N723FD

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 49,090 hrs · 29,735 cycles

ON DESCENT INTO MEM RECEIVED ECAM YELLOW SYS PUMP LO PRESS. DETERMINED YELLOW SYS LOW QUANTITY. COMPLIED WITH ECAM/QRH. UPON INVESTIGATION OF HYDRAULIC LEAK, FOUND YELLOW SYS ISOLATION VALVE BLOCK LEAKING. FOUND O-RINGS FROM VALVE BLOCK PLUGS TORN. REPLACED O-RINGS IAW MM 27-14-21-04. LEAK CHECK GOOD. A/C OK FOR SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (E/E BAY) · airframe 48,256 hrs · 29,265 cycles

AVIONICS SMOKE LIGHT CAME ON DURING APPROACH TO KABE. DECLARED AN EMERGENCY. LANDED WITH NO VISIBLE SMOKE APPARENT. INSPECTED AVIONICS BAY AND NO SMOKE OR FUMES NOTED. DID NOTE HIGH HUMIDITY LEVELS IN THE LOWER CARGO/AVIONICS BAY AREAS. DEPARTURE STATION, IND, HAD PRECIPITATION REPORTED EARLIER, BUT NO NOTED RAIN INGRESSION NOTED IN AVIONICS BAY ON ARRIVAL IN ABE. REMOVED PLUG CONNECTOR FROM 13WA SMOKE DETECTOR AND AVIONICS SMOKE ALERT WAS REMOVED, CONNECTED PLUG BACK AND FAULT REAPPEARED. FAULT OF AVOINICS SMOKE WAS INDICATION ONLY DUE TO SUSPECT HIGH HUMIDITY ON A/C. REMOVED AND REPLACED SMOKE DETECTORS 11WA, 12WA AND 13WA, REF A300 AMM 26-15-12-04. ALL OPERATIONS TEST PASS. NO AVIONICS SMOKE WARNINGS PRESENT, ITEM CLOSED.

Part: SKIN — DELAMINATED (RT WING SPOILER) · airframe 48,134 hrs · 29,193 cycles

RH WING 3# SPOILER WITH DELAMINATED RH WING 3# SPOILER WITH DELAMINATED, COMPLIED WITH FEDEX EA:6-5750-T0355587 P1, MAJOR REPAIR IAW GMM 6-2-100,

Part: SKIN — DELAMINATED (LT WING SPOILER) · airframe 48,134 hrs · 29,193 cycles

LH WING 3# SPOILER WITH DELAMINATED LH WING 3# SPOILER WITH DELAMINATED, COMPLIED WITH EA:6-5750-T0355485 P1.

Part: SKIN — DELAMINATED (RT WING SPOILER) · airframe 48,134 hrs · 29,193 cycles

RH WING NR 4 SPOILER WITH DELAMINATION. COMPLIED WITH EA:6-5750-T0355586 P1. MAJOR REPAIR IAW GMM6-2-100, THIS IS A CAT A REPAIR.

Part: SKIN — DELAMINATED (LT WING SPOILER) · airframe 48,134 hrs · 29,193 cycles

LH WING 5# SPOILER WITH DELAMINATION COMPLIED WITH FEDEX EA:6-5750-T0355486 P1, MAJOR REPAIR IAW FEDEX GMM6-2-100, THIS IS A CAT A REPAIR.

Part: SKIN — DELAMINATED (RT WING SPOILER) · airframe 48,134 hrs · 29,193 cycles

RH WING NR 5 SPOILER WITH DELAMINATION. COMPLIED WITH EA:6-5750-T0355513 P1. MAJOR REPAIR IAW GMM6-2-100, THIS IS A CAT A REPAIR.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12A-14) · corrosion level 2 · airframe 48,134 hrs · 29,193 cycles

MAIN DECK CARGO, FRAMES 12A - 14, Y1456, FLOOR SUPPORT CORRODED AROUND BOLT HOLES. EXCEEDED THE ALLOWABLE THICKNESS IAW SRM 53-12-15-001. CUT OUT THE CORRODED AREA AND MANUFACTURED REPAIR PARTS IAW SRM 53-12-15, FIG.207. INSTALLED THE REPAIR IAW SRM 53-12-15, FIG.207, & SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100. THIS IS A CAT B REPAIR.

Part: SKIN — CRACKED (FRAMES 53-54) · airframe 48,134 hrs · 29,193 cycles

LOWER FUSELAGE SKIN LAP FR54 STGR44RH MARKED FASTENER FOUND A SUSPECT CRACK (1EA) REPAIRED THE CRACKED FUSELAGE SKIN AT FR54 STGR44RH PER EA# 6-5330-T0355811 P1. EA TITLE: FUSELAGE - PLATES & SKINS - FASTENER LOCATION CRACK INDICATION REPAIR - BETWEEN FR53 AND FR54 AT STGR 44RH. THE REPAIR LIFE LIMITATION WAS 6 MONTHS PER RDAS REF: 80816911/004/2020 ISSUE: A. THIS IS A CAT B REPAIR. MINOR REPAIR IAW FEDEX GMM 6 BETWEEN FR53 AND FR54 AT STGR 44RH. THE REPAIR LIFE LIMITATION WAS 6 MONTHS PER RDAS REF: 80816911/004/2020 ISSUE: A. THIS IS A CAT B REPAIR. MINOR REPAIR IAW FEDEX GMM 6-2-100.

Part: FLANGE — CRACKED (FRAME 52) · airframe 48,134 hrs · 29,193 cycles

NDT INSPECTION, CRACK WAS FOUND AT THE RH FLANGE OF GANTRY 4.RH FR52.A.

Part: BEAM — CRACKED (ZONE 200) · airframe 48,134 hrs · 29,193 cycles

NDT INSPECTION, CRACK WAS FOUND AT THE RH FLANGE OF GANTRY 4.RH FR52.A. REPAIRED THE CRACK OF THE GANTRY RH #4 AT FR52A PER AIRBUS DWG: R53810581 ISSUE: C. DETAIL REPAIR STEPS: DRILLED CRACK STOP HOLES DIA 4 TO 4.012MM AT EACH END OF CRACK AND INSTALLED THE CRACK STOP HOLE PLUGS PER AIRBUS DWG: R53810581 ISSUE: C. WET INSTALLED THE REPAIR ANGLE AND STRAP OF MOD MATERIAL KIT PER A300-600 SRM 51-40-21 & AIRBUS DWG: R53810581 ISSUE: C. MANUFACTURED AND INSTALLED A NEW BRACKET TO BE ADAPTED THE REPAIR CRACK AREA PER A300-600 SRM 51-40-21. MAJOR REPAIR IAW FEDEX GMM 6-2-100. THIS IS A CAT A REPAIR

