N671FE

Part: SWITCH — INOPERATIVE (ZONE 200) · airframe 35,659 hrs · 19,910 cycles

FOUND DOOR INTERIOR EMERGENCY EXIT LIGHTS ALWAYS ILLUMINATED. NOTICED RED EMERGENCY LIGHT SWITCH FWD OF L1 DOOR IS STUCK INSIDE. RELEASED FOR SERVICE PER MEL : 33-XX-XX-XX CAT: C EXP: 15DEC23 "MEL 33-XX-XX-XX: COURIER COMPARTMENT INTERIOR EMERGENCY LIGHTS L1 AND R1 EXIT LIGHTS - INOP. NO JUMPSEATERS ALLOWED TO OCCUPY THE COURIER AREA." REPLACED EMERGENCY SWITCH (CPN 3310656) @ L-1 PANEL, REF ESPM 20-45-10 OK FOR SERVICE.

Part: PSU — FAILED (UNKNOWN) · airframe 35,328 hrs · 19,654 cycles

ON PRE-DEPARTURE CHECK FOUND THAT COUIER COMPARTMENT INTERIOR EMERGENCY EXIT LIGHTS ARE INOP, WILL NOT TEST. RELEASED FOR SERVICE PER MEL : 33-XX. INSTALLED NEW BATTERY, NO HELP. REINSTALLED ORIGIONAL BATTERY. A300 AMM 33-XX. RELAMPED PER IPC. NO HELP. POSSIBLE BROKEN WIRE, TSM FAULT TREE 33-51 COMPLIED WITH.NO HELP. A/C OK TO CONTINUE ON MEL. IN HARNESS 300VB FOUND WIRE (33_51_1056 SEE A300 AWM 33_51_05) DIRECTLY BEHIND MCD CONTROL BOARD CHAFFED, REPAIRED WIRE VIA SPLICE A300 ESPM 20-43-11, OPS CHECK GOOD PER A300 33_51_00_00_0 ESPM 20-43-11.

Part: TRANSFORMER — FAILED (N/A) · airframe 35,008 hrs · 19,467 cycles

WHILE ATTEMPTING TO START APU, GOT AN APU FAULT, THEN ELECTRICAL FUMES AND SMOKE IN COCKPIT PULLED APU/ START C/B. OPEN FRONT PANEL OFF OF 120 VU, INSPECTED WIRING, AND APU START CONTACTOR 5KA, APPEARS TO BE IN GOOD SHAPE, NO DAMAGE, 50 AMP BREAKER 10XH POPPED AND WILL NOT RESET. ATTEMPTED TO START APU TWICE AND RECEIVED APU FAULT. RPM NEVER ABOVE 17% AND EGT STAYS AROUND 5. ECB FAULTS NO FLAME AND INLET DOOR. MEMORY ERASED ON ECB AND RESTART OF APU ATTEMPTED WITH SAME RESULT. DURING BOTH START ATTEMPTS, SMELLED STRONG ELECTRICAL BURNING FUMES COMING FROM E&E AREA. UNABLE TO PINPOINT ISSUE CAUSING BURNING SMELL. AMM: 24-37-00-0AMM: 24-35-11-04 AMM: 24-00-00-06 REF TSI 24-32/3860, 1) VERIFIED OVERHEAD GAUGES, ECAM DC VOLTS AND DC AMPS OK FOR THE ESS T/R. 2) INSPECTED 2PC AND 3PC WITH NO VISUAL DEFECTS NOTED. 3) OPENED 106VU PANEL, INSPECTED, NO DEFECTS NOTED. 4) OPENED 101VU PANEAL AND INSPECTED COMPONENTS WITH NO DEFECTS NOTED.5) REF WRI #49-40/3862, R/R'D APU STARTER AMM: 49-00-00-5 REF MTSI 24-32/3860 FOR FUNCTION CHECK. AMM: 24-32-11-04 R/R'D ESSENTIAL T/R AND CONFIRMED BURNED SMELL. OPS CHECKS GOOD. REFERENCE ABOVE. ESS BUS NOW POWERED BUT #3 BATTERY READS 24 VOLTS AND WILL NOT CHARGE. (W/KIT) TRANSFORMER RECTIFIER MPN: F11QY3714 SRL OFF: 1.546R.. MPN: F11QY3714 ON SRL: 2736

Part: NONE — DAMAGED (ZONE 300) · airframe 34,259 hrs · 18,963 cycles

STABILIZER - RUDDER RH PANEL FOUND WATER INGRESS AROUND FASTENER #36, #37, #38 AND #39 COMPLIED WITH FEDEX EA: 6-5540-T0332902 A PT3, EA TITLE: STABILIZERS - RUDDER - RH - WATER INGRESS - AIRBUS SERVICE BULLETIN A300-55-6050 INSPECTIONS/EO 6-5540- E0319362A PART 1. REPAIRED STABILIZER - RUDDER RH PANEL AROUND FASTENER #36, #37, #38 AND #39. THIS IS CATEGORY B REPAIR.THE FOLLOWING INSPECTION PER FEDEX EA: 6-5540-T0332902 A. MAJOR REPAIR IAW FEDEX GMM6-2-100.

Part: NONE — CRACKED (ZONE 200) · airframe 34,259 hrs · 18,963 cycles

RH FWD PAX DOOR - FRAME SEGMENT AT FR14C FOUND 1EA CRACK COMPLIED WITH FEDEX EA: 6-5210-T0368735 PT1, EA TITLE: DOORS - PASSENGER/CREW - LOCAL FABRICATION AND REPLACEMENT OF FRAME SEGMENT ON R1 DOOR - RSC TRACKING. REPAIRED RH FWD PAX DOOR - FRAME SEGMENT AT FR14C . THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 34,259 hrs · 18,963 cycles

MAIN DECK CARGO COMPARTMENT FLOOR SUPPORT STRUCTURE - SEAT TRACK CRACKED, BETWEEN FR20 AND FR21, Y1959 COMPLIED WITH FEDEX EA: 6-5310-T0368594 PT1, EA TITLE: FUSELAGE - MAINFRAME - MCD Y1959 SEAT TRACK BENT AND CRACKED BETWEEN FR20 AND FR21 - REPAIR. REPAIRED MAIN DECK CARGO COMPARTMENT FLOOR SUPPORT STRUCTURE - SEAT TRACK, BETWEEN FR20 AND FR21, Y1959. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 33,348 hrs · 18,403 cycles

EMERGENCY LIGHTS PUSH TO TEST SWITCH IN COURIER AREA DOES NOT ILLUMINATE DURING TEST. DURING LIGHTING TEST, ALSO NOTED RED LED ON FRONT FACE OF POWER SUPPLY UNIT (29WL1) WAS ILLUMINATED.REMOVED AND REPLACED POWER SUPPLY UNIT (29WL1) REF AMM 33-51-14-04. OPS TEST GOOD. COURIER AREA EMERGENCY LIGHTING PUSH TO TEST SWITCH (25WL) NOW ILLUMINATES DURING TEST. ITEM CLOSED.

Part: PAWL — OUT OF ALIGNMENT (L1 DOOR) · airframe 33,022 hrs · 18,204 cycles

L1 DOOR ESCAPE SLIDE HANDLE DIFFICULT TO DISARM HANDLE STIFF AND WE COULDN'T MOVE IT FAR ENOUGH INTO THE DISARM POSITION TO PIN IT. . RELEASED FOR SERVICE PER MEL : 52-XX-XX-XX CATEGORY : C EXP "MEL 52-XX-XX-XX: CREW ENTRY DOOR ESCAPE SLIDE L1 - INOP. SLIDE REMAINS INSTALLED ON DOOR. APPEARS AFT FLOOR ENGAGEMENT PAWL IS CATCHING WHEN ARMING LEVER IS MOVED TO THE DISARM POSITION. OUND L1 DOOR DIFFICULT TO DISARM INTERMITTANTLY. FORWARD ENGAGEMENT PAWL AND AND GIRT BAR POSSIBLY WORN. CLEANED ENGAGEMENT TRACKS.FOUND MINOR BURS ON FORWARD FORWARD GIRT BAR BASE PLATE. CLEANED BURS AND LUBRICATED FORWARD AND AFT GIRT BAR BASE PLATE REF SMP. PERFORMED ADJ TEST REF A300-600 AMM 52-10-30-05-02. OPS CHECKED GOOD. MOVED ARMING HANDLE SEVERAL TIMES WITH NO DEFECTS AFTER MULTIPLE SMOOTH APPLICATIONS, ARMING LEVER JAMMED. ONCE RELEASED, OPERATED SMOOTHLY AGAIN FOR MULTIPLE CYCLES.

Part: HOSE — WORN (HYD SYSTEM) · airframe 33,015 hrs · 18,199 cycles

LOST GREEN HYDRAULIC SYSTEM PASSING THROUGH FL290. FLUID LEVEL DECREASED TO RED DOT ALMOST IMMEDIATELY. LEVELED A\C AT FL330, SLOWED TO GREEN DOT. COMPLIED WITH QRH. DESCENDED TO FL310 AND MAINTAINED .65 MACH. CONTINUED TO MEMPHIS, EMERGENCY DECLARED WITH CENTER, MANUAL GRAVITY EXTENDED GEAR. LANDED 18R EXITED HIGH SPEED TO BE TOWED IN. I CAPT. GREEN/REPORTS HYD PUMPS WERE ONLY OPERABLE FOR 10S DURING FLUID DECREASE. BOTH WERE TURNED OFF WITHIN 10 SECONDS. FOUND #2 ENG GREEN HYD PUMP SUCTION LINE LEAKING AT FIRST CLAMP ABOVE PUMP. BRACKET THAT SHOULD HOLD CLAMP WAS BROKEN AND WORE THRU LINE. REMOVED AND REPLACED LINE AND BRACKET.

