# N939FR: 2005 Airbus A319-112, registration cancelled 2022-08-22

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 22, 2022
- Status when cancelled: Valid registration
- Airframe: [Airbus A319-112](https://openairdocs.org/model/airbus-a319-112) (registry code 3940009)
- Engine: [CFM International CFM56-5B6/P series](https://openairdocs.org/engine/cfm-international-cfm56-5b6-p-series) (registry code 13018)
- Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM) (OpenAirDocs)
- Serial number: 2448
- Year built: 2005
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 26, 2013
- Certificate issued: February 26, 2013
- Last registry action: November 12, 2021
- Mode S code: AD07A5
- Owner when cancelled: [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N939FR
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=939FR
- Page: https://openairdocs.org/deregistered/N939FR-2022-08-22

From the FAA registry file of November 3, 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 A319-112: https://openairdocs.org/model/airbus-a319-112.md

## Service difficulty reports (67, newest 50)

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

- [SDR F3LA2018112800479](https://openairdocs.org/sdr/F3LA2018112800479), Nov 23, 2018: HYDRAULIC LINE. LEAKING. HYD G RSVR LO LVL. AIRCRAFT WAS GROUNDED DUE TO THIS DISCREPANCY. REMOVED AND REPLACED NR 1 ENG PRESSURE/SUCTION/RETURN LINE, REF AMM 29-11-49 PB401. NO LEAKS A
- [SDR F3LA2018090400420](https://openairdocs.org/sdr/F3LA2018090400420), Aug 22, 2018: DOOR FRAME. CRACKED. FOUND CRACKS ON LT NR 1 EMERGENCY EXIT. LOCATED ON FWD AND AFT SEGMENTS AND ON THE FWD AND AFT SEGMENTS ON RT NR 1 EMERGENCY EXIT. ACCOMPLISHED OVERWING EMERGEN
- [SDR F3LA2018083000418](https://openairdocs.org/sdr/F3LA2018083000418), Aug 19, 2018: HYDRAULIC LINE. CRIMPED. HYDRAULIC LINE IN THE RT AFT UPPER MLG WW WAS DAMAGED. REMOVED AND REPLACED THE HYD LINE IAW AMM 32-43-00-710-001-A, 32-43-00-870-002-A, 12-12-29-611-002-A, AND
- [SDR F3LA2018083000417](https://openairdocs.org/sdr/F3LA2018083000417), Aug 19, 2018: HYDRAULIC LINE. RUPTURED. HYDRAULIC LINE AT THE LT AFT UPPER MLG WW WAS RUPTURED. REMOVED RUPTURED ALTERNATE BRAKING HYDRAULIC LINE & REPLACED WITH NEW IAW AMM 20-23-11-911-001-A. PERFOR
- [SDR F3LA2018083000419](https://openairdocs.org/sdr/F3LA2018083000419), Aug 17, 2018: FLOORBEAM. CORRODED. DISCREPANCY: CORROSION AROUND HARD POINT, BEAM -Y765 FR66. CORRECTIVE ACTION: REFERENCE PEMCO N/R 2082N289 REMOVED AND REPLACED NEW FLOOR BEAM -Y765 IAW A319 SR
- [SDR F3LA2018082700409](https://openairdocs.org/sdr/F3LA2018082700409), Aug 17, 2018: FLOOR SUPPORT. CORRODED. CORROSION FOUND ON THE RT FLOOR SUPPORT, -Y1292, FRAMES 66 - 68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, 51-44-11, AND 53-41-14-283-004.
- [SDR F3LA2018082700408](https://openairdocs.org/sdr/F3LA2018082700408), Aug 16, 2018: FLOOR SUPPORT. CORRODED. LEFT FLOOR SUPPORT, Y1162 WAS CORRODED BETWEEN FRAMES 66 - 69. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001, AND 53-00-14-282-002.
