N159UP

Part: SLIDE — OBSTRUCTED (ZONE 800) · airframe 25,768 hrs · 15,621 cycles

ON GROUND WHILE SECURING FOR FLIGHT, MAIN ENTRY DOOR SLIDE WOULD NOT ARM - LEVER WOULD NOT MOVE TO THE ARMED POSITION. UPON TROUBLESHOOTING INSPECTED L1 & MCD SEALS. NO FAULTS FOUND AT THIS TIME. FOUND L1 DOOR SLIDE EJECTOR BAG RELEASE CABLE/ QUICK DISCONNECT ASSY, DROOPING AND PUSHING GRIT BAR UP AND NOT ALLOWING IT TO ENGAGE INTO THE FLOOR FITTING. INSPECTED AND RE-STOWED INTO SLIDE AND OP CHECKED DOOR ARMING SYSTEM A300 AMM 52-10-00/301, SYSTEM OPERATES NORMALLY AT THIS TIME. THIS CLEARS MEL 2863247, MEL 52-11-01-2-3. PLACARD REMOVED OKAY TO CONTINUE SERVICE.

Part: BOTTLE — DISCHARGED (ZONE 800) · airframe 25,167 hrs · 15,281 cycles

L-1 DOOR EMERGENCY OPERATING CYLINDER INADVERTENTLY DISCHARGED REPLACED DIAPHRAGM, SEALS, SHEAR PIN, AND SERVICED DOOR DAMPER CYLINDER - OPS CHECKS GOOD AT THIS TIME. SAFETY PIN REMOVED IAW MM 52-10-14/301

Part: SLIDE — MALFUNCTIONED (ZONE 800) · airframe 24,969 hrs · 15,165 cycles

DOOR SLIDE ONLY DISARMS WITH EXTREME FORCE LUBRICATED GIRT BAR AND SEVERAL OTHER MECHANISMS IN THE SYSTEM REF AMM 52-10-30/601 OPS CHECKS GOOD

Part: UNKNOWN — NOISE (ZONE 800) · airframe 24,755 hrs · 15,051 cycles

VERY HIGH PITCH NOISE FROM MAIN CABIN DECK CARGO DOOR OR CREW ENTRY DOOR AREA. CABIN PRESSURE AND CABIN ALTITUDE WERE ALL NORMAL (DIFF 8.0 V/S 0, CABIN ALTITUDE 5 AT FL 320). ALL ECAM DOOR INDICATIONS PRESSURIZED A/C PER AMM 05-51-00/001. NO NOISE FROM CREW ENTRY DOOR OR MAIIN CARGO AREA. OK FOR SERVICE.

Part: SWITCH — WORN (ZONE 800) · airframe 24,524 hrs · 14,953 cycles

IMMEDIATELY AFTER TAKEOFF "FORWARD CARGO DOOR NOT CLOSED" AND "CHECK 0001 TIMES" WHICH LED US TO COMPLETE AN AIR TURN BACK AS AIRCRAFT DIDNT SEEM TO BE PRESSURIZING. REMOVED & REPLACED DOOR WARNING SWITCH 14WS PER AMM 52-71-00/401. OPS CHECK GOOD. ADJUSTMENT OF SPRING LEAF WITHIN LIMITS PER AMM 52-71-00/501. DMP REVERSED, PLACARD REMOVED

Part: HANDLE — BINDING (ZONE 800) · airframe 23,846 hrs · 14,588 cycles

AFTER BLOCK IN, CREW WAS UNABLE TO DISARM THE ESCAPE SLIDE. DISARM HANDLE MOVES 3/4 WAY, BUT WILL BOT FULLY DISARM. INSPECTED PASSENGER CREW ENTRY DOOR JAWS SLIDERS AND GIRT BAR TOLERANCES IAW AMM 52-10-30/601. ALL ARE WITHIN TOLERENCES. CLEANED ALL MECHANICAL MECHANISMS AND OPS CHECKED DOOR SLIDE ARM/DISARM HANDKE. OPS CHECK GOOD.

Part: GIRT BAR — FOD (ZONE 200) · airframe 23,700 hrs · 14,501 cycles

DIFFICULTY DISARMING SLIDE. LEVER WAS CATCHING ON SOMETHING. REMOVED DEBRIS FROM GIRT BAR FITTINGS AND CLEANED AS REQUIRED. SLIDE ARMING LEVER OPS CHECKS GOOD. REF AMM 52-10-11

Part: LATCH — OUT OF POSITION (CREW DOOR) · airframe 23,656 hrs · 14,470 cycles

CREW ENTRY DOOR AFT LATCH INDICATION HALF RED HALF GREEN. OPEN

Part: LATCH — OUT OF ADJUST (CREW DOOR) · airframe 23,656 hrs · 14,470 cycles

CREW ENTRY DOOR AFT LATCH INDICATION HALF RED HALF GREEN. MADE ADUSTMENT AND PERFORMED FUNCTIONAL TEST OF FWD PASSENGER/CREW DOOR IAW AMM 52-10-11. OPS CHECK GOOD

Part: SKIN — CRACKED (RT WING) · airframe 23,656 hrs · 14,470 cycles

RT WING, UPPER SURFACE, APPROX RIB 18, HAVE A CRACK ON SKIN. DOT 103-199 INSTALLED REPAIR AS REQUIRED IAW SRM 57-51-12 PARA G FIG 207 RIVETS INSTALLED.

Part: FRAME — DAMAGED (FR 47) · airframe 23,656 hrs · 14,470 cycles

LEFT FR47 HOLE IS REAMED TO A SIZE OF .610" WITH NO DAMAGE INDICATIONS. ACCOMPLISH THE REPAIR PER EO-90513-REQ1 AND EA 300-5710-27-A3600 REV. -.

Part: PANEL — DAMAGED (UNKNOWN) · airframe 23,656 hrs · 14,470 cycles

PANEL 131GE HAS DAMAGED EDGE SEAL . REPAIRED DAMAGE EDGE SEAL IN PANEL 131GE, I.A.W. EO NO.: A300-5320-42722-F. PANEL #131GE, WAS REPAIRED IAW EO A300-5320-42722-F. NO FURTHER ACTON REQUIRED.

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 23,656 hrs · 14,470 cycles

**SUPPLEMENTAL SDR** FAULT: PANEL 132G HAS FIBERGLASS DAMAGE AND EDGE DAMAGE. DOT 109/080. REPAIRED FIBERGLASS TORN AND EDGE DAMAGE IN PANEL 132 QG, IAW (SREO) EO NO: A300-5320-42722-F. REVIEWED

Part: PANEL — DAMAGED · airframe 23,656 hrs · 14,470 cycles

PANEL 132SG HAS TORN FIBERGLASS AND EDGE DAMAGE. DOT 109/078. REPAIRED FIBERGLASS BREAKS AND EDGE DAMAGE IAW EO NO: A300-5320-42722-F. MAJOR REPAIR

Part: PANEL — TORN (NOT REPORTED) · airframe 23,656 hrs · 14,470 cycles

PANEL 132SG HAS TORN FIBERGLASS AND EDGE DAMAGE. REPAIRED FIBERGLASS BREAKS AND EDGE DAMAGE IAW EO NO: A300-5320-42722-F.

Part: PANEL — DAMAGED · airframe 23,656 hrs · 14,470 cycles

PANEL 132G HAS FIBERGLASS DAMAGE AND EDGE DAMAGE. DOT 109/080. REPAIRED FIBERGLASS TORN AND EDGE DAMAGE IN PANEL 132 QG, IAW (SREO) EO NO: A300-5320-42722-F. MAJOR REPAIR

Part: PANEL — DAMAGED · airframe 23,656 hrs · 14,470 cycles

PANEL 152QF HAS TORN FIBERGLASS AND DELAMINATED. DOT 109/075. REPAIRED TORN FIBERGLASS AND DELAMINATION OF PANEL 152QF, I.A.W. EO. A300-5320-42722-F. MAJOR REPAIR

Part: PANEL — TORN (NOT REPORTED) · airframe 23,656 hrs · 14,470 cycles

PANEL 152QF HAS TORN FIBERGLASS AND DELAMINATED. REPAIRED TORN FIBERGLASS AND DELAMINATION OF PANEL 152QF, I.A.W. EO. A300-5320-42722-F.

Part: FLOOR PANEL — DELAMINATED (FWD CARGO) · airframe 23,656 hrs · 14,470 cycles

FLOOR PANEL 143DF SOAKED AND DELAMINATE. FABRICATED FWD CARGO FLOOR PANEL 143DF IAW A300-5320-40552. JOB COMPLETE. REVIEWED

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 23,656 hrs · 14,470 cycles

THE L/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 26, AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90269-REQ1 AND EA 300-5750-27-A3581 REV.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 23,656 hrs · 14,470 cycles

THE L/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 27, AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90269-REQ1 AND EA 300-5750-27-A3581 REV.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 23,656 hrs · 14,470 cycles

THE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 19 AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 23,656 hrs · 14,470 cycles

THE R/H CENTER FLAP ASSY HAS MULTIPLE CRACKS (2EA) AT RIB LOCATION 26 AFT & FWD SIDES. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV-.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 23,656 hrs · 14,470 cycles

THE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 18 AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV -.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 23,656 hrs · 14,470 cycles

THE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 17 AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 23,656 hrs · 14,470 cycles

THE RT CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 25 AFT SIDE. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV -.