Part: MOUNT — CRACKED (K FLAP) · airframe 32,715 hrs · 18,018 cycles

ON SLAT EXTENSION ON APPROACH GOT ECAM "KREUGER NOT EXTENDED" REMAINED NOT EXTENDED THROUGH LANDING. ON POSTFLIGHT WALKAROUND FOUND LEFT KRUEGER FLAP VANE OUTBOARD BRACKET MOUNT CRACKED AND INBOARD BRACKET BROKEN. REMOVED KRUEGER FLAP MOVEABLE VANE, PER MM 27-87-12-04-0. INSTALLED KRUEGER FLAP PER AMM A300 27-87-11-04. RIG AND OPS CHECK GOOD.

Part: INDICATION SYS — INOPERATIVE (R1 DOOR) · airframe 31,678 hrs · 17,388 cycles

PDIS 671 52-70 0953 17MAR20 IND OPEN U LOGPAGES:3230401 R1 DOOR SLIDE WILL NOT ARM MEL 17MAR20 00:00 IND U RELEASED FOR SERVICE PER MEL : 52-30-04 CATEGORY : C EXPIRATION : 27MAR20 "MEL 52-30-04: ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE." C/7220723

Part: INDICATION SYS — MALFUNCTIONED (R1 DOOR) · airframe 31,678 hrs · 17,388 cycles

PDIS 671 52-70 0953 17MAR20 IND OPEN U LOGPAGES:3230401 R1 DOOR SLIDE WILL NOT ARM MEL 17MAR20 00:00 IND U RELEASED FOR SERVICE PER MEL : 52-30-04 CATEGORY : C EXPIRATION : 27MAR20 "MEL 52-30-04: ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE." C/7220723 FACT 18MAR20 01:32 IND RESET ASPSU SUPPLY C/B IN REF TO AMM 52-73-00-05-02 OPS TEST OK A/C OK FOR SERVICE.

Part: SKIN — CRACKED (FRAME 40) · airframe 31,333 hrs · 17,182 cycles

FR40 CTR WING JOINT AT UPPER SKIN LEVEL LH MIDDLE HOLE NDT HFEC INSPECTION FOUND CRACK SIGNAL. FR40 CTR WING JOINT AT UPPER SKIN LEVEL LH MIDDLE HOLE CRACK. COMPLIED WITH FEDEX EA:6-5710-T0350731 P1. TITLE: WINGS - BASIC WING STRUCTURE - CRACK IN THE MIDDLE HOLE AT FR40 LHS CENTER WING JOINT. THIS IS MAJOR REPAIR IAW FEDEX GMM6-2- 100. REPAIR LIFE LIMITATION: 6 MONTHS.

Part: CROSSBEAM — CRACKED (FRAME 64) · airframe 31,333 hrs · 17,182 cycles

MDC FLOOR - FR64 Y-1456 - Y-1959, CROSSBEAM CRACKED APPROX 0.5 INCH IN LENGTH. MDC FLOOR FR64 B/W Y-1456 AND Y-1959 CROSSBEAM CRACKED APPROX 0.5 INCH . REPAIRED THE CRACKED CROSSBEAM PER A300-600F SRM53-10-15 FIGURE211. THIS REPAIR CATEGORY IS A. MAJOR REPAIR IAW FEDEX GMM 6-2-100.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 31,333 hrs · 17,182 cycles

RH WING - MID FLAP RIB21 AFT AREA FOUND CRACK ON X-RAY INSPECTION. RH WING - MID FLAP RIB21 UPPER FLANGE CRACK BETWEEN STGR2.7 AND STGR2.8 . REPAIRED THE CRACKED RIB FLANGE PER A300-600F SRM57-50-00-201 FIG.201. TRACKING EA:6-5750-T0350993 HAS BEEN ISSUED TO TRACK THIS REPAIR. EA TITLE: WINGS - FLIGHT SURFACES - RH CENTER FLAP RIB 21 UPPER FLANGE CRACK BETWEEN STGR2.7 AND STGR2.8 - RSC TRACKING. THIS REPAIR CATEGORY IS A. MAJOR REPAIR IAW FEDEX GMM6-2-100.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 28,151 hrs · 15,298 cycles

LEFT WING INBD FLAP UPPER SURFACE HAS SEVERAL GOUGES. REPAIRED THE FLAP UPPER SURFACE IAW EA 6-5750-T0332914, PART 1. MAJOR REPAIR.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 28,151 hrs · 15,298 cycles

RIGHT INBD FLAP UPPER SURFACE HAS SEVERAL GOUGES. ACCOMPLISHED EA 6-5750-T0333072, PART 1. MAJOR REPAIR.

Part: SEAT TRACK — WORN (FRAME 78) · airframe 28,151 hrs · 15,298 cycles

SEAT TRACK IS HEAVILY WORN IN MAIN CABIN JUST AFT OF FRAME 78, Y852. REMOVED AND REPLACED THE SEAT TRACK SECTION IAW SRM 53-10-16. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FRAMES 33-34) · airframe 28,151 hrs · 15,298 cycles

MAIN CABIN SEAT TRACK HAS CORROSION AT Y0 BETWEEN FRAMES 33 AND 34. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-10-16, 51-4-21, AND SRM 51-40-44. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (FRAME 63) · airframe 28,151 hrs · 15,298 cycles

FLOOR PANEL 161AF HAS DELAMINATION ON BOTTOM SIDE. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-0005, REV M. MAJOR REPAIR

Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 28,151 hrs · 15,298 cycles

MAIN CABIN FLOOR PANEL 251VF IS BROKEN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-0005. MAJOR REPAIR.

Part: FLOORBOARD — DENTED (MAIN CABIN) · airframe 28,151 hrs · 15,298 cycles

MAIN CABIN FLOOR PANEL 241TH HAS SEVERAL DENTS AND MISSING EDGE FILLER. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-0005. MAJOR REPAIR.

Part: SUPPORT — CRACKED (FRAME 45) · airframe 28,151 hrs · 15,298 cycles

MAIN CABIN SUPPORT WEB IS CRACKED AT FRAME 45. REMOVED AND REPLACED THE SUPPORT WEB IAW SRM 51-40-21 AND SRM 51-40-44. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,151 hrs · 15,298 cycles

MAIN CABIN SEAT TRACK HAS CORROSION BETWEEN FRAME 54.1 -Y1959. REMOVED AND REPLACED MAIN CABIN SEAT TRACK BETWEEN FR 54.1 -Y1959 IAW SRM 51-40- 21. THIS IS A MAJOR REPAIR.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 28,151 hrs · 15,298 cycles

MAIN CABIN FLOOR PANEL 242UJ HAS DISBONDED CORNER. REPAIRED DAMAGE ON MAIN CABIN FLOOR PANEL 242UJ IAW SRM 53-10-20 PARA 8B FIG 203. THIS IS A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,151 hrs · 15,298 cycles

MAIN CABIN SEAT TRACK HAS CORROSION AT FR 40 -Y1456. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, REMOVED SEAT TRACK AND 5EA FLOOR SUPPORTS AND DRILLED NEW SEAT TRACK, INSTALLED SEAT TRACK AND AND 5EA FLOOR SUPPORTS IAW SRM 53-10-16, 51-40-21, 51-40 40-40. THIS IS A MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 28,151 hrs · 15,298 cycles

MAIN CABIN FLOOR PANEL 241DF HAS IMPACT DAMAGE. FABRICATED MAIN CABIN FLOOR PANEL 241DF REF 70013348480001 AND DWG SRZ 25-005 REV M. THIS IS A MAJOR REPAIR.

Part: FLOOR PANEL — DENTED (CABIN) · airframe 28,151 hrs · 15,298 cycles

MAIN CABIN FLOOR PANEL 242UJ HAS SEVERAL DENTS. FABRICATED MAIN CABIN FLOOR PANEL 242UJ REF 70013348500001 AND DWG SRZ 25-005 REV M. THIS IS A MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (MDC) · airframe 28,151 hrs · 15,298 cycles

MDC FLOOR PANEL 252DH IS BROKEN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (MDC) · airframe 28,151 hrs · 15,298 cycles

MDC FLOOR PANEL 262VF IS BROKEN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (MAIN CARGO) · airframe 28,151 hrs · 15,298 cycles

MAIN DECK CARGO FLOOR PANEL 261AH BROKEN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005 REV M, MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (MAIN CABIN) · airframe 28,151 hrs · 15,298 cycles

MAIN CABIN FLOOR PANEL 241EK HAS SEVERAL PUNCTURES. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.

Part: FLOORBOARD — DENTED (MAIN CABIN) · airframe 28,151 hrs · 15,298 cycles

MAIN CABIN FLOORBOARD 242ZJ HAS SEVERAL DENTS. FABRICATED A NEW FLOOBOARD IAW DWG SRZ 25-005

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 28,151 hrs · 15,298 cycles

MAIN CABIN FLOOR PANEL 251YH HAS PUNCTURED/CRACKED/DISBONDED. REPAIRED DAMAGED ON MAIN CABIN FLOOR PANEL 251YH IAW A300-600-SRM 53-10-20 PARA 8B FIG 203.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 28,151 hrs · 15,298 cycles

MAIN CABIN FLOOR PANEL 241HK IS DISBONDED. REPAIRED DAMAGE ON MAIN CABIN FLOOR PANEL 241HK IAW A300-600 SRM 53-10-20 PRA 8B FIG 203. THIS IS A MAJOR REPAIR.

