N935FR

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 36,682 hrs · 18,200 cycles

FLAP JAM AT SLAT ONLY, FLAPS LOCKED. PERFORMED BITE TEST OF SFCC IAW AMM 27-51-00-740-002-A. PERFORMED 2 FULL FLAPS & SLATS CYCLES, NO DEFECTS NOTED. PERFORMED VISUAL INSPECTION OF THE FLAPS & SLATS, NO DEFECTS NOTED LP 893710.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,053 hrs · 17,915 cycles

LEFT EPSU BATTERY FAILS TEST. REPLACED LT EPSU IAW AMM 33-51-38 PB 401. OPERATIONS CHECKED NORMAL. LOG PAGE 843284.

Part: BATTERY — DISCHARGED (CABIN) · airframe 34,332 hrs · 17,028 cycles

EPSU BATTERY 12WL FAILED THE TEST ON THE HEAVY SERVICE CHECK. R & R EPSU BATTERY 12WL IAW AMM 33-51-38-000-002-A & 33-51-38-400-002 A.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 32,402 hrs · 16,029 cycles

EMERGENCY LIGHT FAULT EPSU AFT LT & NO GREEN SYS OK LIGHT UPON TESTING. R & R AFT LT EPSU BATTERY IAW AMM 33-51-38 PB 401, OPERATIONS CHECKED GOOD.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 32,077 hrs · 15,866 cycles

AIRCRAFT OUT OF SERVICE DUE TO C6 CHECK. EMERGENCY LIGHTING WIRING AT SEAT ROW 25L IS BROKEN. R & R EMERGENCY LIGHTING WIRING HARNESS IAW AMM 33-51-19. OPERATIONS CHECKED GOOD IAW AMM 33-51-00-710-001-A AT SEAT ROW 25L.

Part: DOOR — OPEN (FWD CARGO) · airframe 23,966 hrs · 11,681 cycles

LP 540215: AIR TURN BACK, FWD CARGO DOOR OPEN AFTER TAKEOFF "OVERWEIGHT LANDING". PLACED THE CARGO DOOR ON MEL 52-70-01H MDDR 1083274 AND PERFORMED INSPECTION RTS 1715 MCI LOCAL TIME.

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 22,744 hrs · 11,116 cycles

A/C REPORT LP NR605872: GREEN HYD SYS RESERVOIR LOW QUANTITY. GRAVITY EXTENSION OF LANDING GEAR APPARENT FLUID LEAKING FROM NR 1 ENGINE. UPON FURTHER INSP FOUND HYD LOW PRESSURE SWITCH TUBE LEAKING. REMOVED IN REF WITH AMM 29-11-49-000-005 AND INSTALLED HYD LOW PRESSURE SWITCH TUBE ON NR1 ENGINE IN REF WITH AMM 29-11-49-400-005, NO LEAKS NOTED. TORQUE WRENCH S/N F9TAB0991C NEXT DUE 01/12 REF FREE FALL ON LP 605731, ITEM 2.

Part: PLATE — CORRODED (ZONE 100) · airframe 21,487 hrs · 10,503 cycles

C-CHECK: NON ROUTINE 0414, AFT CARGO DOORS SILL SHEET HAS 4 AREAS OF CORROSION MEASURING 4.5 SQUARE INCHES TOTAL. REMOVED CORROSION IAW A319 SRM 51-74-00 PARA 5.A (3). ALL AREAS WITHIN LIMITS IAW A319 SRM 51-73-11 PARA 1. B RE-PROTECTED AREAS IAW A319 SRM 51-21-11 PARA 2.B AND SRM 51-75-12 PARA 4.

Part: EPSU — INOPERATIVE (CABIN) · airframe 21,487 hrs · 10,503 cycles

C-CHECK NON ROUTINE N0769, L-1 AND R-1 LOWER DOOR INTERIOR EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED EPSU ON (10WL) AND TEST GOOD IAW A319 AMM 33-51-38-PB 401.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 21,487 hrs · 10,503 cycles

C-CHECK: NON ROUTINE N0383, CABIN FLOOR PANEL 252SF DISBONDED. REPAIRED DISBONDED SKIN AREA ON THE FLOOR PANEL 252SF USING FILLER METHOD. REPAIRED DISBONDED IAW A319 SRM 53-02-00 PARA 8. A, (2) FIG. 204.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 21,487 hrs · 10,503 cycles

C-CHECK: NON ROUTINE N0384, CABIN FLOOR PANEL 251AF DISBONDED. REPAIRED DISBOND ON FLOOR PANEL 251AF IAW A319 SRM 53-02-00 PARA 8. A, (2) FIG. 204.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 21,487 hrs · 10,503 cycles

C-CHECK: NON ROUTINE N0494, AFT CABIN SEAT TRACK Y1292 AT FRAME 68L HAS 2 AREAS OF CORROSION UPPER SURFACE. CORROTIONS OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 102. REMOVED AND REPLACED SEAT TRACK Y1292 BETWEEN FRAMES 68L AND 69L.

