N154UP

Part: LIGHT — INTERMITTENT (ZONE 200) · airframe 25,983 hrs · 15,510 cycles

LT OTBD CEILING LIGHT OUT SUPERNUMERARY AREA. PERFORMED OPS CK IAW AMM 33-21-00-501. TESTS GOOD.

Part: CONTROL HANDLE — INOPERATIVE (ZONE 700) · airframe 25,983 hrs · 15,510 cycles

AFTER T/O GEAR HANDLE SELECTED UP-GEAR DID NOT RETRACT. PER ECAM PLACED TO SYS#2 AND GEAR RETRACTED NORMALLY. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW AMM 32-31-11/401. OPS TEST GOOD. QA REPORTED GEAR SWING IS BEST PRACTICE BUT NOT REQUIRED. SUPERVISION OPTED NOT TO DO GEAR SWING. THIS CLEARS MEL. PLACARD REMOVED.

Part: WINDSHIELD — DELAMINATED (ZONE 200) · airframe 25,685 hrs · 15,351 cycles

SERIOUS DELIMITATION ON CAPT SIDE FRONT WINDSHIELD DELIMITATION INDICATES POSSIBLE EVIDENCE OF ARCING DELAMINATION ON CAPTAIN WINDSHIELD WAS FOUND TO BE WITHIN LIMITS IAW AMM 56-11-11/601

Part: GROUND WIRE — UNLOCKED (DOOR SLIDE) · airframe 25,427 hrs · 15,222 cycles

DURING OPERATIONAL CHECK OF ESCAPE SLIDE WARNING LIGHT AND ANNUNCIATOR, BOTH THE LIGHT AND ANNUNCIATOR ARE NOT WORKING. PERFORMED FAULT ISOLATION IAW AMM 52-73-01 PAGE 5, DURING THE WIRING CHECK THE GROUND LINE IN THE TERMINAL BLOCK 6035VT CONTACT "B" FOUND UNLOCK , THE CONTACT "B" LOCKED IAW ESPM 20-48-20-02, OPS CHECK GOOD IAW AMM 52-10-00/301.

Part: ANNUNCIATOR — INOPERATIVE (ZONE 800) · airframe 25,427 hrs · 15,222 cycles

DURING OPERATIONAL CHECK OF ESCAPE SLIDE WARNING LIGHT AND ANNUNCIATOR, BOTH THE LIGHT AND ANNUNCIATOR ARE NOT WORKING.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 25,427 hrs · 15,222 cycles

AFT CARGO FR 54 RH SIDE HAS A CRACKED FLOOR SUPPORT ANGLE DOT 07586-02. INSTALLED FLOOR SUPPORT ANGLE AT AFT CARGO FR54 RH SIDE IAW A300-600 SRM 51-40-21. FASTENERS P/N:DAN5-6-6, BATCH:0004085822, P/N:BACC30M5, BATCH:0004143638, P/N:MS21060-3, BATCH:0004201914, P/N:CCR264SS3-07, BATCH:0004149148.

Part: WEB — CRACKED (ZONE 100) · airframe 25,427 hrs · 15,222 cycles

LH SIDE OF THE E&E BAY HAS A CRACKED WEB BETWEEN FR 11 - 12 DOT 07586-01. INSTALLED WEB NEW P/N: UP513100-1.IAW A300-600 SRM 51-40-21.

Part: UNKNOWN — NOISE (ZONE 100) · airframe 25,369 hrs · 15,195 cycles

DURING CLIMB THROUGH 10,000 EXPERIENCED A VERY LOUD NOISE AND VIBRATION WITH A TEMPORARY BURNING SMELL THAT LASTED APPROX TWO MINUTES. SUSPECT NOSE WHEEL ROTATION. EMERGENCY DECLARED, PERFORMED GVI OF AIRFRAME, NOSE WHEEL AND WHEEL WELL, FLIGHT BRAKE BAND. TIRE PRESSURES NORMAL. ALSO PERFORMED GVI OF EE BAY. RAN BOTH PACKS NO ABNORMALTIES.GMM 05-00-00, OK FOR SERVICE.

Part: OIL SYSTEM — LOW PRESSURE (NR 1 ENGINE) · airframe 24,606 hrs · 14,744 cycles

*** DIVERSION *** ENG 1 OIL LO PR ECAM WARNING IMMEDIATELY AFTER LIFT OFF. DETERMINED IT WAS AN ERRONEOUS MESSAGE BASED ON ECAM AND ANALOGUE OIL PRESSURE GAUGES. DIVERT TO CAE WITH BOTH ENGINES OPERATING NORMALLY. OPS CHECKED LOW OIL PRESSURE SWITCH REF AMM 71-00-00, REPLACED RELAY 19ES REF AIRBUS ESPM 20-46-50-1. OPERATED ENGINE AT TAKEOFF POWER, NO LOW OIL PRESSURE LIGHT, PRESSURE FLUCTUATIONS OR ECAM MESSAGES OCCURED. ACFT OK THIS SYSTEM

Part: RELAY — FAULTED (OIL SYSTEM) · airframe 24,610 hrs · 14,748 cycles

ENG 1 OIL LO PR ECAM WARNING IMMEDIATELY AFTER LIFT OFF. DETERMINED IT WAS AN ERRONEOUS MESSAGE BASED ON ECAM AND ANALOGUE OIL PRESSURE GAUGES. DIVERT TO CAE WITH BOTH ENGINES OPERATING NORMALLY. OPS CHECKED LOW OIL PRESSURE SWITCH REF AMM 71-00-00, REPLACED RELAY 19ES REF AIRBUS ESPM 20-46-50-1. OPERATED ENGINE AT TAKEOFF POWER, NO LOW OIL PRESSURE LIGHT, PRESSURE FLUCTUATIONS OR ECAM MESSAGES OCCURED. ACFT OK THIS SYSTEM, DIVERSION

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 23,292 hrs · 13,963 cycles

SLIDE PRESSURE IN RED ZONE. R&R L1 DOOR ESCAPE SLIDE IAW AMM 25-61-21-0401, NO DEFECTS NOTED. PRESSURE GAUGE IS IN THE GREEN .

Part: CEILING PANEL — CRACKED (FWD CARGO) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:C FWD CARGO COMP CEILING SUPPORT STRUCTURE AT FRAME 20 -Y2462 HAS CRACK.REMOVED, REPAIRED, AND INSTALLED IAW SRM 51-40-21.

Part: ADAPTER — DELAMINATED (SEAT TRACK) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:C AFT CABIN SEAT TRACK ADAPTER AT FR 72 BETWEEN Y1456 AND Y1959 EXFOLIATED.REMOVED AND REPLACED CLS ADAPTER IAW-SRM 51-40-21.

Part: CROSSBEAM — BENT (CABIN FR48) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:C CROSSBEAM AT FR48 -Y450 AND -Y953 IS BENT REMOVED AND REPLACED CROSSBEAM IAW SRM 51-40-21

Part: SUPPORT WEB — CRACKED (SUPPORT WEB) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:C L/H MAIN CABIN COMPARTMENT BEHIND LOWER SIDEWALL PANEL BETWEEN FR 38.1 AND FR 38.2 SUPPORT WEB CRACKED.INSTALLED SIDEWALL SUPPORT WEB IAW-SRM 51-40-21.

Part: NONE — CRACKED (CLS ADAPTER) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CCLS ADAPTER AT FRAME 20 FRAME 20 APPROX -Y1959 BROKEN.INSTALLED NEW CLS ADAPTER IAW-SRM 51-40-21.

