# N912FR: 2002 Airbus A319-111, registration cancelled 2016-02-05 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 5, 2016 - 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: 1803 - Year built: 2002 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 27, 2002 - Certificate issued: September 10, 2002 - Last registry action: December 19, 2015 - Mode S code: AC9EA6 - Owner when cancelled: [Afs Investments Xv LLC](https://openairdocs.org/faa-owner/AFS%20INVESTMENTS%20XV%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/N912FR - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=912FR - Page: https://openairdocs.org/deregistered/N912FR-2016-02-05 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 (62, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR F3LA2015031101118](https://openairdocs.org/sdr/F3LA2015031101118), Mar 9, 2015: BATTERY PACK. FAILED. EPSU EMER LIGHT BATTERY 12WL, MIDDLE RT FAILED CAPACITY TEST ON A6 CHECK. R & R EPSU BATTERY 12WL IAW AMM 33-51-38-000-002A & 33-51-38-400-002A. OPERATIONS CHEC - [SDR F3LA2014100101073](https://openairdocs.org/sdr/F3LA2014100101073), Sep 28, 2014: BATTERY. DISCHARGED. AFT EPSU BATTERY FAILED A CHECK TASK CARD FFT-335100-03-1, CAPACITY CHECK. R & R BATTERY ASSEMBLY IAW AMM 33-51-39-000-005A & AMM 33-51-39-400-005-A. - [SDR F3LA2014013001004](https://openairdocs.org/sdr/F3LA2014013001004), Jan 16, 2014: SKIN. SATURATED. AIRCRAFT OUT OF SERVICE DUE TO C8 52 CHECK. RT ELEVATOR SN CC2574 THERMO GRAPHIC INSPECTION REVEALED INDICATIONS ON UPPER PANEL IRREGULAR IN SHAPE & BLACK IN CO - [SDR F3LA2014013001003](https://openairdocs.org/sdr/F3LA2014013001003), Jan 11, 2014: SHEAR PLATE. CRACKED. AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. MAIN CABIN RT SIDE SHEAR PLATE FR 69 TO FR 70 IS CRACKED. REMOVED RT SHEAR PLATE FROM FR 69 - FR 70, REPLACED WITH N - [SDR F3LA2014013001002](https://openairdocs.org/sdr/F3LA2014013001002), Jan 11, 2014: FLOORBEAM. CORRODED. AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. MAIN CABIN AFT FLOOR SUPPORT BEAM AFT OF SEAT TRACK BEAM Y 1732 HAS CORROSION AT FR 68. REMOVED CORROSION ON AFT CAB - [SDR F3LA2014013001001](https://openairdocs.org/sdr/F3LA2014013001001), Jan 11, 2014: FLOORBEAM. CORRODED. AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. MAIN CABIN FLOOR BEAM Y 1292 HAS CORROSION AT FR 16. R & R MAIN CABIN FLOOR BEAM LAW A319 SRM 51-72-11 PARA 5 & 6. - [SDR F3LA2014013001000](https://openairdocs.org/sdr/F3LA2014013001000), Jan 10, 2014: FLOORBEAM. CORRODED. AIRCRAFT OUT OF SERVICE FOR C8 S2 CHECK. AFT CABIN FLOOR SUPPORT BEAM INBD OF SEAT TRACK BEAM Y 765 6 INCHES FWD OF FR 66 HAS CORROSION. R & R FLOOR BEAM AT AFT - [SDR F3LA2014013000959](https://openairdocs.org/sdr/F3LA2014013000959), Jan 4, 2014: SHEAR PLATE. CORRODED. AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. AFT CABIN LT LATERAL SHEAR PLATE CRACKED AT FRAME 69. R & R LT LATERAL SHEAR PLATE WITH NEW PART IAW SRM 51-42-11, P - [SDR F3LA2014013000958](https://openairdocs.org/sdr/F3LA2014013000958), Jan 4, 2014: FLOORBEAM. CORRODED. AIRCRAFT OUT OF SERVICE FOR C8 S2 CHECK. MAIN CABIN FLOOR BEAM Y 254 HAS CORROSION AT FR 18. REMOVED CORROSION AT MAIN CABIN FLOOR BEAM Y 254, FR L8 IAW SRM 51- - [SDR F3LA2014013000957](https://openairdocs.org/sdr/F3LA2014013000957), Jan 2, 2014: FLOORBEAM. CORRODED. AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. FLOOR SUPPORT BEAM AFT OF SEAT TRACK Y 1292 HAS CORROSION AT FR 68. REMOVED FLOOR SUPPORT BEAM Y 1292 AT FR 68. REPL - [SDR