Part: SKIN — CRACKED (FRAME 54) · airframe 48,134 hrs · 29,193 cycles

LOWER FUSELAGE SKIN LAP FR54 STGR44RH MARKED FASTENER FOUND A SUSPECT CRACK (1EA)

Part: FLOOR SUPPORT — CORRODED (FRAMES 12A-14) · airframe 48,134 hrs · 29,193 cycles

MDCC - FR12A~FR14 Y1456, FLOOR SUPPORT CORRODED AROUND BOLT HOLES

Part: GUSSET — CRACKED (WINDOW FRAME) · airframe 48,075 hrs · 29,158 cycles

F/O WINDSHIELD LOWER FRAME WORK CARD 5311010-41 FOUND HOLE 10 CRACK INDICATION IN GUSSET COMPLIED WITH E.A. 6-5310-T0354496 CRACK IN F/O WINDOW FRAME 4 GUSSET. INSTALLED NEW GUSSET IN REF TO A300 SRM 51-40-20.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 48,075 hrs · 29,158 cycles

F/O WINDSHIELD LOWER FRAME WORK CARD 5311010-41 FOUND HOLE 10 CRACK INDICATION IN GUSSET.

Part: CONTROL UNIT — INOPERATIVE · airframe 46,109 hrs · 27,938 cycles

THE RIGHT CABIN SLIDE DID NOT INDICATE ARMED AT BLOCK IN. ALSO FOUND THAT BOTH MAIN ENTRY DOORS SLIDE TEST BUTTONS WOULD NOT ENGAGE RED BLINKING LIGHT BARS. R&R AUTONOMOUS STANBY UNIT PER AMM 52-73-18-04. OPS CHECKS GOOD AND SLIDE ARM WORK PLUS DOOR ALARM MECH WAS WORKING.

Part: WIRE HARNESS — DAMAGED (MLG) · airframe 45,735 hrs · 27,726 cycles

AFTER LANDING, NO NOSE WHEEL STEERING. FO PITOT & TAT, ENG 2 ON OVERHEAD ILLUMINATED. SPOILER 4 & 1 AND 3 & 2 ON OVERHEAD ILLUMINATED. LEFT ECAM SHOWED SPOILER 4 & 1, 3 & 2, YAW DAMPER 1 OFF, PITCH TRIM 1 OFF, FO PITOT OVERHEAT, CABIN PRESS REG 1 FAULT. CAPT SPEED TAPE SHOWED RED LINE, AND BOTTOM ZIPPER. FO SPEED TAPE SHOWED THIN RED LINE WITH SPD ACFT IN SYS 1, THE PROX DET BOX 54GB HAD FAULT RED LIGHT ILLUMINANED AND FOUND ON HISTORY RECALL SHOWS FAULT CODE 27,63 AND ACP'D BITE TEST CHANNEL 7 FAILED WITH FAULT CODE 27AND RED BOX FAULT LIGHT ILLUMINANED, ALL OTHER CHANNELS PASSED. CHANNEL 7 POINTS TO RT MLG SHOCK ABSORBER. 64GB. REMOVED CONNECTOR AT 64GB AND PROX BOX DET. CHECKED WIRES A/B TO GRD AND SHIELDING NO FAULTS NOTED. CHECKED PIN C TO GROUND, FOUND OK. AT 64GB CHECKED PIN A TO PIN 16, FOUND TO BE OPEN WHEN SHAKING. PIN B TO 15 CHECKED GOOD. COMPLIED WITH A NORMAL EXTENSION AND RETRACTION TEST IAW AMM 32-31-00-05, AND CONTINUITY TEST OF PROXIMITY DETECTORS IAW AMM 32-00-00-05. ALL TESTS PASSED. AMM 32-11-43-04.

Part: BRAKE — DESTROYED (NR 1) · airframe 45,610 hrs · 27,651 cycles

WHILE REMOVING THE NR 1 TIRE, FOUND THE NR 1 BRAKE ASSY DISINTEGRATING. REMOVED AND REPLACED THE BRAKE ASSY IAW 32-42-27-04.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 45,567 hrs · 27,627 cycles

SEAT TRACK SCALLOPS BROKEN IN MAIN DECK CARGO BETWEEN FR 57 AND FR 57.1 Y953. REMOVED AND REPLACED DAMAGED SEAT TRACK SECTION AT Y953 FR 56 TO FR 57.2 IAW SRM 53-10-16 PARA 10, FIG 208. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 45,567 hrs · 27,627 cycles

COURIER FLOOR PANEL 221PF DAMAGED AT PREVIOUS REPAIR AREA. FABRICATED COURIER FLOOR PANEL 221PF ON T17/1316881 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN DECK) · airframe 45,567 hrs · 27,627 cycles

MAIN DECK FLOOR PANEL 231HG CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 45,567 hrs · 27,627 cycles

SEAT TRACK SCALOPS GOUGED / BROKEN IN MAIN DECK COMPT AT FR59 -Y1930. REMOVED DAMAGE SEAT TRACK SECTION AND FABRICATED NEW REPAIR SEAT TRACK AT IAW SRM 53-10-16. INSTALLED NEW REPAIR SECTION FROM FRAME 58-60 RT -Y1930 IAW SRM 51-40-21, MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (MAIN DECK) · airframe 45,567 hrs · 27,627 cycles

MAIN DECK FLOOR PANEL 231DH HAS PUNCTURES. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (MAIN DECK) · airframe 45,567 hrs · 27,627 cycles

MC FLOOR PANEL 242SH BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (MAIN DECK) · airframe 45,567 hrs · 27,627 cycles

MD FLOOR PANEL 241GJ BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (MAIN DECK) · airframe 45,567 hrs · 27,627 cycles

MAIN DECK FLOOR PANEL 241XJ BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (MAIN DECK) · airframe 45,567 hrs · 27,627 cycles

MD FLOOR PANEL 241KJ BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (MAIN DECK) · airframe 45,567 hrs · 27,627 cycles

MD FLOOR PANEL 231RH HAS MULTIPLE PUNCTURES. FABRICATED A FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN DECK) · airframe 45,567 hrs · 27,627 cycles

MAIN DECK FLOOR PANEL 231VG WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 45,567 hrs · 27,627 cycles

MAIN DECK FLOOR PANEL 242HK BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (MAIN DECK) · airframe 45,567 hrs · 27,627 cycles

MD FLOOR PANEL 231WG HAS MULTIPLE PUNCTURES. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN DECK) · airframe 45,567 hrs · 27,627 cycles

MD FLOOR PANEL 241DF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (MAIN DECK) · airframe 45,567 hrs · 27,627 cycles

MAIN DECK FLOOR PANEL 242CF BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (MAIN DECK) · airframe 45,567 hrs · 27,627 cycles

MD FLOOR PANEL 241FK BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (MAIN CARGO) · airframe 45,567 hrs · 27,627 cycles

MC FLOOR PANEL 242AJ BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN DECK) · airframe 45,567 hrs · 27,627 cycles