Part: RIB — CRACKED (L/H HORIZONTAL) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:C L/H HORIZONTAL STAB LEADING EDGE PANEL 331CB O/B RIB CRACKED INSTALLED RIB PANEL 331CB IAW SRM 51-40-21

Part: PLATE — CRACKED (L/H KRUEGER FLAP) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:1CLEFT KRUGER FLAP WING ACCESS PANEL HAS A CRACK ON PANEL PLATE. DOT A-13REMOVED AND REPLACED IAW SRM 51-40-21.

Part: PLATE — ELONGATED (FUSLEAGE) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CL/H PYLON FAIRING PANEL 475AL LH SIDE UPPER EDGE 35EA ELONGATED FASTENER HOLES FWD TO AFT EDGES AS MARKED.INSTALLED NEW PLATE IAW-SRM 5-40-21.

Part: NONE — DAMAGED (E/E COMPARTMENT) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CE/E FLOOR PANEL 122LF FOUND DAMAGEREPAIR IAW SREO A300-5320-42722F

Part: LONGERON — NONE (FUSELAGE) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CR/H PYLON FAIRING PANEL 485AL R/H SIDE UPPER EDGE 35EA ELONGATED FASTENER HOLES FWD TO AFT EDGESINSTALLED NEW LONGERON IAW SRM 51-40-21

Part: BRACKET — BROKEN (POWERPLANT) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:C#1 ENG I/B T/R COWL CIRCUMFERENTIAL LATCH UPPER BRACKET BROKENREMOVED AND REPLACED BRACKET #1 ENG I/B T/R IAW SRM 51-40-21

Part: LONGERON — NONE (FUSELAGE) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CR/H PYLON FAIRING PANEL 485AL L/H SIDE UPPER EDGE 35EA ELONGATED FASTENER HOLES FWD TO AFT EDGESINSTALLED NEW LONGERON IAW SRM 51-40-21

Part: SUPPORT — BROKEN (POWERPLANT) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CENG 2 PYLON SUPPORT WEB BTW PANEL 423AL/424AR AND 423BL CRACKEDINSTALLED SUPPORT WEB IAW SRM 51-40-21

Part: PLATE — NONE (FUSELAGE) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CR/H PYLON FAIRING PANEL 485AL R/H SIDE UPPER EDGE 35EA ELONGATED FASTENER HOLES FWD TO AFT EDGESINSTALLED NEW PLATE IAW SRM 51-40-21

Part: PLATE — NONE (FUSELAGE) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CR/H PYLON FAIRING PANEL 485AL L/H SIDE UPPER EDGE 35EA ELONGATED FASTENER HOLES FWD TO AFT EDGESINSTALLED NEW PLATE IAW SRM 51-40-21

Part: SUPPORT — BENT (FUSELAGE) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CW/W REAR ZONE FLOOR PANEL SUPPORT MIDDLE WEB IS BENTREFORMED SUPPORT WEB 2EA IAW SREO M-5100-41097-41097-E APPENDIX A STEP 11

Part: LONGERON — NONE (FUSELAGE) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:C#1 PYLON FAIRING PANEL 475AL R/H SIDE UPPER EDGE 34EA ELONGATED HOLES FWD TO AFT EDGESINSTALLED NEW LONGERON IAW SRM 51-40-21

Part: PLATE — ELONGATED (FUSELAGE) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CL/H PYLON FAIRING PANEL 475AL R/H SIDE UPPER EDGE 34EA ELONGATED HOLES FWD TO AFT EDGESINSTALLED NEW PLATE IAW SRM 51-40-21

Part: FLOOR PANEL — DAMAGED (LWR CARGO) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CPNL 13ZRG BROKENFABBED PER SREO A300-532-16407-E

Part: FLOOR PANEL — DAMAGED (FWR CARHO) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:C PNL 132SG DAMAGED FABBED PER SREO A3005320-16407-E

Part: FLOOR PANEL — BROKEN (LWR CARGO) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:C PNL 131 RG BROKENFABBED PER SREO A300-5320-16407-E

Part: FLOOR PANEL — DAMAGED (LWR CARGO) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CPNL 132PG DAMAGEDFABBED PER SREO A300-5320-16407-E

Part: FLOOR PANEL — DAMAGED (LWR CARGO) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CPNL 152 SF DAMAGEDFABBED PER SERO A300-5320-6407-E

Part: FLOOR PANEL — DAMAGED (LWR CARGO) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:A300PNL 152NG DAMAGED FABBED PER SREO A300-5320-16407-E

Part: FLOOR PANEL — DAMAGED (LWR CARGO) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:A300PNL 151VF DAMAGEDFABBED PER SREO A300-5320-16407-E

Part: FLOOR PANEL — DAMAGED (LWR CARGO) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:C PN 15ZLG DAMAGE FABBED PER SREO A300-5320-16407-E

Part: BRACKET — CRACKED (LT WING KRUEGER) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CLT WING KRUGER FLAP BOX BEHIND WEB PIN LOWER CHORD HAS 3EA BRACKET CRACKEDREMOVED, FABRICATED AND INSTALLED NEW BRACKETS IAW SRM 57-40-11 AND SRM 51-40-21

Part: FLOOR PANEL — DAMAGED (LWR CARGO) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CPNL 132MG DAMAGEDFABBED PER SREO A300-5320-16407-E

Part: FLOOR PANEL — DAMAGED (LWR CARGO) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CPNL 151KG DAMAGEDFABBED PER SREO A300-5320-16407-E

Part: FLOOR PANEL — CRACKED (LWR CARGO) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CPNL 152VF CRACKED FABBED PER SREO A00-5320-16407-E

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CPNL 252FK IS DAMAGED FABBED IAW SREO A300-5320-40552-B

Part: FLOOR PANEL — CRACKED (ZONE 240) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:A300MDC FLOOR PANEL 242PK CRACKEDREPAIRED MDC FLOOR PANEL 242PK AS NEEDED IAW EO NO A300-5320-42722-F

Part: ANGLE — BROKEN (2 FLAP) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CRT WING 2 FLAP O/B END ANGLE BRACKET BROKEN/MISSINGREMOVED AND REPLACED IAW SRM 51-40-21

Part: FLOOR PANEL — DAMAGED (B53270756001) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CPNL 242LH CRACKED FABBED IAW SREO A300-5320-40552-B

Part: FLOOR PANEL — NONE (ZONE 240) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:A300MDC FLOOR PANEL 241TK HAS HOLEREPAIRED MDC FLOOR PANEL 241TK AS NEEDED IAW E.O NO:A300-5320-42722-F

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:C PNL 241GN BROKEN FABBED IAW SREO A300-5320-40552-B

Part: FLOOR PANEL — CRACKED (ZONE 240) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:A300MDC FLOOR PANEL 242DQ CRACKEDREPAIRED MDC FLOOR PANEL 242DQ AS NEEDED IAW E.O NO:A300-5320-42722-F

Part: FLOOR PANEL — DELAMINATED (ZONE 240) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:A300MDC FLOOR PANEL 242BQ DELAMINATEDREPAIRED MDC FLOOR PANEL 242BQ AS NEEDED IAW E.O NO:A300-5320-42722-F

Part: FLOOR PANEL — PUNCTURED (ZONE230) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:A300MDC FLOOR PANEL 232LF HAS PUNCTUREREPAIRED MDC FLOOR PANEL 232LF AS NEED IAW E.O NO:A300-5320-42722-F

Part: FLOOR PANEL — BROKEN (ZONE 240) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:A300MDC FLOOR PANEL 241FN IS BROKENREPAIRED MDC FLOOR PANEL 241FN AS NEEDED IAW EO NO A300-5320-42722-F

Part: FLOOR PANEL — DELAMINATED (ZONE 240) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:A300MDC FLOOR PANEL 242YK DELAMINATEDREPAIRED MDC FLOOR PANEL 242TK AS NEEDED IAW AE.O NO:A300-5320-42722-F

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:C PNL 252BN BROKEN FABBED IAW SREO A300-5320-40552-B

