N408UA

Part: COMPUTER — FAULTED (FLAP/SLAT SYS) · airframe 88,752 hrs · 34,582 cycles

THE TOMC CONTROLLER AND SENIOR MANAGER CONCUR THAT THE AIRCRAFT CAN BE RELEASED BACK TO SERVICE AFTER EXPERIENCING A DIVERSION O R AIR TURN BACK DUE TO A MECHANICAL REASON LOCKED BY SYSTEM. TOMC CONCURRED WITH SHIFT MANAGER WITH CORRECTIVE ACTION WITH REPLACEMENT OF BOTH SFCCS. UPON ARRIVAL, NO FLAP SYST 1 FAULT. CREW COULD NOT ENGAGE FLIGHT DIRECTORS 1 OR 2, RED "SPD LIMIT" FAULTS ON BOTH CAPT & F/O''SEADI. POST FLIGHT REPORT FAULTED SFCC 1, AFS TEST FAULTED SAME. RESET SFCC 1 & FCDC 1= FAULTS CLEARED. AFS & SFCC 1 TEST PASSED,SWAPPED SFCC TO #2 POSITION, NO FAULT,OPA TEST GOOD. DUE TO GATE RETURN, REPLACED SFCC 1 I.A.W. AMM 27-51-34, OPS TEST NORMAL.T/S PER TSM 27-51-00-810-845-A.

Part: RESERVOIR — INOPERATIVE (GREEN HYD SYS) · airframe 85,150 hrs · 32,848 cycles

ECAM CAUTION MESSAGE - G RSVR LO LVL MESSAGE INOP - HYD LOST G HYD SYTM 25 MININ FLT FOUND HYDRAULIC LINE LEAKING ON #1 ENGINE THRUST REVERSER HYDRAULIC CONTROL UNIT. REMOVED HYDRAULIC LINE PN D2901005300000 REF IPC 29-11-06-02C ITEM 120A. INSTALLED HYDRAULIC LINE IN #1 PYLON REF AMM 29-11-06 LEAK CHECKS GOOD AT THIS TIME

Part: PROFILE — CRACKED (LT OVERWING EXIT) · airframe 84,159 hrs · 32,395 cycles

(A3NB-52-4-6031) POSSIBLE CRACKS ON LT AFT OVERWING EXIT DOOR IN AREA OF RH TRANSMITTING PROFILE (MARKED). REF BY PEMCO NR.10449.0511. REMOVED AND REPLACED 1EA FRAME SEGMENT IAW A320 SRM 51-72-11-91 -001 SHT. 1-3, COMPLETED BY V910555, CO-SIGNED BY P181, INSP BY Q957, ENTERED BY V928371. V REMOVED AND REPLACED 1EA FRAME SEGMENT IAW A320 SRM 51-72-11-9 -001 SHT. 1-3, COMPLETED BY V910555, CO-SIGNED BY P181, INSP B Q957, ENTERED BY V928371.

Part: PROFILE — CRACKED (RT OVERWING EXIT) · airframe 84,159 hrs · 32,395 cycles

(A3NB-52-4-6031) POSSIBLE CRACKS ON RT AFT OVERWING EXIT DOOR IN AREA OF LOAD TRANSMITTING PROFILE (MARKED). REF BY PEMCO NR. 10449.0514. REMOVED AND REPLACED 1EA FRAME SEGMENT IAW A320 SRM 51-72-11-91 -001 SHT. 1-3, COMPLETED BY V916555, CO-SIGNED BY P181, INSP BY Q957, ENTERED BY V928371. REMOVED AND REPLACED 1EA FRAME SEGMENT IAW A320 SRM 51-72-11-91 -001 SHT. 1-3, COMPLETED BY V916555, CO-SIGNED BY P181, INSP BY Q957, ENTERED BY V928371.

Part: PROFILE — CRACKED (LT OVERWING EXIT) · airframe 84,159 hrs · 32,395 cycles

(A3NB-52-4-6031) POSSIBLE CRACKS ON LT AFT OVERWING EXIT DOOR IN AREA OF LH TRANSMITTING PROFILE (MARKED). REF BY PEMCO NR. 10449.0510. REMOVED AND REPLACED 1EA FRAME SEGMENT IAW A320 SRM 51-72-11-911 -001 SHT. 1-3, COMPLETED BY V910555, CO-SIGNED BY P181, INSP BY Q957, ENTERED BY V928371. REMOVED AND REPLACED 1EA FRAME SEGMENT IAW A320 SRM 51-72-11-911 -001 SHT. 1-3, COMPLETED BY V910555, CO-SIGNED BY P181, INSP BY Q957, ENTERED BY V928371.

Part: PROFILE — CRACKED (RT OVERWING EXIT) · airframe 84,159 hrs · 32,395 cycles

(A3NB-52-4-6031) POSSIBLE CRACK ON RT FWD OVERWING EXIT DOOR IN AREA OF RH LOAD TRANSMITTINF PROFILE (MARKED). REF BY PEMCO NR.10449.0516. REMOVED AND REPLACED 1EA FRAME SEGMENT IAW A320 SRM 51-72-11-91 -001 SHT. 1-3, COMPLETED BY V916555, CO-SIGNED BY P181, INSP BY Q957, ENTERED BY V928371. REMOVED AND REPLACED 1EA FRAME SEGMENT IAW A320 SRM 51-72-11-91 -001 SHT. 1-3, COMPLETED BY V916555, CO-SIGNED BY P181, INSP BY Q957, ENTERED BY V928371.

Part: PROFILE — CRACKED (LT OVERWING EXIT) · airframe 84,159 hrs · 32,395 cycles

(A3NB-52-4-6031) POSSIBLE CRACKS ON LT FWD OVERWING EXIT DOOR IN AREA OF LH LOAD TRANSMITTING PROFILE (MARKED). REF BY PEMCO NR.10449.0518 REMOVED AND REPLACED 1 EA. FRAME SEGMENT IAW A320 SRM 51-72-11-9 11-001 SH1-3. COMPLETED BY V916555 CO-SIGN P181. INSP BY Q957, ENTERED BY V928371. REMOVED AND REPLACED 1 EA. FRAME SEGMENT IAW A320 SRM 51-72-11-9 11-001 SH1-3. COMPLETED BY V916555 CO-SIGN P181. INSP BY Q957, ENTERED BY V928371.

Part: FRAME ANGLE — CRACKED (ZONE 800) · airframe 84,158 hrs · 32,395 cycles

PEMCO NR 10449.0516 DISCREPANCY. POSSIBLE CRACK ON RT FWD OVER WING EXIT DOOR IN AREA OF RH LOAD TRANSMITTING PROFILE. CORRECTIVE ACTION R & R FRAME SEGMENT IAW A320 SRM 51-72-11-911 SH 1-3.

Part: FRAME ANGLE — CRACKED (ZONE 800) · airframe 84,158 hrs · 32,395 cycles

PEMCO NR 10449.0510 DISCREPANCY. POSSIBLE CRACKS ON LT AFT OVER WING EXIT DOOR IN AREA OF LH TRANSMITTING PROFILE. CORRECTIVE ACTION R & R FRAME SEGMENT IAW A320 SRM 51-72-11-911-001 SH 1-3.

Part: FRAME ANGLE — CRACKED (ZONE 800) · airframe 84,158 hrs · 32,395 cycles

PEMCO NR 10449.0510 DISCREPANCY. POSSIBLE CRACKS ON RT AFT OVER WING EXIT DOOR IN AREA OF LH TRANSMITTING PROFILE. CORRECTIVE ACTION R & R FRAME SEGMENT IAW A320 SRM 51-72-11-911-001 SH 1-3.