MAIN DECK FLOOR PANEL 231QG CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 45,567 hrs · 27,627 cycles

MAIN DECK FLOOR PANEL 231BH HAS EDGE DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (MAIN CARGO) · airframe 45,567 hrs · 27,627 cycles

MC FLOOR PANEL 242TH BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (MAIN DECK) · airframe 45,567 hrs · 27,627 cycles

MAIN DECK FLOOR PANEL 231FF HAS MULTIPLE PUNCTURES. FABRICATED FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — TORN (MAIN DECK) · airframe 45,567 hrs · 27,627 cycles

MD FLOOR PANEL 231JG TORN ON UPPER SURFACE. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (MAIN DECK) · airframe 45,567 hrs · 27,627 cycles

MD FLOOR PANEL 232DF PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (MAIN DECK) · airframe 45,567 hrs · 27,627 cycles

MD FLOOR PANEL 232KG PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 45,567 hrs · 27,627 cycles

MD FLOOR PANEL 231KG HAS EDGE DAMAGE & BROKEN INSERTS. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 45,567 hrs · 27,627 cycles

MD FLOOR PANEL 231CF HAS EDGE DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 45,567 hrs · 27,627 cycles

MAIN DECK FLOOR PANEL 231LG HAS EDGE DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005. MAJOR REPAIR.

Part: LINE — FAILED (SHUTOFF VALVE) · airframe 45,340 hrs · 27,500 cycles

CLIMBING THROUGH 12000FT, THE NR 1 BLEED VALVE FAULT LIGHT ILLUMINATED. TURNED OFF & ON BLEED VALVE SWITCH MULTIPLE TIMES WITH NO RESET. FAULT LIGHT REMAINED AFTER MULTIPLE ATTEMPTS. FOLLOWED QRH WITH NO SUCCESS. . VERIFIED NR 2 PACK OFF. JUMPSEATER IN COURIER HEARD A LOUD POP ON LEFT SIDE OF THE ACFT. BITE CHECKED THE NR 1 CONTROLLER, CURRENT FLIGHT FAULTED C- CONTROLLER, TROUBLESHOT FAULT IAW TSM 36-00-01, FIG 101, NO DEFECTS NOTED, RAN APU BLEED AND CHECKED FOR PRECOOLER BYPASSING, NOTHING HEARD OR FELT. PRESSURE TESTED HP PRSOV SENSE LINE FROM VALVES TO PRESSURE SENSORS, CHECKED GOOD, PRESSURE CHECKED FAV SENSE LINE AND FOUND FLEX LINE BLOWN, R & R THE SENSE LINE IAW AMM 36-11-16-04-04, LEAK AND OPS CHECKED GOOD,

Part: DAMPER — MALFUNCTIONED (MLG) · airframe 45,048 hrs · 27,225 cycles

AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. PERFORMED LANDING GEAR RETRACTION TEST IAW AMM 32-31-00-5 ON SYSTEMS 1 & 2. TEST WAS SATISFACTORY. REMOVED AND REPLACED THE LT PITCH DAMPER IAW AMM 32-11-15-04 AND PERFORMED FULL SREVICING IAW AMM 12-12-32-00. .

Part: STATIC INVERTER — FAILED (E/E BAY) · airframe 44,971 hrs · 27,155 cycles

JUST PRIOR TO TAKEOFF, ALL FUEL INDICATIONS DISPLAYED XX AND ALL FUEL INDICATIONS ON OVERHEAD PANEL WENT BLANK. ACRID ODOR AND SMOKE WAS PRESENT AND TWO LOUD BANGS WERE HEARD FROM THE E& E COMPARTEMENT. SHUTDOWN ENGINES AND ALL ELECTRICAL POWER TO THE AIRCRAFT, FIRE DEPARTMENT RESPONDED TO THE AIRCRAFT AND NOTED THE ACRID ODOR IN THE E & E COMPARTEMENT. DURING TROUBLESHOOTING, FOUND THE STATIC INVERTER BURNED WITH INTERNAL PARTS EXPLODED. PERFORMED A DETAILLED VISUAL INSPECTION OF ALL WIRES AND BUNDLE CABLES FOR BURNING, NOTHING FOUND. REMOVED AND REPLACED THE STATIC INVERTER IAW MM 24-24-11-04, OPS CHECKED OK . ALL SYSTEM ARE WORKING NORMALY, ACFT READY FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (THRUST REVERSER) · airframe 44,871 hrs · 27,055 cycles

NR 2 ENGINE THRUST REVERSER LIGHT ON DURING TAKE OFF. REJECTED THE TAKE OFF. TROUBLESHOOTING PERFORMED IAWTSM 78-31-40. PERFORMED ADJUSTEMENT ON THE NR 2 ENGINE, RT SIDE OF TRANSLATING SLEEVE MASTER AND SLAVE ACTUATORS IAW MM 78-31-15-02. PERFORMED FURTHER DEPLOYEMENT AND RETRACTATION OF THE NR 2 THRUST REVERSER IAW MM 78-32-11-05. ALL PARAMETERS ARE WITHIN LIMITS AND THE NR 2 THRUST REVERSER OPERATED NORMALLY, NO FAULT NOTED. ENGINE RUN UP PERFORMED WITH NO FAULT OBSERVED.

Part: SERVO VALVE — LEAKING (HYD SYSTEM) · airframe 44,811 hrs · 27,010 cycles

RECEIVED A GREEN HYDRAULIC SYSTEM LOW PRESSURE ECAM, FOLLOWED BY GREEN RESERVOIR LOW LEVEL ECAM. FOLLOWED QRH INCLUDING MLG GRAVITY EXTENSION AND LANDED. OVERHEAD GREEN RESERVOIR GAUGE INDICATED AT THE BOTTOM OF THE YELLOW BAND. REMOVED AND REPLACED ARTIFICIAL FEEL UNIT SERVO VALVE ON ACTUATOR IAW MM 27-33-14-04. OPS AND LEAK CHECKED GOOD.. GREEN HYDRAULIC SYSTEM SERVICED IAW MM 12-12-29-00. RESTORED UPLOCK MECHANISMS TO NORMAL CONFIGURATION, FREE FALL EXTENSION RESET IAW MM 32-33-00-02. ACFT OK FOR SERVICE.

