LH FR 40 LOWER JUNCTION MIDDLE FASTENERS HOLE CRACKS 9 O CLOCK POSITIONREPAIR HOLE PER EA A300-5710-27-A2619 STEPS 1-14

Part: ACCESS PANEL — CRACKED (NR 2 NACELLE) · airframe 23,526 hrs · 14,404 cycles

INSPECTION TYPE:A300ACCESS, PANEL 424AR EXTERNAL SURFACE WITH DENTREMOVED AND REPLACED 424AR P/N A7521502500300 IAW AMM 54-52-61-04-01

Part: BRACKET — CRACKED (NR 3 SPOILER) · airframe 23,526 hrs · 14,404 cycles

INSPECTION TYPE:CLT WING BELOW #3 SPOILER I/B END RIB INTER-COSTAL FWD BRACKET CRACKED.REMOVED AND REPLACED IAW SRM 51-40-21

Part: PANEL — CRACKED (NR 1 NACELLE) · airframe 23,526 hrs · 14,404 cycles

INSPECTION TYPE:A300PANEL RACK PANEL 413BL HAS A CRACKREPAIRED IAW 54-52-51-PARA 5.E FIGURE205

Part: RUB STRIP — CRACKED (LT WING TE FLAP) · airframe 23,526 hrs · 14,404 cycles

INSPECTION TYPE:A300 LT WING CENTER FLAP L/E TOP SURFACE ROLLER RUB PLATE CRACKEDREMOVED,FABRICATED,AND INSTALLED IAW A300 SRM 51-40-21 AND 57-53-12

Part: SPAR — CRACKED (LT WING) · airframe 23,472 hrs · 14,365 cycles

INSPECTION TYPE:A300DURING ROTO OF LH WING FR47 FASTENER HOLES PER EO A300-5710-68606-G A CRACK INDICATION WAS NOTED IN HOLE D.REPAIRED IAW UPS EO A30-5710-80684-A

Part: BLOWER — INOPERATIVE (EVAS) · airframe 23,235 hrs · 14,211 cycles

INSPECTION TYPE:N/ALH EVAS FAILS BLOWER CHECKLH EVAS UNIT REPLACED OPS CK GOOD. REF:AMM 25-69-00.

Part: JACKSCREW — CONTAMINATED (SLAT SYSTEM) · airframe 22,761 hrs · 13,947 cycles

EMERGENCY DECLARED, NO EQUIP USED. A/C WAS OUT OF SERVICE. DURING APPROACH GOT SLATS SYS 1 & SYS 2 FAULT. FOLLOWED QRH. T/S SLAT SYS, PER TSM 27-80-02. BOTH SFCC'S FLGING JAM. FOUND LT SLAT TORQ LIMIT TRIPPED & NR 3 SCREWJACK ACT TRIPPED. PERFORMED OIL LEVEL CHECK/SERVICE AMM 12-13-27. PERFORMED BALL NUT GREASE, IAW 12-22-27 & SIG AMT OF WATER PUSHED OUT. REMOVED & REPLACED LT NR 3 SCREW JACK, IAW AMM 27-84-22. OPERATIONS CHECKS GOOD.

Part: FUEL TANK — CORRODED (CENTER) · airframe 22,170 hrs · 13,592 cycles

INSPECTION TYPE:SEG, CENTER FUEL TANK LOWER EXTERNAL SKIN LT FRAM FWD AREA HAS CORROSION. EA 300-5710-27-A2476 REV: PREM 3

Part: FUEL TANK — CORRODED (CENTER) · airframe 22,170 hrs · 13,592 cycles

INSPECTION TYPE: SEG, CENTER FUEL TANK EXTERNAL SKIN L/H FRAME FWD AREA HAS CORROSION, EA 300-5710-27-A2476 REV: PREM 3

Part: SKIN — CORRODED (CENTER) · airframe 22,170 hrs · 13,592 cycles

INSPECTION TYPE:SEG, CENTER FUEL TANK LOWER EXTERNAL SKIN L/H FRAM FWD AREA HAS CORROSION, EA 300-5710-27-A-2476 REV: PREM 3

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 22,170 hrs · 13,592 cycles

INSPECTION TYPE:SEGR/WING I/B FLAP LOWER SURFACE HAS SEVERAL DENTSREPAIRED PER EA 300-5750-27-A2474 & SRM 57-52-12-001, FIG 3, LHT3.

Part: LONGERON — DAMAGED (NR 2 PYLON) · airframe 22,170 hrs · 13,592 cycles

INSPECTION TYPE:SEG NR 2 PYLON FAIRING 485AL MIDDLE LONGERON HAS ELONGATED HOLES IN ATTACH FLANGE. REMOVED AND INSTALLED NEW LONGERON IAW SRM 51-40-21.

Part: LONGERON — DAMAGED (NR 1 PYLON) · airframe 1,815 hrs · 1,134 cycles

INSPECTION TYPE:SEG NR 1 PYLON FAIRING 475AL HAS ELONGATED HOLES IN I/B MIDDLE LONGERON ATTACH FLANGE. REMOVED AND INSTALLED NEW LONGERON IAW SRM 51-40-21.

Part: SKIN PANEL — CHAFED (RT WING) · airframe 22,170 hrs · 13,592 cycles

INSPECTION TYPE:SEG PANEL 481AT HAS HOLE CHAFED THRU ON INNER SKIN. REPLACED PANEL 481AT IAW IPC 57-41-41-18.

Part: PANEL — DAMAGED (LT COWLING) · airframe 22,170 hrs · 13,592 cycles

INSPECTION TYPE:SEG PANEL 413BL HAS (2) ELONGATED HOLES IN ATTACH FLANGE. RECEIVED NEW PNL ASSY INSTALLED ON ACCESS M10 IAW SRM 51-40-21.

Part: TAB — BROKEN (LT WING TE FLAP) · airframe 22,170 hrs · 13,592 cycles

INSPECTION TYPE:SEG, LEFT WING MIDDLE FLAP OTBD FACE HAS A BROKEN TAB. REMOVED AND REPLACED THE TAB IAW SRM 51-40-21.

Part: SIDEWALL PANEL — BROKEN (FWD CARGO) · airframe 22,170 hrs · 13,592 cycles

INSPECTION TYPE:SEG, FWD MDC SIDEWALL PANEL 232BK BROKEN. FABRICATED FWD MDC SIDEWALL PANEL IAW SREO A300-2550-40641-A.

Part: HANDLE — STIFF (L1 DOOR) · airframe 21,077 hrs · 12,978 cycles

INSPECTION TYPE:N/ASLIDE ARM / DISARM LEVER DOES NOT MOVE FREELYOPS CHECK SLIDE ARM /DISARM LEVER UNABLE TO DUPLIDATE THE PROBLEM . ITS OK FOR SERVICE REF MM 52 10

Part: SWITCH — FAULTY (COCKPIT) · airframe 20,923 hrs · 12,888 cycles

INSPECTION TYPE:N/A EMERGENCY LIGHT FUNCTION OF CAPT'S & F/O'S DOME LIGHTS INOP. FROM OVERHEAD PNL & PURSERS PNL. BY CREW ENTRY DOOR.REPLACED EMERGENCY LIGHTING SWITCHING RELAY 43 LE, NO HELP. REPLACED DOME LIGHT SWITCH 14LE - REF ASM 33-12-00. OPS CHECK GOOD PER AMM 33-12-00-0501.

