N406UA

Part: SEAL — CRACKED (NR 2 PYLON) · airframe 84,671 hrs · 32,964 cycles

PDA 2 #2 ENG INBD SIDE PYLON TO NACELLE FLEX SEAL (SECOND FROM AFT) CRACKED AND MISSING A SEGMENT. PHOTO ADDED REF ECRA 5450-02357 REV- B FIGURE 3 ITEM 100 IS CRACKED & MISSING A SECTION. PERFORMED INTERIM REPAIR PER PART 1D AND APPLIED SPEED TAPE. ISSUE DIP TO ACCOMPLISH VISUAL INSP PER PART 2A ONCE EVERY FLIGHT CYCLE & ACCOMPLISH PERMANENT REPAIR PER PART 3 WITHIN 50 FLIGHT HOURS. APPROVED THE DIP FOR THE INBOARD PYLON TO NACELLE FLEX SEAL. ACCOMPLISH VISUAL INSPECTIONS OF THE SPEED TAPE ONCE EVERY FLIGHT CYCLE. ACCOMPLISH PERMANENT REPAIR PER PART 3 OF EC/RA 5450-02357 WITHIN 50 FLIGHT HOURS. TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: STRINGER — CRACKED (FRAMES 35-36) · airframe 83,893 hrs · 32,603 cycles

LH STR 30L BETWEEN FR 35-36 IS CRACKED. -AD TASK A3NB-53-4-6159- GENERATED BY MECH V892442 AT HAECO LCQ. WORK GENERATED ON N/R 9292184/ 44184. INSTALLED REPAIR DOUBLER & FILLER @ L/H STR 30L BETWEEN FR35-36 PER AIRBUS REF 80875677/025 ECRA 5331-02693 AND REO-L22914 THIS REPAIR FOUND TO BE A MAJOR REPAIR WITH NO RE-INSP CATEGORY A BY MECH V061737

Part: DOOR FRAME — CRACKED (R2) · airframe 83,893 hrs · 32,603 cycles

R2 DOOR FRAME 68 STOP #1 LOWER INBOARD HOLE IS CRACKED IN THE WE B AT 7:00 PER HAECO LCQ NON-ROUTINE 9292169 GENERATED BY V061633 REPAIRED R2 DOOR STOP FITTING #1 IAW SRM 53-41-12-300-011 FIG 008 SHEET 1 AND SHEET 2 AND SRM 53-41-12-300-008. THIS REPAIR FOUND TO BE A CAT B REPAIR WITH SRI RE-INSPECTION IAW SRI 53-41-12-205-010. INSPECTION THRESHOLD FROM ADL/REPAIR EMBODIMENT 13100 FLIGHT CYCLES. FLIGHT HOURS NOT RELEVANT. SUBSEQUENT INSPECTIONS INTERVALS 5800 FLIGHT CYCLES. FLIGHT -08. REPAIR ACCCOMPLISHED ON HAECO LCQ NONROUTINE 9292169. HOURS NOT RELEVANT. INSPECTION METHOD HFEC REF NTM CHAPTER 51-10 A FREEZE PLUG INSTALL PER SRM 51-23-12-801 PARA 6 4.A 7 WITH A FINAL REAM TO FIRST OVERSIZE TO .282 IAW AMM 53-41-12-300-011 FIG 001. REAM HOLES D2, D3, D4 TO FIRST OVERSIZE TO .282 IAW SRM 53-41-12-300-011. NO CRACK INDICATION NOTED AT D1, D2, D3, OR D4 FINAL REAM FOR CRACK INDICATION REMOVAL FOR D1 .672 REQUIRING CYCLES FROM REPAIR EMBODIMENT. FLT HRS NOT RELEVANT. SUBSEQUENT INSPECTIONS TO BE ACCOMPLISHED EVERY 5800 FLT CYCLES. FLT HRS NOT RELEVANT OK TO CARRY REPAIR INSPECTION TO BE ACCOMPLISHED BY 13100 FLT TOMC-APPROVAL FROM SC1ELBYC COMMENT TOMC APPROVED : QC REVIEWED. TOMC APPROVED : QC REVIEWED. RECORDS UPDATE INIT: W/I 13100 FC **INIT TO AUTO-ITO TO RIR (-3612) RIR: EVERY 5800 FC...AN/U345625

Part: PROFILE — CRACKED (L EMERGENCY EXIT) · airframe 83,893 hrs · 32,603 cycles

OFF-AIRCRAFT PART: LT AFT EMERGENCY EXIT HATCH FWD LOAD TRANSMITTING PROFILE CRACKED, PER HAECO LCQ NON ROUTINE 9292230. REMOVED CRACKED SEGMENT INSTALLED NEW SEGMENT, IAW A320 SRM 51-42 -11-801.

Part: PROFILE — CRACKED (L EMERGENCY EXIT) · airframe 83,893 hrs · 32,603 cycles

LT AFT EMERGENCY EXIT HATCH AFT LOAD TRANSMITTING PROFILE CRACKED OFF. AIRCRAFT PART: (A3NB-52-4-6031) PER HAECO LCQ NON ROUTINE 9292231. REMOVED CRACKED SEGMENT INSTALLED NEW SEGMENT, IAW A320 SRM 51-42 -11-801.

Part: INTERLOCK — MISSING (CARGO DOOR) · airframe 80,976 hrs · 31,301 cycles

FWD/CARGO DOOR OPEN MSGIN FLT FOUND FWD CARGO DOOR INTERLOCK MECHANISM PIVOT LINK MISSING UPPER PIN AND CIRCLIP, FOUND PIN IN LOWER DOOR, REINSTALLED PIN AND CIRCLIP. OPS CHECKED DOOR SEVERAL TIMES, HANDLE STOWS FIRMLY NO ECAM MESSAGES.

Part: VALVE — LEAKING (PARKING BRAKE) · airframe 80,208 hrs · 30,958 cycles

NEED TO COMPLY WITH AMM 29-00-00-280-006-A01 CHECK OF Y HYD SYS AFTER PUMP FAILURE OR OPERATION IN A POSSIBLE CAVITATION COND. FOUND PARKING BRAKE VALVE LEAKING REPLACED PER AMM 32-45-14-400 REPLACED NR 2 ENG DRIVEN PUMP DUE TO CAVITATION PER AMM 29-13-51-4 00 REPLACED YELLOW LOW PRESSURE FILTER PER AMM 29+-13-44-400 REP LACED YELLOW HP FILTER PER AMM 29-13-45-610-001-A PERFORMED ENG RUN NR 2 LEAK CKS NONE FOUND ROTABLE PARTS CHANGE WAS INDICATED - TT # 1452258 SN OFF 0494 TT # 1259843 SN OFF 1466 IPC REFERENCE # 29-13-51-01B VALVE, PARKING OFF 31-3245-9-9003 0494 ON 31-3245-9-9003 7400.

Part: SLIDE — UNSECURE (L2 DOOR) · airframe 77,926 hrs · 29,948 cycles

REPORTED BY PILOT AND CATERING THAT L2 DOOR SLIDE IS COMING APART AT THE BOTTOM OF THE SLIDE. REMOVED AND REPLACED L2 DOOR SLIDE AND TESTED IAW AMM 25-62-44-0 0-002Q, AND 25-62-44-400-006A. DOOR SLIDE SECURE AND TESTS PASSED.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 77,026 hrs · 29,560 cycles

AFT RIGHT EMER FLASHLIGHT BRACKET IS BROKEN INSTALLED SERVICEABLE EMERG. FLASHLIGHT BRACKET & OPS CHECKS GOOD. ORIGINAL FLASHLIGHT WAS SERVICEABLE & RE-INSTALLED.