Part: SWITCH — FAILED (SMOKE DETECTOR) · airframe 27,648 hrs · 15,014 cycles

ON TAXI ECAM AVIONICS SMOKE WARNING. NO INDICATION OF SMOKE. FOUND AVIONICS SMOKE INDICATOR BULB CONTACTS WORN FLAT. REMOVED AND REPLACED THE BULBS AND PERFORMED SATISFACTORY ANNUCIATOR LIGHT TEST IAW AMM 33-14-00-05. STARTED TROUBLESHOOTING IAW AMM 26-15-00-05. WHEN PERFORMING PTT AVIONICS SMOKE WARNING LIGHT DID NOT ILLUMINATE. TAPPED ON WARNING LIGHT AND WAS ABLE TO GET LIGHT TO COME ON. TAPPED SEVERAL TIMES AND WAS ABLE TO GET LIGHT TO GO OUT AND COME ON. ALSO TESTED IN NORMAL CONFIGURATION AND WAS ABLE TO GET THE LIGHT TO COME ON AND GO OFF BY TAPPING ON THE SWITCH. REPLACED THE THE SWITCH. TEST OF AVIONICS COMPARTMENT SMOKE DETECTION NORMAL IAW MM 26-15-00-05.

Part: SMOKE DETECTOR — MALFUNCTIONED (E/E BAY) · airframe 27,523 hrs · 14,934 cycles

AVIONICS SMOKE WARNING WITH CHIME ACTIVATED FL330 AND CONTINUED TO COME ON INTERMITTENTLY FOR REMAINDER OF FLIGHT. INSTALLED SMOKE DETECTOR 11WA AND 13 WA. OPS CHECKED GOOD IAW AMM 26-15-12-04 AND 26-15-00-05. ACFT OK FOR SERVICE IAW GMM 12-7-600

Part: SMOKE DETECTOR — MALFUNCTIONED (E/E BAY) · airframe 27,523 hrs · 14,934 cycles

AVIONICS SMOKE WARNING WITH CHIME ACTIVATED FL330 AND CONTINUED TO COME ON INTERMITTENTLY FOR REMAINDER OF FLIGHT. INSTALLED SMOKE DETECTOR 11WA AND 13 WA. OPS CHECKED GOOD IAW AMM 26-15-12-04 AND 26-15-00-05. ACFT OK FOR SERVICE IAW GMM 12-7-600.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 27,350 hrs · 14,826 cycles

NR 1 ENGINE GREEN SYS HYDRAULIC PUMP LOW PRESSURE. FLIGHT CREW VERIFIED GOOD PRESSURE FROM NR 1 ENGINE HYD GREEN PUMP BY SHUTTING DOWN NR 2 ENGINE AND ECAM INDICATIONS ARE NORMAL AND DID NOT GET A CHIME WHEN LIGHT ILLUMINATED. QTY IS NORMAL. RELEASED FOR SERVICE IAW MEL: 29-34-01-A CATEGORY: C-EXPIRATION. MEL 29-34-01-A: ENG NR 1 HYD PUMP LOW POWER LIGHTS INOPERATIVE REF TO MEL 29-34-01-A FOR PROCEDURE TO VERIFY CORRECT PUMP OPERATION PRIOR TO DEPARTURE.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 26,623 hrs · 14,421 cycles

PRESSURE REG 1 & 2 FAULT IN CLIMB OUT. AFTER RESET, FAILED AGAIN. AFT OUTFLOW VLV REMAINED FULL OPEN, WOULD NOT CLOSE, IN MANUAL. INSPECTED E & E, COURIER AREA & MAIN CARGO DECK. FOUND WATER IN ALL THREE AREAS. INSPECTED E & E COMPARTMENT NO WATER FOUND IAW MM 05-50-01-0. OPERATIONAL CHECK OF CABIN PRESS CONTROL SYS FOUND THAT THE AFT OUTFLOW VLV NOT WORKING IN AUTO MODE & SLOW IN MANUAL MODE. REMOVED & AFT OUTFLOW VLV IAW MM 21-31-12-04. OPERATIONS CHECK & TEST IAW 21-31-00-05. ALL TEST PASSED. ACFT OK FOR SERVICE. PART REMOVED PN 88005B0306 & SN 786.

Part: PROBE — UNKNOWN (PITOT/STATIC SYS) · airframe 263 hrs · 14,282 cycles

AIRCRAFT AUTOPILOT DID A POOR JOB, /- 10, OF HOLDING AIRSPEED IN CLIMB & DESCENT. IN PROFILE IN DECENT AIRSPEED KEPT CREEPING INTO ZIPPER. WENT LEVEL & CHG DIALED AIRSPEED BACK WITH NO HELP. BROUGHT THROTTLES TO IDLE MANUALLY & ACFT WENT INTO THRUST LATCH & TRIED TO CLIMB, WITH AUTOPILOT & AUTO THROTTLES OFF. AIRPLANE ATTEMPTED TO DIVE TO 10 DEG NOSE LOW @ 6000 FT PER MIN DIVE. SELECTED ADC 2 & RECOVERED. R & R NR 1 ADC IAW 34-11-34-04, R & R NR 1 FLIGHT AUGMENTATION COMPUTER IAW 22-26-34-04. R & R CAPTAINS PITOT PROBE IAW 34-11-15-04. DUE TO LLM PARTS BEING CHANGED PERFORMED AFS LAND TEST IAW 22-40-00-5, 22-00-00-2-0, NO FAULTS FOUND. ALL CHECKED NORMAL. ACFT OK FOR SERVICE.

Part: BRACKET — BROKEN (PROX SENSOR) · airframe 260 hrs · 14,138 cycles

AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT IN SYS 1 OR 2. ECAM SHOWED LG RETRACTION FAULT. FOUND PROXIMITY SENSOR BRACKET BROKEN, REMOVED AND FABRICATED IAW AMM 32-11-14-04. INSTALLED PROXIMITY DETECTOR IAW AMM 32-00- 00-4. PERFORMED GEAR SWING OF SYSTEM 1 AND 2 IAW AMM 32-31-00. OPS CHECKED GOOD.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 260 hrs · 14,136 cycles

PRESSURIZATION SAFETY VALVE SHOWED OPEN & AMBER ON ECAM. ACFT WOULD NOT PRESSURIZE MORE THAN 2.1 DIFFERENTIAL, CABIN CLIMBED TO 10,000 RETURNED. PRESSURIZED ACFT AGAIN AND FOUND NR 1 SAFETY VALVE FAULTY, REMOVED AND REPLACED THE SAFETY VALVE IAW MM 21-31-15-04. SAFETY VALVE OPERATES NORMAL, ACFT PRESSURIZATION OPERATES NORMAL IAW MM 21-31-00-05.

Part: FRAME — DAMAGED (FRM 27) · airframe 25,174 hrs · 13,625 cycles

MAIN DECK CARGO FRAME 27 DAMAGED STRINGER 13 - 23R. REPAIRED IAW EA 6-5310-T0314096.

Part: FRAME — DAMAGED (FRM 28) · airframe 25,174 hrs · 13,625 cycles

MAIN DECK CARGO FRAME 28 DAMAGED STRINGERS 8 - 22L. REPAIRED IAW EA 6-5310-T0314096.

Part: UNION — LOOSE (HYD LINE) · airframe 25,174 hrs · 13,625 cycles

LEFT PYLON AFT FAIRING FROM FWD TO AFT NR 4 HYD TUBE CONNECTOR LOOSE. REMOVED THE FITTING OF THE HYD TUBE BETWEEN WING AND PYLON IAW AMM 29-00-00-04 & DWG A29011098. MINOR REPAIR IAW GMM 6-2-100

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 25,174 hrs · 13,625 cycles

MDCC Y1456 SEAT TRACK FOUND CRACK BETWEEN FRAME 71 - 72.

Part: CARGO TRACK — CORRODED (FRAMES 56-57) · corrosion level 2 · airframe 25,174 hrs · 13,625 cycles

MAIN DECK CARGO TRACK FOUND CORRODED BETWEEN FRAME 56 - 57. REPAIRED IAW SRM 53-10-16-201 PARA.4 FIG 201. MAJOR REPAIR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 25,174 hrs · 13,625 cycles

MDCC Y0 SEAT TRACK FOUND CRACK BETWEEN FRAME 57.3 - 58.

Part: FRAME — CRACKED (FRM 40) · airframe 25,174 hrs · 13,625 cycles

FRAME 40 CRACKED. EA 6-5710-T0313842. MAJOR REPAIR IAW GMM 6-2-100.

Part: FRAME — CRACKED (FRM 40) · airframe 25,174 hrs · 13,625 cycles

FRAME 40 CRACKED. REPAIRED IAW EA 6-5710-T0313842. MAJOR REPAIR IAW GMM 6-2-100.

Part: FRAME — CRACKED (FRM 40) · airframe 25,174 hrs · 13,625 cycles

FRAME 40 CRACKED. REPAIRED IAW EA 6-5710-T0313842. MAJOR REPAIR IAW GMM 6-2-100.

Part: SKIN — CRACKED (FRAME 47) · airframe 25,174 hrs · 13,625 cycles

RIGHT FUSELAGE SKIN FOUND CRACKED. REPAIRED IAW EA6-5710-T0313870. MAJOR REPAIR IAW GMM 6-2-100.

Part: SKIN — CRACKED (FRAME 47) · airframe 25,174 hrs · 13,625 cycles

INSPECTION OF REAR SPAR BOTTOM SKIN AROUND E HOLE FOUND CRACKED. REPAIRED IAW EA6-5710-T0313870. MAJOR REPAIR IAW GMM6-2-100.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 24,326 hrs · 13,201 cycles

RIGHT RIB 5 HAS CORROSION IN BORE & FWD & AFT FACES. COMPLIED WITH EA 6-5710-T0307409 WINGS BASIC WING STRUCTURE RT RIB 5 BORE CORROSION.

Part: LUG — CORRODED (LT MLG) · corrosion level 2 · airframe 24,326 hrs · 13,201 cycles

LEFT MLG FITTING FWD LUG CORRODED ON FWD & AFT FACE & IN THE BORE. REPAIRED IAW EA 6-5710-T0307354 PART 1.

