N393HA

Part: COOLING DUCT — CRACKED (ZONE 400) · airframe 48,005 hrs · 7,676 cycles

ETOPS - ON WALK AROUND, FOUND #2 ENG EEC COOLING INLET DUCT CRACKED. REMOVED AND REPLACED #2 ENG EEC COOLING DUCT INLET PER CMM 71-60-00. SEC CHK GOOD. OK FOR SVC

Part: LINE — LEAKING (NR 1 ENG OIL) · airframe 47,855 hrs · 7,655 cycles

ETOPS - ON WALK AROUND FOUND OIL LEAKING FROM FAN COWLS ON #1 ENG. FOUND #1 ENG OIL PRESSURE TRANSDUCER LINE LEAKING (AFT LINE) REMOVED AND REPLACED BOTH OIL PRESSURE TRANSDUCER LINES PER TASK CARD 330-79-HIW-03. LEAK CHK OK. OK FOR SVC.

Part: MOUNT — SHEARED (ZONE 400) · airframe 47,724 hrs · 7,637 cycles

ETOPS - ENG 1 REV FAULT ON LANDING (CLEARED ON SHUTDOWN). PERFORMED TSM 78-37-00-810-833-A. FOUND ENG 1 PCM SUPPORT MOUNTING BRACKET SHEARED FROM MOUNTS. REMOVED ENG 1 PCM PER AMM 73-21-34. REPAIRED MOUNTING BRACKET PER E105-C20228-INI. INSTALLED #1 ENG PCM PER AMM 78-37-61. OPS CHECK GOOD. OK FOR SVC.

Part: TRANSFER SYS — FAULTED · airframe 47,324 hrs · 7,576 cycles

ETOPS - BTB ON TAXI OUT ECAM FUEL AFT XFR FAULT. REMOVED & REPLACED LEFT INNER TANK INLET VALVE ACTUATOR PER AMM 28-26-53/400. OPS CHECK GOOD. OK FOR SVC.

Part: EXCITER — OUT OF LIMITS (NR 2 ENGINE) · airframe 46,792 hrs · 7,477 cycles

ETOPS - #2 ENG IDG EXCITER FIELD CHECKS OUT OF LIMITS PER TSM 24-20-00-810-875-A PARA 4 (A) (1). IDG REMOVED UP TO AMM 24-21-51-000-804A STEP 4(A). CONTINUED REMOVAL OF #2 IDG AND REPLACED #2 IDG PER AMM 24-21-51 OPS AND DISCONNECT TEST CHECK GOOD OK FOR SVC.

Part: TRANSCEIVER — FAULTED (WX RADAR) · airframe 46,635 hrs · 7,450 cycles

ETOPS - ECAM: "NAV PRED W/S DET FAULT" DISPLAYED WHEN WXR/PWS SWITCH IS SELECTED TO 1. REMOVED AND REPLACED #1 RTU PER 34-41-00. BITE TEST PASSED. NO FAULT NOTED. OK FOR SERVICE.

Part: CLAMP — DISCONNECTED (ZONE 500) · airframe 46,620 hrs · 7,448 cycles

ETOPS - AIR- L- WING LEAK. FOUND CLAMP DISCONECTED FROM TRIM AIR PRESSURE REGULATING VALVE. INSTALLED NEW SEAL PER AMM 21-63-52. INSTALLED CLAMP PER M105 #R0483. OPS CHECK GOOD. LEAK CHECK GOOD. NO DEFECTS NOTED. OK FOR SERVICE.

Part: BOOST PUMP — FAULTED (NR 1) · airframe 46,434 hrs · 7,416 cycles

ETOPS - ECAM FUEL LEFT PUMP 1 LO PR. C/B TRIPPED FUEL L PUMP 1 SUPPLY. REMOVED AND REPLACED LH PUMP 1 (121QA1) PER AMM 28-21-51. OPS AND LEAK CHECK GOOD.

Part: SEAT TRACK — CORRODED (ZONE 200)

DURING ROUTINE MAINTENANCE INSPECTION, FOUND SEAT TRACK CORRODED AT FR62 - 63 (-Y450).

Part: SEAT TRACK — CORRODED (ZONE 200)

DURING ROUTINE MAINTENANCE INSPECTION, FOUND SEAT TRACK CORRODED AT FR61-62 (-Y1959).

Part: WEB — CORRODED (ZONE 200)

DURING ROUTINE MAINTENANCE INSPECTION, FOUND LONGITUDINAL WEB CORRODED AT AFT OF D1R AT B/W FR 16 -18 (Y-2462).

Part: SEAT TRACK — CORRODED (ZONE 200)

DURING MAINTENANCE INSPECTION, FOUND SEAT TRACK CORRODED AT FR53.6 (Y1959).

Part: SEAT TRACK — CORRODED (ZONE 200)

DURING ROUTINE MAINTENANCE INSPECTION, FOUND SEAT TRACK CORRODED AT FR74 - 75 (Y450).

Part: SEAT TRACK — CORRODED (ZONE 200)

DURING ROUTINE MAINTENANCE INSPECTION, FOUND SEAT TRACK CORRODED AT FR62 - 63 (-Y450).

Part: SEAT TRACK — CORRODED (ZONE 200)

DURING ROUTINE MAINTENANCE INSPECTION, FOUND SEAT TRACK CORRODED AT FR53.6 (Y1959).

Part: SEAT TRACK — CORRODED (ZONE 200)

DURING ROUTINE MAINTENANCE INSPECTION, FOUND SEAT TRACK CORRODED AT FR61 - 62 (Y1959).

Part: SEAT TRACK — CORRODED (ZONE 200)

DURING ROUTINE MAINTENANCE INSPECTION, FOUND SEAT TRACK CORRODED AT FR71 (-Y1959).

Part: BLEED VALVE — FAULTED (NR 2 ENGINE) · airframe 46,192 hrs · 7,375 cycles

ETOPS - DURING ENG 2 IDLE RUN. HP VALVE NOT WORKING. REMOVED AND REPLACED #2 HP BLEED VALVE PER AMM 36-11-51. OPS/LEAK CHECK GOOD. OK FOR SVC.

Part: THERMOCOUPLE — BROKEN (NR 1 ENGINE) · airframe 45,428 hrs · 7,253 cycles

ETOPS - #ENG 1 HP/IP TURBINE VENT OVERHEAT CHANNEL A THERMOCOUPLE BROKEN. REPLACED THERMOCOUPLE AS HP/IP BEARING COMPARTMENT VENT TUBE BORESCOPE AND CLEANING PER TC A2010-0709-PART 01 OPS/LK CHK GOOD OK FOR SVC.

Part: FIRE LOOP — FALSE ACTIVATION (NR 2 ENG) · airframe 45,260 hrs · 7,230 cycles

ETOPS - MOMENTARY ENG 2 FIRE LOOP A FAULT ECAM IN CLIMB. REMOVED AND REPLACED FDU 2 PER AMM 26-12-34-400-803-A AND 26-12-34-000-803-A. OPS CHECK GOOD. OK FOR SVC.

Part: CLAMP — BROKEN (RT A/C PACK) · airframe 45,204 hrs · 7,220 cycles

ETOPS - FOUND BAND CLAMP ON BELLOWS UP STREAM OF RH PACK BROKEN. REPLACED CLAMP AS NEEDED PER AMM 21-52-41-400-801-A. OK FOR SERVICE

Part: FIRE DETECTOR — FAULTED (NR 2) · airframe 45,198 hrs · 7,218 cycles

ETOPS - ENG 2 FIRE LOOP A FAULT. REMOVED AND REPLACED ENG 2 FDU PER AMM 26-12-34. OPS CHECK FAILED, CONDITION REMAINS. PERFORMED T/S OF ENG#2 FIRE LOOP A PER TSM 26-12-00-810-937-A. FOUND SHORT CIRCUIT FROM 3015VC TO ZONE 2 DETECTOR. REMOVED AND REPLACED HARNESS FROM 3015VC TO ZONE 2 DETECTOR PER ESPM 20-48-13 & AMM 71-51-05. REMOVED AND REPLACED ZONE 2 FIRE DETECTOR ASSEMBLY PER AMM 26-12-19. NO FAULTS FOUND.

Part: UNKNOWN — ODOR (CABIN) · airframe 45,199 hrs · 7,219 cycles

ATB - HEAVY DIRTY SMELL THROUGHOUT CABIN AND COCKPIT DURING TAKEOFF & CLIMB. HEAVY SMELL DURING LANDING IN AFT CABIN. ODOR LASTED ABOUT 34 MINUTES. FLT CREW DONNED OXYGEN MASK. PERFORMED SMOKE AND/OR OIL SMELL IN THE CABIN TROUBLE SHOOTING PER TSM 71-00-81-810-805-A. NO DEFECTS NOTED. NO 30 DAY HISOTRY. OK FOR SERVICE

Part: SEAL — BROKEN (OIL FILLER) · airframe 44,988 hrs · 7,186 cycles

ETOPS - ENG #2 FILLER #21 SEALS BROKEN. REPLACED ANNULUS FILLER PER AMM 72-31-41-400-802-A

Part: ACTUATOR — FAULTED (APU LP VALVE) · airframe 44,450 hrs · 7,105 cycles

ETOPS - BTB FUEL APU LP VALVE FAULT. REMOVED AND REPLACED APU LP VALVE ACTUATOR PER AMM 28-29-52. OPS CHECK GOOD. SECURITY CHECK GOOD. BTB AGAIN FOR SAME ISSUE. REMOVED AND REPLACED RELAY 6QF, NO CHANGE FAULT STILL ACTIVE AT SHUT DOWN.ECB RERACKED, FAULT CONTINUES, APU ISO VALVE STILL SHOWING OPEN WHEN SUPPOSED TO BE CLOSED. REMOVED AND REPLACED RELAY 6QF PER TSM 28-29-00 OPS CHECKED GOOD NO FAULTS NOTED OK FOR SERVICE.

Part: FAN — INOPERATIVE (ZONE 100) · airframe 44,308 hrs · 7,084 cycles

BULK CARGO VENT FAULT. DIV TO OAK. REMOVED AND REPLACED BULK CARGO EXTRACTION FAN PER AMM 21-28-53. OP CHK GOOD OK FOR SVC.

Part: A/C PACK — FAULTED (NR 2) · airframe 44,255 hrs · 7,073 cycles

ETOPS - PACK 2 REG FAULT. FAULT CODE 215352. REPLACED PACK 2 AIR OUTLET FLAP ACTUATOR AMM 215352. OK FOR SERVICE.

Part: CONTROL UNIT — FAULTED (NR 2 VSV) · airframe 43,957 hrs · 7,026 cycles

ETOPS - "BTB" DURING START #2 ENG ECAM "ENG 2 CTL SYST FAULT". REMOVED AND REPLACED #2 ENGINE VSV CONTROL UNIT PER AMM 75-33-51. LEAK AND OPS CHECK GOOD - OK FOR SERVICE.

Part: COUPLER — FAULTED (NR 2 HF COMMS) · airframe 43,755 hrs · 6,993 cycles

ETOPS - HF #2 DOES NOT TUNE. REMOVED AND REPLACED HF #2 COUPLER PER AMM 23-11-36. OPS TEST GOOD. OK FOR SERVICE.

Part: BRACKET — BROKEN (DRAIN LINE) · airframe 43,393 hrs · 6,939 cycles

ETOPS - UPON PERFORMING SCHEDULED TASK CARDS, DISCOVERED BROKEN DRAIN LINE BRACKET. REMOVED AND REPLACED DRAIN LINE BRACKET IN REF WITH AMM 72-00-41. SECURITY CHECK GOOD . A/C OK FOR SVC.