Part: SKIN — DAMAGED (RUDDER) · airframe 76,844 hrs · 29,464 cycles

PUNCTURE DISCOVERED ON THE UPPER RIGHT SIDE OF THE RUDDER. THE PUNCTURE WAS LOCATED 14.5 INCHES FROM TRAILING EDGE AND 9.7 INCHES FROM CAP SEAM. THE DAMAGE IS 1.1 INCHES IN WIDTH AND .8 INCH IN LENGTH.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,766 hrs · 28,080 cycles

CORROSION AROUND FASTENER HOLE STRINGER 41 RIGHT 6 INCH AFT OF FRAME 58 IN AFT CARGO. REMOVED AND REPLACED AFT CARGO STRINGER 41R FR 64 TO FR 59 IAW SRM 51-42-11.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,766 hrs · 28,080 cycles

RT FUSE AT FR35 STR 30 HOLE MARKED 3 IS OUT OF ROUND. INTERIM RPR ACP IAW ECRA5330-05797 PART1 ACP PERM RPR OF THE FASTENER HOLES AT FR35 STR 30L 30R ON OR BEFORE MARCH 26 2017.

Part: SKIN — DENTED (CARGO DOOR) · airframe 73,766 hrs · 28,080 cycles

AFT CARGO DOOR SKIN DENT FR54A+5. INSTALLED DOUBLER IAW SRM 52-32-00 FIG 205.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,766 hrs · 28,080 cycles

LT FUSE AT FR35 STR 30 HOLE MARKED AS 1 IS CRACKED IN SKIN AND SIDESHELL. INTERIM RP ACP IAW ECRA 5330- 05797 PART1 ACP PERM RPR OF THE FASTENER HOLES AT FR35 STR 30L, 30R ON OR BEFORE MARCH 26 2017.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,766 hrs · 28,080 cycles

LT FUSE AT FR 35 STR 30 HOLE MARKED AS 2 IS CRACKED IN SIDESHELL AND FRAME FLANGE. INTERIM RPR ACP IAW ECRA 5330-05797 PART1ACP PERM RPR OF THE FASTENER HOLES AT FR 35 STR 30L, 30R ON OR BEFORE MARCH 26 2017.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,766 hrs · 28,080 cycles

LT FUSE AT FR35 STR30 HOLE MARKED AS 4 IS OUT OF ROUND. INTERIM RPR ACP IAW ECRA5330-05797 PART1 ACP PERM RPR OF THE FASTENER HOLES AT FR35 STR 30L, 30R ON OR BEFORE MARCH 26 2017.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,766 hrs · 28,080 cycles

LT FUSE AT FR35 STR30 HOLE MARKED 3 IS OUT OF ROUND. INTERIM RPR ACP IAW ECRA5330-05797 PART1 ACP PERM RPR OF THE FASTENER HOLES AT FR35 STR 30L, 30R ON OR BEFORE MARCH 26 2017.

Part: SKIN — DENTED (CARGO DOOR) · airframe 73,766 hrs · 28,080 cycles

AFT CARGO DOOR SKIN DENT FR55. INSTALLED DOUBLER IAW SRM 52-32-00 FIG 205.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,766 hrs · 28,080 cycles

FUSELAGE EXT SKIN AT WASTE VENT HAS MINOR CORROSION FR 69-FR 70, STR 28R. DAMAGED FOUND TO BE OUT OF LIMITS IAW SRM 53-41-11 TABLE 108. INSTALLED REPAIR DOUBLER AT FR69-FR70 STR 28R EXT SKIN AT WASTE VENT, IAW SRM 53-41-11 PARA 5 D.

Part: ANGLE — CORRODED (EMERGENCY EXIT) · corrosion level 2 · airframe 73,766 hrs · 28,080 cycles

CORROSION ON LEFT AFT EMERGENCY EXIT LOWER FRAME NEXT TO DRAIN HOLE. REMOVED AND REPLACED T-ANGLE FWD AND LEFT LOWER CORNER CURVED WEBS IAW SRM 51-42-11.

Part: SKIN — DENTED (FUSELAGE) · airframe 73,766 hrs · 28,080 cycles

FUSELAGE EXTERNAL DENT FR3, 11" ABOVE LOWER LAP SEAM. ACCOMPLISHED REPAIR IAW SRM 53-00-11, PAR 4 W FIG 240.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,766 hrs · 28,080 cycles

FWD CARGO FR 31 STR 43L-43R CLEAT HAS CORROSION. REMOVED AND REPLACED FWD CARGO FR31 STR 43L-43R CLEAT SRM 51-42-11.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,766 hrs · 28,080 cycles

FWD CARGO PIT FR33 STR43R-43L CLEAT IS CORRODED. R&R CLEAT IAW SRM 51-42-11.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,766 hrs · 28,080 cycles

FWD CARGO PIT FR33 STR40R-41R CORROSION ON CLEAT. R&R CLEAT IAW SRM 51-42-11.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,766 hrs · 28,080 cycles

FWD CARGO FR33 STR 42-43R CLEAT HAS CORRSION. REMOVED AND REPLACED FWD CARGO FR33 STR 42-43R CLEAT IAW SRM51-42-11.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,766 hrs · 28,080 cycles

FWD CARGO PIT FR32 STR 40R-41R CLEAT HAS CORROSION. R&R CLEAT IAW SRM 51-42-11.

Part: SHEAR TIE — CORRODED (FRAME 28) · corrosion level 2 · airframe 73,766 hrs · 28,080 cycles

FWD CARGO BAY FRAME 28 STRINGERS 41-40L SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.

Part: SHEAR TIE — CORRODED (FRAME 28) · corrosion level 2 · airframe 73,766 hrs · 28,080 cycles

FWD CARGO FR28, STR 43R - 44R CLEAT HAS CORROSION. REMOVED & REPLACED IAW A320 SRM 51-42-11.

Part: SHEAR TIE — CORRODED (FRAME 30) · corrosion level 2 · airframe 73,766 hrs · 28,080 cycles

FWD CARGO FR30 CLEATS HAVE CORROSION AT STR'S 42L - 43L AND 44 - 43R. REPLACED 2 EA CLEATS IAW A320 SRM 51-42-1 1.

Part: SHEAR TIE — CORRODED (FRAME 30) · corrosion level 2 · airframe 73,766 hrs · 28,080 cycles

FWD CARGO BAY, FRAME 30 STRINGERS 40, 41, 42, 43R CLEATS HAVE CORROSION. REPLACED THE CLEATS IAW SRM 51-42-1 1.

Part: SHEAR TIE — CORRODED (FRAME 33) · corrosion level 2 · airframe 73,766 hrs · 28,080 cycles

FWD CARGO BAY FRAME 33 STRINGERS 42-43L SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.

Part: SHEAR TIE — CORRODED (FRAME 34) · corrosion level 2 · airframe 73,766 hrs · 28,080 cycles

FWD CARGO BAY FRAME 34 STRINGERS 42-43L SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.

Part: SHEAR TIE — CORRODED (FRAME 27) · corrosion level 2 · airframe 73,766 hrs · 28,080 cycles

FWD CARGO FRAME 27 STRINGERS 43L - 42L AND 43L - 43R CLEATS HAVE CORROSION. REPLACED THE CLEATS IAW SRM 51-42-1 1.

Part: SHEAR TIE — CORRODED (FRAME 28) · corrosion level 2 · airframe 73,766 hrs · 28,080 cycles

FWD CARGO BAY FRAME 28 STRINGERS 42-43R SHEAR TIE HAS CORROSION, REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.

Part: SHEAR TIE — CORRODED (FRAME 33) · corrosion level 2 · airframe 73,766 hrs · 28,080 cycles

FWD CARGO BAY FRAME 33 STRINGERS 40-41L HAS CORROSION. REMOVED AND REPLACED THE SHEART TIE IAW SRM 53-42-11.

Part: SHEAR TIE — CORRODED (FRAME 28) · corrosion level 2 · airframe 73,766 hrs · 28,080 cycles

FWD CARGO BAY FRAME 28 STRINGERS 42-43L SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.

Part: SHEAR TIE — CORRODED (FRAME 27) · corrosion level 2 · airframe 73,766 hrs · 28,080 cycles

FWD CARGO BAY FRAME 27 STRINGERS 42-41 SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.

Part: SHEAR TIE — CORRODED (FRAME 28) · corrosion level 2 · airframe 73,766 hrs · 28,080 cycles

FWD CARGO BAY FRAME 28 STRINGERS 41-42R SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.