Part: WINDOW — CRACKED (R1) · airframe 20,788 hrs · 12,808 cycles

DIVERSION - R1 WINDOW CRACKED AT FL 320. R&R R1 WINDOW PER MM 56-11-11-0401, OPS CK GOOD

Part: HANDLE — MISSING (ENTRY DOOR) · airframe 20,751 hrs · 12,787 cycles

INSPECTION TYPE:N/A INTERIOR DOOR ASSIST HANDLE ON MAIN ENTRY DOOR UPPER HANDLE MISSING REF IPC 52-11-11-03C ITEM 270. INSTALLED ENTRY DOOR HANDLE COVER W. IAW 52-11-11. THIS CLEARS M678099.

Part: SWITCH — INTERMITTENT (CREW DOOR) · airframe 20,631 hrs · 12,724 cycles

INTERMITTENT CREW ENTRY DOOR OPEN WARNING OTHER INDICATIONS SHOWED DOOR PROPERLY CLOSED. REPLACED CREW DOOR WARNING SWITCH 7WS W/R/T AMM 52-71-00-0401 OPS CK GOOD.

Part: LEVER — INOPERATIVE (L1 DOOR SLIDE) · airframe 20,619 hrs · 12,716 cycles

MAIN ENTRY DOOR SLIDE ARMING LEVER WILL NOT MOVE TO ARMED POSITION. REMOVED AND REPLACED MAIN CABIN L1 DOOR SLIDE IAW MM 52-10-30-0401.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR SLIDE) · airframe 20,613 hrs · 12,709 cycles

MAIN DOOR EMERGENCY SLIDE WILL NOT ARM. READJUSTED GIRT BAR IAW A300 AMM 52-10-11-0501

Part: SUPPORT — GOUGED (NR 1 ENGINE TR) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:12Y#2 ENGINE T/R, OUTBOARD CASCADE SUPPORT FRAME HAS A GOUGE/KNICK IN THE FRAME ON THE EDGE, UPPER SECTION.REPAIRED IAW UPS EO A300-7830-72740-A, DATED 06JUN19.

Part: SPLICE — CRACKED (NR 2 PYLON) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:124C #2 PYLON PRECOOLER PANEL, FWD SUPPORT PLATE CRACKED. REMOVED AND REPLACED SPLICE/FISHPLATE IAW SRM 51-40-21 AND DWG A54612371.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:124C FWD CARGO COMPARTMENT DOOR FRAME FORK AT FR21 HOLE 7, HAS A CRACK INDICATION AT THE 12 O'CLOCK POSITION WITH A DEPTH OF 0.120 - 0.122 FROM OUTER SURFACE. REPAIRED IAW REO-G22024 REV.IR DATE 22-MAY-19.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:124C FWD CARGO COMAPRTMENT DOOR FRAME FORK AT FR23A HOLE 7, HAS CRACK INDICATION AT THE 6 O'CLOCK POSITION WITH A DEPTH OF 0.119 - 0.122 FROM OUTER SURFACE. REPAIRED IAW REO-G22024 REV IR DATED 22-MAY-19.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:124C FWD CARGO COMPARTMENT DOOR FRAME FORK AT FR23A HOLE 9, HAS A CRACK INDICATION AT THE 6 O'CLOCK POSITION WITH A DEPTH OF 0.120 - 0.122 FROM OUTER SURFACE. REPAIRED IAW REO-G22024 REV.IR DATED 22-MAY-19.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:124C FWD CARGO COMPARTMENT DOOR FRAME FORK AT FR24 HOLE 9, HAS A CRACK AT THE 6 O'CLOCK POSITION WITH A DEPTH OF 0.120 FROM OUTER SURFACE. REPAIRED IAW REO-G22024 RE.IR 22-MAY-19.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:124C FWD CARGO COMPARTMENT DOOR FRAME FORK AT FR24 HOLE 2, HAS A CRACK INDICATION AT THE 6 O'CLOCK POSITION WITH A DEPTH OF 0.120 FROM OUTER SURFACE. REPAIRED IAW REO-G22024 REV.IR DATED 22-MAY-19.

Part: HINGE — DAMAGED (RT MLG DOOR) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:12Y, RMLG DOOR CENTER DOOR HINGE LUG ID FOR BEARING EXCEEDS TOLERANCE.INSTALLED SLEEVE PER UPS EO A300-5280-72802-A.

Part: RETAINER — DAMAGED (APU DOOR CUTOUT) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:12YRAPU R/H AFT DOOR CUTOUT AT C101 SEAL RETAINER AND SEAL DAMAGED.REMOVED AND REPLACED DAMAGED SEAL AND SEAL RETAINERS PER A300-600 SRM 51-40-44 AND 51-40-21.

Part: HINGE FITTING — DAMAGED (LT MLG DOOR) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE: 124CL, MLG DOOR CENTER DOOR HINGE LUG ID FOR BEARING EXCEEDS TOLERANCEINSTALLED SLEEVE PER EO A300-5280-72802-A

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:12YR FWD CARGO PIT FLOOR PANEL 131DE CRACKED FR25-FR27. REPAIRED PANEL 131DE IAW EO#A300-5320-42721-F APPENDIX - A.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:12Y, MAIN CABIN FLOOR PANEL 231TG HAS A CRACKED INSERT.REPAIRED PER UPS DWG B53270744 REV A.

Part: FITTING — CRACKED (FRAME 40) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:12Y, CRACK INDICATION IN 3 EA. LOCATIONS, L/H FR 40 UPPER JUNCTION, UPPER HOLE.REPAIRED PER HAECO REO G22035 REV IR AND UPS EO A300-5710-72842-A.

Part: BULKHEAD WEB — CRACKED (NR 1 NACELLE) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:12YR#1 ENG INLET COWL INBD SIDE AT THE 3 O'CLOCK POSITION, THE INLET COWL AFT BULKHEAD IS CRACKED BELOW THE RIGID FITTINGREPAIRED PER P&W SRM 54-10-00 REPAIR #14

Part: FRAME — CRACKED (FRM 46) · airframe 20,613 hrs · 12,709 cycles

POSSIBLE CRACK FOUND AT R/H FR 46 REF AD 2016-25-27. REPAIRED PER EO A300-5310-46789-F APPENDIX K

Part: ANGLE — CRACKED (NR 2 NACELLE) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:12, R#2 PYLON I/B PYLON FAIRING TO ENG ANGLE CRACKED.REPAIRED PER P&W SRM 54-56-10 FG 201.

