# N935FR: 2004 Airbus A319-111, registration cancelled 2017-04-12 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 12, 2017 - Exported to: Ireland - 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: 2318 - Year built: 2004 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 23, 2004 - Certificate issued: October 22, 2004 - Last registry action: December 19, 2015 - Mode S code: ACF8C9 - Owner when cancelled: [Afs Investments 55 LLC](https://openairdocs.org/faa-owner/AFS%20INVESTMENTS%2055%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/N935FR - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=935FR - Page: https://openairdocs.org/deregistered/N935FR-2017-04-12 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 (31) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR F3LA2016062100051](https://openairdocs.org/sdr/F3LA2016062100051), Jun 19, 2016: ENGINE. SHUTDOWN. DURING CRUISE FLIGHT THE CREW NOTED, ECAM ENGINE 2 STALL WHICH WAS SOON FOLLOWED BY ENGINE 2 SHUTDOWN. THE CREW DECLARED EMERGENCY LANDING. MAINTENANCE R & R NR - [SDR F3LA2015040601127](https://openairdocs.org/sdr/F3LA2015040601127), Apr 2, 2015: UNKNOWN. MALFUNCTIONED. FLAP JAM AT SLAT ONLY, FLAPS LOCKED. PERFORMED BITE TEST OF SFCC IAW AMM 27-51-00-740-002-A. PERFORMED 2 FULL FLAPS & SLATS CYCLES, NO DEFECTS NOTED. PERFORMED - [SDR F3LA2015020401104](https://openairdocs.org/sdr/F3LA2015020401104), Feb 3, 2015: BATTERY PACK. DISCHARGED. LEFT EPSU BATTERY FAILS TEST. REPLACED LT EPSU IAW AMM 33-51-38 PB 401. OPERATIONS CHECKED NORMAL. LOG PAGE 843284. - [SDR F3LA2014082001054](https://openairdocs.org/sdr/F3LA2014082001054), Aug 19, 2014: BATTERY. DISCHARGED. EPSU BATTERY 12WL FAILED THE TEST ON THE HEAVY SERVICE CHECK. R & R EPSU BATTERY 12WL IAW AMM 33-51-38-000-002-A & 33-51-38-400-002 A. - [SDR F3LA2014012700956](https://openairdocs.org/sdr/F3LA2014012700956), Jan 24, 2014: BATTERY PACK. DEFECTIVE. EMERGENCY LIGHT FAULT EPSU AFT LT & NO GREEN SYS OK LIGHT UPON TESTING. R & R AFT LT EPSU BATTERY IAW AMM 33-51-38 PB 401, OPERATIONS CHECKED GOOD. - [SDR F3LA2013121900951](https://openairdocs.org/sdr/F3LA2013121900951), Dec 17, 2013: WIRE HARNESS. BROKEN. AIRCRAFT OUT OF SERVICE DUE TO C6 CHECK. EMERGENCY LIGHTING WIRING AT SEAT ROW 25L IS BROKEN. R & R EMERGENCY LIGHTING WIRING HARNESS IAW AMM 33-51-19. OPERATIO - [SDR F3LA2011061400656](https://openairdocs.org/sdr/F3LA2011061400656), Jun 7, 2011: DOOR. OPEN. LP 540215: AIR TURN BACK, FWD CARGO DOOR OPEN AFTER TAKEOFF "OVERWEIGHT LANDING". PLACED THE CARGO DOOR ON MEL 52-70-01H MDDR 1083274 AND PERFORMED INSPECTION R - [SDR F3LA2011020400598](https://openairdocs.org/sdr/F3LA2011020400598), Jan 28, 2011: LINE. LEAKING. A/C REPORT LP NR605872: GREEN HYD SYS RESERVOIR LOW QUANTITY. GRAVITY EXTENSION OF LANDING GEAR APPARENT FLUID LEAKING FROM NR 1 ENGINE. UPON FURTHER INSP FOUND - [SDR F3LA2010072500515](https://openairdocs.org/sdr/F3LA2010072500515), Sep 23, 2010: FLOOR PANEL. DAMAGED. C-CHECK NON ROUTINE N0479, 6 EACH