- [SDR F3LA2018082400402](https://openairdocs.org/sdr/F3LA2018082400402), Aug 16, 2018: FLOORBEAM. CORRODED. DISCREPANCY: REFERENCE NR 2082N250, LH FLOORBEAM Y765 HAS CORROSION AT FR66. CORRECTIVE ACTION: REMOVED AND REPLACED AFT WET AREA FLOORBEAM AT FR66 LOC Y765 IAW
- [SDR F3LA2018082400401](https://openairdocs.org/sdr/F3LA2018082400401), Aug 16, 2018: FLOORBEAM. CORRODED. DISCREPANCY: REFERENCE NR 2082N247, RH AFT FLOORBEAM -Y1162 HAS CORROSION AROUND FASTENER HOLE FR68. CORRECTIVE ACTION: REMOVED AND REPLACED FLOORBEAM -Y1162 IA
- [SDR F3LA2018082300400](https://openairdocs.org/sdr/F3LA2018082300400), Aug 16, 2018: FLOOR SUPPORT. CORRODED. LH FLOOR SUPPORT Y512 HAS CORROSION AROUND FASTENER HOLE FR66. REMOVED AND REPLACED FLOOR SUPPORT Y512 FR66 TO 70 IAW SRM 51-72-11-911-002, 53-00-14-283-002 AND
- [SDR F3LA2016100400063](https://openairdocs.org/sdr/F3LA2016100400063), Sep 22, 2016: DOOR FRAME. CRACKED. RIGHT EMERGENCY OVERWING EXIT FWD AND AFT I/B FRAME HAS INDICATIONS OF CRACKS. REMOVED AND REPLACED IAW SRM 51-42-11.
- [SDR F3LA2016100400062](https://openairdocs.org/sdr/F3LA2016100400062), Sep 20, 2016: DOOR FRAME. CRACKED. LEFT EMERGENCY OVERWING EXIT AFT INBD DOOR FRAME HAS INDICATIONS OF CRACKS. REMOVED AND REPLACED EMERGENCY EXIT AFT DOOR FRAME IAW SRM 51-42-11.
- [SDR F3LA2016100400064](https://openairdocs.org/sdr/F3LA2016100400064), Sep 19, 2016: FLOOR SUPPORT. CORRODED. AFT CABIN FRAME 66+10 THROUGH 68+6 Y1292 FLOOR SUPPORT TOP FLANGE CORRODED AT MULTIPLE LOCATIONS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.
- [SDR F3LA2016091900059](https://openairdocs.org/sdr/F3LA2016091900059), Sep 10, 2016: FLOORBEAM. CORRODED. AFT CABIN, FRAME 66, Y508 FLOORBEAM CORRODED AT MULTIPLE LOCATIONS. REMOVE CORROSION MAXIMUM DEPTH OF REWORK IS .016, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14
- [SDR F3LA2016091900058](https://openairdocs.org/sdr/F3LA2016091900058), Sep 10, 2016: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM Y1292, FASTENER HOLE BETWEEN FRAME 20 AND FRAME 18. R & R FLOORBEAM AT Y1292, FRAME 12-24 IAW SRM 51-72-11-911 AND SRM 51-21-11.
- [SDR F3LA2016091900057](https://openairdocs.org/sdr/F3LA2016091900057), Sep 10, 2016: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM Y1292 BETWEEN FRAME 17 AND FRAME 20. R & R FLOORBEAM AT Y1292, FRAME 17 AND FRAME 20 IAW SRM 51-72-11, 51-42-11, 51-44-11.
- [SDR F3LA2016091900056](https://openairdocs.org/sdr/F3LA2016091900056), Sep 10, 2016: FLOORBEAM. CORRODED. AFT CABIN FRAME 67-FRAME 68, Y765, FLOORBEAM TOP FLANGE CORRODED AT MULTIPLE LOCATIONS. R & R AFT CABIN FLOORBEAM Y765 AT FRAME 67-FRAME 68 IAW SRM 51-72-11.
- [SDR F3LA2014091101069](https://openairdocs.org/sdr/F3LA2014091101069), Sep 11, 2014: STRUCTURE. CORRODED. C6 CHECK. PAX CABIN FROM FRAME 69 - 70 RT - Y1292 HAS SURFACE CORROSION AT FIVE EACH MULTIPLE FASTENERS HOLES AT SKIN PLATE. R & R SKIN PLATE IAW EO A0-53EO-314