Part: WARNING SYSTEM — INOPERATIVE (R1 DOOR SLIDE) · airframe 44,557 hrs · 26,863 cycles

ON CABIN FINAL PREP, R1 DOOR SLIDE WOULD NOT ARM. FOUND NONE OF THE DOOR WARNING OR SLIDE INDICATIONS WORKING. RESET APSCU AND COMPLIED WITH ADJUSTMENT AND TEST IAW AMM 52-73-00-05-01. PAR 1. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: SMOKE DETECTOR — FAULTY (E&E BAY) · airframe 43,316 hrs · 26,072 cycles

AT CRUISE ALTITUDE ECAM INDICATION OF AVIONICS SMOKE. OPERATING THE SNIFFER FAN IAW QRH YIELDED NO SMOKE INDICATIONS. THE ECAM ALERT EXTINGUISHED AFTER 3 MINUTES. THE SITUATION REOCCURRED UPON LANDING. REPLACED AVIONICS SMOKE DETECTORS 11WA & 13WA.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 431 hrs · 25,991 cycles

LOBE DAMAGE TO SEAT TRACK AT C33. NO RESTRICTION REF SR30-53-003 LOBE DAMAGE AT LOCK POS A840. OK IAW SR 30-53-003. INSPECTED DAMAGED AREA IAW SR 30-53-003. TRACK ONLY HAS LOBE DAMAGE. REMOVED FLOORBOARDS IAW AMM 53-10-23-04, REMOVED LOADING SYS IAW AMM 25-58-00, REMOVED CARGO LOADING SYS IAW AMM 25-58-00, REMOVED FLOORBOARDS IAW AMM 53-10-23-04, IDENTIFIED PARTS REMOVED ADDITIONAL CARGO LOADING SYS IAW AMM 25-58-00 & REMOVED ONE ADDITIONAL FLOORBOARD IAW AMM 53-10-23-04. REMOVED FASTENERS IN PAN AT FWD SEAT TRACT SPLICE FOR ACCESS IAW SRM 51-40-21. CUT OUT DAMAGED SEAT TRACK, CUT NEW SPLICE TRACK & MADE CUT OUTS IAW SRM 53-10-16. LOCATED & DRILLED PARTS IAW SRM 53-10-16. FWD SEAT TRACK SPLICE OKAY TO INSTALL IAW SRM 53-10-16. INSTALLATION COMPLETE AFT OF FWD SEAT TRACK SPLICE IAW SRM 53-10-16.

Part: STIFFENER — CRACKED (NR 1 PYLON) · airframe 430 hrs · 25,918 cycles

NR 1 PYLON SPAR STIFFENER, FOUND CRACKED BETWEEN RIB 9 & 10 DURING NDT. REPAIRED IAW EA 6-5450-T0320597 P1. MAJOR REPAIR IAW GMM 6-2-100.

Part: COVER PLATE — CRACKED (CARGO DOOR) · airframe 430 hrs · 25,918 cycles

FORWARD CARGO DOOR INNER COVER PLATE, JUST AROUND THE ACTUATOR ATTACH FITTING, FOUND CRACKED. REPAIRED IAW EA 6-5230-T0320449 P1. MAJOR REPAIR IAW GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FRAME 66) · airframe 430 hrs · 25,918 cycles

BULK CARGO FRAME 66, -Y140, FLOOR SUPPORT WITH EXFOLIATING CORROSION. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.

Part: FLOORBEAM — CRACKED (FRAME 15) · airframe 430 hrs · 25,918 cycles

MAIN DECK CARGO BAY FRAME 15A, Y1456, FLOORBEAM CRACKED APPROX 3.0 INCH LENGTH. REPAIRED IAW SRM 53-12-15 FIG 207. MAJOR REPAIR IAW GMM 6-2-100.

Part: WEB — CRACKED (ZONE 200) · airframe 430 hrs · 25,918 cycles

MAIN DECK CARGO BAY FRAME 47, Y450 - Y0, WEB CRACKED APPROX 1.0 INCH IN LENGTH. REPAIRED IAW SRM 53-15-15 FIGURE 201. MAJOR REPAIR IAW GMM 6-2-100.

Part: WEB — CRACKED (FRAME 47) · airframe 430 hrs · 25,918 cycles

MAIN DECK CARGO COMPARTMENT FRAME 47, -Y450 - Y0, WEB CRACKED APPROX 1.0 INCH IN LENGTH. REPAIRED IAW DWG A53832100. REPLACED THE CRACKED WEB OF MDCC FRAME 47, -Y450 - Y0 IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.

Part: WEB — CRACKED (FRAME 47) · airframe 430 hrs · 25,918 cycles

MAIN DECK CARGO BAY FRAME 47, Y953 - Y1456, WEB CRACKED APPROX 1.0 INCH IN LENGTH. REPLACED THE WEB IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 430 hrs · 25,918 cycles

AFT CARGO DOOR ACTUATOR ATTACH FITTING FOUND CRACK. REPLACED THE ACTUATOR FITTING OF AFT CARGO DOOR IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.

Part: FITTING — CRACKED (FRAME 47) · airframe 430 hrs · 25,918 cycles

CENTER WING BOX, FRAME 47 RT SIDE, CORNER ANGLE FITTING K HOLE FOUND CRACKED. COMPLIED WITH EA 6-5710-150908 A P 3. MAJOR REPAIR IAW GMM 6-2-100.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 430 hrs · 25,918 cycles

FORWARD CARGO DOOR ACTUATOR ATTACH FITTING CRACKED. REPLACED THE CRACKED FITTING OF FWD CARGO DOOR IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.

Part: COVER PLATE — CRACKED (CARGO DOOR) · airframe 430 hrs · 25,918 cycles

AFT CARGO DOOR INNER COVER PLATE, JUST AROUND THE ACTUATOR ATTACH FITTING FOUND CRACKED. REPAIRED IAW EA 6-5230-T0320275 P1. MAJOR REPAIR IAW GMM 6-2-100.

Part: SEALANT — MISSING (CARGO BAY) · airframe 41,843 hrs · 25,415 cycles

AFTER THE INITIAL REPAIR OF THE PREVIOUS FUEL QTY INDICATION PROBLEM, THE PROBLEM REOCCURRED & THEN SMELL OF SMOKE BECAME EVIDENT. FUEL QTY INDICATING IS NORMAL. GVI CHECKED FOUND 90VU, 80VU,107VU & T CAS COMPUTER UMBRELLA PANEL AREA WATER DROP FROM CEILING FLOOR. REMOVED ALL BALL MAT & PROTECTIVE WALK WAY COVERS ON MAIN DECK, DISCOVERED WET WATER ALL BALL MAT FLOOR AREA & BLOCKED 6 D RAIN SIEVE ON ZONE 230. DISCOVERED BAFFLE PLATE ASSEMBLY & FLOOR NOT SEALED BETWEEN FRAME 18 - 20, REFER TO IPC 25-58-02-60X. INSPECTED AVIONICS COMPARTMENT 90VU, 80VU, 101VU, 107VU, 106VU, 282VU, 105VU, 104VU, 103VU, 281 ACFT BATTERIES & TCAS COMPUTER UMBRELLA PANEL, NO DEFECT FOUND. CLEANED & DRIED MAIN DECK CARGO FLOOR & AVIONIC COMPARTMENT. NO MORE WATER DROP & MOISTURE. SEALED COMPOUND ON BAFFLE PLATE ASSEMBLY & MAIN DECK CARGO FLOOR WITH PR-1436 GB1/2 IAW SMP. DRAINAGE SYS INSPECTION CHECKED, NO DEFECT FOUND IAW AMM 53-12-29 -06. COMPLIED WITH ACFT EXTERNAL POWER CONTROL ADJUSTMENT, TESTED NORMAL IAW AMM 24-41-00-05. COMPLIED WITH BATTERIES DC GENERATION ADJUSTMENT, TESTED NORMAL IAW MM 24 -31-00-05. COMPLIED WITH EMER AC GENERATION ADJUSTMENT, TESTED NORMAL IAW AMM 24-24-00-05-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,302 hrs · 25,198 cycles

