# N930FR: 2004 Airbus A319-111, registration cancelled 2013-05-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 28, 2013 - Exported to: Bermuda - 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: 2241 - Year built: 2004 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 7, 2004 - Certificate issued: June 8, 2004 - Last registry action: August 10, 2011 - Mode S code: ACE636 - 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/N930FR - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=930FR - Page: https://openairdocs.org/deregistered/N930FR-2013-05-28 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 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 F3LA2012041900746](https://openairdocs.org/sdr/F3LA2012041900746), Apr 18, 2012: TRANSDUCER. DEFECTIVE. ELAC 2 FAULT (UNCOMMANDED PITCH +/··150'). TROUBLESHOT IAW TM 27-93-Q0-810-808-A, R & R F/O SIDE STICK TRANSDUCER (4E4) REF AMM 27-92-41-Q00-002-A AND 27-92-41- - [SDR F3LA2011090800668](https://openairdocs.org/sdr/F3LA2011090800668), Sep 4, 2011: O-RING. DETERIORATED. HYD Y RESERVOIR LOW LEVEL DURING FLIGHT. SUBSEQUENT Y SYS FAILURE INDICATIONS. REMOVED AND INSTALLED SERVICEABLE O-RING ON REDUCER ON PTU MANIFOLD. PERFORMED OP - [SDR F3LA2010041500390](https://openairdocs.org/sdr/F3LA2010041500390), Apr 13, 2010: WIRE HARNESS. BROKEN. REFERENCE C CHECK NON ROUTINE N0636. EMERGENCY LIGHTS AT SEAT 20C AND RIGHT AFT DOOR DO NOT ILLUMINATE. REMOVED AND REPLACED WIRING HARNESS 860W AT SEAT 20C IAW - [SDR F3LA2010041400382](https://openairdocs.org/sdr/F3LA2010041400382), Apr 5, 2010: LEG ASSY. CORRODED. REF C-CHECK NON ROUTINE N0565. AFTER REMOVAL OF RT MLG SLIDING TUBE FOUND CORROSION ON INNER BORE AT LOWER BRG AREA. REPAIRED CORRODED AREA IAW EA A9-32R-31730. - [SDR F3LA2010041500389](https://openairdocs.org/sdr/F3LA2010041500389), Apr 2, 2010: FRAME. CORRODED. REFERENCE C CHECK NON ROUTINE N0307. AFT CARGO COMPARTMENT FRAME 59 TWELVE INCHES RIGHT OF CENTERLINE PROFILE TOP SURFACE CORRODED. REMOVED AND REPLACED PROFILE - [SDR F3LA2010041500388](https://openairdocs.org/sdr/F3LA2010041500388), Apr 2, 2010: PLATE. CORRODED. REFERENCE C CHECK NON ROUTINE N0291. FORWARD CARGO COMPARTMENT TRANSITION PLATE BETWEEN FRAME 28 RIGHT AND FRAME 30 RIGHT CORRODED. REMOVED AND REPLACED PLATE I - [SDR F3LA2010041500387](https://openairdocs.org/sdr/F3LA2010041500387), Apr 2, 2010: PLATE. CORRODED. REFERENCE C CHECK NON ROUTINE N0289. FORWARD CARGO COMPARTMENT TRANSITION PLATE AT STRINGER 38 LEFT BETWEEN FRAME 28 AND FRAME 30 IS CORRODED. REMOVED AND REPLA - [SDR F3LA2010041500385](https://openairdocs.org/sdr/F3LA2010041500385), Apr 2, 2010: BLANKING PLATE. CORRODED. REFERENCE C CHECK NON ROUTINE N0290. FORWARD CARGO COMPARTMENT AFT BULKHEAD PLATE BETWEEN FRAME 28 AND FRAME 29 CORRODED. REMOVED AND REPLACED BULKHEAD PLATE IA - [SDR F3LA2010041500384](https://openairdocs.org/sdr/F3LA2010041500384), Apr 2, 2010: FLOOR PANEL. DEBONDED. REFERENCE C CHECK NON ROUTINE N0295. AFT CARGO FLOOR PANEL 151ZG DISBONDED. REPAIRED DISBONDED AREA IAW AIRBUS A319 SRM 53-02-00. - [SDR F3LA2010041400383](https://openairdocs.org/sdr/F3LA2010041400383), Mar 31, 2010: FLOOR PANEL. DEBONDED. REF C-CHECK NON ROUTINE N0135. MAIN CABIN FLOOR PANEL 252 NF DISBONDED. REPAIRED DISBONDED AREA IAW SRM 53-02-00. - [SDR F3LA2010041400381](https://openairdocs.org/sdr/F3LA2010041400381), Mar 31, 2010: FLOOR PANEL. DELAMINATED. REF C-CHECK NON ROUTINE N0136. MAIN CABIN FLOOR PANEL 252 HG DISBONDED. REPAIRED FLOOR PANEL IAW SRM 53-02-00. - [SDR F3LA2009060100088](https://openairdocs.org/sdr/F3LA2009060100088), May 28, 2009: WINDSHIELD. CRACKED. PILOT REPORTED THAT THE CAPTAIN'S FORWARD WINDSCREEN CRACKED DURING CLIMB THROUGH FL210. MAINTENANCE REMOVED AND REPLACED THE WINDSHIELD, REFERENCE AMM 56-11-11 - [SDR F3LA2009040800074](https://openairdocs.org/sdr/F3LA2009040800074), Apr 8, 2009: WINDSHIELD. CRACKED. DURING CRUISE FLIGHT, PILOT REPORTED THE RT