Part: SHEAR TIE — CORRODED (FRAME 28) · corrosion level 2 · airframe 73,766 hrs · 28,080 cycles

FWD CARGO BAY FRAME 28 STRINGERS 41-42L SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.

Part: SKIN — CONTAMINATED (LT ELEVATOR) · airframe 73,766 hrs · 28,080 cycles

LEFT ELEVATOR UPPER SKIN PANEL HAS A TRAPPED WATER INDICATION, 47.5" FROM INBOARD, 5" FROM TE, 3 X 2.5 DIA . REPAIRED IAW SRM 55-21-11 PAR. 5.E.

Part: SKIN — CONTAMINATED (RT ELEVATOR) · airframe 73,766 hrs · 28,080 cycles

RIGHT ELEVATOR UPPER SKIN PANEL HAS TRAPPED WATER INDICATIONS 186" FROM INBOARD, 9" FROM TE, 4 X 5.5 DIA A ND 150" FROM INBOARD, 14" FROM TE, 4.5 X 6.0 DIA. REPAIRED IAW SRM 55-21-11 PAR. 5.N.

Part: SKIN — DENTED (FRAME 7) · airframe 73,766 hrs · 28,080 cycles

EXTERIOR FUSELAGE SKIN HAS DENT FRAME 7 8.5 INCH ABOVE LOWER LAP SEAM. FOUND TO BE OUT OF LIMITS. CUT OUT THE DAMAGED AREA & FABRICATED A REPAIR DOUBLER AND INSTALLED IAW SRM53-00-11 FIG 239.

Part: ENGINE — STALLED (LEFT) · airframe 73,762 hrs · 28,079 cycles

AT FL 360, ECAM INDICATION LEFT ENGINE STALLED. DIVERTED, ENGINE DISPLAYED STALL INDICATIONS TWICE AT ALTITUDE BUT PERFORMED NORMAL REST OF FLIGHT. TROUBLESHOOT IAWTSM. REPLACED EEC AS A PRECAUTION. LEAK CHECK AND PURGE OF PB SENSE LINE, INSPECTED FOR DEFECTS. HIGH POWER ENGINE RUN OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 72,832 hrs · 27,644 cycles

AFTER REPLACEMENT OF 1R SLIDE, FOUND SEVERAL LIGHTS OUT FROM CTR BATTERY PACK WITH A-C POWER OFF. REPLACED CTR BATTERY PACK WITH SERVICEABLE UNIT. TESTED SUCCESSFUL.

Part: SLIDE — ACTIVATED (L2 DOOR) · airframe 70,685 hrs · 26,705 cycles

DOOR 2L SLIDE INFLATED DURING CLEANING. REMOVED INFLATED SLIDE FROM DOOR 2L IAW AMM 25-62-44-000-011-A.

Part: SKIN — DAMAGED (RT WING) · airframe 69,111 hrs · 26,032 cycles

RIGHT WING TANK ACCESS PLATE 640PB HAS DAMAGED FASTENER HOLE ON LANDING. HOLE WAS REPAIRED IAW HAECO REO-L187 08 & CONSIDERED CAT B REPAIR IAW -B RDAS 80022401-003-2015. HOLE WAS OVERSIZED & BUSHING WAS INSTALLED. IAW CRA THRESHOLD SUPPLEMENTAL INSPECTIONS TO BEGIN AT 42900C OR 85800T WHICHEVER OCCURS FIRST & EVERY 3300C OR 6600T THEREAFTER.

Part: SKIN — DAMAGED (RT WING) · airframe 69,111 hrs · 26,032 cycles

RIGHT FUEL TANK ACCESS LANDING, TWO EACH HOLES HAS ELONGATION 640HB. R & R BUSHING HOLE 565 & INSTALLED BUS HINGE HOLE 562 IAW A320. SRM 57-21-11 PG 210-216 PAR B.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,111 hrs · 26,032 cycles

R2 DOOR SILL BEAM HAS CORROSION ON PREVIOUS REPAIR & FRAME 68, JUST FWD OF THE AFT GIRT BAR FITTING PLATE. R & R DOOR SILL IAW SRM 51-42-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,111 hrs · 26,032 cycles

R2 DOOR AFT SHAPE SILL CORNER FITTING FOUND CORROSION DURING REMOVAL. R & R CORNER FITTING IAW SRM 51-44-11 & 51-75-12.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,111 hrs · 26,032 cycles

R2 DOOR SHAPE SILL HAS CORROSION AROUND FASTENERS. REPLACED DOOR SHAPE SILL IAW SRM 51-73-11.

Part: SEAL — UNSECURE (ENGINE) · airframe 65,750 hrs · 24,725 cycles

LT SIDE OF BOTH ENGS CNA OUTER DUCT SEALS HANGING OUT. SECURED SEAL IAW AMM.

Part: SEAL — UNSECURE (COWLING) · airframe 65,750 hrs · 24,725 cycles

BOTH ENGS HAVE COWL SEALS HANGING. INBD SIDE OF BOTH ENG CNA OUTER DUCT SEALS HANGING OUT.

Part: SDAC — FAULTY (NR 1) · airframe 65,497 hrs · 24,627 cycles

OXY PAX BOTTLES CLOSED ECAM, OXY SYS FAULT DISPLAYED. REPLACED NR 1 SDAC, FAULTS CLEARED & SDAC GND SCAN IS GOOD.

Part: SELECTOR VALVE — FAULTY (LANDING GEAR) · airframe 65,459 hrs · 24,615 cycles

LG WOULD NOT EXTEND NORMALLY, HAD TO EXTEND MANUALLY. REPLACED SELECTOR VLV IAW AMM 32-31-12-400-001-A & SAFETY VLV IAW 32-31-17. ACCOMPLISHED FUNCTIONAL CHECK OF NORMAL EXTENSION & RETRACTION OF LG SYS IAW AMM32-31-00-720-002.

Part: SELECTOR VALVE — FAULTY (LANDING GEAR) · airframe 65,459 hrs · 24,615 cycles

LG WOULD NOT EXTEND, REPLACED LG SELECTOR VLV IAW AMM. ACCOMPLISHED FUNCTIONAL TEST OF NORMAL EXTENSION & RETRACTION OF LANDING IAW AMM. ACCOMPLISHED REPLACEMENT OF SELECTOR VLV & NORMAL EXTENSION & RETRACTION OF LG IAW ABOVE REFERENCES.

Part: DRAIN VALVE — LEAKING (YELLOW SYSTEM) · airframe 65,227 hrs · 24,523 cycles

FOUND YELLOW RESERVOIR DRAIN VLV LEAKING. REPLACED YELLOW HYD RESERVOIR DRAIN VLV, REPLENISHED YELLOW SYSTEM. PRESSURIZED & LEAK CHECKED & NO LEAKS NOTED.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR) · airframe 64,831 hrs · 24,381 cycles

DOOR 1L WON’T CLOSE, LEVER WILL NOT GO DOWN. ADJUSTED GIRT BAR & GIRT AREA. RE-POSITIONED RELEASE STRAP & SURVIVAL KIT LANYARD TO FWD POSITION. DOOR OPENS & ARMS NORMAL. SLIDE REMOVED & REINSTALLED TO ADJUST GIRT & LANYARDS IAW AMM.

Part: STRAKE — MISSING (NR 2 NACELLE) · airframe 64,499 hrs · 24,254 cycles

CREW FOUND THE INBD NACELLE STRAKE FOR THE NR 2 ENG MISSING. REPLACED NR 2 ENG FAN COWL INBD STRAKE.

Part: WIRE HARNESS — FAILED (LT MLG) · airframe 64,389 hrs · 24,211 cycles

TROUBLESHOT LEFT MLG INDICATION PROBLEM. FOUND RESISTANCE ERRATIC ON THE HARNESS AT UPPER SECTION OF LT MLG WHILE SHAKING HARNESS. REPLACED HARNESS IAW MM. OPS CHECKED IAW AMM`S 32-69-00-74 -001, 32-42-00-710-001 AND 32-47-00-710-001.

Part: SEAL — MISSING (SLIDE) · airframe 64,387 hrs · 24,210 cycles

SLIDE RAFT ABOVE SEAT 1B MISSING SEAL. INSTALLED NEW SEAL.