Part: DOUBLER — CRACKED (ZONE 600 FLAP) · airframe 23,656 hrs · 14,470 cycles

MAJOR REPAIR, THE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 11 AFT SIDE. AREA MARKED IN RED. INSTALLED NEW REPAIR FLANGE AND REINFORCEMENT REPAIR ANGLE I.A.W. A300-600 S.R.M. 51-40-21.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 23,656 hrs · 14,470 cycles

THE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 12 AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 23,656 hrs · 14,470 cycles

THE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 13 AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV -. MAJOR REPAIR.

Part: BULKHEAD WEB — DAMAGED (NR 2 INLET) · airframe 23,656 hrs · 14,470 cycles

FAULT: #2 ENGINE INLET COWL AFT BULKHEAD IS DAMAGED AROUND I/B P-2 LINE. DOT 142-53. INSTALLED NEW WEB AND SPLICE. IAW A300-600 SRM 51-40-21. REVIEWED

Part: FLOOR PANEL — BROKEN (MAIN DECK) · airframe 23,656 hrs · 14,470 cycles

MAIN DECK CARGO FLOOR PANEL 232WG IS BROKEN FABRICATE PNL FROM 5024N400001SS-G BACH #4055277 IAW SREO-40552-REQ001 C/W

Part: INLET — CRACKED (NR 2 ENGINE) · airframe 23,656 hrs · 14,470 cycles

NR 2 ENGINE INLET COWL ANTI-ICE DUCT FLANGE IS CRACKED AT INLET COWL AFT BULKHEAD. INSTALLED INLET COWL ANTI-ICE DUCT IAW AMM 30-21-00-401.- PERFORMED LEAK TEST IAW AMM 71-00-00/501 NO LEAKS FOUND. DYE PENETRANT INSPECTION FOR THE NR 2 ENGINE INLET COWL WAS PERFORMED IAW NTM 51-90-00 ON TRAVELER #T24/1758355. APPLIES TO ANTI-ICE DUCT FLANGE ONLY.

Part: FLOOR PANEL — BROKEN (MAIN DECK) · airframe 23,656 hrs · 14,470 cycles

MAIN DECK CARGO FLOOR PANEL 221CG IS BROKEN FABRICATED PNL 221CG FROM 5024N400001SS-G BACH # 4055277 IAW SREO-40552-REQ001 (APPX B) C/W.

Part: FLOOR PANEL — BROKEN (MAIN DECK) · airframe 23,656 hrs · 14,470 cycles

MAIN DECK CARGO FLOOR PANEL 232LF IS BROKEN FABRICATED PANEL FROM 5024N400001SS-G, BATCH #4055277 IAW S.R.E.O A300-5320-40552-B C/W.

Part: FLOOR PANEL — BROKEN (MAIN DECK) · airframe 23,656 hrs · 14,470 cycles

RH FLOOR PANEL 252 KM BROKEN DOT 44-007 FABRICATED PANEL 252KM FROM 5024N400001SS-G, BATCH# 4055277 PER SREO A300-5320-40552--B C/W.

Part: COVER — DAMAGED (CREW DOOR) · airframe 23,656 hrs · 14,470 cycles

CREW DOOR, EXTERNAL SKIN HEX COVERS DAMAGED; DOT 117-020. REMOVED AND REPLACED CREW DOOR HIST POINT COVERS IAW AMM 11-00-11/001.

Part: SKIN — DAMAGED (CREW DOOR) · airframe 23,656 hrs · 14,470 cycles

CREW DOOR, EXTERNAL SKIN HEX COVERS DAMAGED;

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 23,656 hrs · 14,470 cycles

E.E COMARTMENT, FR 10 UNDER RH FLOOR OF COCKPIT (BL 7097) BRACKET SUPPORT IS CRACKED. DOT 103-33 INSTALLED WEB AND ANGLE IAW-A300-600 SRM-51-40-21.

Part: HINGE — DAMAGED (NOT REPORTED) · airframe 23,656 hrs · 14,470 cycles

DAMAGE FOUND IN AFT HINGE OF PIANO HINGE FITTINGS (ALUMINIUM LAYER 19F, 20F, 21F, 22F, 24F, 25F, 26F) (STEEL LAYER 20D). INSTALLED NEW HINGE AT MDC DOOR AFT SECTION, IAW A300-600 SRM 51-40-21, AND SRM 51-49-00. (T89019). VERIFIED HINGE WAS INSTALLED USING EXISTING PARTS.

Part: CROSSBEAM — MECHANIC ERROR (FRM 16A) · airframe 23,656 hrs · 14,470 cycles

E/E COMPARTMENT, FR16A, UNDER PANEL 121RF, DOUBLE DRILLED SCREW HOLE, BRACKET SUPPORT IS DAMAGE. INSTALLED NEW CROSSBEAM IAW SRM 51-40-21.

Part: BRACKET — CRACKED (FRM 38) · airframe 23,656 hrs · 14,470 cycles

CRACKED BRACKETS AT FWD CARGO BULKHEAD FR38.2 INNER SIDE OF AFR CARGO WALL. VERIFIED INSTALLATION OF 5 EA BRACKETS ON FWD CARGO BULKHEAD FR38.2 IAW-A300-600 SRM-51-40-21.

Part: SEAT TRACK — CORRODED (FRS 79-80) · airframe 23,656 hrs · 14,470 cycles

SEAT TRACK BETWEEN FR79 AND FR80 HAS CORROSION AT Y0. INSTALLED NEW SEAT TRACK, U-SECCTION SPLICE (02 E/A) AND REPAIR ANGLE (01 E/A) IAW SRM 53-10-16 AND S.R.M. 51-40-21. ACCOMPLISH CATEGORY A REPAIR PER SRM REV 40 CHAPTER 53-10-16-201 PARAGRAPH 4 FIGURE 201B.

Part: BRACKET — BROKEN (FRM 38) · airframe 23,656 hrs · 14,470 cycles

BROKEN BRACKETS SUPPORT AT FWD CARGO BULKHEAD FR 38.2 L/H WALL (2 EA). APPLIED PROTECTIVE SURFACE TREATMENT IAW SRM 51-21-10 AND EO M-5100-2780-L REQUEST TO INSTALL. INSTALLED BRACKETS (2EA) IAW SRM A300-600 51-40-21.

Part: SKIRT — CRACKED (NR 1 NACELLE) · airframe 23,656 hrs · 14,470 cycles

NR 1 ENGINE OBD T/R CENTER UPPER EDGE PYLON SIDE FWD FINGER ( SKIRT ) CRACKED. INSTALLED NEW PART EXTRUSION EDGING ON NR 1 ENGINE OBD T/R CENTER UPPER EDGE PYLON SIDE FWD. FINGER IAW SRM 51-40-21.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 23,311 hrs · 14,278 cycles

ATB. GEAR DID NOT RETRACT, PUT HANDLE DOWN GOT 3 GREEN T/S PER TSM 32-61-00/101, REPLACED PROXIMITY DETECTOR PROCESSING UNIT, 54GB, PER AMM 32-31-71/401; OPS CHKS GOOD, OK FOR SVC

Part: CONTROL LEVER — INOPERATIVE (MLG) · airframe 22,764 hrs · 13,942 cycles

AFTER TO IN IAH PLACED THE GEAR LEVER IN THE "UP" POSITION. GEAR REMAINED DOWN, "L/G RETRACTION INOP" ON ECAM. MOVED GEAR LEVER TO "DOWN" POSITION CYCLED BACK TO "UP" AND GEAR EXTENDED NORMALLY IN AUS. LANDING GEAR RETRACT SYS DEFERRED PER MEL 32-30-01. DMP 32-30-01, PLACARD INSTALLED. DI LOG UPDATED.TROUBLESHOT PER ASM 32-31-00. CHECK RESISTANCE ON 3GA L/G SELECTOR VALVE C TO BE AND E TO F, RESISTANCE CHECK GOOD. REMOVED AND REPLACED L/G CONTROL LEVER 2GA IAW AMM 32-31-11. PERFORMED OPS TEST WITH SIMULATOR BOX AND OPS CHECK OF SELECTOR VALVE PER AMM 32-31-12. OPS TEST GOOD, NO DEFECTS NOTED.

Part: DOOR — INOPERATIVE (DOORS) · airframe 22,340 hrs · 13,664 cycles

INSPECTION TYPE:N/ADURING CLIMB WITH NO ECAM INDICATIONS THE AUDIBLE MAIN CABIN DOOR TONE ACTIVATED WITH ASSICIATED ILLUMINATED RED BAR BY THE SLIDE ARM HANDLE. THE DOOR CONTROL HANDLE WAS IN THE DOWN CLOSED POSITION BUT DID HAVE SOME SLIGHT PLAY. I PUSHEDVERIFIED ADJUSTMENT AND OPERATION OF ENTRY DOOR PER AMM 52-10-20 STEP B (6) NO DEFECTS NOTED

Part: LANYARD — BROKEN (L1 DOOR) · airframe 21,960 hrs · 13,432 cycles

LANYARD BROKEN ON CREW ENTRANCE DOOR. THE LANYARD HOLDS PIN FOR ARMING CREW ENTRANCE DOOR. REMOVED DOOR PANELS IAW AMM 52-10-13 PB 401. REPAIRED LANYARD AND REINSTALLED LANYARD ON CREW ENTRY DOOR. REINSTALLED DOOR PANELS. A/C OK TO CONTINUE

Part: NONE — WARNING LIGHT (DOOR) · airframe 21,869 hrs · 13,378 cycles

INSPECTION TYPE:SDRCLIMBING THROUGH 32,000' DOOR (L1 ) SLIDE WARNING BUZZER ACTIVATED AND RED WARNING LIGHT ILLUMINATED PUSHED ON DOOR HANDLE AND WARNINGS CEASED. GREEN LOCK INDICATOR VISIBLE. NO ECAM WARNING OF PRESSURIZAITON LOSS.PERFORMED DOOR WARNING SWITCH TEST REF AMM 52 71 00. TEST GOOD IDICATIONS ARE NORMAL. NO DEFECTS NOTED.

