# N924FR: 2003 Airbus A319-111, registration cancelled 2016-04-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 28, 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: 2030 - Year built: 2003 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 24, 2004 - Certificate issued: December 5, 2003 - Last registry action: December 19, 2015 - Mode S code: ACCD93 - Owner when cancelled: [Afs Investments Xxii LLC](https://openairdocs.org/faa-owner/AFS%20INVESTMENTS%20XXII%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/N924FR - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=924FR - Page: https://openairdocs.org/deregistered/N924FR-2016-04-28 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 (37) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR F3LA2015080701143](https://openairdocs.org/sdr/F3LA2015080701143), Aug 6, 2015: LIGHT. INOPERATIVE. LIGHT INOPERATIVE AT LT EMER ESCAPE HATCH HANDLE. R & R EMER LIGHT 70WL1. OPERATIONS CHECKED GOOD IAW AMM 33-51-11-400-001-A. REF LOG PAGE 895364 ITEM 2. - [SDR F3LA2014022401024](https://openairdocs.org/sdr/F3LA2014022401024), Feb 13, 2014: SHEAR PLATE. CRACKED. AIRCRAFT OUT OF SERVICE DUE TO C7 S2 CHECK. AFT MAIN CABIN LT SHEAR PLATE HAS CRACK AT FR 69 - FR 70 STRINGER Y 1292. R & R SHEAR PLATE, AIRBUS A319 SRM 53-41-1 - [SDR F3LA2014022401023](https://openairdocs.org/sdr/F3LA2014022401023), Feb 3, 2014: FLOORBEAM. CORRODED. AIRCRAFT OUT OF SERVICE DUE TO C7 S2 CHECK. MAIN CABIN FLOOR BEAM RT AT Y 1292, FR 65 - FR 66 HAS CORROSION, BEAM CORROSION IS OUT OF LIMITS. R & R BEAM, AIRBUS - [SDR F3LA2014022401022](https://openairdocs.org/sdr/F3LA2014022401022), Jan 31, 2014: FLOORBEAM. CORRODED. AIRCRAFT OUT OF SERVICE DUE TO C7 S2 CHECK. FWD CABIN FLOOR BEAM AT FR 20 RT, Y 1292 HAS LIGHT CORROSION. REMOVED CORROSION ON FLOOR BEAM AT FR 20 RT, Y 1292 IN - [SDR F3LA2014022401021](https://openairdocs.org/sdr/F3LA2014022401021), Jan 31, 2014: FLOORBEAM. CORRODED. AIRCRAFT OUT OF SERVICE DUE TO C7 S2 CHECK. FWD CABIN FLOOR BEAM AT FR 20 LT, Y 1292 HAS LIGHT CORROSION. REMOVED CORROSION ON FLOOR BEAM AT FR 20 LT, Y 1292 IN - [SDR F3LA2014022401020](https://openairdocs.org/sdr/F3LA2014022401020), Jan 31, 2014: COVER PLATE. CORRODED. AIRCRAFT OUT OF SERVICE DUE TO C7 S2 CHECK. AFT CARGO COMPARTMENT DOOR SILL SUB FLOOR COVER PLATE CORRODED IN SPOTS FROM FR 58 TO FR 59. REMOVED SURFACE CORROSI - [SDR F3LA2010041100380](https://openairdocs.org/sdr/F3LA2010041100380), Apr 7, 2010: STRUCTURE. DAMAGED. REF LOG PAGE 503298, ITEM 1. ON DESCENT, HAD A LOUD POP FROM THE CAPTAIN'S SLIDING WINDOW, WINDOW THAN BEGAN TO OVERHEAT. SOON THERE AFTER GOT LIGHT FUMES IN TH - [SDR F3LA2009111800232](https://openairdocs.org/sdr/F3LA2009111800232), Nov 14, 2009: INLET. DAMAGED. THE FLIGHT CREW MADE AN AIR RETURN DUE TO MULTIPLE BIRD STRIKES DURING CLIMB OUT CAUSING THE NR 2 ENG COMPRESSOR TO STALL. MX REMOVED AND REPLACED THE NR 2 ENG - [SDR F3LA2009111800231](https://openairdocs.org/sdr/F3LA2009111800231), Nov 14, 2009: ENGINE. BIRD