N407UA

Part: PROFILE — CRACKED (RH FWD DR) · airframe 88,548 hrs · 34,587 cycles

RH FWD EMERGENCY EXIT HATCH, LH LOAD TRANSMITTING PROFILE SHOWS EVIDENCE OF A CRACK EMANATING FROM RIVET HOLE. REPAIR ACCOMPLISHED AT RH FWD OF THE LATEST REVISION OF THE ECRA 5211-01792 ON OR BEFORE EMERGENCY EXIT HATCH, ACCOMPLISH INITIAL INSPECTION PER PART 2 98,857 TC. CURRENT AC TC IS 34,587. THE REPAIR WAS ACCOMPLISHED IN PART 1 OF ECRA 5211-01792 AND IS A CAT B REQUIRING REPETITIVE INSPECTION (RIR) STATED IN PART 2 FOR THE INTERIM REPAIR ACCOMPLISHED AT RH FWD EMERGENCY EXIT TOMC-APPROVAL FROM SC1ELBYC COMMENT HATCH, ACCOMPLISH INITIAL INSPECTION PER PART 2 OF THE LATEST REVISION OF THE ECRA 5211-01792 ON OR BEFORE 98,587 TOTAL AIRCRAFT FLIGHT CYCLES.

Part: SKIN — DAMAGED (L2 DOOR) · airframe 88,548 hrs · 34,587 cycles

L2 DOOR OUTER BOTTOM SKIN HAS SCRATCHES.

Part: CVR — NO TEST · airframe 88,548 hrs · 34,587 cycles

CVR ULB FAILS OP CHECK. REMOVED AND REPLACED CVR ULB; OPS CHECK C/W GOOR IAW AMM 23-71-35-920-001-A.

Part: WARNING MESSAGE — ILLUMINATED (MLG DOWNLOCK) · airframe 84,345 hrs · 32,603 cycles

*DECLARED EMERGENCY* GEAR NOT UPLOCKED DISPLAYED ON UPPER ECAM SCREEN - L-G . OPEN

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 83,425 hrs · 32,218 cycles

EPSU 11WL FAILS CHECK FOR EPSU BATT (SUPPORT TASK).

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 83,425 hrs · 32,218 cycles

13WL FAILS OPERATIONS CHECK (A3NB 33-3-6013). GENERATED BY V894373. GENERATED AT HAECO LCQ, PER NR. 9292015.

Part: INTERCOSTAL — DAMAGED (EMERGENCY EXIT) · airframe 83,425 hrs · 32,218 cycles

LT AFT EMERGENCY EXIT HATCH HAS A FRAME-SUPPORT TASK-NR 9292383 GENERATED BY V077960 AT HAECO LCQ. REMOVED AND REPLACED SUPPORT ANGLE AT LT AFT EMERGENCY EXIT HATCH, IAW A320 SRM 51-72-11-911-001 REMOVED DOT. ACCOMPLISHED BY V90 0592, INSP BY V914670.

Part: INTERCOSTAL — CRACKED (EMERGENCY EXIT) · airframe 83,425 hrs · 32,218 cycles

LT FWD EMERGENCY EXIT HATCH HAS A FRAME CRACKED-SUPPORT TASK-NR 9292384 GENERATED BY V077960 AT HAECO LCQ. LT FWD EMERGENCY EXIT HATCH FRAME THAT WAS CRACKED WAS REPLACED WITH A NEW FRAME, IAW A320 SRM 51-72-11-911-001 PART 2C AND 51-72-11-911-001 PART D. APPLIED CIC IAW A320 SRM 51-23-12-801 PG 3 (B) 1-3. REMOVED DOT K004. ACCOMPLISHED BY V914609 INSP BY V914 670.

Part: DOUBLER — DAMAGED (FRAMES 73-74) · airframe 83,425 hrs · 32,218 cycles

REMOVE AND REPLACE AFT FUSELAGE INTERNAL DOUBLER BETWEEN FR 73-FR 74 STR 33L-33R JACKING POINT AREA. EC/RA: 5351-01177-NR 929 2286. REMOVED AND REPLACED AFT FUSELAGE INTERNAL DOUBLER BETWEEN FR 73-FR 74, STR 33L-STR 33R AT JACKING POINT, IAW UNITED EC/RA 5351-01 127 AND AIRBUS DWG D53571511.

Part: ATTACH FITTING — CRACKED (LT MLG DOOR) · airframe 83,425 hrs · 32,218 cycles

EA 5330-04821 002 AD 2015-02-14 LT MLG DOOR FORWARD LOWER ATTACH FITTING IS CRACKED AROUND FORWARD LOWER FASTENER HOLE. REMOVED AND REPLACED LT MLG DOOR FWD ATTACH FITTING, IAW A320 SRM 51-42-11-801 AND AIRBUS REPAIR INSTRUCTION R33 70500F.

Part: SKIN — DAMAGED (FRAMES 57-58) · airframe 83,425 hrs · 32,218 cycles

LT FUSELAGE SKIN FR 57-58 AT STR 37L HAS PREVIOUS DENT REPAIRED WITH INSTALLATION OF FASTENER THAT IS OUT OF LIMITS, IAW A320 SRM 53-00-11-283-005. SKIN REQUIRES REPAIR (SUPPORT TASK). REPAIR ACCOMPLISHED LT FUSELAGE EXTERIOR SKIN BETWEEN FR 57-58 AT STR 37L, IAW SRM 53-00-11-300-042. THIS REPAIR IS CATEGORY B WITH DEFINED INSPECTION INTERVALS, IAW SRI 53-00-11-205-052. INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT AT FC 21 200/FH 42400, WHICHEVER IS ACHIEVED FIRST. SUBSEQUENT INSPECTION AT INTERVALS OF FC 2200/FH 4400, WHICHEVER IS ACHIEVED FIRST, FIGURE 004. CURRENT FC: 32218, FH: 83424:41. INSPECTION METHODS HFEC AND ULTRASOUND, IAW SRI 53-00-11-205-052. OK TO CARRY REPAIR OF DENT FOR 21200 FLT CYCLES OR 42400 FLT HOURS, WHICHEVER IS ACHIEVED FIRST FROM TIME OF REPAIR WITH RECHECKS TO BE ACCOMPLISHED EVERY 2200 CYCLES OR 4400 FLT HRS THEREAFTER .

Part: SKIN — DENTED (FRAMES 57-58) · airframe 83,425 hrs · 32,218 cycles

LT FUSELAGE SKIN FR 57-58 AT STR 37L HAS PREVIOUS DENT REPAIRED WITH INSTALLATION OF FASTENER THAT IS OUT OF LIMITS, IAW A320 SRM 53-00-11-283-005. SKIN REQUIRES REPAIR (SUPPORT TASK). GENERATED BY V061619 AT HAECO LCQ, PER NR 9292324. REPAIR ACCOMPLISHED LT FUSELAGE EXTERIOR SKIN BETWEEN FR 57-58 A T STR 37L, IAW SRM 53-00-11-300-042. THIS REPAIR IS CATEGORY B WITH DEFINED INSPECTION INTERVALS, IAW SRI 53-00-11-205-052. INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT AT FC 21 200/FH 42400 WHICHEVER IS ACHIEVED FIRST. SUBSEQUENT INSPECTION AT INTERVALS OF FC 2200/FH 4400 WHICHEVER IS ACHIEVED FIRST, FIGURE 004. CURRENT FC: 32218, FH: 83424:41. INSPECTION METHODS HFEC AND ULTRASOUND, IAW SRI 53-00-11-205-052. OK TO CARRY REPAIR OF DENT FOR 21200 FLIGHT CYCLES OR 42400 FLIGHT HOURS WHICHEVER IS ACHIEVED FIRST FROM TIME OF REPAIR WITH RECHECKS TO BE ACCOMPLISHED EVERY 2200 CYCLES OR 4400 FLIGHT HOURS THEREAFTER TOMC-APPROVAL FROM SC1ELBYC COMMENT. QC REVIEWED QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 83,425 hrs · 32,218 cycles

ROW 30-31 EMERGENCY LIGHTS ARE INOPERABLE. A3NB-33-3-6033, PER HAECO LCQ N/R 9292017/40017 GENERATED BY V894373. REPAIRED BROKEN EEPL WIRE FOR SEATS 30-31 LT, PER A310/A320 AWM 3 3-51-08 PG 2, ESPM 20-43-11-0101 A. OPERATION CHECKS GOOD, PER AMM 33-51-00-710-009-A.