Part: LANDING — DAMAGED (PANEL OPENING) · airframe 64,374 hrs · 24,204 cycles

RT WING LOWER FUEL TANK ACCESS PANEL LANDINGS FOUND DAMAGED. REPAIRED.

Part: COVER — WRONG PART (R1 DOOR SLIDE) · airframe 64,374 hrs · 24,204 cycles

R1 DOOR SLIDE COVER INCORRECT FOR CONFIGURATION. R & R R1 DOOR SLIDE ASSY IAW NMM 25-62-44-000-012A, 25-62-44-400-007A.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 64,374 hrs · 24,204 cycles

STRINGER 31R, FRAME 65, EXFOLIATED WITH 100 PERCENT MATERIAL LOSS. REPLACED STRINGER 31R FROM FR 64 - 69 IAW SRM 51-42-11,PARA 5, 6, 7. MAJOR REPAIR.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,294 hrs · 24,175 cycles

BATTERY FAULT FWD LEFT ON EMERGENCY LIGHT TEST. REPLACED BATTERY PACK, TEST PASSED. EMERGENCY LIGHTS TESTED OK.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 64,294 hrs · 24,175 cycles

BATTERY FAULT AFT LEFT DURING EMERGENCY LIGHT TEST. REPLACED BATTERY PACK TEST PASSED.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHT) · airframe 64,294 hrs · 24,175 cycles

BATTERY FAULT LIGHT ON EMERGENCY LIGHT TEST. REPLACED BATTERY PACK TEST PASSED.

Part: SKIN — DENTED (FUSELAGE) · airframe 64,251 hrs · 24,161 cycles

DENT IN FUSELAGE BELOW DOOR 2L, 1.250 LENGTH, .750 WIDTH, .031 DEPTH. DAMAGE IS LOCATED BETWEEN FR 69-70 AND STR 32-33. ACCOMPLISHED VISUAL INSPECTION, NO CRACKS. FOUND DAMAGE IS WITHIN ALLOWABLE LIMITS IAW SRM 53-41-11, DIAGRAM 103, PG 163.

Part: ROLLER — OUT OF ADJUST (R1 DOOR) · airframe 63,509 hrs · 23,875 cycles

R1 DOOR DIFFICULT TO OPEN. FOUND LOWER ROLLERS HANGING UP ON PULL IN RAMPS. RAISED DOOR. OPS CHECKED GOOD. SAFTIED ADJUSTMENT ROD, REINSTALLED DOOR LINER. SLIDE WAS NOT REMOVED.

Part: PANEL — UNSECURE (CABIN) · airframe 63,075 hrs · 23,699 cycles

CENTER CEILING PANEL ROW 28-29 RT SIDE HANGING DOWN APPROX 2 INCHES. REPOSITION CEILING PANEL. CHECK OKAY.

Part: TIRE — VIBRATION (NLG) · airframe 63,002 hrs · 23,675 cycles

NOSE TIRES VIBRATE EXCESSIVELY ON GEAR RETRACTION ON TAKEOFF. REPLACED BOTH NLG TIRES PER AMM.

Part: SEAL — DIRTY (COCKPIT WINDOW) · airframe 62,984 hrs · 23,669 cycles

HIGH PITCH SQUEAL BEHIND FIRST OFFICERS SEAT. CHECKED FIRST OFFICERS SLIDING WINDOW AND DOOR 1R. CLEANED SEALS. NO DEBRIS FOUND. OK PER AMM MT52-020.

Part: SENSOR — FAILED (NLG STEERING) · airframe 62,920 hrs · 23,641 cycles

NOSE WHEEL STEERING FAILED DURING TAXI IN. NLG STEERING FAILED AS A RESULT OF FAILED NLG DOWNLOCK PROX SENSOR FAILURE. THE REPLACEMENT OF THIS SENSOR IS DOCUMENTED IN AMSITM 9202012. NOSE WHEEL STEERING TESTED OK WITH A TAXI TEST.

Part: SEAT — INOPERATIVE (COCKPIT) · airframe 62,629 hrs · 23,537 cycles

FIRST OBSERVER'S SEAT INOPERATIVE. INTERIOR CREW COMMENTS: SEAT WILL NOT SLIDE OVER. REPLACED SEAT ASSY.

Part: PACKING — LEAKING (HYDRAULIC SYS) · airframe 62,469 hrs · 23,469 cycles

YELLOW HYD SYSTEM LEAKING. FOUND PTU MANIFOLD CHECK VALVE (3094GM) LEAKING. REPLACED PACKING. SERVICED, BLED, AND LEAK CHECKED. NO LEAKS NOTED. OPS CHECKS NORMAL.

Part: STRING — MISSING (COCKPIT) · airframe 62,328 hrs · 23,423 cycles

CAPTAINS SIDE STICK SECURING STRING NOT INSTALLED. INSTALLED NEW STRING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,287 hrs · 23,409 cycles

EMERGENCY LIGHT INOP AT SEATS 11ABC. RELAMPED, OPS CHECK GOOD.

Part: LOUVER — BROKEN (LT ENGINE) · airframe 62,066 hrs · 23,317 cycles

LEFT ENGINE TAI EXHAUST LOUVER IS BROKEN AND LOOSE. REMOVED DAMAGED LOUVER. OK TO CONTINUE IN SERVICE UNTIL GRILL REPLACEMENT.

Part: ENGINE — FOD (RIGHT) · airframe 61,363 hrs · 23,050 cycles

PAX REPORTED LARGE PIECE OF PLASTIC INGESTED INTO RIGHT ENGINE. ACCOMPLISHED INSPECTION OF THE NR 2 ENGINE FOUND A PIECE OF 'PLASTIC-BAG' IN THE SECONDARY GAS PATH ON THE FAN EXIT GUIDE VANES. DID REVIEW WITH FLIGHT CREW AND THEY SAW NO UNUSUAL PARAMETERS. BAG HAS BEEN CLEARED. VISUAL INSPECTION OF THE REST OF THE ENGINE ACCOMPLISHED, NO DEFECTS FOUND.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 60,511 hrs · 22,731 cycles

RIGHT AIR COND BAY, HEAT EXCH AFT UPPER SUPPORT BRACKET, ATTACHED TO CTR WING LWR SKIN IS CRACKED AT FWD INBD CORNER OF THE BRACKET. VERIFIED WITH HFEC. INSTALLED NEW FITTING. STATIC LEAK CHECKED OK.

Part: LANYARD — BROKEN (EVAC SLIDE) · airframe 60,437 hrs · 22,704 cycles

2L DOOR SLIDE REMOVED. SURVIVAL KIT LANYARD BROKEN ON REMOVED SLIDE. SURVIVAL KIT LANYARD BROKEN. REPLACED SLIDE REF AMM. TESTS OK. INSPECTED INSTALLATION, VERIFIED ALL PINS REMOVED AND EMERGENCY LIGHT TEST OK. DOOR 2L ESCAPE SLIDE-RAFT SURVIVAL KIT LANYARD TORN -LOOP IS MISSING. PCN 649-9003 NIS DEN. REPLACED REF AMIS ITEM 4372029 AND 4372030. INSPECTED INSTALLATION, VERIFIED ALL PINS REMOVED AND EMERGENCY LIGHT TEST OKAY.

Part: DOOR — DAMAGED (COCKPIT) · airframe 60,263 hrs · 22,639 cycles

UNABLE TO CLOSE DOOR TO F/O`S O2 MASK, IT IS STUCK BEHIND SLIDING WINDOW. REPAIRED BY REPOSITIONING O2 MASK DOOR.