INSERTS PULLED OUT WITH SKIN DAMAGE. REPAIRED THE SKIN DAMAGE AT 6 EACH HOLE LOCATIONS USING PATCH METHOD IAW A319 SRM 53-02-0 - [SDR F3LA2010072500514](https://openairdocs.org/sdr/F3LA2010072500514), Sep 23, 2010: EPSU. INOPERATIVE. C-CHECK NON ROUTINE N0769, L-1 AND R-1 LOWER DOOR INTERIOR EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED EPSU ON (10WL) AND TEST GOOD IAW A319 AMM 33-51-38-PB - [SDR F3LA2010072500513](https://openairdocs.org/sdr/F3LA2010072500513), Sep 23, 2010: PANEL. PUNCTURED. C-CHECK NON ROUTINE N0473, AFT CARGO FLOOR PANEL 151VG HAS 7 PUNCTURES. FABRICATED AND REPLACEMENT PANEL IAW MCG IRM 9701 REV G. - [SDR F3LA2010072500512](https://openairdocs.org/sdr/F3LA2010072500512), Sep 23, 2010: FLOOR PANEL. DAMAGED. C-CHECK NON ROUTINE N0649, AFT CARGO FLOOR PANEL 151FE HAS COMPOSITE DAMAGE ON BOTH SIDES. REPAIRED COMPOSITE DAMAGE IAW A319 SRM 53-02-00 PARA 5. - [SDR F3LA2010072500511](https://openairdocs.org/sdr/F3LA2010072500511), Sep 23, 2010: FLOOR PANEL. PUNCTURED. C-CHECK NON ROUTINE N0507, AFT CARGO FLOOR PANEL 151UG HAS 2 PUNCTURES AND 4 EACH DAMAGED PREVIOUS REPAIRS. FABRICATED AND REPLACED PANEL IAW MCG IRM 9701 REV G - [SDR F3LA2010072500510](https://openairdocs.org/sdr/F3LA2010072500510), Sep 23, 2010: SUPPORT. CORRODED. C-CHECK NON ROUTINE N0413, FRAME SUPPORT FROM 69 TO 70 STRINGER 23R BELOW SHEAR PLATE HAS 2 AREAS OF CORROSION TOTALING 2 SQUARE INCHES. REMOVED AND REPLACED FR - [SDR F3LA2010072500509](https://openairdocs.org/sdr/F3LA2010072500509), Sep 23, 2010: FLOOR PANEL. PUNCTURED. C-CHECK NON ROUTINE N0479, AFT CARGO FLOOR PANEL 151PE HAS A 2 EACH PUCTURES. REPAIR USING GLASS CLOH WET LAYUP IAW A319 SRN 53-00 PARA 8 B. - [SDR F3LA2010072500508](https://openairdocs.org/sdr/F3LA2010072500508), Sep 23, 2010: SEAT TRACK. CORRODED. C-CHECK: NON ROUTINE N0494, AFT CABIN SEAT TRACK Y1292 AT FRAME 68L HAS 2 AREAS OF CORROSION UPPER SURFACE. CORROTIONS OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 1 - [SDR F3LA2010072500507](https://openairdocs.org/sdr/F3LA2010072500507), Sep 23, 2010: PANEL. PUNCTURED. C-CHECK: NON ROUTINE AFT CARGO TRANSITION PANEL 151AE HAS 6 PUNCTURES. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 PARA 13 REVISION G. - [SDR F3LA2010072500506](https://openairdocs.org/sdr/F3LA2010072500506), Sep 23, 2010: FLOORBEAM. CORRODED. C-CHECK: NON ROUTINE N0410, AFT MAIN CABIN FLOORBEAM Y1292 AT FRAME 68R HAS 2 AREAS OF CORROSION. REMOVED AND REPLACED FLOORBEAM - Y1292 FROM FRAME 68R TO FRAME - [SDR F3LA2010072500505](https://openairdocs.org/sdr/F3LA2010072500505), Sep 23, 2010: PLATE. CORRODED. C-CHECK: NON ROUTINE 0414, AFT CARGO DOORS SILL SHEET HAS 4 AREAS OF CORROSION MEASURING 4.5 SQUARE INCHES TOTAL. REMOVED CORROSION IAW A319 SRM 51-74-00 PARA 5 - [SDR F3LA2010072500504](https://openairdocs.org/sdr/F3LA2010072500504), Sep 23, 2010: BATTERY. DISCHARGED. C-CHECK: NON ROUTINE N0074, FWD MEGAPHONE INOPERATIVE. REPLACED BATTERIES IN THE MEGAPHONE IAW A319 AMM 25-65-51-920-001. MEGAPHONE