Part: WARNING MESSAGE — FALSE INDICATION (HYD SYSTEM) · airframe 23,196 hrs · 12,560 cycles

GREEN HYD LOW QTY, ECAMS DURING FLIGHT WAS INTERMITTENT AT FIRST BUT THEN BECAME STEADY. QTY OVERHEAD INDICATED JUST ABOVE RED DOT, ECAM INDICATION WAS AT TO SLIGHTLY ABOVE MIN LEVEL (RED). COMPLIED WITH ECAM AND TURNED OFF GREEN PUMPS. FOUND NO EVIDENCE OF HYD FLUID LEAK ON ARRIVAL TO GATE. RESERVOIR GAGE READING SIX GALLONS AND COCKPIT HYD QTY INDICATOR READING MIDDLE OF GREEN BAND, ECAM HYD PAGE READING WAS NORMAL. AFTER 30 MINUTES AT GATE, RESEVOIR READING DOWN TO 4.7 GALLONS AND COCKPIT INDICATION OUT OF GREEN BAND. PERFORMED WIRE SHAKE TEST AROUND RESEVOIR, GROUND SERVICE PANEL, UNABLE TO DUPLICATE THE PROBLEM. R & R GREEN RESERVOIR QTY TRANSMITTER IAW MM 29-31-11 AND OPERATE GREEN HYD SYS ALL INDICATION NORMAL.

Part: CARGO TRACK — CORRODED (MAIN CARGO) · corrosion level 2 · airframe 22,091 hrs · 11,926 cycles

MAIN DECK CARGO TRACK 3R CORRODED AT APPROXIMATEY EIGHT INCHES AFT OF FR 69, R & R CARGO TRACK IAW FSRM 51-72-10.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 22,091 hrs · 11,926 cycles

SEAT TRACK 4L HAS 2SQ CORROSION BETWEEN FR 75 AND FR 76. AFTER REMOVAL OF LEVEL 1 CORROSION FROM SEAT TRACK 4L BETWEEN FR 75 AND 76. FOUND TO BE OUT OF LIMITS IAW FSRM 53-10-16, PG 103, FIG 101. FABRICATED AND INSTALLED NEW SEAT TRACK 4L BETWEEN FR 74 AND 77 WITH SPLICES IAW FSRM 53-10-16, FIG 201A.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 22,091 hrs · 11,926 cycles

SEAT TRACK 3R AT APX 11" FWD OF FR57.2 HAS CORROSSION. AFTER REMOVAL OF LEVEL 1 CORROSION SEAT TRACK WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 101. R & R SEAT TRACK IAW SRM 53-10-16.

Part: FLOOR PANEL — CORRODED (ZONE 160) · airframe 22,091 hrs · 11,926 cycles

FLOOR PANEL NR 162HF HAS CORROSION TOP SURFACE. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 22,091 hrs · 11,926 cycles

FLOOR PANEL NR 161CF BACK SIDE HAS DELAMINATION ON EDGE. FLOOR PANEL DAMAGE IS BEYOND REPAIR. FABRICATED FLOOR PANEL IAW DWG SRZ-25-005 REV J & DWG SRZ-25-011, REV D.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 22,091 hrs · 11,926 cycles

MAIN CABIN DUMMY TRACK CENTER LINE SEAT TRACK 1 BETWEEN FR 38.2 AND FR 40 HAS A BROKEN SCALLOP. R & R MAIN CABIN DUMMY TRACK CENTER LINE SEAT TRACK 1 BETWEEN FR 38.2 AND FR 40 IAW FSRM 51-72-10, PG 2, PARA 6, FSRM 53-15-16, PG 3 AND AMM 20-21-12. DUE MATERIAL DEFORMATION AND CRACKED .5" LONG IS FOUND TO BE OUT OF LIMITS IAW FSRM 53-10-16, FIG 101.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 22,091 hrs · 11,926 cycles

AFT CARGO FLOOR PANEL 151WF HAS TWO DAMAGED CORNERS APPROX NINE SQUARE INCHES. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 22,091 hrs · 11,926 cycles

AFT CARGO FLOOR PANEL 151UF HAS TWO DAMAGED CORNERS APPROX TEN SQUARE INCHES. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 22,091 hrs · 11,926 cycles

FLOOR PANEL 241LK IS BROKEN. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 22,091 hrs · 11,926 cycles

FLOOR PANEL 242ZJ HAS ONE, TEN INCH CRACK. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 22,091 hrs · 11,926 cycles

FLOOR PANEL 242EK HAS TWO, TEN INCH CRACKS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 22,091 hrs · 11,926 cycles

FLOOR PANEL 132MG, BACKSIDE OF PANEL HAS SEVERAL CRUSHED HONEYCOMB CORE & FOUR MISSING INSERTS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 22,091 hrs · 11,926 cycles

FLOOR PANEL 242QJ, HAS TWO, TEN INCH CRACKS. FARICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.

Part: HANDLE — INOPERATIVE (MLG) · airframe 21,019 hrs · 11,288 cycles

ON TAKEOFF WITH GEAR DETECTION SYS NR 2 DEFERRED, GEAR HANDLE WOULD NOT RAISE PAST NEUTRAL POSITION USING SYS NR 1. SWUNG GEAR IN SYS 1 & 2 SEVERAL TIMES IN EA. AND WAS ABLE TO DUPLICATE PROBLEM DEPENDING ON SPEED OF HANDLE MOVEMENT. R & R HANDLE MODULE IN REF MM 32-31-11-04. OPS CHECKS GOOD AND UNABLE TO DUPLICATE PROBLEM NO MATTER HOW QUICKLY HANDLE WAS RAISED. ALSO R & R SYS 2 RELAYS 14GB, 17GB, AND 18GB PRECAUTIONARY IN REF SMP. ALSO, JACKED AFT AXLE OF LT AND RT BOGIE BEAMS AND BOTH RETURNED TO CENTER WHEN RELEASED.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 20,904 hrs · 11,222 cycles

COURIER EMERGENCY LIGHT TEST NOT FUNCTIONING. COURIER EMERGENCY LIGHTING POWER SUPPLY REPLACED IAW AMM 33-51-14-04-0. OP CHECKS OK. PREMATURE REMOVAL/INSTALLATION. COURIER EMERGENCY LIGHTING POWER SUPPLY REPLACED IAW AMM 33-51-14-04-0. OPS CHECKS OK.

Part: RADAR — INOPERATIVE (WX RADAR) · airframe 20,709 hrs · 11,113 cycles

RADAR WENT INOP AFTER TAKEOFF ON SYS 1 & 2, REMOVED BOTH WEATHER RADARS T/R AND CLEANED CONECTORS AND SWAPPED BOTH T/R IAW AMM34-41-33-04-02, AND OPS CHECK OUT BOTH WEATHER RADARS AMM-34-41-00-05-01, ALL OPS CHECKED GOOD.

Part: SELECTOR VALVE — INOPERATIVE (MLG) · airframe 20,343 hrs · 10,913 cycles

DURING T/O AT GEAR RETRACTION, ECAM INDICATED AUTO BRAKES FAULT ALONE WITH ILLUMINATION OF THE BRAKE FAIL LIGHT. COMPLIED WITH ECAM SELECTED AUTOBRAKES TO ALTN/OFF. AFTER LANDING BRAKE FAIL LIGHT OUT. DURING TAXING IN, SELECTED NORMAL (BRK-ANTISKID SWITCH). APPLIED BRAKE PRESSURE. BRAKE PRESSURE INDICATOR SHOWED YELLOW SYS PRESSURE SWITCH BREAK - ANTISKID SELECTOR BACK TO ALT/OFF. TAXI TO PARKING. R & R BRAKE SELECTOR VALVE IAW AMM 32-42-11-04.

Part: PROXIMITY SENSOR — MALFUNCTIONED (MLG) · airframe 19,729 hrs · 10,556 cycles

LANDING GEAR FAILED TO RETRACT. COULD NOT MOVE HANDLE TO "UP" POSITION. REMOVED AND REPLACED PROXIMITY ELEC UNIT PER AMM REF 32-31-71-04. REMOVED AND REPLACED LEFT MAIN LANDING GEAR BOGIE BEAM PROXIMITY DETECTORS FOR SYSTEM NR 1 AND 2. PRESSURE LUBRICATED BOTH BOGIE BEAM PIVOT PINS. PERFORMED GEAR SWING BOTH SYSTEMS PER 32-31-00-05. NO DEFECTS NOTED. SMOOTH PIVOT OF BOGIE BEAMS OBSERVED.

Part: PROXIMITY SENSOR — FAILED (MLG) · airframe 19,721 hrs · 10,551 cycles

UNSAFE GEAR ON RETRACTION; HANDLE WOULD NOT PASS DET ENT 3 RED UNSAFE; GEAR LOWERED AND GOT 3 GREEN DOWN AND LOCKED, LANDED, NO FURTHER INCIDENT-INFO: AUTO THROTTLE ALSO INOP. PILOT SAID NO OVERWEIGHT LANDING WAS MADE. INTERRAGATED 54GB. FOUND FAULT CODE 63 AND A "BOX" AND "FAULT" FAULT LIGHTS ON. CHANGED IAW AMM ATA 32-31-71-04-0. DID GEAR RETRACTION AND EXTENSION TEST ON SYS 1 AND SYS 2. OPS CHECKED GOOD IAW AMM ATA 32-31-00-05.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 19,182 hrs · 10,264 cycles

MAIN DECK CARGO COMPARTMENT SEA TRACK 4 RT,FR 29 HAS 4 EA BROKEN SCALLOPS. REMOVED DAMAGED SECTION OF SEAT TRACK 4RT AND INSTALLED SEAT TRACK SPLICE REPAIR AT TRACK 4RT BETWEEN FR 26 AND 30 IAW FREIGHTER SRM 53-10-16, PG 201.