- [SDR F3LA2014081801053](https://openairdocs.org/sdr/F3LA2014081801053), Aug 18, 2014: BATTERY. DISCHARGED. EPSU EMER LIGHTS BATTERY 12WL FAILED CAPACITY TEST ON TASK CARD A332204-02. R & R THE EPSU BATTERY ASSEMBLY IAW AMM 33-51-38-000-002A & 33-51-38-400-002A.
- [SDR F3LA2014020701005](https://openairdocs.org/sdr/F3LA2014020701005), Feb 7, 2014: SLIDE. LOW PRESSURE. DOOR R2 SLIDE PRESS LOW. R & R R2 DOOR ESCAPE SLIDE IAW AMM 25-62-44 PB 401.
- [SDR F3LA2013062100868](https://openairdocs.org/sdr/F3LA2013062100868), Jun 17, 2013: BLEED AIR SYS. ODOR. ODOR IN CABIN AT LOW ALTITUDES, BOTH TAKEOFF AND APPROACH (AROUND 10,000' AGL) STRONG ODOR AROUND ROW 20-22. RAN APU, ENGINE NR 1 AND ENGINE NR 2 AND COULD NOT 
- [SDR F3LA2012121900822](https://openairdocs.org/sdr/F3LA2012121900822), Dec 17, 2012: POWER SUPPLY. INOPERATIVE. C-CHECK, EMERGENCY LIGHT SYS TEST FAILED FOR FWD EPSU 10WL. R & R EPSU IAW AMM 33-51-38-020-051-A. SYSTEM OPS GOOD IAW 33-51-38-740-050-B.
- [SDR F3LA2012082300778](https://openairdocs.org/sdr/F3LA2012082300778), Aug 21, 2012: A/C PACK. SMOKE. ECAM MESSAGE NR 2 PACK OVERHEAT, ON DEPARTURE CLIMBING THROUGH 11,000 F/A CALLED WITH INFO ON SMOKE IN CABIN (AFT), ODOR WAS NOTABLE BUT DISSIPATING. EMERGENCY 
- [SDR F3LA2011051900646](https://openairdocs.org/sdr/F3LA2011051900646), May 19, 2011: FLOORBEAM. CORRODED. C-CHECK: NON ROUTINE NR 1287; CORROSION ON UPPER SURFACE OF RT AFT ENTRY AREA, FLOORBEAM AT FR 68, RBL 48, FOUND TO BE OUT OF LIMITS. R & R FLOORBEAM AT FR 68, 
- [SDR F3LA2011501900645](https://openairdocs.org/sdr/F3LA2011501900645), May 13, 2011: FLOOR PANEL. DELAMINATED. C-CHECK: CABIN FLOOR PANEL 241JF HAS DELAMINATION IN SEVERAL AREAS AND FOUND TO BE OUT OF REPAIRABLE LIMITS. R & R FLOOR PANEL 241JF IAW SRM 53-02-00, PB 101.
- [SDR F3LA201151900644](https://openairdocs.org/sdr/F3LA201151900644), May 13, 2011: FLOOR SUPPORT. CORRODED. C-CHECK: CORROSION ON UPPER SURFACE OF RT AFT ENTRY AREA, FLOORBEAM AT FR 68, RBL 30. R & R FLOORBEAM AT FR 66-70, RBL 30 IAW SRM 51-74-00.
- [SDR F3LA201151900643](https://openairdocs.org/sdr/F3LA201151900643), May 13, 2011: SHEAR PLATE. CRACKED. C-CHECK: NON ROUTINE NR1262; LT AFT LATERAL SHEAR PLATE IS CRACKED, FR69, STR 24. REPLACED LT AFT LATERAL SHEAR PLATE WITH NEW CONFIGURATION IAW EO A0-53EO-3143
- [SDR F3LA201151900642](https://openairdocs.org/sdr/F3LA201151900642), May 13, 2011: FLOORBOARD. DAMAGED. C- CHECK: NON ROUTINE NR1329: COCKPIT FLOORBOARD, 211GF SURFACE IS DAMAGED. FOUND DAMAGE TO FLOORBOARD 211GF BEYOND REPAIRABLE LIMITS. REPLACED FLOORBOARD IAW S
- [SDR F3LA2010071800471](https://openairdocs.org/sdr/F3LA2010071800471), Jul 15, 2010: COMPUTER. FAULTED. REF: PILOT REPORT LOG PAGE 549851 ITEM 1. CLIMBING THROUGH FLIGHT LEVEL 380 ELAC NR 2 FAULTED, ACFT WENT INTO ALTERNATE LAW. AIR TURN BACK TO SMF. REPLACED NR 2