Part: SUPPORT RIB — CRACKED (NR 1 PYLON) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:12Y, LH #1 ENGINE PYLON L/E, AFT PANEL SUPPORT RIB, FOR SPRING DOORS, 413AL AND 414AR, UPPER INSIDE RADIUS IS CRACKED.REMOVED AND REPLACED RIB ON #1 PYLON IAW AIRBUS DWG A54611461 AND A300 AMM 54-52-61.

Part: RIB — CRACKED (NR 2 PYLON) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:12Y #2 PYLON FRAME FWD OF PRECOOLER CRACKED IN RADIUS. REMOVED AND REPLACED RIB ASSY PER DWG A54611461 AND AMM 54-52-61.

Part: SKIN — CRACKED (LT WING) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:12Y LT L/E PANEL LAND CRACKED JUST AFT OF #1 SLAT NUMBER 2 MAIN TRACK. REMOVED AND REPLACED PER SRM 51-40-21 AND DWG # A57246439.

Part: SKIN — CRACKED (LT WING) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:12Y LT I/B LOWER ACCESS PANEL 513AB LAND IS CRACKED. REPAIRED PER SRM 53-15-63.

Part: SKIN — CRACKED (LT WING) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:12Y LT L/E PANEL LAND JUST O/B OF #1 PYLON IS CRACKED. REPAIRED PER SRM 57-41-12 FIG 207.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:124C FWD CARGO COMPARTMENT DOOR FRAME AT FR24 HOLE 3, HAS A CRACK INDICATION AT THE 6 O'CLOCK POSITION WITH A DEPTH OF 0.120 FROM OUTER SURFACE. REPAIRED IAW REO-G22024 REV.IR DATED 22-MAY-19.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:12YR FWD PIT CARGO FLOORBOARD CRACKED AND DELAMINATED. FAB'D NEW FLOORBOARD IAW EO A300-5320-16407-E.

Part: ATTACH ANGLE — CORRODED (FRAME 40) · airframe 20,613 hrs · 12,709 cycles

FWD CARGO PIT, CWB FRONT SPAR CORRODED AT FRAME #40 RBL 38.5-47.5REMOVED AND REPLACED ANGLE PER A300-600 SRM 51-40-21

Part: WEB — CRACKED (FUSELAGE) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:124C MAIN CABIN, WEB CRACKED BETWEEN FRAME C37 AND 38 RBL98. REMOVED AND REPLACED PER DWG B53774151 REV A AND SRM 51-40-21.

Part: FLOORBOARD — CRACKED (NOT REPORTED) · airframe 20,613 hrs · 12,709 cycles

LOWER SKIN WAS CRAKED IN SEVERAL PLACES AND DELAMINATED. FABRICATED NEW PANEL IAW EO A300-5320-16407-E

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:124C FWD CARGO COMPARTMENT DOOR FRAME FORK AT FR23A HOLE 1, HAS A CRACK INDICATION AT THE 6 O'CLOCK POSITION WITH A DEPTH OF 0.120 - 0.122 FROM OUTER SURFACE. REPAIRED IAW REO-G22024 REV.IR DATED 22-MAY-19.

Part: FORK — CRACKED (CARGO DOOR FRAME) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:12Y, FWD CARGO COMPARTMENT DOOR FRAME FORK AT FR 23A HOLE 2, HAS A CRACK INDICATION AT THE 6 O'CLOCK POSITION WITH A DEPTH OF 0.118 - 0.120 FROM OUTER SURFACE.REPAIRED IAW REO G22024 REV IR DATED 22 MAY 19 AND UPS EO A300-5230-57953-C APPX A.

Part: WEB — CRACKED (FUSELAGE) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:124C MAIN CABIN, WEB CRACKED BETWEEN FRAME # 73 AND 74 LBL 86. REMOVED AND REPLACED PER DWG A53981360 REV:M.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:12YR AFT CARGO FORWARD END WALL PANEL SUPPORT BRACKET @ BL0 IS CRACKED. REMOVED AND REPLACED IAW SRM 51-40-21.

Part: FLOOR SUPPORT — CRACKED (FRAME 38) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:12Y CABIN FLOOR LEVEL STIFFENER BETWEEN RT FR 38.1 AND FR 38.2.REMOVED AND REPLACED CRACKED SUPPORT PER AIRBUS DWG B53774151 AND A300-600 SRM 51-40-21.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:124C FLOOR SUPPORT BRACKET IN THE E&E BAY, RIGHT HAND SIDE AT FR10 IS CRACKED.REMOVED AND REPLACED IAW SRM 51-40-21.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:124C AFT CARGO FORWARD END WALL PANEL SUPPORT BRACKET AT RBL 77 IS CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-40-21.

Part: SHEAR WEB — CRACKED (FRAMES 76 - 77) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:12Y, MAIN CABIN WEB CRACKED BETWEEN FRAME 76 AND 77 APPROX RBL 75 STREAMER ATTACHED.REMOVED AND REPLACED CRACKED WEB IAW DWG A53981418 AND SRM A300-600 51-40-21.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:12YR AFT CARGO FORWARD END WALL PANEL SUPPORT BRACKET @ RBL 36 IS CRACKED. REMOVED AND REPLACED WITH NEW SUPPORT BRACKET IAW SRM 51-40-21.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:124C AFT CARGO FORWARD END WALL PANEL SUPPORT BRACKET AT RBL 39 IS CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-40-21.

Part: SUPPORT PLATE — CRACKED (FRAME 73-74) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:124CMAIN CABIN, WEB CRACKED BETWEEN FR73 & FR74 RBL 86REMOVED, FABRICATED AND INSTALLED NEW SUPPORT PLATE PER A300-600 SRM 51-40-21 AND DWG (AIRBUS) A53981360

Part: SMOKE DETECTOR — CRACKED (FWD CABIN) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE: 12YR, CABIN FLOOR LEVEL LT SMOKE DETECTOR DUCT CRACKED FWD OF FR 53REPAIRED DUCT PER DUCT REPAIR MANUAL

Part: BULKHEAD WEB — CRACKED (NR 2 NACELLE) · airframe 20,613 hrs · 12,709 cycles

INSPECTION TYPE:12YR#2 INBD INLET COWL AFT BLKHD WEB IS CRACKED AT SENSE LINEREPAIRED PER P&W SRM 54-10-00 REPAIR #14

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,487 hrs · 12,044 cycles

EMERG LIGHT IN LAV BURNT OUT. R&R EMERGENCY EGRESS LIGHT IN LAV REF AMM 33-51-21. OPS CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 19,327 hrs · 11,955 cycles

FLOOR PANEL DAMAGED. FABRICATED A NEW FLOOR PANEL IAW EO A300-5320-68509A

Part: LINER — LOOSE (ENTRY DOOR) · airframe 18,501 hrs · 11,470 cycles

LEFT GREEN LOCK INDICATOR ON CREW ENTRY DOOR HARD TO READ (UP TOO HIGH). WHEN DOOR CLOSED INSPECTED FOUND UPPER DOOR LINING LOOSE AND OUT OF POSITION. TIGHTEN DOOR (DH 2020268 9-17-17) LINING, INDICATOR IN CENTER. OP'S CK GOOD IAW MM 52-10-13-04.