Part: NONE — NONE (LANDING GEAR) · airframe 21,132 hrs · 12,955 cycles

INSPECTION TYPE:N/ALANDING GEA DELAYED ITS RETRACTION GEAR DOORS OPENED GEAR STILL SHOWED DOWN& LOCKED. GEAR LEVER WAS VERIFIED IN UP DETENT. FIRST OFFICER TOUCHED GEAR LEVER RETRACTION INITIATED THEN NORMAL.REMOVED AND REPLACED LANDING GEAR NORMAL CONTROL MICRO SWITCH UNIT 2GA PER 32-31-11-04-01. OPS NORMAL

Part: NONE — INDICATION (DOOR) · airframe 20,935 hrs · 12,851 cycles

INSPECTION TYPE:N/ADURING CRUISE FLIGHT DOOR UNLOCK LIGHT APPEARED AND TONE SOUNDED. DOOR WAS VERFIED CLOSE BY ECAM. PHONE PATCH TO AMC. RECOMMEND JIGGLE DOOR. AFTER JIGGLING DOOR LIGHT EXTINGUISHED & TONE CEASED.RESTED DOOR WARNING SYSTEM ON CREW ENTRY DOOR PER MM 52-70-00 TEST GOOD. OK FOR CONTINUED USE.

Part: NONE — CRACKED (FR 11Y953) · airframe 20,797 hrs · 12,780 cycles

INSPECTION TYPE:1CAT FRAME 11 APPROX Y953 FOUND Z ANGLE CRACKED AT LAV MOUNTING PLATEREPAIR PER EO A300-5310-82088-A

Part: NONE — CRACKED (FR 11Y953) · airframe 20,797 hrs · 12,780 cycles

INSPECTION TYPE:1CAT FRAME 11 APPROX Y953 FOUND Z ANGLE CRACKED AT LAV MOUNTING PLATEREPAIR PER EO A300-5310-82088-A

Part: FITTING — CRACKED (FR 6 LH) · airframe 20,797 hrs · 12,780 cycles

INSPECTION TYPE:A300REF EO A300-5310-46789-G FR 46 LH NEEDS FURTHER INSPECTION FOR POSSIBLE CRACKREPAIRED PER EO A300-5310-46789-G APPENDIX J

Part: FITTING — CRACKED (FR 46 LH) · airframe 20,797 hrs · 12,780 cycles

INSPECTION TYPE:A300REF EO A300-5310-46789-G FR 46 RH NEEDS FURTHER INSPECTION FOR POSSIBLE CRACKREPAIRED PER EO A300-5310-46789-G APPENDIX K

Part: FITTING — CRACKED (FR 45 LH) · airframe 20,797 hrs · 12,780 cycles

INSPECTION TYPE:A300REF EO A300-5310-46789-G FR 45 LH NEEDS FURTHER INSPECTION FOR POSSIBLE CRACKREPAIRED PET EO A300-5310-46789-G APPENDIX J

Part: CLEAT — CRACKED (L/H WING) · airframe 20,797 hrs · 12,780 cycles

INSPECTION TYPE:CLT WING BELOW #3 SPOILER I/B HINGE END RIB INTERCOSTAL WEB FWD BRACKET CRACKEDFABRICATED AND INSTALLED IAW SRM DRAWING 25A57240071 AND SRM 51-40-21

Part: BRACKET — CRACKED (L/H WING) · airframe 20,797 hrs · 12,780 cycles

INSPECTION TYPE:CLT WING BELOW #3 SPOILER I/B HINGE END RIB INTERCOSTAL WEB FWD BRACKET CRACKEDFABRICATED AND INSTALLED IAW SRM DRAWING 25A57240071 AND SRM 51-40-21

Part: BRACKET — CRACKED (#2 FLAP) · airframe 20,797 hrs · 12,780 cycles

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

Part: DOUBLER — PUNCTURED (LH WING) · airframe 20,795 hrs · 12,779 cycles

INSPECTION TYPE:A300LT WING TOP SURFACE JUST FWD OF #1 SPOILER WING FIXED T/E PANEL PUNCTUREDREPAIRED PER SRM 57-51-12

Part: DOUBLER — PUNCTURED (LH WING) · airframe 20,795 hrs · 12,779 cycles

INSPECTION TYPE:A300LT WING TOP SURFACE JUST FWD OF #1 SPOILER WING WING FIXED T/E PANEL PUNCTUREDREPAIRED PER SRM 57-51-12

Part: SEAL DEPRESSOR — NONE (AFT CARGO DOOR) · airframe 20,795 hrs · 12,779 cycles

INSPECTION TYPE:CAFT CARGO DOOR CUT OUT UPPER AFT CORNER SEAL DEPRESSOR HAS GOUGE AND CRACKEDREMOVED AND REPLACED IAW SRM 51-40-21

Part: BRACKET — CRACKED (#3 FLAP) · airframe 20,698 hrs · 12,717 cycles

INSPECTION TYPE:CLT WING #3 FLAP I/B END ANGLE BRACKET CRACKEDREMOVED AND REPLACED IAW SRM 50-40-21

Part: WARNING BUZZER — FALSE ACTIVATION (DOORS) · airframe 20,644 hrs · 12,684 cycles

INSPECTION TYPE:N/ADURING CLIMB PASSING APPROX F230 FOOR SLIDE WARNING BUZZER AND LIGHT WERE ON. TRIED DISARMING; REARMING SLIDE LEVER. NO EFFECTS. LIGHT & HORN DID STOP WITH SLIDE DISARMED.CLEANED LIMIT SWITCH 9WN, OPS TESTED NO FAULTS NOTED IAW AMM 52-73-13-0501. GROUND CHKS SATISFACTORY

Part: SEAL — LEAKING (DOOR) · airframe 20,518 hrs · 12,616 cycles

CREW ENTRY DR LK - SEAL LK APPEARS TOP RT SIDE OF DR. LK START@FL340. DESCENDED FL320, NO CHG. CABIN PRESS IND NRML @FL340 DELTA P 8.1 CABIN ALT 6000FT. PASSING FL210 DELTA P 5.5 PSI CABIN ALT 5400FT.R&R'D DR SEAL 52-10-18-0401. OPS LK CK OK. LP 090741 FWD DR SEAL RPLCD 52-10-18-0104 PARD-5 MAT#16-003. DEF EO A300-5210-58385A.ACCOMPLISHED PERM REPAIR OF FWD ENTRY DOOR SEAL LACQUER INSTALL IAW EO A300-5210-58385-A.

Part: SEAL — LEAKING (L1 DOOR) · airframe 20,250 hrs · 12,444 cycles

INSPECTION TYPE:NAREACHING FL 330A LOUD HIGH PITCH SOUND STARTED NEAR COCKPIT ENTRY WAY. PRESSURE STABLE AND ALL DOORS SHOWING CLOSED. CABIN ALT 5560 STOPPED @ 19200 AND 11940 CABIN ALTREPAIRED CREW ENTRY DOOR SEAL IAW EO A300-5210-20334-C

Part: DOOR — MALFUNCTIONED (CABIN) · airframe 20,250 hrs · 12,444 cycles

INSPECTION TYPE:N/ACREW ENTRY DOOR MECH FLAG SHOWING HALF LOCKED ON LOCK POSITION WHEN DOOR IS COLOSED. CREW ENTRY FLAG DEFERRED UNDER MEL 52-11-02. THIS OPENS M745049.PERFORMED ADJUSTMENT AND OPS CK OF FWD CREW DOOR IAW AMM 52-10-00-0501. OPS CK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. THIS CLEARS M745049

Part: FLAP — MALFUNCTIONED (K FLAP SYSTEM) · airframe 19,576 hrs · 12,065 cycles

INSPECTION TYPE: NA ATB, NO EMERGENCY DECLARED/NO EQUIPMENT USED. A/C WAS OUT OF SERVICE. KRUEGER DID RETRACT IN FLIGHT. THE KRUGER LIGHT ILLUMINATED AT FL 346, INCREASED. RAN ECAM AND DESCENDED TO COMPLY WITH ECAM/ILLEG OF A300/.65 MAX. REMOVED AND REPLACED LEFT NOTCH FLAP ACTUATOR, REF A300 AMM 27-88-15-0401 1 THRU AND 1D (1).

