# N903FR: 2001 Airbus A319-111, registration cancelled 2009-02-17 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 17, 2009 - 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 CFM56-5B5/P series](https://openairdocs.org/engine/cfm-international-cfm56-5b5-p-series) (registry code 13016) - Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM) (OpenAirDocs) - Serial number: 1560 - Year built: 2001 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 8, 2008 - Certificate issued: September 4, 2008 - Last registry action: November 26, 2008 - Mode S code: AC7ADE - 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/N903FR - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=903FR - Page: https://openairdocs.org/deregistered/N903FR-2009-02-17 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 (28) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR F3LA200800587](https://openairdocs.org/sdr/F3LA200800587), Aug 25, 2008: POWER SUPPLY. FAILED. REFERENCE NON ROUTINE 104231. DURING EXIT CHECK, INSPECTION NOTED LT FORWARD EMERGENCY POWER SUPPLY UNIT FAILED EMERGENCY LIGHTS TEST. MX R&R LT FORWARD EMERGEN - [SDR F3LA200800071](https://openairdocs.org/sdr/F3LA200800071), Feb 18, 2008: SEAL. CORRODED. DURING C5 C CHECK, MAINTENANCE REPORTED CORROSION FOUND ON RIGHT WING AILERON HINGE SEAL NEAR OUTBOARD HINGE LOCATION. MAINTENANCE REMOVED AND REPLACED AILERON - [SDR F3LA200800070](https://openairdocs.org/sdr/F3LA200800070), Feb 17, 2008: THRESHOLD. CORRODED. DURING C5 C CHECK, INSPECTION REPORTED LEVEL 1 CORROSION OF AFT CARGO PIT DOOR THRESHOLD AT EIGHTEEN (18) LOCATIONS AROUND ATTACHMENT HOLES AND ADJACENT TO THRE - [SDR F3LA200800057](https://openairdocs.org/sdr/F3LA200800057), Feb 17, 2008: PROFILE. CORRODED. DURING C5 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ALONG THE ATTACHMENT HOLES OF THE AFT CARGO PIT PROFILE AT FRAME 58, FROM THE RIGHT TO THE LEFT SIDE. - [SDR F3LA200800056](https://openairdocs.org/sdr/F3LA200800056), Feb 17, 2008: PROFILE. CORRODED. DURING A C5 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ALONG THE ATTACHMENT HOLES OF THE AFT CARGO PIT PROFILE AT FRAME 59, FROM THE RIGHT TO THE LEFT SID - [SDR F3LA200700047](https://openairdocs.org/sdr/F3LA200700047), Apr 2, 2007: CONNECTOR. DAMAGED. 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 - [SDR F3LA200600105](https://openairdocs.org/sdr/F3LA200600105), Sep 2, 2006: ODOR. DETECTED. BLOCK TURNBACK IN CUN. FLIGHT ATTENDANTS REPORTED SMELL OF SMOKE IN FWD PASSENGER CABIN AREA (APPROXIMATELY ROW 6 AND FWD). MAINTENANCE PERFORMED INSPECTION OF - [SDR F3LA200600102](https://openairdocs.org/sdr/F3LA200600102), Aug 24, 2006: EPSU. FAILED. 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. - [SDR F3LA200600101](https://openairdocs.org/sdr/F3LA200600101), Aug 24, 2006: BATTERY PACK. FAILED. 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. - [SDR F3LA200600100](https://openairdocs.org/sdr/F3LA200600100), Aug 24, 2006: EPSU. FAILED. 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 - [SDR F3LA200600095](https://openairdocs.org/sdr/F3LA200600095), Aug 18, 2006: SLAT TRACK. DAMAGED. 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 - [SDR F3LA200600092](https://openairdocs.org/sdr/F3LA200600092), Aug 18, 2006: VALVE. CORRODED. 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 - [SDR F3LA200600094](https://openairdocs.org/sdr/F3LA200600094), Aug 15, 2006: THRESHOLD. CORRODED. 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 - [SDR F3LA200600093](https://openairdocs.org/sdr/F3LA200600093), Aug 15, 2006: THRESHOLD. CORRODED. 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 - [SDR F3LA200600089](https://openairdocs.org/sdr/F3LA200600089), Aug 10, 2006: FLOOR SUPPORT. CORRODED. 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. - [SDR F3LA200600099](https://openairdocs.org/sdr/F3LA200600099), Aug 9, 2006: SEAT TRACK. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED AFT FUSELAGE CABIN FLOOR STRUCTURE FR66, Y1292, CORRODED UNDER NUT CLIPS. BURNISHED CORROSION ON SEAT TRACK/STRUCTURE AT F - [SDR F3LA200600098](https://openairdocs.org/sdr/F3LA200600098), Aug 9, 2006: BEAM. CORRODED. 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, F - [SDR F3LA200600097](https://openairdocs.org/sdr/F3LA200600097), Aug 9, 2006: FLOOR SUPPORT. CORRODED. 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 - [SDR F3LA200600096](https://openairdocs.org/sdr/F3LA200600096), Aug 9, 2006: DUMMY RAIL. CORRODED. 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 DU - [SDR F3LA200600091](https://openairdocs.org/sdr/F3LA200600091), Aug 8, 2006: SWITCH. CORRODED. RIGHT HAND CABIN PRESSURE SAFETY VALVE (GHL) FAILED OPERATION TEST. POSITION SWITCH WAS CORRODED. NO OPEN INDICATION ON ECAM. VALVE WAS REPLACED PER AMM 21-31-5 - [SDR F3LA200600090](https://openairdocs.org/sdr/F3LA200600090), Aug 6, 2006: GUIDE VANE. CRACKED. 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. - [SDR F3LA200600011](https://openairdocs.org/sdr/F3LA200600011), Mar 22, 2006: ENGINE. BIRD INGESTION. 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 - [SDR F3LA200500041](https://openairdocs.org/sdr/F3LA200500041), Sep 7, 2005: FITTING. CORRODED. 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. - [SDR F3LA200500040](https://openairdocs.org/sdr/F3LA200500040), Sep 7, 2005: FITTING. CORRODED. 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. - [SDR F3LA200500039](https://openairdocs.org/sdr/F3LA200500039), Sep 7, 2005: FITTING. CORRODED. INSPECTION REPORTED CORROSION ON AFT FACE, FWD LUG, LT WING LANDING FITTING, RIB 5. MACHINED CORROSION PER SRM 57-26-13. - [SDR F3LA200500038](https://openairdocs.org/sdr/F3LA200500038), Aug 15, 2005: COFFEEMAKER. ODOR. 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 COFF - [SDR F3LA200500005](https://openairdocs.org/sdr/F3LA200500005), Feb 17, 2005: SMOKE. DETECTED. 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. INSPEC - [SDR F3LA200300126](https://openairdocs.org/sdr/F3LA200300126), Sep 6, 2003: SKIN. DENTED. 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 ## Other aircraft with N903FR - [Cancelled 1991-04-24](https://openairdocs.org/deregistered/N903FR-1991-04-24): Dassault/Sud FAN JET FALCON, S/N 20. Exported to United Kingdom. Owner: [Mercantile-Save Dep & Tr Co Trustee](https://openairdocs.org/faa-owner/MERCANTILE-SAVE%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.