Part: FLOOR PANEL — BROKEN (ZONE230) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:A300MDC FLOOR PANEL 231RG IS BROKENREPAIRED MDC FLOOR PANEL 231RG AS NEEDED IAW EO NO A300-5320-42722-F

Part: FLOOR PANEL — DELAMINATED (ZONE 240) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:A300MDC FLOOR PANEL 242TK DELAMINATEDREPAIRED MDC FLOOR PANEL 242TK AS NEEDED IAW EO NO:A300-5320-42722-F

Part: FLOOR PANEL — BROKEN (ZONE 230) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:A300MDC FLOOR PANEL 231NJ BROKENREPAIRED MDC FLOOR PANEL 231NJ AS NEED IAW E.O NO:A300-5320-42722-F

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:C PNL 252LJ BROKEN FABBED IAW SREO A300-5320-40552-B

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:C PNL 231SG BROKEN FABBED IAW SREO A300-5320-40552-B

Part: ANGLE — CRACKED (FLIGHT DECK) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CFLIGHT DECK R/H UNDER FLOOR ATTACH ANGLE HAS CRAKED ABOUT 24" OF THE R/H OBSERVOR SEAT AT FR-10REMOVED AND REPLACED IAW SRM 51-40-21

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:C PNL 251VJ BROKEN FABBED IAW SREO A300-5320-40552-B

Part: FLOOR PANEL — PUNCTURED (ZONE 230) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:A300MDC FLOOR PANEL 232TG HAS PUNCTURESREPAIRED MDC FLOOR PANEL 232TG AS NEEDED IAW EO NO:A300-5320-42722-F

Part: NONE — DAMAGED (EE COMPT FLOOR) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CEE COMPT FLOOR PANEL 121PF HAS DAMAGEREPAIR IAW SREO A300-5320-42722-F

Part: NONE — DAMAGED (EE COMPT FLOOR) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CEE COMPT FLOOR PANEL 122LF HAS DAMAGESREPAIR IAW SREO A300-5320-42722-F

Part: WEB — CRACKED (FWD CARGO UNDER) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:1CFWD CARGO UNDER FLOOR LH SIDE BELLOW ROLLERS LINE SUPPORT WEB CRACKED BTW FR20 AND 21 AND FASTENER LOOSE.REMOVED, FABRICATED, AND INSTALLED NEW WEB IAW SRM 53-13-18 AND SRM 51-40-21.

Part: NONE — DAMAGED (EE COMPT FLOOR) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CEE COMPT FLOOR PANEL 121LF DELAMINATIONREPAIR IAW SREO A300-5320-42722-F

Part: WEB — BROKEN (R/H MAIN CABIN) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CRH MAIN CABIN COMPT, BEHIND LOWER SIDEWALL PANEL BETWEEN FRAME 38 AND FRAME 38.1 SUPPORT WEB CRACKED.REMOVED AND REPLACED IAW-SRM 51-40-21

Part: WEB — BROKEN (R/H MAIN CABIN) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CRH MAIN CABIN COMPT, BEHIND LOWER SIDEWALL PANEL BETWEEN FRAME 38 AND FRAME 38.1 SUPPORT WEB CRACKED.REMOVED AND REPLACED IAW-SRM 51-40-21.

Part: DOUBLER — BROKEN (L/H WING) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:A300L/H WING LE CUT OUT OF ACCESS 513 AB HAS CRACKINSTALLED REPAIR DOUBLER A300-600 SRM 51-40-21

Part: WEB — BROKEN (AFT CARGO) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CAFT CARGO FR54 BULKHEAD WEB AT-Y953 LH CRACKED.REMOVED AND REPLACED IAW-SRM 51-40-21.

Part: WEB — BROKEN (AFT CARGO) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CAFT CARGO FR54 BULKHEAD WEB AT Y0 CRACKED.REMOVED AND REPLACED IAW-SRM 51-40-21.

Part: WEB — BROKEN (AFT CARGO) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CAFT CARGO FR54 BULKHEAD WEB AT Y953 LH CRACKED.REMOVED AND REPLACED IAW-SRM 51-40-21.

Part: WEB — BROKEN (AFT CARGO) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CAFT CARGO FR54 BULKHEAD WEB AT Y1959 CRACKED.REMOVED AND REPLACED IAW-SRM 51-40-21.

Part: WEB — BROKEN (AFT CARGO) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CAFT CARGO FR54 BULKHEAD WEB AT Y953 RH CRACKED.REMOVED AND REPLACED IAW-SRM 51-40-21.

Part: BRACKET — BROKEN (2 FLAP O/B) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CLT WING 2 FLAP O/B EDGE ANGLE BRACKET BROKEN / MISSINGREMOVED AND REPLACED IAW SRM 51-40-21

Part: BRACKET — BROKEN (3 FLAP I/B) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CLT WING 3 FLAP I/B EDGE ANGLE BRACKET BROKEN/MISSINGREMOVED AND REPLACED IAW SRM 51-40-21

Part: BRACKET — CRACKED (LT WING BELOW #3) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:ICLT WING BELOW #3 SPOILER I/B HINGE ARM END RIB INTERCOSTAL WEB FWD BRACKET CRACKED.REMOVED, FABRICATED AND INSTALLED BRACKET IAW 57-51-11 AND SRM 51-40-21

Part: ROLLER TRAY — CRACKED (2 FLAP) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CLT WING 2 FLAP TOP SURFACE ROLLER RUB PLATE CRACKE DREMOVED AND REPLACED IAW SRM 51-40-21

Part: BRACKET — BROKEN (ENG 2 I/B TR) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:A300ENG 2 I/B TR HALF BRACKET OF OPENING MANIFOLD ITS CRACKEDREMOVED AND REPLACED BRACKET AT ENG 2 I/B IAW SRM 51-40-21

Part: BRACKET — BROKEN (ENG 2 O/B TR) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:A300ENG 2 O/B TR HALF BRACKET OF OPENING MANIFOLD ITS CRACKEDREMOVED AND REPLACED BRACKET AT ENG 2 O/B IAW SRM 51-40-21

Part: WEB — EXCESS PLAY (WEB) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:1CPYLON #1 REAR LOWER ZONE HYD PRESSURAZATION LINE HAS EXCESSIVE PLAY AT LOWER SPAR.REMOVED, FABRICATED AND INSTALLED NEW WEB IAW SRM 51-31-00, SRM 51-27-11 AND SRM 51-40-21

Part: DOUBLER — DAMAGED (PANEL 424CR) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:C ENGINE PANEL 424CR HAS WEAR DAMAGED AROUND 2 EA FASTENER HOLES.FABRICATED DOUBLER AND FILLER IAW SRM 54-52-51

Part: BRACKET — BROKEN (NLG W/W) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CNLG W/W RH SIDE WALL AFT AREA NOSE LANDING LIGHT WIRING CONDUIT BRACKET BROKEN/DEFORMED.REMOVED, FABRICATED, AND INSTALLED IAW SRM 51-40-21.

