# N904FR: 2001 Airbus Industrie A319-111, registration cancelled 2016-04-14 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 14, 2016 - Exported to: Bermuda - Status when cancelled: Valid registration - Airframe: [Airbus Industrie A319-111](https://openairdocs.org/model/airbus-industrie-a319-111) (registry code 3930336) - 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: 1579 - Year built: 2001 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 19, 2001 - Certificate issued: June 21, 2007 - Last registry action: January 30, 2015 - Mode S code: AC7E95 - 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/N904FR - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=904FR - Page: https://openairdocs.org/deregistered/N904FR-2016-04-14 From the FAA registry file of October 29, 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 Industrie A319-111: https://openairdocs.org/model/airbus-industrie-a319-111.md ## Service difficulty reports (58, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR F3LA2013062500869](https://openairdocs.org/sdr/F3LA2013062500869), Jun 25, 2013: LAMP. BURNED OUT. EMERGENCY LIGHT EPSU TEST FAILED DURING A SCHEDULED HEAVY CHECK. R & R LAMPS IAW AMM 33-51-16-400-001A. - [SDR F3LA2013051700856](https://openairdocs.org/sdr/F3LA2013051700856), May 15, 2013: SKIN. CONTAMINATED. ACCOMPLISHED THERMOGRAPHIC INSPECTION OF LT ELEVATOR. SIX AREAS IN UPPER SKIN INDICATING WATER INGRESS, THREE AREAS ON LOWER SKIN. REPAIRED IAW SRM 55-20-00, PB - [SDR F3LA2012101500806](https://openairdocs.org/sdr/F3LA2012101500806), Oct 15, 2012: SHEAR PLATE. CORRODED. FRAME 70 RIGHT SIDE SHEAR PLATE CORROSION. R & R SHEAR PLATE IAW EO AO-53EO-31434. - [SDR F3LA2012101500805](https://openairdocs.org/sdr/F3LA2012101500805), Oct 15, 2012: PLATE. CORRODED. FRAME 70 LT SIDE SHEAR PLATE CORROSION. R & R SHEAR PLATE IAW EO AO-53EO-31434. - [SDR F3LA2012101500804](https://openairdocs.org/sdr/F3LA2012101500804), Oct 15, 2012: SILL. CORRODED. FRAME 66 RIGHT DOOR SILL BEAM SURFACE CORROSION AROUND FASTENER HOLE. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 53-41-14 PB101, PARAGRAPH 4 B, FIG - [SDR F3LA2012101500803](https://openairdocs.org/sdr/F3LA2012101500803), Oct 15, 2012: FLOORBEAM. CORRODED. FR66, -Y1292 FLOORBEAM CORROSION. R & R FLOORBEAM REF SRM 51-42 -11 , PARAGRAPH 5. - [SDR F3LA2012101500802](https://openairdocs.org/sdr/F3LA2012101500802), Oct 15, 2012: SILL. CORRODED. L2 DOOR CUT OUT AT DOOR SILL HAS CORROSION 5 PLACES. R & R SHAPE SILL IAW SRM 51-42-11 PARA 6.B AND D. - [SDR F3LA2012101500801](https://openairdocs.org/sdr/F3LA2012101500801), Oct 15, 2012: SILL. CORRODED. AFT CARGO DOOR SILL HAS CORROSION IN SEVERAL PLACES FROM FRAMES 55A TO 59. R & R DOOR SILL IAW REF SRM 51-42- 11 , PARA 6.B. AND 7.B. - [SDR F3LA2012003200728](https://openairdocs.org/sdr/F3LA2012003200728), Mar 20, 2012: BLADE. LACK OF LUBE. NR 1 ENGINE VIBRATION IN CLIMB OVER 4.0. VIBRATION