# N807FR: 2004 Airbus A318-111, registration cancelled 2011-09-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 28, 2011 - Status when cancelled: Valid registration - Airframe: [Airbus A318-111](https://openairdocs.org/model/airbus-a318-111) (registry code 3940019) - 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: 2276 - Year built: 2004 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 26, 2004 - Certificate issued: October 25, 2004 - Last registry action: July 9, 2010 - Mode S code: AAFC6B - Owner when cancelled: [Afs Investments X LLC](https://openairdocs.org/faa-owner/AFS%20INVESTMENTS%20X%20LLC) - Location: [Stamford, CT](https://openairdocs.org/faa-place/CT/Stamford) - Owner type: Corporation - Owner's area on the map: 41.0534° N, 73.5387° W: Placed by OpenAirDocs: center of Stamford, CT, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N807FR - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=807FR - Page: https://openairdocs.org/deregistered/N807FR-2011-09-28 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 A318-111: https://openairdocs.org/model/airbus-a318-111.md ## Service difficulty reports (15) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR F3LA2009122900274](https://openairdocs.org/sdr/F3LA2009122900274), Dec 28, 2009: COVER. OUT OF POSITION. DURING CLIMB OUT, THE FLIGHT CREW RECEIVED SPURIOUS ECAM INDICATIONS RT DOOR EMERGENCY EXIT. MX REINSTALLED RT OVERWING EXIT HANDLE COVER FLAP AND ECAM INDICATI - [SDR F3LA2009021600027](https://openairdocs.org/sdr/F3LA2009021600027), Feb 16, 2009: CABLE. LACK OF LUBE. DURING C3 C-CHECK, INSPECTION NOTED THAT THE RIGHT OVERWING EMERGENCY SLIDE CABLE FAILED THE FUNCTIONAL TEST OF THE SLIDE RELEASE SIGNAL AND OPERATIONAL TEST OF - [SDR F3LA2009021600026](https://openairdocs.org/sdr/F3LA2009021600026), Feb 15, 2009: SILL. CORRODED. DURING C3 C-CHECK, INSPECTION NOTED CORROSION AT THE FASTENER HOLE OF THE AFT GIRT BAR FITTING, L2 DOOR THRESHOLD. MAINTENANCE REMOVED THE CORROSION. FABRICATED - [SDR F3LA2009021300025](https://openairdocs.org/sdr/F3LA2009021300025), Feb 11, 2009: FLOORBEAM. CORRODED. REFERENCE NON-ROUTINE C057562. DURING C3 C-CHECK, INSPECTION NOTED CORROSION ON FLOORBEAM -Y1292 BETWEEN FRAME 66 AND FRAME 68. MAINTENANCE REMOVED AND REPLACED - [SDR F3LA2008121600726](https://openairdocs.org/sdr/F3LA2008121600726), Dec 13, 2008: ISOLATION VALVE. CRACKED. ENROUTE AT FL330, PILOT REPORTED INDICATION OF HYDRAULIC RESERVOIR LOW LEVEL FOLLOWED BY ENGINE NR 2 PUMP LOW LEVEL AND NOTED THE YELLOW SYSTEM FLUID QUANTITY D - [SDR F3LA200800507](https://openairdocs.org/sdr/F3LA200800507), Jul 17, 2008: FLOOR PANEL. PUNCTURED. LINE MAINTENANCE NOTED THE AFT CARGO PIT TRANSITION PANEL 151FG HAS PUNCTURE DAMAGE IN THREE PLACES ON UPPER SKIN. MAINTENANCE REPAIRED DAMAGE IN ACCORDANCE WIT - [SDR F3LA200800506](https://openairdocs.org/sdr/F3LA200800506), Jul 17, 2008: FLOOR PANEL. PUNCTURED. LINE MAINTENANCE NOTED THE AFT CARGO PIT TRANSITION PANEL 151FH HAD PUNCTURE DAMAGE IN THREE PLACES ON THE UPPER SKIN. MAINTENANCE REPAIRED DAMAGE IN ACCORDANCE - [SDR F3LA200800077](https://openairdocs.org/sdr/F3LA200800077), Mar 3, 2008: COOLING FAN. BINDING. DURING CRUISE, AT 35000, FLT CREW REPORTED LOUD NOISE AND VIBRATION FOLLOWED BY ACRID ODOR AND SMOKE IN COCKPIT. ECAM DISPLAYED BLOWER AND EXTRACTOR FAN FAULT. - [SDR F3LA200700195](https://openairdocs.org/sdr/F3LA200700195), Aug 7, 2007: LINE. LEAKING. FLIGHT CREW REPORTED GREEN HYD QTY LOW IN CRUISE. PERFORMED LANDING GRAVITY EXTENSION PER FOM VOL II. REPLACED NR 1 ENGINE T/R ISOLATION VALVE PRESSURE HYDRAULI - [SDR F3LA200700177](https://openairdocs.org/sdr/F3LA200700177), Jul 12, 2007: FLOOR PANEL. PUNCTURED. DURING C-2 CHECK, INSPECTION REPORTED PUNCTURE ON TOPSIDE OF AFT CARGO COMPARTMENT FLOOR PANEL 161QF. REPAIRED AFT CARGO COMPARTMENT FLOOR PANEL 161QF IAW SRM 5 - [SDR F3LA200700176](https://openairdocs.org/sdr/F3LA200700176), Jul 12, 2007: FLOOR PANEL. DAMAGED. DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR PANEL 161QF DAMAGED. REPAIRED FLOOR PANEL 161QF IAW A318 SRM 53-02-00, FIG 204. - [SDR F3LA200700175](https://openairdocs.org/sdr/F3LA200700175), Jul 12, 2007: PANEL. PUNCTURED. DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT TRANSITION PANELS 151FH, 151HH, AND 162SF DAMAGED. REPAIRED PUNCTURES IN PANELS IAW A318 SRM 53-20-0 - [SDR F3LA200700174](https://openairdocs.org/sdr/F3LA200700174), Jul 12, 2007: PANEL. DAMAGED. DURING C-2 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT TRANSITION PANEL 131BF DAMAGED. REPAIRED PUNCTURE IAW A318 SRM 53-20-00, PB 201, PARA 8.C., FIG. 204 - [SDR F3LA200700031](https://openairdocs.org/sdr/F3LA200700031), Feb 16, 2007: WINDSHIELD. CRACKED. AIR TURN BACK, CAPTAIN'S FWD WINDSHIELD SHATTERED. REPLACED CAPTAINS FWD WINDSHIELD IAW 56-11-11, PB401. - [SDR F3LA200600088](https://openairdocs.org/sdr/F3LA200600088), Aug 15, 2006: FLAP SYSTEM. MALFUNCTIONED. ON APPROACH ECAM FLAPS LOCKED. FLAPS WOULD NOT EXTEND BEYOND F2, SLATS EXTEND NORMALLY. MAINTENANCE PERFORMED TROUBLESHOOTING PER TSM 27-51-00-810-818, OPERATIO --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). 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