Part: SUPPORT ANGLE — CRACKED (LH WING KRUEGER) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:1CLH WING KRUEGER FLAP WELL O/B SIDE WEB SUPPORT CRACKED.REMOVED, FABRICATED AND INSTALLED NEW WEB SUPPORT IAW SRM 51-31-00, SRM 51-70-12 AND SRM 51-40-21

Part: RETAINER — BROKEN (KRUGER FLAP) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CLH KRUGER FLAP UPPER EDGE SEAL RETAINER BROKEN AT O/B END.REMOVD AND REPLACED IAW SRM 51-40-21

Part: RETAINER — CRACKED (RH KRUGER FLAP) · airframe 22,538 hrs · 13,551 cycles

INSPECTION TYPE:CRH KRUGER FLAP WELL FWD O/B CORNER HAS A CRACKED CLIPREMOVD AND REPLACED IAW SRM 51-40-21

Part: NONE — BROKEN (DOORS) · airframe 21,805 hrs · 13,151 cycles

INSPECTION TYPE:N/ADOOR SLIDE PIN BROKE UPON ARRIVALREPLACED PIN IAW IPC 52-11-11-15A. NO FURTHER DEFECTS NOTED

Part: TRANSMITTER — FALSE INDICATION (OIL PRESSURE) · airframe 21,337 hrs · 12,887 cycles

INSPECTION TYPE:N/A**IFSD*ATB*EMERG DECL'D*NO EQUIP USED*AC LANDED UNEVENTFULLY*RED ECAM LO OIL PRESS ON #1 TAKE OFF AT APPROX 400FT. SHUT #1 ENG DWN AT LEVEL OFF & RETURN TO BHM. REF LP 679709 ITEM 2,3 FOR FINDINGS. PRFRMED OPS CHECK AMM 71-00-00-0501. OIL PRESS RECORDED 112 PSI, QTY 16 QTS, OIL TEMP 86C.REPLACED #1 ENG OIL PRESS XMITTER & SWITCH IAW AMM 79-33-11 & 79-34-11. FOUND ALL INDICATION NORMAL. THIS CLEARS DISCREPANCY.

Part: FLOOR PANEL — NOT REPORTED (MAIN DECK) · airframe 21,216 hrs · 12,821 cycles

MAIN DECK FLLOR PANEL 252 HJ NEEDS REPLACEMENTFABRICATED NEW PANEL PER EO A300-5320-16407

Part: CONNECTOR — DAMAGED (CARGO LIGHTING) · airframe 21,216 hrs · 12,821 cycles

INSPECTION TYPE:N/ACONNECTOR 4003VCA ON PANEL 923VU & SURRONDING AREA DAMAGED. ACCOMPLISHED EO A300 2450 80917A PARA 6 MAINTENANCE ACTIONS AND TRANSFERRED TO DEFERRAL #D749223 FERRY PERMIT 9022 ISSUED TO OPERATE ONE TIME FLIGHT FROM PHX TO SDF.REPLACED C/B PANEL 923VU, REF AWM 24-51-05, 24-54-02, & 25-52-04. REPLACED CONNECTOR 4003VCA AND RETERMINATED PINS A,B,C,D & G IAW SWPM 20-48-23. REVERSED MAINTENANCE ACTIONS CALLED OUT IN EO A300 2450 80917-A TO NORMAL CONFIGURATION, NO FUTHER DEFECTS NOTED. THIS CLEARS D749223.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 21,216 hrs · 12,821 cycles

INSPECTION TYPE:N/AMAIN DECK FOOR PANEL 252 XG NEEDS REPLACEMENTFABRICATED NEW FLOOR PANEL PER EO A300-5320-16407

Part: HYDRAULIC SYSTEM — FLUID LOSS (GREEN) · airframe 20,084 hrs · 12,203 cycles

INSPECTION TYPE: N/A DIVERSION, NO EMERGENCY DECLARED. LANDED UNEVENTFULLY, TOWED TO PARKING. GREEN HYDRAULIC LOSS OF FLUID THEN LOSS OF GREEN HYD PRESSURE FLUID LEVEL INDICATED NORMAL AFTER ENGINE SHUTDOWN. ATS SHOWS PUMPS SELECTED OFF WHILE STILL SUPPLYING PRESSURE FOUND GREEN SYSTEM QUANTITY AT MINIMUMS SERVICED, IAW AMM 12 12 29 CYCLED FLIGHT CONTROLS, NO LEAKAGE NOTED.

Part: ACCESS DOOR — CHAFED (THRIUST REVERSER) · airframe 19,138 hrs · 11,675 cycles

INSPECTION TYPE:SEGR/H ENGINE REAR FAN DUCT LATCH ACCESS DOOR HAS DEEP CHAFE ON INNER SIDER&R PANEL SRM 51-40-21

Part: SKIN — GOUGED (FWD CARGO DOOR) · airframe 19,138 hrs · 11,675 cycles

INSPECTION TYPE:SEGLOWER FORWARD LEADING EDGE OF FWD CARGO DOOR HAS GOUGEREMOVED DAMGE IAW SRM 53-13-12 FIG 102.

Part: SUPPORT BRACKET — CRACKED (LT SPOILER) · airframe 19,138 hrs · 11,675 cycles

INSPECTION TYPE:A300SUPPORT BRACKET UNDEER LH SPOILER #5 INBOARD SIDE IS CRACKED APPROX 1/2 INH IN LENGTH ON LWR FWD SIDE.R&R SUPPORT BRACKET IAW SRM 51-410-21

Part: LIGHT — FAULTY (CABIN) · airframe 18,349 hrs · 11,233 cycles

EXIT LIGHT REMAINS ON IN FLIGHT WITH ASSOCIATED SWITCH IN ARM STAYED ON IN ALL 3 POSITIONS, PLACED EXIT LIGHT SWITCH INTO "AUTO" POSITION LIGHT OPS CHECKS GOOD PER AMM 31 51 00 501

Part: CONNECTOR — NOT SEATED (CABIN PRESSURE) · airframe 17,793 hrs · 10,925 cycles

RED RESIDUAL PRESSURE LIGHT ILLUMINATED ON CABIN DOOR AND MCD CONTROL PANEL. CABIN PRESSURE AT ZERO.REMOVED ELECTRICAL CONNECTOR 71WN-A FROM CABIN PRESSURE DETECTION SWITCH. RECONNECTED CONNECTOR RESIDUAL PRESSURE LIGHT WENT OUT. SYSTEM OPERATES NORMAL REF A300 AMM 52-73-00.

Part: WARNING LIGHT — ILLUMINATED (DOOR SLIDE) · airframe 16,871 hrs · 10,437 cycles

SLIDE WARNING SYSTEM LIGHT INOPERATIVE. PERFORMED TSM 52-73-00, RESET ASPSU IAW AMM 52-73-18. OPS CHECKED NORMAL.

Part: CYLINDER — LOW PRESSURE (ENTRY DOOR) · airframe 16,611 hrs · 10,294 cycles

CREW ENTRY DOOR EMER CYLINDER LOW. SERVICED CREW ENTRY DOOR EMERGENCY CYLINDER AS REQUIRED IAW MM 52-10-14-0301. NO LEAKS NOTED AT THIS TIME.

Part: PSU — INOPERATIVE (L1 DOOR) · airframe 15,746 hrs · 9,799 cycles

L1 DOOR ESCAPE SLIDE WARNING LIGHT DOES NOT FLASH. R & R 70WN PSU AUTONOMUS STANDBY. ADJUSTED AND TESTED GOOD. OK FOR SERVICE.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 15,405 hrs · 9,577 cycles

INSPECTION TYPE: 12Y, FABRICATED FLOORBOARD 262DM IS CRACKED. FABRICATED A NEW FLOORBOARD IAW SREO A300-5320-16407-E.

Part: ADAPTER — CRACKED (FRAME 19) · airframe 15,405 hrs · 9,577 cycles

INSPECTION TYPE: 123C, MAIN CABIN AT FRAME 19 -Y1959, ADAPTER PLATE IS BROKEN. REMOVED, FABRICATED, AND INSTALLED A NEW ADAPTER IAW EO A300-5310-65205-A

Part: FLOORBEAM — CRACKED (FRAME 80) · airframe 15,405 hrs · 9,577 cycles

INSPECTION TYPE: 1C, MAIN DECK RT CORNER FLOOR SUPPORT CRACKED. REMOVED, AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-21/51-40-44

Part: STRUCTURE — CHAFED (RT WING TE FLAP) · airframe 15,405 hrs · 9,577 cycles

INSPECTION TYPE: 123C, RT WING CENTER FLAP LEADING EDGE OTBD EDGE CHAFFED. REPAIRED THE FLAP LE OTBD EDGE IAW SRM 57-50-00, FIG 208.

