N410UA

Part: SHOCK ABSORBER — FAULTY (NLG) · airframe 89,173 hrs · 34,514 cycles

L/G SHOCK ABSORBER FAULT ON ECAM. AHM SHOWS NLG SHOCK ABSORBER 2526GM ID''D BY LGCIU 1 AND 2 31-3231-3-0007 24 GA AND 25 GA INSTOCK SAFTY VALVE ON ORDER FOUND STRUT WITH LESS THAN 100PSI IN STRUT AND LOW ON FLUID , ACP REMOVAL PER AMM 32-21-13-000-001-A-01 OF SHOCK STRUT PICTURE UPDATE 31-3230-9-9006 FILLED WITH FLUID AND NITROGEN , STUT FLUID STARTED POURING OUT ABSORBER ASSY. , STARTED AMM 32-21-13-960-001-A REPLACEMENT OF OF STRUTS SEALS AND WEEP HOLE . SEAL KIT NEDDED 31-3221-3-0006 SHOCK ABSORBER DYNAMIC SEAL COMPLETED UP TO STEP 4 B ON AOG ADD EMP:U107568,U103224,U241476 REPLACWD NLG SHOCK SEALS I/A/W AMM 32-21-13-960-001-A AND IPC RII ITEM REF: GMM 09-25-05; INSPECTED NLG SHOCK SEALS 32-21-11-43 AND 32-21-13-11A. INSTALLED NLG SHOCK STRUT I/A/W REPLACEMENT - REF: AMM 32-21-13-960-001-A AND IPC 32-21-11-43 AMM 32-21-13-400-001-A01 UP TO STEP B14. AND 32-21-13-11A. INSPECTED INSTALLATION OF NLG SHOCK STRUT REF: AMM 32-21-13-400-001-A01 COMPLETED UP TO STEP B14. COMPLETED ALL JOB CARDS PER AMM 32-21-13-960-001-A , 32-21-13-000-001-A-01 . NO ABSORBER MESSAGES AFTER REPAIR AND GEAR SWING . NO FAULTS WHEN TAXIING ACFT TO GATE . VERIFIED LOWER NLG ACTUATOR ATTACH CORRECT AND SECURE TO NLG. REF AMM 32-31-22-400-001-A. NORMAL EXT AND RET TEST OF NLG GOOD. REF AMM 31-31-00-720-002-A

Part: BATTERY — FAULTY (BOTH) · airframe 88,273 hrs · 34,080 cycles

BOTH BATTERIES SHOWING 25 VOLTS AND AMBER, ZERO AMPS. BATT PB/SW''S MATCH ECAM ELECTRICAL SYNOPTICS PAGE. REF TSM''S 24-38-00-810-848 AND 24-3800-810-832 FOR CIRCUIT UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V925166 REPLENISH BATT UNTIL FULL CHG NORMALLY. BREAKER CHECKS. NOTE: SEVERAL CBS ON THE 105VU, 121VU AND PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. CONTACT TOMC FOR MAC RELATED WORK ORDER 000000003033078 AND PRTR 122VU. CIRCUIT BREAKER CHECKS. CHILD, HAYDEN (V925166), PERFORMED BCL TEST PER AMM 24-38-00-710-001-A, EMERG GEN SYS OPERATIONAL TEST PER AMM 24-24-00-710-001-A AND STATIC INV OPERATIONAL TEST PER AMM 24-28-00-710-001-A ALL TESTS PASSED NO FAULTS NOTED BATTERY VOLTAGES AT 27 VOLTS. DURING TEST FOUND CHARGERS KICK ON AND CHILD, HAYDEN (V925166), PERFORMED BCL TEST PER AMM VOLTAGES AT 27 VOLTS. DURING TEST FOUND CHARGERS KICK ON AND 24-38-00-710-001-A, EMERG GEN SYS OPERATIONAL TEST PER AMM REPLENISH BATT UNTIL FULL CHG NORMALLY. 24-24-00-710-001-A AND STATIC INV OPERATIONAL TEST PER AMM 24-28-00-710-001-A ALL TESTS PASSED NO FAULTS NOTED BATTERY ADD EMP:V925166

Part: EIU — FAILED (NR 1 ENGINE) · airframe 87,209 hrs · 33,592 cycles

EIU FAULT DISPLAYED ON UPPER ECAM SCREEN. - ENG 1 OCCURED ON GNDRESET AND ECAM CLRDOCCURED AGAIN INFLT- FADEC 1B FAULT. BITE TEST OF FADEC HAD EIU/HC/EEC1. REPLACED #1 EIU. AND FADEC BITE TEST CK GOOD. RAN ENGINE,NO FAULTS NOTED. REF MM 73-25-00-810-887A. PARTS REPLACED. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1249686 SN OFF 9275 UNIT, ENGINE IN OFF 31-7330-9-0001 9275 ON 31-7330-9-0001 5307

Part: BRAKE ASSY — DRAGGING (NR 1) · airframe 86,655 hrs · 33,338 cycles

HOT BRAKES INDICATED AFTER TAKEOFF. #1 BRAKE WAS INDICATING APPX 330 AND 2-3-4 APPX 70. CREW DID NOT NOTICE ANY PULLING DURING TAXI. WILL NEED TO CONFIRM NO DRAGGING BRAKE ON ARRIVAL. SEE LOG PAGE 6614720(RPL #1 MLG BRAKE ASSY REF AMM 32-42-27,BRAKE FUNCTION NORMAL)

Part: BRAKE ASSY — DRAGGING (NR 1) · airframe 86,655 hrs · 33,338 cycles

HOT BRAKES INDICATED AFTER TAKEOFF. #1 BRAKE WAS INDICATING APPX 330 AND 2-3-4 APPX 70. CREW DID NOT NOTICE ANY PULLING DURING TAXI. WILL NEED TO CONFIRM NO DRAGGING BRAKE ON ARRIVAL. SEE LOG PAGE 6614720(RPL #1 MLG BRAKE ASSY REF AMM 32-42-27,BRAKE FUNCTION NORMAL)

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 86,098 hrs · 33,094 cycles

L/H AFT EMERG. EXIT DOOR (Z834) Z ANGLE BETWEEN LOAD TRANSMITTER AND EDGE BEAM CRACKED. REF TO PEMCO NR 10670.0168 REMOVED AND REPLACED L/H AFT EMERG DOOR Z-ANGLE IAW A320 SRM 51- 42-11 AND A320 SRM 51-44-11. ALODINED, PRIMED AND TOPLOCATED REP AIR AREA IAW A320 SRM 51-21-11 AND A320 SRM 51-23-11 AND AIRBUS DRAWING D522.79040. COMPLETED BY P174, INSP BY Q910, ENTERED BY V928371. WORK HAS BEEN ACCOMPLISHED AND INSPECTED. COMPLETED BY P174. INS P BY Q910. APPROVED BY INSP Q911.

Part: PROFILE — CRACKED (DOOR FRAME) · airframe 86,098 hrs · 33,094 cycles

L/H AFT EMERG. EXIT DOOR (Z834) L/H LOAD TRANSMITTER CRACKED. REF TO PEMCO NR 10670.0167 REMOVED AND REPLACED L/H AFT EMER, DOOR LOAD TRANSMITTER (SEGMEN T) IAW A320 SRM 51-42-11 AND 51-44-11. ALODINED, PRIMED AND TOPL OCATED REPAIR AREA IAW A320 SRM 51-21-11 AND SRM 51-23-11 AND AI RBUS DRAWING D522.79040. COMPLETED BY P174, INSP BY Q910, ENTERE D BY V928371. WORK HAS BEEN ACCOMPLISHED AND INSPECTED. COMPLETED BY P174. INS P BY Q910. APPROVED BY INSP Q911.

Part: STRUCTURE — CRACKED (EMERGENCY EXIT) · airframe 86,098 hrs · 33,094 cycles

L/H AFT EMERG. EXIT DOOR (Z834) L/H LOAD TRANSMITTER CRACKED. REMOVED AND REPLACED L/H AFT EMER, DOOR LOAD TRANSMITTER (SEGMEN T) IAW A320 SRM 51-42-11 AND 51-44-11. ALODINED, PRIMED AND TOPL OCATED REPAIR AREA IAW A320 SRM 51-21-11 AND SRM 51-23-11 AND AI RBUS DRAWING D522.79040. COMPLETED BY P174, INSP BY Q910, ENTERE D BY V928371.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 86,098 hrs · 33,094 cycles

L/H AFT EMERG. EXIT DOOR (Z834) Z ANGLE BETWEEN LOAD TRANSMITTER AND EDGE BEAM CRACKED. REF TO PEMCO NR 10670.0168 REMOVED AND REPLACED L/H AFT EMERG DOOR Z-ANGLE IAW A320 SRM 51- 42-11 AND A320 SRM 51-44-11. ALODINED, PRIMED AND TOPLOCATED REP AIR AREA IAW A320 SRM 51-21-11 AND A320 SRM 51-23-11 AND AIRBUS DRAWING D522.79040.

Part: BEAM — CRACKED (R/H FWD EM DR.) · airframe 86,098 hrs · 33,094 cycles

(A3NB-52-4-6031) R/H FWD. EMERG. EXIT DOOR (Z843) R/H LOAD TRANSMITTER CRACKED. REFER TO PEMCO N/R 10670.0171.