COURIER COMPARTMENT INTERIOR EMER LIGHTS TEST INOPERATIVE. MANUAL TEST OK. R & R THE EMER POWER SUPPLY BATTERY, TEST NORMAL IAW AMM33-51-14-04-09. PART INFO SEE WR I 05-25 1105.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 40,872 hrs · 25,023 cycles

RIGHT RIB NR 5 HAS CORROSION IN BORE & FACE. REPAIRED IAW EA 6-5710-T0307642 P2.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 40,872 hrs · 25,023 cycles

LEFT RIB NR 5 HAS CORROSION IN BORE & FACE. REPAIRED IAW EA 6-5710-T0307642 P1.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 40,792 hrs · 24,981 cycles

MAIN CABIN FLOOR PANEL 241KK HAS BROKEN EDGE. FABRICATED FLOOR PANEL IAW DWG SRZ-25-005.

Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 40,792 hrs · 24,981 cycles

MAIN DECK CARGO FLOOR PANEL 242LK CRACKED. FABRICATED FLOOR PANEL IAW DWG SRZ-25-005.

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 40,792 hrs · 24,981 cycles

MAIN CARGO COMPARTMENT FLOOR PANEL 252GF HAS PUNCTURE. FABRICATED FLOOR PANEL 252G IAW DWG SRZ-25-005 ON STAM TRAVELER T14 1049828.

Part: CHECK VALVE — LEAKING (HYD SYSTEM) · airframe 40,082 hrs · 24,286 cycles

MAIN CARGO DECK SMOKE DETECTOR ACTIVATED WHEN APU BLEED SELECTED ON. SMOKE FILLED MAIN DECK. CLOSED APU BLEED AND SHUTDOWN APU, BATTERIES. FOUND BOTH RELIEF VALVES STUCK OPEN ON BOTH SIDES. REPLACED APU PRESSURE LINE CHECK VALVE IAW MM 29-14-17-04, REPLACED YELLOW RESERVOIR AIR PRESSURE RELIEF VALVE IAW MM 29-14-00-00 & MM 29-11-11-04. DECONTAMINATION CHECK IAW MM21-51-00-03.

Part: WARNING LIGHT — FALSE ACTIVATION (HYD SYSTEM) · airframe 39,599 hrs · 23,839 cycles

AT CRUISE, ECAM ALERT GREEN SYS HYD LO LEVEL, ECAM SHOWED GREEN SYS NEAR ZERO. C/W 11-3-05 "HYD RSVR LO LEVEL" PROCEDURE. MANUAL GEAR EXTENSION. EMERGENCY DECLARED. NO NOSEWHEEL STEERING. AFTER LANDING, GREEN HYD SYS QUANTITY SHOWED IN NORMAL RANGE. WHEN ON RUNWAY VISUALLY CHECKED GREEN HYD RSVR AND SHOWED 5.0 USG. HYD LEAK INSPECTION COMPLIED WITH NO FINDINGS. NO EVIDENCE OF HYD LEAK. GREEN HYD RSVR SERVICED WITH 1 US GALLON IAW AMM 12-12-29-00-0. LANDING GEAR SYS RESTORED TO NORMAL OPERATION AFTER LANDING FREE FALL EXTENSION IAW AMM 32-33-00-02-0. INSPECTED PX TRANSMITTER 17WV, QTY TRANSMITTER AND ALL FILTERS DPI WITH NO FINDINGS. PERFORMED BOTH ENG RUN-UP IAW JRH, ALL FLIGHT CONTROLS CYCLED SEVERAL TIMES AND NO CHANGE IN QTY OR PRESSURE. PRECAUTIONARY R & R SDAC IAW AMM 31-55-22-04-0, TESTED SERVICEABLE. ACFT OK FOR SERVICE.

Part: CABLE — DISCONNECTED (LT WING) · airframe 39,569 hrs · 23,811 cycles

LEFT WING ASA OTBD PCA JAM DETECTION CABLE FOUND CAPPED AND STOWED. CABLE RECONNECTED AND HYD ACTUATION (AILERON) TEST CARRIED OUT IAW AMM 27-14-00-05. ALL OPS SERVICEABLE IAW SERVO CONTROL JAMMING DETECTION TEST.

Part: SMOKE DETECTOR — INOPERATIVE · airframe 39,115 hrs · 23,395 cycles

AFTER GEAR UP, IN-FLIGHT AVIONICS SMOKE ON ECAM ON GND CONTINUOUS ECAM WARNING. INSPECTED AVIONICS BAY FOR SMOKE/EVIDENCE OF OVERHEATING, NONE FOUND. TESTED AVIONICS COMPARTMENT DETECTORS IAW TSM 26-15-00-05, FOUND MAIN BAY AND MINIMUM EQUIPMENT BAY DETECTORS TESTED OK. COCKPIT DETECTOR NO TEST. REMOVED AND RECONNECTED PLUG AND SUBSQUENT TESTS OK. SMOKE DETECTOR 13WA FAILING TEST. R & R SMOKE DETECTOR 13WA IAW AMM 26-15-12-04 AND OP TEST PERFORMED IAW AMM 26-15-00-05. TEST PASSED.

Part: SMOKE DETECTOR — FALSE ACTIVATION (E/E BAY) · airframe 39,115 hrs · 23,395 cycles

AFTER GEAR UP, IN FLIGHT "AVIONICS SMOKE" ON ECAM. ON GROUND CONTINUOUS ECAM WARNING. INSPECTED AVIONICS BAY FOR SMOKE & EVIDENCE OF OVERHEATING NONE FOUND.

Part: PANEL — CHAFED (ZONE 500) · airframe 39,110 hrs · 23,391 cycles

NR 1, PYLON HYD LINE UNIONS AT AFT FAIRING DISCONNECT POINT FRETTING IN WING REAR SPAR FITTING. REWORK ACCOMPLISHED ON EA 6-5720-150921.

Part: PANEL — CHAFED (ZONE 600) · airframe 39,110 hrs · 23,391 cycles

RT PYLON HYD LINE UNIONS AT AFT FAIRING DISCONNECT POINT FRETTING IN WING REAR SPAR FITTING REWORKED, ACCOMPLISHED ON EA 6-5720-150920.