WOULD FOLLOW THRUST. AIR TURN BACK. PERFORMED TSM TASKS 77-00-00-81 0-863-A AND 77-00-00-81 O-B64-A INCLUDING - [SDR F3LA2011122100696](https://openairdocs.org/sdr/F3LA2011122100696), Dec 21, 2011: ELECTRICAL BOX. ODOR. PAX & F/A'S REPORTED THE STRONG BURNING ELECTRICAL ODOR IN ROW 20-22 A/C LEFT. FOUND SEB ROW 21ABC EMITTING ELECTRICAL ODOR, PERFORMED INSPECTIONS OF AFT GALLEY - [SDR F3LA2011121100692](https://openairdocs.org/sdr/F3LA2011121100692), Dec 7, 2011: SWITCH. FAILED. EMERGENCY EXIT LIGHT SWITCH NOT INDICATING OFF WHEN PLACED IN THE OFF POSITION. REPLACED TOGGLE SWITCH 4WL (ON/OFF/ARM) REF ESPM 20-45-21, TEST OK REF AMM 33-51 - [SDR F3LA2011052300653](https://openairdocs.org/sdr/F3LA2011052300653), May 20, 2011: SUPPORT FITTING. CORRODED. C-CHECK: RT WING MLG SUPPORT RIB 5 FWD LUG INNER BORE HAS CORROSION. IAW EO A0-57EO-20243. REMOVED CORROSION BY OVER SIZING BORE TO 3.8772" AND INSTALLING NEW B - [SDR F3LA2011022100606](https://openairdocs.org/sdr/F3LA2011022100606), Feb 17, 2011: STOP. SEIZED. ACFT LOG PAGE 590497: AIR TURN BACK AT 01302. ECAM WARNING NR 2 ENGINE COMPRESSOR VANE (AIR RETURN. REPLACED NR 2 ENGINE MASTER BALLSCREW ACTUATOR STOP. REF AMM - [SDR F3LA2010043000392](https://openairdocs.org/sdr/F3LA2010043000392), Apr 27, 2010: WARNING LIGHT. ILLUMINATED. PILOT REPORT REF LOG PAGE 508494 ITEM(S) 1 FCTL FLAP FAULT (FLIGHT CONTROL FLAP FAULT)AND ITEM 2 FCTL SLAT FAULT (FLIGHT CONTROL SLAT FAULT) EMERGENCY DECLARED. - [SDR F3LA2010022300353](https://openairdocs.org/sdr/F3LA2010022300353), Feb 20, 2010: BULB. BURNED OUT. DURING VISUAL INSPECTION IT WAS NOTED THE EXIT SIGN BULB WAS BURNED OUT OVER FORWARD ENTRY. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT SIGN BULB IAW AMM 33 - [SDR F3LA2009112400237](https://openairdocs.org/sdr/F3LA2009112400237), Nov 23, 2009: COFFEEMAKER. ODOR. REFERENCE LOG PAGES 492755 AND 492756. FLIGHT CREW MADE AN AIR RETURN DUE TO A BURNING ODOR IN THE AFT GALLEY. MX PERFORMED TROUBLESHOOTING IAW TSM 21-00-00-810 - [SDR F3LA2009100500194](https://openairdocs.org/sdr/F3LA2009100500194), Sep 30, 2009: HOOK. BROKEN. DURING C6 C-CHECK, INSP NOTED THAT THE L1 DOOR HANDLE WAS ABLE TO CLOSE WITHOUT THE DOOR BEING IN THE CLOSED POSITION. MX REMOVED AND REPLACED THE L1 DOOR HOOK - [SDR F3LA2009100500195](https://openairdocs.org/sdr/F3LA2009100500195), Sep 27, 2009: FLOOR PANEL. CORRODED. DURING C6 C-CHECK, INSP NOTED THE L2 ENTRY DOOR FLOOR PANEL HAS SEVERAL SPOTS OF CORROSION AROUND FASTENER HOLES. MX REMOVED AND REPLACED THE FLOOR PANEL AT POS - [SDR F3LA2009100100189](https://openairdocs.org/sdr/F3LA2009100100189), Sep 26, 2009: STRINGER. CORRODED. DURING C6 C-CHECK, INSP NOTED CORROSION ON STR 44, SIX INCHES AFT OF FRAME 65 NEAR POTABLE WATER SERVICE PANEL. MX CUT OUT DAMAGED AREA, FABRICATED REPAIR STR A - [SDR F3LA2009100100188](https://openairdocs.org/sdr/F3LA2009100100188), Sep 26, 2009: HOOK. BROKEN. DURING C6 C-CHECK, INSP