# N942FR: 2005 Airbus A319-111, registration cancelled 2012-10-17

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 17, 2012
- 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: 2497
- Year built: 2005
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 24, 2005
- Certificate issued: June 23, 2005
- Last registry action: July 27, 2011
- Mode S code: AD1523
- 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: 41.0534° N, 73.5387° W: Placed by OpenAirDocs: center of Stamford, CT, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N942FR
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=942FR
- Page: https://openairdocs.org/deregistered/N942FR-2012-10-17

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 (40)

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

- [SDR F3LA2012051600756](https://openairdocs.org/sdr/F3LA2012051600756), May 15, 2012: BATTERY. DISCHARGED. WHILE ACCOMPLISHING CARD A332204-02 ON THE A6 CHECK THE POWER SUPPLY UNIT, 10 WL BATTERY FAILED THE CAPACITY TEST. ACFT OUT OF SERVICE. POWER SUPPLY UNIT BATTER
- [SDR F3LA2012041800741](https://openairdocs.org/sdr/F3LA2012041800741), Apr 13, 2012: SWITCH. INTERMITTENT. PATH LIGHTING AND EMERGENCY EXIT LGHTS COMING ON INTERMITTENTLY. REPLACED TOGGLE SWITCH, SIGNS & EMERGENCY EXIT LIGHT IAW ESPM 20-45-21. TEST OK REF AMM 33-51-0
- [SDR F3LA2011092600680](https://openairdocs.org/sdr/F3LA2011092600680), Sep 25, 2011: HOSE. RUPTURED. ON DEPARTURE, GREEN SYS FAILURE (FLUID LOSS) R & R LT MLG SWIVEL JOINT REF AMM 32-31-38-000, PB401. R & R FLEX HOSE ASSY REF AMM 32-31-39-000, PB 401. OPS LEAK 
- [SDR F3LA2011080300662](https://openairdocs.org/sdr/F3LA2011080300662), Aug 3, 2011: CONNECTOR. MISINSTALLED. EXTERIOR OVERWING EMERGENCY LIGHTS INOP". "FOUND BOTH EXTERNAL OVERWING EMERGENCY LIGHTS ON THE RT SIDE WERE NOT CONNECTED TO ACFT WIRING. RECONNECTED CONNECTOR
- [SDR F3LA2011063000658](https://openairdocs.org/sdr/F3LA2011063000658), Jun 25, 2011: SILL. CORRODED. C-CHECK: L-2 DOOR SILL AT FR66 HAS CORROSION. REPAIRED L-2 DOOR SILL AT FR66 IAW 53-41-14, FIG 201, REPAIR PRINCIPLE 6.
- [SDR F3LA2011063000657](https://openairdocs.org/sdr/F3LA2011063000657), Jun 25, 2011: SILL. CORRODED. C-CHECK: NON ROUTINE NR 38830; R-2 DOOR SILL AT FR66 Y-1500 HAS CORROSION OUT OF LIMITS. REPAIRED R-2 DOOR SILL AT FR66 IAW SRM 53-41-14, FIG 201, REPAIR PRINCI
- [SDR F3LA2011052300652](https://openairdocs.org/sdr/F3LA2011052300652), May 19, 2011: PUMP. LEAKING. PILOT REPORT YELLOW HYDRAULIC LOW RESERVOIR LEVEL. REMOVED AND REPLACED ENGINED NR2 HYDRAULIC PUMP DRIVER IAW AMM 29-13-51, PB 401, OPS CHECKS GOOD. FOUND SEVER
- [SDR F3LA2011031500615](https://openairdocs.org/sdr/F3LA2011031500615), Mar 11, 2011: BATTERY PACK. FAILED. EPSU BATTERY 13WL FAILED OPS TEST IAW REPLACED BATTERY PACK 13WL IAW AMM 33-51-38-400-002.
