# N945FR: 2006 Airbus A319-112, registration cancelled 2013-07-02 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 2, 2013 - Exported to: Bermuda - Status when cancelled: Valid registration - Airframe: [Airbus A319-112](https://openairdocs.org/model/airbus-a319-112) (registry code 3940009) - 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: 2751 - Year built: 2006 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 3, 2009 - Certificate issued: April 21, 2006 - Last registry action: January 21, 2011 - Mode S code: AD2048 - Owner when cancelled: [Afs Investments 58 LLC](https://openairdocs.org/faa-owner/AFS%20INVESTMENTS%2058%20LLC) - Location: [Stamford, CT](https://openairdocs.org/faa-place/CT/Stamford) - Owner type: Corporation - Owner's area on the map: 41.0593° N, 73.5444° W: Placed by OpenAirDocs at the center of ZIP code 06902, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N945FR - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=945FR - Page: https://openairdocs.org/deregistered/N945FR-2013-07-02 From the FAA registry file of November 3, 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 A319-112: https://openairdocs.org/model/airbus-a319-112.md ## Service difficulty reports (20) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR F3LA2013031100837](https://openairdocs.org/sdr/F3LA2013031100837), Feb 24, 2013: LAMP. BURNED OUT. EMERGENCY EXIT SIGN AT L1 DOOR HAS BURNED OUT LAMP. R & R L1 EMERGENCY SIGN IAW AMM 33-51-13-020-050-C AND AMM 33-51-13-420-050-C. OPS CHECKED GOOD IAW AMM 33-5 - [SDR F3LA2013012400824](https://openairdocs.org/sdr/F3LA2013012400824), Jan 18, 2013: LINE. FAILED. DURING CRUISE FLIGHT LOST GREEN SYSTEMS HYD; GREEN SYS HYD INOPERATIVE. FOUND BROKEN HYD LINE AT RT MLG DOOR ACTUATOR. R & R AFT HYD LINE ON RT MLG DOOR ACTUATO - [SDR F3LA2012122800822](https://openairdocs.org/sdr/F3LA2012122800822), Dec 23, 2012: CONTROL UNIT. INOPERATIVE. AIRCRAFT BEING POWERED BY APU. ALL DROPPED OFF WITH APU STILL INDICATING AVAILABLE - STRONG ODOR OF ELECTRICAL SMOKE IN COCKPIT. R & R GAPCU-(GROUND AUX POWER C - [SDR F3LA2012042300747](https://openairdocs.org/sdr/F3LA2012042300747), Apr 23, 2012: SILL. CORRODED. C-CHECK: FWD CARGO EIGHT INCHES AFT OF FRAME 27 DOOR SILL WEB HAS LIGHT SURFACE CORROSION. BLENDED AREA AND FOUND TO BE WITHIN LIMITS IAW SRM 51-73-00, PAR 5.F - [SDR F3LA2012041800745](https://openairdocs.org/sdr/F3LA2012041800745), Apr 16, 2012: SILL. CORRODED. C-CHECK: MAIN CABIN FRAME 66 AT L2 DOOR, DOOR SILL BEAM HAS CORROSION AT FASTENER HOLE. REPAIRED IAW SRM 53-41 -14 PB201 . - [SDR F3LA2012041800744](https://openairdocs.org/sdr/F3LA2012041800744), Apr 16, 2012: FLOORBEAM. CORRODED. C-CHECK: MAIN CABIN FLOORBEAM AT FRAME 68 Y765 HAS CORROSION. R & R FLOORBEAM IAW SRM 51-42-11 PARA 5. - [SDR F3LA2012041800743](https://openairdocs.org/sdr/F3LA2012041800743), Apr 16, 2012: FLOORBEAM. CORRODED. C-CHECK: MAIN CABIN FLOORBEAM AT FRAME 68 -Y1292 AFT OF SPLICE HAS LIGHT SURFACE CORROSION. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5. - [SDR F3LA2012041800742](https://openairdocs.org/sdr/F3LA2012041800742), Apr 16, 2012: FLOORBEAM. CORRODED. C-CHECK: MAIN CABIN FLOORBEAM AT FRAME 68 -Y1292 FWD OF SPLICE HAS LIGHT SURFACE CORROSION. R & R FLOORBEAM IAW SRM 51-42-11, PARAGRAPH 5. - [SDR F3LA2010122000570](https://openairdocs.org/sdr/F3LA2010122000570), Dec 17, 2010: PLATE. CORRODED. C-CHECK: NON ROUTINE N0596; FR69-70 SHEAR WEB PLATE HAS CORROSION AROUND FASTNER HOLES AND IS OLD CONFIGURATION. FOUND TO BE OUT OF LIMITS. REPLACED SHEAR WEB P - [SDR F3LA2010122000569](https://openairdocs.org/sdr/F3LA2010122000569), Dec 17, 2010: SHEAR TIE. CORRODED. C-CHECK: NON ROUTINE N0595; LT MAIN CABIN SHEAR PLATE HAS CORRORION AROUND FASTENER HOLES. SHEAR PLATE IS UNMODIFIELD TYPE ACFT IS IN C-CHECK. REPLACED THE SHEA - [SDR F3LA2010122000568](https://openairdocs.org/sdr/F3LA2010122000568), Dec 17, 2010: SILL. CORRODED. C-CHECK: NON ROUTINE N0484; R2 DOOR SILL HAS 3 SQ INCHES OF CORROSION AROUND AFT GIRT BAR FITTING. FOUND TO BE OUT OF LIMITS. REPLACED THE R2 DOOR SILL IAW SRM - [SDR F3LA2010122000567](https://openairdocs.org/sdr/F3LA2010122000567), Dec 17, 2010: SPLICE. CORRODED. C-CHECK: NON ROUTINE N0438; LT FLOORBEAM, Y1292 SPLICE COUPLING AT FRAME 66L HAS 2 INCHES OF CORROSION. CORROSION IS OUT OF LIMITS. REPLACED SPLICE COUPLING AT - [SDR F3LA2010122000565](https://openairdocs.org/sdr/F3LA2010122000565), Dec 17, 2010: FLOORBEAM. CORRODED. C-CHECK: NON ROUTINE N0436; LT FLOORBEAM, Y1292 AT FRAME 68L HAS A 2 SQ. INCHES OF CORROSION ON THE UPPER AND LOWER SIDERS. CORROSION IS OUT OF LIMITS. REPLACED - [SDR F3LA2010122000563](https://openairdocs.org/sdr/F3LA2010122000563), Dec 17, 2010: FLOOR PANEL. CHAFED. C-CHECK: NON ROUTINE N0399; AFT CARGO PANEL 151VG AFT EDGE IS WORN THROUGH TOP PLY. AREA IS 10 SQ INCHES. DAMAGE IS OUT OF LIMITS. FABRICATED REPLACEMENT PANEL - [SDR F3LA2010110800535](https://openairdocs.org/sdr/F3LA2010110800535), Nov 3, 2010: THERMOSTAT. DEFECTIVE. LOST BLEED NR1 AT 36,000 CAUSING CABIN PRESSURE EXCESS CABIN ALTITUDE. EMERGENCY WAS DECLARE AND DECENTED TO 10,000. FOUND THERMOSTAT DEFECTIVE, R & R THE THERM - [SDR F3LA2010063000444](https://openairdocs.org/sdr/F3LA2010063000444), Jun 27, 2010: UNKNOWN. ARCED. UPON ENGINE SHUTDOWN BRIGHT ARCHING FROM AFT CIRCUIT BREAKER PANEL WITH LOUD BANG FROM WITHIN CIRCUIT BREAKER PANEL. ALSO PUFF OF SMOKE. PERFORMED TSM PROCESS R - [SDR F3LA2009051300086](https://openairdocs.org/sdr/F3LA2009051300086), May 9, 2009: SERVO CONTROL. FAULTED. IN DEN, AIRCRAFT RETURNED TO BLOCK DUE TO NR 1 ELEVATOR AILERON COMPUTER PITCH FAULT DURING FLIGHT CONTROL CHECK. MAINTENANCE REMOVED AND REPLACED THE LEFT OUTB - [SDR F3LA200700283](https://openairdocs.org/sdr/F3LA200700283), Oct 12, 2007: LANYARD. MISSING. DURING C-1 CHECK, INSPECTION REPORTED RT OVERWING EMERGENCY ESCAPE SLIDE RELEASE CABLE FAILED TO RETRACT DURING MANUAL RELEASE TEST. REMOVED AND REPLACED PULL C - [SDR F3LA200700282](https://openairdocs.org/sdr/F3LA200700282), Oct 12, 2007: LANYARD. MISSING. DURING C-1 CHECK, INSPECTION REPORTED LT OVERWING EMERGENCY ESCAPE SLIDE LOWER ACTUATING CABLE WAS MISSING THE LOWER END PIECE TO ATTACH TO THE SLIDE RELEASE BO - [SDR F3LA200700010](https://openairdocs.org/sdr/F3LA200700010), Jan 22, 2007: BUSHING. OUT OF ADJUST. R1 DOOR WOULD NOT LATCH IN OPEN POSITION. RESEATED BUSHING UNDER PUSHBUTTON. PERFORMED OPS CHECK IAW AMM 52-10-00, PAGE 201. CHECKED GOOD. INSPECTED R1 DOOR GUS ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20101102050499I](https://openairdocs.org/incident/20101102050499I), Nov 2, 2010: Airbus A319-112 (N945FR), Denver, CO, No damage. On F3LA log page 581559 pilot reported with APU bleed on, a hissing was heard coming from the nr 2 engine cowl. This lead to deferral of nr 2 fan air valve per… --- 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.