N903FR

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 19,612 hrs · 8,597 cycles

MAINTENANCE REPORTED EPSU AFT L FAULTED. CLEANED AND INSPECTED PINS ON CONNECTOR TO EPSU AFT L POWER SUPPLY. PERFORMED EMERGENCY LIGHT TEST PER AMM 23-73-00-861-001 AND 33-51-38. OPS TEST GOOD.

Part: ODOR — DETECTED (CABIN) · airframe 17,403 hrs · 7,662 cycles

BLOCK TURNBACK IN CUN. FLIGHT ATTENDANTS REPORTED SMELL OF SMOKE IN FWD PASSENGER CABIN AREA (APPROXIMATELY ROW 6 AND FWD). MAINTENANCE PERFORMED INSPECTION OF AIRCRAFT MM 24-00-00-810-823. NO SMOKE ODOR OR DISCREPANCIES WERE FOUND. AIRCRAFT WAS RELEASED FOR SERVICE AND COMPLETED FLIGHT WITH NO INCIDENTS.

Part: EPSU — FAILED (CABIN) · airframe 17,309 hrs · 7,621 cycles

DURING C-4 CHECK, INSPECTION REPORTED FWD EMERGENCY POWER SUPPLY UNIT (EPSU) FAILED EMERGENCY LIGHTS CAPACITY TEST. REPLACED EPSU 10WL. OPS CHECK NORMAL PER AMM 33-51-38, PB 401.

Part: BATTERY PACK — FAILED (CABIN) · airframe 17,309 hrs · 7,621 cycles

DURING C-4 CHECK, INSPECTION REPORTED LT. MID CABIN EPSU 12WL FAILED CAPACITY TEST. REPLACED BATTERY PACK 12WL. OPS CHECK NORMAL IAW AMM 33-51-38, PB 401.

Part: EPSU — FAILED (CABIN) · airframe 17,309 hrs · 7,621 cycles

DURING C-4 CHECK, INSPECTION REPORTED MID CABIN EPSU FAILED CAPACITY TEST. REPLACED 11WL MID CABIN EPSU. OPS CHECK GOOD IAW AMM 33-51-38, PB401.

Part: SLAT TRACK — DAMAGED (NR 1 SLAT) · airframe 17,309 hrs · 7,621 cycles

DURING C-4 CHECK, INSPECTION REPORTED LT WING, NR 1 SLAT I/B SLAT TRACK CUTOUT DAMAGED. REMOVED DAMAGED AREAS AND PERFORMED HFEC INSPECTION. NO FAULTS OR CRACKS NOTED. APPLIED ALODINE TREATMENT EPOXY PRIMER AND PAINT TO AFFECTED AREAS. REFERENCE A319 SRM 51-23-11, 51-21-11 AND EA A9-57R-11539.

Part: VALVE — CORRODED (CABIN PRESSURE) · airframe 17,309 hrs · 7,621 cycles

LEFT HAND CABIN PRESSURE SAFETY VALVE (7HL) POSITION SWITCH STICKS AND IS CORRODED. NEW VALVE WAS INSTALLED PER AMM 21-31-52-400-001. BONDING CHECK PERFORMED ON BONDING STRAP PER AMM 20-28-00-912-004. CHECK WAS GOOD.

Part: THRESHOLD — CORRODED (L1 DOOR) · corrosion level 2 · airframe 17,309 hrs · 7,621 cycles

DURING C-4 CHECK, INSPECTION REPORTED MINOR CORROSION ON L1 DOOR THRESHOLD STRIP. FOUND L1 DOOR THRESHOLD STRIP TO BE OUT OF LIMITS PER SRM 51-70-00. FABRICATED AND INSTALLED REPLACEMENT L1 DOOR SILL COVER PER AIRBUS DWG B5 D53610197, SRM 51-27-00, SRM 51-44-11 AND SRM 51-21-11.