Part: WEDGE — GOUGED (RT WING SLAT) · airframe 15,405 hrs · 9,577 cycles

INSPECTION TYPE: 123C, RT WING NR 1 SLAT TRAILING EDGE WEDGE LOWER OUTBOARD SURFACE GOUGED. REPAIRED IAW REO-G20971.

Part: FLOOR PANEL — PUNCTURED (AFT CARGO BAY) · airframe 15,405 hrs · 9,577 cycles

AFT CARGO FLOOR PANEL 52-SF HAS EDGE DAMAGE. ACCOMPLISHED THE REPAIR IAW SREO A300-5320-42721-F

Part: FLOOR PANEL — CRACKED (FWD CARGO BAY) · airframe 15,405 hrs · 9,577 cycles

FLOOR PANEL 32-AH IS CRACKED. ACCOMPLISHED A REPAIR IAW SREO A300-5320-42721-F.

Part: FLOOR PANEL — CRACKED (AFT CARGO BAY) · airframe 15,405 hrs · 9,577 cycles

AFT CARGO BAY FLOOR PANEL 151-KG FOUND CRACKED. ACCOMPLISHED A REPAIR IAW SREO A300-5320-42721-F.

Part: FLOOR PANEL — PUNCTURED (FWD CARGO BAY) · airframe 15,405 hrs · 9,577 cycles

FLOOR PANEL 131-MG HAS EDGE DAMAGE. ACCOMPLISHED A REPAIR IAW SREO A300-5320-42721-F.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 15,405 hrs · 9,577 cycles

AFT CARGO BAY FLOOR PANEL 151-SF DAMAGED ON THE CORNER. ACCOMPLISHED REPAIR IAW SREO A300-5320-42721-F.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 15,405 hrs · 9,577 cycles

AFT CARGO FLOOR PANEL 152-QF HAS DAMAGED. ACCOMPLISHED REPAIR IAW SREO A300-5320-42721-F.

Part: FLOOR PANEL — PUNCTURED (FWD CARGO BAY) · airframe 15,405 hrs · 9,577 cycles

FLOOR PANEL 132SG HAS EDGE DAMAGE. ACCOMPLISHED A REPAIR IAW SREO A300-5320-42721-F.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 15,405 hrs · 9,577 cycles

AFT CARGO PIT FLOOR PANEL 152VF DAMAGED. ACCOMPLISHED A REPAIR IAW SREO A300-42721-F

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 15,405 hrs · 9,577 cycles

AFT CARGO FLOOR PANEL 152-MG HAS DAMAGE. ACCOMPLISHED REPAIR IAW SREO A300-5320-42721-F.

Part: FLOOR PANEL — CRACKED (FWD CARGO BAY) · airframe 15,405 hrs · 9,577 cycles

FLOOR PANEL 132-PG IS CRACKED. ACCOMPLISHED A REPAIR IAW SREO A300-5320-42721-F.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 15,405 hrs · 9,577 cycles

AFT CARGO FLOOR PANEL 151-QF HAS DAMAGE. ACCOMPLISHED A REPAIR IAW SREO A300-5320-42721-F.

Part: FLOOR PANEL — CRACKED (AFT CARGO BAY) · airframe 15,405 hrs · 9,577 cycles

AFT CARGO BAY FLOOR PANEL 151-TF CRACKED. ACCOMPLISHED A REPAIR IAW SREO A300-5320-42721-F.

Part: FLOOR PANEL — DAMAGED (FWD CARGO BAY) · airframe 15,405 hrs · 9,577 cycles

FLOOR PANEL 131-RG HAS EDGE DAMAGE. ACCOMPLISHED A REPAIR IAW SREO A300-5320-42721-F.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 15,405 hrs · 9,577 cycles

AFT CARGO BAY FLOOR PANEL 152TF HAS DAMAGE. ACCOMPLISHED A REPAIR IAW SREO A300-5320-42721-F

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 15,405 hrs · 9,577 cycles

AFT CARGO BAY FLOOR PANEL 151VF HAS EDGE DAMAGE. ACCOMPLISHED A REPAIR IAW SREO A300-5320-42721-F.

Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 15,405 hrs · 9,577 cycles

INSPECTION TYPE: C1,2, FLOORBEAM, FRAME 79 IS CRACKED. REPAIRED IAW EO A300-5310-65033-A.

Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 15,405 hrs · 9,577 cycles

INSPECTION TYPE: C1,2. FLOORBEAM AT FRAME 79 IS CRACKED. REPAIRED IAW EO A300-5310-65033-A.

Part: LAMP — INOPERATIVE (LAVATORY MIRROR) · airframe 14,779 hrs · 9,183 cycles

LAVATORY MIRROR LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM33-51-21-401.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 14,354 hrs · 8,921 cycles

SHORTLY AFTER DEPARTURE, RECEIVED CABIN PRESSURE REGULATOR FAULT FOLLOWED BY CABIN PRESSURE EXCESSIVE MESSAGE. CREW DECLARED AN EMERGENCY AND RETURNED. FOUND NR 1 AND NR 2 CABIN PRESSURE CONTROLLERS 105 HM AND 106 HM FAILING TEST OK AND BITE TEST IAW AMM 21-31-00-501. R & R 1 AND NR 2 PRESSURE CONTROLLERS IAW MM 21-31-11-401 TESTS OF SYSTEMS OK, EFF SOURCE REF IPC 21-31-08-03A-010.

Part: BUSHING — MIGRATED (LT MLG) · airframe 13,084 hrs · 8,111 cycles

INSPECTION TYPE:C1, LT MLG RIB 5 AFT BEARING BUSHING FLANGE. EVIDENCE OF BUSHING MIGRATING REMOVED LT MLG, R & R BUSHING IAW REO-G19070, REINSTALLED LT MLG AND ALL OPS CHECKS PERFORMED.

Part: DOOR FRAME — CRACKED (FRM 61) · airframe 13,081 hrs · 8,109 cycles

INSPECTION TYPE: C-1, AFT CARGO DOOR FRAME 61 IS CRACKED. R & R THE FRAME IAW SREO A300- 5230-57988-A.

Part: SMOKE DETECTOR — MALFUNCTIONED (AVIONICS BAY) · airframe 12,880 hrs · 7,986 cycles

EMERGENCY DECLARED - JUST PRIOR TO LEVEL OFF, 15 MINUTES INTO FLIGHT, AVIONICS SMOKE LIGHT ILLUMINATED WITH AVONICS SMOKE WARNING ON ECAM. AFTER CHECKLIST PUSHED AVONICS EXTRACT BUTTON, WARNING DISAPPEARED FOR ABOUT 1 MINUTE, THEN REAPPEARED. TESTING FOR SMOKE R & R SMOKE DETECTORS 11WA &13WA IAW MM 26-15-12 PB 0401. OPS CHECKS NORMAL IAW MM 26-15-00-PB 0501. NO DEFECTS NOTED.

Part: SKIN — DENTED (FRAME 85)

DENT ON SKIN REPAIR DOUBLER WITH GOUGE AT FRAME 85 BETWEEN S44 --45L. REPAIRED IAW EO 5330-55466-A.