Part: EXCITER — FAULTED (APU) · airframe 43,383 hrs · 6,937 cycles

ETOPS - APU CLASS 2 FAULTS, IGNITION/EXCITER FAULTS ON PREVIOUS FLIGHT LEGS. REF:TSI 003228. TROUBLESHOT PER TSM 49-00-00-810-881-A. MAINT MESSAGE IGN PLUG (59KA31)/IGN EXCITER (59KA10) FAULT CODE 072 RECEIVED. REMOVED AND REPLACED 2EA UPPER.LOWER IGNITER PLUGS PER AMM 49-41-41-000-801A AND 49-41-41-400-801-A. PERFORMED GROUND SCAN. NO FAULTS DETECTED. OPS CHECK GOOD, AIRCRAFT OK FOR CONTINUED SERVICE. TSI 003228 UPDATED IN TRAX

Part: ACTUATOR — FAULTED (FUEL SYS) · airframe 43,218 hrs · 6,907 cycles

ETOPS - AFTER STARTING ENG 1 AT TYHE GATE WITH EXTERNAL AIR FUEL- AFT XFER FAULT RESET FCMC 1 AND 2 PER MOC AND MESSAGE CLEARED THEN RETURNED. REMOVED SMA FIN 501 QU IN SERVICEABLE COND. REMOVED & REPLACED SMA FIN 603QL1 WITH 501QU. REF. AMM 28-25-57-000-802

Part: FADEC — FAULTED (NR 1) · airframe 43,075 hrs · 6,884 cycles

ETOPS - BTB AFTER ENG #1 START FADEC 1 FAULT 2 START ATTEMPT AS PER MX FAULT REACURED. PERFORMED WIRING CHECKS PER AMM SUB TASK 77-11-00-810-210-A CONTINUITY CKS GOOD NO STORT TO GROUND INSULATION CK OF WIRES GOOD 6/28/24 8054 REPLACED OVERSPEED PROTECTION UNIT PER AMM 73-21-36 (4072KS) OPS CHECK GOOD

Part: CONTROL UNIT — FAULTED (NR 1 ENG VSV) · airframe 42,998 hrs · 6,872 cycles

ETOPS - ENG 1 CONTROL SYS FAULT ON ECAM PAGE. REMOVED AND REPLACED VSV CONTROL UNIT PER AMM 75-33-51 ON #1 ENG. VERIFICATION FLIGHT FOR #1 ENGINE EEC COMPLETED SATISFACTORILY.

Part: SLIDE — FAULTED (L2 & R2 DOORS) · airframe 42,993 hrs · 6,871 cycles

WHILE PERFORMING BITE TEST PER TASK CARD 330-335100-1 FOUND CLASS 1 FAULT (13WL AND 14 WL) FOR ESCAPE SLIDE LIGHT DOOR 2L AND 2R. REMOVED AND INSTALLED LH DOOR 2 SLIDE/RAFT ASSEMBLY PER AMM 25-62-42. REMOVED AND REPLACED RH DOOR 2 SLIDE RAFT ASSEMBLY PER AMM 25-62-42. SYS AND OPS TEST GOOD. FAULTS CLEARED OK FOR SERVICE.

Part: HANDSET — INTERMITTENT (INTERPHONE) · airframe 42,987 hrs · 6,870 cycles

ETOPS - 1R INTERPHONE INTERMITTENT. REMOVED AND REPLACED 1R HANDSET PER AMM 23-73-44. OK FOR SVC.

Part: CHECK VALVE — LEAKING (HYD SYSTEM) · airframe 42,475 hrs · 6,794 cycles

ETOPS - IN CRUISE @ FL380 ECAM HYD Y RSVR LO LVL HYD Y SYS LO PR ECAM ACTIONS FOLLOWED. YELLOW HYD QUANTITY INDICATING EMPTY. FOUND YELLOW HP MANIFOLD- SUPPLY CHECK VALVE LEAKING. REPLACED O-RING PER AMM 29-13-53-000-813-A. OPS AND LEAK CHECK GOOD. PERFORMED ENG #2 ENGINE RUN. OPS CHECK OF YELLOW EDP GOOD. NOTED BY MX, YELLOW RESERVOIR STILL HAD FLUID AND SYSTEM DID NOT CAVITATE. OK FOR SVC.

Part: LINE — UNKNOWN (FUEL TRIM) · airframe 41,788 hrs · 6,688 cycles

ETOPS - APU FAULT APU AUTO SHUT DOWN. PERFORMED AMM 28-27-53 OPS CHECK APU. REMOVED AND REPLACED FUEL TRIM PIPE ISOLATION-VALVE ACTUATOR. NO FAULT NOTED OK FOR SVC.

Part: HINGE FITTING — DAMAGED (COWL DOOR) · airframe 41,788 hrs · 6,688 cycles

WHILE OPENING IMBOARD(RIGHT) FAN COWL DOOR ON ENG 1 FOR ENGINE 1A CHECK, FOUND CRACK ON FAN COWL DOOR. SECONDARY STRUCTURE ON PYLON TO NACELLE STRUCTURE CRACKED 3.5" ON RIVET LINE. RH FAN COWL DOOR SECOND HINGE MOUNTING BOLT NUT/WASHER ASSEMBLY HAS WORN THROUGH AND ELONGATED HOLE. SECOND FWD MOUNTING BOLT FOUNBD DAMAGED. REMOVED ITEMS 96 AND 100 FROM FITTING #2 PER AIRBUS DRAWING F50534860-04. REMOVED RH FWD MOUNTING BOLTS. BROKE TORQUE ON ICU PER AMM 78-31-41-000-803-A.(REF LOG 1028150-1) REMOVED #2 FAN COWL BOLT PER AMM 71-13-92-802-A. REMOVED AND INSTALLED #2 HINGE FITTING PER DRAWING F5453527.

Part: BLEED VALVE — FAULTED (NR 1 ENGINE) · airframe 41,697 hrs · 6,674 cycles

ETOPS - AFTER LANDING ENG 1 HP VALVE NOT OPEN ECAM APPEARED UNTIL ENGINE SHUTDOWN. PERFORMED BITE TEST ON BMC 1, FAULTING HP BLEED-V. REMOVED AND REPLACED ENG #1 HP VALVE IN REF W/ AMM 36-11-51 OPS CHECK IDLE RUNON ENG #1 COMPLETE. OK FOR SVC.

Part: BLEED VALVE — FAILED (NR 2 ENGINE) · airframe 41,477 hrs · 6,641 cycles

ETOPS - AIR ENG 2 BLEED NOT-CLOSD REPEATED WRITE UP. MESSAGE EXTINGUISHED ON ARRIVAL #2 BLEED VALVE POSITION SHOWING CLOSED ON ECAM. DUE TO HISOTORY, REMOVED + REPLACED BMC 2 PER AMM 36-11-34. TEST OKAY. OK FOR SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,923 hrs · 6,559 cycles

ETOPS - ELEC IDG 2 OIL LO PR. ELEC C/B TRIPPED, GEN 2 FAULT. REMOVED AND REPLACED #2 IDG PER AMM 24-21-51. OPS OK, LEAK CHECK GOOD. OK FOR SERVICE

Part: WIRE — DAMAGED (FIRE DETECTION) · airframe 45,278 hrs · 7,232 cycles

ETOPS - ENG 2 FIRE LOOP A FAULT. WIRING CHECK AT FDU 2A CONNECTOR PIN J TO K 1.5K OHMS. J TO GND 1.5K OHMS. K TO GND 25.3 OHMS. AFTER DISCONNECTED 3015VCA READING CHANGED J TO GND 1.9K OHMS. K TO GND 29.3 OHMS. FOUND WIRE 3K001(B AND R)20 DAMAGED NEAR 3822VC2-A. REMOVED AND REPLACED WIRE PER AMM 70-71-24. OPS CHECK OK PER AMM 26-12-00.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,819 hrs · 6,542 cycles

ETOPS - POSSIBLE OIL LEAK ON #2 ENGINE. QTY DECREASING BY APPROX 1.5 QT/HR. FOUND #2 ENGINE PRESSURE OIL FILTER WITH WRONG PACKING INSTALLED. REMOVED AND INSTALLED NEW FILTER AND PACKING PER AMM 79-22-43. PRECAUTIONARY REMOVED AND REPLACED SCAVENGE OIL FILTER AND PACKING PER AMM 79-22-45. RAN #2 ENG - NO LEAKS NOTED. VERIFIED OIL QUANTITY DID NOT REACH ZERO. OIL QUANTITY SHOWED 8 ON SERVICING REPORT. OK FOR SVC

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,739 hrs · 6,528 cycles

ETOPS - IN CRUISE FLIGHT, WX/PWS SWITCH IN POSITION 2 SHOWED RED WX CTL MESSAGE ON NAV DISPLAY - INTERMITTENTLY. SWITCHED TO POSITION 1 - OPS NORMAL. REMOVED AND REPLACED WX RADAR CONTROL PANEL (3SQ). PERFORMED WX RADAR BITE TEST PER AMM 34-41-00. NO FAULTS, OK TO CONT. SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,323 hrs · 6,462 cycles

ETOPS - ECAM ENG1 OIL CHIP DETECTED AFTER LANDING. PERFORMED TSM 79-20-00-810-823-A. FOUND & COLLECTED MINISCUAL DEBRIS BRIDGING GAP. WILL SEND TO ENGINEERING. CHANGED SCAVENGE FILTER & INSPECTED. 79-00-00-200-804. NO DEBRIS FOUND. ENGINE RUN LEAK CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 39,882 hrs · 6,393 cycles

ETOPS - ECAM: HYD G RSVR LO AIR PR AFTER LANDING. T/S IAW TSM 29-11-00-810-806-A FOUND G RSVR AIR RELIEF VALVE FAULT. REPLACED. FUNCTIONAL TEST OK. LEAKAGE CHECK OK. HYDRAULIC FLUID SERVICED. A/C OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 39,712 hrs · 6,365 cycles

ATB - CREW REPORTING LIGHTNING STRIKE AND ENG2 STALL MSG, BUT REPORTS TO DISPATCH BOTH ENGS ARE OPERATIONAL. PER POWERPLANT ENGINEERING, MUST ACCOMPLISH ENG SURGE AMM TASK WHICH WILL REQUIRE A BORESCOPE. NO REPORTS OF ANY FINDINGS ON THE LIGHTNING STRIKE AND OVERWEIGHT LANDING INSPECTION. MX FOUND FUEL LINE SUPPORT BRACKET BROKEN. ATB LIGHTING STRIKE FOLLOWED BY BURNING SMELL. PERFORM PHASE ONE INSPECTION IAW AMM05-51-18-200-801-A NO DAMAGE FOUND. FOUND CRACK IN MAIN FUEL LINE SUPPORT BRACKET ON ENG #2 DURING BORESCOPE PROCEDURE. REMOVED AND REPLACED FUEL LINE SUPPORT BRACKET IAW AMM72-00-41-400-804 OPERATIONAL CHECK OK NO LEAKS NOTED. A/C OK TO CONTINUE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 39,504 hrs · 6,331 cycles

ETOPS - ENG 2 ADVISORY VIB N1 IN CLIMB FL380 VIB N1 - 5.7 VIB N2 - 0.6 VIB N3 - 0.7 N1 - 87% N3 - 90.1% EGT 700 DEG C IN CRUISE OK. REMEOVED/REPLACED #2 ENG FAN BLADE SET AND APPLIED DRY FILM LUBE PER T/C: E1128-330-77-001 WO#265361. PERFORMED TEST 11 ENG VIBE SURVEY RESULTS (0.9 N1) W/IN LIMITS. OK TO CONT ON DMI 529232 (#2 ENGINE UNDERWENT FAN BLADE LUBE AND MAY EXPIERENCE HIGHER THAN NORMAL VIBES.) .