Part: PIN — MISSING (L1 DOOR SLIDE) · airframe 18,089 hrs · 11,215 cycles

INSPECTION TYPE: AS-E, L1 DOOR ESCAPE SLIDE SAFETY PIN MISSING. FLAG PIN REPLACED.

Part: GIRT BAR — OUT OF ADJUST (DOOR SLIDE) · airframe 17,906 hrs · 11,087 cycles

DURING POST FLIGHT SLIDE FOR MCD WILL NOT PHYSICALLY DISARM AND BAR WILL NOT TRAVEL FULL RANGE. FOUND FWD GIRT BAR NOT ON DOOR GUIDE FITTING. ADJUSTED ESCAPE SLIDE RELEASE MECHANISM IAW MM 52-10-30-501 OPS NORMAL.

Part: RELAY — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,668 hrs · 10,950 cycles

EXIT LIGHT OVER L1 DOOR INOPERATIVE. R & R 69WL 107VU RELAY IAW ESPM 20-46-50. OPS CHECKED GOOD.

Part: FITTING — CRACKED (FRAME 40) · airframe 17,577 hrs · 10,884 cycles

ONE CRACK INDICATION FITTING AT FRAME 40. REPAIRED IAW REO-G20358 REV D

Part: LAMP — INOPERATIVE (LAVATORY) · airframe 16,652 hrs · 10,319 cycles

INSPECTION TYPE: PS1, LAVATORY MIRROR LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-21.

Part: LIGHT — UNKNOWN (CABIN) · airframe 16,497 hrs · 10,235 cycles

EMERGENCY EXIT LIGHT INOPERATIVE ON ENTRY DOOR. CYCLED LIGHT SWITCHS, OPS CHECKED GOOD IAW AMM 33-51-00-0501.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 16,464 hrs · 10,216 cycles

INSPECTION TYPE: PS1, EMERGENCY EXIT LIGHT INOPERATIVE. TERMINATED PINS ON ENTRY DOOR CONNECTOR WIRES IAW WDM 33-51-05 AND SWPM 20-48-25. INSTALLED NEW SIGN IAW AMM 33-51-13-0401. OPS CHECKED NORMAL.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 16,073 hrs · 9,956 cycles

INSPECTION TYPE: 5YR, FWD LWR CARGO DOOR SKIN CRACKED AT FR 21. REPAIRED IAW EO A300-5230-41004-A.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 16,073 hrs · 9,956 cycles

INSPECTION TYPE: 5 YR, FWD LWR CARGO DOOR SKIN CRACKED AT FR 21. REPAIRED IAW EO A300-5230-41004-A.

Part: STRUCTURE — CONTAMINATED (LT ELEVATOR) · airframe 16,073 hrs · 9,956 cycles

INSPECTION TYPE:5 YR, TRAPPED WATER INDICATIONS FOUND 2 EA LT ELEVATOR UPPER SURFACE INBD OF ER13 IN INSPECTION AREA NR 4, LT ELEVATOR ASSY REPLACED ON NR 040460.

Part: STRUCTURE — CONTAMINATED (LT ELEVATOR) · airframe 16,073 hrs · 9,956 cycles

INSPECTION TYPE:5 YR, TRAPPED WATER INDICATION FOUND LT ELEVATOR UPPER SURFACE OTBD OF OTBD ER2 IN INSPECTION AREA NR 1 REPLACED LT ELEVATOR ASSY ON 040460.

Part: STRUCTURE — CONTAMINATED (RT ELEVATOR) · airframe 16,073 hrs · 9,956 cycles

INSPECTION TYPE: 5 YR, RIGHT ELEVATOR UPPER INSPECTION AREA 6, BETWEEN ER16 & ER18. 4(EA) TRAPPED WATER INDICATIONS FOUND & MARKED IN BLACK. RT ELEVATOR ASSY REPLACED ON NR 040410.

Part: STRUCTURE — CONTAMINATED (RT ELEVATOR) · airframe 16,073 hrs · 9,956 cycles

INSPECTION TYPE:5 YR, RT ELEVATOR UPPER INSPECTION AREA 4 BETWEEN ER10 & ER13. 3(EA) TRAPPED WATER INDICATIONS FOUND & MARKED IN BLACK. RIGHT ELEVATOR REPLACED ON NR 040462.

Part: STRUCTURE — CONTAMINATED (RT ELEVATOR) · airframe 16,073 hrs · 9,956 cycles

INSPECTION TYPE: 5 YR, RIGHT ELEVATOR UPPER INSPECTION AREA 5, BETWEEN EF13, ER16. 3(EA) TRAPPED WATER INDICATIONS FOUND AND MARKED IN BLACK. RT ELEVATOR ASSY REPLACED ON NR 040410.

Part: BRACKET — CORRODED (NR 1 NACELLE) · airframe 16,073 hrs · 9,956 cycles

INSPECTION TYPE: 5 YR, NR 1 PYLON OTBD SIDE METAL ATTACH FITTING CORRODED AT RIB 7. REPLACED FITTING.

Part: BRACKET — CORRODED (NR 1 NACELLE) · airframe 16,073 hrs · 9,956 cycles

INSPECTION TYPE: 5YR, NR 1 PYLON OTBD SIDE METAL ATTACH FITTING CORRODED AT RIB 7 REPLACED FITTING.

Part: CROSSBEAM — CORRODED (FRAME 65) · airframe 16,073 hrs · 9,956 cycles

INSPECTION TYPE: 5YR, FR 65 CROSSBEAM CORRODED BEYOND SRM LIMITS REPAIRED IAW EO A300-5310-57841-A.

Part: PRESSURE PANEL — CORRODED (FRAMES 39-40) · airframe 16,073 hrs · 9,956 cycles

INSPECTION TYPE: 5YR, FWD LOWER CARGO COMPARTMENT HORIZONTAL PRESSURE PANEL NR 6 STRINGER CORRODED FR 39-FR 40; LBL 203-LBL 209. REMOVED CORROSION, TREATED AND PRIMED IAW EO A300-5310-57833-A.

Part: FLOOR SUPPORT — CRACKED (FRAMES 79-1589.5) · airframe 16,073 hrs · 9,956 cycles

INSPECTION TYPE: 5YR, MAIN CABIN UNDER FLOOR, CROSSBEAM LT FR 79-FR 1589.5 HAS CRACKED ANGLE FABRICATED NEW ANGLES IAW EO A300-5310-57761-A.

Part: FLOOR SUPPORT — CRACKED (FRAMES 79-1589) · airframe 16,073 hrs · 9,956 cycles

INSPECTION TYPE:5YR, MAIN CABIN UNDER FLOOR, CROSSBEAM RT FR 79-FR 1589.5 HAS CRACKED ANGLE FABRICATED NEW ANGLES IAW EO A300-5310-57761-A.

Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 16,072 hrs · 9,955 cycles

INSPECTION TYPE: 5YR, MAIN CABIN FLOORBEAM FRAME 79 +Y1580 HAS SUSPECTED CRACK. REPAIRED IAW EO A300-5310-57228A.

Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 16,072 hrs · 9,955 cycles

INSPECTION TYPE: 5YR, MAIN CABIN FLOORBEAM RT FRAME 79 -Y1580 HAS SUSPECTED CRACK. REPAIRED IAW EO A300-5310-57728-A.

Part: PITOT TUBE — CLOGGED (STBY AIRSPEED)

DURING TAKEOFF ROLL, CAPTAIN`S AND F/O`S STANDBY AIRSPEED INDICATORS MALFUNCTIONED. CAPTAIN`S AND F/O PRIMARY AIRSPEED INDICATOR OPERATED NORMALLY AT 240 KIAS CAPT AND F/O STBY AIRSPEED INDICATED 95 KNOTS. FOUND STBY AIRSPEED PITOT TUBE PLUGGED. R & R STBY PITOT TUBE 42DA IAW AMM 34-11-15 C/W LEAK TEST IAW AMM 34-10-00-501. OPS AND LEAK CK NORMAL

Part: LIGHT — UNKNOWN (CABIN)

EMERGENCY EXIT LIGHTS INOPERATIVE. PERFORMED ADJUSTMENT AND TEST OF EMERGENCY LIGHTING IAW MM 33-51-00-501. SYSTEM OPERATES NORMALLY.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 15,002 hrs · 9,239 cycles

3C INSPECTION, LT ELEVATOR CUTOUT HAS SKIN DAMAGED AROUND SCREW HOLE AT INBD SIDE. REPAIRED LT ELEVATOR IAW EO 5520-54150-A AND EA 300-5520-01-A5275 IR.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 15,002 hrs · 9,239 cycles

3C INSPECTION, RT WING INNER FLAP UPPER SKIN AT RIB 1C, AFT OF FRONT SPAR GOUGED AND CRACKED. REPAIRED FLAP SKIN IAW STASA EA 300-5750-01-A5279-IR AND EO A300-5750-54171-A.

Part: LIGHT — MALFUNCTIONED (CABIN)

EMERGENCY EXIT LIGHT FLICKERS ON AND OFF ABOVE CABIN DOOR. PERFORMED OPS TEST OF DOOR EXIT SIGN IAW MM 33-51-13-0401. OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHT ABOVE ENTRY DOOR IS INTERMITTENT. GOES ON AND OFF AS TAXIING, OFF PRIOR TO TAKE OFF AND THEN WHILE TAXIING. LAMPED EXIT LIGHT AND OPS CHECKED GOOD IAW AMM 33-51-13-0401.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 12,918 hrs · 7,924 cycles

INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD NR 231QH HAS HONEYCOMB DAMAGE AT LOWER SURFACE. FABRICATED MAIN CABIN FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B

Part: FLOORBOARD — CORRODED (MAIN CABIN) · airframe 12,918 hrs · 7,924 cycles

INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD NR 231MJ HAS RUSTED INSERTS. FABRICATED MAIN CABIN FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 12,918 hrs · 7,924 cycles

INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD NR 222CG LOWER SKIN IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — BROKEN (MAIN CABIN) · airframe 12,918 hrs · 7,924 cycles

INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD NR 232HG IS BROKEN OFF AT CORNER. FABRICATED MAIN CABIN FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 12,918 hrs · 7,924 cycles

INSPECTION TYPE:SV, MAIN CABIN FLOORBOARD NR 232NG IS DELAMINATED AT CORNER. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOOR SUPPORT — CORRODED (MAIN CABIN) · airframe 12,918 hrs · 7,924 cycles

INSPECTION TYPE: SV, MAIN CABIN FLOOR SUPPORT HAS COROSION AT FR13A TO FR 17 AT Y1959. ACCOMPLISHED REPAIR ON MAIN CABIN FLOOR SUPPORT AT FR13A TO FR 17 AT Y1959 IAW EO A300-5310-46758-A, PARA 6A.

Part: VALVE — MALFUNCTIONED (REFUEL)

ONE HOUR AFTER TAKE OFF, NOTICED LT OUTER FUEL QTY HAD DECREASED 900 LBS. FOLLOWED QRH PROCEDURES. SUSPECTED FUEL LEAK. TURNED OFF FUEL BOOST PUMPS, TANK WOULD CONTINUE TO DECREASE ANOTHER 350 LBS. DIVERTED AND LANDED. SWAPPED LEFT OTBD FUEL REFUEL VALVE IAW MM 28-25-12-04 & GMM 03-32-01 WITH CENTER TANK VALVE FOR TROUBLE SHOOTING PURPOSES. VALVE IN LT OTBD TANK OPS CHECKED NORMAL IAW MM 28-25-12-04.

Part: SKIN — DAMAGED (FUSELAGE)

SKIN DOUBLER DAMAGED S-45/S44R, FRAME 85. REPLACED DOUBLER IAW EO A300-5320-45890-B.

Part: SKIN — DENTED (FUSELAGE)

SKIN DENTED FWD OF FRAME 58 AT STA 34R/35R. REPAIRED IAW EO A300-5330-42566-B.

Part: WARNING LIGHT — INOPERATIVE (EVAC SLIDE)

EVACUATION SLIDE WARNING LIGHT INOP DEFERRED IAW MEL 52-72-01-1. ASSIGNED D448139. PLACARD INSTALLED. WARNING BUZZER IS OPERATIVE.

Part: WARNING LIGHT — INOPERATIVE (ESCAPE SLIDE)

EVACUATION SLIDE WARNING LIGHT INOP. DEFERRED IAW MEL 52-72-01-1. ASSIGNED M448319. PLACARD INSTALLED. WARNING BUZZER IS OPERATIVE. RESET CONNECTOR 70WN A ON ASPU W/R/T ACMX AMB 3 52 08 02 4 AND CHECKED SYS W/R/T MM 52 73 11 04 PARA 2 D AND ASPU BITE CK W/R/T MM 52 73 00 Q5. NO FAULTS NOTED. THIS CLEARS M448319, PLACARD REMOVED.

Part: SLIDE — UNKNOWN (COCKPIT)

SLIDE WILL NOT DISARM. OPERATED SLIDE ARM/DISARM THROUGH SEVERAL TIMES. NO FAULTS NOTED. PERFORMED FUNCTIONAL TEST OF SLIDE RELEASE MECHANISM IAW MM 52-10-30-05. NO FAULTS NOTED. ESCAPE SLIDE WARNING, ALSO OPS CK NORMAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

EXIT LIGHT FLICKERS ON AND OFF WITH LANDING GEAR DOWN. RELAMPED 7 EA BULBS IN EMERG EXIT SIGN REF IPC 33-51-04 FIG 09B. OPS CK GOOD REF TO 33-51-13-04.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, EXFOLIATED SEAT TRACK LBL 31 BETWEEN FR79-80. CUT OUT DAMAGED SEAT TRACK, FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK SECTION IAW SRM 53-10-16, FIG 201, PARA.4.