Part: SEAL — CRACKED (NR 1 NACELLE) · airframe 85,805 hrs · 32,976 cycles

PDA 2 NR 1 ENGINE OUTBOARD SIDE PYLON TO NACELLE AFT MOST FLEX SEAL CRACKED AND MISSING A SEGMENT (AT FWD END OF FLEX SEAL) SEE PHOTO PARTS ADDED, REF ECRA 5450-02357 REV-B. ACCOMPLISH PERM REPAIR PER PART 3 WITHIN 50 FLIGHT HOURS, REF ECRA 5450-02357. PERFORMED PART 1D SPEED TAPE MISSING SECTION. APPLIED SPEED TAPE REF ECRA 5450-02357 PART 1D. DIP TO PERFORM VISUAL INSP, PER PART 2A EVERY FLIGHT CYCLE AND E1 OUTBOARD PYLON TO NACELLE FLEX SEAL FORWARD EDGE OF AFT SEAL SECTION INTERIM REPAIR (SPEED TAPE REPAIR) MUST BE CHECKED PRIOR TO EACH DEPARTURE AND MUST BE REPAIRED WITHIN 50 FLIGHT HOURS, REF TRM EC/RA 5450-02357 PART 1D. TOMC-APPROVAL FROM SC1ELBYC COMMENT. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT UPDATE. Q/C REVIEWED.

Part: SENSOR — FAILED (#2 P2/T2) · airframe 83,103 hrs · 31,774 cycles

ENG 2 EPR MODE FAULT N1DEGRADED MODE REPEAT FAULT. CONTACT TOMC TO DISCUSS CORRECTIVE ACTION. UNLOCK REPLACED #2 P2/T2 SENSOR REF.AMM 73-22-11, TESTED REF. TSM 73-22 -00-810-813

Part: PRESSURE PANEL — CRACKED (FRAME 35) · airframe 81,374 hrs · 31,009 cycles

RH PRESSURE PANEL AT FR35 ALL OPEN FASTENER HOLES BETWEEN -Y765 AND -Y1535 WITH THE EXCEPTION OF HOLES 8-13, 17,19 AND 22 PRODUC ED CRACK INDICATIONS DURING ABEEC BOLT HOLE INSP. CRACK LOCATION S ARE MARKED ON ACFT. REF AD 2018-06-04. REF HAECO NR 9294388. FR35 RH PRESSURE PANEL REPAIRED IAW ECRA 5331-02354. WILL REQUIR E DTA PER PART 1 STEP 2 TO ACCOMPLISH PERMANENT REPAIR AT FUSELA GE FR35-36 RH PRESSURE PANEL HOLES PER PART 3 OF ECRA 5331-02354 ON OR BEFORE 16 OCT 2019. PLANNING TO CONTACT ENGINEERING AFTER 16 SEP 2019 BUT BEFORE 01 OCT 2019 FOR PERMANENT REPAIR. OK TO DIP ?ACCOMPLISH THE PERMANENT REPAIR AT FUSELAGE FR35-36 RH PRESSURE PANEL HOLES PER PART 3 OF ECRA5331-02354 ON OR BEFORE 16-OCT-2019. PLANNING TO CONTACT ENGINEERING AFTER 16-SEP-2019 BUT / BEFORE 01-OCT-2019 FOR PERMANENT REPAIR.? TOMC SMITH

Part: PRESSURE PANEL — CRACKED (FRAME 35) · airframe 81,374 hrs · 31,009 cycles

LEFT PRESSURE PANEL AT FR35 ALL OPEN FASTENER HOLES BETWEEN Y765 A ND Y1535 WITH THE EXCEPTION OF NR 3 AND 8-13 PRODUCED CRACK INDICA TIONS DURING ABHEC BOLT HOLE INSP. LH PRESSURE PANEL REPAIRED IAW ECRA 5331-02356. ACCOMPLISHED A PERMANENT REPAIR AT FUSELAGE FR35-36 RH PRESSURE PANEL HOLES PER PART 3 OF ECRA 5331-02356.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 81,374 hrs · 31,009 cycles

FWD AND AFT CABIN EMERGENCY LIGHTS DO NOT COME ON WITH SWITCH AR MED AND 49VU CIRCUIT BREAKERS H05 AND H06 OPENED PER HAECO LCQ N R LP NO 9294465 GENERATED BY V039704 TROUBLESHOT EMERGENCY LIGHTS IAW A320 TSM 33-33-51-00-810-812-A REMOVED AND REPLACED 10WH AND 13WH IAW A320 MM 33-51-38 OPS CK G OOD IAW A320 MM 33-51-00-710-001A PERFORMED BY V061674 INSP BY V 077960 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1103644 SN OFF 8186 TT # 1249140 SN OFF 8228 IPC REFERENCE # 33-51-38-01B IPC REFERENCE # 33-51-38-01B POWER SUPPLY, C OFF 31-3350-9-9001 8186 ON 31-3350-9-9001 2917 POWER SUPPLY, C OFF 31-3350-9-9001 8228 ON 31-3350-9-9001 4893

Part: ANGLE — DAMAGED (FRAMES 73-74) · airframe 81,374 hrs · 31,009 cycles

EXTERNAL FUSELAGE SKIN FR73-74 AT STR33-34L HAS WAVINESS REF HAECO NR 9294186. REPLACED 3 EA FRAME CLIPS AT FR73-74 STR 33-34L IAW SRM 51-72-11 REPAIRED 2 O/S HOLES WITH BUSHINGS REF SRM 53-00-11-300. SRI 53- 00-11-205-029 PG 9 REQUIRES INSP AT 60000FC OR 120000FH FROM RPR EMBODIMENT. SUBSEQUENT INSP INTERVALS TBD. SKIN CONTOUR AFTER RPR WITHIN LIMITS IAW 51-10-00 FIG 16. WAVINESS NO MORE THAN .010 OVER 4 INCHES. OK TO DIP REF SRM 53-00-11-300-022 MUST BE REINSPECTED AT DEFINE D INTERVALS AS PER SRI 53-00-11-205-023 FISRT INSPECTION FROM REPAIR EMBODIMENT 60000 FC 120000 FLIGHT HOURS SUBSEQUENT INSPS TO BE DETERMINED. TOMC SMITH TOMC-APPROVAL FROM SC1ELBYC COMMENT REVIEWED QC REVIEWED RECORDS UPDATE RECORDS UPDATE T/A: 60,000 F/C OR 120,000 F/H.....DH

Part: WEB — CRACKED (FRAME 68) · airframe 81,374 hrs · 31,009 cycles

RT FWD WEB AT FRAME 68 +6" HAS CRACK JUST AFT OF R2 DOOR. REMOVED AND REPLACED FABRICATED NEW WEB AND INSTALLED @ R/H FWD FR 68 +6" AFT OF R-2 DOOR PER A320 GMM/UAL 07-35-05 PG 5 & SRM 5 1-2-11-911-001.

Part: DOOR SILL — CORRODED (R2 DOOR) · airframe 81,374 hrs · 31,009 cycles

R-2 DOOR SILL AFT UPPER SURFACE HAS CORROSION A3NB-53-3-6222 PER HAECO LCQ NR 9294212 GENERATED BY N078570 REPAIRED CORRODED AREA WITH REPAIR ANGLE & FILLER PIECES IAW AIR BUS A320 SRM 53-41-14-300-01 FIGURE 01 REPAIR PRINCEPLE 7 SHT 4 -3 FILLER 5.0" X 0.945" X 0.071", -2 ANGLE 9.08" X 1.855" X 0.07 1" WORK ACCOMPLISHED BY V924341 INSPECTED BY LC-66

Part: WEB — CRACKED (FRAME 68) · airframe 81,374 hrs · 31,009 cycles

LEFT FRAME 68 + 6" FWD WEB HAS A CRACK JUST AFT OF L2 DOOR. REMOVED AND REPLACED FABRICATED NEW WEB @L/H FR 68 +6" FWD WEB A ND INSTALLED PER GMM 07-35-05 PG 5 & STEP 8 & SRM 51-72 -11-911-001.

Part: DOOR SILL — CORRODED (R2 DOOR) · airframe 81,374 hrs · 31,009 cycles

R-2 DOOR SILL FWD EDGE 1EA FASTENER HOLE HAS CORROSION. REPLACED R2 DOOR SILL IAW AIRBUS A320 SRM 52-41-14-300-001 PRINCIPLE 9

Part: FITTING — CORRODED (L2 DOOR) · airframe 81,374 hrs · 31,009 cycles

L-2 DOOR SILL FWD CORNER FITTING HAS CORROSION (A3NB-53-3-6222), PER NR LOG PAGE NO. 9294217, GENERATED BY N078570. REMOVED AND REPLACED L2-DOOR SILL FWD CORNER FITTING IAW A320 SR M 51-72-11. MECH V061603 AND INSP BY V919150, PER NR LOG PAGE NO . 9294217.

Part: FITTING — CORRODED (L2 DOOR GIRT BAR) · airframe 81,374 hrs · 31,009 cycles

L-2 DOOR SILL AFT GIRT BAR FITTING AREA HAS CORROSION ON UPPER S URFACE AND AROUND FASTENER HOLES (A3NB-53-3-6222) PER NON ROUTIN E LOG PAGE NO. 9294219, GENERATED BY N078570. REMOVED AND REPLACED L2 DOOR SILL IAW A320 SRM 51-72-11-001. MEC H V061603 AND INSP BY V919150. PER NR LOG PAGE NO. 9294219.

Part: FITTING — CORRODED (L2 DOOR SILL) · airframe 81,374 hrs · 31,009 cycles

L-2 DOOR SILL AFT CORNER FITTING HAS CORROSION (A3NB-53-3-6222) PER NR LOG PAGE NO. 9294220. GENERATED BY N078570. L2 DOOR SILL TO BE REPLACED ON NR 44219. REMOVED AND REPLACED L2 DOOR SILL AFT CORNER FITTING IAW SRM 51-72-11. MECH V06160 3 AND INSP BY V919150. PER NR LOG PAGE NO. 9263497.

Part: CHECK VALVE — BROKEN (HYDRAULIC SYS) · airframe 80,619 hrs · 30,692 cycles

Y RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. HYD FOUND CHECK VALVE ON YELLOW SYSTEM MANIFOLD TO BE BROKEN. REPLACING CHECK VALVE AND THEN WILL LEAK CHECK.

