# N936FR: 2005 Airbus A319-111, registration cancelled 2012-11-06 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 6, 2012 - Exported to: Belgium - 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: 2392 - Year built: 2005 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 9, 2005 - Certificate issued: February 8, 2005 - Last registry action: July 9, 2010 - Mode S code: ACFC80 - 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: 41.0593° 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/N936FR - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=936FR - Page: https://openairdocs.org/deregistered/N936FR-2012-11-06 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 (27) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR F3LA2011101800685](https://openairdocs.org/sdr/F3LA2011101800685), Oct 14, 2011: SOLENOID VALVE. FAILED. A/C PACK 2 FAILED IN FLIGHT. PACK 1 ON MEL SO PACK 2 FAIL CAUSED A CABIN DEPRESSURIZATION AND 02 MASK TO DEPLOY. R & R PRESSURE REGULATOR VALVE SOLENOID 10HA2 I - [SDR F3LA2011032100616](https://openairdocs.org/sdr/F3LA2011032100616), Mar 16, 2011: SERVO. SLOW. ON ROTATION ACFT ROLLS RT REGARDLESS OF WIND. PERFORMED FLT CONTROL MOVEMENT CHECKS FOUNFD LT ELEVATOR SERVO SLOW TO REACT. REF LP 596444, ITEM 1, R & R SERVO C - [SDR F3LA2011022100607](https://openairdocs.org/sdr/F3LA2011022100607), Feb 17, 2011: COMPUTER. MALFUNCTIONED. AT LIFT OFF, AN UNCOMMANDED ACFT ROLLED RT. AT TOUCHDOWN, AT SPEEDBRAKE DEPLOYMENT, ACFT AGAIN ROLLED RT AND REQUIRED SIGNIFICANT LT AILERON INPUT TO KEEP LT ML - [SDR F3LA2011011800585](https://openairdocs.org/sdr/F3LA2011011800585), Jan 7, 2011: SILL. CORRODED. L2 DOOR SILL BEAM HAS 3 SQ INCH OF CORROSION AND IS OUT OF LIMITS. R & R L2 DOOR SILL BEAM IAW SRM 51-72-11, PG 1-2. - [SDR F3LA2011011800584](https://openairdocs.org/sdr/F3LA2011011800584), Jan 7, 2011: SILL. CORRODED. R2 DOOR SILL BEAM HAS 1 SQ INCH OF CORROSION AND IS OUT OF LIMITS. R & R R2 DOOR SILL BEAM IAW SRM 51-72-11 PG 1-2. - [SDR F3LA2011011800583](https://openairdocs.org/sdr/F3LA2011011800583), Jan 7, 2011: SHEAR PLATE. CORRODED. LT SHEAR PLATE BETWEEN FRAMES 69 TO 70 HAS 3 SQ INCHES OF CORROSION AND IS OLD CONFIGURATION. R & R SHEAR PLATE WITH NEW CONFIGURATION IAW EO AO-53EO-31434. - [SDR F3LA2011011800582](https://openairdocs.org/sdr/F3LA2011011800582), Jan 7, 2011: SHEAR PLATE. CORRODED. RT SHEAR PLATE BETWEEN FRAMES 69 TO 70 HAS 8 SQ INCHES OF CORROSION AND IS OLD CONFIGURATION. R & R SHEAR PLATE WITH NEW CONFIGURATION IAW EO AO53EO31434. - [SDR F3LA2011011800581](https://openairdocs.org/sdr/F3LA2011011800581), Jan 7, 2011: SHOCK ABSORBER. SCRATCHED. LT