Part: PANEL — CHAFED (ZONE 500) · airframe 39,110 hrs · 23,391 cycles

LT PYLON HYD LINE UNIONS AT AFT FAIRING DISCONNECT POINT FRETTING IN WING REAR SPAR FITTING. REWORKED ACCOMPLISHED ON EA 6-5720-150921.

Part: ANGLE — BENT (ZONE 100) · airframe 39,110 hrs · 23,391 cycles

AFT CARGO DOOR CUTOUT FWD UPPER ANGLE FOUND DISTORTED. AFT CARGO DOOR CUTOUT UPPER ANGLE REPLACED.

Part: FITTING — CHAFED (ZONE 300) · airframe 39,110 hrs · 23,391 cycles

SUSPECT WEAR CHAFE DAMAGE TO LUG FITTING, LWR RUDDER PCA FITTING AT RUDDER ATTACHMENT. REWORK C/OUT ON EA 6-5500-150939 AND RAS 7055.

Part: ROLLER TRACK — CORRODED (ZONE 100) · airframe 39,110 hrs · 23,391 cycles

ROLLER TRACK AT FR32-FR38.2 Y1420 CORRODED ON INBD SIDE, BEYOND SRM 53-10-15 LIMITS ROLLER TRACK REPLACED IAW AMM 25-52-21-04-0.

Part: FITTING — CHAFED (ZONE 300) · airframe 39,110 hrs · 23,391 cycles

SUSPECT WEAR CHAFE DAMAGE TO LUG FITTING MID RUDDER PCA FITTING AT RUDDER ATTACHMENT. ATTACHMENT CUT OUT ON EA 6-5500-150939 AND RAS 70550958/003/2011.

Part: PANEL — MISREPAIRED (ZONE 100) · airframe 39,110 hrs · 23,391 cycles

REPAIR FOUND AT FR 52-53 RT FUSE SKIN MLG BAY CUTOUT AREA AFT CORNER, SKIN EVALUATED ON NRC N00570 AND FOUND TO NOT CONFORM TO ANY APPROVED DOCUMENTATION. DOUBLER REPAIR INSTALLED ON EA 6-5315-150928

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,110 hrs · 23,391 cycles

SEAT TRACK FOUND CORRODED.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,110 hrs · 23,391 cycles

SEAT TRACK FOUND CORRODED.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,110 hrs · 23,391 cycles

SEAT TRACK FOUND CORRODED.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,110 hrs · 23,391 cycles

FLOOR SUPPORT FOUND CORRODED

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,110 hrs · 23,391 cycles

FLOOR SUPPORT FOUND CORRODED.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,110 hrs · 23,391 cycles

AFT CARGO HOLD FR54 TO 54.1, S57R FUSELAGE SKIN CORRODED. REPAIR ACCOMPLISHED ON EA 6-5316-150940.

Part: ANGLE — CORRODED (DOOR SILL) · corrosion level 2 · airframe 39,110 hrs · 23,391 cycles

BULK CARGO DOOR SILL INNER ANGLE FR67-69 FOUND CORRODED AT FR67 BULK CARGO DOOR SILL INNER ANGLE FR67-69 REPLACED.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,110 hrs · 23,391 cycles

FLOORBEAM FR67 Y-430 CORRODED FLOORBEAM, FR67 Y-430, REPLACED.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,110 hrs · 23,391 cycles

SEAT TRACK FOUND CORRODED AT Y-450, FR 14 TO 15A. SEAT TRACK REPLACED.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,110 hrs · 23,391 cycles

SEAT TRACK FOUND CORRODED AT -Y953, FR15A TO 18/19. SEAT TRACK REPLACED.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,110 hrs · 23,391 cycles

SEAT TRACK FOUND CORRODED AT Y450, FR14 TO 15A. SEAT TRACK REPLACED.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,110 hrs · 23,391 cycles

Y730, FR11-14, FLOOR SUPPORT FOUND CORRODED Y730, FR11-14 FLOOR SUPPORT REPLACED IAW SRM 51-40-21

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,110 hrs · 23,391 cycles

FLOOR SUPPORT Y953 FOUND CORRODED AT FR 11-13 AREA FLOOR SUPPORT Y953 REPLACED FROM FR11 TO FR15A IAW SRM 51-40-21

Part: SKIN — DAMAGED (ZONE 100) · corrosion level 2 · airframe 39,110 hrs · 23,391 cycles

AFTER TAKING REPAIR OFF AT FR 13 DAMAGE FOUND AT BUTTJOINT. REPAIR ACCOMPLISHED ON EA 6-5315-150936.

Part: FRAME — DAMAGED (ZONE 100) · corrosion level 2 · airframe 39,110 hrs · 23,391 cycles

DURING REMOVAL OF REPAIR ON FR 13 RAS/AS/305/95 ISSUE A, FRAME 13 FOUND DAMAGED. REPLACED ON EA 6-5315-150936.

Part: SKIN — DETERIORATED (ZONE 100) · airframe 39,110 hrs · 23,391 cycles

AFT CARGO DOOR SKIN CUTOUT FWD SKIN AREA HAS SURFACE FINISH DETERIORATION, STR 39. REPAIR ACCOMPLISHED ON EA 6-5317-150914.

Part: ROLLER TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,110 hrs · 23,391 cycles

ROLLER TRACK FR 30-38.2 -Y1470 HAS CORROSION ON THE INNER FLANGE TRACK ASSY. REPLACED SRM 53-14-15 AND AMM 25-52-51-04-01.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 39,110 hrs · 23,391 cycles

SKIN REPAIR FOUND AT FR 28-29, STR 38-39 FOUND NOT TO CONFORM TO APPROVED DOCUMENTATION. REPAIR REWORKED ON EA 6-5315-150935. REPAIR EVALUATED USING EA AND SRM 53-10-12 FIG 229. NOW COMFORMS TO SRM

Part: ROLLER TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,110 hrs · 23,391 cycles

ROLLER TRACK -Y140 FR32-38.2 CORRODED ROLLER TRACK REPAIR C/OUT IAW SRM 53-10-15, FIG 203.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 39,110 hrs · 23,391 cycles

LT GANTRY 4 FOUND CRACKED AT FR 52.A. REPAIRED IAW DRAWING R53810581 AND SRM 51-40-00, AS INSTRUCTED BY EO E6-5310-7-2021PT6

Part: SKIN — DAMAGED (ZONE 200) · airframe 39,110 hrs · 23,391 cycles

FWD RT DOOR CUT OUT, NDT INSPECTION HIGHLIGHTED SEVERAL AREAS OF SURFACE ANOMALIES IN THE FWD LWR CORNER AREA . REWORK ACCOMPLISHED ON EA 6-5315-150930.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 39,110 hrs · 23,391 cycles

F/O WINDSHIELD LWR FRAME OTBD AND INBD CORNERS HAVE TOOLING MARKS DAMAGE F/O WINDSHIELD LWR FRAME OTBD AND INBD CORNERS REWORK ACCOMPLISHED ON EA 6-5118-150932.