Part: FRAME ANGLE — CRACKED (ZONE 800) · airframe 84,158 hrs · 32,395 cycles

PEMCO NR 10449.0510 DISCREPANCY. POSSIBLE CRACKS ON LT AFT OVER WING EXIT DOOR IN AREA OF RH TRANSMITTING PROFILE. CORRECTIVE ACTION R & R FRAME SEGMENT IAW A320 SRM 51-72-11-911-001 SH 1-3.

Part: PROFILE — CRACKED (DOOR FRAME) · airframe 84,158 hrs · 32,395 cycles

PEMCO N/R 10449.0518 DISCREPANCY: POSSIBLE CRACKS ON LT FWD OVER-WING EXIT DOOR IN AREA OF LT LOAD TRANSMITTING PROFILE. CORRECTIVE ACTION: REMOVED AND REPLACED FRAME SEGMENT, IAW A320 SRM 51-72-11-911-001 SH 1-3.

Part: ENGINE — MAKING METAL (NR 1) · airframe 82,079 hrs · 31,480 cycles

STALL DISPLAYED ON UPPER ECAM SCREEN DURING STEADY STATE CLIMB OR CRUISE. ENGINE NOT SHUTDOWN - ENG 1. ENG 1 MOMENTARY STALL AT CRUISE FL330. SELF RECOVERED NORMAL THRUST. REF LOG PAGE 3743159. METAL FOUND IN ENG 1, 7TH STAGE BLEED VALVE. PROCEEDING TO CHANGE #1 ENG. LP 3743159- WHILE ACCOMPLISHING TSM 75-30-00-810-827-B13 FOR ENG 1 STALL, IPCV ( CHECK VALVE) CONDITION IS GOOD. VSV MECHANISM CONDITION IS GOOD AND MOVEMENT IS GOOD. UPON FUNCTIONAL CHECK OF 7 STAGE BLEED VALVES, FOUND METAL IN 7TH STAGE BLEED VALVE. PROCEEDING WITH ENG CHANGE. REMOVED ENG SN#V11071 AND INSTALLED ENG SN#V10487. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1142925 SN OFF 1071 ENGINE, V2500-A OFF 31-7200-9-0001 1071 ON 31-7200-9-0001 0487 INSPECTED REMOVAL # 1 ENGINE SN V11071 AND INSTALLATION SN V10487 PER GMM 09-25 05.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 82,068 hrs · 31,476 cycles

STALL DISPLAYED ON UPPER ECAM SCREEN DURING STEADY S TATE CLIMB OR CRUISE. ENGINE NOT SHUTDOWN. - ENG 1 ENG STALLED SECOND TIME OPERATED DEGRADED TOLANDING WHILE ACCOMPLISHING TSM 75-30-00-810-827-B13 FOR ENG 1 STALL. IPCV ( CHECK VALVE) CONDITION IS GOOD. VSV MECHANISM CONDITION IS GOOD AND MOVEMENT IS GOOD. UPON FUNCTIONAL CHECK OF 7 STAGE BLEED VALVES, FOUND METAL IN 7TH STAGE BLEED VALVE. PROCEEDING WITH ENG CHANGE. REMOVED ENG SN#V11071 AND ISTALLED ENG SN#V10487 REF MT71-017 SE E MT71-017 THIS DATE FOR APLICABLE SIGN OFFS. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1142925 SN OFF 1071 ENGINE, V2500-A OFF 31-7200-9-0001 1071 ON 31-7200-9-0001 0487 INSPECTED REMOVAL # 1 ENGINE SN V11071 AND INSTALLATION SN V10487 PER GMM 09-25 05.

Part: BATTERY — FAILED (CABIN) · airframe 76,693 hrs · 29,106 cycles

LT FWD AND RT MID CABIN EPSU FAILED CAPACITY CHECK. REMOVED AND REPLACED LT FWD AND RT MID CABIN EPSU BATTERIES IAW AMM 33-51-38. PERFORMED EMERGENCY LIGHT CAPACITY CHECK AFTER BATTERY REPLACEMENT. OPS CHECK GOOD.

Part: INDICATION SYS — FAULTY (R2 DOOR) · airframe 74,319 hrs · 28,038 cycles

DOOR 2R SLIDE INDICATION WENT OUT IN FLIGHT. MECHANICAL INDICATORS ON DOOR SHOW ARMED PERFORMED OPERATIONAL CHECK OF DOOR 2R PER AMM 52-71-00-710-01-A . COULD NOT DUPLICATE PROBLEM. R&R PROX SENSOR 7WN2 PER AMM 52- 73-11 AS PRECAUTIONARY. SYSTEM OPS CHECK NORMAL.

Part: COVER — LOOSE (EMERGENCY EXIT) · airframe 74,287 hrs · 28,028 cycles

L FWD EMERG COVER FELL OFF AGAIN. REMOVED LT EMERGENCY EXIT HATCH COVER FLAP IAW AMM 52 -21-11-000-001-A. REINSTALLED LT EMERGENCY EXIT HATCH COVER FLAP IAW AMM PERFORMED PULL TEST IN LT EMERGENCY EXIT HATCH COVER FLAP IAW AMM 52-21-11-400-001-A PULL TEST GOOD

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,271 hrs · 28,020 cycles

REMOVED CRACKED CROSSBEAM CONNECTING FITTING. REMOVED CRACKED CROSS BEAM CONNECTING FITTING IAW SRM 51-72 -11. REPLACED FR68 CROSSBEAM CONNECTING FITTING WITH NEW PART IAW SRM 51-72-11.

Part: PLATE — CORRODED (FUSELAGE) · airframe 74,271 hrs · 28,020 cycles

CORROSION AT LAV E XHAUST VENT OUTLET CUTOUT. REMOVED CORRODED LAV EXHAUST VENT OUTTER REINFORCEMENT PLATE IAW SRM 51-72-11. INSTALLED NEW LAV EXHAUST VENT OUTLET REINFOR CEMENT PLATE IAW SRM 51-72-11.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 74,271 hrs · 28,020 cycles

AFT CARGO DOOR INBD SILL CORRODED, FRAMES 53 - 56. REMOVED AND REPLACED THE CARGO DOOR SILL IAW SRM 51-42-11, PG 9, & SRM 51-72-11.

Part: SWITCH — BROKEN (EMERGENCY LIGHTS) · airframe 74,271 hrs · 28,020 cycles

FT ATTENDANTS PANEL EMERGENCY LIGHT SWITCH IS BROKEN . REMOVED AND REPLACED THE PANEL IAW AMM 23-73-13-000- 001-A, AND AMM 23-73-13-400-001-A, OP TESTED GOOD IAW AMM 23 -73-00-740-005-A.

Part: FRAME — CORRODED (FRAME 58) · airframe 74,271 hrs · 28,020 cycles

AFT CARGO BAY AT FRAME 58 BETWEEN STRINGERS 42 - 43L HAS CORROSION. REPAIRED IAW SRM 51-72-11, PARA 5.A.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 74,271 hrs · 28,020 cycles

R2 DOOR SILL CORRODED. REMOVED R2 DOOR SILL FOUND TO BE OUT OF LIMITS IAW SRM 53-41 -14 FIG 101. RECEIVED NEW R2 DOOR SILL AND INSTALLED IAW SRM 51-72-11 PARA 5-A.

