# N908FR: 2002 Airbus A319-111, registration cancelled 2016-03-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 21, 2016 - Exported to: Austria - 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: 1759 - Year built: 2002 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 17, 2002 - Certificate issued: June 18, 2002 - Last registry action: December 19, 2015 - Mode S code: AC8D71 - Owner when cancelled: [Afs Investments Xvi LLC](https://openairdocs.org/faa-owner/AFS%20INVESTMENTS%20XVI%20LLC) - Location: [Norwalk, CT](https://openairdocs.org/faa-place/CT/Norwalk) - Owner type: Corporation - Owner's area on the map: 41.1382° N, 73.4016° W: Placed by OpenAirDocs at the center of ZIP code 06851, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N908FR - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=908FR - Page: https://openairdocs.org/deregistered/N908FR-2016-03-21 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 A319-111: https://openairdocs.org/model/airbus-a319-111.md ## Service difficulty reports (83, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR F3LA2015121801155](https://openairdocs.org/sdr/F3LA2015121801155), Dec 16, 2015: FLOORBEAM. CORRODED. AIRCRAFT DUE C 9 CHECK. MAIN CABIN FLOORBEAM HAS CORROSION 5" AFT OF FRAME 66, & 10" INBD OF Y765. CORRODED AREA FOUND TO HAVE OVER 50% MATERIAL LOSS. R & R FLO - [SDR F3LA2015103001151](https://openairdocs.org/sdr/F3LA2015103001151), Oct 27, 2015: CONTROLLER. DEFECTIVE. FIRST OFFICERS WINDOW HEAT & WINDSHIELD HEAT ECAM. R & R WINDOW HEAT CONTROLLER 2DG2. OPERATIONAL CHECK & BITE TESTED GOOD IAW AMM 30-42-34 PB401. REFERENCE LP - [SDR F3LA2014123001096](https://openairdocs.org/sdr/F3LA2014123001096), Dec 23, 2014: BATTERY PACK. DISCHARGED. EPSU EMER LIGHT BATTERY 10WL, FWD LT, FAILED CAPACITY TEST AT A CHECK. R & R BATTERY ASSEMBLY IAW AMM 33-51-36-000-002A & 33-51-36-400-002A. - [SDR F3LA2013121700950](https://openairdocs.org/sdr/F3LA2013121700950), Dec 14, 2013: RIB. CRACKED. AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. WHILE CLEANING AREA TECHNICIAN FOUND INBD LE RIB, AT SLAT TRACK 12, CRACKED BETWEEN TWO FASTENER HOLES. R & R SLAT T - [SDR F3LA2013121700949](https://openairdocs.org/sdr/F3LA2013121700949), Dec 11, 2013: SKIN. DELAMINATED. AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. RT ELEVATOR THERMO GRAPHIC INSPECTION REVEALED 9 EACH INDICATIONS, BETWEEN UPPER & LOWER PANELS, THAT ARE IRREGULAR - [SDR F3LA2013121700948](https://openairdocs.org/sdr/F3LA2013121700948), Dec 11, 2013: SKIN. DELAMINATED. AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. RT ELEVATOR THERMO GRAPHIC INSPECTION REVEALED 1 EACH INDICATION RU9 ON UPPER PANEL THAT IS IRREGULAR IN SHAPE & BLA - [SDR F3LA2013121700946](https://openairdocs.org/sdr/F3LA2013121700946), Dec 11, 2013: FLOORBEAM. CORRODED. AIRCRAFT OUT OF SERVICE FOR C8 S2 CHECK. AFT CABIN FLOOR BEAM, FWD