Part: LAMP — INOPERATIVE (LAV MIRROR)

DURING MX INSPECTION, THE LAVATORY MIRROR LIGHT WAS INOPERATIVE. REPLACED LAMP IAW AMM, OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY EXIT LIGHTS STAY ON IN THE ARMED POSITION WITH THE ACFT POWERED. R & R EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-14.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MDCC FLOOR PANEL 221FG HAS 2 AREAS OF DAMAGE ON LOWER SKIN WITH CORE DAMAGE. FABRICATED NEW FLOOR PANEL IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 222AG LOWER SKIN IS DAMAGED. REPAIRED MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-D, PARA 6A.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 231RH HAS LOWER SKIN PUNCTURED. REPAIRED FLOORBOARD IAW EO A300-5320-42721-D, PARA 6A.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 231RJ HAS LOWER SKIN PUNCTURED. REPAIRED FLOORBOARD IAW EO A300-5320-42721-D, PARA 6A.

Part: FLOORBOARD — TORN (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 231SG LOWER SKIN IS TORN. REPAIRED MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-D, PARA 6A.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 251JF IS DELAMINATED AT LOWER SURFACE REPAIRED FLOORBOARD IAW EO A300-5320-42721-D, PARA 6A.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 232BH LOWER SKIN IS PUNCTURED. REPAIRED MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-D, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 231QH HAS LOWER SKIN CRACKED. REPAIRED MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-D, PAR 6A.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 231NJ HAS LOWER SKIN TORN. REPAIRED FLOORBOARD IAW EO A300-5320-42721-D, PARA 6A.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 232NG HAS LOWER SKIN PUNCTURED. REPAIRED FLOORBOARD IAW EO A300-5320-42721-D, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 222EG HAS LOWER SKIN CRACKED FABRICATED MAIN CABIN FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 231MJ LOWER SKIN IS CRACKED. FABRICATED MAIN CABIN FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 232LF HAS LOWER SKIN CRACKED. REPAIRED MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-D, PARA 6A.

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 232EF HAS LOWER SKIN PUNCTURED. REPAIRED MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-D, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 241VM IS CRACKED AT LOWER SURFACE. REPAIRED FLOORBOARD IAW EO A300-5320-42721-D, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 251UJ IS CRACKED AT LOWER SURFACE. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-D, PARA 6A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, COURIER COMPARTMENT FLOOR SUPPORT IS CORRODED AND HAS DEEP SCRATCHES BETWEEN FR 15 AND FR 17 STA Y1959. R & R COURIER COMPARTMENT FLOOR SUPPORT BETWEEN FR12 AND FR17 STA Y1959 IAW DWG A53613109.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 251CH IS CRACKED AT LOWER SKIN. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-D, PARA 6A.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK IS CORRODED AT FR 62 Y953. ACCOMPLISHED REPAIR ON MAIN CABIN SEAT TRACK IAW SRM 53-10-16, FIG 201.

Part: FLOORBOARD — BROKEN (FWD CARGO) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, FWD CARGO FLOORBOARD 131SG IS BROKEN AT FWD CORNERS. FABRICATED FWD CARGO FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX C. (MAJOR)

Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 252LM IS PUNCTURED ON LOWER SURFACE REPAIRED FLOORBOARD IAW EO A300-5320-42721-D, PARA 6A.

Part: FLOORBOARD — DELAMINATED (FWD CARGO) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, FWD CARGO FLOORBOARD 132SG IS DELAMINATED AT FWD CORNER. FABRICATED FWD CARGO FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX C.

Part: FLOOR PANEL — PUNCTURED · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, FLOOR PANEL 252UJ HAS UPPER SKIN PUNCTURED AND HAS A PIECE BROKEN OUT OF LOWER SKIN. FABRICATED NEW FLOOR PANEL IAW EO A300-5320-40552-B, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 251HJ IS CRACKED AT LOWER SURFACE. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-D, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR MAIN CABIN FLOORBOARD 242SN LOWER SKIN IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-D, PARA 6A.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 261DM IS CRACKED AT LOWER SURFACE. REPAIRED MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-D, PARA 6A.

Part: FLOORBOARD — PUNCTURED (AFT CARGO) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, AFT CARGO FLOORBOARD 152UF LOWER SURFACE IS PUNCTURED. ACCOMPLISHED REPAIR ON AFT CARGO FLOORBOARD IAW EO A300-5320-42721-D, PARA 6A.

Part: ADAPTER — CORRODED · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, CLEVIS ADAPTER IS CORRODED BETWEEN FR21 AND FR27 AT Y0 LT. REPAIRED CLEVIS ADAPTER IS CORRODED BETWEEN FR21 AND FR27 AT Y0 IAW EO A300-5310-49688-C.

Part: FITTING — CRACKED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN FLOOR RT FR12A FITTING IS CRACKED. R & R MAIN CABIN FLOOR RT FR12A FLOOR FITTING IAW EO A300-5310-23539-F, APPENDIX E.

Part: FLOORBOARD — CRACKED (AFT CARGO) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, AFT CARGO FLOORBOARD 152SF HAS A CRACK ON LOWER SKIN. FABRICATED AFT CARGO FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX C.

Part: FLOORBOARD — CRACKED (AFT CARGO) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, AFT CARGO FLOORBOARD 151UF HAS THREE CRACKS AND DELAMINATION ON LOWER SURFACE. FABRICATED AFT CARGO FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX C.

Part: FLOORBOARD — CRACKED (AFT CARGO) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, AFT CARGO FLOORBOARD 152QF LOWER SKIN IS CRACKED. ACCOMPLISHED REPAIR ON AFT CARGO FLOORBOARD IAW EO A300-5320-42721-D, PARA 6A.

Part: FLOORBOARD — PUNCTURED (AFT CARGO) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, AFT CARGO FLOORBOARD 152TF LOWER SKIN IS PUNCTURED AND DISBONDED. ACCOMPLISHED REPAIR ON AFT CARGO FLOORBOARD IAW EO A300-5320-42721-D, PARA 6A.

Part: FLOORBOARD — PUNCTURED (AFT CARGO) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, AFT CARGO FLOORBOARD 152VF HAS LOWER SKIN PUNCTURED. ACCOMPLISHED REPAIR ON AFT CARGO FLOORBOARD IAW EO A300-5320-42721-D, PARA 6A.

Part: FLOORBOARD — PUNCTURED (AFT CARGO) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, AFT CARGO FLOORBOARD 151VF IS PUNCTURED THROUGH FABRICATED AFT CARGO FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX C.

Part: FLOORBOARD — CRACKED (AFT CARGO) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, AFT CARGO FLOORBOARD 151SF IS CRACKED AT FWD END. FABRICATED AFT CARGO FLOORBOARD IAW EO A300-5320-16407-E, APENNDIX C.

Part: FLOORBOARD — CRACKED (BULK CARGO) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, BULK CARGO FLOORBOARD 162MF IS CRACKED IN 2 PLACES AT FWD CORNER. FABRICATED BULK CARGO FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX D. (MAJOR)

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK IS CORRODED BETWEEN FR79 AND 80 Y794.3. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK IS CORRODED BETWEEN FR 79 AND 80 -Y794.3. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK IS CORRODED BETWEEN FR 79 AND FR 80 Y450. ACCOMPLISHED REPAIR ON MAIN CABIN SEAT TRACK BETWEEN FR79 AND FR80 STA Y450 IAW SRM 53-10-16, FIG 201. (MAJOR)

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK IS CORRODED BETWEEN FR79 AND FR80 STA -Y1137. ACCOMPLISHED REPAIR ON MAIN CABIN SEAT TRACK BETWEEN FR79 AND FR80 STA -Y1137 IAW SRM 53-10-16, FIG 201. (MAJOR)

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK IS CORRODED BETWEEN FR79 AND FR80 AT STA Y0. ACCOMPLISHED REPAIR ON MAIN CABIN SEAT TRACK BETWEEN FR79 AND FR80 STA Y0 IAW SRM 53-10-16, FIG 201. (MAJOR)

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE: 10YR, MAIN CABIN SEAT TRACK IS CORRODED BETWEEN FR 79 AND 80 -Y1137. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,212 hrs · 6,905 cycles

INSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK IS CORRODED BETWEEN FR79 AND 80 Y450. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201.