Part: CONTROL UNIT — FAULTY (FUEL SYSTEM) · airframe 59,959 hrs · 22,535 cycles

LEFT FUEL IS 1100 LBS LESS THAN RIGHT TANK DURING CRUISE AND DESCENT. FUEL ERROR READING LEFTW-49 RIGHT W-2400. BURN EQUAL AND LOAD EQULAT TAXI. TROUBLESHOOT REF TSM. SWAPPED FLSCU 1&2 SYS TEST NO FAULTS. TESTED FUEL TRANS VLVS PER TSM. NO LEAKS NOTED NEED FURTHER TS. APPROX 800 LBS USED FROM RT TANK ON NEXT FLIGHT ( 3 HOURS). TANK ENTRY NEEDED. SEE-FEEL INDICATOR ON XFEED VLV. ALSO MAKE SURE OUTER CELLS ARE FULL & INTERCELL XFR VLVS NORMAL BEFORE ACP TSM. REPLACED LEFT WING REFUEL VALVE PER MM. COULD NOT DUPLICATE UNWANTED FUEL TRANSFER. OPS CHECK GOOD.

Part: VALVE — FAULTY (LT WING) · airframe 59,958 hrs · 22,534 cycles

UNWANTED FUEL USE FROM RT WING. *SUPPLEMENTAL DATA UPDATE* OPBLM PROG TEXT: - ITEM ROLLED FORWARD. SAMC TEXT: APPROX 900 LBS IMBALANCE DURING A 3 HOUR FLT IAD- SJU. WORK WITH LM2750. OPBLM. REPLACED LEFT WING REFUEL VALVE SEE SEQ 9582001.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 59,532 hrs · 22,375 cycles

EMERGENCY EXIT LIGHT AT LOWER AFT OF 2 LEFT, LENSE WILL NOT STAY ON. REPLACED LIGHT ASSY.

Part: CONTROL PANEL — FAULTY (F/A STATION) · airframe 59,451 hrs · 22,346 cycles

CREW REPORTS SMOKE ODOR IN CABIN AND PES CIRCUIT BREAKER 5 TRIPPED AT 2000 VU PANEL. CAPT NOTED THAT THE EMERGENCY CALL BUTTON WAS ILLUMINATED WITH NO ONE CALLING AND THAT THE EMERGENCY CALL CHIME WAS GOING OFF. CIRCUIT BREAKER 21MK COLLARED. REMOVED AND REPLACED FWD ATTENDANT PANEL IAW AMM, OPS CHECKED OK.

Part: CONTROLLER — FAULTY (WASTE DISPOSAL) · airframe 59,410 hrs · 22,327 cycles

ALL TOILETS INOP, FLIGHT DIVERTED. SAMC TEXT: CFDS SHOWS '38-31-62 LIQUID LEVEL XMTR'. OPBLM -- AND CREW REPORTS FWD ATTEND PNL LAV WASTE QTY SHOWS 'ZERO'. REPLACED VACUUM SYSTEM CONTROLLER PER AMM. ALL 3 LAVS FLUSH NORMALLY.

Part: FLOAT VALVE — WORN (LT WING) · airframe 59,151 hrs · 22,220 cycles

FUEL SEEMS TO TRANSFER INFLT FROM RIGHT WING TO LEFT W- CROSSFEED CLOSED. BURN +TOTAL CORRECT. T/S FOR WING TO WING TXFER COULD NOT DUPLICATE BUT DID FIND LT WING OUTER TANK VENT FLOAT WORN OUT CAUSING TXFER FROM OUTER TO INNER TXFER AT APPROX 200LB PER HOUR REPLACED LT WING VENT FLOAT VLV 15QM REF AMM. NO LEAKS, OP CHECK OKAY.

Part: INDICATOR — INOPERATIVE (ADIRU) · airframe 58,352 hrs · 21,905 cycles

GROUND POWER DROPPED OFF THE AIRCRAFT. AFTER POWER WAS RESTORED THE COCKPIT SCREENS WOULD NOT COME ON AND THE GRND WARNING HORN GOES OFF WHEN ALIGNING ADIRU'S NR 1 AND NR 3. UPPER ECAM 'BCL2' FAULT DISPLAYED, BUT BCL2 TESTS OKAY. REPLACED BCL2, NO HELP WITH ORG PROBLEM. ECAM FAULT CLEARED. REPLACED SHIP BAT2 PER AMM, NO HELP. ADIRU1-3 CAUSE CREW HORN AND 'ON BAT' LIGHT ON ADIRU'S CDU. FOUND ADIRU NR 1 AND ADIRU NR 3 WITH FAULTS. REPLACED BOTH ADIRU(S) - AIRCRAFT SYSTEMS NOW OPS CHECK GOOD. NO ECAM FAILURE MESSAGES NOTED.

Part: SEAL — MISSING (WASTE CONTAINER) · airframe 58,255 hrs · 21,864 cycles

FWD AFT LAV WASTE CONTAINER COMPARTMENT DOOR SEAL MISSING. 2 FEET SECTION OF SEAL IS MISSING PART NUMBER 023-6600 TRASH DOORS TAPED CLOSED. LAV IS LOCKED CLOSE NOT TO BE USED. REPLACED MISSING SEAL SECTION.

Part: VALVE — FAULTY (OXYGEN SYSTEM) · airframe 57,483 hrs · 21,562 cycles

O2 SYSTEMS FAULTY, FLIGHT DIVERTED. FOUND TANK DUMP OVERFLOW VALVE PARTIALLY OPEN. CYCLED FILL AND DUMP VALVES. ALL OP'S NORMAL. RESERVICED AND PRESSURIZIED SYSTEM. NO LEAKS NOTED.

Part: BOTTLE — READS LOW (ESCAPE SLIDE) · airframe 57,485 hrs · 21,563 cycles

CIDS CAUTION AT DEPARTURE. LT EMERGENCY SLIDE BOTTLE PRESSURE LOW. CANNOT APPLY MEL AS BOTTLE PRESSURE NEEDLE IN RED. BOTTLE REPLACED.

Part: STRAP — OUT OF POSITION (L1 DOOR SLIDE) · airframe 57,236 hrs · 21,471 cycles

FOUND STRAP FROM SLIDE PACK DOOR 1L HANGING OUTSIDE DOOR WHEN AIRCRAFT ARRIVED AT GATE. STRAP CAME OFF SLIDE PACK, GLUE DID NOT HOLD STRAP TO SLIDE PACK. BONDED STRAP AND BUCKLE ASSY ONTO ESCAPE SLIDE COVER AT MED 1L. NO SLIDE REPLACEMENT REQUIRED.

Part: COMPRESSOR — VIBRATES (NR 2 ENGINE) · airframe 56,553 hrs · 21,204 cycles

ENG 2 COMPRESSOR VANE ON UPPER ECAM. ENGINE WAS SHUTDOWN AND RESTARTED. FAULT CLEARED BUT RETURNED WHEN THROTTLE ADVANCED TO BREAKAWAY THRUST. LAST LEG FAULT CHANNEL A & B VSV ACT-HC-EEC2 WITH FLT DATA FAULT SVA TK IN FLT PH 02. CHECKED IAW TSM. ACCOMPLISHED VISUAL CHECK. NO DEFECTS FOUND. LUBED VSV SYS IAW MM. ACCOMPLISHED POWER ASSURANCE CHECK IAW JRH. SYS CHECKED OK.

Part: ACTUATOR — FAULTY (RUDDER PEDAL) · airframe 56,389 hrs · 21,132 cycles

F/O RUDDER PEDAL ADJUST DOES NOT SPRING INTO SELECTED POSITION. DROPS TO FLOOR WHEN PULL. REPLACED PEDAL POSITION ADJ ASSY REF MM. OPS CHECK NORMAL.

Part: WIRE — SMOKE (GALLEY) · airframe 54,962 hrs · 20,524 cycles

GALLEY PIGTAIL- ELECTRICAL CORD SMOKING OR SPARKING AT 106. (LOCATION NOT DEFINED - CK CABIN FORM FOR SPECIFIC LOCATIONS), AFT CBN LT AFT LAV. THIS ACFT HAS NO GALLEY ELECTRICAL CORDS INSTALLED, INSPECTED AFT LAV, NO LOOSE ELECTRICAL CONNECTIONS VISIBLE.

Part: BOTTLE — FAULTY (ESCAPE SLIDE) · airframe 54,939 hrs · 20,515 cycles

LT OFF WING SLIDE INFLATION RESERVIOR, SLEEVE NUT LOCK WIRE HOLE BROKEN (OPEN). R & R LT OVERWING SLIDE BOTTLE. OPS & LEAK CKS GOOD IAW AMM.