Part: SERVO CONTROL — DEFECTIVE (NLG STEERING) · airframe 82,030 hrs · 31,577 cycles

NW STEER FAULT DISPLAYED ON UPPER ECAM SCREEN. - WHEEL FAULT OCCURED ON FINAL.AFTER RECYCLING THE GEAR THE FAULT CLEARE D. REMOVED & REPLACED NOSE WHEEL STEERING SERVO CONTROL IAW AMM32-51-51-400-001-A, PERFORMED OPS CHECK WITH HANDWHEEL OPS CHECKED GOOD IAW AMM 32-51-00-720-003-A, PERFORMED OPS CHECK WITH THE PEDALS OPS CHECKED GOOD NO DEFECTS NOTED IAW AMM 32-51-00-720-004A ROTABLE PARTS CHANGE WAS INDICATED - TT # 1160282 SN OFF 0118 IPC REFERENCE # 32-51-51

Part: STOP FITTING — CRACKED (L1 DOOR FR16) · airframe 79,724 hrs · 30,577 cycles

L1 DOOR FRAME 16 STOP FITTING NO. 1 LOWER OUTBOARD HOLE IS CRACK ED IN FRAME LAYER AT 6:00. LOWER INBOARD HOLE CRACKED IN FRAME A T 6:00 ON HAECO LCQ REF 9296158 SPEC A3NB-53-4-6304 AD 2017-22-0 3. NR GENERATED BY V061633 REPAIRED AND INSPECTED PER ECRA 5311-02050. ACCOMPLISH INITIAL I NSPECTION PER PART 2 OF ECRA 5311-02050 ON OR BEFORE AIRCRAFT RE ACHES 42677 FC''S. ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 12,100 FLIGHT CYCLES THEREAFTER. OKAY TO CARRY FORWARD WITH INITIAL INSPECTION OF L1 DOOR FRAME 16 STOP FITTING NO. 1 LOWER OUTBOARD HOLE PER PART 2 OF ECRA 5311-02050 AT OR BEFORE AIRCRAFT REACHES 42,677 FLIGHT CYCLES (FC). ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 12,100 FC THEREAFTER. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED. QC REVIEWED. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: INTERCOSTAL — CRACKED (L1 DOOR FR16) · airframe 79,724 hrs · 30,577 cycles

L1 DOOR FRAME 16 STOP FITTING NO. 7 LOWER INBOARD HOLE IS CRACKE D IN INTERCOSTAL FLANGE 12:00. UPPER INBOARD HOLE IS CRACKED IN INTERCOSTAL FLANGE AT 12:00 ON HAECO LCQ REF 9296161 SPEC A3NB-5 3-4-6304 AD 2017-22-03. NR GENERATED BY V061633 REMOVED AND REPLACED INTERCOSTAL AT FR16 AND REPAIR PER ECRA 531 1-02050. ACCOMPLISH INITIAL INSPECTIONS PER PART 2 OF ECRA 5311- 02050 ON OR BEFORE AIRCRAFT REACHES 42,677 FLIGHT CYCLES AND REP ADD EMP:V061616 ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 12,100 FLIGHT CYCLES THEREAFTER. OKAY TO CARRY FORWARD WITH INITIAL INSPECTION PER PART 2 OF ECRA 5311-02050 AT OR BEFORE AIRCRAFT REACHES 42,677 FLIGHT CYCLES (FC). ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 12,100 FC THEREAFTER. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED. QC REVIEWED. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: SKIN — DENTED (BS 6311-7087) · airframe 79,724 hrs · 30,577 cycles

DENT BETWEEN STA 6311 & STA 7087 AT FLOOR LEVEL FORWARD OF L1 DO OR IS OUT OF LIMITS. PREVIOUS DENT ON HAECO LCQ REF 9296486 SUPP ORT TASK. REF. CLRD LP8398453. LIMITED CUTOUT REPAIR OF THE EXTERNAL SKIN ACCOMPLISHED AND INSP ECTED AT LCQ DURING C-2 VISIT IAW SRM 53-00-11-300-029. IT IS NE CESSARY TO INSPECT THIS REPAIR AT DEFINED INTERVALS REF. SRI 53-00-11-205-017. AT TIME OF ADL/REPAIR EMBODIMENT 60000 FC, 120000 FH. WHICHEVER VALUE FC/FH IS ACHIEVED FIRST. SUBSEQUENT INSPECTION TBD. AREA OF REPAIR IS LOCATED BETWEEN FRAMES 13 AND 14. PER SRI 53-0 0-11-205-017 REPAIR IS IN ZONE A. REFERENCE SRM 53-11-11-001, NO MINAL SKIN THICKNESS IN THE REPAIR AREA IS .079 (CODE F). OKAY TO DIP FOR 60,000FC / 120,000 FH REF SRI 53-00-11-205-017. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED. QC REVIEWED. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: STOP FITTING — CRACKED (R1 DOOR) · airframe 79,724 hrs · 30,577 cycles

R1 DOOR FRAME 16 STOP FITTING NO. 7 UPPER INBOARD HOLE IS CRACKE D IN FRAME WEB AT 1:00 & CRACKED IN INTERCOSTAL FLANGE AT 6:00. LOWER INBOARD HOLE IS CRACKED IN THE FRAME WEB AT 6:00 ON HAECO LCQ REF 9296166 SPEC A3NB-53-4-6304 AD 2017-22-03. NR GENERATED BY V061633 REMOVED AND REPLACED R-1 DOOR FR16 STOP FITTING INTERCOSTAL AND REPAIRED #7 UPPER I/B HOLE IAW ECRA 5311-02050. ACCOMPLISH INITI AL INSPECTIONS PER PART 2 OF ECRA 5311-02050 ON OR BEFORE A/C ADD EMP:V061616 REACHES 42,677 TOTAL FC. ACCOMPLISH REPEAT INSPECTION INTERVALS NOT TO EXCEED 12,100 AIRCRAFT FC THEREAFTER OKAY TO CARRY FORWARD WITH INITIAL INSPECTION OF R1 DOOR FRAME 16 STOP FITTING NO. 7 UPPER INBOARD HOLE PER PART 2 OF ECRA 5311-02050 AT OR BEFORE AIRCRAFT REACHES 42,677 FLIGHT CYCLES (FC). ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 12,100 FC THEREAFTER. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED. QC REVIEWED. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: SPACER — WORN (L2 DOOR) · airframe 79,724 hrs · 30,577 cycles

L-2 RIG PINS FAILED RIG CHECK DOOR STICKING WHEN OPENING A3NB-52 -3-6085 PER HAECO LCQ NR 9296251 GENERATED BY V071330 REMOVED L2 DOOR TO FOM BUSHING AND HAS DENSE REPLACEMENT IAW A32 0 AMM 52-13-11-000-001A ERMOVED AND REPLACED BUSHING AS REQUIRED IAW A320 SRM 51-72-12-911-002, REMOVED AND REINSTALLED UPPER AN D LOWER CONNECTED LEAKS IAW A320 AMM 52-13-21, REMOVED AND REPLA CED L2 DOOR SUPPORT ARM UPPER AND LOWER FITTINGS IAW A320 -400-001 WORK ACCOMPLISHED BY V061634 INSP BY LC-10 Y AND RIGGED IAW A320 AMM 52-13-12-400-001 AND A320 AMM 52-13-11 \MM 52-13-31-000-008A AND 52-13-31-400-002 INSTALLED L2 DOOR ASS Y