Part: UNKNOWN — MULTIPLE FAIL

AIR RETURN DUE TO MULTIPLE ADC ISSUES. R & R CAPT'S PITOT TUBE IAW MM 34-11-15-04-1 LEAK AND OPS CK GOOD. R & R AIR DATA COMPUTER 1FC1 IAW MM 34-11-34-0401. ALL CHECKS NORMAL. OK FOR CONTINUED SERVICE.

Part: SKIN — DAMAGED (RT FUSELAGE FR12)

RT FUSELAGE SKIN DAMAGED AT FRAME 12 BETWEEN UPPER AND LWR WEB. REPAIRED IAW EO A300-5330-42808-C.

Part: SIGNAL COND UNIT — INOPERATIVE (LEFT ENGINE)

ATB ON CLIMBOUT AT 7000 FT, RECEIVED AN ADVISORY ENGINE VIBRATION LT ENGINE N1 WAS 3.8. STOPPED CLIMB AT 10,000 FT N1 ENGINE VIBRATION 4.0, RAN CHECKLIST, RETURNED TO DEPARTURE. LANDING WEIGHT 345,000 LBS TOUCHDOWN 20FT IAW MINUTE. ALSO APU WOULD NOT START IN FLIGHT OR ON THE GROUND. FELT VIBRATION MORE DURING DESCENDED. R & R ENGINE VIBRATION SIGNAL CONDITIONER UNIT REF MM 77-32-21 21-0401 PERFORMED VIB TEST AND ENGINE RUN ALL INDICATIONS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

LAVATORY EMERGENCY LIGHT INOPERATIVE. RELAMPED LAVATORY EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: SKIN — DENTED (FUSELAGE)

FUSELAGE SKIN DENTED FR 65 BETWEEN STR 53 AND 57L. REPAIRED IAW EO A300-5330-43906-C.

Part: STRINGER — DAMAGED (54L)

STRINGER 54L DEFLECTED. REPAIRED IAW EO A300-5330-43906-C.

Part: STRINGER — DAMAGED (FUSELAGE)

STRINGER 55L DEFLECTED. REPAIRED IAW EO A300-5330-43905-C.

Part: SKIN — GOUGED (FUSELAGE)

FUSELAGE SKIN FWD OF FWD LWR CARGO OPENING DAMAGED. DOUBLER REPAIR IAW A300-5330-43120-B.

Part: LIGHT — INOPERATIVE (SLIDE WARNING)

EVAC SLIDE/SLIDE RAFT RELEASE WARN SYS LIGHTS INOP. DEFERRED ASSIGNED M446280 IAW MEL 52-73-01-1. PLACARD INSTALLED.(OPEN)

Part: WARNING LIGHT — INOPERATIVE (COCKPIT)

EVAC SLIDE/SLIDE RAFT RELEASE WARN SYS LIGHTS INOP. DEFERRED ASSIGNED M446280 IAW MEL 52-73-01-1. PLACARD INSTALLED. REMOVED AND INSTALLED CONNECTOR PLUG FROM AUTONOMOUS STANDBY POWER SUPPLY UNIT IAW MM 52-73-18-04. OPS CK GOOD IAW MM 52-73-00-05. THIS CLEARS DEFERRAL M446280.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 8,317 hrs · 5,160 cycles

INSPECTION TYPE:3C, LT CTR FLAP UPPER SURFACE GOUGED, RIB 13 TO 15, STR 2.6 TO 2.8. ACCOMPLISHED REPAIR ON LT CTR FLAP IAW A300-600, SRM 57-50-00, PARA 4E, FIG 205 AND EO A300-5750-35931-C.

Part: SKIN — DENTED (FUSELAGE) · airframe 8,317 hrs · 5,160 cycles

INSPECTION TYPE:3C. ALLOWABLE DAMAGE MAP VALIDATION. VERIFY LOCATION AND DESCRIPTION /LIMITS OF D-432611. DENT ON LT FUSELAGE JUST BELOW CREW ENTRY DOOR AT FR 15-15A, STR 30L. ACCOMPLISHED REPAIR IAW EO A300-5330-41054-A, AND EA 300-5330-01-A2816 IR.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 8,317 hrs · 5,160 cycles

INSPECTION TYPE:3C, REPAIR VALIDATION SURVEY, REPAIR OF AFT BULK PIT FLOOR APPROX 2FT INBD OF DOOR THRESHOLD. FABRICATED BULK PIT FLOORBOARD NR161LF IAW EO A300-5320-16407-E, APPENDIX D.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 8,317 hrs · 5,160 cycles

INSPECTION TYPE:3C, REPAIR VALIDATION SURVEY, REPAIR OF FWD CARGO FLOORBOARD NR 132MG. FABRICATED FWD CARGO FLOORBOARD NR132MG IAW EO A300-5320-16407-E, APPENDIX C.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 8,317 hrs · 5,160 cycles

INSPECTION TYPE:3C, REPAIR VALIDATION SURVEY,REPAIR OF BULK CARGO FLOORBOARD 162HF. FABRICATED BULK CARGO FLOORBOARD NR162HF IAW EO A300-5320-16407-E, APPENDIX D.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 8,317 hrs · 5,160 cycles

INSPECTION TYPE:3C, REPAIR VALIDATION SURVEY, REPAIR OF AFT CARGO FLOORBOARD NR151UF. ACCOMPLISHED REPAIR ON AFT CARGO FLOORBOARD 151UF IAW EO A300-5320-16407-E, APPENDIX C.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 8,317 hrs · 5,160 cycles

INSPECTION TYPE:3C, REPAIR VALIDATION SURVEY, REPAIR OF LT FWD CARGO FLOORBOARD NR 131AH. FABRICATED FWD CARGO FLOORBOARD NR 131AH IAW EO A300-5320-16407-E, APPENDIX C.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 8,317 hrs · 5,160 cycles

INSPECTION TYPE:3C, REPAIR VALIDATION SURVEY, REPAIR OF BULK CARGO FLOORBOARD NR161HF. FABRICATED BULK CARGO FLOORBOARD NR161HF IAW EO A300-5320-16407-E, APPENDIX D.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 8,317 hrs · 5,160 cycles

INSPECTION TYPE:3C, REPAIR VALIDATION SURVEY, REPAIR OF HOLE IN BULK PIT FLOOR. ACCOMPLISHED REPAIR ON BULK CARGO FLOORBOARD NR161GF IAW EO A300-5320-16407-E, APPENDIX D

Part: SKIN — DAMAGED (FUSELAGE)

FUSE SKIN DAMAGED FR59 STR 57. REPAIRED IAW EO A300-5330-37373-B.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

LAV EMERGENCY LIGHT INOP. RELAMPED LAV EMERGENCY LIGHT OPS CHECK GOOD.

Part: GIRT BAR — OUT OF POSITION (PAX DOOR SLIDE)

INSPECTION TYPE:N/A MAIN CABIN DOOR SLIDE INOP - WILL NOT ARM DEFERRED PER MEL M411022 ASSIGNED. REPOSITIONED GIRT BAR IN GIRT EXTENSION PER MM 25-61-21-04. TESTS OK.

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A FLOOR PANEL AT POS 11 DAMAGED. REPAIR PER EO A300-5320-16407-C.