Part: DOOR FRAME — CORRODED (FRAMES 66-68) · airframe 74,271 hrs · 28,020 cycles

L2 DOOR SILL CORRODED AT FRAMES 66-68. REMOVED THE DOOR SILL FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14, FIG 101. INSTALLED IAW SRM 51-72-11 PARA 5.A

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,271 hrs · 28,020 cycles

AFT CARGO PIT HAS CORROSION ON STRINGER 39RT BETWEEN FR59-60. REPLACED STRINGER SECTION 39RT BETWEEN FR59-60 IN THE AFT CARGO IAW SRM 53-00-13 FIG 201.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,271 hrs · 28,020 cycles

AFT CARGO PIT BETWEEN FR63-64 STRINGER 40RT HAS CORROSION. REPLACED STRINGER SECTION 40RT BETWEEN FR63-64 IN THE AFT CARGO IAW SRM 53-00-13 FIG 201.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,271 hrs · 28,020 cycles

AFT PIT STRINGER 41RT BETWEEN FR58-59 HAS CORROSION. REPLACED STRINGER SECTION 41RT BETWEEN FR58-59 IN THE AFT CARGO IAW SRM 53-00-13 FIG 201.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,271 hrs · 28,020 cycles

AFT CARGO PIT BETWEEN FR63-64 STRINGER 39RT HAS CORROSION. REPLACED STRINGER SECTION 39RT BETWEEN FR63-64 IN THE AFT CARGO IAW SRM 53-00-13 FIG 201.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,271 hrs · 28,020 cycles

AFT CARGO PIT STRINGER 43LT BETWEEN FR56-59 HAS CORROSION. REMOVED AND REPLACED STR43LT FR54-60 IAW SRM 51-42-11.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,271 hrs · 28,020 cycles

AFT CARGO PIT STR 42LT BETWEEN FR56-FR59 HAS CORROSION. REMOVED AND REPLACED STRINGER 42LT FR53-60 IAW SRM 51-42-11.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,271 hrs · 28,020 cycles

AFT CARGO PIT STRINGER 31RT AT FR65 HAS EXFOLIATED CORROSION. REMOVED AND REPLACED STRINGER 31RT AT FRAMES 64-67 IAW SRM 51-42-11

Part: BRACKET — DAMAGED (FUSELAGE) · airframe 74,271 hrs · 28,020 cycles

UPON REMOVAL OF CLIP AT FR65 BETWEEN STR 31-32 FOUND TWO EACH OUT OF ROUND HOLES REMOVED & REPLACED CLIP ON AFT CARGO FR65 STR 31-32R IAW SRM 51-42-11 P 25 PARA 7.

Part: ANGLE — CORRODED (FRAME 27) · airframe 74,271 hrs · 28,020 cycles

C2 FWD CARGO BAY FRAME 27, STRINGER 39L CORROSION SEAL ANGLE. REMOVED AND REPLACED CORRODED SEAL ANGLE IAW SRM 51-42-11.

Part: LANDING — DAMAGED (RT WING) · airframe 69,465 hrs · 25,881 cycles

RIGHT WING FUEL TANK ACCESS LANDING FOR ACCESS PANEL 640RB HOLE C BETWEEN RIB 21 - 22 HAS AN ELONGATED HOLE. CLEANED & REPAIRED HOLE C WITH A BUSHING REPAIR IAW SRM 57-21-11.

Part: WIRE — CHAFED · airframe 65,351 hrs · 24,273 cycles

IAW TO EM4478-1 SEQ 3512011 FOUND CHAFED WIRE IN 90 DEGREE CONNECTOR 4021KS-A, WIRE GOES TO SOCKET E WIRE 5B416B20.

Part: FAN — FAULTY (E&E BAY) · airframe 64,660 hrs · 24,008 cycles

CREW REPORTS ACRID ODOR IN AIRCRAFT. CREW DEBRIEFED & REPORTED THEY HEARD RUMBLING NOISE AT FL 200, FOLLOWED BY ACRID BURNT RUBBER ODOR THROUGHOUT AIRCRAFT. CREW REPORTED NO SMOKE PRESENT, NO ECAM FAULTS DISPLAYED & PACK OPERATIONS GOOD THROUGHOUT FLIGHT. INSPECTED AIRCRAFT FOUND AVIONICS COMPARTMENT BLOWER FAN AT FAULT, R & R. OPERATIONS & LEAK CHECKED GOOD, NO OTHER FAULTS NOTED AT THIS TIME.

Part: RIVET — SHEARED (NR 1 PYLON) · airframe 64,515 hrs · 23,949 cycles

PYLON BLOWOUT PANEL HAS POPPED NR 1 ENG OTBD SIDE. PERFORMED FIM TASK INSPECTION IAW TSM 36-14-00-810-801A. SHEAR RIVETS ON DOOR BROKEN, NO OTHER PROBLEMS FOUND, NO HISTORY. INSTALLED ROBBED DOOR FROM HANGAR AIRCRAFT.

Part: HANDLE — UNSECURE (R2 DOOR) · airframe 64,347 hrs · 23,881 cycles

DOOR 2R DOOR ASSIST HANDLE NOT SECURE WILL NEED PCN 110-0938 & 110-0972. SECURED COVER TO HANDLE WITH TAPE. DID OPERATIONAL CHECK OF HANDLE, OPERATIONS CHECKED GOOD, REPLACED HANDLE.

Part: PROXIMITY SENSOR — BROKEN (NLG) · airframe 64,264 hrs · 23,854 cycles

LGCIU 1 FAULT DISPLAYED ON UPPER ECAM SCREEN L-G. CONNECTOR BROKEN OFF ON NLG EXT PROX SENSOR 24GA. REPLACED PROX SENSOR 24GA IAW MM.

Part: LINK — BENT (PROX SENSOR) · airframe 64,168 hrs · 23,814 cycles

NOSE GEAR FAULT, RETURNED TO FIELD. INSPECTED NOSE GEAR & FOUND LOWER PROXIMITY LINK ASSEMBLY BENT & 25GA PROXIMITY SENSOR INOPERATIVE. REPLACED LINKS IAW AMM 32-21-27 & SENSOR IAW AMM 32-31-73. PERFORMED NOSE GEAR SWING IAW AMM, NO DEFECTS NOTED.

Part: PLENUM — DELAMINATED (LT ACM) · airframe 64,125 hrs · 23,797 cycles

LT AIR CYCLE MACHINE PLENUM DELAMINATION ON INSIDE. REMOVED LT AIR CYCLE MACHINE PLENUM. INSTALLED SERVICEABLE AIR CYCLE MACHINE IAW AMM 21-51-21 THRU STEP 4.D. INSTALLED SERVICEABLE FAN AIR PLENUM CHAMBER IAW AMM. COMPLETED ACM INSTALL OPERATIONS CHECKED GOOD IAW AMM & FAN AIR PLENUM CHAMBER IAW AMM 21-52-22. PACK OPERATION NORMAL.

Part: PROXIMITY SENSOR — INOPERATIVE (MLG) · airframe 63,968 hrs · 23,732 cycles

CREW REPORTED GEAR WOULD NOT RETRACT ON INITIAL ATTEMPT. INDICATION FAULT ON NLG. CYCLED GEAR HANDLE AND GEAR RETRACTED NORMALLY, INDICATIONS GOOD. NLG EXT PROXIMITY SENSOR 25GA TARGET SENSOR BY LGCIU 2. REPLACED 24GA AND 25GA, ALSO BOTH TARGET ARMS AND PIVOT PINS IAW AMM.