OF L2 DOOR AT FR 67, HAS CORROSION. DETERMINED CORROSION TO BE OUT OF LIMITS. R & R AFT CABIN - [SDR F3LA2013121700947](https://openairdocs.org/sdr/F3LA2013121700947), Dec 9, 2013: SKIN. DELAMINATED. AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. LT ELEVATOR THERMO GRAPHIC INSPECTION REVEALED 12 INDICATIONS ON UPPER PANEL THAT ARE IRREGULAR IN SHAPE & BLACK IN - [SDR F3LA2013121700945](https://openairdocs.org/sdr/F3LA2013121700945), Nov 25, 2013: FLOORBEAM. CORRODED. AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. AFT CABIN RT AFT LAVATORY ATTACHMENT POINT HAS MINOR CORROSION ON FLOOR BEAM. R & R FLOOR BEAM IAW SRM 51-42-11 PARA - [SDR F3LA2013121700944](https://openairdocs.org/sdr/F3LA2013121700944), Nov 24, 2013: SHEAR PLATE. CORRODED. AIRCRAFT IS OUT OF SERVICE DUE TO C8 S2 CHECK. AFT CABIN LT LATERAL SHEAR PLATE HAS CORROSION BETWEEN FR 69 - FR 70, STRINGER 23. R & R LT SHEAR PLATE IAW SRM 5 - [SDR F3LA2013121700943](https://openairdocs.org/sdr/F3LA2013121700943), Nov 24, 2013: SHEAR PLATE. CORRODED. AIRCRAFT IS OUT OF SERVICE DUE TO C8 S2 CHECK. AFT CABIN RT LATERAL SHEAR PLATE HAS CORROSION BETWEEN FR 69 - FR 70, STRINGER 23. R & R RT SHEAR PLATE IAW SRM 5 - [SDR F3LA2013121700942](https://openairdocs.org/sdr/F3LA2013121700942), Nov 19, 2013: SILL. CORRODED. AIRCRAFT IS OUT OF SERVICE DUE TO C8 S2 CHECK. DOT 086, 023 SILL FRAME IN FWD BAG PIT HAS CORROSION, DOOR SILL. REMOVED LIGHT SURFACE CORROSION FROM FWD DOOR SI - [SDR F3LA2013121700941](https://openairdocs.org/sdr/F3LA2013121700941), Nov 17, 2013: THRESHOLD. CORRODED. AIRCRAFT IS OUT OF SERVICE DUE TO C8 S2 CHECK. FWD CARGO COMPARTMENT THRESHOLD WEB FWD OF FRAME 26 RT HAS SURFACE CORROSION AT NUTPLATE UPPER & LOWER SURFACES. - [SDR F3LA2012110600808](https://openairdocs.org/sdr/F3LA2012110600808), Nov 2, 2012: ENGINE. LEAKING. SMOKE IN THE CABIN, AIR RETURN TO DEPARTURE. BORESCOPED LT AND RT ENGINES, FOUND OIL WETTING IN RT ENGINE. R & R ENGINE. - [SDR F3LA2012080100776](https://openairdocs.org/sdr/F3LA2012080100776), Aug 1, 2012: LIGHT. INOPERATIVE. EMERGENCY LIGHT ON SEAT 15 ABC INOPERATIVE. R & R ROW 15 ABC EMERGENCY SEAT LIGHT IAW AMM 33·51·19 PB 401. OPS CHECKED GOOD. - [SDR F3LA2012061400770](https://openairdocs.org/sdr/F3LA2012061400770), Jun 13, 2012: FILTER. CONTAMINATED. BLOCK TURN BACK OILY SMELL IN CABIN AFTER TAXI OUT. RAN BOTH ENGINES AND APU WITH AIR CONDITIONING PACKS FULL HOT AND FULL COLD TO VENT AIR CONDITIONING SYS. R - [SDR F3LA2012053000763](https://openairdocs.org/sdr/F3LA2012053000763), May 29, 2012: BATTERY. DISCHARGED. EMERGENCY LIGHT POWER SUPPLY BATTERY 11WL FAILED TEST AT HEAVY SERVICES CHECK. R & R BATTERY UNIT IAW 33-51-38-000-002A AND 33-51-38-400-002A, UNIT CHECK NORMAL - [SDR F3LA2012052300760](https://openairdocs.org/sdr/F3LA2012052300760), May 21, 2012: BATTERY PACK. FAILED. DURING C-CHECK, AFT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM 33-51-38. OPS CHECKED GOOD. - [SDR F3LA2011012800596](https://openairdocs.org/sdr/F3LA2011012800596), Jan 25, 2011: FLOORBEAM. CORRODED. C-CHECK: NON ROUTINE N305; CABIN FLOORBEAM Y1292 BETWEEN FRAMES 66 AND 68 HAS 3 AREAS OF EXFLOTATION. R & R FLOORBEAM Y1292 AT FRAME 66 TO 68 IAW SRM 51-42-11 P - [SDR F3LA2011012800595](https://openairdocs.org/sdr/F3LA2011012800595), Jan 25, 2011: FLOOR PANEL. DELAMINATED. C-CHECK: NON ROUTINE N403; AFT CARGO BAY PANEL FOR LIVETV ON THE FLOOR PANEL 161EF HAS DELAMINATION AND SKIN DAMAGE AT CORNER. FABRICATED REPLACEMENT PANEL 161E - [SDR F3LA2011012800593](https://openairdocs.org/sdr/F3LA2011012800593), Jan 24, 2011: NUT. LOOSE. C-CHECK: NON ROUTINE N0743; PAX DOOR R1 ESCAPE SLIDE WOULD NOT ARM PROPERLY. FOUND SEALING NUT OUT OF FLEXIABLE CONTROL UPPER END. - [SDR F3LA2011012800592](https://openairdocs.org/sdr/F3LA2011012800592), Jan 24, 2011: NUT. LOOSE. C-CHECK: NON ROUTINE N0742; PAX DOOR L1 ESCAPE SLIDE WOULD NOT ARM PROPERLY. FOUND SEALING NUT OUT OF FLEXIABLE CONTROL UPPER END. RETORQUED SEALING NUT IAW AMM - [SDR F3LA2011012800591](https://openairdocs.org/sdr/F3LA2011012800591), Jan 24, 2011: POWER SUPPLY. INOPERATIVE. C-CHECK: NON ROUTINE N0707; DURING EMERGENCY LIGHT TEST, SEATS 19, 21, 23 AND AFT OVERHEAD EMERGENCY LIGHTS FLASHED. R & R EPSU 13WL IAW AMM 33-51-38 PB 401. PE - [SDR F3LA2011012800590](https://openairdocs.org/sdr/F3LA2011012800590), Jan 24, 2011: PLATE. CORRODED. C-CHECK: NON ROUTINE N0539; LT SHEAR PLATE BETWEEN FRAMES 69L TO 70L HAS 1 SQUARE INCH CORROSION AND IS THE OLD CONFIGURATION. R & R SHEAR PLATE WITH NEW CONFIG - [SDR F3LA2011012800589](https://openairdocs.org/sdr/F3LA2011012800589), Jan 24, 2011: PLATE. CORRODED. C-CHECK: NON ROUTINE N0538; MAIN CABIN RT SIDE FROM FRAME 69 TO FRAME 70 SHEAR PLATE HAS 6 SQUARE INCHES OF CORROSION. R & R SHEAR PLATE AT FRAME 69 TO 70 IAW S - [SDR F3LA2011012800588](https://openairdocs.org/sdr/F3LA2011012800588), Jan 24, 2011: FLOORBEAM. CORRODED. C-CHECK: NON ROUTINE N0319; FLOORBEAM -Y1292 BETWEEN FRAMES 67.5 AND 68 HAS 2 HOLES WITH CORROSION OUT OF LIMITS IAW SRM 53-00-14, FIG 102. R & R FLOORBEAM -Y12 - [SDR F3LA2011012800587](https://openairdocs.org/sdr/F3LA2011012800587), Jan 24, 2011: FLOORBEAM. CORRODED. C-CHECK: NON ROUTINE N0316; CABIN FLOORBEAM Y1292 AT FRAME 68, 3 INCHES FORWARD OF THE FRAME HAS A 0.5 INCH X 0.5 INCH AREA OF CORROSION. R & R FLOORBEAM IAW SR - [SDR F3LA2010012800321](https://openairdocs.org/sdr/F3LA2010012800321), Jan 24, 2010: OVEN. ODOR. THE FLIGHT CREW REPORTED A BURNING ODOR COMING FROM THE NR 2 OVEN. THE CIRCUIT BREAKER WAS PULLED AND MX DEFERRED THE NR 2 OVEN IAW NEF 25-99-30AE. - [SDR F3LA2009070700098](https://openairdocs.org/sdr/F3LA2009070700098), Jul 3, 2009: TRANSPONDER. FAILED. DURING SCHEDULED MX TASK CARD TC34210-07, ATC TRANSPONDER NR 2 FAILED FUNCTIONAL TEST. MX REMOVED AND REPLACED