F3LA2012083100782](https://openairdocs.org/sdr/F3LA2012083100782), Aug 28, 2012: ACTUATOR. INTERMITTENT. ACFT LEFT C-CHECK AFTER COMPLETE SET LANDING GEAR TIME, DEPARTED. NLG DID NOT LOCK UP, GEAR DOORS DID NOT CLOSE. ACFT WAS PREPPED FOR GEAR DOWN FERRY FLIGHT. FE - [SDR F3LA2011022200609](https://openairdocs.org/sdr/F3LA2011022200609), Feb 19, 2011: SUPPORT. CORRODED. C-CHECK: NON ROUTINE 2994; LATERAL SHEAR PLATE, FRAME 69 - 70 RIGHT, HAS OUT OF LIMITS CORROSION AT FASTENER HOLES. REMOVED AND REPLACED SHEAR PLATE IAW AO-53EO - [SDR F3LA2011022200608](https://openairdocs.org/sdr/F3LA2011022200608), Feb 19, 2011: SUPPORT. CORRODED. C-CHECK: NON ROUTINE # 29844; LATERAL SHEAR PLATE, FRAME 69 - 70 LEFT, HAS OUT OF LIMITS CORROSION AT FASTENER HOLES. REMOVED AND REPLACED SHEAR PLATE IAW AO-53 - [SDR F3LA2011022200610](https://openairdocs.org/sdr/F3LA2011022200610), Feb 19, 2011: FRAME. CORRODED. C-CHECK: NON ROUTINE 29941; FRAME 69 -Y765 HAS OUT OF LIMITS CORRORION AT FASTER HOLES, PER SRM 53-00-14 FIG 102. REMOVED AND REPLACE BEAM IAW A319 SRM 51-42-1. - [SDR F3LA2010033000377](https://openairdocs.org/sdr/F3LA2010033000377), Mar 29, 2010: THERMOSTAT. INOPERATIVE. CAPTAIN REPORTED BLEED 2 FAULT AND LOSS OF CABIN PRESSURISATION. MAXIMUM CABIN ALTITUDE 10,500. FLIGHT NR 963 DIVERTED FOR AN UNSCHEDULED LANDING. MX TROUBLESHO - [SDR F3LA2009121600258](https://openairdocs.org/sdr/F3LA2009121600258), Dec 16, 2009: EPSU. MALFUNCTIONED. THE FLIGHT CREW NOTED THAT THE EMERGENCY EXIT LIGHTS AND ESCAPE PATH LIGHTS IN CABIN ARE CONTINUOUSLY ON WITH THE EMERGENCY EXIT LIGHT SWITCH IN THE ARM POSITIO - [SDR F3LA2009040100070](https://openairdocs.org/sdr/F3LA2009040100070), Mar 30, 2009: WINDOW. CRACKED. AT FL 390, PILOT REPORTED THE RIGHT SLIDING WINDOW CRACKED IN BOTH PANES. MAINTENANCE REMOVED AND REPLACED THE RIGHT SLIDING WINDOW AND PERFORMED LEAK CHECK IAW - [SDR F3LA200800010](https://openairdocs.org/sdr/F3LA200800010), Jan 16, 2008: CABIN PRESSURE. FLUCTUATES. THE FLIGHT CREW REPORTED, DURING CLIMB-OUT, PRESSURIZATION FLUCTUATED 200 FEET PER MINUTE BETWEEN FLIGHT LEVEL 350 UP TO AND LEVELING AT FLIGHT LEVEL 380. AT TH - [SDR F3LA200700404](https://openairdocs.org/sdr/F3LA200700404), Dec 23, 2007: FLOOR PANEL. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 262FF CORRODED ON LOWER SURFACE. REMOVED AND REPLACED FLOOR PANEL 262FF IAW EO A0-53T-11996. - [SDR F3LA200700393](https://openairdocs.org/sdr/F3LA200700393), Dec 20, 2007: FASTENER. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED CORRODED FASTENERS THAT SECURE LIGHT TO RT WING-TO-BODY FAIRING 192DT. REMOVED AND REPLACED RT UPPER WING LIGHT COVER MO - [SDR F3LA200700392](https://openairdocs.org/sdr/F3LA200700392), Dec 20, 2007: FASTENER. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED RT WING-TO-BODY FAIRING 192DT HAD CORRODED FASTENERS AT LOWER SEAL. REMOVED AND REPLACED RT WING UPPER WING-TOO-BODY FAI - [SDR F3LA200700403](https://openairdocs.org/sdr/F3LA200700403), Dec 16, 2007: PLATE. DAMAGED. DURING C4/S1 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT AFT BULKHEAD CROSSOVER BEAM HAD FASTENERS PULLING THROUGH THE CENTER PLATE. REMOVED AND REPLACED A - [SDR F3LA200700391](https://openairdocs.org/sdr/F3LA200700391), Dec 16, 2007: PLATE. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED L2 DOOR FWD GIRT BAR LATCH FLOOR FILLER HAD A SMALL SPOT OF CORROSION. REMOVED AND REPLACED L2 DOOR FWD GIRT BAR LATCH F - [SDR F3LA200700390](https://openairdocs.org/sdr/F3LA200700390), Dec 16, 2007: PLATE. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED R2 DOOR AFT GIRT BAR LATCH FILLER CORRODED. REMOVED AND REPLACED R2 DOOR AFT GIRT BAR LATCH FILLER PANEL IAW AMM 53-42-1 - [SDR F3LA200700389](https://openairdocs.org/sdr/F3LA200700389), Dec 16, 2007: PLATE. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED L2 DOOR AFT GIRT BAR LATCH FILLER CORRODED. REMOVED AND REPLACED L2 DOOR AFT GIRT BAR LATCH FILLER IAW AMM 53-42-12-PB40 - [SDR F3LA200700402](https://openairdocs.org/sdr/F3LA200700402), Dec 15, 2007: BLANKING PLATE. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED F1 DOOR AFT GIRT BAR STOP LEVER FITTING BLANKING PLATE CORRODED ON BOTTOM SIDE. REMOVED AND REPLACED R1 DOOR AFT GIRT BA - [SDR F3LA200700397](https://openairdocs.org/sdr/F3LA200700397), Dec 15, 2007: FLOORBEAM. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM AT FR16, STA Y254, CORRODED ON THE TOP CAP. DETERMINED CORROSION TO BE OUT OF LIMITS IAW SRM 53-11-14. REMOVED - [SDR F3LA200700388](https://openairdocs.org/sdr/F3LA200700388), Dec 15, 2007: FLOOR PANEL. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 221FF (L1 DOOR) CORRODED ON BOTTOM SIDE. REMOVED AND REPLACED FLOOR PANEL 221FF IAW AMM 53-12-12-PB401. - [SDR F3LA200700387](https://openairdocs.org/sdr/F3LA200700387), Dec 15, 2007: FLOOR PANEL. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 222FF (R1 DOOR) CORRODED ON BOTTOM SIDE. REMOVED AND REPLACED FLOOR PANEL 222FF IAW AMM 53-12-12-PB401. - [SDR F3LA200700386](https://openairdocs.org/sdr/F3LA200700386), Dec 15, 2007: DUMMY RAIL. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED DUMMY RAIL AT Y503.2, FR 12 TO FR 16, CORRODED ON TOP. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14. REMOVED AND - [SDR F3LA200700384](https://openairdocs.org/sdr/F3LA200700384), Dec 15, 2007: FLOORBEAM. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AT Y1292 AND FR16, AT ATTACH POINT. REMOVED AND REPLACED FLOORBEAM AT Y1292 IAW SRM 51-42-11. - [SDR F3LA200700401](https://openairdocs.org/sdr/F3LA200700401), Dec 14, 2007: SUPPORT BEAM. BENT. DURING C4/S1 CHECK, INSPECTION REPORTED AFT CARGO FWD BULKHEAD PANEL SUPPORT BEAM AT APPROX STR 42L, FR47 TO FR51, BENT. REMOVED, FABRICATED AND INSTALLED REPLA - [SDR F3LA200700400](https://openairdocs.org/sdr/F3LA200700400), Dec 14, 2007: LOCK FASTENER. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED L2 DOOR SILL AFT GIRT BAR FITTING CORRODED AT LOCK FASTENER. REMOVED AND REPLACED FASTENER IAW SRM 51-42-11. - [SDR F3LA200700399](https://openairdocs.org/sdr/F3LA200700399), Dec 14, 2007: SHEAR PLATE. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED SHEAR PLATE AT Y1292, BETWEEN FR69 AND FR70, CORRODED. REMOVED AND REPLACED SHEAR PLATE AND FLOORBEAM IAW SRM 51-42-11 A - [SDR F3LA200700398](https://openairdocs.org/sdr/F3LA200700398), Dec 14, 2007: FLOORBEAM. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM AT Y765, FR68, CORRODED. DETERMINED CORROSION TO BE OUT OF LIMITS IAW 53-00-14. REMOVED AND REPLACED FLOOR BEA - [SDR F3LA200700396](https://openairdocs.org/sdr/F3LA200700396), Dec 14, 2007: FLOORBEAM. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM AT Y1292, FR68, CORRODED. DETERMINED CORROSION TO BE OUT OF LIMITS IAW SRM 53-00-14, PAR 4 B. REMOVED AND REPL - [SDR F3LA200700395](https://openairdocs.org/sdr/F3LA200700395), Dec 14, 2007: SILL. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED L2 DOOR SILL CORRODED AT VARIOUS LOCATIONS BETWEEN FR 66 AND FR 68. REMOVED AND REPLACED L2 DOOR SILL PLATE IAW SRM 51-4 - [SDR F3LA200700394](https://openairdocs.org/sdr/F3LA200700394), Dec 14, 2007: FLOORBEAM. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM AT Y1292, FR66, CORRODED AT NUTPLATE HOLES. REMOVED AND REPLACED FLOORBEAM AT Y1292, FR66, IAW SRM 51-42-11. - [SDR F3LA200700383](https://openairdocs.org/sdr/F3LA200700383), Dec 14, 2007: ATTACH BOLT. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED LWR ATTACHMENT BOLT ON INBD AFT CORNER OF LAV "A" SEVERELY CORRODED. REMOVED AND REPLACED BOLT IAW AMM 25-41-41-PB401. - [SDR F3LA200700381](https://openairdocs.org/sdr/F3LA200700381), Dec 14, 2007: SHEAR PLATE. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED SHEAR PLATE AT BS -Y1292 BETWEEN FR 69 AND FR 70 CORRODED. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14-101. REM - [SDR F3LA200700380](https://openairdocs.org/sdr/F3LA200700380), Dec 14, 2007: FLOORBEAM. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM AT BS -Y1292 HAD CORROSION AT NUT PLATE HOLES BETWEEN FR 68 AND FR 69. FOUND CORROSION TO BE OUT OF LIMITS IAW - [SDR F3LA200700378](https://openairdocs.org/sdr/F3LA200700378), Dec 14, 2007: RIVET. SHEARED. DURING C4/S1 CHECK, INSPECTION REPORTED SHEARED RIVETS ON WEB AT STA. -Y1292 BETWEEN FR68 AND FR69. REMOVED AND REPLACED RIVETS IAW A319 SRM 51-44-11, 51-46-11 - [SDR F3LA200700405](https://openairdocs.org/sdr/F3LA200700405), Dec 13, 2007: MOUNT BOLT. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED LAV E LOWER FLOOR MOUNT BOLTS CORRODED. REMOVED AND REPLACED CORRODED FLOOR MOUNT BOLTS IN LAV E IAW AMM 25-43-42-PB401. - [SDR F3LA200700382](https://openairdocs.org/sdr/F3LA200700382), Dec 13, 2007: BOLT. CORRODED. DURING C4/S1 CHECK, INSPECTION REPORTED LAV "D" MOUNT BOLTS CORRODED. REMOVED AND REPLACED CORRODED MOUNT BOLTS IAW AMM 25-43-41-PB401. - [SDR F3LA200700410](https://openairdocs.org/sdr/F3LA200700410), Dec 12, 2007: BATTERY PACK. NO TEST. DURING C4/S1 CHECK, INSPECTION REPORTED AFT EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED AND INSTALLED SERVICEABLE AFT EMERGENCY LIGHT BATTERY PACK IA - [SDR F3LA200700409](https://openairdocs.org/sdr/F3LA200700409), Dec 12, 2007: BATTERY PACK. FAILED. DURING C4/S1 CHECK, INSPECTION REPORTED LT OVERWING EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED AND INSTALLED SERVICEABLE BATTERY IN LT OVERWING EPSU - [SDR F3LA200700408](https://openairdocs.org/sdr/F3LA200700408), Dec 12, 2007: BATTERY PACK. FAILED. DURING C4/S1 CHECK, INSPECTION REPORTED RT OVERWING EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED AND INSTALLED SERVICEABLE BATTERY PACK IN RT OVERWING - [SDR F3LA200700407](https://openairdocs.org/sdr/F3LA200700407), Dec 12, 2007: BATTERY PACK. FAILED. DURING C4/S1 CHECK, INSPECTION REPORTED FWD EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED AND INSTALLED SERVICEABLE BATTERY IN FWD EPSU (10WL) IAW AMM - [SDR F3LA200700406](https://openairdocs.org/sdr/F3LA200700406), Dec 12, 2007: RELEASE CABLE. INOPERATIVE. DURING C4/S1 CHECK, INSPECTION REPORTED RT OVERWING EXIT SLIDE RELEASE CABLE WOULD NOT RETRACT. REMOVED AND REPLACED RT OVERWING SLIDE RELEASE CABLE IAW AMM 25- - [SDR F3LA200700377](https://openairdocs.org/sdr/F3LA200700377), Dec 12, 2007: RELEASE CABLE. INOPERATIVE. DURING C4/S1 CHECK, INSPECTION REPORTED LT OVERWING EMERGENCY EXIT SLIDE RELEASE CABLE WOULD NOT RETRACT. REMOVED AND REPLACED LT OVERWING EXIT SLIDE RELEASE CA All 62: https://openairdocs.org/deregistered/N912FR-2016-02-05/reports.md --- 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.