Part: FRAME — CRACKED (LT OWING SLIDE) · airframe 54,939 hrs · 20,515 cycles

LT OVERWING SLIDE BOX AFT FRAME HAS A 5 INCH CRACK. REPLACED SLIDE ASSY.

Part: CABLE — FRAYED (L2 DOOR SLIDE) · airframe 54,939 hrs · 20,515 cycles

L-2 DOOR SLIDE-RAFT COVER RELEASE CABLE IS FRAYED. REPLACED PER JIC 4R2592037 ON N-R C7015K.

Part: SKIN — CORRODED (FUSELAGE) · airframe 54,939 hrs · 20,515 cycles

CORROSION AT FWD PIT FR 26-27 STRINGER 42R-41R ON SKIN. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER REPAIR.

Part: OXYGEN GEN — MISINSTALLED (CABIN) · airframe 54,939 hrs · 20,515 cycles

O2 GENERATORS AT SEAT LOCATIONS 17DEF, 21DEF AND 20ABC FOUND WITH SHIPPING PINS INSTALLED. ALSO FWD ATT O2 GENERATOR FOUND WITH HOSE DISCONNECTED. R & R O2 GENERATORS CORRECTLY. THE FWD ATT MASK REPLACED ON NR C5767R.

Part: SLIDING WINDOW — DELAMINATED (COCKPIT) · airframe 54,304 hrs · 20,257 cycles

FO-S SLIDING WINDOW HAS DELAMINATION AT BOTTOM EDGE. VISIBILITY IS NOT IMPAIRED. DELAMINATION MEASURED AT APPROX 5.25 X 3.25. EXCEEDS LIMIT IAW MM. ACCOMPLISHED F/O SLIDING WINDOW REPLACEMENT.

Part: DIAPHRAGM — DAMAGED (R1 DOOR) · airframe 53,838 hrs · 20,060 cycles

DOOR 1R ACCUMULATOR PRESSURE IS LOW. REPLACED DIAPHRAGM IN THE PERCUSSION MECHANISM. SERVICED BOTTLE TO PREVAILING LIMITS.

Part: PANEL — CRACKED (RT WING) · airframe 53,754 hrs · 20,033 cycles

RT WING NEAR ROOT SMALL PANEL BELOW SLAT IS DAMAGED, CRACKED. PANEL IS 621BB, OUT OF LIMITS FOR SRM. CRACK IS APPROX 6 INCHES, ACROSS ENTIRE PANEL. REPLACED DAMAGED PANEL AND INSPECTED AREA WITH NO DAMAGE FOUND.

Part: GIRT BAR — OUT OF ADJUST (DOOR 1R) · airframe 53,129 hrs · 19,798 cycles

UNABLE TO ARM DOOR 1R. WHEN DOOR 1R IS ARMED, SLIDE MESSAGE ON ECAM DOOR PAGE DISPLAYS, THEN GOES AWAY. ADJUSTED GIRT BAR AND GIRT CURTAIN, REINSTALLED SLIDE.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 53,129 hrs · 19,798 cycles

UNABLE TO ARM DOOR 1R. CREW REPORTS: WHEN DOOR 1R IS ARMED, SLIDE MESSAGE ON ECAM DOOR PAGE DISPLAYS, THEN GOES AWAY. ADJUSTED GIRT BAR AND GIRT CURTAIN, REINSTALLED SLIDE.

Part: FIRE DETECTOR — FAULTY (NR 1 NACELLE) · airframe 53,013 hrs · 19,752 cycles

NR 1 ENG HAS HAD 3 OCCURENCES OF FIRE WARNING POST CK ON FLIGHT. INDICATION COMES AND GOES. ALL PARAMETERS NORMAL INCLUDING FUEL FLOW. SAMC TEXT: CREW REPORTS MALFUNCTION IS IN LOOP 'A'. REF TSM 26-12-00-810-803, NR1 FDU TESTS OK. RESISTANCE VALUES OF DET'S CHK OK AT 1506 OHMS. RPLCD FDU 2WD1 REF MM 26-12-34.CHKS OK AND OP CHK LOOP & SQUIB OK. VISUAL CHK OF ENG NO DEFECTS NOTED. NO CURRENT FAULTS, NO AMIS HISTORY.

Part: SKIN — DENTED (FUSELAGE) · airframe 53,011 hrs · 19,751 cycles

FOUND DENT ON FUSELAGE LT SIDE JUST AFT OF RADOME APPROX 4 O'CLOCK POSITION. MAJOR REPAIR ACCOMPLISHED: DENT FALLS WITHIN 'OUT OF NEARNESS' CRITERION, DUE TO PROXIMITY TO A FASTENER. DENT IS .5 INCH IN DIAMETER, WITH A DEPTH OF.023. DENT IS LOCATED 5 INS AFT OF FR NR 1 AND APPROX 8 INS ABOVE BUTT SPLICE AT LWR LT SIDE. REMOVED DAMAGED SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 52,676 hrs · 19,598 cycles

LEFT FWD EPSU BATTERY FAILING PTP TEST. REPLACED EPSU AND BATTERY AT DOOR 1 LEFT.

Part: SLIDE — DAMAGED (OVERWING EXIT) · airframe 52,333 hrs · 19,434 cycles

LEFT OVERWING SLIDE PACK DAMAGED BEYOND LIMITS. REPLACED SLIDE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 51,195 hrs · 18,935 cycles

FOUND CORROSION IN THE BELLY SKIN BELOW THE FWD-PIT DOOR. DETERIORATION COMPLETELY THRU SKIN. SKIN REPAIR IS COMPLETE, CLOSING UP. SEALED & PAINTED.

Part: SKIN — DENTED (L2 DOOR) · airframe 50,191 hrs · 18,557 cycles

DOOR 2L HAS DENT 16.0" AFT OF FWD EDGE AND 13.5" FROM BOTTOM. EVALUATED DENT & FOUND OUT OF LIMITS. CUT OUT DAMAGE. FABRICATED & INSTALLED EXTERNAL DOUBLER REPAIR. RESTORED THE PROTECTIVE COATING.

Part: SILL — CORRODED (FUSELAGE) · airframe 50,191 hrs · 18,557 cycles

L2 DOOR SILL HAS CORROSION AT AFT GIRT FITTING. MAJOR REPAIR. INSTALLED ANGLE REPAIR.

Part: SUPPORT — CORRODED (R2 DOOR SILL) · airframe 50,191 hrs · 18,557 cycles

R2 DOOR SILL HAS CORROSION AT AFT GIRT SUPPORT BLOCK. MAJOR REPAIR. INSTALLED REPAIR ANGLE.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHT) · airframe 49,391 hrs · 18,220 cycles

EMERGENCY LIGHT SYS TEST FAULTS "UNIT EMER R". *S/D* REPLACED POWER SUPPLY, OP CHECKS OKAY.

Part: BATTERY — FAILED (CABIN) · airframe 47,801 hrs · 17,639 cycles

DURING EMERGENCY LIGHT TEST R BATTERY FAULTED. BATTERY FAILURE. REPLACED R EMER LIGHT BATTERY. OPS CHECKED NORMALLY.

Part: ACTUATOR — WEAK (PAX O2) · airframe 47,426 hrs · 17,500 cycles

OXYGEN MASK 6ABC FELL OUT. WEAK ACTUATOR. REPLACED DOOR ACTUATOR AND TESTED O2 SYSTEM, SYSTEM OPS CHECKS NORMAL AND DOOR REMAINS IN PLACE.

Part: BATTERY — FAILED (CABIN) · airframe 47,046 hrs · 17,365 cycles

EMERGENCY LIGHT TEST FAILS LEFT FORWARD DOOR BATTERY. BATTERY FAULTY. REPLACED DOOR LIGHT BATTERY AT DOOR 1L.

