# N934FR: 2004 Airbus A319-111, registration cancelled 2016-09-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 12, 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: 2287
- Year built: 2004
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 13, 2004
- Certificate issued: September 29, 2004
- Last registry action: December 19, 2015
- Mode S code: ACF512
- 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/N934FR
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=934FR
- Page: https://openairdocs.org/deregistered/N934FR-2016-09-12

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 (60, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR F3LA2015041501129](https://openairdocs.org/sdr/F3LA2015041501129), Apr 12, 2015: HYDRAULIC LINE. CHAFED. REFERENCE LOG PAGE 802478 ITEM NR 1. AIR TURN BACK AT 14:55 Z HYD RESERVOIR LOW LEVEL. YELLOW HYD QTY WENT TO ZERO JUST AFTER TAKEOFF. R & R HYD PRESS LINE, PN 
- [SDR F3LA2014022401019](https://openairdocs.org/sdr/F3LA2014022401019), Feb 24, 2014: BATTERY. DISCHARGED. EMERGENCY POWER SUPPLY UNIT LT 11WL FAILED BATTERY DURING HEAVY SERVICE CHECK. R & R EPSU LT 11WL BATTERY ASSEMBLY IAW AMM 33-51-39-000-005A & AMM 33-51-39-400-
- [SDR F3LA2014022401018](https://openairdocs.org/sdr/F3LA2014022401018), Feb 24, 2014: BATTERY. DISCHARGED. EMERGENCY POWER SUPPLY UNIT FWD LT BATTERY FAULT DURING HEAVY SERVICE CHECK. R & R EPSU FWD LT 10WL BATTERY ASSEMBLY, IAW AMM 33-51-39-000-005A & AMM 33-51-39-4
- [SDR F3LA2013032000838](https://openairdocs.org/sdr/F3LA2013032000838), Mar 18, 2013: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHT FAILED TEST, R & R POWER SUPPLY IAW AMM 33-51-00-710-001. OPS CHECKED NORMAL.
- [SDR F3LA2012061200768](https://openairdocs.org/sdr/F3LA2012061200768), Jun 7, 2012: POWER UNIT. OVERHEATED. GREEN SERVICE, ENG 1 OVERHEAT, TROUBLE SHOT GREEN HYD SYS IAW TSM 29-11-00-810-800-A. REPLACED PTU IAW AMM 29-23-41 PB401. LEAK AND OPS CHECKED NORMAL.
- [SDR F3LA2012060800766](https://openairdocs.org/sdr/F3LA2012060800766), Jun 4, 2012: HOSE. FAILED. AFTER GEAR RETRACTION ECAM - "HYD G ENG 1 PUMP LO PR". THIS WAS FOLLOWED BY "HYD GR RSVR LO LVL". AIR TURN BACK. PERFORMED ECAM ACTIONS AND RETURNED TO DEPARTUR
- [SDR F3LA2010090100496](https://openairdocs.org/sdr/F3LA2010090100496), Sep 3, 2010: ROLL PIN. BROKEN. C-CHECK: NON ROUTINE N0785. LT EMERGENCY EXIT SLIDE ARMING MECHANISM WILL NOT STAY IN ARMED POSITION. R & R SLIDE RELEASE MECHANISM SPRING PIN IAW AMM 52-21-11-
- [SDR F3LA2010090100495](https://openairdocs.org/sdr/F3LA2010090100495), Sep 3, 2010: SILL. CORRODED. C-CHECK: NON ROUTINE N0590, R2 DOOR SILL TRAY AT FRAME 66 HAS 1 AREA OF CORROSION AROUND NUT PLATE HOLE. REMOVED CORROSION IAW SRM 51-74-00. OPENED HOLE TO .310