Part: FLOORBEAM — BENT (ZONE 200) · airframe 19,182 hrs · 10,264 cycles

MDCC FLOORBEAM AT FR 65 BETWEEN SEATTRACKS 3L AND 4L IS BENT/ DISTORTED APPROX 18 " IN LONG X .08 DEFLECTION. REPAIRED FLOORBEAM AT FR 65 BETWEEN 3L AND 4L USING SPLICING METHOD IAW SRM 53-10-15, CONFIG 2, PG 27, FIG 3, SHEET 2 COMPLIED WITH REQUIRED OPS TEST REFERRED TO ON JPF ATTACHED FOR INDIVIDUAL SIGNOFFS.

Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 19,182 hrs · 10,264 cycles

FLOORBEAM AT FR 64 BETWEEN SEAT TRACKS 3L AND 4L IS BENT/DISTORTED APPROX 18 IN LENGTH X .05 IN DEFLECTION. REPAIRED FR 64 CROSSBEAM USING SPLICING METHOD IAW FREIGHTER SRM 53-10-15, FIG 207, SHT 41.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 19,182 hrs · 10,264 cycles

SEATRACK 4-R HAS 2EA AREAS OF CORROSION BETWEEN FR 39-44 UPON INSP FOUND SEAT TRACK 4R NR FR 39 TO FR 44 CRACKED BY A LENGTH 5IN". REMOVED DAMAGED DUMMY TRACK & INSTALLED NEW DUMMY TRACK IAW SRM 51-72-10. TOPCOATED FASTENERS IAW SRM 51-75-10.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 19,182 hrs · 10,264 cycles

CROSSBEAM AT FR 31 FWD SIDE 1 IN BELOW FLOOR AND LBL 67 IN CRACKED .5 IN LENGTH. ROUTED OUT CRACK ON CROSSBEAM AT FR 31 FWD 1 IN. BELOW FLOOR LBL 67 IN FABBED DOUBLER AND INSTALLED IAW SRM 53-10-15 FIG 212 SHEET 1.

Part: ADAPTER — CORRODED (ZONE 200) · airframe 19,182 hrs · 10,264 cycles

MDCC CLS ADAPTER UPR SURFACE BETWEEN SCALLOPS CORRODED LOCATED FRAME 24 RBL, 63 INCHES TO RBL 65 INCHES. REMOVED LEVEL 1 CORROSION. FOUND OUT OF LIMITS. R & R MDCC CLS ADAPTER FRAME 24 RBL 63 INCHES IAW SRM 51-72-10.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 19,182 hrs · 10,264 cycles

MDCC SEAT TRACK 4L BETWEEN FRAMES 38 AND 40 HAS 4 EA AREAS OF CORROSION. DEFECT MEASURES 4 SQ INCHES. REMOVED LEVEL 1 CORROSION FOUND TRACK OUT OF LIMITS. R & R DUMMY SEAT TRACK BETWEEN FRAMES 38 AND 40 IAW SRM 51-72-10.

Part: ADAPTER — GOUGED (ZONE 200) · airframe 19,182 hrs · 10,264 cycles

MDCC CLS ADAPTER BETWEEN SEAT TRACKS 4L AND 5L WORN .37 SQ INCHES FRAME 30. REMOVED AND REPLACED CLS ADAPTER BETWEEN SEAT TRACKS 4L AND 5L FRAME 30 IAW SRM 51-72-10.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 19,182 hrs · 10,264 cycles

DUMMY TRACK 4R BETWEEN FRAMES 54.1 AND 54.2 IS CRACKED AT THE SCALLOPS APPROX 6 INCHES. R & R DUMMY TRACK 4R BETWEEN FRAMES 54.1 AND 54.2 IAW SRM 53-15-16.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 19,182 hrs · 10,264 cycles

FUSELAGE INT DUMMY SEAT TRACK RT 3R AT FRAME 38.2 ATTACHMENT GAP IS .019 INCH. EXCEEDS LIMITS IAW EO E6-5310-7-3322 PT 1. REMOVED DUMMY SEAT TRACK RT 3R AT FRAME 38.2. FABBED 1 EA INSERT BUSHING AND BONDED INSERT IN DUMMY SEAT TRACK IAW SRM 53-15-16. REINSTALLED DUMMY SEAT TRACK RT 3R AT FRAME 38.2 IAW SRM 53-15-16.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 19,182 hrs · 10,264 cycles

MDCC SEAT TRACK 3R HAS A 1 SQ INCH AREA OF CORROSION BETWEEN FRAMES 38.1 AND 38.2. REMOVED LEVEL 1 CORROSION. FOUND OUT OF LIMITS. R & R SEAT TRACK 3R BETWEEN FRAMES 38.1 AND 38.2 IAW SRM 53-10-16. SEAT TRACK FABRICATED FROM EXTRUSION PN 60-22457/7075T76511.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 19,182 hrs · 10,264 cycles

FUSELAGE INT, DUMMY SEAT TRACK LT NR 2 AT FRAME 38.2, ATTACHMENT GAP IS .017 IN. EXCEEDS LIMITS IAW EO 6-5310-7-3322 PT1. REMOVED DUMMY SEAT TRACK LT NR 2 AT FRAME 38.2 AND REPAIRED IAW SRM 53-15-16. FABBED BUSHING INSERT AND BONDING INSERT IN TRACK IAW SRM 53-15-16. REINSTALLED DUMMY SEAT TRACK LT NR 2 AT FRAME 38.2 IAW SRM 53-15-16.

Part: ADAPTER — CORRODED (ZONE 200) · airframe 19,182 hrs · 10,264 cycles

CLS ADAPTER UPR SURFACE CORRODED AT SCALLOPS LOCATED FRAME 22 RBL 63 INCH TO 65 INCH. REMOVED LEVEL 1 CORROSION. FOUND OUT OF LIMITS. R & R CLS ADAPTER IAW SRM 51-72-10.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 19,182 hrs · 10,264 cycles

MDCC SEAT TRACK 3R BETWEEN FRAMES 54 TO 54.1 HAS A 1 SQ INCH AREA OF CORROSION ON TRACK AND SCALLOPS. R & R SEAT TRACK 3R BETWEEN 54 AND 54.1 IAW SRM 51-72-10.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 19,182 hrs · 10,264 cycles

FUSELAGE INT DUMMY SEAT TRACK RT 2R AT FRAME 38.2 ATTACHMENT GAP IS .020 IN. EXCEEDS LIMITS IAW EO 6-5310-7-3322 PT1. REMOVED DUMMY SEAT TRACK RT 2R FRAME 38.2 IAW SRM 53-15-16. FABBED 1 EA INSERT BUSHING AND BONDED INSERT IN DUMMY SEAT TRACK IAW SRM 53-15-16. REINSTALLED DUMMY SEAT TRACK RT 2R AT FRAME 38.2 IAW SRM 53-15 16.

Part: RESTRICTOR VALVE — DIRTY (MLG) · airframe 17,607 hrs · 9,426 cycles

ON APPROACH, LOWERED LANDING GEAR, LT MAIN GEAR SHOWED UNSAFE IN BOTH SYS 1 AND SYS 2 AND NR 3 GEAR SYS. ON GO AROUND, GEAR CAME DOWN. CREW AND STATED LIGHTS WENT SAFE AFTER GO AROUND, RAISED GEAR AND TRIED AGAIN. RECEIVED UNSAFE LIGHTS AGAIN FOR LT MLG. FOUND LT GEAR WOULD TAKE APPROX 90-120 SECONDS TO START TO EXTEND AFTER RT GEAR, THEN WOULD OPERATE NORMALLY REF TSM 32-30-00. REMOVED MLG RESTRICTOR VALVE & FOUND IT CONTAMINATED. REPLACED VALVE, REMOVED MLG DOOR RESTRICTOR VALVE, NO CONTAMINATION FOUND. REPLACED AS A PRECAUTION. PERFORMED NUMEROUS GEAR SWINGS. OPS CHECKS NORMAL. R & R GREEN SYSTEM LOW PRESSURE & HIGH PRESSURE FILTERS. FOUND SMALL AMOUNT OF PARTICLES IN GREEN SYSTEM HIGH PRESSURE BOWL. SYSTEM LEAKS CHECKS GOOD INFORMED MOCC. ACFT OK FOR SERVICE, REF MM 32-31-57-4 & 32-31-58-4.

Part: OUTFLOW VALVE — DAMAGED (CABIN PRESS SYS) · airframe 16,760 hrs · 8,970 cycles

CLIMBING THROUGH FL 320 RECEIVED CABIN PRESS ADVISORY. ATTEMPTED TO SLOW CABIN ALTITUDE BUT OBSERVED FWD OUTFLOW VALVE OPEN HALFWAY. ATTEMPTED CYCLING BETWEEN REG 1 AND 2 TO TRY AND GET PRESS SYSTEM TO RESPOND. SLOWED A/C CLIMB AND RECEIVED CABIN ALTITUDE ABV 10K. FOLLOWED CHECKLIST PROCEDURES AND DIVERTED TO KELP. REMOVED ACCESS PANEL IN LWR FWD CARGO PIT TO ACCESS FWD OUTFLOW VALVE. ON INSPECTION FOUND SMALL AMOUNT OF ADJACENT INSULATION BLANKET IN VALVE AND DAMAGE TO VALVES DEBRIS SCREEN. VALVE AND SCREEN ON ORDER. PART NIS ELP. REMOVED AND REPLACED FORWARD OUTFLOW CONTROL VALVE REF 21-31-12-4, OPS CK GOOD.