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 37,943 hrs · 6,089 cycles

DURING C CK, THE RHW RIB 6 FITTING FWD LUG WAS FOUND CORRODED. RH WING MLG RIB 6 FWD LUG, FWD SPT FACE FOUND CORROSION BEYOND WORK CARD, TO CARRY OUT CORROSION REMOVAL. CORRECTIVE ACTION: NEW OVERSIZE BUSHES WERE MANUFACTURED AND INSTALLED IN ACCORDANCE WITH R575-58471 ISSUE E AS WELL AS THE TR TO ALLOW FOR THE USE OF A PREVIOUS REVISION OF THE SERVICE BULLETIN.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 37,943 hrs · 6,089 cycles

SHIP 393 DURING CCK AT SIAEC (SIN), THE LHW RIB 6 FITTING FWD AND AFT BORES WERE FOUND CORRODED. NEW BUSHES WERE MANUFACTURED AND INSTALLED. THIS WAS COMPLETED IAW REFERENCE REPAIR INSTRUCTIONS (R575-58471 ISSUE E)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 37,203 hrs · 5,952 cycles

SHIP 393 FLOOR STRIP PANEL IN F/C FRONTING STOWAGE F104 & F105 IS DEFECTIVE (PEELING OFF). CORRECTIVE ACTION: RESECURED FLOOR STRIP AT F/C AREA. (9792680)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,943 hrs · 6,089 cycles

SHIP 393 HAL 393 EXPERIENCED SEVERE TURBULENCE EVENT WHICH CAUSED DAMAGE TO THE WALLS AND CEILINGS OF LAV H (L53) AND LAV V (L81) (REFERENCE ER/A 605060-14 FOR TIME LIMITED REPAIRS). THE OEM FOR BOTH DISCREPANT LAVATORIES IS DIEHL AVIATION. DIEHL PROVIDED TN-TK0295 ISSUE 04 TO PERMANENTLY REPAIR THE DAMAGE TO LAVATORY L53 AND L81 AND AIRBUS PROVIDED RDAF APPROVAL. SECTION I OF THIS ER/A GIVES INSTRUCTIONS TO PERMANENTLY REPAIR DAMAGE LAV H (L53) AND LAV V (L81) BASED ON THE SUBJECT DIEHL TN REPAIR SCHEME. CORRECTIVE ACTION: ASSOCIATED ER/A CHANGED FROM 14-605060 TO 14-605061. REF ER/A 605061-14AD. (2588446)

Part: DEU — INOPERATIVE (CABIN PRESSURE) · airframe 36,306 hrs · 5,796 cycles

SHIP 393 2L CABIN PRESSURE LIGHT INOP DUE TO DEU B INOP AT 2L STATION. OK TO CONTINUE PER MEL 52-71-1H. CORRECTIVE ACTION: REMOVED AND REPLACED DEU B FIN (300RH3) PER AMM 23-73-47. (9752241)

Part: NONE — NONE · airframe 36,130 hrs · 5,764 cycles

SHIP 393 - ATB - THS WHEEL MOVES ERRATICALLY AND FAST WHEN AUTOPILOT IS ON. WHEN AUTOPILOT IS OFF, TRIM FEELS NORMAL. CORRECTIVE ACTION: "FCPC 1 (2EC1) PITCH TRIM ACT (1CS) OVERRIDE SWITCH" FAULT ON PFR. T/S. REMOVED AND REPLACED PITCH TRIM ACTUATOR. OPS CHECKED. (7273861)

Part: NONE — NONE · airframe 35,768 hrs · 5,696 cycles

ETOPS - PER MOC GVI OF APU COMPARTMENT NEEDED DUE TO OIL SMELL, REF LOG PAGE 7732245 & 7732248. CHECK FOUND OIL LEAKING FROM FWD DRAIN MAST. REPLACED SEAL BETWEEN FUEL CONTROL UNIT AND OIL PUMP UNIT. LEAK CHECK OK. OK FOR SERVICE.

Part: NONE — NONE · airframe 35,574 hrs · 5,663 cycles

SHIP 393 2L DOOR SLIDE PRESSURE IN YELLOW ZONE. CORRECTIVE ACTION: OPERATED DOOR AND ARMED SLIDE. COULD NOT DUPLICATE FAULT. (9335902)

Part: NONE — NONE · airframe 34,912 hrs · 5,542 cycles

SHIP 393 1L DOOR INTERMITTENT. CORRECTIVE ACTION: NO LAST LEG FAULTS OR CURRENT FAULTS ON PSCU. 1L DOOR OPERATION/ INDICATION OK. (9317657)

Part: NONE — NONE · airframe 33,897 hrs · 5,368 cycles

ETOPS - FUEL R STBY PUMP CB A11 TRIPPED// REMOVED AND REPLACED RH FUEL STBY PUMP PER AMM 28-21-51. LEAK CHECK OK. OPS CHCEK GOOD. PUMP, FUEL, AD; OFF 33-2822-9-0007 S/N 05409 ON 33-2821-9-0003 S/N 03972

Part: NONE — NONE · airframe 33,502 hrs · 5,304 cycles

NEED TO REPLACE EEC DUE TO MCC REQUEST (MULTIPLE MINOR FAULTS) #1 ENGINE // REMOVED AND REPLACED #1 ENGINE EEC PER AMM 73-21-34 AWAITING CAT 3 AUTOLAND TEST PAUL JOHNSON 2172396 31JAN22 PERFORMED CAT 3 CAPABILITY TEST PER MM 22-97-00 ALL TESTS PASS NO FAULT NOTED OK FOR SVC 434937 CONTROL, ENGINE OFF 33-7321-9-0004 S/N 91116 ON 33-7321-9-0004 S/N 91685

Part: GENERATOR — DEFECTIVE · airframe 33,374 hrs · 5,283 cycles

ETOPS - APU GEN FAULT BEFORE ENGINE START // PERFORMED FIM 24-20-00-810-985-A. REMOVED AND REPLACED APU GEN PER AMM UP TO STEP 4. C. 3. SIGNED 2069773 01/19/2022 INSTALLED INLET AND PERFORMED LEAK/OPS CHECK REF AMM 24-23-51-400-801-A FROM STEP 4.C.3. NO DEFECTS NOTED. GENERATOR, APU, OFF 33-2423-9-0001 04193 ON 33-2423-9-0001 04919

Part: CONTROLLER — INOPERATIVE · airframe 33,197 hrs · 5,255 cycles

ATB - AFTER T/O ENG 2 CTL SYS FAULT AIR TURN BACK AVOID RAPID THR CHANGES // PERFORMED WIRE CHECKS PER TSM 75-33-00-810-808-A. WIRES CHECKS GOOD NO FAULTS FOUND 12/30/21 MECH 634066PER TSM 75-33-00-810-808A. REMOVED AND REPLACED #2 VENG VSV CONTROL UNIT PER AMM 75-33 -51 LEAK CHECK OK NO DEFECTS NOTED. PERFORMED HIGH POWER RUN PER AMM 71-00-00-700-827-A. OPS CHECK GOOD 1/1/22 MECH 1269276 CONTROL, VARIAB OFF 43-7533-9-0001 S/N 75251 ON 43-7533-9-0001 S/N 75714

Part: VALVE — INOPERATIVE · airframe 33,115 hrs · 5,238 cycles

ETOPS - ON DESCENT AMBER A ICE L INR WING HI PR ON ECAM DISPLAY // REPLACED L/W INNER (10DL1) WING ANTI ICE VALVE PER AMM 30-11-51. OPS CK OK.A/C OK FOR SVC. VALVE, ANTI-ICE OFF 33-3011-9-0001 S/N 12050 ON 33-3011-9-0001 S/N 08016

Part: DOOR — DAMAGED · airframe 33,015 hrs · 5,223 cycles

SHIP 393 DAMAGE FOUND ON FWD CARGO DOOR. FWD PANEL 821AR. CORRECTIVE ACTION: REWORKED FWD CARGO DOOR PANEL 821AR PER SRM 52-31-00. INSTALLED. (8447327)

Part: NONE — NONE · airframe 32,799 hrs · 5,181 cycles

SHIP 393 DENT DAMAGE NEXT TO THE L2 DOOR DUE TO A TOWING IMPACT. THE DENT IS IN THE SKIN AT STR 28L/FR32. STRINGER 28L IS ALSO VISIBLY DISTORTED. IT IS LOCATED 2.2" FWD OF FR31, WHICH IS AT A BUTT SPLICE. THE DAMAGE IS BEYOND ALLOWED LIMITS. CORRECTIVE ACTION: ACCOMPLISHED HFEC INSPECTION AT DAMAGED AREA. NO CRACKS NOTED. FOUND GOUGE . BLENDED GOUGE TO SMOOTHEN. HFEC PERFORMED, CONFIRMED NO CRACKS/HOLES. ACCOMPLISHED ER/A 595279-14. (7742704)

Part: NONE — NONE · airframe 32,779 hrs · 5,179 cycles

SHIP 393 FIRST CLASS GALLEY FLOOR LUMINOUS STRIP IS LOOSE. CORRECTIVE ACTION: SECURED LOOSE STRIP. (7716877)

Part: SLIDE — NO TEST (L2 DOOR) · airframe 32,239 hrs · 5,093 cycles

SHIP 393 UPON ACCOMPLISHING 1L DOOR SLIDE SCHEDULED REPLACEMENT, PERFORMED EPSU SYS TEST AND FOUND "ESCAPE SLIDE LT SW/EPSU (13WL ) DOOR 2 FAULT". CORRECTIVE ACTION: PERFORMED TSM TASK 25-62-00. FOUND 7910MS SLIDE/RAFT DOOR 2 LH BAD. REPLACED 2L DOOR SLIDE. (7274989)

Part: DISPLAY — FAULTED (MAIN) · airframe 32,250 hrs · 5,095 cycles

ETOPS - THIRD (CENTER) MCDU BACKLIGHT IS VERY DIM ON BRIGHTEST SETTING // REMOVED AND REPLACED THIRD MCDU PER AMM 22-82-12. OPS CHECK OK. OK FOR SERVICE UNIT, DISPLAY, OFF P/N 33-2282-9-0003 S/N 49347 ON P/N 33-2282-9-0003 S/N 05685

Part: UNKNOWN — UNKNOWN (R4 DOOR) · airframe 32,161 hrs · 5,083 cycles

SHIP 393 DOOR 4R DISARM HANDLE WILL NOT MOVE TO DISARM POSITION. CORRECTIVE ACTION: OPS CHECK MOVEMENT OF 4R ARM/DISARM HANDLE. NO DEFECTS NOTED. FAP AND ECAM INDICATIONS NORMAL. (7274938)

Part: LEVER — FAULTED (R4 DOOR) · airframe 32,161 hrs · 5,083 cycles

SHIP 393 4R DOOR ARMING LEVER IS NOT MOVING TO THE FULL DISARM POSITION. PERFORMED OPERATIONAL CHECK OF 4R DOOR IAW AMM 52-13-00. NO FAULTS NOTED. OK TO CONTINUE. ARMING LEVER FUNCTIONS CORRECTLY.