Part: SEAT TRACK — CORRODED (RBL 31 FR 79-80) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, EXFOLIATED SEAT TRACK, RBL 31 BETWEEN FR 79-80. CUT OUT DAMAGED SEAT TRACK, FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK SECTION IAW SRM 53-10-16 FIG 201, PARA 4.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, EXFOLIATED SEAT TRACK, LBL 44 BETWEEN FR 79-80. CUT OUT DAMAGED SEAT TRACK, FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK SECTION IAW SRM 53-10-16 FIG 201, PARA 4.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, EXFOLIATED SEAT TRACK LBL 17 BETWEEN FR 79-80. CUT OUT DAMAGED SEAT TRACK, FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK SECTION IAW SRM 53-10-16 FIG 201, PARA.4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, EXFOLIATED SEAT TRACK, RBL 17 BETWEEN FR 79-80. CUT OUT DAMAGED SEAT TRACK, FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK SECTION IAW SRM 53-10-16 FIG 201, PARA.4.

Part: FLOORBOARD — DELAMINATED (AFT CARGO BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, AFT CARGO COMP PANEL NR 151NG HAS DELAMINATION FABRICATED AFT CARGO FLOORBOARD NR 151NG IAW EO A300-5320-16407-D, APPENDIX C.

Part: FLOORBOARD — PUNCTURED (AFT CARGO BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, AFT CARGO FLOORBOARD PANEL NR 151SF HAS A PUNCTURE. FABRICATED AFT CARGO FLOORBOARD NR 151SF IAW EO A300-5320-16407-D, APPENDIX C.

Part: FLOORBOARD — DELAMINATED (FWD CARGO BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, FWD PIT FLOORBOARD PANEL 132PG DELAMINATED AT CORNER (FWD) ACCOMPLISHED REPAIR ON FWD PIT FLOORBOARD 132PG IAW EO A300-5320-38221-B.

Part: FLOORBOARD — PUNCTURED (FWD CARGO BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, FWD CARGO FLOORBOARD PANEL NR 132FE HAS A PUNCTURE. ACCOMPLISHED REPAIR ON FWD CARGO FLOORBOARD NR 132FE IAW EO A300-5320-38221-B.

Part: FLOORBOARD — PUNCTURED (FWD CARGO BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, FWD PIT FLOORBOARD PANEL 131BH HAS A PUNCTURE ACCOMPLISHED REPAIR ON FWD PIT FLOOR BOARD 131BH IAW EO A300-5320-38221-B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 242YK IS CRACKED IN (2) PIECES. FABRICATED MAIN CABIN FLOORBOARD NR 242YK IAW EO A300-5320-16407-D, APPENDIX B.

Part: FLOORBOARD — PUNCTURED (FWD CARGO BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, FWD PIT FLOORBOARD NR 132QT HAS PUNCTURES. FABRICATED FWD CARGO FLOORBOARD NR 132QT IAW EO A300-5320-16407-D, APPENDIX C.

Part: FLOORBOARD — PUNCTURED (AFT CARGO BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, AFT CARGO COMPARTMENT FLOORBOARD NR152VF IS PUNCTURED. ACCOMPLISHED REPAIR ON AFT CARGO COMPARTMENT FLOORBOARD NR 152VF IAW EO A300-5320-38221-B.

Part: FLOORBOARD — CRACKED (AFT CARGO BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, AFT CARGO FLOORBOARD 151UF HAS A CRACK. ACCOMPLISHED REPAIR ON AFT CARGO FLOORBOARD 151UF IAW EO A300-5320-38221-B.

Part: FLOORBOARD — PUNCTURED (AFT CARGO BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR AFT CARGO FLOORBOARD PANEL 151LG HAS PUNCTURES ACCOMPLISHED REPAIR ON AFT CARGO FLOORBOARD 151LG IAW EO A300-5320-38221-B.

Part: FLOORBOARD — PUNCTURED (AFT CARGO BAY) · airframe 10,686 hrs · 6,716 cycles

INSPECTION TYPE:10YR, AFT CARGO FLOORBOARD 151KG HAS A PUNCTURE ACCOMPLISHED REPAIR ON AFT CARGO FLOORBOARD 151KG IAW EO A300-5320-38221-B.

Part: FLOORBOARD — PUNCTURED (MAIN CARGO BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, MAIN CARGO FLOORBOARD 251LJ IS PUNCTURED. ACCOMPLISHED REPAIR ON AFT FLOORBOARD 251LJ IAW EO A300-5320--38221-B.

Part: FLOORBOARD — DEBONDED (MAIN CARGO BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT FLOORBOARD NR 251LG IS DISBONDED. ACCOMPLISHED REPAIR ON MAIN CARGO COMPARTMENT FLOORBOARD NR 251LG IAW EO A300-5320-38221-B.

Part: FLOORBOARD — DEBONDED (MAIN CABIN) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOOR PANEL 241KF LOWER SKIN DEBONDED, CORE EXPOSED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOOR PANEL NR 241KF LOWER SKIN IAW EO A300-5320-38221-B.

Part: FLOORBOARD — DELAMINATED (MAIN CARGO BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT FLOORBOARD NR 251XJ IS DISBONDED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 251XJ IAW EO A300-5320-38221-B.

Part: FLOORBOARD — PUNCTURED (MAIN CARGO BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 251BF IS PUNCTURED AT AFT INBD SIDE. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 251BF IAW EO A300-5320-38221-B.

Part: FLOORBOARD — CRACKED (MAIN CARGO) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT FLOORBOARD 251GJ AFT OTBD CORNER IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CARGO FLOORBOARD NR251GJ IAW UPS EO A300-5320-38221-B.

Part: FLOOR PANEL — CRACKED (MAIN CARGO BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOOR PANEL 241RN IS CRACKED ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 241RN IAW UPS EO A300-5320-38221-B.

Part: FLOORBOARD — DEBONDED (MAIN CARGO BAY) · airframe 10,686 hrs · 6,716 cycles

INSPECTION TYPE:10YR, MAIN CARGO FLOORBOARD 251DF FWD EDGE IS DEBONDED ACCOMPLISHED REPAIR ON MAIN CARGO FLOORBOARD 251DF IAW EO ZL-251-04-1-L-251.

Part: FLOORBOARD — PUNCTURED (MAIN CARGO BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT FLOORBOARD NR252KG IS PUNCTURED. ACCOMPLISHED REPAIR ON MAIN CARGO COMPARTMENT FLOORBOARD NR 252KG IAW EO A300-5320-38221-B.

Part: FLOORBOARD — DEBONDED (MAIN CARGO BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT FLOORBOARD NR 251 LJ IS DISBONDED AT AFT EDGE. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 251LJ IAW EO A300-5320-38221-B.