Part: UNKNOWN — UNKNOWN · airframe 16,192 hrs · 8,679 cycles

IMMEDIATELY AFTER SELECTING TOGA ON THE RUNWAY GOT A CHIME AND ECAM MESSAGE. INITIATED AN ABORT THEN SAW AN ECAM MESSAGE INDICATING FMS DISAGREE. TAXIED CLEAR AND RELOADED THE RUNWAY IN THE FMS. ON THE SECOND TAKEOFF ATTEMPT THE TOGA LEVERS WOULD NOT ENGAGE WHEN SELECTED. CYCLED ALL FCC, FAC, AND TCC C/B'S REALIGNED ALL 3 IRU'S AND PERFORMED AFS LAND TEST IAW A300-600 MM 22-40-00. OP'S GOOD TOGA SYSTEM OP'S GOOD IAW A300-600 MM 22-30-00-5-01. GOOD LEG INTO YMX, 2:47 FLT TIME.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 16,186 hrs · 8,674 cycles

MCC SEAT TRACK SECTION 3R HAS CORROSION AT FR'S 57.1, 57.3 AND 57.5 REMOVED CORROSION IAW A300 SRM 51-74-10. ALODINED AND PRIMED IAW A300 SRM 51-75-10. AREA WAS FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK IAW A300 SRM 53-10-16. REPAIRED AND INSTALLED NEW SEAT TRACK IAW A300 SRM 53-10-16 AND A300 SRM 51-75-10.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 16,186 hrs · 8,674 cycles

MCC SEAT TRACK 2R HAS CORROSION AT FR75, 77, AND 78. INSTALLED SECTION OF SEAT TRACK AND 2 EA SPLICE AT 2 RT FR 75-77- AND 78 IAW A300 SRM 53-10-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,186 hrs · 8,674 cycles

MCC SEAT TRACK SECTION 2L HAS CORROSION AT FRAMES 77 AND 78. REMOVED AND INSTALLED SEAT TRACK IAW A300-600 SRM 53-1-16 AND 51-40-21.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 16,186 hrs · 8,674 cycles

FWD CARGO COMPT MAIN CABIN CROSSBEAM C-27 BETWEEN RT SEAT TRACK 2-3 CRACKED ON VERTICAL STIFFENER UPPER CONTOUR APPROX 1/4 IN LONG. REPAIRED CROSSBEAM C-27 BETWEEN RT SEAT TRACK 2-3 IAW A300-600 FSRM 53-10-15.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 16,186 hrs · 8,674 cycles

FWD CARGO COMPT FR 29 BETWEEN SEAT TRACKS 3R-2R APPROX 3/4 INCH CRACK IN FLOORBEAM REPAIRED CROSSBEAM AT FR 29 BETWEEN SEAT TRACK RT 2-3 IAW A300-600 FSRM 53-10-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,186 hrs · 8,674 cycles

MCC SEAT TRACK SECTION 3 R HAS CORROSION AT FRAMES FR 64.5 , 65.5 , AND 66. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 53-10-16. INSTALLED NEW SEAT TRACK, SECTION AND REPAIR SPLICES IAW A300-600 SRM 53-10-16 FROM FR 64 TO FR 68.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,186 hrs · 8,674 cycles

MCC FR 72 SEAT TRACK 3R HAS CORROSION I PLACE. REMOVED AND REPLACED SEAT TRACK SECTION BETWEEN FR 71 TO FR 73 IAW A300-600 SRM 53-10-16 AND 51-40-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,186 hrs · 8,674 cycles

MAIN CABIN LT NR 3 SEAT TRACK HAS 3 EACH AREAS OF CORROSION INSIDE/TOP OF SCALOPE HOLES WITH APPROX MEASUREMENTS FR 43=3-SQ IN, BETWEEN FR 44-45 =3 SQ IN ,FR 45- 46= 1 SQ IN. REMOVED AND REPLACED SEAT TRACK PER A300-600 SRM 51-40-21 AS FOUND BEYOND LIMIT PER A300-600 SRM 53-10-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,186 hrs · 8,674 cycles

MAIN CABIN LT SEAT TRACK NR 2 HAS THREE AREAS OF CORROSION INSIDE SCALOPE HOLES ON FOLLOWING; FR 42 = 2 IN LONG, FR 43 AFT 3 SQ IN, FR44- 45 2.5 SQ IN. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 51-72-10, DUE BEYOND LIMITS.

Part: SEAT TRACK — CORRODED (FUELAGE) · airframe 16,186 hrs · 8,674 cycles

MAIN CABIN LT NR 5 SEAT TRACK HAS 3 AREAS OF CORROSION INSIDE/TOP SCALOPE HOLES WITH APPROXIMATE MEASUREMENTS AS FOLLOWS; BETWEEN FR 44 -45 = 4 SQ IN, AFT OF FR 42 =4 SQ IN FR 41 = 3.5 SQ IN. REMOVED SEAT TRACK L5 FR 40 TO FR 45, AND REINSTALLED NEW PART PER A300-600 SRM 51-72-10, AS FOUND BEYOND LIMIT.

Part: ADC — FAILED (NR 2) · airframe 15,829 hrs · 8,473 cycles

DIVERTED TO IAD, CLIMBING THRU 16,000', GOT APPROX 25 KT DIFFERENCE IN AIR SPEED IND. SECONDARY GEAR IND INOP. ENG N-1 MODE FAULT. BLOWING OUT NR 2 SYS, REMOVED AND REPLACED ADC NR 2 PER MM 34-11-34-4. REMOVED AND REPLACED PROX BOX PER MM 32-31-71-4. ACN RELEASED FOR SERVICE PER MEL/CDL: 73-23-01-05-1.

Part: FLOW VALVE — MALFUNCTIONED (COCKPIT OXYGEN) · airframe 15,141 hrs · 8,107 cycles

ACFT DIVERTED INTO LBB WITH CREW LP SUPPLY READING 0 PSI AND NO AIR FLOW TO ANY POSS ON FLT DECK. TROUBLE SHOT PROBLEM TO CREW LP FLOW VALVE. SWAPED FLOW VALVE FROM COURIER POSS TO CREW POSS. CREW LP SYSTEM NOW OPERATIONAL. NO LEAKS NOTED AT THIS TIME. WILL MEL COURIER LP OXY SYSTEM.

Part: COUPLING — LEAKING (IDG) · airframe 13,765 hrs · 7,346 cycles

ON T/O ROLL, WHEN N1 WAS 80 - 90%, GOT GEN 1 FAULT ALERT. ABORTED T/O AT 70KTS. RESET GEN 1 AND ATTEMPTS A SECOND T/O WITH THE SAME RESULT. ABORTS AGAIN AT 70KTS. ACN RELEASED FOR SERVICE PER MEL/CDL: 24-11-01 CATEGORY: B EXPIRATION: 31MAR06 "MEL 24-11-01: GEN (IDENTIFY 1 OR 2) NR 1 INOP. A PU GEN MUST BE USED TO POWER AFFECTED BUS THROUGHOUT FLIGHT. VERIFY AND RECORD IN AML/EAML THAT OIL QTY OF IDG IN DISCONNECT MODE, REMAINING OPERATIVE IDG, AND APU GEN ARE CHECKED ONCE EACH FLIGHT DAY. FOUND LEAK AT COUPLING ON LINE FROM IDG TO COOLER. TIGHTENED COUPLING, SERVICED IDG, LEAK CHECKS GOOD. DISCONNECTED IDG C/0269806. LEAKING COUPLING IS ROOT CAUSE.

Part: HYDRAULIC LINE — CHAFED · airframe 13,680 hrs · 7,303 cycles

PDIS 671 29-11 0007374 22FEB06 OAK OPEN R LOGPAGES: 01086620 ECAM ALERT AT FL320 GREEN HYD SYS QNT LOW ALERT. MANUAL GEAR EXTENSION ACCOMPLISHED. FLUID DRIPPING FROM NR1 ENG RESEARCHING. FOUND 2 HYDR LINES LEAKING THAT HAD BEEN CHAFED THROUGH AT A CLAMP IN THE PYLON REF IPC 29-11-06-01 FIGURE 01 SHEET 1 IN BETWEEN ITEMS 390 AND 380. ORDERING THE LINES AOG. PART 23FEB06 00:45 OAK R ADDED MPN A2911503000400 ADDED MPN A2911503500000 LINES AND MISC HARDWARE WILL BE REPLACED.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 13,336 hrs · 7,117 cycles

RT WINDSHIELD CRACKED. REMOVED AND REPLACED RT WINDSHIELD PANEL PER A300 AMM 56-11-11-4. NEEDS SEALANT CURE CHECK, WINDSHIELD WIPER INSTALLED AND OPS CHECK.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 13,336 hrs · 7,117 cycles

RT WINDSHIELD CRACKED. CREW NOTICED A SMALL CRACK DURING CLIMB, DID NOT HEAR OR FEEL ANYTHING HIT WINDOW. NOTICED WINDOW ARCHING, WINDOW HEAT WAS TURNED OFF, THEN THE WINDSHIELD SPIDER WEBBED. REMOVED AND REPLACED RT WINDSHIELD PANEL PER A300 AMM 56-11-11-4, NEEDS SEALANT CURE CHECK, WINDSHIELD WIPER INSTALLED AND OPS CHECK. REINSTALLED RT WINDSHIELD WIPER ARM. REMOVED AND REPLACED RT WINDSHIELD TEMP REGULATOR REF.

Part: SKIN — DENTED (FLAP) · airframe 12,695 hrs · 6,847 cycles

LT I/B T/E FLAP, LWR SURFACE SKIN DENTED/GOUGED BEHIND NR 2 LT FLAP JACK SCREW. MEASURED DEPTH OF DENT AT .162 OUT OF LIMITS IAW SRM 57-50-00 FIG 101. INSTALLED REPAIR IAW SRM 57-52-12. REVIEW OF REPAIR REVEALS IT AS UNSAT DUE TO UNAPPLICABLE SRM SCHEME. SEE NR N00768 FOR REWORK. REPAIR AFFECTED ON NR N00759 FOUND UNSAT. SRM REQUIRES AREA BE BOUNDED BY RIBS AND STRINGERS. IT IS NOT. REPAIR REFERENCE IS N/A. COMPLIED WITH EA 6-5750- 82120 WING INBD FLAP LOWER SKIN REPAIR ON S00013. COMPLY WITH EA 6-5750-82120 WING-INBD FLAP-LOWER SKIN REPAIR. COMPLIED WITH EA 6-5750-82120 WING-FLAP-LOWER SKIN REPAIR.