Part: INTERCOSTAL — CRACKED (L1 DOOR FR16) · airframe 79,724 hrs · 30,577 cycles

L1 DOOR FRAME 16 STOP FITTING NO. 1 LOWER OUTBOARD HOLE IS CRACK ED IN FRAME LAYER AT 6:00. LOWER INBOARD HOLE CRACKED IN FRAME A T 6:00 ON HAECO LCQ REF 9296158 SPEC A3NB-53-4-6304 AD 2017-22-0 3. NR GENERATED BY V061633 REPAIRED AND INSPECTED PER ECRA 5311-02050. ACCOMPLISH INITIAL I NSPECTION PER PART 2 OF ECRA 5311-02050 ON OR BEFORE AIRCRAFT RE ACHES 42677 FC''S. ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 12,100 FLIGHT CYCLES THEREAFTER. OKAY TO CARRY FORWARD WITH INITIAL INSPECTION OF L1 DOOR FRAME 16 STOP FITTING NO. 1 LOWER OUTBOARD HOLE PER PART 2 OF ECRA 5311-02050 AT OR BEFORE AIRCRAFT REACHES 42,677 FLIGHT CYCLES (FC). ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 12,100 FC THEREAFTER. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED. QC REVIEWED. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: SELECTOR VALVE — INOPERATIVE (LANDING GEAR) · airframe 78,727 hrs · 30,148 cycles

GEAR NOT DOWNLOCKED DISPLAYED ON UPPER ECAM SCREEN. LG CYCLED GEAR AND WAITED OVER ONE MINUTE PER ECAM GEAR THEN XTENDED VERBAL FROM CREW. ON INITIAL ATTEMPT 3 GEAR DOORS OPENED GEAR DID NOT COME DOWN. CYCLED HANDLE TO UP. ON SECOND ATTEMPT EVER DOWN GEAR DID NOT COME DOWN AGAIN AND GOT AN ECAM MSG TO WAIT 120 SECONDS. AFTER ABOUT A MINUTE WITH LEVER STILL DOWN GEAR CAME DOWN WITH 3 GREEN LIGHTS. TROUBLESHOT PER TSM 32-31-00-810-808-A. REMOVED ASND REPLACED LANDING GEAR DOOR SELECTOR VALVE 1GA REF MM 32-31-34. PERFORMED FUNCTIONAL CHECK OF LANDING GEAR. REF MM 32-31-00. ALL LANDING GEAR AND DOOR INDICATIONS AND OPERATION NORMAL. NO LEAKS NOTED. ACFT RETURNED TO NORMAL CONFIG.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 76,724 hrs · 29,258 cycles

EMERGENCY LIGHT ELECTRICAL COVERS MISSING AT ROW 11,36 A INSTALLED EMERGENCY LIGHT ELECTRICAL COVERS AT ROW 11,36 A

Part: BATTERY PACK — FAULTY (CABIN) · airframe 75,845 hrs · 28,841 cycles

LEFT AFT EMERGENCY LIGHT POWER SUPPLY FAULTING REF 2 SVC ITEM 16. REPLACED BATTERY PACK, REF AMM 33-51-00, EMERG LIGHTS OPS CHECK OK.

Part: ACTUATOR — FAULTY (LT A/C PACK) · airframe 75,556 hrs · 28,700 cycles

ZONE REGUL FAULT, PACK REG DISPLAYED ON UPPER ECAM SCREEN . UNABLE TO CONTROL CABIN TEMP. EMERGENCY DECLARED. REPLACED THE LT A/C PACK INLET ACTUATOR IAW AMM 21-61-51-400-001-B. NO FAULTS NOTED.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 75,538 hrs · 28,691 cycles

EMER LIGHTS TEST FAILED. UNIT EMER RT FAULT ON CABIN PTP PNL. REPLACED EPSU AND BATTERY UNIT. EMER LIGHTS TEST PASSED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 75,462 hrs · 28,659 cycles

R FWD CABIN DISPLAYED ON UPPER ECAM SCREEN. DOOR INTERMITTENT ECAM-PRESSURE NORMAL. WHEN ON-ACCOMPANIED BY SLIDE ARMED RED LIGHT ON DOOR. REF TSM 52-10-00 NO FAULTS OR DEFECTS FOUND.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 75,341 hrs · 28,611 cycles

L2 DOOR EMERGENCY EXIT LOWER AFT LIGHT ASSY INOPERATIVE. SECURED A LOOSE CONNECTION.

Part: STRAP — LOOSE (R2 DOOR SLIDE) · airframe 74,895 hrs · 28,412 cycles

R2 DOOR DISARMED IN FLIGHT, HANDLE POPPED OUT OF ARMED POSITION. FOUND TH SLIDE COVER LOWER STRAPS LOOSE AND HANGING DOWN UNDER THE GIRT BAR, SECURED THE STRAPS. PERFORMED AMM 52-10-00-860-001-A, AMM 52-10-00-720-005-A, AND AMM 52-73-00-710-001-A, OPS CHECKED NORMAL.

Part: ALTIMETER — FAULTY (STANDBY) · airframe 74,798 hrs · 28,372 cycles

STANDBY ALTIMETER INDICATION ERRONEOUS STANDBY ALTIMETER READS BETWEEN 280 AND 380 FEET AT FL 360 STANDARD ALT SET REPLACED THE STDBY ALTIMETER IAW 34-21-22, CKS OK

Part: FITTING — DIRTY (L2 DOOR) · airframe 74,502 hrs · 28,244 cycles

LEFT AFT SLIDE INDICATION INOP ON DOOR-OXY SYSTEM ECAM PAGE - DOOR-OXY DOOR 2L ARMED ON GROUND SLIDE ARM DISAPPEARS IN FLIGHT. ONLY SHOWS ARM WHEN FA PUSHES HANDLE CLEANED FLOOR FITTINGS AND OPERATED ARM/DISARM LEVER MULTIPLE TIMES REF AMM 25-62-44. OP'S CHECKS NORMAL AND INDICATION NORMAL. OK TO CONTINUE.

Part: STRINGER — CORRODED (FRAMES 32-33) · corrosion level 2 · airframe 74,383 hrs · 28,190 cycles

EVIDENCE OF CORROSION ON STRINGER 43R , BETWEEN FRAMES 32 AND 33. REMOVED & REPLACED THE STRINGER IAW SRM 51-42-11.

Part: SHEAR TIE — CORRODED (FRAME 31) · corrosion level 2 · airframe 74,383 hrs · 28,190 cycles

SHEAR TIE AT FRAME 31, BETWEEN STRINGERS 41-42L HAS CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-42-11.

Part: SHEAR TIE — CORRODED (FRAME 30) · corrosion level 2 · airframe 74,383 hrs · 28,190 cycles

FWD CARGO BAY AT FRAME 30, BETWEEN STRINGERS 42-43R SHEAR TIE HAS CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-42-11.

Part: SHEAR TIE — CORRODED (FRAME 32) · corrosion level 2 · airframe 74,383 hrs · 28,190 cycles

FWD CARGO BAY AT FRAME 32 BETWEEN STRINGERS 42-43R SHEAR TIE HAS CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-42-11.

Part: SHEAR TIE — CORRODED (FRAME 32) · corrosion level 2 · airframe 74,383 hrs · 28,190 cycles

FWD CARGO BAY FRAME 32 BETWEEN STRINGERS 41-42R SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-44-11.