Part: SUPPORT — LOOSE · airframe 63,968 hrs · 23,732 cycles

FOUND PLAY IN NOSE GEAR TARGET ARMS FOR 24 GA AND 25GA. REMOVED TARGET SUPPORT IAW AMM. REPLACED TARGET ARMS & PIVOT PINS, REF IPC 32-21-11, ITEMS 50,100 & 120, REINSTALLED TARGET SUPPORT ASSY IAW AMM TASK 32-21-27-400-001-A ITEM 4D(3) CONT FROM 4E(12) TO END.

Part: FAN — FAILED · airframe 63,550 hrs · 23,559 cycles

AMBER FAN INDICATION ON ECAM CONDITION PAGE. LOCKED OUT RT FAN CIRCUIT BREAKER ON ACCOUNT OF TRIPPING TWICE. CIRCUIT BREAKER DOES NOT POWER ANYTHING ELSE IAW AWM.

Part: SLIDING WINDOW — DAMAGED (COCKPIT) · airframe 63,413 hrs · 23,502 cycles

CAPTAIN`S LEFT WINDOW VERY HOT AND MULTIPLE BUBBLES. REPLACED SLIDING WINDOW. ANTI-ICE OPS CHECKED OK.

Part: COMPUTER — MALFUNCTIONED (FUEL QTY) · airframe 63,169 hrs · 23,411 cycles

FUEL ERROR LEFT TANK. CFDS SHOWS 19QT1 LT FUEL DENISTOMETER. DURING TROUBLESHOOTING, SWAPPED FQIC, NO HELP. RETURNED TO ORIGINAL POSITION. SUMPED LT TANK AND FOUND APPROXIMATELY 2 GALS OF WATER. ACCOMPLISHED CLASS-3 FAULTS & FOUND LEFT CADENSICON (19QT1) FAULT MSG. AFTER SUMP OF WATER THE INPUT PARAMETERS STAYED THE SAME. WILL REQUIRE TANK ENTRY TO REPLACE 19QT1. LEFT TANK READS LOW BY 2000 LBS. RE-SUMPED TANKS NO WATER NOTED. CHECKED FQIS STATUS NO FAULTS, FQIC 3QT HAD SEVERAL HITS ON PLR. REPLACED FQIC TESTS GOOD.

Part: SEAL — DETERIORATED (FAIRING) · airframe 63,169 hrs · 23,411 cycles

AFT FUSELAGE FAIRING 198GB SEAL IS DETERIORATED. R & R THE TORN SEAL IAW ECRA 5335-01013.

Part: EXTINGUISHER — DAMAGED (AFT GALLEY) · airframe 63,128 hrs · 23,396 cycles

AFT GALLEY HALON EXTINGUISHER HANDLE DAMAGED. REPLACED FIRE EXTINGUISHER.

Part: LATCH — BROKEN (02 BOX SEAT 11) · airframe 62,994 hrs · 23,341 cycles

OXYGEN MASKS DROPPED AT 11 ABC. OXYGEN PANEL DOOR LATCH BROKE OFF DOOR. SECURED O2 PANEL AT 11 SEATS 11ABC. PERFORMED OPERATIONAL CHECK OF MANUAL MASK RELEASE OF ALL O2 MASKS. SEATS OK FOR SERVICE.

Part: ENGINE — STALLED (NR 2) · airframe 62,993 hrs · 23,340 cycles

STALL DISPLAYED ON UPPER ECAM SCREEN DURING OFF IDLE ACCELERATION. ENGINE NOT SHUTDOWN. STALL OCURRED AT 210 DURING LEVEL OFF. RAN CHECKLIST. DID NOT REOCCUR. HEARD AUDIBLE STALL. TROUBLESHOOT PER TSM 71-00-00-810-809-A. REPLACED INEENG PER MT 71-01-7 REV Q.

Part: LATCH — DETACHED (NR 1 NACELLE) · airframe 62,830 hrs · 23,271 cycles

STRANGE PIECE OF METAL PROTRUDING FROM NR 1 ENGINE JUST BEHIND DRAIN VENT. OPENED FAN COWLING, WAS ABLE TO SEE A LOOSE LATCH MECHANISM. THAT HAS BEEN PROPERLY SECURED. CHECKED ALL THE OTHER LATCHES, FOUND SECURE. CLOSED AND LATCHED THE FAN COWL. PROPERLY SECURED. OK TO CONTINUE.

Part: SDAC — MALFUNCTIONED (NR 2) · airframe 62,793 hrs · 23,259 cycles

BCL 1 FAULT. NR 2 SDAC REPLACED IAW MM 31-55-34 AND 31-32-00. SYSTEM OPS OK. CHECKED WIRING PER TSM 24-30-00-810-807-A AND 24-38-00-810-807-A. NO FAULTS FOUND.

Part: BATTERY — FAULTED (MASTER) · airframe 62,781 hrs · 23,255 cycles

ELEC BCL 1 FAULT DISPLAYED ON UPPER ECAM. REPLACED NR 1 BATTERY IAW AMM 24-38-51. FAULT CLEARED.

Part: UNKNOWN — DAMAGED (STRUCTURE) · airframe 62,740 hrs · 23,235 cycles

PAN-LAM DAMAGED AFT RIGHT WALL JUST FWD OF GALLEY. PAN LAM DAMAGED NO SHARP EDGES. REPLACED AFT RIGHT WALL PAN-LAM.

Part: HINGE — OUT OF ADJUST (COCKPIT OXYGEN) · airframe 62,650 hrs · 23,203 cycles

OXYGEN MASK COVER ON CAPTAINS SIDE HAS COME LOOSE ON ONE END. ADJUSTED HINGE, OPS CHECKED GOOD.

Part: OXYGEN MASK — MISINSTALLED (COCKPIT) · airframe 62,457 hrs · 23,128 cycles

CREW OXYGEN SYSTEM LOW. CREW REPORTED LOOSING PRESSURE SLOWLY DURING FLIGHT. FOUND F/O MASK NOT INSTALLED CORRECTLY, REINSTALLED. MX CHECKED, NO LEAKS FOUND AND SERVICED BOTTLE PER AMM.

Part: DOOR SEAL — DIRTY (R2 DOOR) · airframe 62,347 hrs · 23,084 cycles

DOOR 2R HAS A LOUD NOISE COMING FROM ITS SEAL. CLEANED AND RESEALED LOWER AFT DOOR SEAL AT R2 DOOR. PERFORMED PRESSURE, OK TO CONTINUE.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 61,595 hrs · 22,798 cycles

CENTER TANK PUMPS RAN WITH TANK EMPTY FOR OVER AN HOUR IN MANUAL MODE. NEVER GOT LOW PRS. RESET SYSTEM. LOW PRESSURE LIGHTS WORKED NORMAL WITH MODE SELECTOR IN MANUAL.

Part: OXYGEN MASK — DEPLOYED (CABIN) · airframe 61,531 hrs · 22,775 cycles

REF CF575. ROWS 30 ABC O2 MASKS FELL. ACCOMPLISHED DROP CHECK PER MT 35- 003 AND AMM 35-23-00-710-001-A.