Part: FAIRING — DELAMINATED (NR 1 PYLON) · airframe 12,695 hrs · 6,847 cycles

NR 1 PYLON AFT FAIRING 473EL DELAMINATED.

Part: SUPPORT BRACKET — CRACKED (NR 1 PYLON) · airframe 12,695 hrs · 6,847 cycles

NR 1 ENG HYDRAULIC CASE DRAIN LINES SUPPORT BRACKET CRACKED ACCESS THRU 473CL PNL.

Part: FLOOR PANEL — CRACKED (MCD) · airframe 12,695 hrs · 6,847 cycles

MAIN CARGO COMPT FLOOR PNL 262ZF IS CRACKED AT ATTACH POINT.

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 12,695 hrs · 6,847 cycles

MDC FLOOR PNL 231FF DAMAGED.

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 12,695 hrs · 6,847 cycles

MDC FLOOR PNL 232TG DAMAGED.

Part: BEARING — DAMAGED (CARGO FLOOR PNL) · airframe 12,695 hrs · 6,847 cycles

MCD FLOOR PNL 232FG HAS BALL BEARING DAMAGE.

Part: FLOOR PANEL — CRACKED (MAIN DECK CARGO) · airframe 12,695 hrs · 6,847 cycles

MAIN CARGO COMPT FLOOR PANEL 242EK IS CRACKED AT SEAT TRACK ATTACH POINT.

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 12,695 hrs · 6,847 cycles

MDC FLOOR PNL 231FG DAMAGE.

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 12,695 hrs · 6,847 cycles

MDC FLOOR PNL 251YG HAS SEVERAL PUNCTURES ON LWR SURFACE AND 1 ON UPPER SURFACE.

Part: FLOOR PANEL — DAMAGED (MDC) · airframe 12,695 hrs · 6,847 cycles

MDC FLOOR PNL 232FF IS DAMAGED.

airframe 12,695 hrs · 6,847 cycles

NR 1 ENG FAN CASE HAS 2 PREVIOUSLY STOP DRILLED CRACK ON AFT DOLLY MOUNT AT APPROX 8 O'CLOCK POSITION. FPI IAW NTM 51-91-00 CRACK CONTAINED BY STOP DRILL. SWAB ETCHED DAMAGED AREA IAW TASK 70-24-01-110-34 OF SPM. STOP DRILLS ACCEPTABLE PER EA 6-7223-82106-NRS00008 AND PER AMM 72-23-00-8-F REMOVED AND REPLACED HANDLING HOIST BRACKETS IAW MM 72-23-01.

Part: POWERPLANT — CRACKED (FLANGE) · airframe 12,695 hrs · 6,847 cycles

W/O 29493, NR N00177, ENGINE NR 1 AT FORWARD INBOARD LOWER HOIST POINT, THE FLANGE IS CRACKED AT IT'S BASE. FPI IAWM NTM 51-91-00 CRACK IS CONTAINED BY STOP DRILL. SWAB ETCHED DAMAGED AREA IAW TASK 70-24-01-110-34 PER GESPM STOP DRILL ACCEPTABLE PER EA 6-7223-82106 AND PER AMM 72-23-00-8-F REMOVED AND REPLACED HOIST BRKTS IAW GE MM 72-23-01

airframe 12,695 hrs · 6,847 cycles

NR 1 ENG FAN CASE HAS 2 PREVIOUSLY STOP DRILLED CRACKS ON FWD DOLLY MOUNTS AT APPROX 8 O'CLOCK. FPI IAW NTM 51-91-00 CRACK IS CONTAINED BY STOP DRILL. SWAB ETCHED DAMAGED AREA IAW TASK 70-24-01-110-34 SPM. STOP DRILL ACCEPTABLE PER EA 6-7223-82106 AND PER AMM 72-23-00-8-F. REMOVED AND REPLACED HOIST BRACKETS IAW GE MM 72-23-01.

Part: WEB — CRACKED (MAIN DECK CARGO) · airframe 12,695 hrs · 6,847 cycles

AFT MAIN DECK REAR CARGO COMPT FR 79 WITH STR 26 WEB IS CRACKED.

Part: WEB — CRACKED (MAIN DECK CARGO) · airframe 12,695 hrs · 6,847 cycles

AFT MAIN DECK REAR CARGO COMPT FR 79 WITH STR 26 WEB IS CRACKED.

Part: SKIN — DAMAGED (TE FLAP) · airframe 12,695 hrs · 6,847 cycles

LEFT WING I/B FLAP BOTTOM SKIN HAS CREASE AT MID SECTION REPAIRED DAMAGED SECTION OF LEFT I/B TRAILING EDGE FLAP LOWER SURFACE SKIN AND 2 EA STRINGERS IAW SRM 57-50-00 FIG 206. PREPPED AND PAINTED IAW MM 51-75-10-8.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 12,695 hrs · 6,847 cycles

MAIN DECK CARGO SEAT TRACK AT FRAME 41 TO 44 BL0 HAS CORROSION ALONG LENGTH NOTED. REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK ON TRAVELER NR T5/534305 IAW SRM 53-15-16. LOCATED AND DRILLED IAW SRM 53-10-16. TREATED AND PRIMED IAW SRM 51-21-10. INSTALLED NEW SEAT TRACK IAW SRM 53-10-16. PAINTED SEAT TRACK IAW SRM 51-23-10.

Part: FITTING — CRACKED (SEAT TRACK) · airframe 12,695 hrs · 6,847 cycles

UPON REMOVAL OF SEAT TRACK AT RBL40 FITTING AT I/B SIDE OF WEB FOUND CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-40-21 AND PAINTED IAW SRM 51-23-10 FITTING LOCATED AT RBL 40, FRAME 40.

Part: FRAME — GOUGED (FUSELAGE) · airframe 12,695 hrs · 6,847 cycles

COMPLY WITH EA 6-5310-82108, FUSELAGE MAIN FRAME, FRAME 28, GOUGE REPAIR STR 18L THROUGH STR 22L. COMPLIED WITH EA 6-5310-82108 FUSELAGE, MAIN FRAME, FRAME 28, GOUGE REPAIR STR 18L THROUGH STR 22L.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 12,695 hrs · 6,847 cycles

MAIN DECK CARGO SEAT TRACK AT FRAME 41 TO 45 RBL 40 HAS CORROSION ALONG LENGTH NOTED. REMOVED CORRODED SEAT TRACK SECTION IAW SRM 53-10-16. FABRICATED NEW SEAT TRACK SECTION ON TRAVELER T5/534306. LOCATED AND DRILLED SECTION IAW SRM 53-10-16 AND 51-40-44. TREATED AND PRIMED IAW SRM 51-21-10. INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-16. PREP AND PAINT IAW AMM 51-75-10-8.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 12,695 hrs · 6,847 cycles

LT WING I/B T/E FLAP LWR SKIN MID O/B SECTION HAS CREASE. FOUND CREASE TO BE OUT OF LIMITS IAW SRM 57-50-00 FIG 101. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS ON MAE TRAVELER T5/532877 LOCATED, DRILLED, AND INSTALLED IAW SRM 57-50-00 FIG 206. TREATED/PRIMED IAW SRM 51-21-10. PREPPED AND PAINTED IAW MM 51-75-10-8.

Part: FITTING — CORRODED (NR 1 PYLON) · airframe 12,695 hrs · 6,847 cycles

FOUND THE NR 1 ENG PYLON, INBD MOUNT OUTBD SHACKLE HAS PITTING CORROSION IN THE FACE SIDE OF THE SHACKLE.

Part: FITTING — CORRODED (NR 1 PYLON) · airframe 12,695 hrs · 6,847 cycles

NR 1 PYLON TO WING ATTACHMENT FITTING SHACKLE OUTBD/INBD LOWER BUSHING HAS CORROSION CHROME PLATING WORN.

Part: SLEEVE — CORRODED (NR 1 PYLON) · airframe 12,695 hrs · 6,847 cycles

NR 1 PYLON TO WING ATTACH FITTING SLEEVE (OUTBD LUG/LWR) HAS GOUGED MARK AND HAS CORROSION ON THE HEAD END INNER COLLAR.