Part: WARNING LIGHT — FALSE ACTIVATION (R1 DOOR SLIDE) · airframe 77,721 hrs · 29,388 cycles

DOOR 1R SLIDE SHOWS ARMED ON DOOR ECAM DIAGRAM. CREW REPORTED TO TOMC AFTER AIRCRAFT POWER DOWN AND REPOWER DOOR 1R INDICATION NOW NORMAL. NO FAULTS NOTED. OK FOR SERVICE.

Part: ALTIMETER — INACCURATE (STANDBY) · airframe 77,364 hrs · 29,213 cycles

STANBY ALTIMETER WAS ERRONEOUS DURING DESCENT, 450 FT HIGH AT LOWER ALTITUDES. REPLACED THE STANBY ALTIMETER IAW AMM 34-21-22.

Part: WARNING LIGHT — FALSE INDICATION (R1 DOOR SLIDE) · airframe 77,299 hrs · 29,176 cycles

R1 DOOR SLIDE SHOWED ARMED WHEN HANDLE IS DISARMED. OPERATED THE DOOR THRU THE ARM AND DISARM CYCLE, ALL ECAM WARNINGS AND VISUAL INDICATIONS ARE NORMAL IAW AMM 52-70-00

Part: SLIDE — CRACKED (OVERWING EXIT) · airframe 77,229 hrs · 29,145 cycles

RT OVERWING EMER SLIDE HAS CRACK, DELAM ON AFT ATTACH FLANGE. REPLACED RT OFF WING ESCAPE SLIDE REF AMM 25-62-42-000-001-A AND AMM 25-62-42-400-001-A.

Part: BATTERY — DISCHARGED (CABIN) · airframe 76,915 hrs · 29,020 cycles

EMERGENCY LIGHTS TEST FAULT AFT L BATTERY. REPLACED AFT L BATTERY PER MM 33-51-38. EMERGENCY LIGHTS TEST OK.

Part: BATTERY — FAULTY (CABIN) · airframe 76,549 hrs · 28,855 cycles

RT EMER LIGHT BATTERY AT RT EMER EXIT LOCATION FAILED TEST. REPLACED RT EMERGENCY LIGHTING BATTERY AT RT EMER EXIT LOCATION. OPS CHECK GOOD. REF AMM 33-51-38.

Part: INDICATOR — FALSE INDICATION (R1 DOOR) · airframe 76,549 hrs · 28,855 cycles

DOOR 1R SLIDE SHOWS ARMED EVEN THOUGH IT’S NOT. CLEANED ARM/DISARM CLEANED ARM/DISARM INDICATOR ON MED 1R. OPS CHECK NORMAL.

Part: WEB — CORRODED (THRESHOLD) · airframe 76,182 hrs · 28,685 cycles

FWD CARGO BAY INBD THRESHOLD HAS CORROSION IN MULTIPLE LOCATIONS. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53 -21-13, PAR 4B, & FIG 103. REMOVED & REPLACED THE FWD CARGO THRESHOLD TORSION BOX WEB IAW SRM 5 1-72-11, & 51-42-11

Part: FLOOR SUPPORT — CORRODED (FRAMES 69-70) · airframe 76,182 hrs · 28,685 cycles

LEFT FRAME FLOOR SUPPORT CORRODED AT FRAMES 69 - 70, STRINGER 23L UNDER SHEAR PLATE AREA. REMOVED AND REPLACED THE FRAME SUPPORT IAW SRM 51-72-11.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 76,182 hrs · 28,685 cycles

L2 DOOR FRAME 68 LOWER DOOR STOP ATTACH POINT, LOWER INBD HOLE HAD A CRACK INDICATION. HOLE REAMED, FREEZE PLUGGED AND REPAIRED PER SRM 53-41-12 PARA 5F FIG 205.

Part: FITTING — CORRODED (FWD CARGO DOOR) · airframe 76,182 hrs · 28,685 cycles

FWD CARGO DOOR CUTOUT CORNER FITTING IS OUT OF LIMITS DUE TO CORROSION. REMOVED AND REPLACED CORNER FITTING IAW SRM 51-42-11.

Part: SHEAR TIE — CORRODED (FRAME 43) · airframe 76,182 hrs · 28,685 cycles

FWD CARGO BAY, CLEAT AT FRAME 34, STRINGER 43L HAS CORROSION ON BOTTOM FLANGE & IS CRACKED. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-42-11, REV 118, & 51-72-11, REV 118.

Part: THRESHOLD — CORRODED (FWD CARGO) · airframe 76,182 hrs · 28,685 cycles

FWD CARGO BAY OTBD THRESHOLD HAS CORROSION AT MULTIPLE LOCATIONS. REMOVED AND REPLACED THE THRESHOLD IAW SRM 51-42-11, PARA 2.D, 2.E, 2.F.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 76,182 hrs · 28,685 cycles

FWD CARGO BAY SHEAR TIE AT FRAME 32, STRINGERS 40 - 41R CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 5 1-42-11, AND SRM 51-72-11, REV 118.

Part: STRINGER — CORRODED · airframe 76,182 hrs · 28,685 cycles

FOUND CORROSION AT FRAMES ABOUT 10 INCHES AFT FRAME 32, STRINGER 41L. BLENDED CORROSION ON THE STRINGER AND FOUND BEYOND LIMITS. REMOVED AND REPLACED THE STRINGER IAW SRM 51-70-0 0, PAR 3, 51-23-13, FIG 102, AND 51-72-11, REV 118.

Part: STRINGER SPLICE — CORRODED (FRAMES 30-31) · airframe 76,182 hrs · 28,685 cycles

FWD CARGO BAY STRINGER SPLICE 42L, FRAMES 30 -31 HAS CORROSION. BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-74-00 , 53-21-13 FIG. 102. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-72-11, REV 118.

Part: STRINGER — CORRODED (FRAME 32) · airframe 76,182 hrs · 28,685 cycles

FOUND CORROSION AT FRAME 32, STRINGER 43L. BLENDED CORROSION ON THE STRINGER AND FOUND BEYOND LIMITS. REMOVED AND REPLACED THE STRINGER IAW SRM 51-70-00, PAR 3, 53-21-13, FIG 102, AND 51-72-11, REV 118.

Part: SHEAR TIE — CORRODED (FRAME 34) · airframe 76,182 hrs · 28,685 cycles

FWD CARGO BAY FRAME 34 SHEARD TIE, STRINGERS 40 - 41L HAS CORROSION. REMOVED & REPLACED SHEAR TIE IAW SRM 51-72-11, PG 1, & 2, REV 118.

Part: THRESHOLD — CORRODED (AFT CARGO BAY) · airframe 76,182 hrs · 28,685 cycles

AFT CARGO BAY THRESHOLD HAS CORROSION . REMOVED & REPLACED THE THRESHOLD IAW SRM 51-42-11.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 76,182 hrs · 28,685 cycles

FWD CARGO BAY SHEAR TIE AT FRAME 32, STRINGERS 42 - 43L CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-4 2-11, REV 118.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 76,182 hrs · 28,685 cycles

FWD CARGO BAY SHEAR TIE AT FRAME 31, STRINGERS 40 - 41R CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-23-11, AND SRM 51-42-11, REV 118.

Part: SHEAR TIE — CORRODED (FRAME 33) · airframe 76,182 hrs · 28,685 cycles

SHEAR TIE CORRODED AT FRAME 33, STRINGERS 42 - 43L. REMOVED AND REPLACED THE SHEAR TIE.

Part: SHEAR TIE — CORRODED (FRAME 33) · airframe 76,182 hrs · 28,685 cycles

SHEAR TIE CORRODED AT FRAME 33, STRINGER 40 - 41R. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51- 72-11, AND SRM 51-42-11, REV 118.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 76,182 hrs · 28,685 cycles

FWD CARGO BAY SHEAR TIE AT FRAME 32, STRINGERS 41 - 42R CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11, AND SRM 51-42-11, REV 118.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 76,182 hrs · 28,685 cycles

FWD CARGO BAY SHEAR TIE HAS CORROSION FRAME 31, STRINGERS 40 - 41L. REMOVED & REPLACED SHEAR TIE IAW SRM 51-72-11, PG 1, 2, REV 118.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 76,182 hrs · 28,685 cycles

FWD CARGO BAY UNDER FLOOR, FRAME 31 SHEAR TIE BETWEEN STRINGERS 42 - 43L HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11, PG 1, AND 2 ,REVISION 118.

Part: SHEAR TIE — CORRODED (FRAME 33) · airframe 76,182 hrs · 28,685 cycles

FWD CARGO BAY FRAME 33 SHEAR TIE, STRINGERS 40 - 41L CORRODED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-72-11.

Part: STRINGER — DAMAGED (FRAMES 64-65) · airframe 76,182 hrs · 28,685 cycles

AFT CABIN STRINGER 19R BETWEEN FRAMES 64 AND 65 IS DAMAGED. REPAIRED THE STRINGER IAW SRM 53-00-13, FIG 20101, SHEET 3.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 76,182 hrs · 28,685 cycles

FWD CARGO BAY, FRAME 32 SHEAR TIE, STRINGERS 40 - 41L HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-72-11.

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · airframe 76,182 hrs · 28,685 cycles

RIGHT AFT EMERGENCY EXIT DOOR BOTTOM DOOR FRAME CORRODED IN CENTER INSIDE AND OUTSIDE. BLENDED CORROSION. REMOVED AND REPLACED DOOR FRAME IAW SRM 51-72-11

Part: STRINGER — CORRODED (FRAMES 54-55) · airframe 76,182 hrs · 28,685 cycles

AFT CARGO BAY STRINGER 43L HAS CORROSION AT 1 SPOT BETWEEN FRAMES 54 - 55. REMOVED AND REPLACED THE STRINGER FROM FRAMES 53 - 60 IAW SRM 51-72-11, AND 51-42-11.