NOTED THE R2 DOOR CLOSING BEFORE DOOR WAS IN DOOR JAM. MX REMOVED AND REPLACED THE HOOK AT THE R2 DOOR HANDLE IAW AMM 52-13-21-400-001. - [SDR F3LA2009100100187](https://openairdocs.org/sdr/F3LA2009100100187), Sep 26, 2009: SHEAR PLATE. CORRODED. DURING C6 C-CHECK, INSP NOTED THE LT HAND SHEAR PLATE AT Y1292 BETWEEN FRAME 69 AND FRAME 70 WAS CORRODED AT THE AFT SCREW HOLE. MX REMOVED AND REPLACED THE SHE - [SDR F3LA2009100100186](https://openairdocs.org/sdr/F3LA2009100100186), Sep 26, 2009: FLOORBEAM. CORRODED. DURING C6 C-CHECK, INSP NOTED CORRODED FASTENER HOLES AT STATION -Y1292 AND FRAME 66. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11 AND 51-44-11. - [SDR F3LA2009100100193](https://openairdocs.org/sdr/F3LA2009100100193), Sep 25, 2009: SHEAR PLATE. CORRODED. DURING C6 C-CHECK, INSPECTION NOTED THE RT SHEAR PLATE AT Y1732 BETWEEN FRAME 69 AND FRAME 70 HAS CORROSION. MX REMOVED AND REPLACED THE SHEAR PLATE IAW SRM 51- - [SDR F3LA2009100100192](https://openairdocs.org/sdr/F3LA2009100100192), Sep 25, 2009: SILL. CORRODED. DURING C6 C-CHECK, INSPECTION NOTED THE L2 DOOR SILL HAS SEVERAL AREAS OF CORROSION. MX REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-42-11 AND D53408505. - [SDR F3LA2009100100184](https://openairdocs.org/sdr/F3LA2009100100184), Sep 24, 2009: FLOORBEAM. CORRODED. SUPPLEMENTAL INFORMATION: REFERENCE NON ROUTINE C070051. DURING DEN C6 C-CHECK, INSPECTION NOTED CORROSION AROUND THE NUT PLATES LOCATED AT R2, Y1292 BETWEEN FR - [SDR F3LA2009100100191](https://openairdocs.org/sdr/F3LA2009100100191), Sep 24, 2009: FLOORBEAM. CORRODED. DURING C6 C-CHECK, INSP NOTED THE COUPLING ATTCH POINT AT L2, STATION Y1292 AND FRAME 68 HAS CORROSION. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11 A - [SDR F3LA2009100100190](https://openairdocs.org/sdr/F3LA2009100100190), Sep 24, 2009: FLOORBEAM. CORRODED. DURING C6 C-CHECK, INSP NOTED CORROSION AROUND THE NUT PLATES AT L2, STATION Y1292 BETWEEN FRAME 66 AND FRAME 68. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM - [SDR F3LA2009100100185](https://openairdocs.org/sdr/F3LA2009100100185), Sep 24, 2009: FLOORBEAM. CORRODED. DURING C6 C-CHECK, INSP NOTED THE COUPLING ATTACH POINT AT STATION Y1292 AND FRAME 68 HAS CORROSION. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM 53-41-14, 51- - [SDR F3LA2009020300019](https://openairdocs.org/sdr/F3LA2009020300019), Feb 2, 2009: BULB. INOPERATIVE. DURING HEAVY CHECK, MAINTENANCE NOTED THE EMERGENCY PATH LIGHTS WERE INOPERATIVE AT SEATS 3, 6, 7, 18 AND 22. MAINTENANCE REMOVED AND REPLACED ALL INOPERATIVE E - [SDR F3LA2008121600724](https://openairdocs.org/sdr/F3LA2008121600724), Dec 13, 2008: FIRE DETECTOR. NO TEST. PILOT REPORTED THE NR 2 ENGINE FIRE PUSHBUTTON SWITCH LIGHT, CONTINUOUS REPETITIVE CHIME, BOTH MASTER WARNINGS AND ENGINE CONTROL PANEL FIRE LIGHT FAIL TO TEST. - [SDR F3LA200800520](https://openairdocs.org/sdr/F3LA200800520), Jul 27, 