Part: PANEL — PUNCTURED (ZONE 100) · airframe 21,487 hrs · 10,503 cycles

C-CHECK: NON ROUTINE AFT CARGO TRANSITION PANEL 151AE HAS 6 PUNCTURES. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 PARA 13 REVISION G.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 21,487 hrs · 10,503 cycles

C-CHECK NON ROUTINE N0479, 6 EACH INSERTS PULLED OUT WITH SKIN DAMAGE. REPAIRED THE SKIN DAMAGE AT 6 EACH HOLE LOCATIONS USING PATCH METHOD IAW A319 SRM 53-02-00 PARA 8 A. INSTALLED INSERTS IAW AIRBUS PMS 01-05-72 PARA 5.

Part: BATTERY — DISCHARGED (MEGAPHONE) · airframe 214,587 hrs · 10,503 cycles

C-CHECK: NON ROUTINE N0074, FWD MEGAPHONE INOPERATIVE. REPLACED BATTERIES IN THE MEGAPHONE IAW A319 AMM 25-65-51-920-001. MEGAPHONE STILL INOPERATIVE, REMOVED AND REPLACED MEGAPHONE IAW A319 AMM 25-65-920-001 AND AMM 25-64-51-010-050 PARA. B (3) AND AMM 25-64-51-050 PARA. A (1).

Part: FLOOR PANEL — PUNCTURED (ZONE 100) · airframe 21,487 hrs · 10,503 cycles

C-CHECK NON ROUTINE N0479, AFT CARGO FLOOR PANEL 151PE HAS A 2 EACH PUCTURES. REPAIR USING GLASS CLOH WET LAYUP IAW A319 SRN 53-00 PARA 8 B.

Part: SUPPORT — CORRODED (ZONE 200) · airframe 21,487 hrs · 10,503 cycles

C-CHECK NON ROUTINE N0413, FRAME SUPPORT FROM 69 TO 70 STRINGER 23R BELOW SHEAR PLATE HAS 2 AREAS OF CORROSION TOTALING 2 SQUARE INCHES. REMOVED AND REPLACED FRAMES SUPPORT IAW A319 SRM 51-42-11 PARA 6 AND 7.

Part: PANEL — PUNCTURED (ZONE 100) · airframe 21,487 hrs · 10,503 cycles

C-CHECK NON ROUTINE N0473, AFT CARGO FLOOR PANEL 151VG HAS 7 PUNCTURES. FABRICATED AND REPLACEMENT PANEL IAW MCG IRM 9701 REV G.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 21,487 hrs · 10,503 cycles

C-CHECK NON ROUTINE N0649, AFT CARGO FLOOR PANEL 151FE HAS COMPOSITE DAMAGE ON BOTH SIDES. REPAIRED COMPOSITE DAMAGE IAW A319 SRM 53-02-00 PARA 5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,487 hrs · 10,503 cycles

C-CHECK: NON ROUTINE N0410, AFT MAIN CABIN FLOORBEAM Y1292 AT FRAME 68R HAS 2 AREAS OF CORROSION. REMOVED AND REPLACED FLOORBEAM - Y1292 FROM FRAME 68R TO FRAME 69R IAW A319 SRM 51-42-11 PARA 7.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 21,487 hrs · 10,503 cycles

C-CHECK NON ROUTINE N0507, AFT CARGO FLOOR PANEL 151UG HAS 2 PUNCTURES AND 4 EACH DAMAGED PREVIOUS REPAIRS. FABRICATED AND REPLACED PANEL IAW MCG IRM 9701 REV G.

Part: CONTROL UNIT — DEFECTIVE (ZONE 200) · airframe 17,387 hrs · 8,587 cycles

CREW MADE AN AIR RETURN, DUE TO THE ALTITUDE SELECTOR KNOB ON THE FLIGHT CONTROL UNIT BEING STUCK ON AN ALTITUDE, RENDERING THE AUTO-PILOT, AUTO-THRUST AND FLIGHT DIRECTORS TO AN UNAVAILABLE STATE. MX REMOVED AND REPLACED THE FLIGHT CONTROL UNIT AND PERFORMED OPS TEST, BITE TEST AND CAT III LAND TEST IAW AMM 22-81-12 PB401, 22-96-00-710-001 AND 22-97-00-710-001.