Part: WEB — CORRODED (AFT CARGO) · airframe 76,182 hrs · 28,685 cycles

AFT CARGO BAY WEB IMMEDIATELY INBOARD OF THE THRESHOLD HAS CORROSION AT MULTIPLE LOCATIONS. REMOVED AND REPLACED THE TORSION BOX WEB IAW SRM 51-32-11.

Part: STRINGER — CORRODED (FRAMES 53-58) · airframe 76,182 hrs · 28,685 cycles

AFT CARGO BAY STRINGER 42L HAS CORROSION AT 2 SPOTS BETWEEN FRAMES 57 - 58. REMOVED AND REPLACED THE STR IAW SRM 51-72-11, AND 5 1-42-11

Part: STRINGER SPLICE — CORRODED (FRAMES 30-31) · airframe 76,182 hrs · 28,685 cycles

FWD CARGO COMPARTMENT STRINGER SPLICE FR 30-31 AT STRINGER 43L CORRODED. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-42-11, PG 7, AND TOP COATED AREA IAW SRM 51-75-12.

Part: STRINGER SPLICE — CORRODED (FRAMES 30-31) · airframe 76,182 hrs · 28,685 cycles

FWD CARGO BAY STRINGER SPLICE, FRAMES 30 - 31 AT STRINGER 41L CORRODED. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-42-11, PG 7, TOP COATED AREA IAW SRM 51-75-12.

Part: DIRECTOR — FAULTY (CIDS) · airframe 71,109 hrs · 26,457 cycles

FLIGHT ATTENDANT EMER CALL LIGHTS INTERMITTENTLY COME ON WITHOUT BEING SELECTED. CONFIRMED ERRATIC EMER CALL LIGHTS FLASHING AT VARIOUS TIMES. R & R CIDS DIRECTOR NR 1. OPERATIONS CHECKED GOOD.

Part: HYDRAULIC SYSTEM — LOW (YELLOW SYS) · airframe 68,110 hrs · 25,235 cycles

HYDRAULIC QTY LOW, YELLOW SYS. SERVICED YELLOW HYD SYS AS NEEDED IAW AMM 12-12-00.

Part: SOLENOID VALVE — LEAKING (HYDRAULIC SYS) · airframe 66,653 hrs · 24,676 cycles

WHILE PERFORMING TASK AMM 27-44-00-710-002 -A, FOUND YELLOW HYD SYS LEAK MEASUREMENT VLV INOPERATIVE. TRIED NEW PUSH BUTTON SWITCH PCN 110-0498, NO HELP. NEED NEW VLV ASSEMBLY FIN 3150GP. R & R MEASUREMENT SOLENOID VLV IAW MM 29-19-51 & PERFORMED OPERATIONS TEST IAW MM 27-44-00. ALL TESTED GOOD AIRCRAFT OK TO CONTINUE.

Part: OXYGEN MASK — DEPLOYED (CABIN) · airframe 66,582 hrs · 24,647 cycles

O2 MASK DEPLOYED ROW 28 DEF. REPACKED, DOOR OPENS SMOOTHLY.

Part: PROXIMITY SENSOR — FAULTY (NR 2) · airframe 67,123 hrs · 24,513 cycles

UPON ARRIVAL LGCIU 2 MESSAGE DISPLAYED ON UPPER ECAM DISPLAY. ACCOMPLISHED TROUBLE SHOOTING FIM TASK 32-31-00-810-839-A VERIFIED 28 V-DC AT PIN 10 AT LGCIU2. ACCOMPLISHED UP TO, BUT NOT INCLUDING STEP 4 SAME TROUBLESHOOTING REFERENCE. REPLACED LGCIU 2 & BSCU, NO HELP. REINSTALLED ORIGINAL UNITS. R & R PROX SENSOR 25GA IAW MM. ACCOMPLISHED LGCIU 2 TEST & NO FAULTS PRESENT.

Part: PROXIMITY SENSOR — FAULTY (EMERGENCY EXIT) · airframe 66,519 hrs · 24,619 cycles

LT AFT EMERGENCY EXIT DISPLAYED ON UPPER ECAM SCREEN. DOOR REPLACED AFT LT OVERWING PROX SENSOR IAW AMM.

Part: UNKNOWN — MALFUNCTIONED (CABIN TEMP) · airframe 66,514 hrs · 24,618 cycles

TRIM AIR SYS FAULT. TRIM AIR HI PRESS ECAM AT START OF TAKEOFF ROLL & 1 MIN INTO FLIGHT. RT AFT SWELTERING HOT, FWD FREEZING.

Part: SEAL — MISSING (TE FLAP) · airframe 66,474 hrs · 24,603 cycles

RT WING FLAP CANOE SEAL MISSING. RT WING MIDDLE FLAP CANOE 632CB OTBD SEAL PORTION REMOVED & EIGHT RIVETS REMOVED IAW CDL 27AC.

Part: SENSOR — OUT OF ADJUST (LANDING GEAR) · airframe 66,429 hrs · 24,586 cycles

ACCOMPLISHED GAP CHECK OF SENSOR 23GA. FOUND GAP TOO LARGE, INSTALLED 0.03 2 IN SHIM.

Part: DISPLAY — FAULTY (COCKPIT) · airframe 66,207 hrs · 24,501 cycles

CAPTS PFD INOPERATIVE INDMC POSITION 1-2-3. CAPTS PFD DOES NOT DISPLAY SHOWS WHITE DIAGONAL LINE. WHEN SELECTING CAPTS PFD XTR SWITCH, ADI DISPLAYED ON ND, HSI DISPLAYED ON PFD. COMPLIED WITH MEL CARD. REPLACED CAPT'S PFD,TESTED OK.

Part: BATTERY — FAILED (CABIN) · airframe 66,000 hrs · 24,427 cycles

EMERGENCY LIGHTS TEST FAILED WITH MESSAGE "L FWD BAT". REPLACED BATTERY ON LT FWD EMERGENCY LIGHTS POWER SUPPLY UNIT. EMERGENCY LIGHTS TEST PASSED.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 65,897 hrs · 24,385 cycles

EMERGENCY LIGHTING IS FAULTING BATTERY FWD LT. R&R THE SAME BATTERY PACK & FAULT CLEARED, RETESTED OKAY.

Part: SKIN — GOUGED (FUSELAGE) · airframe 65,569 hrs · 24,267 cycles

FUSELAGE SKIN GOUGED, 2 INCHES FWD OF FRAME 66 S26L. ACCOMPLISHED VISUAL INSPECTION NO CRACKS NOTED. BLENDED DAMAGED AREA IAW SRM 53-41-11. PERFORMED NDT, NO DEFECTS NOTED, INSTALLED RIVET WET.

Part: SEAL — LEAKING (NR 2 ENGINE) · airframe 65,342 hrs · 24,178 cycles

OIL LEAKING FROM NR 2 ENGINE RT SIDE. POSITIONED NR 2 ENGINE OIL BREATHER TUBE MATING GROMMET SEAL, CHECKED OIL, FOUND NORMAL.

Part: STRAP — UNSECURE (GIRT BAR) · airframe 65,331 hrs · 24,173 cycles

BOTH AFT ENTRY-SERVICE DOORS, WHITE STRAP MISSING FROM GIRT BAR. DOORS. FOUND STRAP AND SECURED IAW AMM.

Part: LINE — LEAKING (GALLEY WATER) · airframe 65,236 hrs · 24,138 cycles

THREE TO FOUR CUPS OF WATER FLOWED FROM UNDER COFFEEMAKER IN AFT GALLEY EVERY TIME AIRCRAFT STOPS OR SLOWS. FOUND EVIDENCE OF LEAK UNDER INBOARD COFFEEMAKER. REMOVED AND CLEANED AREA AND TIGHTENED WATER LINE THAT APPEARED TO BE LOOSE. INSTALLED COFFEEMAKER AND LEAK CHECKED AREA AND FOUND NO LEAKS. OK TO CONTINUE.

Part: LIGHT — INOPERATIVE (SEAT 28) · airframe 65,146 hrs · 24,104 cycles

EMERGENCY LIGHT ASSY AT SEAT 28 FOUND INOPERATIVE. R & R EMERGENCY LIGHT ASSY AT ROW SEAT 28, OPS CHECKED GOOD.

Part: IGNITION UNIT — INOPERATIVE (APU) · airframe 65,141 hrs · 24,103 cycles

APU WILL NOT CRANK ON START. TROUBLESHOT IAW TSM 49-40-00. R & R IGNITION UNIT REF AMM 49-41-38. OPS NORMAL.

Part: COVER — UNSECURE (R2 DOOR SLIDE) · airframe 65,027 hrs · 24,059 cycles

R2 DOOR SLIDE COVER LOOSE. R2 SLIDE PACK COVER FELL OFF. REINSTALLED.

Part: UNKNOWN — ODOR (CABIN) · airframe 64,969 hrs · 24,036 cycles

F/A REPORTED ELECTRICAL BURNING ODOR FROM AFT GALLEY DURING TAXI OUT, NO SMOKE. FOUND RT AFT GALLEY CEILING LIGHT BULB INTERMITTENT, REPLACED LAMPS SAME PROBLEM, INSPECTED AREA ABOVE AFT GALLEY IN CEILING AREA, NO EVIDENCE OF OVERHEATED OR BURNED COMPONENTS, NO EVIDENCE OF AIR LEAKS OR ODOR DETECTED IN AREA ON 5 MINUTE IDLE ENGINE RUN. NO ODOR COMING FROM COFFEEMAKERS, OVENS, OR GALLEY CHILLERS. NO EVIDENCE OF ODOR IN EITHER AFT LAV, OK FOR SERVICE.

Part: CIRCUIT BREAKER — SHEARED (GALLEY POWER) · airframe 64,405 hrs · 23,820 cycles

FOUND MAIN FWD GALLEY FEEDER "F" CIRCUIT BREAKER HEAD SHEARED OFF. REMOVED & REPLACED MAIN FWD GALLEY FEEDER "F" CIRCUIT BREAKER PER ASM:24-56-01. OPS CHECKED GOOD.