MLG SHOCK ABSORBER SCRATCHED IN CHROME AREA. 60 TO 80 SCRATCHES 18 INCHES LONG X .003 INCHES DEEP ON FWD SIDE OF STRUT. R & R LT MLG SHOCK ABSORBER IAW AMM 3 - [SDR F3LA2011010600580](https://openairdocs.org/sdr/F3LA2011010600580), Jan 6, 2011: FLOOR PANEL. PUNCTURED. C-CHECK: NON ROUTINE N0665; AFT CARGO COMPARTMENT FLOOR PANEL 151AE HAS 3 EACH PUNCTURES. REPAIRED 3 EACH PUNCTURES WITH WET LAYUP IAW SRM 53-02-00, PARA 8B. - [SDR F3LA2011010600579](https://openairdocs.org/sdr/F3LA2011010600579), Jan 6, 2011: FLOOR PANEL. PUNCTURED. C-CHECK: NON ROUTINE N0660; AFT CARGO COMPARTMENT FLOOR PANEL 151DE HAS 2 EA PUNCTURES. REPAIRED 2 EACH PUNCTURES IAW SRM 53-02-00, PARA 8B. - [SDR F3LA2011010600578](https://openairdocs.org/sdr/F3LA2011010600578), Jan 6, 2011: FLOOR PANEL. PUNCTURED. C-CHECK: NON ROUTINE N0659; AFT CARGO COMPARTMENT FLOOR PANEL 152TG HAS 1 INCH PUNCTURE. REPAIRED PUNCTURE WITH WET LAYUP REPAIR IAW SRM 53-02-00, PARA 8B. - [SDR F3LA2011010600577](https://openairdocs.org/sdr/F3LA2011010600577), Jan 6, 2011: FLOORBOARD. PUNCTURED. C-CHECK: NON ROUTINE NR N0657; AFT CARGO COMPARTMENT FLOOR PANEL 162CF PUNCTURED. REPAIR PUNCTURE WITH WET LAYUP REPAIR IAW SRM 53-02-00, PARA 8B. - [SDR F3LA2011010600576](https://openairdocs.org/sdr/F3LA2011010600576), Jan 6, 2011: FLOOR PANEL. DELAMINATED. C-CHECK: NON ROUTINE N0644; CABIN FLOOR PANEL 242BF DELAMINATED. REPAIRED 56 SQUARE INCHES OF DEBONDED TOP GLASS LAYER OF PANEL 242BF USING MYLAR FOIL IAW SRM 5 - [SDR F3LA2011010600575](https://openairdocs.org/sdr/F3LA2011010600575), Jan 6, 2011: SKIN. GOUGED. C-CHECK: NON ROUTINE N0633; NR 2 ENGINE OTBD THRUST REVERSER LOWER BLOCKER INTERNAL SIDE THE PERFORATED SKIN HAS A GOUGE MEASURING .7500 INCH LONG, .2500 INCH W - [SDR F3LA2011010600574](https://openairdocs.org/sdr/F3LA2011010600574), Jan 6, 2011: COWL DOOR. DENTED. C-CHECK: NON ROUTINE NR N0636; NR 2 ENGINE OTBD THRUST REVERSERS INNER PERFORATED COWL BELOW THE UPPER BLOCKER DOOR THERE IS A DENT MEASURING .1250 INCH CIRCUMF - [SDR F3LA2011010600573](https://openairdocs.org/sdr/F3LA2011010600573), Jan 6, 2011: FLOOR PANEL. DAMAGED. C-CHECK: NON ROUTINE NR N0282; AFT CARGO FLOOR PANEL 152WG DAMAGED, SKIN SEPARATED FROM HONEYCOMB. FABRICATED REPLACEMENT PANEL IAW IRM 9701, REV G. - [SDR F3LA2011010600572](https://openairdocs.org/sdr/F3LA2011010600572), Jan 6, 2011: FLOORBOARD. DAMAGED. C-CHECK: NON ROUTINE N0278; MAIN CABIN FLOORBOARD 252NF HAS COMPOSITE DAMAGE DAMAGE 40 SQUARE INCHES. REPAIRED 40 SQUARE OF COMPOSITE DAMAGE, IAW A319 SRM 53-02 - [SDR F3LA2009071700106](https://openairdocs.org/sdr/F3LA2009071700106), Jul 14, 2009: FLOOR PANEL. CRACKED. REF: NON ROUTINE C064113. DURING C3 C-CHECK, INSP NOTED THE L2 DOOR FWD SIDE FLOOR PANEL IS CRACKED. MX REMOVED AND REPLACED THE FWD L2 DOOR BLANKING PLATE IAW - [SDR F3LA2009071700105](https://openairdocs.org/sdr/F3LA2009071700105), Jul 12, 2009: FLOORBEAM. CORRODED. DURING C3 C-CHECK, INSP NOTED CORROSION IN AND AROUND NUT CLIP HOLES ON FLOORBEAM Y1292 RT, BETWEEN FR 66 AND FR 68. CORROSION WAS FOUND BEYOND SRM LIMITS. MX R - [SDR F3LA2009071700104](https://openairdocs.org/sdr/F3LA2009071700104), Jul 12, 2009: FLOORBEAM. CORRODED. DURING C3 C-CHECK, INSP NOTED CORROSION IN AND AROUND NUT CLIP HOLES ON FLOORBEAM Y1292 LT, BETWEEN FRAME 66 AND FRAME 68. CORROSION WAS FOUND BEYOND SRM LIMITS - [SDR F3LA2009071500103](https://openairdocs.org/sdr/F3LA2009071500103), Jul 12, 2009: SHEAR PLATE. CORRODED. DURING C3 C-CHECK, INSP NOTED THAT RT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 AT STR 23 RT SHOWS EVIDENCE OF CORROSION AROUND NUT CLIPS. MX REMOVED AND REPL - [SDR F3LA2009071500100](https://openairdocs.org/sdr/F3LA2009071500100), Jul 12, 2009: SUPPORT. CORRODED. DURING C3 C-CHECK, INSP NOTED THAT THE RT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 AT STR 23 RT, SHOWS EVIDENCE OF CORROSION AROUND NUT CLIPS. MX REMOVED AND - [SDR F3LA2009071500102](https://openairdocs.org/sdr/F3LA2009071500102), Jul 12, 2009: SHEAR PLATE. CORRODED. DURING C3 C-CHECK, INSP NOTED LT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 AT STR 23 LT SHOWS EVIDENCE OF CORROSION AROUND NUT CLIPS. MX REMOVED AND REPLACED - [SDR F3LA2009071500101](https://openairdocs.org/sdr/F3LA2009071500101), Jul 12, 2009: SUPPORT. CORRODED. DURING C3 C-CHECK, INSP NOTED THE LT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 AT STR 23 LT SHOWS EVIDENCE OF CORROSION AROUND NUT CLIPS. MX REMOVED AND REPLA - [SDR F3LA2009072000107](https://openairdocs.org/sdr/F3LA2009072000107), Jul 11, 2009: STRUT. CHAFED. DURING C3 C-CHECK, INSP NOTED THE ELECTRICAL CABLE FOR THE TOWING BYPASS SWITCH WAS RUBBING ON THE NLG STRUT. MX REMOVED DAMAGE, PERFORMED FLUORESCENT PENETRANT - [SDR F3LA200700046](https://openairdocs.org/sdr/F3LA200700046), Mar 19, 2007: LIGHT. INOPERATIVE. MAINTENANCE REPORTED RT AFT EMERGENCY OVERWING OUTSIDE LIGHT (62WL) INOP. REPLACED LIGHT ASSY (62WL) IAW 33-51-15-400-001. - [SDR F3LA200600086](https://openairdocs.org/sdr/F3LA200600086), Jul 29, 2006: LIGHT. FAILED. EPSU TEST FAILED IAW HEAVY CHECK WORK CARD. REPLACED RT OVERWING EXIT HATCH HANDLE LIGHT IAW MM 23-73-47, PB 401 AND 33-51-11-420-052A, PERFORMED ANOTHER EPSU T --- 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.