Part: SILL — CORRODED (ZONE 200) · airframe 15,658 hrs · 7,684 cycles

DURING C3 C-CHECK, INSPECTION NOTED THE L2 DOOR SILL BEAM HAS TWO CORRODED NUT PLATE HOLES AT FRAME 68. MAINTENANCE TRIMMED OUT DAMAGED AREA, FABRICATED REPAIR ANGLE AND INSTALLED IAW SRM 53-41-14 FIGURE 201.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,658 hrs · 7,684 cycles

DURING C3 C-CHECK, INSPECTION NOTED THE LEFT AFT GALLEY FLOORBEAM Y1292 HAS CORROSION AROUND FASTENER HOLES BETWEEN FRAME 67 AND FRAME 68. MAINTENANCE REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11, PARAGRAPHS 5 AND 7.

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 15,658 hrs · 7,684 cycles

DURING C3 C-CHECK, INSPECTION NOTED FLOOR PANEL 262FF HAS CORROSION. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL PER TASK CARD C534103-2.

Part: SILL — CORRODED (ZONE 200) · airframe 15,658 hrs · 7,684 cycles

DURING C3 C-CHECK, INSPECTION NOTED THE LEFT GALLEY FLOOR STRUCTURE AT FRAME 66 HAS TWO NUT PLATE HOLES CORRODED AFT OF GIRT BAR FITTING ADAPTER PLATE. MAINTENANCE TRIMMED OUT DAMAGED AREA, FABRICATED REPAIR ANGLE AND FILLER AND INSTALLED IN REFERENCE TO ENGINEERING AUTHORIZATION A9-53R-30909.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 11,882 hrs · 5,850 cycles

REFERENCE LOG PAGES 369125 AND 369126. DURING FLIGHT THE FA REPORTED A STRONG ODOR AND HEAT. MAINT RAN APU AND ENGINE (1) AND (2) AT IDLE WITH BOTH PACKS ON. MAINT VISUALLY INSPECTED CARGO PITS, FWD AVIONICS COMPARTMENTS AND FUSELAGE, AFT OF PRESSURE BULKHEAD NO UNUSUAL ODERS NOTED. MAINT INSPECTED CABIN AND FOUND AND UNUSUAL ODOR COMING FROM AFT COFFEE MAKERS WHILE BREWING. PLACED NR (2) AFT COFFEE MAKER ON NEF 25-99-30AD. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLAP SYSTEM — OUT OF ALIGNMENT (TE FLAPS) · airframe 11,631 hrs · 5,652 cycles

DURING THE APPROACH, THE FLIGHT CREW RECEIVED AN ECAM MESSAGE THAT THE FLIGHT CONTROLS - FLAPS - WERE LOCKED DUE TO AN ALIGNMENT FAULT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE RESET THE WING TIP BREAK IN ACCORDANCE WITH AMM 27-50-00-869-006 AND PERFORMED EXTENSION AND RETRACTION TESTS IN ACCORDANCE WITH AMM 27-50-00-866-008. MAINTENANCE ALSO PERFORMED BITE TEST OF SFCC 1 AND 2 IN ACCORDANCE WITH AMM 27-51-00-740-002 AND NO FAULTS WERE FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT BEAM — CORRODED (FUSELAGE) · airframe 10,119 hrs · 4,945 cycles

DURING C-2 CHECK, INSPECTION REPORTED FR C-20 TOP SUPPORT BEAM IN LT FWD ELECTRICAL EQUIPMENT COMPARTMENT FRETTING. FOUND FITTING TO BE OUT OF LIMITS IAW AIRBUS DRAWING D53113988. PERFORMED HFEC OF FR C-20 INBD SUPPORT BEAM LUG ON NLG WHEEL WELL UPPER AFT LT CORNER IAW NTM 51-10-08, PART 6. NO CRACKS FOUND ON LUG. OVERSIZED SLOT AND FABRICATED BUSHING IAW EA A9-53R-12068. INSTALLED NEW BUSHING IAW A319 SRM 51-42-11, P6, AND EA A9-53R-12068.

Part: CONTROL SYSTEM — FAILED (EMERGENCY EXIT) · airframe 4,740 hrs · 2,274 cycles

DURING C-1 CHECK, MAINTENANCE REPORTED RT OVERWING EMERGENCY EXIT FAILED FUNCTION TEST (PER WORK CARD C522101-3, EMERGENCY ESCAPE SYSTEM FAILURE). ADJUSTED RT OVERWING EMERGENCY EXIT FLEXIBLE CONTROL ASSY IAW AMM 25-62-43-820-050. PERFORMED OPERATIONAL CHECK AND WAS IN SERVICEABLE LIMITS.