Part: AUDIO PANEL — FAULTY (VHF COMM) · airframe 64,256 hrs · 23,769 cycles

VERY HIGH FREQUENCY RADIO (VHF) 1 INOP. VHF 1 ALMOST UNREADABLE PROG TEXT: - ITEM ROLLED FORWARD. REMOVED AND REPLACED FAULTY NR 1 RMP. UNIT TEST OKAY.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 63,911 hrs · 23,636 cycles

L1 DOOR EXIT SIGN LOOSE. INSTALLED NEW EXIT SIGN LENS ASSY AND CHECKED SECURE.

Part: CABLE — FROZEN (R1 DOOR) · airframe 63,743 hrs · 23,566 cycles

R1 DOOR LEVER FROZEN, WOULD NOT OPEN. SLIDE PARTIALLY OUT. REPLACED FLEXIBLE CONTROL CABLE.

Part: BATTERY — FAILED (CABIN) · airframe 63,533 hrs · 23,491 cycles

EMERGENCY LIGHT SYSTEM FAIL TEST MSG EMERGENCY BATTERY AFT LEFT EMERGENCY BATTERY RIGHT MSG. REPLACED EMERGENCY BATTERY 12 WL AND 13 WL, OPS CHECK OKAY.

Part: LIFE VEST — OUT OF POSITION (CABIN) · airframe 63,530 hrs · 23,490 cycles

LIFE VESTS IMPROPERLY STOWED ROW 36. RE-INSTALLED VEST.

Part: WARNING LIGHT — FALSE INDICATION (FAN) · airframe 63,459 hrs · 23,464 cycles

LAVATORY AND GALLEY FAN FAULT DISPLAYED ON UPPER ECAM SCREEN. INSPECTED , OPS CHECKED GOOD.

Part: WATER SYSTEM — CONTAMINATED (GALLEY) · airframe 63,308 hrs · 23,413 cycles

LOUD VIBRATION IN AFT GALLEY. COULD BE WATER PUMP. STARTED WHEN SYS PRESSURE CAME UP. FOUND A LOT OF AIR IN AFT GALLEY SYSTEM. REMOVED BOTH COFFEEMAKERS AND ALL FAUCETS IN AFT GALLEY AND LAVS, NOISE WENT OFF AFTER ABOUT 4-4 SECONDS. INSTALLED BOTH COFFEEMAKERS. NOISE WAS STILL OFF.

Part: COMPUTER — FAULTY (FUEL SYSTEM) · airframe 63,246 hrs · 23,392 cycles

RIGHT WING TANK LO LVL DISPLAYED ON UPPER ECAM SCREEN. FUEL CREW COMMENTS: FUEL QUANT PLUS OR MINUS 1000 LBS. REPLACED FQIC 3QT AND ACCOMPLISHED QTY TEST. FQIC MR28429-163 FROM AC 4019.

Part: COMPUTER — FAULTY (ELAC) · airframe 62,961 hrs · 23,275 cycles

ELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. - F-CTL. RESET BOTH ELAC 1 & 2. PERFORMED OPERATIONAL TEST OF ELAC 1 AND 2 PER AMM. NO FAULTS. ELAC 2 FAULT SHOWED AGAIN AT POWER TRANSFER. REPLACED ELAC 2 PER AMM, OPS TESTED OKAY. PERFORMED CAT III PER AMM, OK.

Part: LEVER — BROKEN (PSU) · airframe 62,519 hrs · 23,096 cycles

SEAT 3DEF EMERGENCY OXYGEN DOOR FLAG PULL LEVER BROKEN. REPAIRED PSU TO SERVICEABLE CONDITION.

Part: BATTERY PACK — FAILED (CABIN) · airframe 62,519 hrs · 23,096 cycles

EMERGENCY TEST FAILS AT FWD FIGHT ATT PANEL. REPLACED RIGHT CENTER EMERGENCY BATTERY PACK, TESTED GOOD. INSP EMERGENCY LIGHT TEST OKAY.

Part: PIN — BROKEN (CABIN O2) · airframe 62,519 hrs · 23,096 cycles

O2 MASKS DROPPED IN ROW 34DEF. FOUND O2 PANEL LATCH BROKEN. FORWARDED TO MEL SECURED PANEL AT 34DEF & BLOCKED SEATS INOP. REPAIRED ROW 34 DEF 02 PANEL ACTUATOR LATCH PIN, OPERATIONAL DROP CHECK OK .

Part: BATTERY PACK — FAILED (CABIN) · airframe 62,519 hrs · 23,096 cycles

EMERGENCY TEST FAILS AT FWD FIGHT ATT PANEL. REPLACED RIGHT CENTER EMERGENCY BATTERY PACK, TESTED GOOD.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 62,487 hrs · 23,083 cycles

THE 10DEF MASKS DROPPED ON LANDING. SECURED AND WILL NEED DROP TEST AT 3 DAYS PER 35003. PER MT 35003 3 DAYS FOR DROP TEST. -OK - :ACCMP'D OPERATIONAL CHECK OF MANUAL MASK RELEASE PER MM TASK 35-23-00-710-001.

Part: SKIN — DAMAGED (L2 DOOR) · airframe 62,428 hrs · 23,058 cycles

L2 DOOR LOWER EXTERNAL SKIN DAMAGE WAS REPAIRED REF SRM 52-10-00 PARAGRAPH 5E FIG.205, CAT B PRP WAS ACCOMPLISHED BY REMOVING DAMAGE. DAMAGE REMOVAL VERIFIED WITH HFEC, AND INSTALLING A REPAIR DOUBLER.

Part: BATTERY — DISCHARGED (NR 2) · airframe 62,428 hrs · 23,058 cycles

DC GENERATION BATTERY DISCHARGED. SUPPLEMENTAL DATA UPDATE, CHANGED NR 2 MAIN BATTERY, OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (NR 1) · airframe 62,428 hrs · 23,058 cycles

2PB1 DC GENERATION BATTERY DISCHARGED. REPLACED 2PB1 BATTERY, NR 1 MAIN, OPS CHECKED GOOD.

Part: GIRT BAR — OUT OF POSITION (R1 DOOR) · airframe 62,105 hrs · 22,943 cycles

DOOR 1R WILL NOT ARM. RE-INSTALLED AND LACE GIRT BAR ASSY.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 61,942 hrs · 22,880 cycles

FUSELAGE DENTED BETWEEN FRAME 10 AND 11 AT STR 23R. INSTALLED DOUBLER REPAIR AND INSPECTED. MUST BE REINSPECTED AT 60000C FROM REPAIR EMBODIMENT.

Part: SEAT — LOOSE (COCKPIT) · airframe 61,268 hrs · 22,629 cycles

CAPTAIN'S SEAT IS LOOSE. ROCKS FORE AND AFT AND SIDE TO SIDE EXCESSIVELY. REPLACED SEAT ASSY.

Part: COMPUTER — FAULTY (COCKPIT) · airframe 61,188 hrs · 22,602 cycles

AFTER ENG START FLIGHT DECK SMELLED OF A STRONG ELECTRICAL BURNING SMELL. FOUND ODOR AT SEC3 COMPUTER. REMOVED & REPLACED SEC 3. SEE SEQ#1886001. ODOR NOW DISSIPATING. OPERATION CHECKING GOOD PER TASK.

Part: INTERFACE UNIT — FAULTY (FIRE WARNING) · airframe 61,007 hrs · 22,544 cycles

NR 2 ENG FIRE LIGHT AT ENG MASTER SWITCH DOES NOT ILLUMINATE DURING TEST. REF TSM 26-12-00, AWM 26- 12-02, MM33-14-33 AND MM 33-14-00, FOUND ANNUNCIATOR LIGHT TEST AND INTERFACE BOARD AT FAULT. INSTALLED NEW BOARD AND TESTED, OP CK'S NORMAL.

Part: ACCUMULATOR — LEAKING (HYD SYSTEM) · airframe 60,427 hrs · 22,335 cycles

CREW REPORTED INFLIGHT LOSS OF YELLOW SYS HYDRAULIC LOSS. FOUND LEAK NEAR PARKING BRAKE ACCUMULATOR. REMOVED & REPLACED YELLOW SYS BRAKE ACCUMULATOR IAW AMM. OPS AND LEAK CHECKED GOOD.

Part: OXYGEN MASK — DISLODGED (ROW 28) · airframe 60,289 hrs · 22,293 cycles

O2 MASKS FELL DOWN AT ROW 28. RESTOWED MASKS, NO EVIDENCE OF O2 ACTIVATION AND LATCH OPERATES NORMAL, OK TO CF PER MT 35-003.

Part: LANYARD — MISROUTED (R2 DOOR) · airframe 59,347 hrs · 21,904 cycles

SURVIVAL KIT LANYARD DOOR 2R NOT ROUTED CORRECTLY. SECURED LANYARD.

Part: LANYARD — MISROUTED (L2 DOOR) · airframe 59,347 hrs · 21,904 cycles

SURVIVAL KIT LANYARD DOOR 2L NOT ROUTED CORRECTLY. SECURED LANYARD.

Part: EXTINGUISHER — UNSERVICEABLE (CABIN) · airframe 59,044 hrs · 21,786 cycles

SEAL BROKEN ON H20 FIRE EXTINGUISHER IN AFT CABIN. REPLACED H2O FIRE EXTINGUISHER.

Part: OXYGEN MASK — DEFECTIVE (COCKPIT) · airframe 59,037 hrs · 21,783 cycles

CAPTAIN'S OXYGEN MASK MICROPHONE IS INOPERATIVE. REPLACED PER MM-35-12-41.