2008: SWITCH. FAULTY. DURING PRE-FLIGHT INSP, CREW NOTED THE EMERGENCY EXIT AND AISLE LIGHTS WERE ILLUMINATED IN THE ARMED POSITION. MAINT REMOVED AND REPLACED THE TOGGLE SWITCH AND - [SDR F3LA200800135](https://openairdocs.org/sdr/F3LA200800135), Apr 6, 2008: SKIN. GOUGED. DURING PRE FLIGHT INSPECTION, THE FLIGHT CREW REPORTED AFT LEFT FUSELAGE SKIN GOUGE AND DENT AT FRAME 61 AND STRINGER 38 LEFT. BLENDED THE GOUGE IN ACCORDANCE W - [SDR F3LA200800133](https://openairdocs.org/sdr/F3LA200800133), Mar 29, 2008: STRINGER. DAMAGED. DURING C5 C CHECK INSPECTION REPORTED DURING PERFORMANCE OF REPAIR STRINGER WAS DAMAGED. MAINTENANCE REPAIRED THE STRINGER IN ACCORDANCE WITH THE REQUIREMENTS O - [SDR F3LA200800132](https://openairdocs.org/sdr/F3LA200800132), Mar 29, 2008: HINGE FITTING. CORRODED. DURING C5 C CHECK INSPECTION REPORTED CORROSION WAS FOUND IN THE MOUNTING HOLES OF THE RIGHT MAIN LANDING GEAR FORWARD HINGE BEARING SUPPORT BRACKET. MAINTENANC - [SDR F3LA200700123](https://openairdocs.org/sdr/F3LA200700123), May 31, 2007: ENGINE. MALFUNCTIONED. AIR TURN BACK AT 1710Z, FLIGHT CREW REPORTED NR 2 ENGINE ROLLBACK TO BETWEEN 45 PERCENT AND 55 PERCENT N1 DURING CLIMB-OUT OF 10,000 FT. ENGINE WAS ALSO MAKING - [SDR F3LA200700110](https://openairdocs.org/sdr/F3LA200700110), Apr 23, 2007: SKIN. GOUGED. DURING TAKEOFF, NR 2 ENGINE FAN COWL DEPARTED AIRCRAFT HITTING INBD UNDER WING AREA. SEVERAL GOUGES AND SCRATCHES WERE FOUND BETWEEN RIBS 4 AND 6 AND STRINGERS - [SDR F3LA200700105](https://openairdocs.org/sdr/F3LA200700105), Apr 23, 2007: SKIN. DELAMINATED. DURING TAKEOFF, NR 2 ENGINE FAN COWL DEPARTED AIRCRAFT HITTING ELEVATOR ABOUT MID-SPAN. OUTER SKIN WAS DELAMINATED AND SHOWED LOSS OF INNER CORE MATERIAL. ALSO, - [SDR F3LA200700104](https://openairdocs.org/sdr/F3LA200700104), Apr 23, 2007: SKIN. PUNCTURED. DURING TAKEOFF, NR 2 ENGINE FAN COWL DEPARTED AIRCRAFT HITTING OTBD HORIZONTAL STABILIZER LEADING EDGE. PUNCTURE WAS FOUND ABOUT MID SPAN OF LEADING EDGE. REPLA - [SDR F3LA200700103](https://openairdocs.org/sdr/F3LA200700103), Apr 23, 2007: SKIN. DENTED. DURING TAKEOFF, NR 2 ENGINE FAN COWL DEPARTED AIRCRAFT HITTING NR 1 SLAT. SLAT HAD SEVERE DENT DAMAGE TO LEADING EDGE OF STRUCTURE. REPLACED NR 1 SLAT IAW AMM 2 - [SDR F3LA200700102](https://openairdocs.org/sdr/F3LA200700102), Apr 23, 2007: SKIN. DENTED. DURING TAKEOFF, NR 2 ENGINE FAN COWL DEPARTED AIRCRAFT HITTING NR 2 SLAT. SLAT HAD SEVERE DENT AND GOUGE TO LEADING EDGE OF STRUCTURE. REPLACED NR 2 SLAT IAW AM - [SDR F3LA200700083](https://openairdocs.org/sdr/F3LA200700083), Apr 22, 2007: STRUCTURE. FAILED. NR 2 ENGINE COWLING DEPARTED AIRCRAFT. CAUSE UNKNOWN AT THIS TIME AND IS UNDER INVESTIGATION BY THE FAA. [SUP 05-15-07] THE NR 2 ENGINE FWD CANTILEVER ASSY SUST - [SDR F3LA200600157](https://openairdocs.org/sdr/F3LA200600157), Nov 8, 2006: BATTERY. INOPERATIVE. FLIGHT CREW REPORTED FRONT EMERGENCY EXIT LIGHTS INOP. IN