# N203FR: 2002 Airbus Industrie A320-214, registration cancelled 2018-12-17

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 17, 2018
- Status when cancelled: Valid registration
- Airframe: [Airbus Industrie A320-214](https://openairdocs.org/model/airbus-industrie-a320-214) (registry code 3930316)
- Engine: [CFM International CFM56-5B4/P series](https://openairdocs.org/engine/cfm-international-cfm56-5b4-p-series) (registry code 13011)
- Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM) (OpenAirDocs)
- Serial number: 1806
- Year built: 2002
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 24, 2009
- Certificate issued: July 29, 2016
- Last registry action: May 7, 2018
- Mode S code: A19DB5
- Owner when cancelled: [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N203FR
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=203FR
- Page: https://openairdocs.org/deregistered/N203FR-2018-12-17

From the FAA registry file of October 31, 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 Industrie A320-214: https://openairdocs.org/model/airbus-industrie-a320-214.md

## Service difficulty reports (48)

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

- [SDR F3LA2018050100336](https://openairdocs.org/sdr/F3LA2018050100336), Apr 23, 2018: DOUBLER. GOUGED. AFT CARGO DOOR LOWER AFT INNER SKIN DOUBLER REPAIR GOUGED. REMOVED AND REPLACED THE AFT CARGO DOOR LOWER INNER SKIN DOUBLER REPAIR IAW AMM 52-32-00-300-016, EA 
- [SDR F3LA2018050100335](https://openairdocs.org/sdr/F3LA2018050100335), Apr 23, 2018: DOUBLER. GOUGED. FWD CARGO DOOR LOWER AFT INNER SKIN DOUBLER REPAIR GOUGED. REMOVED AND REPLACED THE FWD CARGO DOOR LOWER AFT INNER SKIN DOUBLER IAW SRM 52-41-11, 52-31-13, PB 4
- [SDR F3LA2018050100334](https://openairdocs.org/sdr/F3LA2018050100334), Apr 23, 2018: DOUBLER. GOUGED. FWD CARGO DOOR LOWER FWD INNER SKIN DOUBLER REPAIR GOUGED. REMOVED AND REPLACED THE DOUBLER AT FWD DOOR INNER SKIN IAW SRM 51-42-11, NTM 51-10-08, AMM 52-31-21-
- [SDR F3LA2017070500184](https://openairdocs.org/sdr/F3LA2017070500184), Jul 2, 2017: WINDSHIELD. FAILED. FOUND THE CAPTAIN'S WINDSHIELD SHATTERED. REPLACED THE WINDSHIELD IAW AMM 56-11-11 PB 401. OPS CHECKED GOOD.
- [SDR F3LA2017051600138](https://openairdocs.org/sdr/F3LA2017051600138), May 10, 2017: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT Y1292 FROM FRAMES 64 - 66 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001.
- [SDR F3LA2017051600139](https://openairdocs.org/sdr/F3LA2017051600139), May 9, 2017: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT -Y254 BETWEEN FRAMES 68 - 70 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, AND 51-72-11-911-001.
- [SDR F3LA2017051700141](https://openairdocs.org/sdr/F3LA2017051700141), May 8, 2017: FLOORBEAM. CORRODED. FLOORBEAM -Y1292 AT FR 66 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED, NEW FLOORBEAM -Y1292 AT FR66 IAW SRM A320-51-42-11 AND 51-72-911-01.