Part: WARNING HORN — FALSE ACTIVATION (DOOR SLIDE) · airframe 19,103 hrs · 11,780 cycles

FORWARED ENTRY DOOR SLIDE WARNING HORN SOUNDS CONTINUOUSLY. WARNING HORN CAME ON DURING CLIMBOUT AT FL 280. HORN EXTINGUISHED DESCENDING THRU 10000 FT.PERFORMED WARNING HORN TEST FOR LT ENTRY DOOR IAW AMM 52-73-12. PERFORMED TEST OF LIMIT SWITCH FOR EMERGENCY ESCAPE SLIDE, NO FAULTS NOTED AT THIS TIME IAW AMM 57-73-13.

Part: LIMIT SWITCH — MALFUNCTIONED (L1 DOOR) · airframe 18,893 hrs · 11,655 cycles

DURING CRUISE FLIGHT AT FL360, RED LIGHT BEHIND DOOR ARMING LEVEL ILLUMINATED. NO OTHER ABNORMAL INDICATIONS OBSERVED. DIFF PRESSURE NORMAL. SLIDE PRESSURE NORMAL, LIGHT EXTINGUISHED AFTER LANDING. MAIN CABIN DOOR LIMIT SWITCH REPLACED, ADJUSTED, AND TESTED IAW AMM 52-73-13-0401/0501.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 18,885 hrs · 11,650 cycles

INSPECTION TYPE:N/A DURING CLIMBOUT, MAIN ENTRY DOOR SLIDE ARMED WARNING HORN AND RED WARNING LIGHT CAME ON STEADY. AT TOP OF CLIMB, SLIDE ARMING LEVER CYCLED "DISARMED" BACK TO "ARMED" HORN AND LIGHT STOPPED IN "DISARMED" POSITION, BUT CAME BACK ON W/ "ARMED" ACCOMPLISHED AMM 52-71-00, PAGE (1) CLOSED DOOR IN ARM & DISARMED POSITION NUMEROUS TIMES OPS CKD NORMAL AT PRESENT TIME.

Part: HANDLE — OBSTRUCTED (PAX DOOR) · airframe 17,585 hrs · 10,901 cycles

CABIN DOOR AUDIO AND LIGHT CAME CLIMBING THROUGH FL250. PUSHED ON DOOR HANDLE BOTH WENT OUTREMOVED LARGE CHUNK OF DEBRIS FROM THE ENTRY DOOR INTERIOR CONTROL HANDLE. ALSO CLEANED AND LUBRICATED THE SAME. OPS CHECKS NORMAL PER AMM 52-70-00 PG 501. OK FOR SERVICE.

Part: SEAL DEPRESSOR — CONTAMINATED (PAX DOOR) · airframe 17,346 hrs · 10,764 cycles

DURING CLIMB FROM FL 230 TO FL 310 ENTRY DOOR SEAL WHISTLED WITH DIFF PRESS @ 7.9 AND CABIN @ 4900' AND CLIMBING AIRCRAFT HELD PRESSURIZATION IN CRUISE @ FL310.FOUND SEAL DEPRESSOR AT TOP FWD CORNER OF DOOR CONTAMINATED AND NOT SEALING PROPERLY CLEANED SEAL AND DEPRESSOR OPS CK NORMAL REF AMM 52-10-11 APU BLEED GOT TO DELTA 4 AND 4100' CABIN ALT FOR OPS CK.

Part: DOOR — OUT OF ADJUST (ENTRY) · airframe 17,333 hrs · 10,751 cycles

INSPECTION TYPE:N/A CLIMBOUT LOUD SQUEAL PASSING 15000 FT TO CRUISE AT FL 290 DESCENT OPS NORMAL SOUND EMANATES FROM ENTRY DOOR AREA. ADJUSTED ENTRY DOOR IN REF TO AMM 52-10-11 PARA 1 A. OPS NORMAL OK FOR CONT FLIGHT.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 17,329 hrs · 10,747 cycles

INSPECTION TYPE:12YR AFT PIT FLOOR PANEL 151MG CRACKED. FABRICATED AFT PIT FLOOR PNL 151MG IAW SREO A300-5320-57698-A.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 17,329 hrs · 10,747 cycles

INSPECTION TYPE:12YR AFT PIT FLOOR PANEL 151VF PUNCTURED. FABRICATED AFT PIT FLOOR PANEL 151VF IAW SREO A300-5320-57698-A.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 17,329 hrs · 10,747 cycles

INSPECTION TYPE:12YR AFT PIT FLOOR PANEL 151VF PUNCTURED. FABRICATED AFT PIT FLOOR PANEL 151VF IAW SREO A300-5320-57698-A.

Part: FLOOR PANEL — CRACKED (CARGOBAY) · airframe 17,329 hrs · 10,747 cycles

INSPECTION TYPE:12YR AFT PIT FLOOR PANEL 151SF CRACKED. FABRICATED AFT PIT FLOOR PANEL 151SF IAW SREO A300-5320-57698-A.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 17,329 hrs · 10,747 cycles

INSPECTION TYPE:12YR AFT PIT FLOOR PANEL 151KG CRACKED. FABRICATED AFT PIT FLOOR PANEL 151KG IAW SREO A300-5320-57698-A.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 17,329 hrs · 10,747 cycles

INSPECTION TYPE:12YR FWD PIT FLOOR PANEL 131DE PUNCTURED. FABRICATED FLOOR PANEL 131DE IAW SREO A300-5320-57698-A.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 17,329 hrs · 10,747 cycles

INSPECTION TYPE:12YR AFT PIT FLOOR PANEL 151NG CORNER DELAMINATED. FABRICATED AFT PIT FLOOR PANEL 151NG IAW SREO A300-5320-57698-A.

Part: FLOOR PANEL — CRACKED (CARGOBAY) · airframe 17,329 hrs · 10,747 cycles

INSPECTION TYPE:12YR AFT PIT FLOOR PANEL 151LG CRACKED. FABRICATED AFT PIT FLOOR PANEL 151LG IAW SREO A300-5320-57698-A.

Part: DOOR SEAL — DIRTY (DOOR) · airframe 17,309 hrs · 10,737 cycles

INSPECTION TYPE:N/A LOUD HIGH PITCHED SQUEAL AT CRUISE FL 330. LOUDER IN SUPERNUMERARY AREA. SQUEAL NOISE REDUCED FL 350. BUT STILL OCCURRED. CHECKED FWD CREW SEALS REF AMM 52-10-18 NO DEFECTS NOTED CLEANED SEAL PRESSURIZED ACFT IN REF TO AMM 05-56-00 CHK'D FOR LEAKS NO LEAKS OR NOISE NOTED IN SUPERNUMERARY AREA ALSO CHKS GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 17,309 hrs · 10,737 cycles

INSPECTION TYPE:NA EMERGENCY EXIT SIGN ABOVE L1 DOOR INOP. R&R DOOR SIGN MODULE IAW AMM 33-51-13/0401. REPAIRED WIRING TO DOOR SIGN IAW ESPM 20-33-00/201 CONFIG 01. OPS CKS GOOD. EFF SOURCE REF: IPC 33-51-04-09B.

Part: LIMIT SWITCH — OUT OF ADJUST (CABNI DOOR) · airframe 17,298 hrs · 10,729 cycles

INSPECTION TYPE:NA ON CLIMBOUT, MAIN CABIN DOOR WARNING HORN & LIGHT ACTIVATED AND REMAINED ON THROUGHOUT FLIGHT. DEF'D PER MEL 52-11-01-4, PLACARD INSTALLED. ACCOMPLISHED DMP 52-11-01-4. **SUPPLEMENTAL SDR** PERFORMED LIMIT SWITCH ADJ TEST FOR PWN PER MM 52-73-13 0501. THIS CLEARS DMI M670213.

Part: GIRT BAR — OUT OF POSITION (CREW DOOR) · airframe 17,294 hrs · 10,726 cycles

INSPECTION TYPE:N/A WARNING LIGHT & HORN FOR CREW DOOR CAME ON DURING CLIMBOUT AND REMAINED ON THRU FLIGHT. DISARM HANDLE TURNED OFF THE WARNING & OPERATED NORMALLY. REPOSITIONED SLIDE ON GIRT BAR. PERFORMED ADJ/TEST PER MM 52 73 00 0501. OPS NORMALLY.

Part: ANGLE — CRACKED (APU FIRE WALL) · airframe 17,285 hrs · 10,718 cycles

INSPECTION TYPE:12YR, Z ANGLE ATTACHED TO THE FORWARD SIDE OF THE APU FIREWALL APPROX 2 FEET DOWN FROM CROWN AT BLO IS CRACKED AT THE SAFETY WIRE HOLEREPAIRED IAW UPS EO A300-5320-53165-B

Part: FITTING — CRACKED (LT WING) · airframe 17,285 hrs · 10,718 cycles

INSPECTION TYPE:C123 LT WING FRAME 40 LOWER FASTENER HOLE HAS A CRACK INDICATION NOTED AT THE 10 O'CLOCK POSITION. CRACK STARTED AT APPROX .18 INCH DEPTH AND ENDS AT APPROX .35 IN DEPTH. REPAIRED PER REO-G21928 REV IR AND EO A300-5710-72400-A.