Part: FLOORBOARD — CRACKED (MAIN CABIN BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, MAIN DECK CARGO COMPARTMENT FLOOR PANEL NR 242HF IS CRACKED AT FR 34 TO FR 37 RT SIDE. ACCOMPLISHED REPAIR ON MAIN CARGO COMPARTMENT FLOORBOARD NR 242HF IAW EO A300-5320-38221-B.

Part: FLOORBOARD — DELAMINATED (MAIN CARGO BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR MAIN DECK CARGO COMPARTMENT FLOORBOARD NR 242LT IS PEELED OFF AT EDGE AS MARKED AT FR 34 TO FR 37 RT SIDE. ACCOMPLISHED REPAIR ON MAIN CARGO FLOORBOARD NR 242LH IAW EO A300-5320-38221-B.

Part: FLOORBOARD — DEBONDED (MAIN CARGO BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, MAIN CARGO COMPT FLOORBOARD NR 251XG FWD EDGE IS DEBONDED. ACCOMPLISHED REPAIR ON MAIN CARGO COMPARTMENT FLOORBOARD NR 251XG IAW EO A300-5320-38221-B.

Part: FLOORBOARD — CRACKED (MAIN CARGO BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT FLOORBOARD NR 251FM IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CARGO COMPARTMENT FLOORBOARD NR 251FM IAW EO A300-5320-38221-B.

Part: FLOORBOARD — BROKEN (MAIN CABIN) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT FLOORBOARD NR 252LM SEGMENT IS BROKEN OFF. FABRICATED MAIN CABIN FLOORBOARD NR 252LM IAW EO A300-5320-16407-D, APPENDIX B.

Part: FLOORBOARD — DEBONDED (MAIN CARGO BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT FLOORBOARD NR 251KJ IS DISBONDED AT FWD OTBD CORNER. ACCOMPLISHED REPAIR ON MAIN CARGO FLOOR PANEL NR 251KJ IAW EO A300-5320-38221-B.

Part: FLOORBOARD — BROKEN (MAIN CARGO BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, MAIN CARGO COMPT FLOORBOARD 251HM OTBD AFT CORNER BROKEN. ACCOMPLISHED REPAIR ON MAIN CARGO FLOORBOARD 251HM IAW EO A300-5320-38221-B.

Part: SEAT TRACK — CORRODED (FR 79-80 RBL 45) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, CORROSION ON SEAT TRACK UPPER SURFACE BETWEEN FR 79-80 RBL 45. CUT OUT DAMAGED SEAT TRACK, FABRICATED AND INSTALLED REPLACEMENT SECTION OF SEAT TRACK IAW SRM 53-10-16 PB 201 PARA 4, FIG 201.

Part: SEAT TRACK — CORRODED (FR 79-80 BL0) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, EXFOLIATED SEAT TRACK AT MAIN DECK FLOOR SUPPORT BETWEEN FR 79-80 BL 0. CUT OUT DAMAGED SEAT TRACK, FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK SECTION IAW SRM 53-10-16 PB 201, PARA 4, FIG 201.

Part: FLOORBOARD — DELAMINATED (MAIN CARGO BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, MAIN CARGO FLOORBOARD NR 262PF IS DELAMINATED ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 262PF IAW UPS EO A300-5320-38221-B.

Part: FLOORBOARD — BROKEN (MAIN CARGO BAY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, MAIN CARGO FLOORBOARD NR 262BH IS BROKEN AT OTBD CORNER ACCOMPLISHED REPAIR IAW ON MAIN CARGO FLOORBOARD NR 262BH IAW UPS EO A300-5320-38221-B.

Part: MOUNT — ELONGATED (GALLEY) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, COURIER COMPT FWD GALLEY UPPER RT MOUNT FITTING INBD AND OTBD LUGS ARE ELONGATED AND PIN HAS EXCCESSIVE PLAY. REPAIRED FWD GALLEY UPPER RT MOUNT FITTING IAW EA 300-2520-01-A2527-I/R.

Part: SKIN — SCRATCHED (RT INBD FLAP) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, RT WING INBD FLAP UNDER SURFACES T/E HAS 4EA SCRATCHES ABOUT 8 TO 11 INCHES WITHIN EACH OTHER. ACCOMPLISHED REPAIR IAW EO A300-5750-38698-A AND STA-SA, EA 300-5750-01-A2525, REV I/R.

Part: SKIN — DENTED (BS 794) · airframe 10,868 hrs · 6,716 cycles

INSPECTION TYPE:10YR, 2EA ROUND BOTTOM DENTS IN LT FWD FUSELAGE EXTERIOR APPROX. STA 794. CUT OUT DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR IAW SRM 53-11-12 PARA 5A FIG 201 AND 51-70-20-001.

Part: SKIN — MISREPAIRED (AILERON) · airframe 9,763 hrs · 6,041 cycles

INSPECTION TYPE:1C REPAIR SURVEY SEQ 126-W4-01 DOES NOT CORRELATE WITH SRM. REMOVED EXISTING REPAIR ON RT ALL SPEED AILERON LOWER SURFACE BETWEEN RIBS 15-16, 7.5 INCHES AFT OF REAR SPAR ON T/E. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF A300-600 SRM 51-77-12, PARA 5D AND FIG 226.

Part: SKIN — GOUGED (FUSELAGE) · airframe 9,763 hrs · 6,041 cycles

INSPECTION TYPE:1C2C REPAIR SURVEY SEQ 126-F1-05 DOUBLER UNDER TAIL BALL IS GOUGED IN SEVERAL PLACES. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW A300 SRM 53-10-12 FIG 210.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 9,763 hrs · 6,041 cycles

INSPECTION TYPE:4C REPAIR SURVEY SEQUENCE 126-F1-04 HAS A BLENDOUT .75 X .75 INCH AT FWD I/B CORNER OF DOUBLER. DOUBLER IS LOCATED JUST FWD OF TAIL BALL. REMOVED, FABRICATED AND INSTALLED NEW REPAIR DOUBLER SRM 53-10-12 FIG 208 SHEET 1.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 9,763 hrs · 6,041 cycles

INSPECTION TYPE:4C REPAIR SURVEY 126-W3-02, CENTER FLAP UPPER SURFACE REPAIR DOUBLER GOUGED, LT WING. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER PER A300-600 SRM 57-50 00 PAGE 220 FIGURE 205.

Part: FLOOR PANEL — MISREPAIRED (CARGO BAY) · airframe 9,763 hrs · 6,041 cycles

INSPECTION TYPE:4C BULK PIT FLOORBOARD 161HF PREVIOUS REPAIR NOT IN ACCORDANCE WITH SRM. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-C, APPX D.

Part: FLOOR PANEL — MISREPAIRED (CARGO BAY) · airframe 9,763 hrs · 6,041 cycles

INSPECTION TYPE:4C MAIN CARGO COMPARTMENT FLOORBOARD 252EN PREVIOUS REPAIR NOT IN ACCORDANCE WITH A300 SRM. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-C, APPX B.