Part: DISPLAY — DEFECTIVE (COCKPIT) · airframe 31,287 hrs · 4,957 cycles

ETOPS - MCDU #3 INTERMITTENTLY LOSES POWER & BLANKS OUT. WHEN IT HAPPENS, ATSU ON OTHER MCDUS INOP. // REMOVED AND REPLACED #3 MCDU PER AMM 22-82-12-400-801-A. OPS CHK GOOD. UNIT, DISPLAY, OFF 33-2282-9-0003 14214 ON 33-2282-9-0003 49347

Part: SKIN — CORRODED (FUSELAGE) · airframe 31,193 hrs · 4,943 cycles

SHIP 393 FUSELAGE SKIN CORRODED AT LWR SIDE OF AFT LAV FWD EXHAUST PORT. CORRECTIVE ACTION: BLENDED AND CHECKED LIMITS PER A330 SRM 53-41-11. REMOVED CORROSION. REMOVED .008. REMAINING SKIN THICKNESS IS .090 WITHIN LIMITS PER A330 SRM 53- 41-11. PERFORMED UT. PRIMED, AND PAINTED AREA. (1783501)

Part: SKIN — CORRODED (FUSELAGE) · airframe 31,193 hrs · 4,943 cycles

SHIP 393 LWR FUSELAGE- FUSELAGE SKIN CORRODED AT LWR SIDE OF AFT LAV AFT EXHAUST PORT. CORRECTIVE ACTION: REMOVED .022 MATERIAL REMAINING SKIN THICKNESS IS .076 WITHIN LIMITS PER A330 SRM 53-41-11. PERFORMED UT. TREATED, PRIMED, AND PAINTED AREA.(1783498)

Part: DOOR — OBSTRUCTED (R4 DOOR) · airframe 31,147 hrs · 4,936 cycles

SHIP 393 4R DOOR DIFFICULT TO DISARM. CORRECTIVE ACTION: REMOVED DEBRIS. (7261048)

Part: LEVER — INOPERATIVE (DOOR ARMING) · airframe 31,027 hrs · 4,915 cycles

SHIP 0393 4R ARMING LEVER INOP. CORRECTIVE ACTION: CHECKED 4R ARMING LEVER FOR DEBRIS AND EASE OF MOVEMENT. COULD NOT REPLICATE FAULT. (7249422)

Part: PITOT TUBE — CLOGGED · airframe 30,989 hrs · 4,910 cycles

ATO - RTO FOR NO AIRSPEED INDICATION ON CAPT PFD. MAX SPD INDICATION FROM FO PFD WAS APPROX. 80 KTS // PITOT PROBE #1 (9DA1) CLOGGED. REMOVED AND REPLACED PROBE #1 PER AMM 34-11-15. #1 PHC OPS TEST GOOD. FLUSHED TOTAL PRESSURE LINE PER AMM 34-11-00. DATA GATHERED PER TASK CARD 3131-7002-HAL AND 3411-7002-HAL. FWD TO HA ENGINEERING. OK FOR SERVICE. PROBE, PITOT, R OFF 33-3411-9-0004 39939 ON 33-3411-9-0004 39653.

Part: BOTTLE — LOW PRESSURE (R3 DOOR ASSIST) · airframe 30,973 hrs · 4,907 cycles

SHIP 0393 3R DOOR ASSIST BOTTLE LOW PRESSURE. CORRECTIVE ACTION: RECHARGED DOOR 3R DAMPER AND EMERGENCY OPERATION CYLINDER PER A330 AMM 52-10. (7269966)

Part: CYLINDER — LOW PRESSURE (R3 DOOR ASSIST) · airframe 30,838 hrs · 4,889 cycles

EMERGENCY EQUIPMENT, 3R DOOR EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED 3R DOOR EMERGENCY OPERATION CYLINDER, PER A330 AMM 52-10-00. OPERATIONS CHECKS GOOD. REQUIRED INSPECTION ITEMS COMPLETED 794859 QC2009.

Part: APU — ODOR · airframe 30,433 hrs · 4,819 cycles

ODOR/FUMES OIL SMELL IN CABIN AND FLIGHT DECK. REMOVED & REPLACED APU. OPERATIONS & LEAK CHECK OK. NO ODOR PRESENT IN CABIN & FLIGHT DECK. APU, AUXILIARY OFF 43-4910-9-0010 01519 ON 43-4910-9-0010 01780.

Part: FMU — LEAKING (NR 2 ENGINE) · airframe 30,425 hrs · 4,816 cycles

ETOPS SIGNIFICANT SYSTEM, FUEL LEAKING FROM NR 2 ENGINE DRAIN MAST. MECHANIC FOUND LEAK COMING FROM FMU LINE. LINE DISCONNECTED FOR PARKING. RECONNECTED FMU LINE PER AMM 73-21-52-400-802-A. REMOVED AND REPLACED THE NR 2 ENGINE FMU IAW AMM 73-21-52-400-802-A. COMPLETED ALL STEP UP TO 5.D. LEAK TESTED OK IAW AMM 71-00-00-700-827A.

Part: CONTROL VALVE — MALFUNCTIONED (CABIN TEMP) · airframe 30,425 hrs · 4,816 cycles

ETOPS SIGNIFICANT SYSTEM, PACK 1 TEMP CONTROL VALVE ECAM MSG. REPLACED PACK 1 TEMP CONTROL VALVE IAW AMM 21-53-53-400-801A. OPS CHECKED OK.

Part: COVER — MISSING (TE FLAP) · airframe 30,095 hrs · 4,768 cycles

OPEN - LEFT HAND WING FIXED FLAP FAIRING #5 MISSING FWD MOST COVER. // AWAITING PARTS. REPLACED MISSING FLAP FAIRING COVER. SECURITY CHK OK.

Part: OIL FILTER — CLOGGED (NR 1 ENGINE) · airframe 29,782 hrs · 4,713 cycles

ETOPS SIGNIFICANT SYSTEM - DURING DESCENT BELOW 12000 FEET ECAM MESSAGE ENG 1 OIL FILTER CLOG. // REMOVED & REPLACED #1 ENGINE OIL FILTER PER A330 AMM 79-22 NO DEBRIS FOUND A/C OK FOR SVC

Part: APU — FAULTED · airframe 28,049 hrs · 4,461 cycles

ETOPS SIGNIFICANT SYSTEM - APU FAULT, AUTO SHUTDOWN. NO FAULTS SHOWN ON PFR OR PREVIOUS FLY LEGS, TROUBLESHOT IAW TSM 49-62-00-810-870A APU OPERATION NORMAL. C/W OPS TEST OF AIR INTAKE FLAP IAW AMM 49-16-51-710-802A, OPS TEST NORMAL NO PREVIOUS SHUTDOWN FAULTS OK FOR SERVICE.

Part: EXCITER — FAILED (APU) · airframe 27,948 hrs · 4,443 cycles

AIRCRAFT FAILED APU COLD SOAK START 3 ATTEMPTS AT OAT -56, -50, -30, FL 400, 350, 270. REPLACED IGNITION EXCITER.

Part: EXCITER — FAULTY (APU) · airframe 27,948 hrs · 4,443 cycles

ETOPS SIGNIFICANT SYSTEM - APU INFLIGHT START OAT - -56 -51 -30 FL 400 350 270 # ATTEMPTS - 3 UNSUCCESSFUL. // R/R APU EXCITER PER A330 AMM 49-41 AND SYSTEM A IGNITER AND LEAD R/R PER A330 AMM 49-41. OPT CHK NML.

Part: LINER — DAMAGED (NR 1 ENGINE) · airframe 27,802 hrs · 4,419 cycles

OPEN - ETOPS SIGNIFICANT SYSTEM - NR 1 ENGINE ATTRITION LINER DAMAGED. ACFT TO MX FERRY FOR REPAIRS.

Part: ACTUATOR — INOPERATIVE (FUEL SYSTEM) · airframe 27,160 hrs · 4,315 cycles

ETOPS SIGNIFICANT SYSTEM - RT WING FUEL TANK OUTER INLET VALVE ACTUATOR INOP. REPLACED RT WING OUTER TANK INLET VALVE ACTUATOR FIN # 500QU2 PER AMM 28-25-57-400-801-A. OPS CHECK OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 26,449 hrs · 4,207 cycles

ETOPS SIGNIFICANT SYSTEM - ELECTRIC APU BAT SYSTEM FAULT ECAM. // T/S PER REF 24-30-00-810-833A. PERFORMED BCL APU TEST. NO FAULTS FOUND DURING TEST. A/C OK FOR SVC.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 26,326 hrs · 4,187 cycles

ETOPS SIGNIFICANT SYSTEM - FUEL CTR TO INNER FAULT ILLUMINATED IN CRUISE WITH CENTER FUEL TANK QUANTITY ZERO. FUEL AFT XFR ALSO SHOWN ON STATUS PAGE BUT CLEARED ITSELF. PREVIOUS HISTORY WITH LT INR TK INLET VLV T/S PER TSM 28-26-00. TRANSFER CK OK. BITE TEST OF FCMC 1/2 OK. NO ACTIVE ECAM FAULT. OK FOR SERVICE.

Part: PANEL — DAMAGED (CARGO BAY) · airframe 26,280 hrs · 4,179 cycles

ETOPS SIGNIFICANT SYSTEM - RAMP REPORTED DAMAGES IN AFT CARGO ON PANEL 41P. DAMAGE MEASURES 3IN X .25IN AND 1.5IN X.25IN. PERFORMED SPEED PATCH REPAIR PER AMM 25-53-00-00-801-A. A/C OK FOR SVC.

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 26,198 hrs · 4,166 cycles

ETOPS SIGNIFICANT SYSTEM - ONCE ON GROUND AND INFLIGHT HOT AIR 2 TRIM AIR VALVE CLOSED AUTOMATICALLY. AMBER LINE FROM VALVE TO MANIFOLD ON COND PAGE. X BLEED VALVE OPENED. RESET ZONE CONTROLLER. PERFORMED BITE TEST CAB TEMP ECS PER AMM 21-63-00. OPS TEST PASSED. NO FAULTS NOTED OK FOR SVC.

Part: OIL COOLER — LEAKING (RT ENGINE) · airframe 25,723 hrs · 4,101 cycles

ETOPS - DURING H1 CHECK IN BNE FOUND R/H ENGINE AIR OIL COOLER HAS EVIDENCE OF OIL LEAKAGE FROM HEAT EXCHANGER AIR MATRIX // ENGINE AIR OIL COOLER REPLACED IAW A330 AMM 79-21-51 FUEL AND OIL LEAK TEST CARRIED OUT IAW A330 AMM 71-00-00 - NIL LEAKS. COOLER, OIL-AIR OFF 43-7921-9-0001 41178 ON 43-7921-9-0001 41498

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · corrosion level 2 · airframe 25,723 hrs · 4,101 cycles

SEAT TRACK BETWEEN FRAME 53.2 AND 54.5 AT -Y1959 IS CORRODED AT LOCATIONS: FR53.5+10", FR53.2 +5", FR53.5+16". // CORROSION REMOVED AS PER SRM 51-74-00 REV 98.01. CORROSION AT LOCATIONS FR53.5+10?, FR53.2+5?, FR53+16? DAMAGE LOCATED IN THE INNER VERTICAL AREA OF THE SEAT TRACK CROWN, DUE TO RESTRICTED ACCESS UNABLE TO FULLY REMOVE CORROSION OR MEASURE THE DAMAGE DEPTH. ASSESSED AS UNSERVICABLE AS PER SRM 53-00-15 REV 98.01. RII CARRIED OUT AS PER HAL GMM VOL 1 CHAP 5. CONFIRMED AS LEVEL 2 CORROSION, PART REPLACEMENT REQUIRED. SEAT TRACK ASSEMBLY REPLACED AS PER SRM 51-72-11 REV 98.01 AND AIRBUS DRAWING F53326941 ISSUE A. JOB COMPLETE.