Part: FLUID — DISCHARGED (HYDRAULIC SYSTEM) · airframe 46,502 hrs · 17,146 cycles

WHILE TAXIING LOST NOSE WHEEL STEERING, FOLLOWED BY HYD GREEN RSVR LOW LVL STATUS MESSAGE. ALL GREEN SYSTEM FLUID DUMPED ONTO RAMP FROM AIRCRAFT WHEEL WELL AREA. FOUND DAMAGED GREEN SYS HYD LINE IN AFT PIT UNDER FLOOR, RING LOCK PULLED APART. REPAIRED GREEN SYS HYD LINE (RING LOCK REPAIR PLUS A NEW LINE) SERVICED GREEN HYD SYS- NO LEAKS NOTED, ALL SYSTEMS REPORTING NORMALLY.

Part: BATTERY — FAULTY (EMERGENCY LIGHTS) · airframe 46,423 hrs · 17,119 cycles

RIGHT SIDE MID CABIN EMERGENCY LIGHT BATTERY DISPLAYED FAULT. 10-26-07 FOUND FAULTY EMERGENCY LIGHT BATTERY. REPLACED EMERGENCY LIGHT BATTERY

Part: HYDRAULIC SYSTEM — LEAKING · airframe 46,295 hrs · 17,068 cycles

EVIDENCE OF HYD LEAK AFT FUSELAGE GREEN SYSTEM. LOST 1 US GAL IN 1.5 HRS.

Part: OXYGEN MASK — UNWANTED DEPLOY (6 DEF) · airframe 45,691 hrs · 16,827 cycles

OXYGEN MASKS DEPLOYED 7DEF ON LANDING. BROKEN O2 LATCH AT ROW 7DEF. REPLACED O2 CONTAINER ASSY.

Part: A/C PACK — OVERHEATED (NR 2) · airframe 45,036 hrs · 16,566 cycles

CREW REPORTED BAD ODOR IN THE CABIN. NR 2 PACK OVERHEATED SO IT WAS SHUT DOWN, THUS DESCENDING TO FL300. CONTINUED TO DESTINATION. REPLACED NR 2 RAM AIR OUTLET ACT. OPS CHECKS GOOD. AND ALSO PACK CONTROLLER AS PRECAUTION. NO REPEATS SINCE 10/13.

Part: LINE — MALFUNCTIONED (HYD SYSTEM) · airframe 45,017 hrs · 6,557 cycles

CREW REPORTS LOSS OF GREEN HYDRAULICS SYSTEM. ALTERNATE GEAR EXTENTION USED FOR LANDING. [06-22-07] FOUND A CRACK UNDERNEATH A CLAMP AREA ON THE HYDRAULIC LINE TO THE MAIN LANDING GEAR UPLOCK. REPLACED HYDRAULIC LINE AND REPLACED EDP AND CASE FILTER AS A PRECAUTIONARY MEASURE.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 44,978 hrs · 16,537 cycles

EMERGENCY LIGHT TEST FAILED ON 3SVC CK. FAULTS INT LOADS EMERG L, EXT LOADS EMERG L, AND COMM EMERG L IN VIEW. SUPPLEMENTAL DATA UPDATE REPLACED POWER SUPPLY AND BATTERY. OP CHECKS GOOD.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 44,607 hrs · 16,387 cycles

GREEN HYDRAULIC PUMP FAILURE JUST AFTER DEPARTURE. REPLACED NR 1 ENGINE PUMP PRESSURE SWITCH. RAN ENGINE PRESSURE AND INDICATION NORMAL.

Part: SLIDE — UNSERVICEABLE (L2 DOOR) · airframe 43,684 hrs · 16,036 cycles

PASSENGER DOOR 2L ESCAPE SLIDE RAFT RELEASE STRAP NOT ROUTED THROUGH GIRT BAR. RELEASE STRAP AND SURVIVAL KIT LANYARD NOT VELCROED TO EACH OTHER. REPLACED 2L SLIDE-RAFT.

Part: SLIDE — UNSERVICEABLE (R2 DOOR) · airframe 43,684 hrs · 16,036 cycles

PASSENGER DOOR 2R ESCAPE SLIDE RAFT RELEASE STRAP NOT ROUTED THROUGH GIRT BAR. RELEASE STRAP AND SURVIVAL KIT LANYARD NOT VELCROED TO EACH OTHER, MOORING LINE LOOSE IN GIRT AND NOT ATTACHED TO GIRT BAR, ELECTRICAL HARNESS LOOSE (NOT SECURED UNDER VELCRO) AND HARNESS CONNECTOR HAS LOOSE PINS AND IS EASILY DISCONNECTED. REROUTED STRAP THROUGH GIRT BAR AND ATTACHED RELEASE STRAP AND SURVIVAL KIT LANYARD TOGETHER USING VELCRO. SECURED MOORING LINE. CLEANED AND SECURED HARNESS CONNECTOR.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 43,684 hrs · 16,036 cycles

PASSENGER DOOR 1L ESCAPE SLIDE RAFT RELEASE STRAP NOT ROUTED THROUGH GIRT BAR. RELEASE STRAP AND SURVIVAL KIT LANYARD NOT VELCROED TOGETHER, PARACHUTE PIN NOT SECURED WITH NYLON THREAD (IT IS SECURED WITH A LACING CORD WHICH LOOKS LIKE IT WILL NOT BREAK EASILY TO RELEASE THE PIN) AND PULL HANDLES ATTACHED TO WIRE LOOPS ON STUD ASSEMBLIES BUT ARE NOT ATTACHED TO THE INFLATION CABLES.

Part: LANDING GEAR — MALFUNCTIONED (NLG & MLG) · airframe 43,476 hrs · 15,958 cycles

FLIGHT DIVERTED DUE TO LANDING GEAR PROBLEMS. GEAR WAS MANUALLY EXTENDED. REPLACED LANDING GEAR CONTROL INTERFACE UNIT NR 1 AND 2. OPS CHECKED GOOD. ALSO REPLACED NORMAL LANDING GEAR CONTROL LEVER. ALL CHECKS NORMAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,943 hrs · 15,755 cycles

EMERGENCY ESCAPE PATH LIGHT INOP ON LAV-D DOOR 2L. RELAMPED BULBS, LIGHT OPS GOOD.

Part: UNKNOWN — UNKNOWN · airframe 42,936 hrs · 15,753 cycles

CREW REPORTS ALTERNATE LAW DISPLAYED WITH NO FLIGHT CONTROL FAULTS. REPLACED NR 2 ELAC AND ACCOMPLISHED TEST, TEST NORMAL.

Part: BATTERY — FAULTY (CABIN) · airframe 42,618 hrs · 15,622 cycles

FOUND 1L EMERGENCY LIGHT BATTERY FAULT. REPLACED BATTERY, SYSTEM TESTS OK.

Part: LANYARD — DAMAGED (L2 DOOR SLIDE) · airframe 41,725 hrs · 15,252 cycles

FOUND LANYARD IS DAMAGED AT L2 DOOR SLIDE. REPLACED SLIDE/RAFT ASSY.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 41,510 hrs · 15,164 cycles

NR 1 ENG HAD A COMPRESSOR STALL DURING CLIMB AT APPROX 3000 FT AGL WITH A UPPER ECAM WARNING. UNDETERMINED CAUSE, TROUBLESHOOTING CHECKS RETURNED NO DEFECTS.

Part: BLOWER — SEIZED (CABIN) · airframe 41,283 hrs · 15,073 cycles

BLOWER FAULT DISPLAYED ON UPPER ECAM SCREEN. BLOWER FAULT DISPLAYED ON UPPER ECAM SCREEN. MAINTENANCE CHECKED AND FOUND BLOWER FAN 20HQ SEIZED AND CIRCUIT BREAKER AD10 TRIPPED. REPLACED AEVC BLOWER FAN 20HQ (MR21211, 644-0089) PER MM 21-26-51. SYSTEM OP-CHECK GOOD. FAN WAS ORIGINALLY REPLACED BY BORROWED PART FROM AMERICA WEST S/N 3976. BORROWED PART WAS REPLACED AND RETURNED TO LENDER WITH UAL PART INSTALLED ON AIRCRAFT. POTENTIAL CAUSE OF FAILURE WAS SEIZED BEARING. UAL HAS PROGRAM IN PLACE TO REPLACE WITH CERAMIC BEARINGS.

Part: ASPIRATOR — UNSERVICEABLE (SLIDE) · airframe 40,019 hrs · 14,521 cycles

TWO (2) DAMAGED ASPIRATORS.