Part: SKIN — DAMAGED (ZONE 500) · airframe 39,110 hrs · 23,391 cycles

LEFT LOWER T/E PANEL RIVET HEAD PULLED.

Part: SKIN — CORRODED (CENTER WING) · airframe 39,110 hrs · 23,391 cycles

CORROSION TO RIGHT WING CENTER WING BOX LOWER SKIN BETWEEN SPLICE PLATE AND PICKUP ANGLE, FRAME 41 AND 42 ADJACENT TO RIB 1. REPAIR ACCOMPLISHED ON EA 6-5710-150913.

Part: SUPPORT — CORRODED (ZONE 600) · airframe 39,110 hrs · 23,391 cycles

CORROSION TO RIGHT WING SUPPORT DOUBLER LOWER SURFACE OTBD OF RIB 8 AT FRONT SPAR ATTACHMENT.

Part: CROSSBEAM — MISREPAIRED (ZONE 100) · airframe 39,110 hrs · 23,391 cycles

FR61 CROSSBEAM Y450 AFT CARGO BAY SPLICE REPAIR FOUND TO NOT COMPLY WITH SRM 53-10-15. REPLACED IAW SRM 53-10-15 FIG 207.

Part: CROSSBEAM — MISREPAIRED (ZONE 100) · airframe 39,110 hrs · 23,391 cycles

SPLICE REPAIRS FOUND ON FR62 AFT CARGO BAY CROSSBEAM TO BE REPLACED DUE TO NOT CONFORMING TO APPROVED DOCUMENTATION. CROSSBEAM REPLACED IAW SRM 53-10-15 FIG 207.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 39,110 hrs · 23,391 cycles

EXTERNAL DOUBLER FOUND AT FR 36-37 STR 38-39 RT FUSE SKIN FOUND NOT TO BE IAW SRM 53-10-12. REPLACED IAW SRM 53-10-12 FIG 225.

Part: CROSSBEAM — MISREPAIRED (ZONE 100) · airframe 39,110 hrs · 23,391 cycles

FR60-61 Y-500 CROSSBEAM SPLICE REPAIR DOES NOT COMPLY WITH SRM 53-10-15. REPLACE IAW SRM 53-10-15 FIG 207

Part: CROSSBEAM — MISREPAIRED (ZONE 100) · airframe 39,110 hrs · 23,391 cycles

FR38.2 Y-360 FWD CARGO BAY CROSSBEAM FLANGE SPLICE REPAIR FOUND TO NOT COMPLY WITH SRM. REPLACED IAW SRM 53-10-15 FIG 207.

Part: CROSSBEAM — MISREPAIRED (ZONE 100) · airframe 39,110 hrs · 23,391 cycles

FR38.2, Y450 FWD CARGO BAY CROSSBEAM SPLICE REPAIR FOUND TO NOT COMPLY TO SRM. REPLACED IAW SRM 53-10-15 FIG 207.

Part: ROLLER TRACK — MISREPAIRED (ZONE 100) · airframe 39,110 hrs · 23,391 cycles

SPLICE REPAIR AT ROLLER TRACK FR 32 Y1470 DOES NOT COMPLY WITH SRM TRACK ASSY REPLACED.

Part: ROLLER TRACK — MISREPAIRED (ZONE 100) · airframe 39,110 hrs · 23,391 cycles

PREVIOUS REPAIR AT FR58-59 Y-140 AFT CARGO BAY ROLLER TRACK FOUND TO NOT BE IAW APPROVED DOCUMENTATION INCORRECT LWR SPLICE PLATE REPLACED AND CORRECT MOUNT OF FASTNERS INSTALLED. REPAIR NOW IS IAW SRM 53-10-15, PB201, FIG 203.

Part: CROSSBEAM — MISREPAIRED (ZONE 100) · airframe 39,110 hrs · 23,391 cycles

FR60-61 Y450 CROSSBEAM SPLICE REPAIR DOES NOT COMPLY WITH SRM 53-10-15. REPLACED IAW SRM 53-10-15 FIG 207

Part: RIB — CRACKED (ZONE 500) · airframe 39,110 hrs · 23,391 cycles

LEFT WING T/E STRUCTURE RIB CRACKED ADJACENT NR 3 SPOILER INBD HINGE ARM. RIB REPLACED IAW SRM 57-51-11 FIG 5 SHEET 1 AND DRAWING A57240389

Part: CROSSBEAM — MISREPAIRED (ZONE 100) · airframe 39,110 hrs · 23,391 cycles

FR38.2 FWD CARGO BAY Y-970 CROSSBEAM SPLICE REPAIR FOUND TO NOT CONFORM TO SRM. REPLACED IAW SRM 53-10-15 FIG 207.

Part: ROLLER TRACK — MISREPAIRED (ZONE 100) · airframe 39,110 hrs · 23,391 cycles

SPLICE REPAIR AT ROLLER TRACK FR 32 Y1470 DOES NOT COMPLY WITH SRM. REMOVED AND REPLACED.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,110 hrs · 23,391 cycles

CORROSION ON INSIDE OF LWR FLANGE OF STR 44 RT AT THE INTERSECTION OF FRAME 13. STRINGER SPLICE REPAIR ACCOMPLISHED ON EA 6-5300-150911.

Part: FLOOR SUPPORT — MISREPAIRED (ZONE 200) · airframe 39,110 hrs · 23,391 cycles

REPAIR AT FR14-15A Y-1959 MAIN DECK FLOOR STRUCTURE SUPPORT FLANGE FOUND TO NOT BE IAW APPROVED DOCUMENTATION.

Part: ROLLER TRACK — MISREPAIRED (ZONE 100) · airframe 39,110 hrs · 23,391 cycles

SPLICE REPAIR AT ROLLER TRACK FR38 Y-1470 DOES NOT COMPLY WITH SRM. ROLLER TRACK ASSY REPLACED.