- [SDR F3LA2010090100494](https://openairdocs.org/sdr/F3LA2010090100494), Sep 3, 2010: SEAT TRACK. CORRODED. C-CHECK: NON ROUTINE N0586, AFT MAIN CABIN, RT SEAT TRACK, YR2 DOOR SILL TRAY AT FRAME 66-Y122 AT FRAME 68 HAS 2 AREAS OF CORROSION ON UPPER SURFACE. REMOVED CO
- [SDR F3LA2010090100493](https://openairdocs.org/sdr/F3LA2010090100493), Sep 3, 2010: SEAT TRACK. CORRODED. C-CHECK, NON ROUTINE N0567, AFT MAIN CABIN RT SEAT TRACK YR2 DOOR SILL TRAY AT FRAME 66-Y122 AT FRAME 68 HAS 2 AREAS OF CORROSION ON UPPER SURFACE. REMOVED CORR
- [SDR F3LA2010083100489](https://openairdocs.org/sdr/F3LA2010083100489), Aug 24, 2010: FLOOR PANEL. CUT. C-CHECK; REF NON-ROUTINE N0681 AFT CARGO FLOOR PANEL 161BF HAS A 2 INCH CUT. REPAIRED 2 INCH CUT BY APPLYING RESIN AND GLASS CLOTH ON PANEL 161BF IAW SRM 53-02-
- [SDR F3LA2010083100488](https://openairdocs.org/sdr/F3LA2010083100488), Aug 24, 2010: FLOOR PANEL. CUT. C-CHECK; REF NON-ROUTINE N680 AFT CARGO FLOOR PANEL 162CF HAS A 7 INCH CUT. REPAIRED 7 INCH CUT BY APPLYING RESIN AND GLASS CLOTH IAW SRM 53-02-00 PARAGRAPH 8B.
- [SDR F3LA2010083100487](https://openairdocs.org/sdr/F3LA2010083100487), Aug 24, 2010: TRANSITION PANEL. PUNCTURED. C-CHECK; REFERENCE NON-ROUTINE N0696 BULK CARGO PIT SIDE TRANSITION PANEL HAS 2 EACH 1 INCH PUNCTURES. FABRICATED REPLACEMENT PANEL 161EF IAW MCG 1RM 9701 REV G
- [SDR F3LA2010031400365](https://openairdocs.org/sdr/F3LA2010031400365), Mar 14, 2010: EPSU. INOPERATIVE. DURING HEAVY SERVICE CHECK, MX NOTED EMERGENCY ISLE LIGHTS ON SEATS ABC ROWS 23, 22, 19, 18, 15, AND 14 ARE INOPERATIVE. MX R & R EMERGENCY POWER SUPPLY UNIT 13
- [SDR F3LA2009122900273](https://openairdocs.org/sdr/F3LA2009122900273), Dec 26, 2009: ADIRU. FAULTY. DURING CLIMB OUT, THE FLIGHT CREW RECEIVED AN IR1 FAULT. THE ACFT RETURNED TO DEPARTURE AND MX TROUBLESHOT AND REPLACED ADIRU 1 AT 1FP1 IAW AMM 34-12-34, AMM 34
- [SDR F3LA2009071400099](https://openairdocs.org/sdr/F3LA2009071400099), Jul 11, 2009: HEAT EXCHANGER. LEAKING. REF LOG PAGE 446358, DURING CLIMB OUT, PILOT REPORTED AN ELECTRONIC CENTRALIZED ACFT MONITORING MESSAGE FOR "AIR ENGINE BLEED LEAK" AND MADE AN AIR RETURN TO DE
- [SDR F3LA2009032700068](https://openairdocs.org/sdr/F3LA2009032700068), Mar 13, 2009: SKIN. DAMAGED. DURING OPERATIONS IN DEN, THE AIRCRAFT SUSTAINED BIRD STRIKE DAMAGE LOCATED ON THE RIGHT FORWARD FUSELAGE AT FRAME 5. 6.50 INCHES ABOVE Z508. MAINTENANCE CUT OU
- [SDR F3LA2009032700067](https://openairdocs.org/sdr/F3LA2009032700067), Mar 13, 2009: SKIN. DAMAGED. DURING OPERATIONS IN DEN, THE AIRCRAFT SUSTAINED BIRD STRIKE DAMAGE LOCATED ON THE RIGHT FORWARD FUSELAGE AT FRAME 4, 6.675 INCHES ABOVE Z508. MAINTENANCE CUT O
- [SDR F3LA2009012900017](https://openairdocs.org/sdr/F3LA2009012900017), Jan 28, 2009: PLATE. CORRODED. INSPECTION NOTED THE R2 DOOR AFT GIRT BAR BLANKING PLATE HAS CORROSION. MAINTENANCE REMOVED AND REPLACED BLANKING PLATE IAW AMM 52-13-31-400-003.