Part: OXYGEN MASK — DEPLOYED (CABIN) · airframe 61,523 hrs · 22,772 cycles

CREW REPORT: O2 MASKS DEPLOYED AT ROW TEN. SEATS 10ABC O2 MASK DROPPED. O2 GEN NOT FIRED, RE- PACKED ASSY AND APPLIED MT 35-003. OK TO CF MANUAL MASK RELEASE OPS CHECK FOR 3 DAYS.

Part: WINDSHIELD — FAULTY (COCKPIT) · airframe 61,296 hrs · 22,687 cycles

L WINDOW DISPLAYED ON UPPER ECAM SCREEN. - ANTI ICE DEFERRED PER MEL. INSTALLED DF STICKER ADJ TO WINDOW HEAT SWITCH. INSTALLED NO AUTOLAND PLACARD ADJ TO CA PFD. INF- :REMOVED AND REPLACED LEFT WINDSHIELD IAW AMM. WINDOW IS IN PLACE WITH FASTENERS, NEEDS TO BE TORQUED. CONTINUE WITH AMM. REPLACE- :COMPLETED INSTALLATION OF WINDSHIELD REF MM 56-11-11 STEP 7 TO END. TEST OKAY.

Part: BATTERY — FAULTY (CABIN) · airframe 61,233 hrs · 22,658 cycles

ATA 33-51-38 BATTERY EMERGENCY L' DISPLAYED AFTER PERFORMING NR 3 SVC CABIN EMERGENCY LIGHT TEST. TROUBLESHOT PER TSM 33-51-00, REPLACED L EPSU BATTERY (11WL) PER MM. OPS CHECKS GOOD.

Part: HANDLE — CONTAMINATED (L1 DOOR) · airframe 60,640 hrs · 22,432 cycles

CS UNABLE TO OPEN DOOR 1L ON ARRIVAL, CREW OPENED FROM INSIDE. FOUND WATER IN DOOR HANDLE RECESS IN OUTER DOOR HANDLE. REMOVED WATER & CLEANED OUT RECESS. SPRAYED ICE RELEASE ON OUTER DOOR HANDLE. DOOR OPERATES NORMALLY AND ARMS AND DISARMS NORMALLY.

Part: LATCH — BROKEN (OXYGEN MASK) · airframe 60,610 hrs · 22,419 cycles

O2 MASK HANGING AT SEAT 21ABC. LATCH IS BROKEN ON DOOR. SECURED LATCH, PACKED MASK IAW AMM 35-23-00-500-003, DROPPED CHECKED IAW AMM 35-23-00-710-001 GND CHECKED GOOD.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 60,192 hrs · 22,275 cycles

DURING 3SV EMERGENCY LIGHT CHECK, FAULTED EMERGENCY BATTERY RIGHT, ON CIDS PANEL. REPLACED RT OVERWING POWER SUPPLY BATTERY, OPS AND TESTED NORMAL PER AMM.

Part: BALLAST — FAILED (GALLEY LIGHT) · airframe 60,161 hrs · 22,263 cycles

FLIGHT ATTENDANTS REPORTED AN ELECTRICAL ODOR IN AFT GALLEY. INSPECTED AFT GALLEY ELECT COMPONENTS, COFFEEMAKERS, OVENS, WORK LIGHTS, FOUND BURNED BALLAST FOR 24LG RT ENTRY LIGHT AT DOOR 2. DISCONNECTED BALLAST AT 7206VC DISCONNECT, VENTILATED CABIN TO DISSIPATE ODOR. REPLACED BALLAST AND LIGHT BULB.

Part: ATTACH FITTING — WORN (NR 2 PYLON) · airframe 59,636 hrs · 22,072 cycles

NR 2 PYLON TO ENGINE LT AND RT SIDE MOUNT FITTING WEAR WAS BLENDED REF ECRA:5451-01086. PERFORMED HFEC INSPECTION WITH NO DEFECTS FOUND.

Part: MOUNT FITTING — WORN (NR 2 PYLON) · airframe 59,636 hrs · 22,072 cycles

NR 2 PYLON TO ENGINE LT AND RT SIDE MOUNT FITTING WEAR WAS BLENDED REF ECRA:5451-01086. PERFORMED HFEC INSPECTION WITH NO DEFECTS FOUND.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 59,636 hrs · 22,072 cycles

RT FUSELAGE SKIN FR 33 AND STR 23R UNDER FILLET PANEL 192AT EXCESSIVE MATERIAL REMOVED REF SMB WU U9578I. MAJOR REPAIR ACCOMPLISHED PER SRM 53-21-11 FIG.215.

Part: SUPPORT BRACKET — CORRODED (L1 DOOR SLIDE) · airframe 59,636 hrs · 22,072 cycles

1 LT MED EMERGENCY SLIDE DOOR SUPPORT BRACKET ON PACK HAS CORROSION EXFOLIATION. REPLACED SLIDE AND INSTALLED.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 59,400 hrs · 21,995 cycles

THE 1 LT EPSU FAILED EMERGENCY LIGHT TEST. REPLACED BATTERY PER AMM, TESTED NORMAL.

Part: BUTTON — MISSING (CABIN) · airframe 59,025 hrs · 21,857 cycles

THE 8ABC O2 MASK COMPARTMENT TEST BUTTON MISSING. REPLACED TEST BUTTON AT SEAT 8ABC. INSTALLED MASK REF AMM. COMPLETED INSTALLATION REF COMPLETED OPERATIONAL REF AMM 35-23-00 ALL INDICATIONS NORMAL.

Part: SLIDE — MISINSTALLED (L1 DOOR) · airframe 59,025 hrs · 21,857 cycles

DOOR 1L SLIDE PACK IS IMPROPERLY INSTALLED ON LOWER PIN OR PIN IS DAMAGED CAUSING SLIDE TO LIFT UP. REMOVED AND REPLACED SAME SLIDE PER MM.

Part: RAM AIR TURB — NO TEST · airframe 58,380 hrs · 21,630 cycles

RAT FAILS CHECK, NO GREEN LIGHT. RAM AIR TURBINE ASSY OPS CHECKED GOOD, NO LEAKS.

Part: OXYGEN MASK — NO TEST (COCKPIT) · airframe 57,231 hrs · 21,153 cycles

CAPTAIN'S O2 MASK FAILS TEST. SWAPPED WITH 2ND OBS POSITION; NOW THE 2ND OBS SEAT IS INOP. REPLACED OXYGEN-MASK STOWAGE-BOX IAW AMM, ALL OK.

Part: TRANSCEIVER — INOPERATIVE (WX RADAR SYS) · airframe 21,113 hrs · 57,126 cycles

WX RADAR INOP, FLIGHT DIVERTED. REPLACED RADAR R-T. OPS NORMAL.

Part: COMPUTER — FAILED · airframe 57,124 hrs · 21,112 cycles

AVNCS SYS FAULT DISPLAYED ON UPPER ECAM SCREEN. SKIN AIR OUTLET DISPLAYING INTERMITTENT AMBER XX'S. DEFERRED PER MEL. REF CALLOUT LM1230 FOR ORD TO CHANGE 2 SWITCHES AND A SENSOR, NO PARTS AT LGA. MX REPLACED THE SKIN AIR OUTLET VALVE AND AEVC.

Part: EEC — FAULTED (NR 1 ENGINE) · airframe 57,090 hrs · 21,098 cycles

NR 1 ENG STALL AT TOP OF DESCENT. DUE TO REPEAT HISTORY OF ENGINE NR 1 STALL ECAM MESSAGES, REPLACE THE STAGE 7 BLEED VALVE 7C, 7C BLEED VALVE SOLENOID AND THE EEC PRECAUTIONARY. REPLACED EEC & 7C BLEED VALVE & 7C BLEED SOLENOID.