- [SDR F3LA2011011800586](https://openairdocs.org/sdr/F3LA2011011800586), Jan 13, 2011: HOSE. LEAKING. DURING CLIM, AFTER RETRACTING THE LANDING GEAR, VISUAL GREEN HYD LOW PRESSURE MESSAGE. MANUAL GEAR EXTENTION PERFORMED. AIR TURN BACK, REPLACED RT MLG AFT HYD H
- [SDR F3LA2010012900322](https://openairdocs.org/sdr/F3LA2010012900322), Jan 28, 2010: PROXIMITY SWITCH. MALFUNCTIONED. DURING C3 C CHECK INSP NOTED EXIT OVERWING EMERGENCY EXTERIOR LIGHTS ON THE RT SIDE DO NOT COME ON WHEN DISARMING OVER WING EXIT DOOR. MX REMOVED AND REPLACED P
- [SDR F3LA2010012900323](https://openairdocs.org/sdr/F3LA2010012900323), Jan 26, 2010: CONNECTOR. INOPERATIVE. REFERENCE NON ROUTINE C078794. DURING C3 C CHECK INSP NOTED THE OPS TEST OF THE EMERGENCY LIGHTS WITH THE MCDU FAULTING. MX REPAIRED IAW AMM 33-51-38-000-001, A
- [SDR F3LA2010012600320](https://openairdocs.org/sdr/F3LA2010012600320), Jan 20, 2010: BLANKING PLATE. CORRODED. DURING C3 C CHECK INSPECTION NOTED BLANKING PLATE CORRODED ON AFT PLATE R2 DOOR. MX REMOVED AND REPLACED PLATE IAW AMM 52-13-31-400-007.
- [SDR F3LA2010012600319](https://openairdocs.org/sdr/F3LA2010012600319), Jan 20, 2010: BLANKING PLATE. CORRODED. DURING C3 C CHECK INSPECTION NOTED BLANKING PLATE CORRODED FORWARD R2 DOOR. MX REMOVED AND REPLACED PLATE IAW AMM 52-13-31-400-007.
- [SDR F3LA2010012600318](https://openairdocs.org/sdr/F3LA2010012600318), Jan 20, 2010: BLANKING PLATE. CORRODED. DURING C3 C CHECK INSPECTION NOTED BLANKING PLATE CORRODED AFT PLATE L2 DOOR. MX REMOVED AND REPLACED PLATE IAW AMM 52-13-31-400-007.
- [SDR F3LA2010012600317](https://openairdocs.org/sdr/F3LA2010012600317), Jan 20, 2010: BLANKING PLATE. CORRODED. DURING C3 C CHECK INSPECTION NOTED BLANKING PLATE CORRODED FORWARD PLATE L2 DOOR. MX REMOVED AND REPLACED PLATE IAW AMM 52-13-400-007.
- [SDR F3LA2010012600316](https://openairdocs.org/sdr/F3LA2010012600316), Jan 20, 2010: FLOORBOARD. CORRODED. DURING C3 C CHECK INSPECTION NOTED FLOOR PANEL 261FF WAS CORRODED. MX REMOVED AND REPLACED FLOOR PANEL 261FF IAW AMM 53-42-12-400-002.
- [SDR F3LA2010012600312](https://openairdocs.org/sdr/F3LA2010012600312), Jan 20, 2010: FLOOR PANEL. CORRODED. DURING C3 C CHECK INSP NOTED FLOOR PANEL 262FF WAS CORRODED. MX REMOVED AND REPLACED FLOOR PANEL 262FF IAW TASK CARD C534103-02.