- [SDR F3LA2009012900016](https://openairdocs.org/sdr/F3LA2009012900016), Jan 28, 2009: PLATE. CORRODED. INSPECTION NOTED THE R2 DOOR FORWARD GIRT BAR FITTING BLANKING PLATE HAS CORROSION. MAINTENANCE REMOVED AND REPLACED BLANKING PLATE IAW AMM 52-13-31-400-007.
- [SDR F3LA2009012900015](https://openairdocs.org/sdr/F3LA2009012900015), Jan 28, 2009: FLOOR PANEL. CORRODED. INSPECTION NOTED THE L2 DOOR FLOOR PANEL 261FF HAS CORROSION. MAINTENANCE REMOVED AND REPLACED PANEL 261FF WITH NEW PER WORK CARD C534103-2 AND AMM 53-42-12-400
- [SDR F3LA2009012700014](https://openairdocs.org/sdr/F3LA2009012700014), Jan 27, 2009: PLATE. CORRODED. INSPECTION NOTED THAT THE L2 AFT DOOR GIRT BAR FITTING BLANKING PLATE HAS CORROSION. MAINTENANCE REMOVED AND REPLACED THE BLANKING PLATE IAW SRM 51-42-00, AMM 5
- [SDR F3LA2009012700013](https://openairdocs.org/sdr/F3LA2009012700013), Jan 27, 2009: PLATE. CORRODED. INSPECTION NOTED THAT THE L2 FORWARD DOOR GIRT BAR FITTING BLANKING PLATE HAS CORROSION. MAINTENANCE REMOVED AND REPLACED THE BLANKING PLATE IAW SRM 51-42-00, A
- [SDR F3LA2009012600012](https://openairdocs.org/sdr/F3LA2009012600012), Jan 25, 2009: BEAM. CORRODED. INSPECTION NOTED THE AFT GALLEY, RT BEAM AT FRAME 68 AND -1292, OUTBOARD ATTACHMENT HOLE HAS CORROSION AROUND IT. MAINTENANCE REPAIRED AREA IAW ENGINEERING AUTH
- [SDR F3LA2009012600011](https://openairdocs.org/sdr/F3LA2009012600011), Jan 25, 2009: FLOORBEAM. CORRODED. INSPECTION NOTED CORROSION AT NUTPLATES ON TOP OF FLOORBEAM LOCATED BETWEEN FRAME 66 AND FRAME 67 AT Y1292 LEFT. MAINTENANCE REMOVED AND REPLACED BEAM IAW SRM 5
- [SDR F3LA2009012600010](https://openairdocs.org/sdr/F3LA2009012600010), Jan 25, 2009: STRINGER. CRACKED. INSPECTION NOTED NR 2 ENGINE UPPER PYLON RIB 06 FORWARD INBOARD STRINGER WAS CRACKED AT CORNER HOLE. MAINTENANCE PERFORMED REPAIR BY FABRICATING SUPPORT ANGLE A
- [SDR F3LA2009012600009](https://openairdocs.org/sdr/F3LA2009012600009), Jan 24, 2009: SHEAR PLATE. CORRODED. INSPECTION NOTED SHEAR PLATE CORROSION IN THE AFT GALLEY, RT FROM FRAME 69 TO FRAME 70. MAINTENANCE REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-00, 51-72-11 
- [SDR F3LA2009012600008](https://openairdocs.org/sdr/F3LA2009012600008), Jan 24, 2009: SHEAR PLATE. CORRODED. INSPECTION NOTED SHEAR PLATE CORROSION IN THE AFT GALLEY, LT FROM FRAME 69 TO FRAME 70. MAINTENANCE REMOVED AND REPLACED THE SHEAR PLATE IAW SRM 51-42-00, 51-72
- [SDR F3LA2009012600007](https://openairdocs.org/sdr/F3LA2009012600007), Jan 24, 2009: SUPPORT FRAME. CORRODED. INSPECTION NOTED CORROSION ON THE SHEAR PLATE SUPPORT FRAME, LOCATED IN THE AFT GALLEY, LT FROM FRAME 69 TO FRAME 70. MAINTENANCE REMOVED AND REPLACED SUPPORT F
- [SDR F3LA2009012600006](https://openairdocs.org/sdr/F3LA2009012600006), Jan 24, 2009: SUPPORT FRAME. CORRODED. INSPECTION NOTED CORROSION ON THE SHEAR PLATE SUPPORT FRAME, LOCATED IN THE AFT GALLEY, RT FROM FRAME 69 TO FRAME 70. MAINTENANCE REMOVED AND REPLACED SUPPORT F