Part: ENGINE — VIBRATION (RIGHT) · airframe 56,983 hrs · 21,062 cycles

(RT ENG VIBES), FLIGHT DIVERTED. LCL MAINT ACCOMPLISHED PRE LIM GENERAL VISUAL INSPECTION ON FAN INELT, ENG EXHAUST, NO EVIDENCE OF FOD OR BIRD STRIKE, NO DAMAGE TO INLET, SURROUNDING AREA OR FAN BLADES REPORTED. CREW REPORTED AT FL360, .79 MACH, NR 2 ENG VIBES AT 7.2. AT IDLE VIBES AT 2.2. FEELING BUZZ THROUGHOUT AIRFRAME. ACP TSM 77-30-00 VISUAL INSP, LPC, LPT BORO, TAP TEST OF FAN BLDS, CHIP DETECTORS, VISUAL OF N1 SPEED SENSOR AND HARNESS, AND VIBRATION SURVEY ALL ITEMS CHECK GOOD.

Part: BLOWOUT PANEL — CRACKED (CARGO BAY) · airframe 56,934 hrs · 21,041 cycles

FWD CARGO BLOWOUT PANEL IS CRACKED. REPLACED FWD CARGO BLOWOUT PANEL.

Part: ENGINE — VIBRATION (NR 2) · airframe 56,214 hrs · 20,752 cycles

NR 2 ENGINE VIBRATION. CHECKED THE MASTER MAGNETIC CHIP DETECTOR FOR DEBRIS. NR 1 ENG INSPECTED ALL 6 AND MASTER CHIP DETECTORS FOR PARTICLES. ALL CHIP DETECTORS CLEAN. ACCOMPLISHED NR 1 ENG VIBRATION SURVEY IAW MM TASK. NR 8 TEST OKAY, MAX VIB WAS 1.3 UNITS.

Part: TANK — LEAKING (RT WING) · airframe 55,589 hrs · 20,525 cycles

FUEL LEAKING FROM WING INBD OF RT ENGINE. RT WING TANK OPENED & VENTED FOR DRY BAY FUEL MX ACCESS. LOCATED AND SEALED SOURCE OF DRY BAY LEAK. SEALANT APPLIED 1500-24. ACCOMPLISHED LEAK CHECK.

Part: ACTUATOR — FAILED (HORIZONTAL STAB) · airframe 55,522 hrs · 20,495 cycles

TRIMMABLE HORIZ STABILIZER ACTUATOR FAILED JAMMING TEST. START REMOVING THS ACTUATOR. ACCOMPLISHED UP TO ITEM NR 5. COMPLETED INSTALLATION OF THS ACTUATOR. INSPECTED THE INSTALLATION OPERATION, SAFETY AND SECURITY OF THE THS ASSY.

Part: VALVE — FAULTY (AFT CARGO HEAT) · airframe 55,270 hrs · 20,391 cycles

AFT CARGO HEAT FAULT DISPLAYED ON UPPER ECAM SCREEN. REPLACED CARGO HEAT PRESS REG VALVE, OPS NORMAL.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 54,265 hrs · 19,964 cycles

MAJOR REPAIR. AFT PIT CORROSION BETWEEN FR65 AND 66 STR 33R UNDER OUTFLOW VALVE MOTOR. REPLACED STRINGER SECTION REF SRM 51-42-11 ON NR C4784K.

Part: SKIN — CORRODED (FUSELAGE) · airframe 54,265 hrs · 19,964 cycles

REPAIR DOUBLER IS INSTALLED DUE TO CORROSION AT CUTOUT FOR AFT LAV SERVICE PANEL ON LOWER AFT FUSELAGE. REPLACED INNER DOUBLER REF SRM ON NR C4392K.

Part: SKIN — CORRODED (FUSELAGE) · airframe 54,265 hrs · 19,964 cycles

CORROSION ON SKIN UNDER DOME NUTS BETWEEN FR 55 & 56 AT ANTENNA MOUNT. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR IAW REO-L01272, EVA-80171 AND SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 54,265 hrs · 19,964 cycles

CORROSION ON SKIN UNDER DOME NUTS BETWEEN FR 58 & 59 AT ANTENNA MOUNT. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR PER RE0-L01272 & EVA-80171 AND SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 54,265 hrs · 19,964 cycles

CORROSION ON SKIN UNDER DOME NUTS BETWEEN FR 57 & 58 AT ANTENNA MOUNT. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR IAW REO-01272, EVA-80171 AND SRM.

Part: RELEASE CABLE — OUT OF ADJUST (R1 GIRT BAR) · airframe 56,265 hrs · 19,964 cycles

R1 DOOR GIRT BAR DOES NOT FULLY LOCK INTO FITTING. ADJUSTED ESCAPE SLIDE RELEASE CABLE IAW MM ON NR C7145K BY NR308039 AND INSPECTED BY LC81.

Part: STRINGER — CORRODED (S40R) · airframe 54,265 hrs · 19,964 cycles

AFT PIT HAS CORROSION ON STR 40R BETWEEN FR 58 & 59. MAJOR REPAIR. REMOVED CORRODED SECTION OF STRINGER AND REPLACED WITH SPLICED SECTION.

Part: STRINGER — CORRODED (S43L) · airframe 54,265 hrs · 19,964 cycles

AFT PIT STRINGER 43L BETWEEN FR 54 AND 59 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: REPLACED STRINGER SECTION.

Part: GIRT BAR — UNKNOWN (R2 DOOR) · airframe 52,462 hrs · 19,245 cycles

DOOR 2R SLIDE WILL NOT DISARM AT GATE. CHECK ASSIST BOTTLE PRESSURE, SURVIVAL KIT LANYARD STRAP ATTACHMENT, AND GIRT BAR AREA FOR FOD. WARMED ACFT. ARM-DISARM HANDLE OPERATES NORMALLY, CHECKED DOOR ASSIST PRESSURE: OK. GIRT BAR LANYARD HAS NO FOULING.

Part: SLIDE — FAULTY (L1 DOOR) · airframe 52,119 hrs · 19,107 cycles

DOOR 1L ESCAPE SLIDE HAS SURVIVAL KIT LANYARD NO VISIBLE AND VELCRO WORN. REINSPECTION OF SURVIVAL RETAINING STRAP SHOWS VELCRO RETAINING STRAP IS WORN AND WILL NOT SECURE. STRAP IS NOT MIS-ROUTED OR ATTACHED TO GRIT BAR. STRAP DOES NOT INTERFER WITH EMERGENCY FUNCTION.

Part: SLIDE — FAULTY (L2 DOOR) · airframe 52,119 hrs · 19,107 cycles

DOOR 2L ESCAPE SLIDE SURVIVAL KIT LANYARD LOOP NOT VISIBLE AND HOOK AND LOOP WORN. REINSPECTION OF SURVIVAL RETAINING STRAP SHOWS HOOK AND LOOP RETAINING STRAP IS WORN AND WILL NOT SECURE. STRAP IS NOT MIS-ROUTED OR ATTACHED TO GRIT BAR. STRAP DOES NOT INTERFER WITH EMERGENCY FUNCTION.