- [SDR F3LA2017051700140](https://openairdocs.org/sdr/F3LA2017051700140), May 8, 2017: FLOORBEAM. CORRODED. FLOORBEAM Y765 AT FR66 HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION ON FLOORBEAM Y765 AT FR66 FOUND TO BE OUT OF LIMITS. REMOVED FLOORBEAM Y765 AT FR66 REP
- [SDR F3LA2017051600132](https://openairdocs.org/sdr/F3LA2017051600132), May 8, 2017: FLOORBEAM. CORRODED. FLOORBEAM Y1292 AT FR68 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, AND 51-72-11-911-001.
- [SDR F3LA2017051500137](https://openairdocs.org/sdr/F3LA2017051500137), May 8, 2017: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT Y765 BETWEEN FRAMES 67 AND 68 HAS CORROSION ON UPPER SERVICE. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001.
- [SDR F3LA2017051500136](https://openairdocs.org/sdr/F3LA2017051500136), May 8, 2017: FLOORBEAM. CORRODED. FLOORBEAM Y254 BETWEEN FR66-FR67 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED NEW FLOORBEAM Y254 BETWEEN FR66-FR67 IAW SRM 51-72-11, 51-42-11 AND 53-41-
- [SDR F3LA2017051500135](https://openairdocs.org/sdr/F3LA2017051500135), May 8, 2017: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT -Y765, FRAMES 67 - 68 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, AND 51-72-11-911-001.
- [SDR F3LA2017051500134](https://openairdocs.org/sdr/F3LA2017051500134), May 8, 2017: FLOORBEAM. CORRODED. FLOORBEAM -Y765 AT FRAME 66 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOORBEAM IAW 51-42-11, AND 51-72-11-911-001.
- [SDR F3LA2017051500133](https://openairdocs.org/sdr/F3LA2017051500133), May 8, 2017: FLOORBEAM. CORRODED. FLOORBEAM Y1292 AT FRAME 67 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11-911-001.
- [SDR F3LA2017051500131](https://openairdocs.org/sdr/F3LA2017051500131), May 8, 2017: FLOORBEAM. CORRODED. FLOORBEAM -Y1292 AT FRAME 67 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, AND 51-72-11-911-001.
- [SDR F3LA2017051500130](https://openairdocs.org/sdr/F3LA2017051500130), May 8, 2017: FLOORBEAM. CORRODED. FLOORBEAM -Y1292 AT FRAME 68 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, AND 51-72-11-911-001.
- [SDR F3LA2016081700001](https://openairdocs.org/sdr/F3LA2016081700001), May 19, 2016: COFFEEMAKER. ODOR. F/A SMELLED ODOR COMING FROM AFT CABIN DESCRIBED AS POSSIBLY POPCORN, BURNING RUBBER, OF BURNED COFFEE. POSSIBLY COMING FROM HIGHER IN THE CABIN PERFORMED TROUB
- [SDR F3LA2016052000048](https://openairdocs.org/sdr/F3LA2016052000048), May 19, 2016: COFFEEMAKER. DIRTY. REFERENCE LOG PAGE 989574, DURING CRUISE THE CREW NOTED AN ODOR COMING FROM THE AFT CABIN & THE ACFT DIVERTED. MX IDENTIFIED THE CAUSE OF THE ODOR TO BE THE AFT
- [SDR F3LA2015112001153](https://openairdocs.org/sdr/F3LA2015112001153), Nov 15, 2015: SAFETY VALVE. INOPERATIVE. DISCREPANCY ITEM 1, SPOILERS 1 & 2 FAULT INFLIGHT. DISCREPANCY ITEM NR 2 NOSE WHEEL STEERING FAULT INFLIGHT. RESET SEC 1 & 2. OPERATIONS CHECKED OK IAW AMM 27-9