WINDSHIELD CRACKED. MAINTENANCE REMOVED AND REPLACED THE WINDSHIELD, REFERENCE AMM 56-11-11 PB 401. - [SDR F3LA2009033000069](https://openairdocs.org/sdr/F3LA2009033000069), Mar 29, 2009: LIGHT. INOPERATIVE. REFERENCE LOG PAGE 371414. MAINTENANCE NOTED THAT THE EMERGENCY LIGHT AT ROW 11 ABC WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMB - [SDR F3LA200800611](https://openairdocs.org/sdr/F3LA200800611), Sep 20, 2008: FLOOR PANEL. DAMAGED. REFERENCE NON ROUTINE CO51333. DURING C3 C CHECK, INSPECTION NOTED FLOOR PANEL 261EF HAD DAMAGED AREA AROUND INSERT ON OTBD EDGE. MX REMOVED FLOOR PANEL AND REP - [SDR F3LA200800612](https://openairdocs.org/sdr/F3LA200800612), Sep 19, 2008: SCUFF PLATE. CORRODED. REFERENCE NON ROUTINE C051324. DURING C3 C CHECK, INSPECTION NOTED THE L2 DOOR AFT OTBD SCUFF PLATE SUPPORT ATTACHMENT HAD A CORRODED FASTENER. MX REMOVED CORNE - [SDR F3LA200800615](https://openairdocs.org/sdr/F3LA200800615), Sep 19, 2008: SILL. CORRODED. REFERENCE NON ROUTINE CO51321. DURING C3 C CHECK INSPECTION NOTED THE L2 DOOR SILL AFT OTBD NUT PLATE HOLE WAS CORRODED. MX CUT CORRODED AREA OUT OF THE SILL WE - [SDR F3LA200800614](https://openairdocs.org/sdr/F3LA200800614), Sep 19, 2008: FLOORBEAM. CORRODED. DURING C3 C-CHECK INSPECTION NOTED FLOORBEAMS INBOARD OF THE L2 DOOR SILL CORRODED AND CORROSION IN ALL NUT PLATE HOLES. MX REMOVED FLOORBEAMS, REMOVED BARREL N - [SDR F3LA200800613](https://openairdocs.org/sdr/F3LA200800613), Sep 18, 2008: SILL. CORRODED. DURING C3 C-CHECK, INSPECTION NOTED THE L2 FORWARD GIRT BAR ATTACH FITTING, AFT INBOARD HOLE HAD CORROSION. MX CUT CORRODED AREA OUT OF THE SILL WEB, FABRICATED - [SDR F3LA200800609](https://openairdocs.org/sdr/F3LA200800609), Sep 16, 2008: FLOORBEAM. CORRODED. DURING C3 C-CHECK, INSPECTION NOTED THE FLOORBEAM IB OF THE R2 DOOR SILL HAS CORROSION IN ALL NUT PLATE HOLES. MAINT REMOVED AND REPLACED FLOORBEAM. Y1292 IAW T - [SDR F3LA200800610](https://openairdocs.org/sdr/F3LA200800610), Sep 16, 2008: SHEAR PLATE. CORRODED. REFERENCE NOT ROUTINE C051378. DURING C3 C-CHECK, INSP NOTED THE RT SHEAR PLATE FROM FR 69 TO FRAME 70 WAS CORRODED. MAINT REMOVED AND REPLACED SHEAR PLATE ASSY - [SDR F3LA200800606](https://openairdocs.org/sdr/F3LA200800606), Sep 12, 2008: PANEL. PUNCTURED. REFERENCE NON-ROUTINE C050859. DURING C3 C-CHECK. INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151FE WAS DAMAGED. MAINTENANCE REPAIRED DAMAGED FLOOR PANEL IAW - [SDR F3LA200800607](https://openairdocs.org/sdr/F3LA200800607), Sep 12, 2008: PANEL. PUNCTURED. REFERENCE NON-ROUTINE C050860. DURING C3-C-CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151BE WAS DAMAGED. MAINTENANCE REPAIRED DAMAGED FLOOR PANEL IAW - [SDR F3LA200800608](https://openairdocs.org/sdr/F3LA200800608), Sep 12, 2008: PANEL. PUNCTURED. REF NON-ROUTINE C050863. DURING C3-C-CHECK. INSP NOTED THE AFT PIT TRANSITION PANEL 151TG WAS DAMAGED. MAINT REPAIRED DAMAGED FLOOR PANEL IAW WITH THE REQUIREME - [SDR F3LA200800618](https://openairdocs.org/sdr/F3LA200800618), Sep 11, 2008: FLOOR PANEL. CORRODED. REFERENCE NON ROUTINE CO51286. DURING C3 C CHECK, INSPECTION NOTED FLOOR PANEL 262FF HAD CORROSION ON AFT BOTTOM SURFACE. MX REMOVED FLOOR PANEL AND INSTALLED N - [SDR F3LA200800617](https://openairdocs.org/sdr/F3LA200800617), Sep 11, 2008: FLOOR PANEL. CORRODED. REFERENCE NON ROUTINE CO51223. DURING C3 C CHECK INSPECTION NOTED FLOOR PANEL 261FF HAD CORROSION ON UPPER AND LOWER SURFACES. MX REMOVED FLOOR PANEL AND INSTAL - [SDR F3LA200700039](https://openairdocs.org/sdr/F3LA200700039), Feb 25, 2007: STRINGER. CORRODED. DURING C-2 CHECK INSPECTION, REPORTED FWD CARGO COMPARTMENT STRINGER 42R AT THE AFT END OF ZONE 131, INBD OF CARGO DOOR FROM F24 TO F28, HAD EXFOLIATION/CORROSI ## Other aircraft with N930FR - [Registered now](https://openairdocs.org/aircraft/N930FR): Socata TBM 700, S/N 1144, built 2016 --- 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.