Part: HOSE — LEAKING (O2 MASK) · airframe 49,855 hrs · 18,150 cycles

CREW REPORTS O2 SYSTEM LOW, POSSIBLE O2 LEAK. SERVICED TO FULL AT SJU, PLEASE INVESTIGATE. FOUND CAPT O2 MASK HOSE LEAKING. SWAPPED WITH SEC OB SEAT AND DEF SECOND OBS. SEAT.MR35114- 10 BAD MASK FROM CAPT POSITION AND INSTALLED -46 IN CAPT POS AND PUT -10 IN SECOND OBS SEAT BUT IS NOT HOOKED UP.

Part: FITTING — FAULTY (L2 DOOR SLIDE) · airframe 49,357 hrs · 17,974 cycles

DOOR 2 LT ESCAPE SLIDE BUSTLE STRAP RETAINING CLIP BROKEN. REPLACED SLIDE ASSY.

Part: ELEVATOR — DAMAGED (LEFT) · airframe 48,677 hrs · 17,704 cycles

OUTBOARD 3FT OF LEFT ELEVATOR DAMAGED. ELEVATOR REMOVED. NEW ELEVATOR INSTALLED. SAFETIED AND RIGGED AND TESTED LT ELEVATOR. OPS CHECKS OK. NO LEAKS NOTED FROM ACTUATORS.

Part: ACTUATOR — FAILED (ELEVATOR) · airframe 48,336 hrs · 17,570 cycles

ELAC 2 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. LEFT ELEV GREEN ACT FAILING. REPLACED ELEV LG ACTUATOR 34CE1, OPS TESTED OK.

Part: UNKNOWN — UNKNOWN (EMERGENCY CALL) · airframe 48,261 hrs · 17,545 cycles

CABIN EMERGENCY CALL GOING OFF BY ITSELF.

Part: CONTROLLER — MALFUNCTIONED · airframe 48,261 hrs · 17,545 cycles

CABIN EMERGENCY CALL GOES OFF BY ITSELF. REPLACED NR 1 CIDS DIRECTOR PER MM 23-73-00, TESTS OK.

Part: PANEL — CORRODED (FUSELAGE) · airframe 48,118 hrs · 17,494 cycles

CORROSION AT CUTOUT FOR AFT LAV SERVICE PANEL ON LWR AFT FUSELAGE. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR DOUBLER.

Part: SWITCH — FAILED (L2 DOOR SLIDE) · airframe 48,009 hrs · 17,452 cycles

LEFT AFT SLIDE INDICATION INOP ON DOOR-OXY SYSTEM ECAM PAGE - DOOR-OXY -SLIDE ARMS BUT INDICATION INOP. *S/D* SLIDE DOOR ARMING PROX SWITCH FAILED. REPLACED PROX SWITCH AT DOOR 2L. ALL INDICATIONS ARE NORMAL.

Part: CONTROL UNIT — FAULTY (ELAC 1) · airframe 47,449 hrs · 17,244 cycles

AIL SERVO FAULT, LAF DEGRADED L AIL AMBER HALF BOX B, R AIL AMBER HALF BOX G. REPLACED ELAC 1, ALL OPS TESTS WERE NORMAL.

Part: CONTROLLER — FAULTY (COCKPIT DOOR) · airframe 46,322 hrs · 16,834 cycles

FLIGHT DIVERTED DUE FLIGHT DECK DOOR LOCK CYCLING OPEN, DOOR NOT SECURE. FAULT LIGHT ILLUMINATED. DOOR CONTROLLER MALFUNCTION. REPLACED DOOR CONTROLLER.

Part: EPSU — FAULTY (CABIN) · airframe 46,293 hrs · 16,822 cycles

LEFT AFT ENTRY DOOR EMERGENCY EXIT LIGHT HAS BATTERY FAULT. EPSU FAULTY. REPLACED EPSU.

Part: COVER — UNSECURE (EVAC SLIDE) · airframe 46,185 hrs · 16,784 cycles

CREW REPORT: SLIDE PACK 2R HAS FALLEN OFF. RESECURED SLIDE COVER, NO REPEATS SINCE ORIGINAL.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 46,185 hrs · 16,784 cycles

CREW REPORT: SLIDE PACK 2R HAS FALLEN OFF.

Part: CONTROL UNIT — FAILED (SMOKE DETECTION) · airframe 46,044 hrs · 16,735 cycles

SMOKE LAV + CARGO DETECTOR FAULT DISPLAYED ON ECAM WHEN RECALL CRG SMOKE TEST FAILS. SDCU FAILURE. REPLACED SDCU AND FWD PIT DETECTOR AS PRECAUTIONARY.

Part: HYDRAULIC LINE — MALFUNCTIONED (GREEN SYSTEM) · airframe 45,901 hrs · 16,681 cycles

GREEN RESERVOIR LOW LEVEL DISPLAYED ON UPPER ECAM SCREEN. LOSS OF GREEN HYD SYSTEM ON TAXI IN. A/C TOWED TO THE GATE. FOUND LT LOCKING STAY SUPPLY HOSE LEAKING. REPLACED LT LOCKING STAY HOSE. RESERVICED GREEN HYD SYSTEM.

Part: BATTERY — FAULTY (EMERGENCY LIGHTS) · airframe 45,417 hrs · 16,496 cycles

FOUND CABIN EMERGENCY LIGHTS DID NOT TEST. 10-19-07 FOUND EPSU FAULTED. REPLACED EPSU ASSY - OPS CHECK OK --NO REPEATS SINCE ORIGINAL.

Part: COMPUTER — FAULTY (NR 1 ELAC) · airframe 45,420 hrs · 16,497 cycles

RECEIVED AN "ELAC1 AILERON ORDER DISAGREE" MESSAGE. NR 1 ELAC COMPUTER FAULTY. REPLACED NR 1 ELAC COMPUTER, NO REPEATS.

Part: ENGINE — SURGES (NR 2) · airframe 45,391 hrs · 16,483 cycles

NR 2 ENGINE SURGED ON RUNWAY AT 140 KNOTS. 10-19-07 ACP HPC, HPT AND CLAPPER BORO INSPECTION. NO DAMAGE NOTED. ACP 7TH AND 10TH STAGE BLEED VALVE AND SOLONID CHECKED GOOD. ALSO LUBED VSV AND LPC. NO REPEATS SINCE ORIGINAL.

Part: STRUCTURE — DAMAGED (THRUST REVERSER) · airframe 45,319 hrs · 16,436 cycles

NR 1 ENG THRUST REVERSER INNER WALL AT 11 O'CLOCK POSITION HAS DAMAGE.

Part: SLIDE — FAULTY (R1 DOOR) · airframe 44,901 hrs · 16,305 cycles

R FWD CABIN DISPLAYED ON UPPER ECAM SCREEN. DOOR CREW COMMENTS: DOES NOT LOCK PROPERLY MECH INFORMS LOOSE OR MISSING. STRAPS COMING LOOSE FROM THE SLIDE AND INTERFERING WITH THE GIRT BAR. REPLACED R1 DOOR SLIDE.

Part: HOOK AND LOOP — WORN (L2 DOOR) · airframe 44,539 hrs · 16,174 cycles

DOOR 2L SLIDE-RAFT LANYARD HOOK AND LOOP STRIP DOES NOT STICK TOGETHER. FOUND WORN HOOK AND LOOP STRIP. REPLACED DOOR SLIDE 2L.

Part: MASK — MALFUNCTIONED (COCKPIT) · airframe 44,354 hrs · 16,105 cycles

CREW REPORT: FIRST OFFICER`S 02 MASK PUSH TO TEST INOP. OBS MASK OKAY.