INGESTION. FLIGHT CREW MADE AN AIR RETURN DUE TO MULTIPLE BIRD STRIKES DURING CLIMB OUT CAUSING THE NR 2 ENGINE COMPRESSOR TO STALL. MX REMOVED AND REPLACED THE NR 2 ENG A - [SDR F3LA2009072800118](https://openairdocs.org/sdr/F3LA2009072800118), Jul 26, 2009: POWER SUPPLY. FAILED. DURING C4 C-CHECK, INSP NOTED THE AFT EMERGENCY POWER SUPPLY UNIT FAILED. MX REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT AND PERFORMED OPS TEST IAW AMM - [SDR F3LA2009072700113](https://openairdocs.org/sdr/F3LA2009072700113), Jul 24, 2009: PROFILE. CORRODED. DURING C4 C-CHECK, INSP NOTED THE AFT CARGO COMPARTMENT STRUCTURAL PROFILE AT FRAME 56 HAS CORROSION AT THE NUT PLATES. MX PERFORMED MAJOR REPAIR BY REMOVING CO - [SDR F3LA2009072700116](https://openairdocs.org/sdr/F3LA2009072700116), Jul 23, 2009: SUPPORT BRACKET. CORRODED. DURING C4 C-CHECK, INSP NOTED THAT THE LT SUPPORT BRACKET AT FRAME 59 HAS CORROSION IN THE FASTENER HOLES. MX REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 5 - [SDR F3LA2009072700115](https://openairdocs.org/sdr/F3LA2009072700115), Jul 23, 2009: FLOOR SUPPORT. CORRODED. DURING C4 C-CHECK, INSP NOTED THAT THE CENTER LONGITUDINAL SUPPORT FROM FR 58 TO FR 59 HAS CORROSION AT THE NUT PLATE HOLE. MX REMOVED AND REPLACED THE SUPPORT - [SDR F3LA2009072700114](https://openairdocs.org/sdr/F3LA2009072700114), Jul 23, 2009: BRACKET. CORRODED. DURING DEN C4 C-CHECK, INSP NOTED AT FR 59, THE AFT CENTER SUPPORT BRACKET HAS CORROSION IN FASTENER HOLES. MX PERFORMED MAJOR REPAIR BY REMOVING CORRODED SUPPO - [SDR F3LA2009072700112](https://openairdocs.org/sdr/F3LA2009072700112), Jul 23, 2009: SUPPORT FITTING. CORRODED. DURING C4 C-CHECK, INSP NOTED THAT THE CENTER SUPPORT FITTING UNDER FRAME 58 HAS CORROSION AT NUT PLATE HOLES. MX REMOVED AND REPLACED THE CENTER SUPPORT FITTIN - [SDR F3LA2009072700117](https://openairdocs.org/sdr/F3LA2009072700117), Jul 22, 2009: PROFILE. CORRODED. DURING C4 C-CHECK, INSP NOTED THAT THE STRUCTURAL PROFILE AT FR 59 HAS SURFACE CORROSION AT NUT PLATE HOLES. MX REMOVED AND REPLACED THE PROFILE AT FR 59 IAW SR - [SDR F3LA2009072700111](https://openairdocs.org/sdr/F3LA2009072700111), Jul 22, 2009: SUPPORT FITTING. CORRODED. DURING C4 C-CHECK, INSP NOTED THAT THE AFT CARGO CENTER SUPPORT FITTING ON FRAME 56 HAS CORROSION AT NUT PLATE HOLE. MX REMOVED AND REPLACED FITTING IAW SRM 51- - [SDR F3LA2009072700110](https://openairdocs.org/sdr/F3LA2009072700110), Jul 20, 2009: COWLING. DAMAGED. DURING C4 C-CHECK, INSP NOTED THAT THE NR 2 ENGINE OTBD FAN COWL HAS DAMAGE ON THE INSIDE OF COWL, 2 FEET FROM THE TOP AND 1 FOOT FROM THE T/E. MX PERFORMED MAJ - [SDR F3LA2009072700109](https://openairdocs.org/sdr/F3LA2009072700109), Jul 18, 2009: BATTERY PACK. NO TEST. DURING C4 C-CHECK, INSP NOTED THAT THE AFT LT EMERGENCY POWER SUPPLY UNIT BATTERY FAILS CAPACITY CHECK. MX REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT - [SDR F3LA2009012600005](https://openairdocs.org/sdr/F3LA2009012600005), Jan 25, 2009: GASKET. DAMAGED. PILOT REPORTED NR 