Part: PANEL — DAMAGED (RT WING) · airframe 59,009 hrs · 21,770 cycles

RT WING INBOARD LEADING EDGE PANEL SKIN BEHIND NR 1 RT SLAT HAS A HOLE IN IT. REPAIRED DAMAGED PANEL. NEEDS TO BE RE-INSTALLED AND PAINTED. PANEL HAS BEEN PREVIOUSLY PAINTED AND INSTALLED.

Part: LIFE VEST — MISSING (CABIN) · airframe 58,907 hrs · 21,732 cycles

MISSING A CREW LIFEVEST ABOVE ROW 36.

Part: COMPUTER — FAULTY (FUEL QUANTITY) · airframe 58,089 hrs · 21,394 cycles

CTR TK PUMP 1 LOW ECAM, FLT DIVERTED. FUEL INNER QTY INDICATION IS LOCKED UP, LEFT INNER APPEARS INACCURATE. REMOVED AND REPLACED FQIC IAW AMM. BITE CHECKS NORMAL. OPERATED CROSSFEED VALVE MULTIPLE TIMES WITH ALL INDICATION NORMAL. RAN BOTH ENGINES IAW THE JRH AND MONITORED FUEL USED AND FUEL FLOW WITH THE CROSSFEED VALVE OPEN AND CLOSED. FUEL FLOW AND FUEL USED FROM EACH TANK WAS EQUAL WITH CROSSFEED VALVE OPEN OR CLOSED. LEFT AND RIGHT FUEL BOOST PUMPS OPERATED NORMAL. AIRCRAFT IS OK FOR SERVICE.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 57,933 hrs · 21,336 cycles

FIRST OFFICER'S FWD WINDSHIELD FOR INOP HEAT. THE SENSOR AND WHC HAVE ALREADY BEEN REPLACED, NO HELP. REPLACE PER AMM. REPLACED FIRST OFFICER'S WINDSHIELD PER MM.

Part: AMU — INOPERATIVE (COCKPIT) · airframe 57,808 hrs · 21,292 cycles

CAPT OXYGEN MASK MICROPHONE IS INOPERATIVE. SUPPLEMENTAL DATA UPDATE MECHANIC SWAPPED MASKS, NO HELP. SUSPECT ELECTRICAL CONNECTION AT BOX. REPLACED AMU IAW MM. ACCOMPLISHED OPS CHECK OF CAPT O2 MASK MIC OKAY.

Part: TRANSCEIVER — FAULTY (VHF SYS) · airframe 57,813 hrs · 21,295 cycles

CAPT HEADSET CANNOT RECEIVE. STARTED DURING DESCENT. SPEAKER AND TRANSMIT WORKS FINE. REPLACED VHF 1. SYSTEM CHECKS NORMAL WHILE AT THE GATE USING 128.95. CAPTS HEADSET STILL INOP, COMPLIED WITH MEL. LOSS OF TRANSMISSION FROM CAPT'S BOOMSET- NEED AMU (1RN). REPLACED AMU REF MM 23-51-34, SYSTEM CHECKS NORMAL AT THE GATE.

Part: DRAIN LINE — LEAKING (NR 2 ENGINE) · airframe 57,747 hrs · 21,263 cycles

NR 2 ENG LEAKING FUEL. RAN NR 2 ENG REF AMM 71-70- 00. FOUND FUEL FROM "CORE", 12 DPM. SHUT ENGINE DOWN, FUEL LEAK, 3 DROPS PER MINUTE FROM "CORE". ACCEPTABLE TO FLY ON 25 HRS PROVIDED THE 25 HR FLYBACK LIMIT IS NOT EXCEEDED. FUEL LEAK IS FROM DRAIN MAST, "CORE' DRAIN PORT. REMOVED DRAIN LINES FROM MASTER ACTUATOR LPC BLEED, VSV ACTUATOR, ACC ACTUATOR, LPC SLAVE ACTUATOR. BAGGED DRAINS & ACCOMPLISHED 5 MIN IDLE RUN. NO LEAKS FOUND FROM ANY COMPONENT. SECURED DRAIN LINES.

Part: DOUBLER — LEAKING (RT WING) · airframe 57,216 hrs · 21,033 cycles

RT WING FIRST FLAP TRACK FAIRING OTBD OF ENG HAS FUEL LEAKING OUT OF WEEP HOLE. LEAK EXIT POINT IS BETWEEN AFT MOUNT DOUBLER PLATE AND WING. AFT INBD CONNER OF THE RT WING NR3 FLAP TRACK BEAM. ALSO LOWER HI-LOCK IN AFT SPAR JUST BEHIND NUT OF AFT CENTERING PIN OF BEAM. AREAS MARKED. RESEALED SUSPECTED FASTENERS. WILL NEED TO BE LEAK CHECKED AFTER 2300-21DEC. REFUELED RT WING AND LEAK CHECKED ACCESS PANELS 640EB AND 640GB. NO LEAKS NOTED.

Part: SKIN — GOUGED (L2 DOOR) · airframe 56,773 hrs · 20,831 cycles

AFT ENTRY DOOR (L2) EXTERIOR SKIN LOWER SECTION AT MID-SPAN GOUGED. MAJOR REPAIR ACCOMPLISHED: EVALUATED DAMAGE FOR CRACK. DENT OUT OF LIMITS. FABRICATED & INSTALLED EXTERNAL DOUBLER REPAIR.

Part: STRINGER — CORRODED (42 LEFT) · airframe 56,773 hrs · 20,831 cycles

CORROSION IN AFT PIT FR 56-57 AT STRINGER 42L. MAJOR REPAIR ACCOMPLISHED: CUT OUT CORRODED STRINGER SECTION. FABRICATED & INSTALLED STRINGER SPLICE REPAIR.

Part: STRINGER — CORRODED (30 RIGHT) · airframe 56,773 hrs · 20,831 cycles

CORROSION ON STRINGER 30R AT FRAME 65 OUTFLOW VALVE. MAJOR REPAIR ACCOMPLISHED: CORRECT STRINGER LOCATION IS 31R. REMOVED CORRODED STRINGER & FABRICATED & INSTALLED STRINGER SPLICE REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,773 hrs · 20,831 cycles

EXISTING FUSELAGE SKIN REPAIR IS DENTED AT FR23 AND STR 23L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED EXISTING REPAIR & FABRICATED & INSTALLED NEW EXTERNAL DOUBLER REPAIR.

Part: STRAP — OUT OF POSITION (L1 DOOR SLIDE) · airframe 56,389 hrs · 20,659 cycles

NR1 MED LT SLIDE ASSY SURVIVAL STRAP IS NOT VISIBLE. ROUTED SURVIVAL STRAP.

Part: STRAP — MISROUTED (R1 DOOR SLIDE) · airframe 56,389 hrs · 20,659 cycles

NR 1 RT MED SLIDE ASSY SURVIVAL STRAP IS NOT VISIBLE. ROUTED SURVIVAL STRAP.

Part: STRAP — MISROUTED (L2 DOOR SLIDE) · airframe 56,389 hrs · 20,659 cycles

LEFT NR 2 MED SLIDE ASSY SURVIVAL STRAP IS NOT VISIBLE. ROUTED SURVIVAL STRAP.

Part: STRAP — MISLOCATED (R2 DOOR SLIDE) · airframe 56,389 hrs · 20,659 cycles

NR 2 RT MED SLIDE ASSY SURVIVAL STRAP IS NOT VISIBLE.

Part: BATTERY — FAULTY (MASTER) · airframe 55,143 hrs · 20,134 cycles

ELEC BAT 1 FAULT ECAM AT GATE 13V 0A. REPLACED BATTERY NR 1 AND THE BATTERY CHARGE LIMITER. TESTS 'PASS' INDICATIONS NORMAL.

Part: SLIDE — FAULTY (R1 DOOR) · airframe 54,732 hrs · 19,949 cycles

SLIDE INDICATION ON ECAM. ARMING HANDLE OPERATED NORMAL WITH SLIDE REMOVED. SUSPECT BAD SLIDE. SLIDE ORDER ON AOG R2295. NEW SLIDE IS PLANESIDE. WORKING INSTALL. REPLACED SLIDE ASSY. ALSO ADJ PROX SW 4WN2 TARGET. ALL OPERATIONS NORMAL.

Part: MICROPHONE — FAULTY (OXYGEN MASK) · airframe 54,496 hrs · 19,843 cycles

2ND OBSVR SEAT O2 MASK MIC NOTED INOP DURING TROUBLESHOOT CAPTS INOP O2 MASK MIC. VERIFIED AUDIO CONTROL FUNCTIONS OPS NORMAL OTHERWISE. INOP 2ND OBSVR SEAT. REPLACED 2 OBSVR MASK.

Part: MICROPHONE — FAULTY (OXYGEN MASK) · airframe 54,496 hrs · 19,843 cycles

CREW REPORT: CAPT O2 MASK MIC NOT TRANSMITTING. SWAP O2 MASK WITH 1ST OBSERVER'S. CAPTAIN'S O2 MASK, OPS NORMAL. AFTER SWAPPING 1ST OBSVR NOW ALSO WORKING. SUSPECT INTERMITTENT OPS. INOP 1ST OBSERVER'S SEAT. REPLACED 1ST OBSERVER'S MASK.

Part: STRAP — MISROUTED (DOOR SLIDE) · airframe 54,254 hrs · 19,744 cycles

FOUND NR 1 RT MED SLIDE WITH WHITE SURVIVAL KIT STRAP NOT ATTACHED TO FWD END OF GIRT BAR RELEASE TRIGGER. ROUTED BOTH WHITE AND YELLOW STRAPS CORRECTLY.

Part: STRAP — MISROUTED (DOOR SLIDE) · airframe 54,254 hrs · 19,744 cycles

AFT RT ENTRY DOOR SLIDE YELLOW RELEASE STRAP IS NOT ROUTED THROUGH RELEASE TRIGGER ON FWD GIRT BAR FITTING. ROUTED AND ATTACHED CORRECTLY BOTH WHITE AND YELLOW STRAPS. STRAP CAPABILITIES FULLY RESTORED.