Part: THRESHOLD — CORRODED (R1 DOORWAY) · corrosion level 2 · airframe 17,309 hrs · 7,621 cycles

DURING C-4 CHECK, INSPECTION REPORTED MINOR CORROSION ON R1 DOOR THRESHOLD STRIP. FOUND R1 DOOR THRESHOLD STRIP TO BE OUT OF LIMITS PER SRM 51-70-00. FABRICATED AND INSTALLED REPLACEMENT R1 DOOR SILL COVER PER AIRBUS DWG B5 D53610197, SRM 51-27-00, SRM 51-44-11 AND SRM 51-21-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 17,309 hrs · 7,621 cycles

FLOORBEAM FROM 68-69 LT SIDE, JUST INSIDE L-2 DOOR WAS CORRODED. NEW FLOORBEAM AND SPLICE ANGLE INSTALLED PER A319 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,309 hrs · 7,621 cycles

DURING C-4 CHECK, INSPECTION REPORTED LT SIDE FLOOR SUPPORT STRINGER NUT CLIPS AND NUT PLATES FOR ATTACHMENT OF FLOOR AND TRANS PANELS IN FWD CARGO COMPARTMENT CORRODED. REMOVED LT SIDE FLOOR SUPPORT STRINGER (TRANSITION PLATE) BETWEEN FR28 AND FR30 PER A319 SRM 51-42-11. LOCATED AND DRILLED NEW PART PER A319 SRM 51-44-21 AND INSTALLED NEW LT SIDE FLOOR SUPPORT STRINGER (TRANSITION PLATE) BETWEEN FR28 AND FR30 PER A319 SRM 51-42-11.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,309 hrs · 7,621 cycles

DURING C-4 CHECK, INSPECTION REPORTED CORROSION IN FWD LAV AREA, FR16 AND Y503.2. DUMMY RAIL WAS FOUND TO BE OUT OF LIMITS PER SRM 53-11-14. REMOVED CORRODED DUMMY RAIL PER SRM 51-42-11. LOCATED AND DRILLED NEW DUMMY RAIL PER SRM 51-44-11 AND AIRBUS DWG B2 D53110984. INSTALLED NEW DUMMY RAIL PER SRM 51-42-11 AND AIRBUS DWG B2 D53110984.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,309 hrs · 7,621 cycles

DURING C-4 CHECK, INSPECTION REPORTED AFT FUSELAGE CABIN FLOOR STRUCTURE FR66, Y1292, CORRODED UNDER NUT CLIPS. BURNISHED CORROSION ON SEAT TRACK/STRUCTURE AT FR66 PER SRM 53-00-15, FIG 101, SECTION E-E, PAGES 101-104. UPON FURTHER INVESTIGATION, MORE CORROSION WAS FOUND. REMOVED FLOOR SUPPORT FROM FRAME C64-C70 PER SRM 51-42-11. INSTALLED SERVICEABLE FLOOR/SEAT TRACK PER SRM 51-42-11 AND A319 DWG D53472815.

Part: BEAM — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 17,309 hrs · 7,621 cycles

DURING C-4 CHECK, INSPECTION REPORTED CORROSION AND HOLE THROUGH Y254 BEAM AT FR20 FWD ENTRY CENTER. FOUND CORRODED AREA TO BE OUT OF LIMITS PER SRM 53-11-14, FIG 104. CUT OUT AND REMOVED CORRODED SECTION FROM TOP FLANGE OF FLOOR SUPPORT PER SRM 53-11-14, FIG 201. FABRICATED REPAIR DOUBLERS AND FILLER PER SRM 53-11-14, FIG 201. TREATED, PRIMED AND PAINTED REPAIR PARTS PER SRM 51-23-00. INSTALLED REPAIR PARTS PER SRM 53-11-14, FIG 201.

Part: SWITCH — CORRODED (VALVE) · airframe 17,309 hrs · 7,621 cycles

RIGHT HAND CABIN PRESSURE SAFETY VALVE (GHL) FAILED OPERATION TEST. POSITION SWITCH WAS CORRODED. NO OPEN INDICATION ON ECAM. VALVE WAS REPLACED PER AMM 21-31-52-400-001.