1 ENGINE FAILURE INFLIGHT, RELIGHT UNSUCCESSFUL. MAINTENANCE INSPECTED NR 1 ENGINE AND FOUND THE GASKET AT THE FUEL FLOW TRANSMITTER DAMAGED. - [SDR F3LA2008100600668](https://openairdocs.org/sdr/F3LA2008100600668), Oct 4, 2008: SERVO CONTROL. UNRESPONSIVE. ON TAXI OUT, SPEED LESS THAN 10KTS, AIRCRAFT SWERVED TO THE LEFT (UNCOMMANDED) AND DID NOT RESPOND TO STEERING IMPUTS. STOPPED AIRCRAFT USING BRAKES, RECEIVED E - [SDR F3LA200800616](https://openairdocs.org/sdr/F3LA200800616), Sep 18, 2008: PIN. FAILED. FLIGHT NR 3183. NR 1 ELECTRONIC CENTRALIZED ACFT MONITOR INDICATED LANDING GEAR CONTROL INTERFACE UNIT FAULT. ACFT VIBRATION WAS FELT AFTER LANDING AND ACFT STO - [SDR F3LA200800041](https://openairdocs.org/sdr/F3LA200800041), Jan 31, 2008: TUBE. LEAKING. DURING DESCENT & APPROACH, CREW REPORTED AN ECAM INDICATION OF LOW HYD PRESSURE & LOW HYD FLUID LEVEL FOR GREEN HYDC SYS. AN EMERGENCY DECLARED & CREW MANUALLY - [SDR F3LA200800035](https://openairdocs.org/sdr/F3LA200800035), Jan 10, 2008: FLOOR PANEL. DAMAGED. DURING C CHECK INSPECTION, CABIN FLOOR PANEL 241F, LOCATED IN THE COCKPIT, HAD THE SECOND SCREW HOLE, ON THE RIGHT FORWARD SIDE, PULLED THROUGH. MAINTENANCE REP - [SDR F3LA200800021](https://openairdocs.org/sdr/F3LA200800021), Jan 7, 2008: CYLINDER DAMPER. INOPERATIVE. DURING C CHECK INSPECTION, THE R1 EMERGENCY DOOR DAMPENER CYLINDER FAILED ITS TEST DUE TO LOW PRESSURE. MAINTENANCE CHARGED THE CYLINDER IN ACCORDANCE WITH THE - [SDR F3LA200800020](https://openairdocs.org/sdr/F3LA200800020), Jan 7, 2008: CYLINDER DAMPER. INOPERATIVE. DURING C CHECK INSPECTION, THE R2 EMERGENCY DOOR DAMPENER CYLINDER FAILED ITS TEST DUE TO LOW PRESSURE. MAINTENANCE CHARGED THE CYLINDER IN ACCORDANCE WITH THE - [SDR F3LA200800019](https://openairdocs.org/sdr/F3LA200800019), Jan 7, 2008: BATTERY. INOPERATIVE. DURING C CHECK INSPECTION, THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY WAS FOUND DEAD. MAINTENANCE REMOVED AND REPLACED THE FLASHLIGHT BATTERY IN - [SDR F3LA200800034](https://openairdocs.org/sdr/F3LA200800034), Jan 6, 2008: SHEAR PLATE. CORRODED. DURING C CHECK INSPECTION, CORROSION WAS FOUND ON THE SHEAR PLATE ON THE RIGHT SIDE, OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 68 AND 70 AT STRINGER 23. MAINTENANCE - [SDR F3LA200800007](https://openairdocs.org/sdr/F3LA200800007), Jan 6, 2008: INERTIA REEL. CORRODED. DURING C-CHECK INSPECTION, THE R1 DOOR SAFETY TAPE INERTIAL REEL WAS FOUND TO HAVE CORROSION ON IT. MAINTENANCE REMOVED AND REPLACED THE R1 DOOR SAFETY TAPE INE - [SDR F3LA200800008](https://openairdocs.org/sdr/F3LA200800008), Jan 6, 2008: FLOORBEAM. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON THE FLOORBEAM, AROUND THE NUT CLIP LOCATIONS (6 EACH) AT THE ATTACH POINTS OF THE FLOOR PANEL, JUST INSIDE THE - [SDR F3LA200600147](https://openairdocs.org/sdr/F3LA200600147), Oct 23, 2006: CONTROL STICK. UNKNOWN. FLIGHT CREW REPORTED THAT UPON APPROACH, AT APPROXIMATELY 10 FT ABOVE THE RUNWAY, AIRCRAFT ABRUPTLY NOSED OVER DURING FLARE WITH FULL AFT STICK HELD (HAND-FLOWN - [SDR F3LA200600085](https://openairdocs.org/sdr/F3LA200600085), Jul 28, 2006: MASK. NO TEST. DURING C-2 CHECK, INSPECTION REPORTED MASK BOX OVER L1 DOOR (40WR) DID NOT DROP. REPACKED O2 MASKS OVER L1 DOOR AND OPS CHECKED IAW AMM 35-23-00-720-454. CHECKE - [SDR F3LA200600083](https://openairdocs.org/sdr/F3LA200600083), Jul 28, 2006: EPSU. NO TEST. DURING C-2 CHECK, INSPECTION REPORTED FWD LT EPSU (EMERGENCY POWER SUPPLY UNIT) FAILED TEST. REPLACED LT FWD EPSU AND PERFORMED OPERATIONAL CHECK. TESTED GOOD. - [SDR F3LA200600082](https://openairdocs.org/sdr/F3LA200600082), Jul 27, 2006: WIRE. MAINT ERROR. DURING C-2 CHECK, PRE-RECORDED ANNOUNCEMENT DID NOT COME ON DURING OXYGEN MASK DROP TEST. FOUND PRE-RECORDED ANNOUNCEMENT OUTPUT WIRES CAPPED & STOWED, LIVE TV - [SDR F3LA200600081](https://openairdocs.org/sdr/F3LA200600081), Jul 27, 2006: PSU. FAILED. DURING C-2 CHECK, INSPECTION REPORTED THE PASSENGER OXYGEN MASK DOOR AT ROW 7 ABC DID NOT OPEN DURING TEST. REPLACED PASSENGER OXYGEN CONTAINER ASSY PER AMM 35- - [SDR F3LA200600080](https://openairdocs.org/sdr/F3LA200600080), Jul 27, 2006: RIVET. SHEARED. DURING C-2 CHECK, INSPECTION REPORTED A RIVET HEAD SHEARED OFF AT LT SIDE FWD A/C BAY, FWD LOWER CORNER WEB AT ZONE 191, I/B SIDE OF WEB, LOCATED O/B OF EMERGEN - [SDR F3LA200500047](https://openairdocs.org/sdr/F3LA200500047), Dec 12, 2005: CONTROLLER. MALFUNCTIONED. BLOCK TURNBACK. FLIGHT CREW REPORTED LOW PRESSURE BOTH ENGINES DURING START WITH FUMES INTO CABIN. REPLACED BMC NR1. LOW BLEED PRESSURE OPS CHECKED GOOD IAW AMM ## NTSB investigations (2) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB CEN10IA053](https://openairdocs.org/ntsb/CEN10IA053), Nov 15, 2009: Airbus A319-111 (N924FR), Kansas City, MO, incident, minor damage. Probable cause: The in-flight engine ingestion of one or more Lesser Snow Geese (Chen caerulescens caerulescens). - [NTSB DEN07IA027](https://openairdocs.org/ntsb/DEN07IA027), Oct 23, 2006: Airbus Industrie A319-111 (N924FR), Denver, CO, incident, no damage. Probable cause: The inadvertent activation of the priority pushbutton on the sidestick by the first officer resulting in a nose down pitch and loss of aircraft control during the landing flare. ## FAA accident and incident reports (2) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20091114051349I](https://openairdocs.org/incident/20091114051349I), Nov 14, 2009: Airbus A319-111 (N924FR), Kansas City, MO, Minor damage. Departed kmci gate 0050Z. Utilized runway 1R. Weather was approximately 2500 overcast with good visibility. First officer matthew cartwright was pilot flying.… - [Incident 20080919853529I](https://openairdocs.org/incident/20080919853529I), Sep 19, 2008: Airbus A319111 (N924FR), Oklahoma City, OK, Minor damage. At 1822, ATC notified okc airport operations about aircraft disabled on runway. A/p ops arrival on scene at 1835. Local maintenance contractor arrival at 1850.… --- 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.