Part: STRAP — MISROUTED (DOOR SLIDE) · airframe 54,254 hrs · 19,744 cycles

AFT LT ENTRY DOOR SLIDE YELLOW RELEASE STRAP IS NOT ROUTED THROUGH RELEASE TRIGGER ON FWD GIRT BAR FITTING. ROUTED BOTH WHITE AND YELLOW STRAPS CORRECTLY. STRAP CAPABILITIES FULLY RESTORED.

Part: OVEN — OVERHEATED (FWD GALLEY) · airframe 52,678 hrs · 19,036 cycles

OVEN OVERHEAT, FLT DIVERTED. OVEN OVERHEAT LEAD CABIN CREW TO DISCHARGE HALON FIRE EXTINGUISHER INTO THE OVEN. NO FLAMES WERE EVER OBSERVED AND ANY OVERHEAT WAS CONTAINED WITHIN THE OVEN. FWD GALLEY HALON FIRE EXTINGUISHER WAS REPLACED. REPLACED FWD OVEN. OPS OKAY.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 51,814 hrs · 18,692 cycles

EMERGENCY LIGHT AT 20C INOP, SUSPECT BROKEN WIRE. REPLACED EMERGENCY LIGHT ASSY. LIGHT OP CHKS OK.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 51,557 hrs · 18,598 cycles

B-ELEC PUMP OVHT DISPLAYED ON UPPER ECAM SCREEN. RTFL. REPLACED BLUE HYD PUMP AND CASE DRAIN FILTERS. LEAK CHECK OK.

Part: MOUNT — OUT OF POSITION (DOOR 2R GIRT BAR) · airframe 51,248 hrs · 18,481 cycles

DOOR 2R ARMING LEVER IS NOT FLUSH WHEN ARMED. FOUND GIRT BAR FLOOR MOUNTS OUT OF POSITION. REPOSITIONED, ACP DOOR 2R SLIDE AND FLOOR MOUNTS ARE CORRECTLY INSTALLED.

Part: MOUNT — OUT OF POSITION (GIRT BAR) · airframe 51,248 hrs · 18,481 cycles

DOOR 2R ARMING LEVER IS NOT FLUSH WHEN ARMED. FOUND GIRT BAR FLOOR MOUNTS OUT OF POSITION, REPOSITIONED.

Part: MOUNT — OUT OF POSITION (GIRT BAR) · airframe 51,248 hrs · 18,481 cycles

DOOR 2R ARMING LEVER IS NOT FLUSH WHEN ARMED. FOUND GIRT BAR FLOOR MOUNTS OUT OF POSITION. REPOSITIONED GIRT BAR FLOOR MOUNTS.

Part: FIRE BOTTLE — UNSECURE (AFT LAVATORY) · airframe 50,196 hrs · 18,043 cycles

AFT LAV WALL FIRE EXTINGUISHER FELL OUT OF BRACKET. SECURED BOTTLE.

Part: OXYGEN BOTTLE — LOW PRESSURE (CABIN) · airframe 50,196 hrs · 18,043 cycles

THE O2 BOTTLE LOW AT FIRST CLASS LOCATION. REPLACED O2.

Part: COMPUTER — FAULTY (SLAT FLAP CONTRL) · airframe 47,211 hrs · 16,990 cycles

FLAPS ARE SLOW TO EXTEND. SFCC FAULTY. REPLACED SLAT FLAP CONTROL COMPUTER.

Part: BOTTLE — LOW (CREW OXYGEN) · airframe 46,236 hrs · 16,632 cycles

THE CREW O2 NEEDS SERVICE. CREW REPORTED CREW O2 READS -TOO FULL- MECH SERVICED O2 SYSTEM TO CORRECT PRESSURE. FIVE DAYS LATER - CREW REPORTS O2 -TOO LOW- SERVICED O2 SYSTEM TO 1820 PSI. NO REPEATS SINCE.

Part: CONTROL UNIT — MALFUNCTIONED (MLG) · airframe 44,284 hrs · 15,894 cycles

GEAR DID NOT RETRACT PROPERLY ON DEPARTURE. ALL OK ON 2ND ATTEMPT. [SUP 05-29-07] REPLACED NR 2 LANDING GEAR CONTROL AND INDICATING UNIT AND LANDING GEAR SELECTOR VALVE. AT OVERHAUL, NOTHING WAS FOUND TO BE OUT OF SPEC WITH THE LGCIU OR THE SELECTOR VALVE. LATER IT WAS DETERMINED THAT THE PROXIMITY SENSOR WAS FAULTY AFTER THE SAME FAULT OCCURRED SEVERAL FLIGHTS LATER.

Part: BLEED AIR SYS — LEAKING (LT WING) · airframe 44,241 hrs · 15,875 cycles

DIVERTED DUE TO A LEFT WING BLEED LEAK. LT WING LEAK DISPLAYED ON UPPER ECAM SCREEN-AIR. FOUND LOOSE DUCTING AND CLAMPS JUST ABOVE THE EXTERNAL AIR CART HOOK UP. RESEATED DUCT AND RESECURED CLAMPS NO FURTHER DEFECTS NOTED. ACCOMPLISHED LEAK CHECK OF DUCK AND NO LEAKS NOTED. ECAM MESSAGE GONE AND SYSTEM OPS CHECKS OK.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 44,016 hrs · 15,784 cycles

FOUND LEFT AND RIGHT KEELBEAM TO BELLY FAIRING SUPPORT FAIRING ATTACH ANGLES ARE CRACKED AT FRAME 46. MAJOR REPAIR ACCOMPLISHED: MFG'D & INSTALLED REPAIR ANGLE SECTION.

Part: WIRE — CUT (EMERGENCY LIGHTS) · airframe 43,956 hrs · 15,766 cycles

EMERGENCY LIGHT TEST INDICATES EPSU COM FWD L AND EPSU EXT LOAD FWD L ON CIDS 1 GROUND SCANNING. EPSU SHOWS FAULT EXT LOADS. FOUND BAD SPLICE ON WIRE 5109, REPLACED WIRE BETWEEN 2871VC AND 2819VC. WIRE 5109 OPERATION TEST FOR EPSU OK.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 43,919 hrs · 15,754 cycles

AFTER REINSTALLING DOOR 2L SLIDE WHILE ACP EMERGENCY LIGHT TEST FAILS TEST SHOWS EPSU COM 1 LT ON CIDS PANEL. MSG WAS EPSU EXT LOADS FWD LT AND COM FWD LT. REPLACED EPSU AND BATTERY, NO HELP. REINSTALLED ORIGINAL EPSU AND BATTERY. ACCOMPLISHED TEST, TEST PASSED, NO FAULTS.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 43,911 hrs · 15,752 cycles

FOUND EMERGENCY LIGHT TEST FAILED AT 3SV. REPLACED LEFT OVERWING EMERGENCY EXIT EPSU BATTERY. EMERGENCY LIGHT TEST PASSED.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 43,817 hrs · 15,715 cycles

FWD L COMM MSG ON TEST EMERGENCY LIGHT SYSTEM TEST. REPLACED EPSU. EMERGENCY LIGHT TEST PASSED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,552 hrs · 15,620 cycles

CABIN EMERGENCY LIGHT TEST FAILED, FAULTS INT LOADS EMER R AND COMM EMER R. REPLACED EPSU. OPS CHECKS GOOD.

Part: LIGHT — ILLUMINATED (CABIN) · airframe 43,531 hrs · 15,612 cycles

THE 1R, 1L DOOR EMERGENCY EXIT LIGHTS ILLUMINATED. ALL OTHER LIGHTS OFF AS NORMAL. REPLACED BATTERY AND 28V FUSE ON POWER SUPPLY. OPS CHECKS OK.

Part: UNKNOWN — SMOKE (CABIN) · airframe 43,492 hrs · 15,599 cycles

RETURN TO FIELD DUE TO SMOKE IN CABIN. REPLACED READING LIGHT POWER SUPPLY AT SEAT 3AB, INSPECTED OVERHEAD AREA FROM 1AB THROUGH 8AB, NO EVIDENCE OF SMOKE OR FIRE. NO SMELL OF SMOKE IN CABIN DURING AIRCRAFT TAXI. ALL CABIN LIGHTS WORKS NORMAL.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHT) · airframe 43,491 hrs · 15,597 cycles

"INT LOADS FWD L" FAULTING DURING EMERGENCY LIGHT TEST. REPLACED 10WL POWER SUPPLY AND 12WL. OPS CHECKED GOOD.

Part: LANYARD — MISROUTED (L2 DOOR SLIDE) · airframe 43,035 hrs · 15,443 cycles

REROUTE SURVIVAL KIT LANYARD ON DOOR 2L SLIDE RAFT. REROUTED LANYARD.

Part: CONTROL UNIT — MALFUNCTIONED (MLG DOORS) · airframe 42,171 hrs · 15,126 cycles

ON SHORT FINAL GEAR DOWN AND LOCKED BUT -LG DOORS NOT CLOSED- ECAM AND THEN LGCIU 1 AND 2 FAIL MESSAGES. REPLACED LGCIU 1.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 39,788 hrs · 14,255 cycles

LARGE DEEP SCRATCHES APPROXIMATLEY 24-28 INCHES LONG APPROXIMATELY 8 INCHES BEHIND FWD FUSELAGE BULKHEAD JUST AFT OF NOSE RADOME, FROM BELOW WATER LINE TO JUST BELOW RVSM AREA LT SIDE OF FUSELAGE. MAJOR REPAIR REPORTING. BLENDED SCRATCHED AREA PER SRM 53-11-11-101 AND SRM 53-00-11-101 FOR RVSM COMPLIANCE.