- [SDR F3LA2009122800272](https://openairdocs.org/sdr/F3LA2009122800272), Dec 25, 2009: FITTING. OUT OF ADJUST. DURING LANDING THE FLIGHT CREW NOTED THE L2 DOOR SLIDING ARMING LEVER DISARMS IN FLIGHT AND APPEARS RELATED TO CABIN PRESSURE DIFFERENTIAL ABOVE 10000 FEET. MX 
- [SDR F3LA2009122800271](https://openairdocs.org/sdr/F3LA2009122800271), Dec 25, 2009: FITTING. OUT OF ADJUST. DURING CRUISE ALTITUDE, THE FLIGHT CREW NOTED THE L2 DOOR ARM LIGHT WAS ON AND INTERMITTENT. MX ADJUSTED THE GIRT BAR FITTING FOR THE L2 DOOR AND PERFORMED A TE
- [SDR F3LA2009122200259](https://openairdocs.org/sdr/F3LA2009122200259), Dec 18, 2009: WIRE. BROKEN. DURING C3 C-CHECK INSP NOTED SEAT ROW 10B AND 10C EMERGENCY EXIT LIGHT WIRE WAS BROKEN AT CONNECTOR OTBD SEAT LEG GOING TO FLOOR. MX REMOVED AND REPLACED EMERGE
- [SDR F3LA2009122300266](https://openairdocs.org/sdr/F3LA2009122300266), Dec 17, 2009: SILL. CORRODED. DURING C3 C-CHECK INSP, NOTED THE L2 DOOR SILL CORRODED AT FWD SPLICE IN AND AROUND THE FLOORBOARD ATTACH HOLE. MX REPAIRED DOOR SILL IAW SRM 53-41-14 AND EA A9
- [SDR F3LA2009122300265](https://openairdocs.org/sdr/F3LA2009122300265), Dec 16, 2009: FLOOR PANEL. CORRODED. DURING C3 C-CHECK INSP, NOTED MAIN CABIN FLOOR PANEL 261FF HAS CORROSION. MX REMOVED AND REPLACED FLOOR PANEL 261FF IAW AMM 53-42-12-400-002.
- [SDR F3LA2009122200261](https://openairdocs.org/sdr/F3LA2009122200261), Dec 16, 2009: FLOORBEAM. CORRODED. DURING C3 C-CHECK INSP NOTED A HOLE IN FLOORBEAM Y1292 JUST AFT OF LAVATORY D FROM FRAME 64 TO FRAME 66 AND WAS ALSO CORRODED. MX REMOVED AND REPLACED FLOORBEAM
- [SDR F3LA2009122200260](https://openairdocs.org/sdr/F3LA2009122200260), Dec 16, 2009: SHEAR PLATE. CORRODED. DURING C3 C-CHECK INSP NOTED THE RT SHEAR PLATE FROM FRAME 69 TO FRAME 70 WAS CORRODED. MX REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11, SRM 51-44-11 AND S
- [SDR F3LA2009122400270](https://openairdocs.org/sdr/F3LA2009122400270), Dec 15, 2009: PLATE. CORRODED. DURING C3 C-CHECK INSP NOTED THE ARMED PLATE FOR THE R2 DOOR WAS CORRODED. MX REMOVED AND REPLACED ARM PLATE IAW AMM 53-42-12-420-051.
- [SDR F3LA2009122300269](https://openairdocs.org/sdr/F3LA2009122300269), Dec 15, 2009: STRIP. CORRODED. DURING C3 C-CHECK INSPECTION, NOTED THE THRESHOLD STRIP FOR PANEL 262EF IS CORRODED. MX REMOVED AND REPLACED STRIP IAW AMM 53-42-12-400-002.
- [SDR F3LA2009122300268](https://openairdocs.org/sdr/F3LA2009122300268), Dec 15, 2009: PLATE. CORRODED. DURING C3 C-CHECK INSPECTION, NOTED ARMED PLATE FOR L2 DOOR IS CORRODED. MX REMOVED AND REPLACED ARMED PLATE ON L2 DOOR THRESHOLD IAW AMM 20-21-11, PB 201.
- [SDR F3LA2009122300267](https://openairdocs.org/sdr/F3LA2009122300267), Dec 15, 2009: THRESHOLD. CORRODED. DURING C3 C-CHECK INSP, NOTED THRESHOLD STRIP FOR L2 DOOR THRESHOLD IS CORRODED. MX REMOVED AND REPLACED THRESHOLD STRIP IAW AMM 53-42-12-400-001.
- [SDR F3LA2009122200263](https://openairdocs.org/sdr/F3LA2009122200263), Dec 15, 2009: FLOOR SUPPORT. CORRODED. DURING C3 C-CHECK INSP NOTED UPON REMOVAL OF THE AFT GALLEY FLOOR CORROSION WAS FOUND AT Y1292 FRAME 66 TO FRAME 69. MX REMOVED AND REPLACED FLOOR SUPPORT Y1292