- [SDR F3LA2008123000729](https://openairdocs.org/sdr/F3LA2008123000729), Dec 25, 2008: MANIFOLD. LEAKING. PILOT RETURNED TO BLOCK DUE TO LOSS OF GREEN SYSTEM HYDRAULIC FLUID. MAINTENANCE REMOVED AND REPLACED LANDING GEAR SAFETY VALVE MANIFOLD IAW A319 AMM 32-32-17 P
- [SDR F3LA200700169](https://openairdocs.org/sdr/F3LA200700169), Jul 2, 2007: SLIDE. LOOSE. DURING C-2 CHECK, INSPECTION REPORTED L1 DOOR SLIDE CAME UNPACKED. REPLACED L1 DOOR SLIDE IAW AMM 25-62-44-000-002. OPERATIONAL CHECK GOOD.
- [SDR F3LA200700168](https://openairdocs.org/sdr/F3LA200700168), Jun 28, 2007: FLOOR PANEL. DELAMINATED. DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR PANEL 151ZG DELAMINATED AT RT SIDE OF PANEL AT CARGO DOOR OPENING. REPLACED FLOOR PANEL 151ZG 
- [SDR F3LA200700162](https://openairdocs.org/sdr/F3LA200700162), Jun 28, 2007: TRANSITION PANEL. PUNCTURED. DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT TRANSITION PANEL 161CF DAMAGED. REPAIRED PUNCTURES IN TRANSITION PANEL 161CF IAW SRM 53-02-00, PB 20
- [SDR F3LA200700161](https://openairdocs.org/sdr/F3LA200700161), Jun 28, 2007: TRANSITION PANEL. PUNCTURED. DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT TRANSITION PANEL 151HE DAMAGED. REPAIRED PUNCTURES IN TRANSITION PANEL 151HE IAW SRM 53-02-00, PB 20
- [SDR F3LA200700160](https://openairdocs.org/sdr/F3LA200700160), Jun 28, 2007: TRANSITION PANEL. PUNCTURED. DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT TRANSITION PANEL 151DE DAMAGED. REPAIRED PUNCTURES IN TRANSITION PANEL 151DE IAW SRM 53-02-00, PB 20
- [SDR F3LA200700167](https://openairdocs.org/sdr/F3LA200700167), Jun 27, 2007: FLOOR PANEL. DAMAGED. DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR PANEL 151CE DAMAGED. REPLACED FLOOR PANEL 151CE IAW AMM 53-42-11-400-001.
- [SDR F3LA200700166](https://openairdocs.org/sdr/F3LA200700166), Jun 27, 2007: TRANSITION PANEL. PUNCTURED. DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT TRANSITION PANEL 161BF PUNCTURED ON TOP SKIN. REPLACED TRANSITION PANEL 161BF IAW AMM 53-42-14-400-0
- [SDR F3LA200700165](https://openairdocs.org/sdr/F3LA200700165), Jun 27, 2007: RELEASE CABLE. OUT OF ADJUST. DURING C-2 CHECK, INSPECTION REPORTED OPERATIONAL TESTS OF BOTH OVERWING RELEASE SLIDE CABLES FAILED. ADJUSTED LT AND RT EMERGENCY SLIDE EXIT RELEASE CABLES IAW
- [SDR F3LA200700164](https://openairdocs.org/sdr/F3LA200700164), Jun 27, 2007: TRANSITION PANEL. PUNCTURED. DURING C-2 CHECK, INSPECTION REPORTED HOLES IN AFT CARGO COMPARTMENT FWD RT LOWER TRANSITION PANEL 152WG. REPLACED TRANSITION PANEL 152WG IAW AMM 53-42-14-400-0
- [SDR F3LA200700163](https://openairdocs.org/sdr/F3LA200700163), Jun 27, 2007: TRANSITION PANEL. PUNCTURED. DURING C-2 CHECK, INSPECTION REPORTED HOLES IN AFT CARGO COMPARTMENT LT UPPER TRANSITION PANEL 151UG. REPLACED TRANSITION PANEL 151UG IAW AMM 53-42-14-000-001.