Part: TRANSCEIVER — FAILED (WX RADAR SYS) · airframe 38,201 hrs · 13,674 cycles

WX RADAR FAILED INFLIGHT. WEATHER RADAR RECEIVER / TRANSMITTER WAS DEFECTIVE. SHOP FINDINGS INDICATED A R/T FAULT. WXR R/T WAS REPLACED, AND NO FURTHER ASSOCIATED PROBLEMS OCCURRED.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 34,083 hrs · 12,295 cycles

DURING CHECK OF EMERGENCY LIGHTS, PTP PANEL FAULTED MESSAGE EXT LOADS FWD LEFT. FOUND WIRE 3351-5109 BROKEN AT DOOR 1-LEFT HINGE POINT UNDER CANVESS CONDUIT. THIS IS THE WIRE TO POWER DOOR 1-LEFT SLIDE LIGHTS. REPAIRED BROKEN WIRE WITH E-BUTT SPLICE, SYS OPS NORMAL IN ALL MODES.

Part: FLAP — FAILED (WINGS) · airframe 33,309 hrs · 12,040 cycles

FLIGHT LANDED SAFELY WITH ZERO FLAPS. ECAM FCTL FLAPS LOCKED WITH CFDS MSG FLP 1 OVERSPEED RT CHECK FLP MECH DRIVE. RT NR 1 FLAP ACTUATOR 6255CM SHAFT WAS FOUND LOOSE AND HAD MORE THAN 0.25 INCH OF RADIAL PLAY. THE CONNECTING U-JOINTS WERE ALSO FOUND LOOSE AND WORN. THE FAULTY FLAP ACTUATOR 6255CM AND THE U-JOINTS WERE REPLACED. OPERATIONS CHECK NORMAL.

Part: SUPPORT BEAM — CORRODED (FUSELAGE) · airframe 33,304 hrs · 12,038 cycles

AFT CABIN STRUCTURE SUPPORT BEAM AT FRAME 67 RBL 50 CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED FLOOR SUPPORT.

Part: SILL — CORRODED (FUSELAGE) · airframe 33,304 hrs · 12,038 cycles

AFT PASSENGER ENTRY DOOR (L2) DOOR SILL PLATE AT FRAME 68 IS CORRODED AT FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NESTED ANGLE & FILLER REPAIR.

Part: SENSOR — MALFUNCTIONED (THRUST REVERSER) · airframe 36,530 hrs · 13,121 cycles

NR 2 ENGINE REVERSER FAULT LIGHT ILLUMINATED. THE CAUSE WAS THE MAIN LANDING GEAR SENSOR 22GA. SENSOR 22GA WAS REPLACED. THE FLIGHT MANUAL PROCEDURES FOR ABNORMAL AND EMERGENCY SECTION 3.03.70 PG 1 SEQ 035 REV 24 WAS REVIEWED AND IT WAS FOUND THAT THE REVERSER FAULT LIGHT ALONE IS NOT CAUSE FOR DIVERSION.

Part: DAMPENER — LEAKING (GREEN SYSTEM) · airframe 32,498 hrs · 11,760 cycles

LANDED UNDER AMBER ALERT DUE TO FAILURE OF GREEN HYDRAULIC SYSTEM. YAW DAMPER NR 1 WAS FOUND LEAKING. SUBSEQUENT REPLACEMENT WITH NEW YAW DAMPER AND OPERATIONS CHECK WERE ACCOMPLISHED WITH NO FURTHER ANOMALY.

Part: SKIN — DENTED (NR 1 LT SLAT) · airframe 30,143 hrs · 10,924 cycles

SKIN ON NR 1 LT SLAT LEADING EDGE IS DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED FLUSH SKIN REPAIR ON #1LH SLAT L/E.

Part: COMPUTER — MALFUNCTIONED (FUEL SYSTEM) · airframe 29,629 hrs · 10,731 cycles

FLIGHT CREW SUSPECTED FUEL LEAK INFLIGHT. SUPPLEMENTAL DATA UPDATE INSPECTED AIRPLANE AND FOUND NO FUEL LEAK. TRANSFERRED FUEL AND TAXI CHECKED AIRPLANE AND UNABLE TO FIND A FUEL LEAK. FUEL QUANTITY CHECKED AND FOUND WITHIN LIMITS BY COMPARING INDICATION AND FUEL LEVEL MAGNETIC LEVEL INDICATORS. REPLACED FQIC TO CLEAR WRITE-UP THAT THE SYSTEM SHOWED DEGRADED.

Part: OXYGEN MASK — MALFUNCTIONED (COCKPIT) · airframe 22,000 hrs · 7,908 cycles

CREW REPORTED THAT WHEN THEY PUT ON THEIR OXYGEN MASK, THEY LOST ALL PRESSURE. *S/D* TESTED OXYGEN MASKS. FOUND OPERATION NORMAL. SERVICED OXYGEN CYLINDER, TESTED ON/OFF SWITCH, MASKS OPERATED NORMALLY.

Part: OUTFLOW VALVE — FLUCTUATES (AFT FUSELAGE) · airframe 21,315 hrs · 7,673 cycles

PASSING THROUGH 18,000 FEET, LARGE FLUCTUATIONS IN CABIN VERTICAL SPEED (SYS 1). *S/D* REPLACED OUTFLOW VALVE AND BOTH PRESSURE CONTROLLERS.

Part: MANIFOLD — LEAKING (HYDRAULIC SYSTEM)

ON DEPARTURE OUT OF IAD FLT 231 LOST YELLOW HYD SYSTEM. COMPLIED WITH AFM. CPT AND DISPATCH AGREED ON CONTINUING TO SJC. *S/D* FOUND GROUND SERVICE MANIFOLD LEAKING. REPLACED MANIFOLD PER AMM. LEAK CHECKED GOOD.

Part: ACTUATOR — FAILED (LT YAW DAMPER)

DIVERTED TO ATL DUE TO LOSS OF HYDRAULIC PRESSURE. *S/D* LT YAW DAMPER ACTUATOR DEVELOPED A PIN HOLE LEAK WHICH CAUSED THE HYD SYSTEM (GREEN) TO BLEED DOWN. ACTUATOR (P/N SC4700-3), (S/N 5030), MR27258-1035. ACTUATOR WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — OUT OF ADJUST (EMER EXIT DOOR)

LEFT FWD OVERWING DOOR GIVING WARNING ECAM MSG. THE LEFT FWD OVERWING DOOR PROXIMITY SWITCH AND TARGET WAS MISALIGNED WHICH RESULTED IN THE ECAM WARNING MESSAGE. THE TARGET WAS ADJUSTED PER AMM TASK 52-71-13-400-001 TO CORRECT THE PROBLEM.

Part: LIGHT — INOPERATIVE (CABIN)

EEL EXIT LIGHTS AT DOOR 2L AND 2R INOPERATIVE.

Part: SAFETY VALVE — FAILED (LANDING GEAR)

AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. WHEELS APPEARED TO VISUALLY CYCLE LOCKED AND UNLOCKED. ECAM MESSAGE L-G NOT UPLOCKED. RECYCLED GEAR AND RETRACTED OK. *S/D* REPLACED SAFETY VALVE. SOLENOID WAS OVERHEATING. SHOP TEST INDICATED NON-OPERATING PILOT VALVE. TEARDOWN INDICATED SCORING ON PILOT VALVE SLIDE.

Part: BOOST PUMP — FAILED (CTR FUEL TANK)

CENTER FUEL TANK LOW PRESSURE INDICATION RESULTED IN RETURN TO FIELD AFTER TAKEOFF. CENTER WING TANK BOOST PUMP THERMAL FUSES TRIPPED. REPLACED BOTH CENTER TANK BOOST PUMPS.

Part: LIGHT — INOPERATIVE (CABIN)

FAILED CABIN EMERGENCY LIGHT TEST PER NR 3 SERVICE CHECK. FAULT MESSAGE IS COMM EMER L. NOTED THAT CENTER AISLE EMERGENCY LIGHT AND LT OVERWING LIGHTS INOP.

Part: BATTERY PACK — DISCHARGED (CABIN)

SEAT EEL LIGHTS ARE INOPERATIVE AT SEAT ROWS 13 THROUGH 15 AND 19 THROUGH 21. *S/D* REPLACED RIGHT HAND AFT ESCAPE PATH BATTERY PACK.

Part: WINDOW TRACK — CRACKED (RT COCKPIT)

FIRST OFFICER'S SLIDING WINDOW LOWER RAIL TRACK FOUND CRACKED. SUPPLEMENTAL DATA UPDATE: REPAIRED TRACK PER STRUCTURAL REPAIR MANUAL SRM-55-11-12.

Part: GIRT TUBE — WORN (SLIDE)

SLIDE REMOVED FOR OVERHAUL. SLIDE HAD 3 HOLES ON THE LOWER SIDE OF THE GIRT INFLATION TUBE. REPAIRED SLIDE PER VENDORS MANUAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

MID CABIN EMERGENCY ESCAPE PATH LIGHTING GOES OUT AFTER ONE MINUTE OF OPERATION. REPLACED MID CABIN EMERGENCY LIGHTING BATTERY PACKS AND OPERATED NORMAL.

Part: APU — SMOKING (APU COMPT)

SMOKE IN CABIN AFTER ENGINE START, RETURNED TO GATE. REPLACED APU AND OPERATIONALLY CHECKED NORMAL WITH NO ODOR IN CABIN.

Part: OIL COOLER — LEAKING (APU)

EXPERIENCED STRONG ODOR AFTER TAKEOFF. ODOR WAS EVIDENT THROUGHOUT CABIN AND FLIGHT RETURNED TO BOSTON. THE SOURCE OF THE ODOR WAS AN OIL LEAK FROM THE APU OIL COOLER ASSEMBLY AT THE IN OIL LINE UNION. OIL COOLER WAS REPLACED AND OPERATIONALLY CHECKED NORMAL.