STILL INOPERATIVE, REMOVED A - [SDR F3LA2010072500503](https://openairdocs.org/sdr/F3LA2010072500503), Sep 23, 2010: FLOOR PANEL. DEBONDED. C-CHECK: NON ROUTINE N0384, CABIN FLOOR PANEL 251AF DISBONDED. REPAIRED DISBOND ON FLOOR PANEL 251AF IAW A319 SRM 53-02-00 PARA 8. A, (2) FIG. 204. - [SDR F3LA2010072500502](https://openairdocs.org/sdr/F3LA2010072500502), Sep 23, 2010: FLOOR PANEL. DEBONDED. C-CHECK: NON ROUTINE N0383, CABIN FLOOR PANEL 252SF DISBONDED. REPAIRED DISBONDED SKIN AREA ON THE FLOOR PANEL 252SF USING FILLER METHOD. REPAIRED DISBONDED IAW - [SDR F3LA2009080300124](https://openairdocs.org/sdr/F3LA2009080300124), Jul 31, 2009: CONTROL UNIT. DEFECTIVE. CREW MADE AN AIR RETURN, DUE TO THE ALTITUDE SELECTOR KNOB ON THE FLIGHT CONTROL UNIT BEING STUCK ON AN ALTITUDE, RENDERING THE AUTO-PILOT, AUTO-THRUST AND FLIG - [SDR F3LA2009020900024](https://openairdocs.org/sdr/F3LA2009020900024), Feb 2, 2009: SILL. CORRODED. DURING C3 C-CHECK, INSPECTION NOTED THE LEFT GALLEY FLOOR STRUCTURE AT FRAME 66 HAS TWO NUT PLATE HOLES CORRODED AFT OF GIRT BAR FITTING ADAPTER PLATE. MAINTENA - [SDR F3LA2009020900023](https://openairdocs.org/sdr/F3LA2009020900023), Feb 2, 2009: SILL. CORRODED. DURING C3 C-CHECK, INSPECTION NOTED THE L2 DOOR SILL BEAM HAS TWO CORRODED NUT PLATE HOLES AT FRAME 68. MAINTENANCE TRIMMED OUT DAMAGED AREA, FABRICATED REPAIR - [SDR F3LA2009020900022](https://openairdocs.org/sdr/F3LA2009020900022), Feb 2, 2009: FLOORBEAM. CORRODED. DURING C3 C-CHECK, INSPECTION NOTED THE LEFT AFT GALLEY FLOORBEAM Y1292 HAS CORROSION AROUND FASTENER HOLES BETWEEN FRAME 67 AND FRAME 68. MAINTENANCE REMOVED A - [SDR F3LA2009020900021](https://openairdocs.org/sdr/F3LA2009020900021), Feb 2, 2009: FLOOR PANEL. CORRODED. DURING C3 C-CHECK, INSPECTION NOTED FLOOR PANEL 262FF HAS CORROSION. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL PER TASK CARD C534103-2. - [SDR F3LA200800275](https://openairdocs.org/sdr/F3LA200800275), May 18, 2008: COFFEEMAKER. ODOR. REFERENCE LOG PAGES 369125 AND 369126. DURING FLIGHT THE FA REPORTED A STRONG ODOR AND HEAT. MAINT RAN APU AND ENGINE (1) AND (2) AT IDLE WITH BOTH PACKS ON. MA - [SDR F3LA200800001](https://openairdocs.org/sdr/F3LA200800001), Jan 7, 2008: FLAP SYSTEM. OUT OF ALIGNMENT. DURING THE APPROACH, THE FLIGHT CREW RECEIVED AN ECAM MESSAGE THAT THE FLIGHT CONTROLS - FLAPS - WERE LOCKED DUE TO AN ALIGNMENT FAULT. AN EMERGENCY WAS DECLARE - [SDR F3LA200700199](https://openairdocs.org/sdr/F3LA200700199), Aug 8, 2007: SUPPORT BEAM. CORRODED. DURING C-2 CHECK, INSPECTION REPORTED FR C-20 TOP SUPPORT BEAM IN LT FWD ELECTRICAL EQUIPMENT COMPARTMENT FRETTING. FOUND FITTING TO BE OUT OF LIMITS IAW AIRBUS - [SDR F3LA200600008](https://openairdocs.org/sdr/F3LA200600008), Feb 27, 2006: CONTROL SYSTEM. FAILED. DURING C-1 CHECK, MAINTENANCE REPORTED RT OVERWING EMERGENCY EXIT FAILED FUNCTION TEST (PER WORK CARD C522101-3, EMERGENCY ESCAPE SYSTEM FAILURE). ADJUSTED RT O --- 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.