Part: FLOOR PANEL — CRACKED (AFT CARGO BAY) · airframe 17,285 hrs · 10,718 cycles

INSPECTION TYPE:123CAFT PIT FLOORPANEL 152VF CRACKEDFABRICATED REPLACEMENT 152VF FLOORPANEL IAW SREO A300-5320-16407-E

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 17,285 hrs · 10,718 cycles

INSPECTION TYPE:12YRMAIN CABIN FLOOR BOARD 241VM DAMAGEDREPAIRED PER EO A300-5320-40552-B

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 17,285 hrs · 10,718 cycles

INSPECTION TYPE:12YR, MAIN CABIN FLOOR BOARD 222DG DAMAGED.REPAIRED FLOOR BOARD PER EA #A300-5320-40552-B

Part: FLOORBOARD — PUNCTURED (AFT CARGO BAY) · airframe 17,285 hrs · 10,718 cycles

INSPECTION TYPE:12YRAFT PIT FLOOR BOARD 152MG PUNCTUREDREPAIRED PER UPS EO A300-5320-16407-E

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 17,285 hrs · 10,718 cycles

INSPECTION TYPE:123C, FWD PIT FLOOR PANEL 132RG CRACKED. FABRICATED REPLACEMENT 132RG FLOOR PANEL IAW SREO A300-5320-16407-E

Part: FLOOR PANEL — CRACKED (AFT CARGO BAY) · airframe 17,285 hrs · 10,718 cycles

INSPECTION TYPE:123CAFT PIT FLOORPANEL 151QF CRACKED.FABRICATED REPLACEMENT 151QF FLOOR PANEL IAW SREO A300-5320-16407-E

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 17,285 hrs · 10,718 cycles

INSPECTION TYPE:123C, BULK PIT FLOORPANEL 161GF CORNER DELAMINATED. FABRICATED REPLACEMENT FLOOR PANEL IAW SREO A300-5320-16407-E.

Part: FLOOR PANEL — CRACKED (AFT CARGO BAY) · airframe 17,285 hrs · 10,718 cycles

INSPECTION TYPE:12YRAFT PIT FLOOR PANEL 152NG CORNER DELAMINATED.REPAIRED PER UPS EO A300-5320-16407-E

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 17,285 hrs · 10,718 cycles

INSPECTION TYPE:12YRMAIN CABIN FLOOR BOARD 231MJ DAMAGEDREPAIRED FLOOR BOARD PER EO A300-5320-40552-B

Part: FLOOR PANEL — CRACKED (FWD CARGO BAY) · airframe 17,285 hrs · 10,718 cycles

INSPECTION TYPE:12YR, FWD PIT FLOOR PNL 132DE CRACKEDREPAIRED PER UPS EO A300-5320-16407-E

Part: FLOOR PANEL — CRACKED (AFT CARGO BAY) · airframe 17,285 hrs · 10,718 cycles

INSPECTION TYPE:12YRAFT PIT FLOOR PANEL 152SF PUNCTUREDREPAIRED PER UPS EO A300-5320-16407-E

Part: FLOOR PANEL — PUNCTURED (AFT CARGO BAY) · airframe 17,285 hrs · 10,718 cycles

INSPECTION TYPE:12YRAFT PIT FLOOR PANEL 152KG PUNCTUREDREPAIRED PER UPS EO A300-5320-16407-E

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 17,285 hrs · 10,718 cycles

INSPECTION TYPE:12YRMAIN CABIN FLOOR BOARD 242LJ DAMAGEDREPAIRED PER EO A300-5320-40552-B

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 17,285 hrs · 10,718 cycles

INSPECTION TYPE:123C, FWD PIT FLOOR PANEL 132PG CRACKED. FABRICATED REPLACEMENT FLOOR PANEL IAW SREO A300-5320-16407-E.

Part: FLOORBOARD — PUNCTURED (FWD CARGO BAY) · airframe 17,285 hrs · 10,718 cycles

INSPECTION TYPE:123CFWD PIT PANEL 132SG PUNCTUREDFABRICATED REPLACEMENT 132SG FLOORPANEL IAW SREO A300-5320-16407-E

Part: BARRIER — CORRODED (FUSELAGE) · airframe 17,285 hrs · 10,718 cycles

INSPECTION TYPE:123C MAIN CABIN LEFT SIDE, AFT SIDE OF L-SHAPED SOLID BARRIER, LOWER SURFACE HAS EVIDENCE OF CORROSION IN SEVERAL AREAS. MARKED AND STREAMER ATTACHED, FR19-FR20REPAIRED PER PROGRESSIVE REO-G21932/EO #A3005310-72396-A/ EO# A300-2550-72399-A

Part: BRACKET — CRACKED (FRAME 54) · airframe 17,285 hrs · 10,718 cycles

INSPECTION TYPE:12YR, AFT CARGO, FR54, LEFT CENTER UPPER STRUCTURE, PANEL IS CRACKED.REMOVED AND REPLACED BRACKET IAW A300-600 SRM 51-40-21.

Part: SUPPORT — CRACKED (FRAME 54) · airframe 17,285 hrs · 10,718 cycles

INSPECTION TYPE:12YR, AFT CARGO, FR54, RIGHT HAND OUTBOARD UPPER STRUCTURE, PANEL SUPPORT IS CRACKED.REMOVED AND REPLACED BRACKET IAW A300-600 SRM 51-40-21.

Part: SUPPORT — CRACKED (FRAME 54) · airframe 17,285 hrs · 10,718 cycles

INSPECTION TYPE:12Y, RAFT CARGO, FR54, CENTER UPPER STRUCTURE, PANEL SUPPORT IS CRACKED.REMOVED AND REPLACED BRACKET IAW A300-600 SRM 51-40-21.

Part: STATIC WICK — CORRODED (RT WING TE FLAP) · airframe 17,285 hrs · 10,718 cycles

INSPECTION TYPE:123C, RIGHT WING OUTBOARD TRAILING EDGE FLAP, STATIC WICK BASE IS COMING LOOSE FROM THE UPPER OUTBOARD SURFACE OF THE FLAP.REPAIRED PER UPS EO A300-5720-72196-A

Part: DOOR SEAL — TORN (ENTRY DOOR) · airframe 17,271 hrs · 10,710 cycles

INSPECTION TYPE:N/A ENTRY DOOR SEAL HAS TEARS THROUGH ALL LAYERS. REPAIRED MAIN ENTRY DOOR SEAL PER EO A300-5210-20334-C.

Part: WARNING SYSTEM — INTERMITTENT (COCKPIT) · airframe 17,247 hrs · 10,696 cycles

INSPECTION TYPE:N/A **DIVERSION** NR 2 REVERSER UNLOCK CAUTION 35K FT. PERFORMED A PRECAUTIONARY APP. NO CHANGE IN YAW. CONTINUALLY CAME ON AND WENT AWAY. DEFERRED REF MEL 78-30-01 NR 2 REVERSER LOCKED OUT REF DMP 78-30-01 PLACARD INST. **SUPPLEMENTAL SDR** SYSTEM RETURNED TO NORMAL, REMOVED STICKER, IAW MEL 78-30-01. DFDR PARAMETER 22 FOR ENGINE NUMBER 2 READS CORRECTLY IAW AMM 31-31-00. THIS CLEARS M665215.

Part: MECHANISM — DIRTY (ENTRY DOOR) · airframe 16,500 hrs · 10,276 cycles

LEFT MAIN ENTRY DOOR DOOR LOCKING QUICK RELEASE PUSH BUTTON STIFF, AND LOCKING UP. CLEANED DOOR STAY MECHANISM OPS CHECK GOOD IAW AMM 52-10-00.

Part: LEVER — OUT OF ADJUST (DOOR) · airframe 16,466 hrs · 10,255 cycles

IN CLIMB PASSING FL200 LT ECAM MSG "DOOR LT FWD CABIN NOT CLOSED". WITH AURALTONE. DID NOT HAVE ABNORMAL CABIN RATE OR SUSPECT DOOR UNLOCKED LT FL330 HAD NORMAL CABIN ALTITUDE AND 0 CABIN RATE. PERFORMED ADJ TO OPERATING LEVER PER AMM 52-71-00-0501 FOR SW 43WS. IND CKS GOOD, ALSO CKD SW 7WS FOUND TO BE GOOD.

Part: NONE — NONE (LIGHT) · airframe 16,418 hrs · 10,235 cycles

DURING PREFLIGHT, FOUND THE SLIDE ARMED WARNING LIGHT WAS INOPERATIVE. BUZZER WORKS. OPS CHECKED NORMAL IAW AMM 52-73-14-04, PAR 2.D.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 16,293 hrs · 10,158 cycles

TAIL BALL DOUBLER GOUGED FR84-FR85 S-43L - S-43R. REPAIRED PER EO A3005330-69043-B.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 16,293 hrs · 10,158 cycles

FUSELAGE TAIL BALL DOUBLER GOUGED FR 84-FR85, S-43L-S-43R. REPAIRED PER EO A300-5330-69043-B. THIS IS A MAJOR REPAIR.

Part: WARNING SWITCH — DEFECTIVE (CREW DOOR) · airframe 16,170 hrs · 10,086 cycles

AT 2000' RECEIVED ECAM MESSAGE L FWD CABIN WARNING LIGHT ILLUMINATED WITH WARNING PRESSURE REMAINED NORMAL WITH ABNORMAL CABIN RATE. DEFERRED CREW ENTRY DOOR CLOSED AND LOCKED INDICATION AND WARNING PER MEL 52 31 01 1 DMP CW. REPLACED FWD CREW DOOR WARNING SWITCH 7WS AS REQUIRED. OPS CK GOOD. REF MM 52-71-00-0401.