Part: UNKNOWN — SMOKE (GALLEY) · airframe 43,681 hrs · 15,838 cycles

FLIGHT CREW REPORTING SMOKE IN AFT GALLEY IN OVEN AREA. [SUP 06-01-07] REMOVED BOTH OVENS, CEILING PANELS AND CIRCUIT BREAKER PANEL AND FOUND NO EVIDENCE OF FIRE. OPERATED OVENS, HOT PLATES AND CHILLERS FOR 4.5 HOURS ON GROUND AND DID NOT NOTICE ANY SMOKE OR BURNING ODOR.

Part: SPRING — BROKEN (L2 DOOR GIRT BAR) · airframe 42,461 hrs · 15,373 cycles

FOUND GIRT BAR STOP LEVER SPRING BROKEN, ON L2 DOOR, AFT GIRT BAR FITTING. REPLACED SPRING IN GIRT BAR FITTING. OPS NORMAL

Part: GIRT BAR — UNSECURE (DOOR 2RT) · airframe 41,935 hrs · 15,182 cycles

FLIGHT ATTENDANT REPORTS DOOR 2R WILL NOT DISARM. FOUND GIRT BAR FORWARD ATTACH POINT UNSECURE. REATTACHED GIRT BAR. OPERATES NORMAL

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 35,692 hrs · 12,818 cycles

FIRST OFFICER'S WINDSHIELD CRACKED. CRACK APPEARS TO HAVE INITIATED FROM A BUBBLE AT THE TOP CENTER OF THE WINDOW WHICH DID NOT IMPAIR VISIBILITY.

Part: CONTROL UNIT — FAILED (SMOKE DETECTORS) · airframe 33,244 hrs · 12,002 cycles

FLIGHT DIVERTED DUE TO AFT CARGO SMOKE ECAM MESSAGE. REPLACED SMOKE DETECTOR CONTROL UNIT (SDCU) AND FOUR AFT CARGO SMOKE DETECTORS.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 32,945 hrs · 11,890 cycles

AFT PIT STRINGER 43L IS CORRODED FROM FRAME 54 TO FRAME 56. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STRINGER SECTION AND SPLICE REPAIRS.

Part: PRESSURE SWITCH — LEAKING (APU OIL SYSTEM) · airframe 23,346 hrs · 8,281 cycles

UNUSUAL SMELL NOTED IN THE CABIN. SUPPLEMENTAL DATA UPDATE AFTER ACCOMPLISHMENT OF TROUBLESHOOTING PROCEDURES, FOUND APU OIL PRESSURE SWITCH LEAKING AND OIL BEING INGESTED INTO APU AIR INLET. SWITCH WAS REPLACED AND NO FURTHER SMELL NOTED.

Part: ENGINE — COKED (NR 2) · airframe 22,656 hrs · 8,060 cycles

CREW REPORTS INFLIGHT SHUTDOWN OF NR 2 ENGINE. ALL ENGINEPARAMETERS ARE NORMAL EXCEPT OIL QUANTITY WAS ZERO. *S/D* AIRCRAFT HAD DEFECTIVE ENGINE REPLACED WITH SERVICEABLE ENGINE. OFF ENGINE IS AT OUTSIDE VENDOR SHOP VISIT FOR DETERMINATION OF CAUSE. PRELIMINARY RESULTS SHOW HEAVY COKING IN THE REAR BEARING AREA.

Part: LIGHT — DAMAGED (CABIN) · airframe 22,554 hrs · 8,024 cycles

EXIT LIGHT DAMAGED NEAR FLOOR AT DOOR 1 LEFT. REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECK OK.

Part: SERVO — FAILED (RUDDER) · airframe 22,283 hrs · 7,937 cycles

AIRFRAME VIBRATION NOTED. *S/D* THE CENTER RUDDER SERVO WAS REPLACED. NO ADDITIONAL PROBLEMS NOTED.

Part: CONNECTOR — DISCONNECTED (RT WING)

CABIN EMERGENCY LIGHTING SYSTEM TEST GIVES STATUS OF 'EXT LOADS EMER R' ON PTP DISPLAY. *S/D* 'EXT LOADS EMER R' WAS SHOWN DURING TEST ON PTP. CANNON PLUG WAS FOUND DISCONNECTED FROM RT WING AFT LIGHT ASSEMBLY (62WL). CANNON PLUG WAS RECONNECTED AND CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

ESCAPE PATH LIGHTS INOP AT ROW 16, 17, 18 AND ROW 22, 23, 24. REPLACED EPSU EMERGENCY POWER SUPPLY UNIT BATTERY PACK AND POWER SUPPLY. P/N 563-1188 AND 565-2005. SYSTEM CHECKS NORMAL.

Part: BATTERY — DISCHARGED (CABIN)

SYSTEM FAILED EMERGENCY LIGHTING TEST. MESSAGE WAS: BATT L. PSU BATTERY WAS REPLACED (PSU P/N IS 565-0038).

Part: RMP — SMOKING (RT COCKPIT)

FIRST OFFICER'S RADIO MANAGEMENT PANEL SMOKING. RADIO MANAGEMENT PANEL (RMP) WAS REMOVED FOR THIS PROBLEM. LATER THE PANEL WAS FOUND TO BE OK AND REINSTALLED IN THE AIRCRAFT. MR23131-0135.

Part: SEAT — CRACKED (CABIN)

DURING FIRST HMV-1 FOR THIS ACFT, ALL COACH SEATS IN PAX CABIN WERE FND CRACKED AT FWD ATTACHMENT HOLES OF THE SEAT PAN. THESE ARE RECARO 720 SERIES SEATS INSTALLED. SEAT MFG DESIGNATES SEAT PAN AS PRIMARY STRUCTURE IN ITS COMPT MM. SEAT PANS BEING REPLACED WITH NEW SEAT PANS THAT ARE OF SAME DESIGN. THESE SEAT PANS WILL FAIL (CRACK) IN SAME PLACES DURING THEIR SERV LIFE. SUBMITTER STATED AD SHOULD BE ISSUED TO INSPECT THESE SEAT PANS FOR CRACKS EACH 90 DAYS AND FOR REMOVAL FROM SERVICE OF SEAT PANS THAT ARE CRACKED. THERE ARE 132 OF THESE SEAT PANS ON ACFT. THIS IS 9TH CONSECUTIVE A320232 THAT HAS EXHIBITED A 100 PERCENT FAILURE RATE OF THESE SEAT PANS. THAT IS 1,188 DEFECTIVE SEAT PANS IN 6 MONTHS.

Part: HYD SYST — REQUIRED SERVICE (GREEN HYD STST)

GREEN HYDRAULIC SYSTEM QUANTITY INDICATION LOW. SHUT DOWN ENGINE 1 GREEN PUMP AND PTU. DIVERTED TO ORD. *S/D* CYCLED GEAR, FLAPS AND SPOILERS SEVERAL TIMES. ALSO, MOTORED ENGINE. NO LEAKS FOUND, SUSPECT AIR IN SYSTEM.

Part: SLIDE INDICATION — MALFUNCTIONED (1R DOOR)

DOOR 1 RIGHT SLIDE INDICATION DOES NOT SHOW ON ECAM. *S/D* DEFECTIVE PROXIMITY SWITCH. REPLACED SWITCH AND OPERATIONALLY CHECKED DOOR ARMING SYSTEM, ECAM MESSAGE OK.