AUTOMATIC. OPERATES OK IN (ON) POSITION. REPLACED EPSU AND BATTERY AT 10WL IAW AMM 33-51-38, PB401. OP - [SDR F3LA200600120](https://openairdocs.org/sdr/F3LA200600120), Sep 13, 2006: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED L2 DOOR THRESHOLD FLOORBEAM AT Y1732 AND FRAME 68 CORRODED ABOVE NUT PLATE. CORROSION DAMAGE ON DOOR SILL BEAM WAS FOUND T - [SDR F3LA200600118](https://openairdocs.org/sdr/F3LA200600118), Sep 7, 2006: PLATE. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED R1 DOOR FWD GIRT BAR FITTING ATTACH PLATE CORRODED. REPLACED FWD GIRT BAR PLATE ASSY. IAW SRM 51-42-11 AND AMM 20-21-11. - [SDR F3LA200600122](https://openairdocs.org/sdr/F3LA200600122), Sep 1, 2006: COVER. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED L2 DOOR FLOORBOARD ACCESS COVER PLATE CORRODED ON LWR SIDE. COVER PLATE WAS FOUND TO BE OUT OF LIMITS PER SRM 53-41-14. FA - [SDR F3LA200600117](https://openairdocs.org/sdr/F3LA200600117), Sep 1, 2006: PLATE. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED R2 DOOR FWD GIRT BAR PLATE CORRODED. REPLACED FWD GIRT BAR PLATE IAW AMM 52-13-31-400-003. SEALED AREA AROUND FWD PLATE AT - [SDR F3LA200600121](https://openairdocs.org/sdr/F3LA200600121), Aug 31, 2006: WEB. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR WEB OB AND AFT OF BEAM AT FR69 AND Y1292. REMOVED FLOOR WEBS IAW SRM 51-42-11. FOUND UPPER WEB TO BE OU - [SDR F3LA200600116](https://openairdocs.org/sdr/F3LA200600116), Aug 31, 2006: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM (LONGERON) FWD OF FR68 AT Y1292. BLENDED OUT CORRODED AREA ON FLOORBEAM AND FOUND AREA TO BE OUT OF - [SDR F3LA200600113](https://openairdocs.org/sdr/F3LA200600113), Aug 30, 2006: FLOOR SUPPORT. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT IB OF L2 AT Y1292 FROM FR66 TO FR68 AT HOLES. FLOORBEAM WAS FOUND TO BE OUT OF LIMITS IAW SRM 5 - [SDR F3LA200600108](https://openairdocs.org/sdr/F3LA200600108), Aug 30, 2006: FLOORBEAM. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AFT OF L2 DOOR CUTOUT AT FR68 TO FR69, Y1292. FLOORBEAM WAS FOUND TO BE OUT OF LIMITS PER 53-00-14. All 58: https://openairdocs.org/deregistered/N904FR-2016-04-14/reports.md ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB ATL07IA078](https://openairdocs.org/ntsb/ATL07IA078), Apr 22, 2007: Airbus Industrie A319-111 (N904FR), Atlanta, GA, incident, minor damage. Probable cause: The mechanics failure to follow procedures and directives in securing the lower engine cowling after maintenance, and the failure of the first officer to follow the checklist to ensure the engine… ## Other aircraft with N904FR - [Cancelled 1993-03-16](https://openairdocs.org/deregistered/N904FR-1993-03-16): Dassault/Sud FAN JET FALCON, S/N 151. Exported to United Kingdom. Owner: [Mercantile-Safe Dep Tr Co Trustee](https://openairdocs.org/faa-owner/MERCANTILE-SAFE%20DEP%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.