Part: ELECTRICAL SYS — UNKNOWN (GALLEY) · airframe 38,568 hrs · 14,034 cycles

FLIGHT ATTENDANT SHOCKED WHILE HOLDING THE G1 AND G2 GALLEY COUNTER TOPS, DURING POWER TRANSFER FROM GROUND TO APU. INSPECTION AND VERIFICATION OF THE ELECTRICAL GROUNDING OF BOTH HOT GALLEY AND COLD GALLEY SECTIONS WERE ACCOMPLISHED IN ACCORDANCE WITH THE AMM 25-33-41. NO SIMILAR INCIDENT HAS BEEN REPORTED SINCE THE ACCOMPLISHMENT OF GROUNDING VERIFICATION.

Part: STRUCTURE — DAMAGED (RT ELEVATOR) · airframe 33,227 hrs · 12,227 cycles

RT ELEVATOR MR55500-006 HAD 4 AREAS OF WATER INGRESS FOUND DURING ACP OF COA 40535. UPPER SURFACE HAD AN AREA 2.6 BY 1.3 INCH LOCATED 160.5 INCHES FROM I/B EDGE, AND 3.5 INCHES FROM T/E LWR SURFACE HAD 3 AREAS, ONE 4.0 BY 1.5 INCH FROM 113 INCHES FROM I/B EDGE, ONE 1.4 BY .7 INCH, 116 INCHES FROM I/B EDGE, AND ONE 1.1 BY 1 INCH, 161 INCHES FROM I/B EDGE. ALL WERE 3.5 INCHES FWD OF THE T/E. MAJOR REPAIR ACCOMPLISHED. REPAIRED PER SRM 55-21-11, REP 5E, PG 226, FIG 205, SHEETS 3 & 4.

Part: STRUCTURE — DAMAGED (LT ELEVATOR) · airframe 33,227 hrs · 12,227 cycles

LEFT ELEVATOR MR55501-006 HAD 2 AREAS OF WATER INGRESS FOUND DURING ACP OF COA 40535. ONE ON THE UPPER SURFACE 2.3 BY 1.4 INCH, 154 INCHES FROM THE I/B EDGE, AND 3.5 INCHES FROM THE T/E. ONE ON THE LWR SURFACE 2.9 BY 1.9 INCH, 139 INCHES FROM THE I/B EDGE AND 3.5 INCHES FROM THE T/E. MAJOR REPAIR ACCOMPLISHED. REPAIRS ACP PER SRM 55-21-11 REP 5E, PG 226, FIG 205 SHEET 3.

Part: BELLOWS — BLOWN (NR 2 PACK) · airframe 27,384 hrs · 9,887 cycles

CABIN ALTITUDE COULD NOT BE MAINTAINED BELOW 10,000 IN AUTO. PACK NR 2 WAS DEFERRED INOPERATIVE, PACK NR 1 WOULD NOT PRESSURIZE THE CABIN, FOUND BLOWN COOLING DUCT BELLOWS NR 1 PACK, REPLACED AND OPERATIONALLY CHECKED NORMAL. PACK NR 2 WAS LATER OPERATIONALLY CHECKED AS NORMAL. NO FURTHER DISCREPANCIES REPORTED.

Part: THERMOSTAT — FAILED (BLEED AIR) · airframe 26,000 hrs · 9,408 cycles

NR 1 ENGINE BLEED FAULT DISPLAYED ON UPPER ECAM SCREEN. *S/D* REPLACED CONTROL THERMOSTAT AS FAULTED IN CENTRALIZED FAULT DISPLAY SYSTEM. IN ADDITION, THE HEAT EXCHANGER OUTLET TEMPERATURE SENSOR AND BLEED MANAGEMENT COMPUTER WERE REPLACED PRECAUTIONARY. NO FURTHER FAULTS NOTED.

Part: COFFEEMAKER — SHORTED (GALLEY) · airframe 23,755 hrs · 8,621 cycles

ELECTRICAL SMELL COMING FROM AFT GALLEY OVEN AREA. *S/D* COFFEEMAKER M42, P/N 11225-1 HAD AN INTERNAL ELECTRICAL FAILURE (WIRING MELTED) WHICH CAUSED AN ELECTRICAL SMELL IN THE AFT GALLEY. THIS COFFEEMAKER WAS REMOVED AND REPLACED. NO REPEAT A/C WRITE-UPS.

Part: TUBE — WILL NOT TEST (ESCAPE SLIDE)

AFT DOOR SLIDE/RAFT LOWER TUBE FAILED PROOF PRESSURE TEST. *S/D* FOUND THE LOWER TUBE TO HAVE A SEAM FAILURE AT THE TOP END CROSSOVER TUBE. SENT UNIT TO VENDOR FOR REPAIR.

Part: PUMP — LEAKING (NR 1 HYD SYSTEM)

INTERMITTENT GREEN HYD SYSTEM LOW ECAM WARNING. PRESSURE NORMAL AND NO FLUCTUATION. FOUND NR 1 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. REPLACED PUMP PER MM29-11-51. LEAK AND OPS CHECKS GOOD.

Part: PAN — CRACKED (PASSENGER SEAT)

DURING THE FIRST HEAVY MAINTENANCE VISIT (HMU-1) VIRTUALLY 100 PERCENT OF THE COACH SEATS IN THE PASSENGER CABIN WERE FOUND TO HAVE SEAT PANS THAT WERE CRACKED AT THE FORWARD ATTACHMENT HOLES FOR THE SEAT PANS. THESE ARE RECARO 720 SERIES SEATS INSTALLED IN A-320-232 AIRCRAFT. THE SEAT MFG DESIGNATES THE SEAT PAN AS PRIMARY STRUCTURE FOR THE SEAT. SUBMITTER STATED AN AD SHOULD BE ISSUED TO INSPECT THESE SEAT PANS FOR CRACKS EACH 90 DAYS AND FOR REMOVAL FROM SERVICE OF ANY PANS THAT ARE CRACKED. THESE PANS ARE BEING REPLACED WITH NEW SEAT PANS THAT HAVE SAME DESIGN FLAWS WHICH WILL CRACK IN SERVICE. THERE ARE 132 SEAT PANS ON THE ACFT. THIS IS THE 6TH A-320 TO SHOW 100 PERCENT FAILURE OF THESE SEAT PANS.

Part: WINDOW — CRACKED (LT COCKPIT)

UPON ARRIVAL, FOUND LOWER ECAM WARNING RELATED TO THE NR 3 CAPTAINS FIXED WINDOW 7DG1. INSPECTED AND FOUND THE NR 3 WINDOW CRACKED 7DG1 NP165313-1 OUT OF LIMITS REF AIRBUS MM 56-11-12-200-001. REPLACED NR 3 CAPTAINS FIXED WINDOW REF MM TASK 56-11-12-400-002. SUBSEQUENT INSPECTION OF WINDOW CONFIRMS A 9 INCH CRACK IN THE LOWER LT CORNER OF THE INNER (STRUCTURAL) GLASS PLY. THERE IS ALSO EVIDENCE OF MOISTURE INGRESS AND DELAMINATION OF THE GLASS PLYS IN THE AREA.

Part: BATTERY PACK — DISCHARGED (CABIN)

AFT LEFT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHT TEST FAILED. REPLACED FWD EMERGENCY POWER SUPPLY UNIT.

Part: LGCIU — FAILED (NR 2)

RECEIVED AN ECAM FLIGHT CONTROL FLAPS LOCKED FAULT MESSAGE. FOLLOWED APPROPRIATE PROCEDURES AND LANDED WITH SLATS, BUT NO FLAPS. LANDING WAS UNEVENTFUL. FOUND SENSOR NR 1 (P/N ABS0121-30) MISADJUSTED AND LGCIU NR 2 HAD A HARD FAULT. SFCC INTERPRETED SIGNAL AS A RUNAWAY FLAP AND WING TIP BRAKES WERE DEPLOYED. REPLACED LGCIU NR 2 AND READJUSTED SENSOR NR 1, OPERATIONALLY CHECKED NORMAL.