Part: SHEAR TIE — CORRODED (FRAME 31) · corrosion level 2 · airframe 74,383 hrs · 28,190 cycles

FWD CARGO BAY SHEAR TIE AT FRAME 31 BETWEEN STRINGERS 42 AND 43R HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-44-11.

Part: SHEAR TIE — CORRODED (FRAME 31) · corrosion level 2 · airframe 74,383 hrs · 28,190 cycles

FWD CARGO BAY SHEAR TIE AT FRAME 31 BETWEEN STRINGERS 42-43R HAS CORROSION. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-44-11

Part: STRINGER — CORRODED (FRAMES 32-33) · corrosion level 2 · airframe 74,383 hrs · 28,190 cycles

FWD CARGO BAY STRINGER 41R HAS CORROSION BETWEEN FRAMES 32 AND 33. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-11.

Part: SHEAR TIE — CORRODED (FRAME 31) · corrosion level 2 · airframe 74,383 hrs · 28,190 cycles

FWD CARGO SHEAR TIE CORRODED AT FRAME 31, BETWEEN STRINGERS 40 - 41R. THE SHEAR TIE WAS REPLACED IAW SRM 51 -42-11. MAJOR REPAIR.

Part: STRINGER — CORRODED (FRAMES 32-33) · corrosion level 2 · airframe 74,383 hrs · 28,190 cycles

FWD CARGO BAY STRINGER 41R CORRODED BETWEEN FRAMES 32 AND 33. THE STRINGER SECTION WAS REPLACED IAW SRM 51-42-11. MAJOR REPAIR

Part: SHEAR TIE — CORRODED (FRAME 31) · corrosion level 2 · airframe 74,383 hrs · 28,190 cycles

FWD CARGO BAY SHEAR TIE CORRODED AT FRAME 31, BETWEEN STRINGERS 41 - 42R. THE SHEAR TIE WAS REPLACED IAW SRM 51 -42-11. MAJOR REPAIR

Part: FITTING — CORRODED (FRAME 70) · corrosion level 2 · airframe 74,383 hrs · 28,190 cycles

FITTING CORRODED ON BACK SIDE ATTACHED TO FRAME 70, Y-1162. REMOVED AND REPLACED THE FITTING.

Part: DOOR SILL — CORRODED (R2 DOORWAY) · corrosion level 2 · airframe 74,383 hrs · 28,190 cycles

DOOR 2R SILL CORRODED AT FWD AND AFT ENDS DOOR SILL WAS REPLACED PER SRM 51-72-11 AND SRM 51-42-11.

Part: SUPPORT — CORRODED (FRAME 70) · corrosion level 2 · airframe 74,383 hrs · 28,190 cycles

AFT CABIN FRAME 70 SUPPORT CORRODED AT STRINGER 23R. FRAME SUPPORT WAS REPLACED IAW SRM 51-42-11

Part: STRAP — CORRODED (FRM 70 BULKHEAD) · corrosion level 2 · airframe 74,383 hrs · 28,190 cycles

AFT PRESSURE BULKHEAD FWD FACE RIGHT SIDE DOUBLER STRAP CORRODED AT FRAME 70, Y1162. DOUBLER STRAP WAS FABRICATED AND REPLACED IAW SRM51-42-11 AND 53-51-16.

Part: WIRE — BROKEN (CABIN) · airframe 68,545 hrs · 25,701 cycles

EMERGENCY LIGHT TEST FAILS WHILE ACCOMPLISHING SVC MSG, EXT LOAD AFT L FAILS. REPLACED BROKEN WIRE BETWEEN 2873VC PIN B & 2961VCA PIN K. WIRE BROKEN ON DOOR WHERE HINGE ARM CONNECTS TO DOOR. OPERATIONS CHECKED OK IAW AMM 33-51-00-710-001A.

Part: COVER — MISSING (LT MLG) · airframe 67,143 hrs · 25,165 cycles

PLASTIC COVER AT LT MLG HINGE POINT IS MISSING. INTERIM REPAIR ACCOMPLISHED. REQUIRES DAILY INSPECTION TO ENSURE INTEGRITY OF THE REPAIR & A NEW LT MLG LEG BEARING BLANKING PLUG MUST BE INSTALLED WITHIN 25 FLT HRS IAW ECRA 3211-01346. DL2030 CREATED TO MONITOR. REPLACED LT MAIN GEAR PLASTIC COVER IAW ECRA 3211-01346.

Part: FLAP — FAULTED (WING) · airframe 66,179 hrs · 24,780 cycles

FLAP SYS FAULT AFTER TAKEOFF, RETURN TO FIELD.

Part: THRUST REVERSER — DAMAGED (NR 2 ENGINE) · airframe 65,889 hrs · 24,668 cycles

SEALS INSTALLED THRUST REVERSE COWL, NR 2 ENG INBD UPPER THRUST REVERSER COWL, TO LOWER PYLON TORN. METAL FLAPPING AGAINST PYLON PANEL PER PASSENGER OBSERVATION. LE OF FILLET IS DAMAGED BEYOND REPAIR & WILL NEED TO BE REPLACED.

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 65,686 hrs · 24,588 cycles

RT WING FUEL TANK ACCESS PLATE 640NB HAS DAMAGED HOLE. INSTALLED BUSHING IAW SRM57-21-11 FIG 202 & BRIDGE REPAIR IAW SRM57-21-11 PAGE 213.

Part: ELECTRICAL BOX — INOPERATIVE (CABIN) · airframe 65,684 hrs · 24,586 cycles

CREW REPORT AT SEATS 27F & 28F, PAX STATED SMELL OF BURNING PLASTIC. FIRST OFFICER FELT SIDE WALL, NOT WARM. INSPECTED AREA IAW AMM 05-51-10 & TSM TASK 24-00-00-810-823-A, FOUND SEAT ELEC BOX UNDER 27E INOPERATIVE, WIRING & CONNECTORS GOOD. DISCONNECTED SEB UNDER SEAT 27E, PAX AUDIO SYSTEM INOPERATIVE, MEL 2522AE APPLIED. REFER TO DF121 FOR SIGN-OFF, NO ODOR OR BURNT WIRES NOTED.

Part: TRANSFER VALVE — FAULTY (FUEL TANK) · airframe 65,163 hrs · 24,381 cycles

LT OUTER TANK HAS 280 LB WON’T HOLD FUEL WITH VLV INDICATING CLOSE. CONFIRMED FUEL MIGRATION ON LT OUTER TANK TO INNER CELL WITH TRANSFER VLVS CLOSED. WHILE FUELING, OUTER TANK NEVER FILLED TO MAX QUANTITY & WAS OBSERVED ON ECAM DECREASING & INNER INCREASING. WILL REQUIRE TANK DIVE & TRANSFER VLVS REPLACEMENT. PCN 644-0294, MEL REMAINS. NEXT MX STATION CONFIRM THIS IS NOT A BAD ACTUATOR OUTSIDE OF TANK THAT DRIVES THE FUEL TRANSFER VLV, ACTUATOR PCN IS 565-0084.

Part: LANDING GEAR — MALFUNCTIONED (MAIN) · airframe 64,889 hrs · 24,271 cycles

TEST FLT FAILED. REPORTEDLY TOOK RT MLG 4 ADDITIONAL SECONDS & LT MLG 6 ADDITIONAL SECONDS TO RELEASE THE BALK SOLENOID TO ALLOW GEAR HANDLE TO BE MOVED UP. REPLACED LT & RT MLG IAW ECRA 3210-02291.