Part: WARNING MESSAGE — FALSE INDICATION (PAX DOOR) · airframe 16,092 hrs · 10,040 cycles

DURING CLIMB OUT, AT 21,000 FT, HAD A CABIN DOOR UNLOCK INDICATION. COMPLETED ECAM ITEMS AND RETURNED TO DEPARTURE. COMPLIED WITH A ADJUSTMENT AND TEST IAW AMM 52-70-00-PB0501, GROUND OPS CHECKED GOOD.

Part: DOOR — NOT SEATED (MAIN PAX) · airframe 16,021 hrs · 10,000 cycles

DURING CLIMB OUT, HAD A FWD ENTRY DOOR OPEN INDICATION WITH ECAM MESSAGE. PRESSURE REMAINED NORMAL. LEVELED AT FL160 AND WENT BACK TO INSPECT DOOR. FOUND DOOR HANDLE TO BE SLIGHTLY OUT OF FULL CLOSED POSITION. RESEATED THE HANDLE AND PERFORMED ADJUSTMENT TEST OF CREW ENTRY DOOR LEFT IAW AMM 52-10-11-0601. ALL FOUND TO BE WITHIN LIMITS. PERFORMED DOOR WARNING TEST IAW AMM 52-70-00. TEST PASS. OK FOR CONTINUED SERVICE

Part: WARNING LIGHT — FALSE INDICATION (L1 DOOR SLIDE) · airframe 15,730 hrs · 9,833 cycles

AIR TURNBACK, MAIN CABIN DOOR SLIDE WARNING LIGHT FLASHES IN FLIGHT. PERFORMED AN OPS TEST OF THE ASPSU IAW MM 52-73-00-501, FAULTS NOTED.

Part: SLIDE — NO TEST · airframe 15,657 hrs · 9,790 cycles

EMERGENCY EXIT SLIDE LIGHT WILL NOT TEST. TROUBLESHOT IAW TSM 52-73-00. NO DEFECTS NOTED. PERFORMED TEST OF ASPSU IAW AMM 52-73-00. OPS CHECKED GOOD.

Part: HANDLE — NOT SEATED (PAX DOOR) · airframe 15,608 hrs · 9,757 cycles

DURING CLIMBOUT, PASSING 14000 FT, RECEIVED A LT FWD CABIN NOT CLOSED ECAM WITH ASSOCIATED DOOR WARNING HORN. PRESSURE WAS NORMAL. VIEWING LOCK WINDOWS ON DOOR SHOWED PARTIAL RED, AIR TURN BACK ACCOMPLISHED. AT BLOCK IN HANDLE WASN'T FULLY SEATED. INSPECTED DOOR LOCKING IAW AMM 52-10-20. NO FAULTS FOUND. PERFORMED DOOR WARNING TEST IAW AMM 52-70-00. ALL TESTS PASSED.

Part: HANDLE — INOPERATIVE (CREW DOOR) · airframe 15,182 hrs · 9,474 cycles

CREW DOOR WILL NOT CLOSE FROM THE OUTSIDE. R & R THE EXTERIOR CONTROL HANDLE IAW AMM 52-11-21-04-01. OPS CHECKED GOOD.

Part: LIFE VEST — UNSECURE (COCKPIT) · airframe 15,097 hrs · 9,425 cycles

PANEL ON CAPTAIN`S LIFE VEST KEEPS FALLING OFF. SECURED THE LIFE VEST IAW AMM 25-60-00-0601.

Part: SKIN — DAMAGED (FRAME 20) · airframe 14,842 hrs · 9,272 cycles

FUSELAGE SKIN DAMAGED AT FRAME 20, STRINGER 28R. REPAIRED IAW EO A300-5330-63906-C.

Part: SMOKE DETECTOR — NO TEST (COCKPIT) · airframe 14,826 hrs · 9,260 cycles

DURING CLIMB OUT AT 21000 FT, RECEIVED AVIONICS SMOKE WARNING. ACCOMPLISHED ECAM & CHECKLIST PROCEEDURES. DIVERTED. NOTED 13WA SMOKE DETECTOR FOR THE COCKPIT WOULD NOT TEST ON ARRIVAL. R & R THE SMOKE DETECTOR IAW AMM 26-15-12-0401. OPS CHECKED NORMAL, WITH NO ALERTS.

Part: LAMP — INOPERATIVE (AUX LIGHT) · airframe 14,747 hrs · 9,206 cycles

LAVATORY AUXILIARY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-21-0401. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (L1 WARNING) · airframe 14,630 hrs · 9,138 cycles

CREW ENTRY DOOR ARMING LEVER RED WARNING LIGHT BULBS INOPERATIVE. R & R AUTONOMOUS BATTERIES IAW AMM 52-73-18-0401 OPS CHECKED GOOD.

Part: SMOKE DETECTOR — INOPERATIVE (E/E BAY) · airframe 14,365 hrs · 8,982 cycles

DURING CLIMB OUT PASSING 3000FT. AVIONICS SMOKE ECAM ANNUCIATED SMOKE NOT CONFIRMED BY SNIFFER FAN. MADE PRECAUTIONARY RETURN TO DEPARTURE, EMERGENCY DECLARED. ON GROUND FOUND NO SMOKE EVIDENT BY ODOR. PERFORMED TROUBLESHOOTING IAW FIM 26-15-00. REMOVED & REPLACED SMOKE SENSOR IAW AMM 26-15-12 . PERFORMED TEST OF SMOKE DETECTION IAW AMM 26-15-001 AND NO DEFECTS FOUND. SYSTEM TESTED OK. ACFT OK TO CONTINUE.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 14,047 hrs · 8,801 cycles

INSPECTION TYPE: 1C, LEFT WING CENTER FLAP OTBD LE SKIN DENTED OUT OF LIMITS. REPAIR IAW SRM 57-50-00 PARA 4H FIG 208 (SHEET 2).

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 14,047 hrs · 8,801 cycles

INSPECTION TYPE:1C, LEFT WING CENTER FLAP OTBD LE DENTED OUT OF LIMITS. REPAIR IAW SRM 57-50-00 PARA 4H FIG 208(SHEET 2).

Part: BRACKET — CRACKED (FRAME 54) · airframe 14,047 hrs · 8,801 cycles

INSPECTION TYPE: 1C, AFT CARGO BAY FORWARD BULKHEAD HAS A CRACKED VERTICAL BRACKET AT FRAME 54, BL 0. REMOVED AND REPLACED THE BRACKET IAW DWG A534107652, AND SRM 51-40-21.

Part: BRACKET — CRACKED (BULKHEAD) · airframe 14,047 hrs · 8,801 cycles

INSPECTION TYPE: 1C, AFT CARGO FWD BULKHEAD WALL HAS A CRACKED VERTICAL BRACKET AT FRAME 54, RBL 37. REMOVED AND REPLACED THE BRACKET IAW SRM 51-40-21

Part: FLOOR PANEL — PUNCTURED (MAIN CABIN) · airframe 14,045 hrs · 8,799 cycles

INSPECTION TYPE: 1C, MAIN CABIN FLOOR PANEL 241DF PUNCTURED. REPAIRED THE FLOOR PANEL IAW SREO A300-5320-42721-F

Part: LAMP — INOPERATIVE (LAVATORY) · airframe 13,258 hrs · 8,299 cycles

LAVATORY EXT POWER LAMP INOPERATIVE. REPLACED THE LAMPED IAW MM 33-51-21.

Part: STOWAGE BOX — NO TEST (COCKPIT OXYGEN) · airframe 12,514 hrs · 7,830 cycles

F/O OXYGEN MASK BOX WILL NOT TEST PROPERLY. R & R THE OXYGEN STOWAGE BOX IAW AMM 35-12-51-0401. OPS AND LEAK CHECKED NORMAL.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 12,358 hrs · 7,729 cycles

FLOOR PANEL FWD LWR CARGO BAY CRACKED. FABRICATED NEW FLOOR PANEL IAW EO 5320-16407.-E.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING MX INSPECTION LAVATORY EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-21-401.

Part: ADC — INOPERATIVE (NR 1)

FL330, ACFT ABRUPTLY STARTED DESCENDING. CAPTAIN'S IAS DROPPED TO 80 KTS, F/O READ OVER 300 IN DESCENT DISCONNECTED AP AND LEVELED ACFT USING STANDBY ADI AND AIRSPEED INDICATOR. ECAM MESSAGE INDICATING TAS AND ADC DISAGREED. ALSO NAV ADC FAILURE INDICATED ON ECAM. PERFORMED AUTOFLIGHT, OPS TEST IAW AMM 22-00-00-0501, FOUND "ADS 1 FLAG " ON MTP FAILURE RECORD. R & R NR 1 ADC IAW AMM 34-11-08-02-130A . BITE TEST CKS GOOD.

Part: FLOOR PANEL — BROKEN (FWD CARGO) · airframe 11,380 hrs · 7,105 cycles

DURING 10 YEAR INSPECTION, FWD CARGO FLOOR PANEL 132PG CORNERS BROKE OFF. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-F, APPD B.

Part: SKIN — CONTAMINATED (RT ELEVATOR) · airframe 11,380 hrs · 7,105 cycles

RIGHT ELEVATOR UPPER SURFACE FORWARD OF FASTENER NR 32 HAS FLUID IN CORE. REPAIRED RT ELEVATOR IAW 55-21-12, PARA 5.J. , FIG 212, SHEET 3, REV 25.