Part: SKIN — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 39,110 hrs · 23,391 cycles

FWD LAV SERVICE DOOR OUTER SKIN HAS 2 AREAS OF CORROSION. AREAS BLENDED AND FOUND TO BE OUT OF SRM 52-42-11 LIMITS. REPAIRED IAW SRM 52-42-11 PB201 CLASSED AS SECONDARY STRUCTURE

Part: DIAPHRAGM — CRACKED (ZONE 100) · airframe 39,110 hrs · 23,391 cycles

RIGHT DIAPHRAGM BETWEEN FR 46-47 ATTACHMENT ANGLE CRACKED STR 43. REPLACED DIAPHRAM IAW DWG A53812215

Part: DIAPHRAGM — CRACKED (ZONE 100) · airframe 39,110 hrs · 23,391 cycles

LT DIAPHRAGM BETWEEN FR 46-47 ATTACHMENT ANGLE CRACKED, STR 43. REPLACED DIAPHRAM IAW DWG A53812215

Part: KEELBEAM — CHAFED (ZONE 100) · airframe 39,083 hrs · 23,369 cycles

KEELBEAM STRUCTURE AT FRM INTERNAL DAMAGE REPAIR CARRIED OUT USING SPLICE ANGLE IAW EA 6-5310-149778.

Part: RIB — CRACKED (ZONE 600) · airframe 39,000 hrs · 23,299 cycles

DURING ACCOMPLISHMENT OF EO-5710-7-3325/1 PART 8 CRACKS WERE FOUND DURING FLOURESCANT NDT INSP ON HOLE 54 RT WING REPAIR OF CRACKS CARRIED OUT IAW REPAIR 22R572-40226 AND EA 6-5710-149764 AREA SPOT FACES REWORKED AND FASTENERS REPLACED WITH 2ND OVERSIZE AREA REINSPECTED NO CRACK INDICATIONS.

Part: RIB — CRACKED (LT WING) · airframe 39,000 hrs · 23,299 cycles

DURING ACCOMPLISHMENT OF EO -5710-7-3325J1 PART 7 CRACKS WERE FOUND DURING FLOURESCENT INSP NDT CHECKS ON HOLES 54 AND 47 LT WING REPAIR OF CRACKS CARRIED OUT IAW REPAIR 22R572-40226 AND EA 6-5710 -149764 AREA SPOT FACES REWORKED ,2ND OVERSIZE FASTENERS FITTED, AREAS REINSPECTED NO CRACK INDICATIONS.

Part: STRUCTURE — DAMAGED (KRUGER FLAP) · airframe 37,550 hrs · 21,989 cycles

RH KRUEGER FLAP DAMAGED AT L/E AND TOP SKIN PANEL AFTER IMPACT WITH GROUND EQUIPMENT. KRUEGER FLAP TOP SKIN PANEL REPAIRED WITH AN EXTERNAL DOUBLER AS PER AIRBUS PROPOSAL. KRUEGER L/E SKIN REPLACED.

Part: RELAY — CONTAMINATED · airframe 37,250 hrs · 21,725 cycles

PASSING APPROX 10000 FT GOT ECAM WARNING "AVIONICS SMOKE WARNING" FOLLOWED ECAM QRH. DECLARED EMERGENCY WITH COPENHAGEN APPROACH. NO SMOKE WAS EVER NOTED. FOUND WATER DRIPPING FROM FLOOR ABOVE RELAY RACK POS .103 VU. RELAY RACK DRIED OUT WITH COMPRESSED AIR AND VENTILATED WITH APU AIR. ALL MOISTURE REMOVED FROM FLOOR ABOVE. MINIMUM EQUIP BAY SMOKE DETECTOR TEST PERF ACC AMM 26-15-00-5. TEST SATIS COMPARTMENT BAY TEST PERF A CC AMM 26-16-00-5-02. TEST SATIS. FOUND WATER DRIPPING FROM FLOOR ABOVE RELAY RACK POS .103VU. RELAY RACK DRIED OUT WITH COMPRESSED AIR AND VENTILATED WITH APU AIR. ALL MOISTURE REMOVED FROM FLOOR ABOVE. MINIMUM EQUIP BAY SMOKE DETECTOR TEST PERF ACC AMM 26-15-00-5. COMPARTMENT BAY TEST PERF ACC AMM 26-16-0 0-5-02. TEST SATIS. RETURNED TO SERVICE. MOCC NOTIFIED.

Part: FRAME — DAMAGED (ZONE 100) · airframe 37,081 hrs · 21,569 cycles

INSPECTION OF HOLES AT FRAME 47 RT SPLICE FITTING BETWEEN STR 24 AND 26 INDICATED DAMAGE ON HOLE "M". COMPLIED WITH EA 6-5310-125501 PART 1.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,081 hrs · 21,569 cycles

FWD FUSELAGE - DENT FOUND ON LOWER FWD FUSELAGE BETWEEN FR 12-12A STR 46-47. THE DENTED SKIN WAS REPAIRED IAW EA 6-5330-125500.

Part: FITTING — CORRODED (PYLONS) · corrosion level 2 · airframe 37,081 hrs · 21,569 cycles

PYLONS, PYLON STRUCTURE, NR 1 AND NR 2 PYLON AFT FITTING BORES AND BOLTS HOLES CORROSION REPAIR.

Part: RUDDER — DEBONDED · airframe 37,081 hrs · 21,569 cycles

RUDDER T/E W/DEBONS BETWEEN RIB 10 AND RIB 12 REPAIR WAS DONE IAW EA 6-5510-125493.

Part: SKIN — DENTED (LE SLAT) · airframe 37,081 hrs · 21,569 cycles

RT WING - (2) DENTS ON NOSE SKIN OF SLAT NR1 BETWEEN RIB 20 AND JACK RIB 2. THE SLAT NR1 WAS REPAIRED IAW EA 6-5750-127034.

Part: PROXIMITY SENSOR — MALFUNCTIONED (MLG) · airframe 35,920 hrs · 20,528 cycles

ON TAKEOFF TRIED TO RAISE GEAR WITH NR 1 SYS WOULD NOT COME UP SWITCHED TO SYS 2 GEAR CAME UP. WHILE GEAR WAS RETRACTING NR 1 PITCH TRIM BOTH ATS LEVERS NR 1 CABIN PRESS REGULATOR KICKED OFF OVERWEIGHT LANDING AT 312K AND DECLARED EMERGENCY. FOUND LT UPPER NOSE GEAR HARNESS DAMAGED. REPLACED THE HARNESS P/N D22296010 AS A PRECAUTION REF A300 SUPP M/M 32-21-43-4. COMPLIED WITH PHASE 1 INSPECTION OF THE OVERWEIGHT INSPECTION NO DEFECTS NOTED AT THIS TIME A-300-600 MM 05-51-11-0. REMOVED AND REPLACED SENSORS 80 AND 81GB. REMOVED AND REPLACED 65GB, NO HELP REFA300-600ASM 32-31-00. REMOVED AND REPLACED 9GA, 8GA AND 64 GB SYSTEM 1 PROX DETECTORS REFA300-600 MM 32-00-00-4. SWUNG GEAR, CKD OK.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 33,616 hrs · 19,245 cycles

RT WINDSHIELD FRAME LOWER SECTION BETWEEN FRAMES 4 AND 2 HOLE WITH FASTENER REMOVED HAS CRACK INDICATION REF N00029. COMPLIED WITH EA 6-5310-93391.