- [SDR F3LA200700159](https://openairdocs.org/sdr/F3LA200700159), Jun 27, 2007: TRANSITION PANEL. PUNCTURED. DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT TRANSITION PANEL 151AE DAMAGED. REPAIRED PUNCTURES IN TRANSITION PANEL 151AE IAW SRM 53-02-00, PB 20
- [SDR F3LA200700158](https://openairdocs.org/sdr/F3LA200700158), Jun 27, 2007: FLOOR PANEL. PUNCTURED. DURING C-2 CHECK, INSPECTION REPORTED TOP SKIN PUNCTURED ON AFT CARGO COMPARTMENT FLOOR PANEL 161NF. REPAIRED PUNCTURES ON FLOOR PANEL 161NF IAW SRM 53-02-00, P
- [SDR F3LA200700157](https://openairdocs.org/sdr/F3LA200700157), Jun 27, 2007: FLOOR PANEL. DAMAGED. DURING C-2 CHECK, INSPECTION REPORTED HOLES IN TOP SURFACE OF AFT CARGO COMPARTMENT FLOOR PANEL 151PE. REPAIRED HOLES IN FLOOR PANEL 151PE IAW SRM 53-02-00, PB2
- [SDR F3LA200700156](https://openairdocs.org/sdr/F3LA200700156), Jun 27, 2007: FLOOR PANEL. DAMAGED. DURING C-2 CHECK, INSPECTION REPORTED HOLES IN TOP SURFACE OF AFT CARGO COMPARTMENT FLOOR PANEL 151VG. REPAIRED HOLES IN FLOOR PANEL 151VG IAW SRM 53-02-00, PB 
- [SDR F3LA200700155](https://openairdocs.org/sdr/F3LA200700155), Jun 27, 2007: FLOOR PANEL. DAMAGED. DURING C-2 CHECK, INSPECTION REPORTED HOLES IN TOP SURFACE OF AFT CARGO COMPARTMENT FLOOR PANEL 161NF. REPAIRED HOLES IAW SRM 53-02-00, FIG 204.
- [SDR F3LA200700154](https://openairdocs.org/sdr/F3LA200700154), Jun 27, 2007: FLOOR PANEL. DAMAGED. DURING C-2 CHECK, INSPECTION REPORTED HOLES IN TOP SURFACE OF AFT CARGO COMPARTMENT FLOOR PANEL 161PF. REPAIRED HOLES IN FLOOR PANEL 161PF IAW SRM 53-02-00, FIG
- [SDR F3LA200700153](https://openairdocs.org/sdr/F3LA200700153), Jun 27, 2007: TRANSITION PANEL. DAMAGED. DURING C-2 CHECK, INSPECTION REPORTED HOLES IN AFT CARGO COMPARTMENT TRANSITION PANEL 152BF. REPAIRED HOLES IN TRANSITION PANEL 152BF IAW SRM 53-02-00, FIG 204.
- [SDR F3LA200700152](https://openairdocs.org/sdr/F3LA200700152), Jun 27, 2007: TRANSITION PANEL. DAMAGED. DURING C-2 CHECK, INSPECTION REPORTED HOLES IN AFT CARGO COMPARTMENT TRANSITION PANEL 162CF. REPAIRED TRANSITION PANEL 162CF IAW SRM 53-02-00, FIG. 204.
- [SDR F3LA200700151](https://openairdocs.org/sdr/F3LA200700151), Jun 27, 2007: FLOOR PANEL. DAMAGED. DURING C-2 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT FLOOR PANEL 131AF DAMAGED. REPAIRED FLOOR PANEL 131AF IAW SRM 53-02-00, FIG 204.

All 60: https://openairdocs.org/deregistered/N934FR-2016-09-12/reports.md

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