Part: SEAT TRACK — CORRODED (FRAMES 54-58) · corrosion level 2 · airframe 25,723 hrs · 4,101 cycles

SEAT TRACK BETWEEN FRAME 54 AND 58 AT -Y1959 IS CORRODED AT LOCATIONS: FR57+12". // CORROSION REMOVED AS PER SRM 51-74-00 REV 98.01. CORROSION LOCATED AT FR57+12? DAMAGE LOCATED IN THE INNER VERTICAL AREA OF THE SEAT TRACK CROWN, DUE TO RESTRICTED ACCESS UNABLE TO FULLY REMOVE CORROSION OR MEASURE THE DAMAGE DEPTH. ASSESSED AS UNSERVICEABLE AS PER SRM 53-00-15 REV 98.01. RII CARRIED OUT AS PER HAL GMM VOL 1 CHAP 5. CONFIRMED AS LEVEL 2 CORROSION, PART REPLACEMENT REQUIRED. SEAT TRACK ASSEMBLY REPLACED AS PER SRM 51 -72-11 REV 98.01 AND AIRBUS DRAWING F53476200 ISSUE S. JOB COMPLETE.

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · corrosion level 2 · airframe 25,712 hrs · 4,099 cycles

DURING H CHECK, SEAT TRACK BETWEEN FR 53.2-54.5 , -Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53326941. LP 1017000

Part: PROFILE — CORRODED (VERTICAL STAB TE) · corrosion level 2 · airframe 25,712 hrs · 4,099 cycles

DURING H CHECK, VERTICAL STAB TRAILING EDGE RIGHT HAD SIDE VERTICAL PROFILE ABOVE NBR 2 T CHORD FOUND CORRODED. REPLACED CHORD TO VERTICAL STAB TRAILING EDGE PER SRM 51-42-11 AND AIRBUS DRAWING F55371707. LP 1017034

Part: SEAT TRACK — CORRODED (FRAMES 54-58) · corrosion level 2 · airframe 25,712 hrs · 4,099 cycles

DURING H CHECK, SEAT TRACK BETWEEN FR 54-58, -Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53476200. LP 1017007

Part: TEE FITTING — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 25,723 hrs · 4,101 cycles

VERTICAL STAB TRAILING EDGE RHS #2 T CHORD SUSPECT CORROSION AROUND FASTENER HOLES. #2 RHS VERT FIN T/E T-CHORD CORROSION BLENDED BEYOND LIMITS IAW HAL A330 SRM 51-74-00 REV 98.01. CHORD REPLACED IAW HAL A330 SRM 51-42-11, REV 98.01 AND AIRBUS DWG F553 71707, ISSUE P. JOB NOW COMPLETE.

Part: SEAT TRACK — CORRODED (FRAMES 54-58) · corrosion level 2 · airframe 25,712 hrs · 4,099 cycles

DURING H CHECK, SEAT TRACK BETWEEN FR 54-58, -Y450 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53476200. LP 1015421

Part: SEAT TRACK — CORRODED (FRAMES 58-62) · corrosion level 2 · airframe 25,712 hrs · 4,099 cycles

DURING H CHECK, SEAT TRACK BETWEEN FR 58-62, +Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F534772112040. LP 1015425

Part: SEAT TRACK — CORRODED (FRAMES 58-62) · corrosion level 2 · airframe 25,723 hrs · 4,101 cycles

SEAT TRACK BETWEEN FRAME 58 AND 62 AT +Y1959 IS CORRODED AT LOCATIONS: FR58+20", FR60+9", FR61+20". // CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR58+20" SUPERIOR L=1.0" W=0.500" DEPTH=0.038", FR60+9" CORROSION SPREAD TO INNER VERTICAL WALL AREA, UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS, FR61+20", SUPERIOR L=1.5" W=0.700" DEPTH= 0.030". GAUGE PN: 07852307, SN: TCN51487 AND PN: 2417, SN: IRFE5005A933. ASSESSED AS OUTSIDE OF SRM 53-00-15 REV 98.01 LIMITS. RII CARRIED OUT AS PER HAL GMM VOL1 CHAP 5 - CONSIDERED LEVEL 2 CORROSION, PART REPLACEMENT REQUIRED. SEAT TRACK REPLACED AS PER SRM 51-72-11 REV 98.01 WITH TRACK P/N F5347721120400 AND AIRBUS DWG F53477040 ISSUE H. JOB COMPLETE.

Part: SEAT TRACK — CORRODED (FRAMES 54-58) · corrosion level 2 · airframe 25,723 hrs · 4,101 cycles

SEAT TRACK BETWEEN FRAME 54 AND 58 AT -Y450 IS CORRODED AT LOCATIONS: FR56+4", FR56+18", FR57+14", FR57+16". // CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR56+4", FR56+18", FR57+14", FR57+16". CORROSION LOCATED ON INNER VERTICAL WALL AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS. ASSESSED AS OUTSIDE OF SRM 53-00-15 REV 98.01 LIMITS. RII CARRIED OUT AS PER HAL GMM VOL1 CHAP 5 - CONSIDERED LEVEL 2 CORROSION, PART REPLACEMENT REQUIRED. SEAT TRACK REPLACED AS PER SRM 51-72-11 REV 98.01 AND AIRBUS F53476200 ISSUE S. JOB COMPLETE.

Part: SEAT TRACK — CORRODED (FRAMES 58-62) · corrosion level 2 · airframe 25,712 hrs · 4,099 cycles

DURING H CHECK, SEAT TRACK BETWEEN FR 58-62, -Y2462 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53477040. LP 1013982

Part: SEAT TRACK — CORRODED (FRAMES 54-58) · corrosion level 2 · airframe 25,712 hrs · 4,099 cycles

DURING H CHECK, SEAT TRACK BETWEEN FR 54-58, +Y450 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53476200. LP 1013984

Part: FLOOR SUPPORT — CORRODED (FRAME 76) · corrosion level 2 · airframe 25,712 hrs · 4,099 cycles

DURING H CHECK, AFT CABIN FLOOR STRUCTURE LONGERON AT FR 76, -Y445 FOUND CORRODED. REPLACED LONGERON PER SRM 51-72-11 AND AIRBUS DRAWING F53478040. LP 1013979

Part: TEE FITTING — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 25,712 hrs · 4,099 cycles

DURING H CHECK, VERTICAL STAB TRAILING EDGE RIGHT HAD SIDE VERTICAL PROFILE ABOVE NBR 3 T CHORD FOUND CORRODED. REPLACED CHORD TO VERTICAL STAB TRAILING EDGE PER SRM 51-42-47 AND AIRCRAFT DRAWING F55371707. LP 1013986

Part: FLOOR SUPPORT — CORRODED (FRAME 76) · corrosion level 2 · airframe 25,723 hrs · 4,101 cycles

AFT CABIN FLOOR STRUCTURE LONGERON AT FR76 -Y445 HAS SUSPECT CORROSION. // CORROSION REMOVED AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: L=1.000? W=0.600? DEPTH=0.110? (FULL THICKNESS). DEPTH GAUGE USED P/N: 2417 S/N: IRFE5005A9EQ. ASSESSED AS OUTSIDE OF SRM 53-41-14 REV 98.01 LIMITS. RII CARRIED OUT AS PER HAL GMM VOL 1 CHAP 5. CONFIRMED AS LEVEL 2 CORROSION, PART REPLACEMENT REQUIRED. LONGERON REPLACED AS PER SRM 51-72-11 REV. 98.01 AND AIRBUS DRAWING F53478040 ISSUE D. JOB COMPLETE.

Part: SKIN — CORRODED (VERTICAL STAB) · airframe 25,723 hrs · 4,101 cycles

VERTICAL STAB TRAILING EDGE RHS #3 T CHORD SUSPECT CORROSION AROUND FASTENER HOLES. // REMOVAL OF CORROSION CARRIED OUT IAW HAL A330 SRM 51-74-00 REV 98.01. CORROSION STILL EVIDENT IAW HAL A330 NTM 51-10-02-221-001-A REV 96. BLEND DEPTH OF .054" IS BEYOND 50% MATERIAL THICKNESS REPAIR BY REPLACEMENT REQUIRED. COMPLETED INSTALLATION OF NEW T CHORD .A.W. A330 SRM 51-21-00, 51-46-11, 51-76-11, 51-42- 11, REV 98.01. CORROSION REPORTED AS LEVEL 2, IAW TOPP 20-50-20.

Part: SEAT TRACK — CORRODED (FRAMES 54-58) · corrosion level 2 · airframe 25,723 hrs · 4,101 cycles

SEAT TRACK BETWEEN FRAME 54 AND 58 AT +Y450 IS CORRODED AT LOCATIONS: FR56, FR57+16", FR57+18". // CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR56, FR57+16", FR57+18". CORROSION LOCATED ON INNER VERTICAL WALL AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS. ASSESSED AS OUTSIDE OF SRM 53-00-15 REV 98.01 LIMITS. RII CARRIED OUT AS PER HAL GMM VOL1 CHAP 5 - CONSIDERED LEVEL 2 CORROSION, PART REPLACEMENT REQUIRED. SEAT TRACK REPLACED AS PER SRM 51-72-11 REV 98.01 AND AIRBUS F53476200 ISSUE S. JOB COMPLETE.

Part: TEE FITTING — CORRODED (VERTICAL STAB) · airframe 25,723 hrs · 4,101 cycles

VERTICAL STAB TRAILING EDGE RT NR 3 TEE FITTING CORRODED AROUND FASTENER HOLES. REMOVAL OF CORROSION CARRIED OUT IAW SRM 51-74-00, REV 98.01. CORROSION STILL EVIDENT IAW NTM 51-10-02-221-001-A REV 96. BLEND DEPTH OF .054" IS BEYOND 50% MATERIAL THICKNESS. REPAIRED BY REPLACEMENT. COMPLETED INSTALLATION OF NEW TEE FITTING IAW SRM 51-21-00, 51-46-11, 51-76-11, 51-42-11, REV 98.01. CORROSION REPORTED AS LEVEL 2, IAW TOPP 20-50-20.

Part: TEE FITTING — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 25,712 hrs · 4,099 cycles

DURING H CHECK, VERTICAL STAB TRAILING EDGE RIGHT HAD SIDE VERTICAL PROFILE ABOVE NBR 3 T CHORD FOUND CORRODED. REPLACED CHORD TO VERTICAL STAB TRAILING EDGE PER SRM 51-21-00, 51-46-11, 51-76-11, AND 51-42-11. LP 1013988

Part: SEAT TRACK — CORRODED (FRAMES 58-62) · corrosion level 2 · airframe 25,723 hrs · 4,101 cycles

SEAT TRACK BETWEEN FRAME 58 AND 62 AT -Y2462 IS CORRODED AT LOCATIONS: FR59, FR60+7.5", FR60+9", FR62. // CORROSION REMOVED AS PER SRM 51-74-00 REV 98.01. DAMAGE AT LOCATIONS FR59", FR60+7.5", FR60+9", FR62" ALL CORROSION LOCATED IN THE INNER VERTICAL PART OF THE CROWN. UNABLE TO FULLY REMOVE THE CORROSION OR MEASURE THE DEPTH. ASSESSED AS OUTSIDE OF SRM 53-00-15 REV 98.01 LIMITS. RII CARRIED OUT AS PER HAL GMM VOL CHAP 5. CONFIRMED AS LEVEL 2 CORROSION PART REPLACEMENT REQUIRED. SEAT TRACK ASSEMBLY REPLACED AS PER SRM 51-72-11 REV 98.01 AND AIRBUS DRAWING F53477040 ISSUE H. JOB COMPLETE.