Part: INTERFACE UNIT — FAILED (LANDING GEAR) · airframe 64,874 hrs · 24,264 cycles

GEAR RETRACT FAILURE, FLT DIVERTED. TROUBLESHOT IAW TSM 73-25-00-810-830-A. REPLACED LGCIU2 IAW MM 32-31-71, BITE TESTED NORMAL. ACCOMPLISHED FUNCTIONAL TEST OF LANDING GEAR EXTENSION & RETRACTION IAW 32-31-00. CHECKED NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 64,734 hrs · 24,217 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE AT LEFT OVERWING. THREE SEAT LIGHTS & TWO EXIT SIGNS. SPLICED PINCHED & BROKEN WIRES. NO POWER TO SEATS FROM WALL DISCONNECT. OPEN AT PIN 10 AT 11WL (POWER SUPPLY) WITH LIGHTS PLUGGED IN. (WD 33-51-07 PG 1)

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 64,628 hrs · 24,176 cycles

RT WING FUEL TANK LANDING HAS AN ELONGATED HOLE AT 640LB, BETWEEN RIBS 16-17. CHECKED LIMITS ON RT WING LANDING HOLE AT 640LB, BETWEEN RIBS 16-17, HOLE IS OUT OF LIMITS. REAMED HOLE, INSTALLED BUSHING & BRIDGING PLATES IAW SRM 57-21-11. REINSPECTION REQ IAW SRI57-21-11,PG207 AT 31100FC OR 54600FH AFTER 1ST FLIGHT, AC CURRENT PTT 64628.25 WHICH EXCEEDING LIMITS. IAW ENG'S USE INTERV MF3101 CREATED TO MONITOR: ITEM MOVED TO CF9. REF SRI 57-21-11-2-002-00, NEED REPETITIVE INSPECTION EVERY 3600CYC- 4500HRS. MF3101 UPDATED. CURRENT PTC 24176, PTT 64628.

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 64,628 hrs · 24,176 cycles

RT WING FUEL TANK LANDING HAS AN ELONGATED HOLE AT 640LB, BETWEEN RIBS 16-17. FOUND TO BE OUT OF LIMITS, REPAIRED HOLE. INSTALLED BUSHING AND BRIDGING PLATE IAW SRM.

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 64,628 hrs · 24,176 cycles

RT WING FUEL TANK LANDING FOR PANEL 640PB HAS ONE ELONGATED FASTENER HOLE. HOLE REPAIRED.

Part: GIRT BAR — DIRTY (L1 DOOR) · airframe 64,568 hrs · 24,149 cycles

ARMING LEVER BINDING WHEN TRYING TO CLOSE 1L. CLEANED AND REMOVED DEBRIS FROM GIRT BAR AREA, DOOR OPENS AND CLOSED NORMALLY. ACFT OK FOR SERVICE.

Part: UNKNOWN — DAMAGED (FUSELAGE) · airframe 64,424 hrs · 24,087 cycles

TWO SCRATCHES IN RVSM AREA ON RT SIDE. BUFFED OUT AND WAVINESS INSPECTION COMPLETED.

Part: COMPUTER — FAILED (COCKPIT) · airframe 64,272 hrs · 24,025 cycles

AVIONICS SMOKE ECAM, AEVC INSTALLED AND TESTED IAW AMM 21-26-34.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHT) · airframe 63,940 hrs · 23,894 cycles

EMERGENCY LIGHTING RT EPSU BATTERY FAULT. REPLACED RT EPSU IAW AMM 33- 51-38-000-002-A. OPS NORMAL.

Part: SEAL — DAMAGED (SLIDNG WINDOW) · airframe 63,485 hrs · 23,727 cycles

CAPTAIN`S SLIDING WINDOW LEAKED WATER INTO ACFT. REPAIRED SEAL IAW MT-56-003.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,476 hrs · 23,725 cycles

DAMAGED FUSELAGE SKIN BETWEEN FR 60 AND 61 S41-44R. REPAIRED PER ECRA 5341-01033.

Part: BLADE — BENT (NR 1 ENGINE FAN) · airframe 63,445 hrs · 23,711 cycles

NR 1 ENGINE FAN BLADE NR 22 HAS A BEND IN THE LEADING EDGE ABOUT 4.5 INCHES FROM TIP. REF AMM 72-31-11-0601, BLADE IS NOT WITHIN LIMITS. REPLACED NR 22 BLADE.

Part: ANTI-ICE VALVE — FAILED (LT WING) · airframe 63,330 hrs · 23,670 cycles

LEFT VALVE OPEN DISPLAYED ON UPPER ECAM SCREEN. REMOVED AND REPLACED LEFT WING ANTI- ICE VALVE, OPS CHECKED NORMAL.

Part: PCU — LEAKING (RUDDER) · airframe 63,101 hrs · 23,578 cycles

UPPER RUDDER PCU IS LEAKING. 60-90 DROPS PER MINUTE. REMOVED UPPER RUDDER PCU. INSTALLED RUDDER SERVO IAW MM 27-24-51-400-001-A. OPS CHECKED IAW 27-24-00-710- 001-A. OPS CHECKED OK, NO LEAKS NOTED

Part: LATCH — LACK OF LUBE (EMERGENCY EXIT) · airframe 63,049 hrs · 23,557 cycles

EMERGENCY EXIT LINE COVER FELL OFF ROW 20DEF. LUBED LATCH ON EMERGENCY EXIT LINE COVER. OPS CHECKED OKAY.

Part: DOOR — UNSECURE (O2 MASK) · airframe 63,008 hrs · 23,543 cycles

CREW REPORTED SEATS 20DEF, OXYGEN MASK DOOR FELL OPEN DURING TAXI. ACCOMPLISHED REPACK OF MASKS AND CONFIRMED GENERATOR DID NOT FIRE. MASK DOOR LATCHED NORMALLY. MANUAL MASK RELEASE OP CHECKS GOOD PER MM.

Part: STRUCTURE — EXPOSED (GALLEY) · airframe 62,670 hrs · 23,415 cycles

GALLEY 303 HAS BARE METAL EXPOSED. REMOVED THE SHARP EDGE AND COULD NOT BREAK THE MFG PART NUMBER TO PCN. INSTALLED SPEED TAPE. MFG PART NUMBER J1240A08GO1. REINSTALLED THE MISSING RIVET THEN RESEALED THE AREA. NO METAL EXPOSED AT THIS TIME. ALL WORK WAS PERFORMED BY SRM.

Part: BATTERY — FAULTY (CABIN) · airframe 62,582 hrs · 23,381 cycles

EMERGENCY LIGHT TEST SHOWS BATTERY FAULT FWD LEFT WILL NOT RESET. REPLACED EMERGENCY LIGHT BATTERY PER MM, OPS NORMAL.

Part: MANIFOLD — LEAKING (HYDRAULIC SYS) · airframe 62,276 hrs · 23,269 cycles

GREEN SYSTEM HYD LO LEVEVL MSG, FLIGHT DIVERTED. PER CREW MANUAL GEAR EXTENSION ACCOMPLISHED AFTER GREEN HYD LOSS. FOUND GREEN SYSTEM GROUND LEAK MEASUREMENT MANIFOLD LEAKING. REPLACED GREEN SYSTEM GROUND LEAK MEASUREMENT MANIFOLD. OPS CHECK NORMAL. NO LEAKS NOTED.

Part: ENGINE — LEAKING (NR 1) · airframe 62,232 hrs · 23,249 cycles

CONFIRMED INTERMITTENT OIL LEAK & LIGHT STREAKING AROUND ENGINE GEARBOX. CONFERRED WITH SFOLM. ENGINE CHANGE REQUIRED. NO ACTIVE LEAKS ALLOWED. REMOVED NR 1 ENGINE.

Part: CONE — CRACKED (NR 1 EXHAUST) · airframe 61,968 hrs · 23,149 cycles

NR 1 ENGINE EXHAUST CONE CRACKED 1.5 INCHES IN LENGTH ZONE-3 AT 9 O'CLOCK POSITION. REPLACED EXHAUST CONE.