THE NR 2 ATC TRANSPONDER AND PERFORMED BITE TEST, - [SDR F3LA2009062200091](https://openairdocs.org/sdr/F3LA2009062200091), Jun 20, 2009: SERVO CONTROL. FAULTED. AIRCRAFT RETURNED TO BLOCK IN DEN DUE TO NR 1 ELAC (ELEVATOR AILERON COMPUTER) FAULT. MAINTENANCE REMOVED AND REPLACED THE RIGHT BLUE SYSTEM ELEVATOR SERVO AND - [SDR F3LA2009062200090](https://openairdocs.org/sdr/F3LA2009062200090), Jun 17, 2009: POWER SUPPLY. FAILED. DURING C5 C-CHECK, INSPECTION NOTED THAT RIGHT OVERWING EXIT ARM LIGHT FAILED OPERATIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT - [SDR F3LA200700342](https://openairdocs.org/sdr/F3LA200700342), Nov 27, 2007: SEAT TRACK. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED SEAT TRACK FLOORBEAM +Y1292 FROM FR 64 TO 4 INCHES AFT OF FR 66 CORRODED AT NUTPLATE HOLES. FOUND CORROSION TO BE OUT OF - [SDR F3LA200700341](https://openairdocs.org/sdr/F3LA200700341), Nov 27, 2007: ATTACH BOLT. CRACKED. DURING C4/S1 CHECK, INSPECTION REPORTED RUDDER ATTACH FITTING NR 7 ATTACHMENT BOLT CRACKED AROUND CENTER CIRCUMFERENCE AREA. REMOVED AND REPLACED HARDWARE IAW A - [SDR F3LA200700340](https://openairdocs.org/sdr/F3LA200700340), Nov 27, 2007: SILL. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED L2 DOOR SILL CORRODED AT NUTPLATE HOLES UNDER FWD L2 GIRT BAR FITTING/PLATE AREA, JUST AFT OF FR66. CORROSION WAS FOUND - [SDR F3LA200700339](https://openairdocs.org/sdr/F3LA200700339), Nov 27, 2007: FAIRING. CRACKED. DURING C4/S1 CHECK, INSPECTION REPORTED NR 1 ENGINE FAN OUTLET FAIRING INSTALLATION HAD CRACKS AT THE 7 O'CLOCK AND 9 O'CLOCK POSITIONS. REMOVED AND REPLACED NR - [SDR F3LA200700328](https://openairdocs.org/sdr/F3LA200700328), Nov 27, 2007: BOLT. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED ONE BOLT FOR FLOOR HOLD DOWN ON LAVATORY E CORRODED. REMOVED AND REPLACED CORRODED BOLT IAW AMM 25-43-42-100-001. - [SDR F3LA200700325](https://openairdocs.org/sdr/F3LA200700325), Nov 26, 2007: ATTACH BOLT. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED RT AILERON NR 3 HINGE SUPPORT FRAME ATTACHMENT BOLTS (ATTACHES TO BRACKET ON WING) WORN AND CORRODED. REPLACED RT AILERO - [SDR F3LA200700338](https://openairdocs.org/sdr/F3LA200700338), Nov 17, 2007: MOUNT. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED TWO CORRODED FASTENERS IN THE R2 AFT GIRT BAR MOUNT PLATE. BLENDED OUT CORROSION ON OTBD MIDDLE FASTENER HOLE, BOTTOM SI - [SDR F3LA200700351](https://openairdocs.org/sdr/F3LA200700351), Nov 15, 2007: SILL. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON R2 DOOR SILL, FWD SPLICE JUST FWD OF FR66. REMOVED SPLICES AND RE-MEASURED AREA. SUBMITTED EAR FOR APPROVAL - [SDR F3LA200700343](https://openairdocs.org/sdr/F3LA200700343), Nov 15, 2007: STRUCTURE. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED CONNECTING SECTION ASSY (BROWN PIECE THAT GOES UNDER THE FLOOR PANEL AND UP THE SIDE OF THE FLOOR PANEL) CORRODED AT FR6 - [SDR F3LA200700337](https://openairdocs.org/sdr/F3LA200700337), Nov 15, 2007: FLOOR SUPPORT. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED FRAME SUPPORT CORRODED AT FR 69-70, -Y1732. REMOVED AND INSTALLED REPLACEMENT FRAME SUPPORT IAW SRM 51-42-11. - [SDR F3LA200700354](https://openairdocs.org/sdr/F3LA200700354), Nov 14, 2007: BLANKING PLATE. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED L2 DOOR AFT GIRT BAR BRACKET CORRODED AROUND ATTACH POINTS. REMOVED AND REPLACED GIRT BAR BLANKING PLATE IAW AMM 52-11-3 - [SDR F3LA200700353](https://openairdocs.org/sdr/F3LA200700353), Nov 14, 2007: BLANKING PLATE. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION AROUND L2 DOOR FWD GIRT BAR ATTACH BRACKET MOUNTING HOLES. REMOVED AND REPLACED GIRT BAR BLANKING PLATE IAW AM - [SDR F3LA200700350](https://openairdocs.org/sdr/F3LA200700350), Nov 14, 2007: FITTING. CRACKED. DURING C4/S1 CHECK, INSPECTION REPORTED CRACK IN HOLE H4 ON THE NLG FITTING MOD (EO NR A0-53EO-20373, REV. B). UPSIZED HOLE FROM .277 TO .309 AND RE-INSPECTED H - [SDR F3LA200700349](https://openairdocs.org/sdr/F3LA200700349), Nov 14, 2007: FLOORBEAM. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED NUTPLATE HOLES CORRODED ON FLOORBEAM +Y1292 (LT), 4 INCHES FWD OF FR68. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11, - [SDR F3LA200700348](https://openairdocs.org/sdr/F3LA200700348), Nov 14, 2007: SILL. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED R2 DOOR SILL CORRODED IN TWO AREAS AFT OF INBD AFT NUTPLATE HOLE LOCATED 1.5 INCHES AND 2.5 INCHES AFT. REPAIRED CORRODE - [SDR F3LA200700347](https://openairdocs.org/sdr/F3LA200700347), Nov 14, 2007: SILL. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON R2 DOOR SILL, INBD AFT TWO NUTPLATE HOLES AND NUTPLATE HOLE LOCATED OTBD AND AFT OF FWD GIRT BAR FITTING ON - [SDR F3LA200700346](https://openairdocs.org/sdr/F3LA200700346), Nov 14, 2007: FLOORBOARD. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBOARD 261FF CORRODED. REMOVED AND REPLACED FLOORBOARD 261FF IAW AMM 53-32-12-400-002. - [SDR F3LA200700344](https://openairdocs.org/sdr/F3LA200700344), Nov 14, 2007: STRAP. CORRODED. DURING C-4/S1 CHECK, INSPECTION REPORTED PANEL 262EF TIE-DOWN STRAP CORRODED. REPLACED AFT TIE-DOWN STRAP ON PANEL 262EF IAW AMM 53-32-12-400-002. - [SDR F3LA200700336](https://openairdocs.org/sdr/F3LA200700336), Nov 14, 2007: SHEAR PLATE. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED LT AFT SHEAR PLATE CORRODED AT FR 69-70 AT BEAM +1732 (APPROX). REMOVED AND INSTALLED LT AFT SHEAR PLATE IAW SRM'S 51-72 All 83: https://openairdocs.org/deregistered/N908FR-2016-03-21/reports.md ## Other aircraft with N908FR - [Cancelled 1993-07-09](https://openairdocs.org/deregistered/N908FR-1993-07-09): Dassault/Sud FAN JET FALCON, S/N 207. 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.