Part: SKIN — CONTAMINATED (LT ELEVATOR) · airframe 11,380 hrs · 7,105 cycles

LEFT ELEVATOR UPPER SURFACE FWD OF FASTENERS NR 20 AND 21 HAS FLUID IN CORE 2.3" X 2.2". REPAIRED LT ELEVATOR UPPER SKIN IAW SRM 55-21-12, PARA 5J, FIG 212, SHEET 1.

Part: SKIN — CONTAMINATED (LT ELEVATOR) · airframe 11,380 hrs · 7,105 cycles

LEFT ELEVATOR UPPER SURFACE FWD OF FASTENER NR 13 HAS FLUID IN CORE. REPAIRED LT ELEVATOR UPPER SKIN FWD OF FASTENER NR 13 IAW SRM 55-21-12, PARA 5J, FIG 212, SHEET 1 REPAIR SCHEME A, REV 25.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 11,380 hrs · 7,105 cycles

MAIN DECK CARGO FLOOR PANEL 231KH LOWER SKIN CRACKED. REPAIRED FLOOR PANEL IAW EO A300-5320-4272 1-F APPENDIX B.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 11,380 hrs · 7,105 cycles

DURING 10 YEAR INSPECTION, FLOOR PANEL 232MH TORN & PUNCTURED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-F, APP B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,380 hrs · 7,105 cycles

DURING INSPECTION, FOUND MAIN CABIN FLOORBOARD 231PH LOWER SKIN IS CRACKED. REPAIRED MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-F, APPENDIX B.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,380 hrs · 7,105 cycles

MAIN CABIN FLOORBOARD 232UG IS CRACKED AT LOWER SURFACE REPAIRED FLOORBOARD IAW EO A300-5320-42721-F, APPENDIX B.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 11,380 hrs · 7,105 cycles

DURING 10 YEAR INSPECTION, MAIN DECK CARGO FLOOR PANEL 232FF CRACKED AND PUNCTURED. REPAIRED FLOOR PANEL IAW EO A300-5320-42722-E, APPD B.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 11,380 hrs · 7,105 cycles

DURING 10 YEAR INSPECTION, MAIN DECK CARGO FLOOR PANEL 241VM CRACKED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-F, APPD B.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,380 hrs · 7,105 cycles

MAIN CABIN SEAT TRACK FOUND CORRODED 8 INCHES AFT OF FRAME 71, Y0. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201, PARA 4A, REV 25.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,380 hrs · 7,105 cycles

MAIN CABIN SEAT TRACK IS CORRODED 3 INCHES FWD OF FRAME 62, -Y953. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201, PARA 4 REV 25.

Part: SEAT TRACK — CORRODED (FRAME 62) · airframe 11,380 hrs · 7,105 cycles

SEAT TRACK CORRODED AT FRAME 62, Y953. REPAIRED SEAT TRACK IAW SRM 53-10-16, PARA 4, FIG 201, REV 25.

Part: FLOORBOARD — CRACKED (AFT CARGO) · airframe 11,380 hrs · 7,105 cycles

AFT CARGO FLOORBOARD 152UF HAS A LARGE CRACK AND DELAMINATION. FABRICATED FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX C.

Part: FLOOR PANEL — BROKEN (AFT CARGO) · airframe 11,380 hrs · 7,105 cycles

DURING 10YEAR INSPECTION, AFT CARGO FLOOR PANEL 151TF CORNER BROKE. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-F, APPD B.

Part: FITTING — CRACKED (MAIN CABIN) · airframe 11,380 hrs · 7,105 cycles

FRAME 12A, RT FUSELAGE FITTING IS CRACKED. ACCOMPLISHED REPAIR IAW EO A300-5310-23539-G, APPENDIX E.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 11,380 hrs · 7,105 cycles

DURING 10 YEAR INSPECTION, LT WING CENTER FLAP UPPER SURFACE REPAIR DOUBLER IS GOUGED BETWEEN RIB 15 AND 16. ACCOMPLISHED REPAIR ON LT WING CENTER FLAP UPPER SKIN BETWEEN RIB 15 AND 16 IAW SRM 57-50-00, FIG 205, REV 25.

Part: SKIN — CORRODED (LT WING TE FLAP) · airframe 11,380 hrs · 7,105 cycles

LEFT OTBD FLAP T/E UPPER SKIN HAS CORROSION UNDER STATIC DISCHARGE RETAINER BASE ACCOMPLISHED REPAIR ON LT OTBD FLAP T/E UPPER SKIN UNDER STATIC DISCHARGE RETAINER BASE IAW EO A300-5750-53941-A, PARA 6A.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,380 hrs · 7,105 cycles

MAIN CABIN SEAT TRACK FOUND CORRODED BETWEEN FRAMES 80-82, STA -Y450. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201, PARA 4, REV 25.

Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 11,380 hrs · 7,105 cycles

DURING INSPECTION, FRAME 79 FLOORBEAM CRACKED AT -Y1580.5. REPAIRED FLOORBEAM IAW EA 300-5310-01-A5200-IR AND EO A300-5310-54040-A.

Part: SEAT TRACK — CORRODED (FRAMES 80-82) · airframe 11,380 hrs · 7,105 cycles

DURING INSPECTION, MAIN CABIN SEAT TRACK FOUND CORRODED BETWEEN FRAMES 80-82, -Y794.3. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201, PARA 4, REV 25.

Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 11,380 hrs · 7,105 cycles

DURING INSPECTION, MAIN DECK CARGO FLOORBEAM CRACKED AT FRAME 79 AND Y1580.5. REPAIRED FLOORBEAM IAW EA 300-5310-01-A5200-IR AND EO A300-5310-54040-A.

Part: SKIN — PUNCTURED (FRAME 85) · airframe 11,380 hrs · 7,105 cycles

FUSELAGE TAIL SECTION, FRAME 85 REPAIR DOUBLER FWD OF TAIL BALL HAS A PUNCTURED SKIN. ACCOMPLISHED REPAIR ON LOWER FUSELAGE SKIN AT FR 85 FWD OF TAIL STAND BALL IAW SRM 53-10-12 PB 201, PARA 13, REV 25.

Part: SEAT TRACK — CORRODED (FRAMES 80-82) · airframe 11,380 hrs · 7,105 cycles

MAIN CABIN SEAT TRACK FOUND CORRODED BETWEEN FRAMES 80-82, Y0. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201, PARA 4, REV 25.

Part: SEAT TRACK — CORRODED (FRAMES 80-82) · airframe 11,380 hrs · 7,105 cycles

DURING INSPECTION , MAIN CABIN SEAT TRACK FOUND CORRODED BETWEEN FRAMES 80-82, Y1137.1. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201, PARA 4, FIG 201.

Part: LIGHT — INOPERATIVE (EVACUATION SLIDE)

SLIDE EVACUATION WARNING LIGHT INOPERATIVE. PERFORMED ADJUSTMENT AND TEST IAW MM 52-73-00-501. OPS CHECKED GOOD.

Part: CIRCUIT BREAKER — INOPERATIVE (SLIDE LIGHT)

MAIN DOOR EVACUATION SLIDE LIGHT INOPERATIVE. R & R CIRCUIT BREAKER 1WN IAW TSM 52-73-00 FIG 103 AND AMM 20-16-00. OPS CHECKED GOOD IAW MM 52-73-11-0401.

Part: PUMP — INOPERATIVE (HYD SYSTEM)

GREEN PUMP 2 LO PR ON ECAM & OVERHEAD. GREEN PUMP 1 LO PR ON ECAM AND OVER TEMP. GREEN HYD FLUID LVL ON ECAM AND OVRDHEAD READ 0. AFTER LANDING GEAR EXT, GREEN HYD FLUID LEVEL CAME BACK BUT LWR THAN BLUE AND YELLOW. FOUND LEAK AT B-NUT ON GREEN PUMP PSI LINE ON NR 2 ENG. REPLACED THE PUMP ON LP 328700 DUE TO LOW PSI LIGHT COMING ON DURING LOAD.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 9,574 hrs · 5,998 cycles

INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 221BG LOWER SKIN IS DELAMINATED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.

Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 9,574 hrs · 5,998 cycles

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

Part: SUPPORT — CRACKED (RT WING) · airframe 8,612 hrs · 5,379 cycles

INSPECTION TYPE: 3C, RT WING T/E SKIN SUPPORT AT ABX 144.2 CRACKED. REPAIRED RT WING T/E SKIN SUPPORT AT ABX 144.2 IAW STA-SA EA 300-5720-01-A3478-I/R AND EO A300-5720-44482-A.

Part: SWITCH — FAULTY (SLIDE WARNING)

EVACUATION SLIDE WARNING LIGHT INOP. TROUBLESHOT IAW FIM 52-73-00, FIG 101, PG 102 AND FOUND TEST SWITCH 39WN FAULTY. R & R TEST SWITCH 39WN IAW WDM 52-73-01 & MM 52-73-14-04 ITEMS 1-2C. WARNING LIGHT TEST NORMAL IAW MM 52-73- 14-04 ITEM 2D. THIS CLEARS M452049. PLACARD REMOVED.