Part: GUIDE VANE — CRACKED (NR 1 ENGINE) · airframe 17,309 hrs · 7,621 cycles

ENGINE NR 1, 14 OUTLET GUIDE VANES DOUBLERS WERE CRACKED AND WERE OUT OF LIMITS. REPAIRED AND REPLACED PER AMM 72-23-00-400-008.

Part: ENGINE — BIRD INGESTION (NR 2) · airframe 15,818 hrs · 7,013 cycles

BIRD STRIKE TO NR 2 ENGINE ON APPROACH TO MKE. DUE TO N1/N2 ROLLBACK, DAMAGE WAS SUSPECTED AND AGENT NR 1 FIRE BOTTLE WAS DISCHARGED. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. A BORESCOPE OF THE NR 2 ENGINE WAS PERFORMED AND MAJOR DAMAGE TO THE ENGINE WAS FOUND, WITH THE HEAVIEST DAMAGE TO THE CORE COMPRESSOR SECTION. THE NR 2 ENGINE IS IN THE PROCESS OF BEING REPLACED.

Part: FITTING — CORRODED (LT WING MLG) · corrosion level 2 · airframe 13,886 hrs · 6,207 cycles

INSPECTION REPORTED CORROSION ON FWD FACE, FWD LUG, LT WING RIB 5, LANDING GEAR FITTING. MACHINED CORROSION ON LUG FACE PER SRM 57-26-13.

Part: FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 13,886 hrs · 6,207 cycles

INSPECTION REPORTED CORROSION ON AFT FACE, FWD LUG, LT WING LANDING FITTING, RIB 5. MACHINED CORROSION PER SRM 57-26-13.

Part: FITTING — CORRODED (LT WING MLG) · corrosion level 2 · airframe 13,886 hrs · 6,207 cycles

INSPECTION REPORTED CORROSION IN FWD BORE FROM 4 O'CLOCK TO 7 O'CLOCK LT WING, RIB 5, LANDING FITTING. BORED OUT CORROSION PER SRM 57-26-13.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 13,764 hrs · 6,157 cycles

AIR DIVERSION, SMOKE SMELL IN AFT GALLEY. DECLARED AN EMERGENCY. MX PERFORMED TSM TASK 24-00-00-810-823, FOUND AFT NR 2 COFFEEMAKER C/B'S POPPED ON REAR OF COFFEEMAKER. REMOVED AFT NR 1 COFFEEMAKER & INSTALLED INTO NR 2 POSITION, OPS NORMAL. NO ARCING OR DEFECTS NOTED ON GALLEY WIRING. REINSTALLED COFFEEMAKERS IN ORIGINAL POSITIONS. DETERMINED AFT NR 2 COFFEEMAKER TO BE THE CAUSE OF ODOR SMELL. PERFORMED ENGINE MINIMUM IDLE CHECK TO OPERATE AIR CONDITIONING PACKS, NO ODORS OR SMOKE. PLACED AFT NR 2 COFFEEMAKER ON MEL. REMOVED & INSTALLED AFT NR 2 COFFEEMAKER. REMOVED MEL.

Part: SMOKE — DETECTED (CABIN) · airframe 11,900 hrs · 5,430 cycles

ON INBOUND TAXI, FLIGHT CREW REPORTED SMOKE IN CABIN. RAN ENGINES PER AMM 71-00-00-710-006. CYCLED AIR CONDITIONING PACKS. RAN APU. CYCLED APU BLEED AIR. INSPECTED CARGO BINS, E/E BAYS AND CABIN FOR SMOKE. NO FAULTS NOTED, COULD NOT DUPLICATE DISCREPANCY.

Part: SKIN — DENTED (FUSELAGE) · airframe 6,837 hrs · 3,250 cycles

DURING WALKAROUND, MAINTENANCE FOUND TWO SMALL DENTS AFT AND EVEN WITH FORWARD ENTRY DOOR, APPROXIMATELY 3 FT. AFT OF DOOR AT STA. 950, STR. 22L. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW EA A9-53R-10127 AND SRM 53-00-11.