Part: WINDSHIELD — DAMAGED (COCKPIT) · airframe 61,852 hrs · 23,097 cycles

CAPTAIN'S WINDSHIELD'S VISIBILITY IS IMPAIRED, NEED TO EVALUATE CONDITION. IF IMPAIRED WILL REQUIRE WINDSHIELD REPLACE. REPLACED 1L WINDSHIELD PER AMM.

Part: SPEAKER — FAILED (AFT GALLEY) · airframe 61,135 hrs · 22,858 cycles

COCKPIT TO AFT GALLEY COMM ALERT INOP. PA ALSO INOP AFT GALLEY. REPLACED AFT GALLEY LOUD SPEAKER, OPS CHECKED OK.

Part: ACTUATOR — LEAKING (NR 2 ENGINE) · airframe 60,018 hrs · 22,442 cycles

NR 2 ENG PH-LP ACTUATOR IS LEAKING FUEL FROM ACTUATOR. REPLACED ACTUATOR, LEAK CHECKED GOOD.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 59,994 hrs · 22,433 cycles

F/O'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). CREW COMMENTS: HARNESS CLIP IS BROKEN HARNESS NOT ATTACHED AT TOP LEFT TEMPLE. SWAP F/O MASK WITH 2ND OBSERVER MASK. COMPLY WITH MEL FOR 2ND OBS SEAT. SWAPPED F/O WITH 2ND OBSERVER MASK. 2ND OBS SEAT BLOCKED PER MEL. RPLC'D MASK ON 2ND OBSERVER WOULD NOT TEST AND REST, NEEDS O2 BOX. REPLACED MASK ASSEMBLY PER MM.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 59,702 hrs · 22,321 cycles

O2 MASKS DROPPED AT MID CABIN, CONTACT CREW FOR LOCATION. ACCOMPLISHED MT35-003 AND FOUND NO DISCREPANCIES WITH DOOR, LATCH OR O2 MASKS. REPACKED MASKS AND ACCOMPLISHED DROP CK AS REQUIRED. WILL NEED MANUAL DROP CHECK WITHIN A MAX OF 3 DAYS. O2 MASKS ARE LOCATED AT SEATS 20ABC. ACP MANUAL DROP CK OF 02 MASK. OPS CK GOOD.

Part: ROTARY ACTUATOR — FAILED (TE FLAP) · airframe 59,397 hrs · 22,218 cycles

FCTL FLAPS FAULT WITH FLP1 SYSTEM JAM CHECK FLP MECH DRIVE AND FLP2 SYSTEM JAM CHECK FLP MECH DRIVE FAILURE MESSAGES. REFERENCE TSM 27-51-00-810-810. RECORD PPU ANGLES PRIOR TO RESETTING ANY CB'S OR MOVING FLAP-SLAT HANDLE. REPLACED NR 2 LT FLAP ROTARY ACT PER AMM. OP CK'D OKAY AFTER REPLACEMENT.

Part: COVER — MISSING (R2 DOOR) · airframe 59,064 hrs · 22,085 cycles

DOOR 2R SLIDE COVER MISSING AND NO LIGHT ON. SECURED SLIDE BUSSEL TO DOOR 2R AND LIGHT TESTS NORMAL.

Part: LENS — MISSING (L2 DOOR) · airframe 59,040 hrs · 22,076 cycles

DOOR 2L SLIDE ARMED LIGHT LENS AT DOOR WINDOW MISSING FOUND AT PRE-DEPARTURE. REPLACED LENS AND ACCOMPLISHED OPERATIONAL TEST OF SLIDE ARMED LIGHT REF AMM AT DOOR 2L. OPS CHECKS OK.

Part: HOSE — CLOGGED (GASPER VENT) · airframe 57,571 hrs · 21,498 cycles

CREW REPORTS NO AIR FLOW AFT GALLEY GASPER VENT. REMOVED AIR SUPPLY HOSE FROM AFT GALLEY GASPER VENT EYEBALL. REMOVED MUCH DEBRIS FROM HOSE AND REPLACED EYEBALL VENT, AS IT WAS CLOGGED. REATTACHED CLEANED HOSE TO NEW GASPER EYEBALL VENT AND FOUND SUFFICIENT AIR FLOW.

Part: FILTER — DIRTY (CABIN) · airframe 57,083 hrs · 21,331 cycles

LGCIU 2 FAULT - ODOR IN COCKPIT, RTFL. REPLACED BOTH RECIRC FILTERS, POWERED A-C TURN ON ALL COMPUTERS IN COCKPIT, TURNED ON ALL LIGHTS IN CABIN, TURN GALLEY UNITS ON, NO ELECTRICAL ODOR THROUGH OUT ACFT.

Part: SCREW — LOOSE (RT WING) · airframe 56,919 hrs · 21,267 cycles

FUEL LEAKING FROM RT WING OUTBOARD FIXED FLAP TRACK PORTION AT A RATE OF 2 DROPS PER MINUTE. LOWERING FLAPS DRAINED APPROX 1 CUP OF FUEL. REMOVED FWD END OF CANOE. FOUND MULTI SCREWS LOOSE. SECURED, NO FURTHER LEAKAGE.

Part: CONTROL MODULE — FAILED (RAT) · airframe 56,469 hrs · 21,095 cycles

HYD RAT FAILS OPS TEST. REPLACED RAT GROUND CONTROL MODULE, NO HELP. REPLACED RAM AIR TURBINE. OPS ARE NORMAL.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 56,263 hrs · 21,005 cycles

DOOR 2R SLIDE PACK HAS FALLEN OUT OF POSITION. REPLACED SLIDE. VERIFIED ALL SAFETIES REMOVED, RII ACCOMPLISHED, CABLE ROUTING CORRECT AND TEST ACCOMPLISHED AND GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 55,903 hrs · 20,860 cycles

LIGHT LENS MISSING FROM RT OVERWING EMERGENCY LIGHT IN CABIN. REPLACED LIGHT LENS.

Part: LANYARD — MISROUTED (L1 DOOR SLIDE) · airframe 55,845 hrs · 20,836 cycles

DOOR 1L SLIDE LANYARD NOT ROUTED CORRECTLY. WHITE LANYARD ROUTED THROUGH GIRT TRIGGER. SECURED LANYARDS IAW MM.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 55,845 hrs · 20,836 cycles

EMERGENCY LIGHT TEST FAIL.*33-51-38 EPSU INT LOAD AFT L*. T-S IAW TSM. LIGHTS WORKED CORRECTLY. NEW POWER SUPPLY CORRECTED PROBLEM.

Part: LANYARD — MISROUTED (R2 DOOR SLIDE) · airframe 55,845 hrs · 20,836 cycles

DOOR 2R SLIDE LANYARD NOT ROUTED CORRECTLY. YELLOW LANYARD DOES NOT PASS THROUGH GIRT TRIGGER AND WHITE LANYARD NOT HOOK AND LOOPED TO GIRT TRIGGER. REROUTED LANYARDS IAW MM.