Part: SEAT TRACK — CORRODED (FRAMES 26-37) · corrosion level 2 · airframe 25,723 hrs · 4,101 cycles

SEAT TRACK BETWEEN FRAME 26 AND 37.4 AT -Y450 IS CORRODED AT LOCATIONS: FR34, FR37+15". // CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR34 SUPERIOR REWORK L: 1" W: 0.5" D: 0.030", FR37(+15") LATERAL REWORK L: 0.5" W: 0.2" D: 0.034". DIAL INDICATOR P/N 2417 S/N IRFE5005A9EQ. ASSESSED AS OUTSIDE OF SRM 53-00-15 REV 98.01 LIMITS.RII CARRIED OUT AS PER HAL GMM VOL1 CHAP 5 - CONSIDERED LEVEL 2 CORROSION, PART REPLACEMENT REQUIRED. SEAT TRACK REPLACED AS PER SRM 51-72-11 REV 98.01 AND AIRBUS DWG F53276421 ISSUE R. JOB COMPLETE.

Part: SEAT TRACK — CORRODED (FRAMES 26-37) · corrosion level 2 · airframe 25,712 hrs · 4,099 cycles

DURING H CHECK, SEAT TRACK BETWEEN FR 26-37-4, -Y450 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53276421. LP 1012345

Part: SEAT TRACK — CORRODED (FRAMES 62-71) · corrosion level 2 · airframe 25,712 hrs · 4,099 cycles

DURING H CHECK, SEAT TRACK BETWEEN FR 62-71, -Y2462 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53477040. LP 1012341

Part: SEAT TRACK — CORRODED (FRAMES 62-71) · corrosion level 2 · airframe 25,723 hrs · 4,101 cycles

SEAT TRACK BETWEEN FRAME 62 AND 71 AT -Y2462 IS CORRODED AT LOCATIONS: FR63+10", FR65, FR65+2", FR66+13". // CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR63+10", FR65", FR65+2", FR66+13" LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS I.A.W. A330 SRM 51-74-00 PARA 6.B (6) RELEASE 98.01 DUE TO INACCESSIBILITY. ASSESSED AS OUTSIDE OF SRM 53-31-15 REV 98.01 LIMITS. RII CARRIED OUT AS PER HAL GMM VOL1 CHAP 5 - CONSIDERED LEVEL 2 CORROSION, PART REPLACEMENT REQUIRED. SEAT TRACK REPLACED AS PER SRM 51-72-11 REV 98.01 AND AIRBUS DWG F53477040 ISSUE H. JOB COMPLETE.

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · corrosion level 2 · airframe 25,723 hrs · 4,101 cycles

SEAT TRACK #19 BETWEEN FRAME 53.2 AND 54.5 AT +Y1959 IS CORRODED AT LOCATIONS: FR53.2+6", FR53.2+7.5", FR53.3+2", FR53.5+11", FR53.6+15", FR53.7+2" FAULT DESCRIPTION: SEAT TRACK BETWEEN FRAME 53.2 AND 54.5 AT +Y1959 IS CORRODED AT LOCATIONS: FR53.2+6", FR53.2+7.5", FR53.3+2", FR53.5+11", FR53.6+15", FR53.7+2". // CORROSION REMOVED AS PER SRM 51-74-00 REV 98.01. DAMAGE LOCATED AT FR53.2+6? AND F53.2+7.5?, CORROSION LOCATED IN INNER VERTICAL AREA UNABLE TO BE FULLY REMOVED OR MEASURED. OTHER DAMAGE DIMENSIONS: FR53.3+2" SUPERIOR L=1.0" W=0.50" DEPTH=0.010", FR53.5+11" SUPERIOR L=1.0" W=0.50" DEPTH=0.005", FR53.6+15" SUPERIOR L=1.50" W=0.50" DEPTH=0.080", FR53.7+2" SUPERIOR L=1.0" W=0.50 DEPTH=0.030". VERNIER CALIPER USED P/N: 505-717 S/N: ITWA17491. ASSESSED AS OUTSIDE OF SRM 53-31-15 REV 98.01 LIMITS. RII CARRIED OUT AS PER HAL GMM VOL 1 CHAP 5. CONFIRMED AS LEVEL 2 CORROSION, PART REPLACEMENT REQUIRED. SEAT TRACK REPLACED AS PER SRM 51-72-11 REV 98.01 AND AIRBUS DRAWING F53326941 ISSUE A. TORQUE WRENCH USED P/N: SLO S/N: TZA04961. JOB COMPLETE.

Part: SEAT TRACK — CORRODED (FRAMES 62-71) · corrosion level 2 · airframe 25,712 hrs · 4,099 cycles

DURING H CHECK, SEAT TRACK BETWEEN FR 62-71, -Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53477040. LP 1010897

Part: SEAT TRACK — CORRODED (FRAMES 62-71) · corrosion level 2 · airframe 25,723 hrs · 4,101 cycles

SEAT TRACK BETWEEN FRAME 62 AND 71 AT -Y1959 IS CORRODED AT LOCATIONS: FR62+12", FR63+11", FR64+2", FR64+18". // CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR62+12", FR63+11", FR64+2", FR64+18". CORROSION LOCATED ON INNER VERTICAL WALL AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS. ASSESSED AS OUTSIDE OF SRM 53-31-15 REV 98.01 LIMITS. RII CARRIED OUT AS PER HAL GMM VOL1 CHAP 5 - CONSIDERED LEVEL 2 CORROSION, PART REPLACEMENT REQUIRED. SEAT TRACK REPLACED AS PER SRM 51-72-11 REV 98.01 AND AIRBUS DWG F53477040 ISSUE H. JOB COMPLETE.

Part: SEAT TRACK — CORRODED (FRAMES 58-62) · corrosion level 2 · airframe 25,712 hrs · 4,099 cycles

DURING H CHECK, SEAT TRACK BETWEEN FR 58-62, -Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53477040. LP 1010908

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · corrosion level 2 · airframe 25,712 hrs · 4,099 cycles

DURING H CHECK, SEAT TRACK BETWEEN FR 53.2-54.5, +Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53326941. LP 1010890

Part: SEAT TRACK — CORRODED (FRAMES 40-47) · corrosion level 2 · airframe 25,723 hrs · 4,101 cycles

SEAT TRACK BETWEEN FRAME 40 AND 47 AT -Y1959 IS CORRODED AT LOCATIONS: FR46-3". // CORROSION REMOVED AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR46-3? L=0.500? W=0.125? EPTH=0.097?. VERNIER CALIPER USED P/N: 505-717 S/N: ITWA17491. ASSESSED AS OUTSIDE OF SRM 53-31-15 REV 98.01 LIMITS. RII CARRIED OUT AS PER HAL GMM VOL 1 CHAP 5. CONFIRMED AS LEVEL 2 CORROSION, PART REPLACEMENT REQUIRED. SEAT TRACK REPLACED AS PER SRM 51-72-11 REV 98.01 AND AIRBUS DRAWING F57112824 ISSUE C. TORQUE WRENCH USED, P/N: SLO S/ N: TZA04961. JOB COMPLETE.

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · corrosion level 2 · airframe 25,712 hrs · 4,099 cycles

DURING H CHECK, SEAT TRACK BETWEEN FR 53.2-54.5, +Y2462 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53326931. LP 1010893

Part: SEAT TRACK — CORRODED (FRAMES 58-67) · corrosion level 2 · airframe 25,712 hrs · 4,099 cycles

DURING H CHECK, SEAT TRACK BETWEEN 58-67, +Y450 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53477044. LP 1010907

Part: SEAT TRACK — CORRODED (FRAMES 58-62) · corrosion level 2 · airframe 25,723 hrs · 4,101 cycles

SEAT TRACK BETWEEN FRAME 58 AND 62 AT -Y1959 IS CORRODED AT LOCATIONS: FR60+10", FR61, FR61+20". // CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR60+10" SUPERIOR L=2.0" W=0.750" DEPTH= 0.020", FR61 AND FR61+20" CORROSION ALSO SPREAD TO INNER VERTICAL WALL AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS, GAUGE PN: 07852307, SN: TCN51487 AND PN: 2417, SN: IRFE5005A933. ASSESSED AS OUTSIDE OF SRM 53-00-15 REV 98.01 LIMITS. RII CARRIED OUT AS PER HAL GMM VOL1 CHAP 5 - CONSIDERED LEVEL 2 CORROSION, PART REPLACEMENT REQUIRED. SEAT TRACK REPLACED AS PER SRM 51-72-11 REV 98.01 AND AIRBUS DWG F53477040 ISSUE H. JOB COMPLETE.

Part: SEAT TRACK — CORRODED (FRAMES 40-47) · corrosion level 2 · airframe 25,712 hrs · 4,099 cycles

DURING H CHECK, SEAT TRACK BETWEEN FR 40-47, -Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F57112824. LP 1010902

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · corrosion level 2 · airframe 25,723 hrs · 4,101 cycles

SEAT TRACK #20 BETWEEN FRAME 53.2 AND 54.5 AT +Y2462 IS CORRODED AT LOCATIONS: FR53.3+3", FR53.3+13", FR53.2 FAULT DESCRIPTION: SEAT TRACK BETWEEN FRAME 53.2 AND 54.5 AT +Y2462 IS CORRODED AT LOCATIONS: FR53.3+3", FR53.3+13", FR53.2. // CORROSION REMOVED AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR53.3+3" SUPERIOR L= 1.50" W=1.0" DEPTH=0.070", FR53.3+13" L=1.50" W=1.0" DEPTH 0.010", FR53.2 L=1.0" W=.25" DEPTH 0.010". VERNIER CALIPER USED P/N: 505-717 S/N: ITWA17491. ASSESSED AS OUTSIDE OF SRM 53-31-15 REV 98.01 LIMITS. RII CARRIED OUT AS PER HAL GMM VOL 1 CHAP 5. CONFIRMED AS LEVEL 2 CORROSION, PART REPLACEMENT REQUIRED. SEAT TRACK REPLACED AS PER SRM 51-72-11 REV 98.01 AND AIRBUS DRAWING F53326931 ISSUE A. TORQUE WRENCH USED P/N: 11037 S/N: TZA04959. JOB COMPLETE.