Part: COMPUTER — INOPERATIVE (NR 1)

CLIMBING THROUGH FL 290 PITCH FEEL SYS NR1 FAILED (SYS NR2 ALREADY DEFERRED). ACCOMPLISHED QRH PROCEDURES. T/S IAW TSM 27-23-1. FOUND COMPUTER FAULT LIGHT ON FLC NR1. R & R FLC NR1 IAW MM 27-23-26-04 AND CHECKED IAW MM 27-23-00 AND MM 27-33-00 CKS NORMAL IAW REQUIRED TEST.

Part: LEVER — FAILED (ENTRY DOOR)

CREW ENTRY DOOR SLIDE DISARMING LEVER TOOK MULTIPLE TIMES TO DISARM. HANGS UP WITH ABOUT 2 INCHES OF TRAVEL LEFT TO GO. EMERGENCY CONTROL HANDLE CHECKS OK IAW MM 52-10-30-05 PAR. F. FUNCTION TEST DUB PAR 1 ITEMS 3 & 4. CLEARED M419603. REMOVED PLACARD.

Part: WARNING LIGHT — INOPERATIVE (ESCAPE SLIDE)

EVACUATION SLIDE WARNING LIGHT INOP. RESEATED CONNECTOR ON AUTONOMOUS STANDBY POWER SUPPLY. PERFORMED BITE CK AND CK OF EVACUATION SLIDE WARNING LIGHT AND BUZZER. TESTS NORMAL IAW AMM 52-73-00.

Part: LIGHT — INOPERATIVE (CABIN)

COURIER AREA INTERIOR EMERGENCY EXIT LIGHT SYSTEM TEST FUNCTION INOP. DEFERRED. DMP ACCOMPLISHED, PLACARD INSTALLED, 412600 ASSIGNED. PERFORMED ADJ/TEST PROCEDURE IAW AMM 33-51-00-05. NO FAULTS FOUND. OPS CHECK GOOD. PLACARD REMOVED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

CAPT GLARESHIELD EMERGENCY LIGHTS INOP. RELAMPED, OPS GOOD.

Part: FLOOR PANEL — DENTED (CARGO BAY) · airframe 5,815 hrs · 3,653 cycles

INSPECTION TYPE:5YR BULK CARGO FLOOR PANEL 161GF HAS SEVERAL DENTS. FABBED FLOOR PANEL IAW IPXA EO A300-5320-16407-C, APPX D.

Part: FLOOR PANEL — BROKEN (MAIN CARGO BAY) · airframe 5,815 hrs · 3,653 cycles

INSPECTION TYPE:5YR MAIN CARGO COMPARTMENT FLOOR PANEL 241LJ HAS BROKEN RT FWD CORNER. FABBED FLOOR PANEL IAW IPXA EO A300-5320-16407-C, APPX B.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 5,815 hrs · 3,653 cycles

INSPECTION TYPE:5YR BULK CARGO FLOOR JUST INSIDE OPENING DAMAGED REF D398737. FABBED FLOOR PANEL IAW IPXA EO A300-5320-16407-C, APPX D.

Part: FLOOR PANEL — BROKEN (MAIN CARGO BAY) · airframe 5,815 hrs · 3,653 cycles

INSPECTION TYPE:5YR MAIN CABIN COMPARTMENT FLOORBOARD 241NK, HAS BROKEN RT FWD CORNER. FABBED FLOOR PANEL IAW IPXA EO A300-5320-16407-C, APPX B.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO BAY) · airframe 5,815 hrs · 3,653 cycles

INSPECTION TYPE:5YR MAIN CABIN COMPARTMENT FLOORBOARD 252D IS DELAMINATED LT SIDE. FABBED FLOOR PANEL IAW IPXA EO A300-5320-16407-C, APPX B.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 5,815 hrs · 3,653 cycles

INSPECTION TYPE:5YR MAIN CABIN COMPARTMENT FLOORBOARD 251LG CRACKED RT SIDE. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-C APPX B.

Part: FLOORBOARD — BROKEN (CABIN) · airframe 5,815 hrs · 3,653 cycles

INSPECTION TYPE:5YR MAIN CABIN FLOORBOARD 252MG BROKEN IN HALF. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-C, APPX B.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 5,815 hrs · 3,653 cycles

INSPECTION TYPE:5YR BULK CARGO COMP FLOOR PANEL 161JF LOWER SURFACE 4 INCHES OF DELAMINATION UNDER FILLER REPAIR. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-C APPX D.

Part: SKIN — GOUGED (TE FLAP) · airframe 5,815 hrs · 3,653 cycles

INSPECTION TYPE:5YR LT WING CENTER FLAP UPPER SKIN GOUGED, 18 INCHES FWD OF RUB STRIP, JUST O/B OF NR 3 FLAP TRACK. FABBED AND INSTALLED REPAIR DOUBLER IAW A300 SRM 57-50-00, PG 217-218, PARAGRAPH 4E AND PG 220 FIG 205, AND 51-31-00, PG 23-24, TABLE 3 SHT 3.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 5,815 hrs · 3,653 cycles

INSPECTION TYPE:5YR BULK CARGO FLOOR PANEL 161HF HAS A LARGE DENT AND SKIN DELAMINATION. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-C APPX D.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 5,815 hrs · 3,653 cycles

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

Part: SKIN — DAMAGED (TE FLAP)

INSPECTION TYPE:N/A CENTER FLAP LOWER SKIN DAMAGED 3.4 INCH T/E BETWEEN RIB 16 AND RIB 16A DENT MEASURES 3 X 3 X .050 INCH. PERMANENT REPAIR REF: EO A300-5750-31446-C APPENDIX A.

Part: FLAP — DENTED (LT WING)

INSPECTION TYPE:N/A LT INBOARD T/E FLAP DENT OUT OF LIMITS.

Part: COALESCER BAG — DEFECTIVE (A/C BAY)

INSPECTION TYPE:N/A HYDRAULIC MIST COMING FROM A/C VENTS. REMOVED AND REPLACED BOTH LEFT AND RIGHT WATER SEPARATOR COALESCERS WITH REFERENCE TO A300 MM 21-51-16-03. OPS CHECK NORMAL.

Part: UNKNOWN — SMOKE (COCKPIT)

INSPECTION TYPE:N/A STARTED APU N2 GOT TO 25% - 30%. THE AVIONICS SMOKE LIGHT Y BELLS CAME ON AND SMOKE ENTERED THE FLT DECK. SHUTDOWN APU AND BATTERY SMOKE STOPPED. REF TSM 21-20-00. OPERATED A/C ELECTRICAL SYSTEM ON GROUND. ENG NOT RUNNING. A/C AND DC OPS GOOD. RAN APU AND PNEUMATICS. COULD NOT DULICATE CONDITION. SUSPECT EXTERNAL FUME INGESTION.

Part: LEVER — STIFF (SLIDE ARM)

WHILE DISARMING SLIDE, LEVER HANGS UP 2/3 OR THE WAY. REQUIRES FIRM MOTION TO GET PAST 2/3 POSITION. CLEANED DEBRIS FROM GIRT BAR FITTINGS AND GREASED GIRT. MEASURED HANDLE FORCE AT 18 LBS. OK PER MM 52-10-11-05.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A LAV EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT.

Part: LIGHT — INOPERATIVE (PAX DOOR SLIDE)

SLIDE TEST LIGHT ON MAIN ENTRY DOOR INOP. REMOVED AND REPLACED ASPSU BATTERY PACKS IAW MM 52-73-18-4, CKS GOOD IAW MM 52-73-00-1 501.

Part: GIRT BAR — TWISTED (COCKPIT)

INSPECTION TYPE:N/A UNABLE TO DISARM ENTRY DOOR SLIDE. HANDLE WILL TRAVEL APPROX 3/4 AFT. ECAM INDICATION REMAINS AS SLIDE ARMED. FOUND GIRT BAR SKIRT TWISTED AND BINDING RELEASE MECH. ADJUSTED SKIRT, OPS CK NORMAL PER MM 25-61-21-4.

Part: SLIDE — UNSERVICEABLE (CABIN)

ESCAPE SLIDE PRESSURE NEEDLE SHOWS IN RED RANGE, DEFERRED M296868. REMOVED AND REPLACED ESCAPE SLIDE PER A300 CH MM 25-61-21-4 M296868 CLEARED, PLACARD REMOVED.

Part: WARNING LIGHT — INOPERATIVE (COCKPIT)

EVACUATION SLIDE WARNING LIGHT INOP. EVAC SLIDE BUZZER AND LIGHT OPS NORMAL. THIS CLEARS M295390 PER MM 52-73-12-4

Part: UNKNOWN — UNKNOWN (FUSELAGE)

CAPTAIN REPORTED A LOUD THUNK 5 TIMES IN FLIGHT. THE NOISE BECAME LOUDER AND EFFECTED THE AIRPLANE AND FLIGHT CONTROLS. AT THIS TIME AN INFLIGHT EMERGENCY WAS DECLARED. PERFORMED BOW TS 1883 REV 0098 WITH NO FAULTS NOTED.

Part: WARNING LIGHT — INOPERATIVE (ESCAPE SLIDE)

INSPECTION TYPE:N/A EVACUATION SLIDE WARNING LIGHT INOP, DFRD M287411. RESET ASPSU, OPS NORMAL, REF AMM 52-73-00-5.