Part: OVEN — CONTAMINATED (FWD GALLEY) · airframe 55,512 hrs · 20,691 cycles

FWD GALLEY OVEN INOP. CREW REPORTED SMOKE COMING FROM THE FWD OVEN. CB'S WERE PULLED AND THE SMOKE DISSIPATED. PER FLT ATTENDANT SMOKE CAME FROM INSIDE THE OVEN. CB'S WERE PULLED AND THE SMOKE DISSIPATED. PER FLT ATTENDANT SMOKE CAME FROM INSIDE THE OVEN. FOUND CHARRED FOOD THAT HAS SPILLED ON THE SLIDE OUT TRAYS. REQUESTED NEW OVEN INSERT FOR OVEN. OVEN OPERATES NORMALLY.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 55,066 hrs · 20,489 cycles

CABIN PRESS SYS FAULT, FLIGHT DIVERTED. ACFT ALSO EXPERIENCED CPC1 FAULT. CREW STATED THAT MANUAL MODE WOULD NOT HOLD PRESSURIZATION, SO THEY DECENDED TO 10,000 FT. TROUBLESHOOT REF MT21-013, PARA 2 "ACFT UNABLE TO MAINTAIN CABIN PRESSURE". REPLACED OUTFLOW VALVE IAW MM AND REPLACED BOTH CABIN PRESSURE CONTROLLERS IAW MM. ACCOMPLISHED PRESSURE CHECK IAW MM. ACFT HELD PRESSURE, NO DEFECTS NOTED. ALL TESTS PASSED WITH NO FAULTS. PRESSURIZED CABIN AND CABIN MAINTAINS PRESSURE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 55,057 hrs · 20,484 cycles

AFT CARGO COMPARTMENT BILGE AT STRINGER 42L BETWEEN FRAMES 56 & 57 CORRODED. MAJOR REPAIR ACCOMPLISHED: CUT OUT CORRODED SECTION OF STRINGER. FABRICATED & INSTALLED STRINGER SPLICE REPAIR COMPRISED OF NEW STRINGER SECTION & 2 SPLICE FITTINGS AT MID FRAME 55 & MID FRAME 56.

Part: LANYARD — MISROUTED (DOOR 1L) · airframe 53,183 hrs · 19,739 cycles

DOOR 1L SURVIVAL KIT LANYARD LOOP NOT VISIBLE. FOUND SURVIVAL KIT LANYARD LOOP MISROUTED. INSTALLED LANYARD LOOP. VERIFIED LANYARD AND LOOP ROUTED PER AMM.

Part: LANYARD — MISROUTED (DOOR 2R) · airframe 53,183 hrs · 19,739 cycles

DOOR 2R SURVIVAL KIT LANYARD LOOP NOT VISIBLE. SUPPLEMENTAL DATA UPDATE FOUND DOOR 2R SURVIVAL KIT LANYARD LOOP MISROUTED. INSTALLED SURVIVAL KIT LANYARD LOOP. VERIFIED LANYARD AND LOOP ROUTED.

Part: LANYARD — MISROUTED (DOOR 2L) · airframe 53,183 hrs · 19,739 cycles

DOOR 2L SURVIVAL KIT LANYARD LOOP NOT VISIBLE. SUPPLEMENTAL DATA UPDATE FOUND DOOR 2L SURVIVAL KIT LANYARD LOOP MISROUTED. INSTALLED LANYARD LOOP. VERIFIED LANYARD AND LOOP ROUTED PER AMM.

Part: LANYARD — MISROUTED (R1 DOOR SLIDE) · airframe 53,183 hrs · 19,739 cycles

NO SLIDE PACK LANYARD VISIBLE DOOR 1R. SUPPLEMENTAL DATA UPDATE FOUND DOOR 1R SLIDE SURVIVAL KIT LANYARD LOOP MISROUTED. INSTALLED SURVIVAL KIT LANYARD LOOP. VERIFIED LANYARD AND LOOP ROUTED PER AMM.

Part: CONTROL VALVE — FAULTY (RT ACM) · airframe 53,111 hrs · 19,710 cycles

PACK FAILURE ON TAXI OUT, FLT DIVERTED. REPLACED THE RIGHT PACK FLOW CONTROL VALVE AND RIGHT PACK CONTROLLER IAW MM. ALL CHECKS GOOD.

Part: ENGINE — STALLED (APU) · airframe 52,822 hrs · 19,586 cycles

APU FAILED DURING ENG START. ABRUPT SHUTDOWN. LOUD COMP STALLS WITH FLAMES SHOOTING OUT TAIL. INSPECTED APU EXHAUST NO DAMAGE FOUND. APU INOPERATIVE. NO ECAM MESSAGES OR WARNING NOTED. OPERATED APU NUMEROUS TIMES LOADED UP, MOTORED ENGINES, PACKS, ELEC. NO DEFECTS NOTED. RAN SELF TEST, TEST PASS.

Part: BRACKET — OUT OF POSITION (AFT FIRE EXTINGU) · airframe 52,763 hrs · 19,557 cycles

AFT FIRE EXT NEEDS TO BE REMOUNTED IN BRACKET. REPLACED BRACKET.

Part: CONNECTOR — LOOSE (CABIN) · airframe 51,211 hrs · 18,844 cycles

SEAT 11 EMERGENCY LIGHT INOP. SECURED CONNECTOR TO EMERGENCY LIGHT. OPS CHECK'S GOOD.

Part: PROXIMITY SENSOR — MALFUNCTIONED (MLG) · airframe 51,136 hrs · 18,809 cycles

LANDING GEAR WOULD NOT RETRACT. RTFL. CFDS SHOWS "323173 R L-G PROX SNSR TGT POS" REPLACED MLG PROX SENSOR 22GA. SWING GEAR TO VERIFY FIX. REPLACED NR 2 LGCIU AND PROX SENSOR 22GA. CHECKS GOOD WITH GEAR SWING.

Part: O-RING — LEAKING (EVAC SLIDE)

LOW PRESSURE. THERE WAS A SLOW LEAK AT THE VALVE BALL SHAFT O-RING. REMOVED & REPLACED O-RING AND BACK-UP O-RING.

Part: RECTIFIER — UNRELIABLE (NR 2) · airframe 50,853 hrs · 18,678 cycles

TR 2 FAULT ECAM. RTFL, TROUBLESHOOTING BUT UNABLE TO DUPLICATE. REPLACED TRANSFORMER RECTIFIER.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 50,821 hrs · 18,665 cycles

AIRCRAFT FAILS EMERGENCY LIGHT TEST 'UNIT EMER L' FAULT. REPLACED POWER SUPPLY, NOW HAVE INTERNAL AND EXTERNAL LOAD EMER L FAULT, RELAMPED BOTH LEFT OW EXT LIGHTS, STILL FAULTS. SUSPECT OW SLIDE. FOUND SEAT 15, 16 AND 17 EEL LIGHTS DIM. NEEDS MORE T/S TO FIND SHORT. REPLACED ROW 16 LIGHT ASSY, SECURED WIRE HARNESS, & RESET POWER SUPPLY. EMERGENCY LIGHT TEST PASSED, NO FAULTS.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 48,839 hrs · 17,889 cycles

LAV F SMOKE DETECTOR INOP. FOUND FAULTY SMOKE DETECTOR. REPLACED SMOKE DETECTOR, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (ROW 20C) · airframe 48,757 hrs · 17,868 cycles

EMERGENCY ESCAPE LIGHT INOP AT 20C.

Part: SERVO VALVE — FAULTY (RT ELEVATOR) · airframe 47,787 hrs · 17,511 cycles

DURING A CHECK, RIGHT ELEVATOR WILL NOT PASS FLIGHT TEST. 34CE1 SERVO FAULTY. REPLACED ELEV SERVO CONTROL, INBD GREEN (34CE1), OPS CHECKED OK.

Part: BATTERY — FAILED (CABIN) · airframe 46,898 hrs · 17,186 cycles

RIGHT OVERWING EMERGENCY BATTERY FAILS TEST.

Part: BATTERY — FAILED (CABIN) · airframe 46,898 hrs · 17,186 cycles

RIGHT OW EMERGENCY BATTERY FAILS TEST. BATTERY FAILURE. REPLACED BATTERY, OPS CHECKED GOOD.

Part: SLIDE — FAULTY (L1 DOOR) · airframe 46,802 hrs · 17,158 cycles

EMERGENCY LIGHT AT DOOR 1L IS INOP. INTERNAL ELECTRICAL FAULT (SLIDE 1L). REPLACED DOOR SLIDE 1L, OPS CHECKED NORMAL.