- [SDR F3LA2010012100308](https://openairdocs.org/sdr/F3LA2010012100308), Jan 19, 2010: SUPPORT. CORRODED. DURING C3 C-CHECK INSP NOTED THE LT FRAME SUPPORT AT FRAME 70 HAS CORROSION ON THE BOTTOM SIDE AT NUTPLATE HOLES. MX REMOVED AND REPLACED SUPPORT FRAME IAW SRM 
- [SDR F3LA2010012600315](https://openairdocs.org/sdr/F3LA2010012600315), Jan 18, 2010: FLOORBEAM. CORRODED. DURING C3 C CHECK INSP NOTED Y1292 FROM FRAME 60 TO FRAME 68 ALL SCREW HOLES ARE CORRODED ON UPPER AND LOWER AREAS. MX REMOVED AND REPLACED FLOORBEAM IAW SRM 51
- [SDR F3LA2010012600314](https://openairdocs.org/sdr/F3LA2010012600314), Jan 18, 2010: PLATE. CORRODED. DURING C3 C CHECK INSP NOTED PLATE BETWEEN Y1292 AND L2 THRESHOLD AT FRAME 66 IS CORRODED. MX REMOVED AND REPLACED PLATE IAW SRM 51-74-00, SRM 51-75-12 AND DWG 
- [SDR F3LA2010012600313](https://openairdocs.org/sdr/F3LA2010012600313), Jan 18, 2010: FLOORBEAM. CORRODED. DURING C3 C CHECK INSP NOTED Y1292 JUST AFT OF FRAME 68 HAS A LARGE AREA OF CORROSION ON TOP SIDE WHICH EXTENDS UNDER GALLEY FLOORBOARD. MX REMOVED AND REPLACED
- [SDR F3LA2010012200311](https://openairdocs.org/sdr/F3LA2010012200311), Jan 18, 2010: PLATE. CORRODED. DURING C3 C CHECK INSP NOTED LT SHEAR PLATE AT FRAME 70 HAS SURFACE CORROSION AND APPEARS TO BE COMING FROM UNDER GALLEY FLOORBOARD. MX REMOVED AND REPLACED SHE
- [SDR F3LA2010012200310](https://openairdocs.org/sdr/F3LA2010012200310), Jan 18, 2010: SILL. CORRODED. DURING C3 C-CHECK INSP NOTED L2 DOOR SILL FASTENER HOLE AFT OF AFT GIRT BAR MOUNT FITTING HAS CORROSION. MX REPAIRED IAW EA A9-53R-31638, SRM 51-74-00, SRM 53-4
- [SDR F3LA2010012200309](https://openairdocs.org/sdr/F3LA2010012200309), Jan 18, 2010: SILL. CORRODED. DURING C3 C CHECK INSPECTION NOTED L2 DOOR FASTENER HOLES INBD OF AFT GIRT BAR MOUNT FITTING HAS CORROSION. MX REPAIRED IAW EA A9-53R-31638, SRM 53-41-14, NTM 5
- [SDR F3LA2010012100307](https://openairdocs.org/sdr/F3LA2010012100307), Jan 18, 2010: PLATE. CORRODED. DURING C3 C-CHECK INSP NOTED THE RT SHEAR PLATE AT FRAME 70 HAS SURFACE CORROSION AND APPEARS TO BE COMING FROM UNDER GALLEY FLOORBOARD. MX REMOVED AND REPLACED
- [SDR F3LA2010012100306](https://openairdocs.org/sdr/F3LA2010012100306), Jan 18, 2010: SILL. CORRODED. DURING C3 C-CHECK INSP NOTED THE L2 DOOR SILL INBD FLANGE FASTENER HOLE CORRODED. MX REPAIRED IAW SRM 53-41-14, SRM 51-23-11 AND SRM 51-42-11.
- [SDR F3LA2010012000305](https://openairdocs.org/sdr/F3LA2010012000305), Jan 18, 2010: PLATE. CORRODED. DURING C3 C-CHECK INSP NOTED THE RT SHEAR PLATE AT FRAME 70 HAS SURFACE CORROSION AND APPEARS TO BE COMING FROM UNDER GALLEY FLOORBOARD. MX REMOVED AND REPLACED
- [SDR F3LA2009063000095](https://openairdocs.org/sdr/F3LA2009063000095), Jun 25, 2009: SENSOR. FAILED. FLIGHT CREW DIVERTED. PILOT REPORTED LOST TOTAL AIR TEMPERATURE AND STATIC AIR TEMPERATURE INDICATIONS. MX REMOVED AND REPLACED THE NR 1 TOTAL AIR TEMPERATURE S
- [SDR F3LA200800518](https://openairdocs.org/sdr/F3LA200800518), Jul 22, 2008: FLOOR PANEL. GOUGED. DURING C-CHECK, INSP NOTED THE AFT CARGO PIT AFT RT LOWER TRANSITION PANEL 162BF WAS GOUGED AND A PREVIOUS REPAIR WAS PEELING UP. MAINT REPAIRED TRANSITION PANE