Part: SEAT TRACK — CORRODED (FRAMES 68-67) · corrosion level 2 · airframe 25,723 hrs · 4,101 cycles

SEAT TRACK BETWEEN FRAME 58 AND 67 AT +Y450 IS CORRODED AT LOCATIONS: FR58+9", FR59+6", FR59+7", FR59+20". // CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR58+9", FR59+6", FR59+7", FR59+20". CORROSION LOCATED ON INNER VERTICAL WALL AREA. UNABLE TO SUFFICIENTLY REMOVE CORROSION AND ESTABLISH REMAINING THICKNESS. ASSESSED AS OUTSIDE OF SRM 53-31-15 REV 98.01 LIMITS. RII CARRIED OUT AS PER HAL GMM VOL1 CHAP 5 - CONSIDERED LEVEL 2 CORROSION, PART REPLACEMENT REQUIRED. SEAT TRACK REPLACED AS PER SRM 51-72-11 REV 98.01 AND AIRBUS DWGF53477044 ISSUE C. JOB COMPLETE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,712 hrs · 4,099 cycles

DURING H CHECK, SEAT TRACK BETWEEN FR 40-47, -Y450 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING F57112821. LP 1005208

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,723 hrs · 4,101 cycles

SEAT TRACK BETWEEN FRAME 40 AND 47 AT -Y450 IS CORRODED AT LOCATIONS: FR40+2";FR40.3+1"FR45. CORROSION REMOVED AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR40+2" INNER VERTICAL: D-0.080" X L-0.400" W-0.120", FR40.3 + 1" O/B LATERAL: D-0.090 X L-1.400: X W-0.400", FR45 INNER VERTICAL: D-0.070" X L-1.520" X W-0.400". DEPTH GAUGE P/N USED: 2417 S/N: IRFE5005A9EQ. ASSESSED AS OUTSIDE OF SRM 53-31-15 REV 98.01 LIMITS. RII CARRIED OUT AS PER GMM VOL CHAP 5. CONFIRMED AS LEVEL 2 CORROSION ? PART REPLACEMENT REQUIRED. SEAT TRACK ASSEMBLY REPLACED AS PER SRM 51-72-11 REV 98.01 AND DRAWING F57112821 ISSUE E JOB COMPLETE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,712 hrs · 4,099 cycles

DURING H CHECK, SEAT TRACK BETWEEN FR 53.2-79.3, FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING F53275878. LP 1002036

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,712 hrs · 4,099 cycles

DURING H CHECK, SEAT TRACK BETWEEN FR 26-37.4, +Y1456 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING F53276421. LP 1002025

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,712 hrs · 4,099 cycles

DURING H CHECK, SEAT TRACK BETWEEN FR 37.4-39.2, -Y450 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING F53311114. LP 1002038

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,712 hrs · 4,099 cycles

DURING H CHECK, SEAT TRACK BETWEEN FR 31-35, -Y1552 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING F53275878. LP 1002031

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,723 hrs · 4,101 cycles

SEAT TRACK BETWEEN FRAME 31 AND 35 AT -Y1552 IS CORRODED AT LOCATIONS: FR32+17", FR33+4". CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR32(+17") SUPERIOR REWORK L: 3.5" W: 0.3" D:0.045", FR33(+4") CENTRAL REWORK L: 3.5" W: 0.3" D: 0.025". DIAL INDICATOR USED P/N 2417 S/N IRFE5005A9EQ. ASSESSED AS OUTSIDE OF SRM 53-00-15 REV 98.01 LIMITS. RII CARRIED OUT AS PER HAL GMM VOL1 CHAP 5 - CONSIDERED LEVEL 2 CORROSION, PART REPLACEMENT REQUIRED. SEAT TRACK REPLACED AS PER SRM 51-72-11 REV 98.01 AND DWG F53275878 ISSUE E. JOB COMPLETE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,723 hrs · 4,101 cycles

SEAT TRACK BETWEEN FRAME 26 AND 37.4 AT +Y1456 IS CORRODED AT LOCATIONS: FR36. CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR36 SUPERIOR REWORK L: 3" W: 0.3" D: 0.115" DIAL INDICATOR P/N 2417 S/N IRFE5005A9EQ. ASSESSED AS OUTSIDE OF SRM 53-00-15 REV 98.01 LIMITS. RII CARRIED OUT AS PER GMM VOL1 CHAP 5 - CONSIDERED LEVEL 2 CORROSION, PART REPLACEMENT REQUIRED. SEAT TRACK REPLACED AS PER SRM 51-72-11 REV 98.01 AND DWG F53276421 ISSUE R. JOB COMPLETE.

Part: CONTROLLER — MALFUNCTIONED (AC BAY) · airframe 25,458 hrs · 4,060 cycles

OPEN - ETOPS SIGNIFICANT SYSTEM - FLIGHT DECK TEMP DIFFICULT TO CONTROL EITHER TO HOT OR TOO COLD. ZONE TEMP INDICATION OVERSHOOTS TO HIGH OR LOW. COCKPIT ZONE TEMP ROTARY SELECTOR, DOES NOT SEEM TO RESPOND IN THE MID RANGE 12 O'CLOCK POSITION. RESET PACK CONTROLLER 1 + 2, ZONE CONTROLLER, CHK COCKPIT ZONE SENSOR. PERFORMED SYS TEST OF PACK CONTROLLING AND INDICATION PER AMM 21-53-00-710-802-A. OK FOR SVC.

Part: CONTROLLER — MALFUNCTIONED (TEMP SYSTEM) · airframe 25,447 hrs · 4,058 cycles

ETOPS SIGNIFICANT SYSTEM, COCKPIT TEMP SYSTEM INOP. VERY HARD TO CONTROL TEMP IN COCKPIT IT EITHER TOO HOT OR TOO COLD. CKPT TEMP SHOWS 80*F BUT FEELS LIKE 70*F. RESET PACK CONT 1/2 AND ZONE CONT. PERFORMED ECS "BITE". NO FAULTS NOTED. OK FOR SVC.

Part: SENSOR — DEFECTIVE (COCKPIT) · airframe 25,436 hrs · 4,056 cycles

ETOPS SIGNIFICANT SYSTEM - COCKPIT TEMP CONTROLLER INOP. ITS EITHER 52 DEGREES OR 132 DEGREES ON COND SYNOPTIC PAGE FOR HOT AIR 2. REMOVED AND REPLACED COCKPIT TEMP SENSOR 650HK PER AMM 21-63-17-400-802-A. OPS TEST GOOD. COCKPIT TEMP CONTROL NORMAL. OK FOR SERVICE.

Part: BRAKE — OVERHEATED (MLG) · airframe 25,311 hrs · 4,036 cycles

ATO, NR 5 BRAKE WAS RAPIDLY CLIMBING & REACH MAX OF 520 DEGREES. REPLACED NR 5 BRAKE.

Part: UNKNOWN — MALFUNCTIONED (TEMP SYSTEM) · airframe 24,871 hrs · 3,969 cycles

ETOPS SIGNIFICANT SYSTEM - COCKPIT TEMPERATURE TRIM AIR VALVE, TEMPERATURE UNCONTROLLABLE, TRIM AIR TEMP GOES FROM 42C TO 124C WITH COCKPIT CONTROLLER SET ON INDEX MAKE. RESET THE C/B OF ZONE CONTROLLER AND PERFORMED THE SYSTEM TEST OF COCKPIT AND CABIN TEMP CONTROL AND THEN TEST PASSED IAW AMM 21-63-00-730-801-A. ACFT OK FOR SVC.

Part: FIRE LOOP — BROKEN (NR 2 NACELLE) · airframe 24,221 hrs · 3,876 cycles

ATB - ENG 2 FIRE LOOP A FAULT ENG 2 FIRE LOOP A/FDU2. // FOUND ENGINE PYLON LOOP 6WD2 BROKEN AT DETECTOR. REMOVED AND REPLACED ENG 2 FIRE LOOP A AND SUPPORT ASSEMBLY PER AMM 26-12-16. OPS CHECK GOOD. OK FOR SVC.

Part: LIGHT — MISSING (CABIN) · airframe 24,123 hrs · 3,863 cycles

EXIT FLOOR LIGHTING MISSING IN FIRST CLASS. // RE-SECURED EXIT FLOOR LIGHTING STRIP IN FIRST CLASS AREA.

Part: TERMINAL — LOOSE (FIRE DETECTOR) · airframe 24,108 hrs · 3,860 cycles

AIR DIVERSION - ENG 2 FIRE LOOP A FAULT. // PER A330 TSM TASK 26-12-00-810-937-A INSPECTED FIRE LOOP ON ENG 2, FOUND FIRE DET- LOOP 2L (4012WD) 3 TERMINAL LOOSE AND FOUND FIRE DET PYLON (6WD2) RESISTANCE CHECK VERIFIED OPEN. REMOVED FIRE DET LOOP (6WD2) WORK STILL IN PROGRESS PER A330 AMM 26-12-16. RE TERMINATED LUGS AT 4012WZ REF A330 ESOM CH.20 AND WDM 71-51-04. REMOVED AND REPLACED ENG 2 LOOP 2 FIRE DETECTOR. REF A330 AMM 26-12. PERFORMED FIRE DETECTION SYSTEM TEST. LOOP 1 & 2 PASSED. TEST OK. OK FOR SVC.

Part: MOTOR — MAKING METAL (STARTER) · airframe 24,093 hrs · 3,858 cycles

ETOPS SIGNIFICANT SYSTEM - METAL CHIPS IN #2 STARTER CHIP DETECTOR. // REMOVED AND REPLACED #2 STARTER ASSEMBLY IAW A330 AMM TASKS 80-11-41-000-803-A & 80-11-41-400-803A, LEAK AND OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,543 hrs · 3,774 cycles

DOOR 1L EMERGENCY LIGHT INOP. RELAMPED DOOR 1L EMERGENCY LIGHT.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 23,457 hrs · 3,762 cycles

R3 DOOR EXIT SIGN LENS DETACHED. SECURED THE EXIT SIGN LENS.

Part: PROBE — FAULTED (NR 1 ENGINE) · airframe 22,254 hrs · 3,583 cycles

ETOPS SIGNIFICANT SYSTEM. UPON LANDING, ECAM ENGINE 1 MINOR FAULT. PFR 732111 P20T20 PROBE (E1-4014KS) T20 A AT ENG START. T/S PER TSM 73-21-71-810-865-A NO FAULTS, NO PREV LEG FAULTS. OK FOR SVC.

Part: IDG — FAULTED (NR 2 GENERATOR) · airframe 21,833 hrs · 3,520 cycles

NR 2 GENERATOR FAULTED. AIR TURNBACK. REMOVED AND REPLACED THE RIGHT IDG IAW AMM 24-21-51, OPS AND LEAK CHECKED OK. OK FOR SERVICE.

Part: OIL SYSTEM — LOW (APU) · airframe 21,639 hrs · 3,490 cycles

APU LOW OIL LEVEL. SERVICED TWO QTS OF APU OIL.

Part: IGNITER — INOPERATIVE (NR 2 ENGINE) · airframe 20,862 hrs · 3,374 cycles

NR 2 ENG IGNITER B INOPERATIVE. PERFORMED AMM 74-21-51, REPLACED THE IGNITER PLUG. PERFORMED BITE TEST OF THE IGNITER SYS, TESTED OK IAW AMM 74-00-00. OK FOR SERVICE.

Part: BLEED VALVE — FAULTED (NR 1 ENGINE) · airframe 20,484 hrs · 3,323 cycles

NR 1 ENGINE BLEED FAULT AFTER TAKE OFF, STALLED DURING CRUISE, NR 1 CONTROL SYS FAULT AFTER LANDING. REPLACE THE NR 1 ENGINE, PRV VALVE, AND LT VSV ACTUATOR.

Part: COVER — UNSECURE (CABIN) · airframe 20,439 hrs · 3,315 cycles

DOOR 3R EXIT LIGHT COVER FELL OFF ON LANDING. RE-INSTALLED AND SECURED DOOR 3R EXIT LIGHT COVER.

