# N909FR: 2002 Airbus A319-111, registration cancelled 2008-07-22 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 22, 2008 - Exported to: Bermuda - Status when cancelled: Valid registration - Airframe: [Airbus A319-111](https://openairdocs.org/model/airbus-a319-111) (registry code 3940000) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM) (OpenAirDocs) - Serial number: 1761 - Year built: 2002 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 4, 2004 - Certificate issued: June 30, 2008 - Last registry action: June 30, 2008 - Mode S code: AC9128 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N909FR - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=909FR - Page: https://openairdocs.org/deregistered/N909FR-2008-07-22 From the FAA registry file of November 7, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Airbus A319-111: https://openairdocs.org/model/airbus-a319-111.md ## Service difficulty reports (34) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR F3LA200700232](https://openairdocs.org/sdr/F3LA200700232), Sep 15, 2007: LIGHT. MISWIRED. BLOCK TURN BACK, FLIGHT CREW REPORTED L2 DOOR EMERGENCY EXIT LIGHT 'ON' DURING TAXI, EMERGENCY EXIT SIGN 'OFF' DURING TAXI. MAINTENANCE FOUND 45WL, EXIT MARKING - [SDR F3LA200700227](https://openairdocs.org/sdr/F3LA200700227), Sep 9, 2007: SLIDE. FAULTED. DURING C4/S1 CHECK, INSPECTION REPORTED EMERGENCY LIGHT TEST SHOWED LEFT EPSU EXTERNAL FAULT. REPLACED R1 DOOR SLIDE IAW AMM 25-62-44-400-007. - [SDR F3LA200700221](https://openairdocs.org/sdr/F3LA200700221), Sep 9, 2007: BATTERY. FAILED. DURING C4/S1 CHECK, INSPECTION REPORTED "TEST EMERG LIGHT BAT" BATTERY CAPACITY CHECK FAILED. REMOVED AND REPLACED EMERGENCY EXIT BATTERIES IAW AMM 33-51-38-PB4 - [SDR F3LA200700229](https://openairdocs.org/sdr/F3LA200700229), Sep 8, 2007: ACCESS PANEL. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON FUEL PANEL 640JB ATTACHMENT HOLES. REMOVED AND REPLACED FUEL PANEL 640JB ON RT WING IAW AMM 57-27-11-400-00 - [SDR F3LA200700228](https://openairdocs.org/sdr/F3LA200700228), Sep 8, 2007: ATTACH FITTING. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED LWR FWD ATTACH FITTING ON RT MLG STRUT DOOR RUSTED. REMOVED AFFECTED PARTS AND INSTALLED LWR FWD ATTACH FITTING IAW MM 3 - [SDR F3LA200700222](https://openairdocs.org/sdr/F3LA200700222), Sep 6, 2007: PLATE. GOUGED. DURING C4/S1 CHECK, INSPECTION REPORTED THE TRIMMABLE HORIZONTAL STAB MECHANICAL LINKAGE INBD OF UPPER CHAIN SPROCKET DAMAGED. SWIVEL PLATE AND LINK PLATE GOUGE - [SDR F3LA200700220](https://openairdocs.org/sdr/F3LA200700220), Sep 6, 2007: BOLT. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED THE FLOOR MOUNT BOLT ON THE AFT INBD CORNER OF THE AFT WALL OF LAV A WAS CORRODED AND COULD NOT BE REMOVED WITH STANDARD - [SDR F3LA200700218](https://openairdocs.org/sdr/F3LA200700218), Sep 5, 2007: FLOOR PANEL. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR THRESHOLD PANEL 221FF CORRODED TO EDGE. REMOVED AND REPLACED THRESHOLD PANEL 221FF IAW AMM 53-12-12 AND WORK CARD - [SDR F3LA200700217](https://openairdocs.org/sdr/F3LA200700217), Sep 5, 2007: FLOOR PANEL. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL THRESHOLD PANEL 222FF CORRODED TO EDGE. REMOVED AND REPLACED FLOOR THRESHOLD PANEL 222FF IAW AMM 53-12-12 AN - [SDR F3LA200700223](https://openairdocs.org/sdr/F3LA200700223), Sep 3, 2007: FLOORBEAM. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED LT FLOORBEAM Y1292 CORRODED ON BOTTOM OF NUTPLATE HOLE AT FR66. FLOORBEAM FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-1 - [SDR F3LA200700216](https://openairdocs.org/sdr/F3LA200700216), Sep 2, 2007: FLOOR PANEL. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON LOWER SURFACE OF FLOOR PANEL 261FF. REMOVED REPLACED FLOOR PANEL IAW SRM 51-24-00 AND AMM 53-42-12-400-002. - [SDR F3LA200700215](https://openairdocs.org/sdr/F3LA200700215), Sep 2, 2007: FLOORBEAM. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED CABIN FLOOR CENTER SUPPORT AT Y254, FR16, CORRODED. REMOVED DAMAGED AREA OF FLOORBEAM Y254 IAW SRM 53-00-14, FIG 204. RE - [SDR F3LA200700214](https://openairdocs.org/sdr/F3LA200700214), Sep 2, 2007: FLOOR PANEL. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON TOP SURFACE OF FLOOR PLANEL 221EF AFT OTBD CONNECTING PLATE. REMOVED AND REPLACED CONNECTING PLATE IAW AMM - [SDR F3LA200700213](https://openairdocs.org/sdr/F3LA200700213), Sep 2, 2007: FLOOR PANEL. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON LOWER SURFACE OF FLOOR PANEL 262FF. REMOVED AND REPLACED FLOOR PANEL 262FF IAW AMM 53-42-12-400-002. - [SDR F3LA200700226](https://openairdocs.org/sdr/F3LA200700226), Sep 1, 2007: FLOORBEAM. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT FLOORBEAM FROM STR 38R TO STR 38L CORRODED AROUND FASTENER HOLES. REMOVED AND REPLACED TRANSITION - [SDR F3LA200700212](https://openairdocs.org/sdr/F3LA200700212), Sep 1, 2007: SUPPORT ANGLE. CRACKED. DURING C4/S1 CHECK, INSPECTION REPORTED RT ENGINE PYLON SUPPORT ANGLE THAT ATTACHES PYLON PANELS 423DL AND 424CR AT RIB 5 CRACKED (AREA AROUND AFT SCREW HOLE). - [SDR F3LA200700225](https://openairdocs.org/sdr/F3LA200700225), Aug 31, 2007: FLOORBEAM. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON UNDERNEATH SIDE OF NUTPLATE HOLE AT FR66. REPLACED COUPLING IAW 51-42-11. - [SDR F3LA200700224](https://openairdocs.org/sdr/F3LA200700224), Aug 30, 2007: SHEAR PLATE. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED SURFACE CORROSION AT AFT END OF LT SHEAR PLATE BETWEEN FR69 AND FR70. REMOVED AND REPLACED SHEAR PLATE BETWEEN FR69 AND - [SDR F3LA200700211](https://openairdocs.org/sdr/F3LA200700211), Aug 30, 2007: SEAL. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED LT DOOR SEAL CORRODED AT NUT PLATE HOLE AT FR66. FABRICATED REPAIR ANGLE, FILLERS AND DOUBLER IAW SRM 53-41-14. INSTALLE - [SDR F3LA200700210](https://openairdocs.org/sdr/F3LA200700210), Aug 30, 2007: SHIM. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED FWD FLOOR PROFILER IN FWD CARGO COMPARTMENT HAD CORROSION AROUND FASTENER HOLE. REMOVED CORROSION ON SHIM FROM AROUND FA - [SDR F3LA200700208](https://openairdocs.org/sdr/F3LA200700208), Aug 30, 2007: BRACKET. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED FWD CARGO DOOR BOTTOM FRAME ALONG STR 38, JUST FWD OF FR26 FITTING BETWEEN 2ND AND 3RD LOCKING ROLLERS, CORRODED AT OTBD - [SDR F3LA200700207](https://openairdocs.org/sdr/F3LA200700207), Aug 30, 2007: FRAME. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED RT SUPPORT FRAME BETWEEN FR69 AND FR70 CORRODED. REMOVED AND REPLACED SUPPORT FRAME IAW A319 SRM 51-42-11. - [SDR F3LA200700209](https://openairdocs.org/sdr/F3LA200700209), Aug 29, 2007: PANEL. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON ATTACHMENT HOLES ON PANEL 540JB. REPLACED PANEL IAW A319 WORKCARD CP757-2 - [SDR F3LA200700206](https://openairdocs.org/sdr/F3LA200700206), Aug 27, 2007: SHEAR PLATE. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED RT SHEAR PLATE BETWEEN FR 69 AND FR 70 CORRODED. REMOVED AND REPLACED SHEAR PLATE IAW A319 SRM 51-42-11, PARA 6.B. - [SDR F3LA200700205](https://openairdocs.org/sdr/F3LA200700205), Aug 27, 2007: DUMMY RAIL. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED CABIN FLOOR LT DUMMY RAIL AT FR12 TO FR16 CORRODED. REMOVED AND REPLACED DUMMY RAIL IAW A319 SRM 51-42-11. - [SDR F3LA200700204](https://openairdocs.org/sdr/F3LA200700204), Aug 27, 2007: PROFILE. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION AROUND FWD CARGO COMPARTMENT AFT FLOOR PROFILE FASTENER HOLES. REMOVED AND REPLACED PROFILE IAW A319 SRM 51-42 - [SDR F3LA200700203](https://openairdocs.org/sdr/F3LA200700203), Aug 27, 2007: FLOORBEAM. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON UPPER SURFACE OF LT FLOORBEAM Y765 AT FR68. FLOORBEAM FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14, PG 1 - [SDR F3LA200700186](https://openairdocs.org/sdr/F3LA200700186), Jul 26, 2007: WINDOW. UNKNOWN. DIVERSION AT FL 370, FLIGHT CREW HEARD A LOUD POP AND HISSING SOUND FROM THE CAPTAIN'S AFT SIDE WINDOW. AIRCRAFT DESCENDED TO 14000 RA AND LANDED AT KMCI. REPLA - [SDR F3LA200700036](https://openairdocs.org/sdr/F3LA200700036), Feb 16, 2007: WINDSHIELD. CRACKED. UPON ARRIVAL AT GATE, CAPTAIN'S WINDSHIELD CRACKED. REPLACED NR 1 WINDSHIELD IAW AMM 56-11-11, PB 401, P/N STA320-2-7-1A, S/N 5910 (MFG SULLY). ON PUSHBACK, FIR - [SDR F3LA200600146](https://openairdocs.org/sdr/F3LA200600146), Oct 19, 2006: FAN. FAILED. DIVERSION, DURING CRUISE EN ROUTE TO MCO, FLIGHT CREW REPORTED BLOWER FAULT WITH ASSOCIATED ODOR. FLIGHT CREW DECLARED AN EMERGENCY AND DIVERTED TO BIRMINGHAM, - [SDR F3LA200600009](https://openairdocs.org/sdr/F3LA200600009), Mar 22, 2006: SUPPORT BEAM. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION AT SCREW HOLES IN FLOOR SUPPORT BEAM BL50L, BETWEEN FS 66 AND FS 68, L2 DOOR THRESHOLD. REMOVED AND REPLACED DAM - [SDR F3LA200500035](https://openairdocs.org/sdr/F3LA200500035), Jul 20, 2005: CONTROL UNIT. UNSERVICEABLE. AIR TURNBACK. ON TAKEOFF, FLIGHT CREW REPORTED LGCIU NR 1 FAULT ON WHEEL PAGE. HAD X'S ON WHEEL PAGE. REVERSER 1 FAULT ON STATUS PAGE. REPLACED NO. 1 LGCIU PER - [SDR F3LA200500012](https://openairdocs.org/sdr/F3LA200500012), Mar 10, 2005: COMPUTER. FAULTY. FLIGHT CREW REPORTED ECAM FLIGHT CONTROL ELAC 2 PITCH FAULT (PASSING THROUGH FL180). AIRCRAFT RETURNED TO DEN AND LANDED WITHOUT INCIDENT. REPLACED NR 2 ELAC CO - [SDR F3LA200400075](https://openairdocs.org/sdr/F3LA200400075), Jul 27, 2004: COMPUTER. FAILED. AIR TURN BACK. FLIGHT CREW REPORTED NUMEROUS SYSTEM FAILURES (GPS, GPWS, NR 1 RA, NR 1 ILS, NR 1 ENGINE REVERSER, NR 1 FADEC). CHECKED LAST LEG ECAM REPORT AND ## Other aircraft with N909FR - [Cancelled 1993-11-30](https://openairdocs.org/deregistered/N909FR-1993-11-30): Dassault/Sud FAN JET FALCON, S/N 209. Exported to United Kingdom. Owner: [Mercantile-Safe Dep & Tr Co Trustee](https://openairdocs.org/faa-owner/MERCANTILE-SAFE%20DEP%20%26%20TR%20CO%20TRUSTEE), [Baltimore, MD](https://openairdocs.org/faa-place/MD/Baltimore) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.