Part: FITTING — CORRODED (NR 1 PYLON) · airframe 12,695 hrs · 6,847 cycles

NR 1 PYLON TO WING ATTACHMENT FITTING SHACKLE OUTBD/INBD LOWER BUSHING HAS CORROSION CHROME PLATING WORN.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,695 hrs · 6,847 cycles

MDCC SEAT TRACK FROM FRAME 54.2-54.3, BL-0 HAS 2 PLACES OF CORROSION REMOVED CORROSION IAW SRM 53-10-16 FOUND SEAT TRACK TO BE OUT OF LIMITS. FABRICATED SEAT TRACK ON TRAVELER NR T5/532242 IAW SRM 53-10-16 TREATED AND PRIMED IAW SRM 51-21-10. FABRICATED SEAT TRACK SPLICES ON TRAVELER T5/532244 IAW SRM 53-10-16. TREATED AND PRIMED SPLICES IAW SRM 51-21-10. REMOVED AND REPLACED SEAT TRACK SPLICES IAW SRM 53-10-16, TOUCHED UP PAINT IAW SRM 51-23-10.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 12,695 hrs · 6,847 cycles

W/O 29493, NR# N00484, BULK CARGO PIT FLOOR PNL 161GF DENTED AND DELAMINATED NEW FLOOR PANEL FABRICATED ON T5/530783 IAW SRZ-25-005

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 12,695 hrs · 6,847 cycles

MCD FLR PNL NR 262AH CRACKED. FABRICATED FLOOR PANEL ON TRAVELER NR T5/531328 IAW SRZ-25-005.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 12,695 hrs · 6,847 cycles

FLOOR PANEL 231VG PUNCTURED AND CRACKED. FABRICATED FLOOR PANEL ON TRAVELER NR T5/531063 IAW SRZ-25-005.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 12,695 hrs · 6,847 cycles

MCD FLOOR PANEL 232NG PUNCTURED AND CRACKED. FABRICATED NEW FLOOR PANEL ON TRAVELER T5/531061 IAW SRZ -25-005.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 12,695 hrs · 6,847 cycles

FWD CGO PIT FLOOR PNL 131MG DELAMINATED AND HAS EDGE DAMAGE. FLOOR PANEL FABRICATED ON TRAVELER T5/530781 IAW SRZ -25-005

Part: FLOOR PANEL — BROKEN (FUSELAGE) · airframe 12,695 hrs · 6,847 cycles

MAIN CARGO COMPT FLOOR PANEL 251WG IS BROKEN AT FWD INBD CUTOUT. REPLACED FLR PNL ON TRAVELER NR T5/530573 REF SRZ-25-005.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 12,695 hrs · 6,847 cycles

MCD FLOOR PANEL 231CF PUNCTURED AND CRACKED. REPLACED FLR PNL ON TRAVELER NR T5/3001556 REF SRZ-25-005.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 12,695 hrs · 6,847 cycles

SEAT TRACK BL 0 FROM FRAME STA 45 TO 53 CORRODED IN SEVERAL AREAS. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED DRILLED AND DEBURRED HOLES IN SEAT TRACK REPLACEMENT AND SPLICE SET. TREATED AND PRIMED ALL PARTS IAW SRM 51-23-10. INSTALLED NEW SEAT TRACK SECTON AND SPLICE SET IAW SRM 53-10-16.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 12,695 hrs · 6,847 cycles

DURING OK TO INSTALLED FOUND PANEL 162EF DELAMINATED. REPLACED FLR PNL ON TRAVELER NR T5/534022 REF SRZ-25-005.

Part: FLOOR PANEL — BROKEN (FUSELAGE) · airframe 12,695 hrs · 6,847 cycles

MCD FLOOR PANEL 242DF IS BROKE AFT END OF BOARD. REPLACED FLR PNL ON TRAVELER NR T5/530576 REF SRZ-25-005.

Part: FLOOR SUPPORT — BROKEN (ZONE 200) · airframe 12,695 hrs · 6,847 cycles

MAIN CARGO DECK BETWEEN FS 13 TO FS 13B RBL 26 FLOOR SUPPORT DAMAGED (BROKEN). REMOVED DAMAGED FLOOR SUPPORT IAW SRM 51-40-20. RECEIVED NEW SUPPORT FROM FAB SHOP AND TRAVELER NR T5/534444 REF SRM 51-26-10 SRM 53-12-15 FIG 19 LOCATED AND DRILLED SUPPORT (NEW) IAW SRM 51-40-44. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40- 20. TOUCHED UP PAINT COATING ON SUPPORT AND FASTENERS IAW SRM 51-23-10.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 12,695 hrs · 6,847 cycles

MAIN CARGO DECK FLOOR PANEL 241PF IS CRACKED IN MIDDLE SECTION OF BOARD. REPLACED FLR PNL ON TRAVELER NR T5/530577 REF SRZ-25-005.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 12,695 hrs · 6,847 cycles

MAIN CARGO FLOOR PANEL 241KJ IS CRACKED AT SEAT TRACK ATTACH POINT. REPLACED FLR PNL ON TRAVELER NR T5/530789 REF SRZ-25-005.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 12,695 hrs · 6,847 cycles

MAIN CARGO FLOOR PANEL 251AH IS CRACKED AT TRACK MAIN ATTACH POINT. REPLACED FLR PNL ON TRAVELER NR T5/530786 REF SRZ-25-005.

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 12,695 hrs · 6,847 cycles

MDC FLOOR PANEL 231EF PUNCTURED AND CRACKED. REPLACED FLR PNL ON TRAVELER NR T5/531062.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 12,695 hrs · 6,847 cycles

MAIN CARGO DECK SUPPORT BETWEEN F38.1 AND F38.2 AT STR 26 RT IS CRACKED. REMOVED DAMAGED SUPPORT, FABBED AND RECEIVED NEW PART ON TRAVELER NR T5/534370 (REF SRM 53-14-15/SRM 51-26-10) AND INSTALLED NEW SUPPORT IAW SRM 51-40-21.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 12,695 hrs · 6,847 cycles

MAIN DECK CARGO SEAT TRACK AT FRAME 41 TO 44 RBL 20, HAS CORROSION ALONG LENGTH NOTED. REMOVED SEAT TRACK, LOCATED AND DRILLED IAW SRM 53-10-16. INSTALLED NEW SEAT TRACK IAW SRM 53-10-16.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 12,695 hrs · 6,847 cycles

MAIN CARGO DECK UNDERNEATH LAVATORY FS 12 TO 13C LBL20 FLOORBEAM HAS CORROSION. REMOVED FLOORBEAM UPPER TEE IAW SRM 51-40-20. FABRICATED NEW PART ON TRAVELER T5/534141 REF SRM 53-12-15 FIG 19 BATCH NR 000823785, DRILL AND LOCATED IAW SRM 51-40-44. INSTALLED NEW PART IAW SRM 51-40-20, PAINTED AREA IAW SRM 51-23-10.

Part: SKIN — CRACKED (ZONE 500) · airframe 12,695 hrs · 6,847 cycles

LT WING FIXED TE UPPER SKIN CRACKED/CUT LOC 5 IN FROM INBD END 2.5 IN FROM AFT END.

Part: STRIP — GOUGED (THURST REVERSER) · airframe 9,285 hrs · 4,943 cycles

NR 265 #2 ENG I/B T/R LOWER FRAME GOUGED. REMOVED AND REPLACED I/B T/R LOWER FRAME IAW S/B 78-1109 @ MAE UNDER WO 22920. ** S/D

Part: DOOR FRAME — DAMAGED (CARGO BAY) · airframe 9,285 hrs · 4,943 cycles

COMPLY WITH E.A. 6-5313-70393 "FUSELAGE-MAIN FRAME-LWR FWD CARGO DOOR FRAME/FUSELAGE SKIN REPAIR AT FRAME 20A FACT 27MAY03 11:35 BFM U COMPLIED WITH E.A. 6-5313-70393 FUSELAGE-MAIN FRAME- LWR FWDCARGO DOOR FRAME/FUSELAGE SKIN REPAIR AT FR20A.

Part: SPAR — DAMAGED (PYLON) · airframe 9,285 hrs · 4,943 cycles

COMPLY WITH E.A.6-5455-70907 PYLON- REPAIR OF FWD FAIRING UPPER SPAR ANGLE 9333M29P112A. FACT 27MAY03 11:32 BFM U WORK COMPLIED WITH IAW/E.A. 6-5455-70907, PYLON-REPAIR OF FWD FAIRING UPPER SPAR ANGLE 9333M29P112A.IAW/51-70-40-FIG 201.

Part: BLOWOUT DOOR — WORN (NR 2 ENGINE T/R) · airframe 9,285 hrs · 4,943 cycles

COMPLY WITH E.A. 6-7830-70395 EXHAUST-THRUST REVERSER-BLOWOUT DOOR EDGE WEAR REPAIR (P/N 491B1220000-029) FACT 23MAY03 03:28 BFM R COMPLIED IAW/E.A. 6-7830-70395 -EXHAUST-THRUST REVERSER-BLOWOUT DOOR EDGE WEAR REPAIR (P/N 491B1220000-029.

Part: BLOWOUT DOOR — WORN (NR 2 ENGINE T/R) · airframe 9,285 hrs · 4,943 cycles

COMPLY WITH E.A. 6-7830-70395 EXHAUST-THRUST REVERSER-BLOWOUT DOOR EDGE WEAR REPAIR (P/N 491B1220000-029) FACT 23MAY03 03:28 BFM R COMPLIED IAW/E.A. 6-7830-70395 -EXHAUST-THRUST REVERSER-BLOWOUT DOOR EDGE WEAR REPAIR (P/N 491B1220000-029.

Part: B-NUT — LOOSE (PITOT/STATIC SYS) · airframe 7,707 hrs · 4,021 cycles

DURING TAKEOFF CAPT A/S INDICATOR READ 40 KIAS AT 110 KIAS. SECURED LOOSE B-NUT PER SMP & REMOVED AND REPLACED NR 1 ADC PER MM 34-11-34-4.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 6,229 hrs · 3,158 cycles

DURING CLIMBOUT NR 1 ENG HAD 2 COMPRESSOR STALLS WITH FLAMES REPORTED BY TOWER DURING 2ND ONE.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 4,668 hrs · 2,332 cycles

ON T/O CLIMBOUT, RT INNER DECREASED AT ABNORMAL RATE BEYOND MAX LIMIT IMBALANCE.

Part: IRU — FAILED (NR 2)

00-86 - ABORTED T/O AT 70 KNOTS DUE TO NR 2 IRU FAILURE. A/C RELEASE FOR SERVICE UNDER PROV OF MEL 34-10A . SWAPPED NR 2 AND NR 3 INERTIAL REF UNITS PER MEL PROC MXP 22-1 AC CAT 2 STATUS. REMOVED AND REPLACED NR 3 IRU IAW AMM 34-25-34-4 AND OPS CK PER 34-25-00-5. ALL CK NORMAL.