Part: LIGHT — LOOSE (CABIN) · airframe 20,355 hrs · 3,299 cycles

EMERGENCY FLOOR LIGHT STRIP LOOSE AT SEAT 25H. REPLACED EMERGENCY FLOOR PATH LIGHT COVER AT SEAT 25H.

Part: UNKNOWN — UNKNOWN (NR 2 ENGINE) · airframe 20,128 hrs · 3,253 cycles

ETOPS SIGNIFICANT SYSTEM - ENG 2 START FAULT NO LIGHT OFF. // PERFORMED START VALVE DUTY CYCLE. PERFORMED PROCEDURES OF ENGINE STARTING PER AMM 74-00-00-704-806-A. A/C STARTED OK.

Part: TUBE — CONTAMINATED · airframe 20,103 hrs · 3,248 cycles

ETOPS SIGNIFICANT SYSTEM - AT TOP OF DES. ECAM ENG1 CTL SYS FAULT.// DID BITE TEST OF EEC1 CH. A. GOT A FAULT OF P30 PRESSURE TUBE. TROUBLE SHOT PER TSM 73-21-78-810-815-A. EMPTIED P30 MOISTURE TRAP PER AMM 73-21-41-100-810-A. WATER WAS FOUND IN WATER TRAP. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. OK FOR SVC.

Part: BLEED VALVE — FAULTED (NR 1 ENGINE) · airframe 19,545 hrs · 3,140 cycles

NR 1 ENGINE BLEED FAULT DURING CLIMB. RESET IAW MOC, OPS NORMAL. TROUBLESHOT IAW TSM 36-11-81-810-909-A. REMOVED AND REPLACED THE NR 1 ENGINE BLEED VALVE IAW AMM 36-11-52. OPS CHECKED OK. NO FAULTS NOTED. BITE CHECKED BMC, OK. LEAK CHECKED OK. NO LEAKS. OK FOR SERVICE.

Part: LIGHT — DETACHED (CABIN) · airframe 19,209 hrs · 3,075 cycles

EMERGENCY PATH LIGHTING ON FLOOR FORWARD OF GALLEY DETACHED. RESECURED EMERGENCY PATH LIGHTING STRIPS IN FORWARD GALLEY.

Part: UNKNOWN — ODOR (CABIN) · airframe 18,443 hrs · 2,936 cycles

PASSENGER AND FLIGHT ATTENDANT REPORT AN ODOR OF PROPANE COMING FROM OVERHEAD VENT INTERMITTENTLY DURING ENTIRE FLIGHT. IAW THE FLT CREW ODOR WAS COMING FROM ROW 26HJ OVERHEAD VENT AREA ONLY. INSPECTED AREA AROUND ROW 26HJ. INSPECTED AIR CONDITIONING DUCT ABOVE ROW 26HJ. NO DEFECT NOTED. INSPECTED IFE SYSTEM FOR SEAT 26HJ AND CARGO AREA, OPERATED AC PACK IAW AMM 12-33-21-618-801-A02. NO ODOR OR DEFECTS NOTED. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (FWC NR 1) · airframe 17,983 hrs · 2,855 cycles

FWC 1 FAULT ON ECAM, 3,3 HOURS INTO CRUISE. TROUBLESHOT IAW TSM 31-50-00-810-807-A. ALL OPS CHECKED NORMAL. OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 175,948 hrs · 2,848 cycles

AFTER TAKE OFF, FLIGHT ATTENDANTS & PASSENGERS COMPLAINED OF THE ODOR OF CHLORINE. ODOR DILUTED AS THE FLIGHT WENT ON. PERFORMED HIGH POWER RUN OF THE NR 1 & 2 ENGINES. PACKS 1 & 2 ON, INSPECTED FWD, MID, & AFT SECTIONS OF CABIN AND LDMCR. NO DEFECTS NOTED. FLIGHT CREW REPORTED NO DEFECTS IN FLIGHT DECK. NO ENGINE OIL SERVICING REQUIRED. OK TO CONTINUE.

Part: LIGHT — UNKNOWN (CABIN) · airframe 17,717 hrs · 2,803 cycles

26B PATH LIGHT STRIP BROKEN. INSTALLED MISSING STRIP AT 26B.

Part: LIGHT — DETACHED (SEAT 27H) · airframe 17,469 hrs · 2,761 cycles

EMERGENCY LIGHT STRIP NEXT TO SEAT 27H IS DETACHED. ATTACHED THE LIGHT STRIP. OPS CHECKED OK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 17,316 hrs · 2,736 cycles

LENS MISSING FROM OVERHEAD AISLE EMERGENCY LIGHT ROW 16 RIGHT. INSTALLED NEW LENS.

Part: FWC — FAULTED (NR 1) · airframe 17,032 hrs · 2,687 cycles

FWC 1 FAULT INFLIGHT. RESET THE CIRCUIT BREAKER FOR THE NR 1 FWC.THEN BACK TO NORMAL. FWS LAST LEG NO FAULT. FWS BITE TEST PASSED IAW AMM 31-51.

Part: LIGHT — UNSECURE (CABIN) · airframe 16,914 hrs · 2,670 cycles

EMER EXIT FLOOR LIGHTING (SEATS 47HJ) NEEDS TO BE RESECURED TO FLOOR. RESECURED FLOOR WAY ILLUMINESCENT STRIP AT 47HJ.

Part: SENSOR — DEFECTIVE (AC BAY) · airframe 16,842 hrs · 2,657 cycles

DIVERTED TO HNL DUE TO THE AIR PACK 2 REGULATOR FAULT ILLUMINATED ON ECAM AFTER TAKEOFF. PACK OUTLET TEMP INDICATION SHOWED X. REPLACED NR 2 PACK DISCHARGE TEMP SENSOR.

Part: GLOWSTRIP — UNSECURE (CABIN) · airframe 16,196 hrs · 2,558 cycles

SEAT 28G FLOOR LIGHT STRIP LIFTING OFF THE FLOOR. RE-SECURED FLOOR GLOW IN THE DARK STRIP.

Part: FILTER — CLOGGED (APU FUEL) · airframe 15,941 hrs · 2,514 cycles

APU INLET FILTER DPI EXTENDED DURING VISUAL CHECK OF APU INLET FILTER DPI. REMOVED AND REPLACED THE APU FUEL INLET FILTER ELEMENT IAW AMM 49-32-41 & OP TESTED OK. LEAK CHECKED OK. RAN APU & NO DISCREPANCIES FOUND. OK FOR SERVICE.

Part: WATER HEATER — LEAKING (LAVATORY) · airframe 21,147 hrs · 3,249 cycles

4L LAV LEAKING, UNABLE TO STOP WITH SHUTOFF VALVE. 4L LAV WATER LINE BENEATH WATER HEATER HAD UNCONTROLLABLE WATER LEAK. CLOSED LAV SUPPLY S/O VALVE AND LAV BLOCKED PER MEL 38-30-1B CAT C. INSPECTED AFT CARGO AREA, NO WATER FOUND. R&R WATER HEATER AT 4L LAV PER AMM 38-12-51. "M" PROCEDURES REVERSED. OPS CHECK GOOD. LAV RETURNED TO SERVICE. MEL & PLACARD REMOVED.

Part: WATER HEATER — LEAKING (LAVATORY) · airframe 15,600 hrs · 2,458 cycles

DIVERTED DUE TO UNCONTROLLABLE WATER LEAK AT L4 DOOR LAV BENEATH THE WATER HEATER LINE. REPLACED WATER HEATER

Part: GROUND WIRE — DAMAGED · airframe 11,229 hrs · 1,787 cycles

ON TAXI OUT "ELEC APU TR FAULT" ANNUNCIATED. REPLACE BCL GROUND OPS CHECK OK, AMM 24-38-35.

Part: APU — MALFUNCTIONED · airframe 10,760 hrs · 1,711 cycles

AIRCRAFT RETURNED TO DEPARTURE DUE TO ELECTRONIC-APU T/R FAULT. REPLACED APU T/R.

Part: APU — FAULTED · airframe 10,755 hrs · 1,709 cycles

APU TR FAULT. FOUND APU TR INOPERATIVE. R & R APU TR IAW AMM 24-32-51. OPS CHECK GOOD. OK FOR SERVICE.

Part: COMPUTER — MALFUNCTIONED (WINDOW HEAT) · airframe 10,546 hrs · 1,676 cycles

RT WINDSHIELD HEAT INOPERATIVE. TRIED RESETTING A COUPLE OF TIMES AFTER A WHILE LIGHT COMES BACK ON. REPLACED RT WINDSHIELD HEAT COMPUTER IAW AMM 30-42-44. OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (WINDOW HEAT) · airframe 10,546 hrs · 1,676 cycles

RT WINDSHIELD HEAT INOPERATIVE. TRIED RESETTING A COUPLE OF TIMES, AFTER A WHILE LIGHT COMES BACK ON. REPLACED RT WINDSHIELD HEAT COMPUTER IAW AMM 30-42-44, OPS CHECK GOOD.

Part: FDU — MALFUNCTIONED (NR 2) · airframe 10,147 hrs · 1,611 cycles

DURING TAXI OUT ENGINE NR 2 FIRE FAULT ECAM BTB. R & R FDU 2 IAW AMM 26-12-34-400-803-A. OPS CHECK OK, OK FOR SERVICE.

Part: ACTUATOR — FAULTED (APU FUEL) · airframe 8,798 hrs · 1,401 cycles

APU WOULD NOT START. RECEIVED AN ECAM FOR FUEL APU LP VALVE FAULT. REPLACED APU LP FUEL SOV ACTUATOR IAW 28-29-52-000-801-4. OPS CHECK OK.

Part: WARNING MESSAGE — ILLUMINATED · airframe 8,551 hrs · 1,359 cycles

ELEC APU TR FAULT ECAM. RESET APR T/R. GROUND OPS CHECKED OK IAW 24-32-00.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 8,358 hrs · 1,331 cycles

DURING OPENING OF R1 DOOR ESCAPE SLIDE DEPLOYED. REMOVED IAW AMM 25-62-41-000-801-A02. REMOVED PN 7A1508-125. . INSTALLED SLIDE IAW AMM 25-62-41-400-801A. OK FOR SERVICE.

Part: SKIN — PUNCTURED (NOSE COWL) · airframe 8,153 hrs · 1,299 cycles

ETOPS SIGNIFICANT SYS - NR 1 ENGINE HAS A SMALL PUNCTURE IN THE INNER SKIN OF THE NOSE COWL AT THE 11:00 POSITION. JUST AFT OF THE EEC COOLING INLET. DEFERRED IAW ERA 534614-14 , REPAIRED APPROVED AND TIME LIMITED IAW PS 900-5-1, NR 4. C/W MAINT PROCEDURES. ACFT OK FOR SERVICE.

Part: PROBE — INOPERATIVE · airframe 5,207 hrs · 820 cycles

DURING CLIMB "ENGINE 1 EPR MODE FAULT", CONDUCTED ECAM ACTIONS. RETURNED TO DEPARTURE. TROUBLESHOT AND FOUND P20/T20 INOPERATIVE. R & R P20/T20 IAW AMM 73-21-11, CONDITION CK OK. OPS CHECK PENDING. PREFORMED TEST OF P20/T20 PROBE HEATER IAW TASK 73-21-00-740-807A, TEST OK. OK FOR SERVICE.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 3,997 hrs · 635 cycles

R3 DOOR EXIT SIGN BROKEN. REPLACED EXIT SIGN. OPS & SECURITY CHECK OK.