- [SDR F3LA2009122200262](https://openairdocs.org/sdr/F3LA2009122200262), Dec 15, 2009: FLOOR SUPPORT. CORRODED. DURING C3 C-CHECK INSP NOTED UPON REMOVAL OF THE AFT GALLEY FLOOR CORROSION WAS FOUND AT FLOOR SUPPORT Y1292 FROM FRAME 66 TO FRAME 69. MX REPLACED FLOOR SUPPOR
- [SDR F3LA2009021900028](https://openairdocs.org/sdr/F3LA2009021900028), Feb 18, 2009: HMU. FAILED. PILOT REPORTED THAT THE NR 2 ENGINE FAILED ON DESCENT FROM FL 350, THE ENGINE RECOVERED AND FURTHER DESCENT, APPROACH AND LANDING WERE UNEVENTFUL ON TWO ENGINES
- [SDR F3LA2008111000711](https://openairdocs.org/sdr/F3LA2008111000711), Nov 9, 2008: BUSHING. OUT OF POSITION. REFERENCE LOG PAGE 420725. PILOT REPORTED THE FORWARD ENTRY DOOR L1 GUST LOCK WILL NOT ENGAGE. MAINTENANCE REINSTALLED BUSHING IN THE FORWARD ENTRY DOOR GUST LO
- [SDR F3LA200800405](https://openairdocs.org/sdr/F3LA200800405), Jun 28, 2008: FLOORBOARD. DAMAGED. DURING C-CHECK INSP NOTED AFT CARGO PIT FWD FLOORBOARD PANEL 151PE HAS A HOLE AT THE AFT LT EDGE. MAINT REMOVED DAMAGED AREA AND FILLED DAMAGED AREA IAW SRM 53-
- [SDR F3LA200800406](https://openairdocs.org/sdr/F3LA200800406), Jun 28, 2008: PANEL. DAMAGED. DURING C-CHECK INSP, NOTED AFT CARGO PIT AFT LT HAND TRANSITION PANEL 161BF HAS A HOLE AT AFT TOP END. MAINT REPAIRED AND INSTALLED SERVICEABLE PANEL 161BF IAW 
- [SDR F3LA200800407](https://openairdocs.org/sdr/F3LA200800407), Jun 28, 2008: PANEL. DAMAGED. DURING C-CHECK INSP NOTED AFT CARGO PIT FWD LT HAND LOWER TRANSITION PANEL 151AE HAS A HOLE AT FWD LOWER END. MAINT REPAIRED AND INSTALLED SERVICEABLE PANEL 151
- [SDR F3LA200800402](https://openairdocs.org/sdr/F3LA200800402), Jun 24, 2008: PANEL. DAMAGED. DURING C-CHECK INSP, NOTED AFT CARGO PIT AFT RT UPPER TRANSITION PANEL 162CF HAS SEVERAL HOLES AT AFT END. MAINT REPAIRED TRANSITION PANEL 162CF IAW SRM 53-02-0
- [SDR F3LA200800401](https://openairdocs.org/sdr/F3LA200800401), Jun 24, 2008: PANEL. DAMAGED. DURING C-CHECK INSP NOTED AFT CARGO PIT AFT LT UPPER TRANSITION PANEL 161CF HAS HOLES IN SEVERAL PLACED. MAINT REPAIRED TRANSITION PANEL 161CF IAW SRM 53-02-00 
- [SDR F3LA200800400](https://openairdocs.org/sdr/F3LA200800400), Jun 24, 2008: PANEL. DAMAGED. DURING C-CHECK INSP, NOTED AFT CARGO PIT FWD LT UPPER TRANSITION PANEL 151FE HAS A HOLE AT FWD TOP CORNER. MAINT REPAIRED TRANSITION PANEL 151FE IAW SRM 53-02-0

All 67: https://openairdocs.org/deregistered/N939FR-2022-08-22/reports.md

## FAA accident and incident reports (1)

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 20090218001729I](https://openairdocs.org/incident/20090218001729I), Feb 18, 2009: Airbus A319111 (N939FR), Omaha, NE, No damage. (-23) N939FR, A319-111, was operated as frontier flight 440, from den to oma. On descent from FL350, the crew received a nr 4 engine control fault message and…

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