Part: WARNING LIGHT — INOPERATIVE (EVAC SLIDE)

EVAC SLIDE WARNING LIGHTS INOP. DEFERRED PER 52-73-01-1. ACCOMPLISHED ASPSU BATTERY CAPACITY TEST FROM BUILT IN TEST PANEL PER MM 52-73-00-05. BATTERY 1&2 FAULTED. REPLACED NR 1 BATTERY OPS NORMAL. NR 2 STILL FAULTED. FOUND BATTERY NOT SEATED. RESEATED BATTERY OPS CHECK GOOD. PLACARD REMOVED.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 5,581 hrs · 3,526 cycles

INSPECTION TYPE:5 YR MAIN CABIN FLOORBOARD 232TG HAS GOUGES. REPAIRED MAIN CABIN FLOORBOARD 232TG REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 5,581 hrs · 3,526 cycles

INSPECTION TYPE:5 YR MAIN CARGO FLOORBOARD 242PM HAS A PUNCTURE. REPAIRED MAIN CARGO FLOOR PANEL REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 5,581 hrs · 3,526 cycles

INSPECTION TYPE:5 YR MAIN CABIN FLOORBOARD 251LJ HAS TEMP REPAIRS. REPAIRED MAIN CABIN FLOOR PANEL 251LJ REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 5,581 hrs · 3,526 cycles

INSPECTION TYPE:5 YR MAIN CABIN FLOORBOARD 231SG PUNCTURED. REPAIRED MAIN CABIN FLOOR PANEL 231SG REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 5,581 hrs · 3,526 cycles

INSPECTION TYPE:5 YR MAIN CABIN FLOORBOARD 241YK HAS TEMP REPAIR. PERMANENTLY REPAIRED MAIN CABIN FLOOR PANEL REF A300-600 SRM 53-10- 20 TABLE 201 PARA 8A.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 5,581 hrs · 3,526 cycles

INSPECTION TYPE:5 YR CREW ENTRY AREA FLOOR PNL IS CRACKED AND DISBONDING ON OUTBOARD CORNER WHERE MARKED. REPAIRED MAIN CABIN FLOOR PANEL 221FF REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOOR PANEL — CRACKED (MAIN CARGO BAY) · airframe 5,581 hrs · 3,526 cycles

INSPECTION TYPE:5 YR MAIN CARGO FLOOR PANEL IS CRACKED IN 3 PLACES, PANEL 232LF. REPAIRED MAIN CARGO FLOOR PANEL 232LF REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 5,581 hrs · 3,526 cycles

INSPECTION TYPE:5 YR MAIN CARGO FLOORBOARD 222AG IS CRACKED ON EACH SIDE. REPAIRED MAIN CARGO FLOORBOARD 222AG REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 5,581 hrs · 3,526 cycles

INSPECTION TYPE:5 YR MAIN CARGO FLOORBOARD 221BG IS CRACKED ON EACH SIDE. REPAIRED MAIN CARGO FLOORBOARD 221BG REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 5,581 hrs · 3,526 cycles

INSPECTION TYPE:5 YR MAIN CARGO FLOORBOARD 221FG IS CRACKED ON EACH SIDE. REPAIRED MAIN CARGO FLOORBOARD 221FG REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOORBOARD — BROKEN (CABIN) · airframe 5,581 hrs · 3,526 cycles

INSPECTION TYPE:5 YR MAIN CABIN FLOORBOARD 232XG BROKEN AT LEFT FWD EDGE. PERMANENTLY REPAIRED MAIN CABIN FLOOR PANEL REF A300-600 SRM 53-10- 20 TABLE 201 PARA 8A.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 5,581 hrs · 3,526 cycles

INSPECTION TYPE:5 YR MAIN CABIN FLOORBOARD 242UJ CRACKED INTERNALLY. REPAIRED MAIN CABIN FLOOR PANEL 242UJ REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 5,581 hrs · 3,526 cycles

INSPECTION TYPE:5 YR 1 EA ROUND BOTTOM DENT WITH INDICATION OF DELAMINATION ON UPPER SURFACE OF LT AFT MAIN CARGO COMPT FLOOR PNL. MKD 261BH. REPAIRED MAIN CABIN FLOOR PANEL 261BH REF A300-600 SRM 51-10-20 TABLE 201 PARA 8A.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 5,581 hrs · 3,526 cycles

INSPECTION TYPE:5 YR MAIN CABIN FLOORBOARD 261FH CRACKED LEFT CORNER. REPAIRED MAIN CABIN FLOOR PANEL 261FH REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 5,581 hrs · 3,526 cycles

INSPECTION TYPE:5 YR MAIN CABIN FLOORBOARD 231XG CRACKED FROM INSIDE. REPAIRED MAIN CABIN FLOOR PANEL 231XG REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 5,581 hrs · 3,526 cycles

INSPECTION TYPE:5 YR MAIN CABIN FLOORBOARD 252WJ HAS TEMPORARY REPAIR RT SIDE CENTER EDGE OF PANEL. REPAIRED MAIN CABIN FLOOR PANEL 252WJ REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A.

Part: RIB — CRACKED (KRUEGER FLAP) · airframe 5,581 hrs · 3,526 cycles

INSPECTION TYPE:5 YR LT WING K-FLAP WELL RIB CRACKED IN LOWER RADIUS. REPAIRED LEFT WING KRUEGER FLAP WELL RIB BY REPLACEMENT OF PART REF A300-600 SRM 51-40-21 PAGE 1 PARA 5, 6 AND 7.

Part: RIB — CRACKED (L/E SLAT) · airframe 5,581 hrs · 3,526 cycles

INSPECTION TYPE:5 YR RT WING KRUEGER FLAP WELL AT INBOARD RIB SUPPORT IS CRACKED. REPLACED RT WING KRUEGER FLAP WELL RIB REF A300-600 SRM 51-40-21 PAGE 1.

Part: RIVET — CHAFED (T/E FLAP) · airframe 5,581 hrs · 3,526 cycles

INSPECTION TYPE:5 YR LT WING CENTER FLAP MID CENTER HAVE RIVET HEADS CHAFED. REPAIRED LT WING CENTER FLAP CENTER AREA REF A300-600 SRM.

Part: SUPPORT — CRACKED (LT WING) · airframe 2,676 hrs · 1,763 cycles

INSPECTION TYPE:1C LT WING ABOVE NR 4 FLAP TRACK; WEB CRACKED. REMOVED AND REPLACED SKIN SUPPORT PER A300 SRM 51-40-00 AND 51-40-21.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 2,676 hrs · 1,763 cycles

MAIN CABIN, CROSSBEAM CRACKED AT FS 49 RBL36. REMOVED AND REPLACED CROSSBEAM PER A300 SRM 51-40-21.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY)

INSPECTION TYPE:N/A CRACK IN MCDECK POS NR 1 RT SIDE NEXT TO LAST ROLLER TRAY. OUT OF LIMITS PER SRM 53-10-20 FIG 102. INSTALLED TEMP REPAIRS AS PRELIMINARY EO A300-5310-24331-A. REMOVED TEMP REPAIRS & REPAIRED FLOOR PANEL PER SRM 53-10-20 FIG 202 & 203.

Part: SLAT SYSTEM — INOPERATIVE

DIVERSION, SLATS SYS 1 AND SYS 2 FAULT WHEN FLAPS 40 SELECTED SLATS REMAINED AT 15; FOLLOWED QRH PROCEDURE AND CYCLED FLAPS SLATS RETRACTED NORMALLY AND EXTENDED NORMALLY ON APPROACH TO MCO. BITE FCC AT MCP NO FAULTS CHECKED ALL TORQUE LIMITERS LT AND RT WING SLATS FOUND OK PER MM FSM 27-80-02-01.

Part: WARNING SYSTEM — FAILED (COCKPIT)

MULTI ELECTRICAL SYS FAILURES. NO ECAM WARNINGS. R&R FIGHT CONTROL UNIT PER A300 MM 22-15-12-4. OPS CHECK OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

WALL MOUNTED EMERGENCY LIGHT ABOVE MIRROR INOP, IN LAVATORY. RELAMPED WITH SERVICEABLE LAMP IAW A-300-600 AMM 33-51-21-4. OPS CHECK NORMAL.