- [SDR F3LA200800509](https://openairdocs.org/sdr/F3LA200800509), Jul 22, 2008: FLOOR PANEL. PEELING. DURING C-CHECK, INSP NOTED THE PREVIOUS REPAIRS PEELING LOOSE ON THE AFT CARGO PIT FWD LT UPPER TRANSITION PANEL 151UG. MAINT REPAIRED TRANSITION PANEL 151UG IA
- [SDR F3LA200800510](https://openairdocs.org/sdr/F3LA200800510), Jul 22, 2008: FLOOR PANEL. PUNCTURED. DURING C2 C-CHECK, INSP NOTED THE AFT CARGO PIT FWD RT LOWER TRANSITION PANEL 152WG WAS PUNCTURED. MAINT REPAIRED TRANSITION PANEL 152WG IAW SRM 53-02-00 FIGURE
- [SDR F3LA200800511](https://openairdocs.org/sdr/F3LA200800511), Jul 22, 2008: FLOOR PANEL. PUNCTURED. DURING C2 C-CHECK, INSP NOTED THE AFT CARGO PIT FWD LT UPPER TRANSITION PANEL 151BE WAS PUNCTURED. MAINT REPAIRED TRANSITION PANEL 151BE IAW SRM 53-02-00 FIGURE
- [SDR F3LA200800512](https://openairdocs.org/sdr/F3LA200800512), Jul 22, 2008: FLOOR PANEL. GOUGED. DURING C-CHECK, INSP NOTED THE AFT CARGO PIT FORWARD LT LOWER TRANSITION PANEL 151AE WAS GOUGED IN THE CENTER OF THE PANEL. MAINT REPAIRED TRANSITION PANEL 151A
- [SDR F3LA200800513](https://openairdocs.org/sdr/F3LA200800513), Jul 22, 2008: FLOOR PANEL. PUNCTURED. DURING C-CHECK, INSP NOTED THE AFT CARGO PIT CENTER LT UPPER TRANSITION PANEL 151FE WAS PUNCTURED. MAINT REPAIRED TRANSITION PANEL 151FE IAW SRM 53-02-00 FIGURE
- [SDR F3LA200800514](https://openairdocs.org/sdr/F3LA200800514), Jul 22, 2008: FLOOR PANEL. PUNCTURED. DURING C-CHECK, INSP NOTED THE AFT CARGO PIT CENTER LT LOWER TRANSITION PANEL 151DE WAS PUNCTURED. MAINT REPAIRED TRANSITION PANEL 151DE IAW SRM 53-02-00 FIGURE
- [SDR F3LA200800515](https://openairdocs.org/sdr/F3LA200800515), Jul 22, 2008: FLOOR PANEL. PUNCTURED. DURING C-CHECK, INSP NOTED THE AFT CARGO PIT FLOOR PANEL 161NF WAS PUNCTURED SEVERAL TIMES. MAINT REPAIRED FLOOR PANEL 161NF IAW SRM 53-02-00 FIGURE 204. UPON C
- [SDR F3LA200800516](https://openairdocs.org/sdr/F3LA200800516), Jul 22, 2008: FLOOR PANEL. PUNCTURED. DURING C-CHECK, INSP NOTED THE AFT CARGO PIT AFT LT UPPER TRANSITION PANEL 161CF WAS PUNCTURED IN THE CENTER, COVERED WITH TAPE. MAINT REPAIRED TRANSITION PANEL
- [SDR F3LA200800517](https://openairdocs.org/sdr/F3LA200800517), Jul 22, 2008: FLOOR PANEL. PUNCTURED. DURING C-CHECK, INSP NOTED THE AFT CARGO PIT AFT LT LOWER TRANSITION PANEL 161BF WAS PUNCTURED. MAINT REPAIRED TRANSITION PANEL 161BF IAW SRM 53-02-00 FIGURE 20
- [SDR F3LA200600124](https://openairdocs.org/sdr/F3LA200600124), Sep 21, 2006: GUST LOCK. INOPERATIVE. FOUND GUST LOCK 1L INOP. ADJUSTED BUFFER PER AMM 52-11-12-820. RII INSPECTION ACCOMPLISHED. AIRCRAFT RELEASED FOR SERVICE.
- [SDR F3LA200500045](https://openairdocs.org/sdr/F3LA200500045), Nov 22, 2005: ODOR. DETECTED. FLIGHT CREW RECEIVED LIVE TV SMOKE INDICATION. FLIGHT ATTENDANT REPORTED AN ELECTRIC ODOR IN AFT GALLEY. DECLARED AM EMERGENCY AND LANDED WITHOUT INCIDENT IN DE

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