Part: FLOOR PANEL — MISREPAIRED (CARGO BAY) · airframe 9,763 hrs · 6,041 cycles

INSPECTION TYPE:4C MAIN CARGO COMPARTMENT FLOORBOARD 252UJ PREVIOUS REPAIR NOT PER SRM. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-C, APPX B.

Part: FLOOR PANEL — MISREPAIRED (MAIN CABIN) · airframe 9,763 hrs · 6,041 cycles

INSPECTION TYPE:4C MAIN CABIN FLOORBOARD 252BN PREVIOUS REPAIR NOT PER A300 SRM. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-C, APPX B.

Part: LENS — BROKEN (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHT LENS BROKEN RED D387788. REMOVED AND REPLACED LENS ASSY PER M/M 33-51-17-04.

Part: WINDSHIELD — FAILED (COCKPIT)

CAPTAIN'S WINDSHIELD SHATTERED IN FLIGHT. REMOVED AND REPLACED LEFT CAPTAIN'S WINDSHIELD WITH REF TO MM 56-11-11-04. WINDOW HEAT OPS CHECKS GOOD.

Part: LIGHT — MALFUNCTIONED (COCKPIT)

INSPECTION TYPE:N/A AT CRUISE WITH SWITCH IN -ARM- POSITION DOOR EXIT LIGHT WAS ON. PERFORMED OPS TEST OF AUTOMATIC EXIT SIGN ACTIVATION PER MM 33-51-00-05. NO DEFECTS FOUND.

Part: WATER SEPARATOR — ODOR

AFTER 4 FLT HOURS HYD FUMES PRESENT. BOTH CREW MEMBERS EXPERIENCED MILD EYE, NOSE AND THROAT IRRITATION. FOUND REDUCING FLOW WITH LEFT PACK OFF HELPED. NO IMPROVEMENT IN FUME LEVEL. REMOVED AND REPLACED LT AND RT WATER SEPARATOR COALESER WITH THE ENG RUNNING. SMELL APPEARS TO GO AWAY. SMELL CAME BACK WITH THE APU RUNNING. PURGED SENSE LINES ON BLUE, GREEN AND YELLOW SYS RESERV OF HYD FLUID (RESIDUAL). REMOVED AND REPLACED BOTH WATER SEP BAGS PER MM 21-51-16-4. GROUND RAN ENGS. PURGED SENSE LINES BETWEEN YELLOW SYS AND PACKS PER MM 20041-11-00. OPS CK GOOD.

Part: GIRT BAR — MISINSTALLED (DOOR SLIDE)

SLIDE ARMING LEVER WILL NOT MOVE DEFERRED PER MEL 52-11-01-3 TO CONTROL NR 330338. DMP 52-11-01-3 C/W. REINSTALLED FWD ENTRY DOOR SLIDE GIRT BAR CORRECTLY. DOOR AND SLIDE OPERATION NORMAL IAW MM 25-61-04. OPS CK NORMAL. PLACARD REMOVED.

Part: LIMIT SWITCH — DEFECTIVE (EVAC SLIDE)

INSPECTION TYPE:N/A SLIDE ARMS INTERMITTENTLY. SOMETIMES TAKES 2 OR 3 TRIES TO GET SLIDE TO ARM CORRECTLY. R&R WARNING LIGHT LIMIT SWITCH IAW ESPM 20-45-25 TESTED GOOD. P/N OFF-ON ABS0309-03.

Part: SLIDE — INTERMITTENT

ESCAPE SLIDE "SLIDE" WORD IN WHITE ON ECAM DOOR PAGE IS INTERMITTENT WHEN SLIDE IS INITIALLY ARMED. AT FIRST THERE IS NO INDICATION AND THEN THE WORD "SLIDE" BLINKS ON AND OFF BEFORE FINALLY STAYING ON. DFRD ECAM SLIDE IND SYS IAW MEL 52-30-04. DMI 326989 OPEN. CHECKED ADJUSTMENT OF LIMIT SWITCH "13WN" IAW AMM 52-73-13-5. FOUND SATISFACTORY, OPS CHECKED ESCAPE SLIDE ARM HANDLE WITH IND NO FAULTS FOUND. THIS CLEARS DMI 326989.

Part: SLIDE — DEPLOYED (CABIN)

INSPECTION TYPE:N/A EMERGENCY SLIDE DEPLOYED. INSTALLED SERVICEABLE ESCAPE SLIDE IAW AMM 25-61-21-4.

Part: SLIDE — WILL NOT TEST (PAX DOOR)

FWD ENTRY DOOR EMERGENCY ESCAPE SLIDE EVACUATION SLIDE WARNING HORN SYS WILL NOT TEST; LIGHTS OK. EMERGENCY ESCAPE SLIDE WARNING HORN INOP; DEFERRED PER MEL 52-73-01-2-4. EMERGENCY DOOR TEST BUTTON SEEMS TO HAVE STICKY SUBSTANCE IN BUTTON CLEANED BUTTON WITH CONTACT CLEANER. BUZZER AND LIGHT WORKS OK. THIS CLEARS M304686.

Part: WARNING SYSTEM — INOPERATIVE (ESCAPE SLIDE)

FWD ENTRY DOOR EVACUATION SLIDE WARNING SYSTEM BUZZER INOPERATIVE. LIGHTS INOPERATIVE. CYCLED POWER. TESTED WARNING SYSTEM. CHECKS GOOD IAW 52-20-00.

Part: LIGHT — INOPERATIVE (EVAC SLIDE)

DURING PREFLIGHT TEST OF EMERGENCY EVACUATION SLIDE, THE AURAL SOUND WORKS BUT THE LIGHT DOES NOT ILLUMINATE. RESET ASPSU IAW MM 52-73-18-4. DEFERRAL CLEARED.

Part: HANDLE — STIFF (ESCAPE SLIDE)

SLIDE ARMING HANDLE ONLY MOVES HALF DISTANCE TO ARMED POSITION. EXERCISED HANDLE UNTIL FREE. NO ADDITIONAL BINDING NOTED. OK FOR CONTINUED SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

EXIT SIGN ABOVE CREW ENTRY DOOR IS INOP. EMERGENCY LIGHTS TEST IS SHOWING FAULT. RELAMPED ALL 9 LAMPS IN EXIT SIGN 31WL1.

Part: WARNING HORN — INOPERATIVE (EVAC SLIDE)

INSPECTION TYPE:N/A EVAC SLIDE WARNING BUZZER INOP M279503. REMOVED & REPLACED ASPSU PER AMM 52-73-18-4, CHECKED GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN)

INSPECTION TYPE:IN EVACUATION SLIDE WARNING SYSTEM LIGHTS INOP WARNING BUZZER OPERATES NORMALLY. DEFERRED M210809. REPLACED AUTONOMOUS STANDBY POWER SUPPLY UNIT PER AMM 527318.