Part: STRUCTURE — DAMAGED (NR 2 SLAT) · airframe 46,319 hrs · 16,979 cycles

LEFT WING L/E SLAT OUTBOARD OF NR 1 ENGINE DAMAGED. REPLACED NR 2 LE SLAT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,693 hrs · 16,745 cycles

EMERGENCY LIGHT TEST FAILED. MESSAGE: EPSU BATTERY EMER L. FOUND EPSU BATTERY FAILURE. REPLACED BATTERY.

Part: BATTERY — FAILED (CABIN) · airframe 45,191 hrs · 16,541 cycles

EMERGENCY LIGHTS FAIL TEST PER 3 SVC. SHOWS BATTERY FWD LEFT. REPLACED FWD LEFT BATTERY.

Part: HYDRAULIC SYSTEM — FAILED (BLUE SYSTEM) · airframe 45,165 hrs · 16,532 cycles

RTFL WITH BLUE SYSTEM HYDRAULICS FAILURE. FLT HAD IDENTICAL PROBLEM ON PREVIOUS LEG.

Part: BULB — MISSING (EMERGENCY LIGHT) · airframe 44,524 hrs · 16,293 cycles

SEAT 22 EMERGENCY LIGHT MISSING FWD BULB SOCKET. [SUP 5-1-07] REPLACED LIGHT ASSY. OPS CHECKS GOOD.

Part: WARNING SYSTEM — ACTIVATED (HYDRAULIC SYS) · airframe 44,335 hrs · 16,219 cycles

AFTER TAKEOFF RECEIVED ECAM FOR GREEN HYDRAULIC LOW LEVEL. AMBER ALERT AND EMERGENCY DECLARED WITH ATC WITH EMERGENCY EQUIPMENT MEETING FLIGHT AT PLANNED DESTINATION. [SUP 06-01-07] A HYDRAULIC PRESSURE LINE IN THE UPPER FORWARD LT PYLON WORN THROUGH FROM CONTACT WITH ADJACENT HYDRAULIC RETURN LINE. MANUFACTURED AND INSTALLED NEW PRESSURE AND RETURN LINES WITH PROPER CLEARANCE.

Part: FLUID — LEAKING (HYDRAULIC SYS) · airframe 43,701 hrs · 15,982 cycles

RTFL WITH GREEN SYSTEM HYD LOSS.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 42,889 hrs · 15,663 cycles

FOUND BATTERY FAULT ON FWD LT ESPU. REMOVED AND REPLACED BATTERY PACK FOR FWD LEFT EPSU. RETEST OK.

Part: LANYARD — OUT OF POSITION (L1 DOOR SLIDE) · airframe 42,848 hrs · 15,648 cycles

FOUND LANYARD HANGING OUT OF DOOR 1L AFTER CLOSING. STOWED LANYARD ON SLIDE.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 42,449 hrs · 15,499 cycles

FWD AND AFT EMERGENCY POWER SUPPLY BATTERIES FAILED 3SVC LIGHT TEST. REPLACED FORWARD AND AFT EMERGENCY POWER SUPPLY BATTERIES. OPS CHECKS GOOD.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 41,613 hrs · 15,161 cycles

DOOR 1L WAS PARTIALLY OPENED AND SLIDE PACK FELL OUT BUT DID NOT DEPLOY. SERVICED DOOR 1 LEFT ASSIST BOTTLE AND REPLACED DIAPHRAGM. REPLACED DOOR 1L SLIDE/RAFT ASSEMBLY.

Part: ENGINE — SURGES (NR 1) · airframe 39,804 hrs · 14,374 cycles

RETURNED TO FIELD AFTER THE NR 1 ENGINE SURGED. ECM SHOWS NO RECORD OF A SURGE/STALL. EEC/FADEC RECORDED NO STALL MESSAGE. FMU WAS REPLACED FOR N1 OVER SPEED AND CHANNEL B FAULT. FMU TEST SHOWS NO FAULT FOUND. CAUSE OF SURGE CAN NOT BE DETERMINED.

Part: LIGHT — MALFUNCTIONED (DOOR LEFT AFT) · airframe 39,630 hrs · 14,287 cycles

LEFT AFT EMERGENCY EXIT DISPLAYED ON UPPER ECAM SCREEN, DOOR. REPLACED EMERGENCY BATTERY AT LEFT OVERWING POSITION AND LEFT AFT POSITION.

Part: LIGHT — MALFUNCTIONED (DOOR LEFT FWD) · airframe 39,630 hrs · 14,287 cycles

LEFT FWD EMERGENCY EXIT DISPLAYED ON UPPER ECAM SCREEN, DOOR. REPLACED FWD EMER BATTERY.

Part: SENSOR — MALFUNCTIONED (MLG) · airframe 38,522 hrs · 13,905 cycles

NR 2 ENGINE REVERSER FAULT EMAC MESSAGE. ENG 2 REV ECAM MESSAGE AIRCRAFT RETURNED TO FIELD. REVERSER FAULT DUE TO LGCIU DUE TO CHRONIC ECAM ENG 2 REV FAULT IN FLIGHT THAT OCCURS AT THE SAME TIME AS A LGCIU2 FAULT. LANDING GEAR SENSOR 23GA REPLACED PER AMM 32-31-73 PG 401.

Part: WARNING LIGHT — ILLUMINATED (HYD SYSTEM) · airframe 34,852 hrs · 12,696 cycles

FLIGHT DIVERTED DUE TO HYDRAULIC (G RSVR LO LVL) ECAM MESSAGE. LOW LEVEL SWITCH FAILED. REPLACED THE LOW LEVEL SWITCH ON THE GREEN HYDRAULIC SYSTEM . OPERATIONS CHECK NORMAL.

Part: FIRE LOOP — MALFUNCTIONED (NR 2 ENGINE) · airframe 29,541 hrs · 10,742 cycles

NUMBER 2 ENGINE FIRE WARNING LIGHT ILLUMINATED DURING DESCENT WITH NO SECONDARY INDICATIONS. THE FIRE DETECTION UNIT WAS CHANGED.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 24,270 hrs · 8,737 cycles

CABIN PRESSURE SYSTEMS 1 AND 2 FAILED IN FLIGHT. *S/D* CABIN PRESSURE CONTROLLERS NR 1 AND NR 2 WERE BOTH REPLACED. THERE HAVE BEEN NO CABIN PRESSURE ANOMALIES SINCE THE REPAIR WAS ACCOMPLISHED.

Part: LIGHT — WILL NOT TEST (CABIN) · airframe 20,407 hrs

EMERGENCY LIGHT TEST FAILED PER A CHECK. *S/D* REPLACED BATTERY POWER SUPPLY PER MM 33-51-38. OPS CHECK NORMAL. CABIN EMERGENCY LIGHTING CHECK PASSED TEST PER ''A'' CHECK PAPERWORK.

Part: PFD — MALFUNCTIONED (RT COCKPIT)

ON APPROACH, F/O PFD AND ND SWAPPING POSITION AFTER TAKEOFF, INTERMITTANTLY DURING FLIGHT.

Part: SEAT — CRACKED (PASSENGER CABIN)

DURING THE FIRST HEAVY MAINTENANCE VISIT (HMV-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 THE AIRBUS A-320-232 AIRCRAFT. THE SEAT MANUFACTURER DESIGNATES THE SEAT PAN AS PRIMARY STRUCTURE FOR THE SEAT. THIS IS THE 7TH CONSECUTIVE A-320-232 TO SHOW A 100 PERCENT FAILURE RATE OF THESE SEAT PANS.

Part: SLIDE — DETACHED (PASSENGER DOOR)

AFT RT ENTRY DOOR ESCAPE RAFT DISMOUNTED AT UPPER END. *S/D* UPPER SPRINGS OF SLIDE PACK DISMOUNTED FROM UPPER STUDS OF DOOR. SLIDE WAS REPLACED PER MM 40-25-62-44.