- [SDR F3LA2015111201152](https://openairdocs.org/sdr/F3LA2015111201152), Nov 8, 2015: LINE. CHAFED. HYD RESERVOIR LOW LEVLE, DURING CRUISE FLIGHT. DECLARED AN EMERGENCY. MX FOUND A HOLE IN THE RETURN LINE FOR THE NR 2 ENG THRUST REVERSER HYDRAULIC LINE. THE LI
- [SDR F3LA2015101401150](https://openairdocs.org/sdr/F3LA2015101401150), Oct 10, 2015: SLIDE. DEFECTIVE. EMERGENCY SLIDE LIGHT AT DOOR 1 RT INOPERATIVE. PLACED ON MEL CONTROL NR 1116039. REPLACED L1 DOOR SLIDE AMM 25-62-44-000-002-A & 25-62-44-400-006-A. OPERATIONA
- [SDR F3LA2015030901117](https://openairdocs.org/sdr/F3LA2015030901117), Mar 7, 2015: WIRE. DAMAGED. DISCREPANCY, EMER EXIT LIGHTS INOPERATIVE AT L1, L2, R1 & R2. RETERMINATED WIRING AT ALL 4 EPSUS AS REQUIRED, COMPLIED WITH EA A2-33R-33040. EMER LIGHTS OPERATI
- [SDR F3LA2013111800934](https://openairdocs.org/sdr/F3LA2013111800934), Oct 30, 2013: SEAT TRACK. CORRODED. DURING C8/S2 CHECK. SEAT TRACK Y1292 HAS CORROSION AT FRAME 16. SEAT TRACK CORROSION EVALUATED AND FOUND OUT OF LIMITS. REMOVED DAMAGED TRACK AND INSTALLED NEW 
- [SDR F3LA2013111800933](https://openairdocs.org/sdr/F3LA2013111800933), Oct 23, 2013: SKIN. DAMAGED. DURING C8/S2 CHECK. THERMOGRAPHIC INSPECTION OF LT ELEVATOR REVEALED INDICATIONS ON UPPER PANEL IRREGULAR IN SHAPE AND BLACK IN COLOR. REPAIRED IAW SRM 55-20-00
- [SDR F3LA2013111800932](https://openairdocs.org/sdr/F3LA2013111800932), Oct 22, 2013: SILL. CORRODED. DURING C8/S2 CHECK. FORWARD CARGO LOWER SILL UPPER SURFACE HAS CORROSION BETWEEN FRAMES 26 AND 27. REPAIRED IAW SRM 51-74-00 PARA 6.A - 6.B(2}(5), SRM 51-75-12,
- [SDR F3LA2013111800931](https://openairdocs.org/sdr/F3LA2013111800931), Oct 22, 2013: SILL. CORRODED. DURING C8/S2 CHECK. FORWARD CARGO DOOR SILL LOWER SKIN HAS SURFACE CORROSION ON UPPER SURFACE AT FRAMES 24 TO 25. REPAIRED IAW SRM 5L-74-00 PARA 6.A-6.B.
- [SDR F3LA2013111800930](https://openairdocs.org/sdr/F3LA2013111800930), Oct 20, 2013: SHEAR TIE. CORRODED. DURING C8/S2 CHECK, LT LATERAL SHEAR PLATE HAS CORROSION AT FRAME 70, STRINGER 24. REMOVED AND REPLACED IAW SRM 51-42-11, PARAGRAPH 6.B., 1 THROUGH 8.
- [SDR F3LA2013111800929](https://openairdocs.org/sdr/F3LA2013111800929), Oct 20, 2013: SHEAR TIE. CORRODED. DURING C8/S2 CHECK. RT LATERAL SHEAR PLATE HAS CORROSION AT FRAME 70, STRINGER 24. R & R IAW SRM 51-42-11, PARA 6.B., 1 THROUGH 8.
- [SDR F3LA2012050400750](https://openairdocs.org/sdr/F3LA2012050400750), May 1, 2012: LAMP. BURNED OUT. SEAT ROW 25 EMERGENCY LIGHT INOPERATIVE. R & R BULBS IAW AMM 33-51-18-400-002A. OPS CHECKED OK.
- [SDR F3LA2012050400749](https://openairdocs.org/sdr/F3LA2012050400749), May 1, 2012: LAMP. BURNED OUT. SEAT ROW 24 EMERGENCY LIGHT INOPERATIVE. R & R BULBS, IAW AMM 33-41-11-400-002A, 33--41-11-000-002A. OPS CHECKED OK.
- [SDR F3LA2012011300699](https://openairdocs.org/sdr/F3LA2012011300699), Jan 12, 2012: ELECTRICAL BOX. FAILED. ODOR OF ELETRICITY BETWEEN ROW 3 AND 4. NO VISIBLE SMOKE. TURNED OFF LIVE TV AND ODOR CLEARED. PERFORMED ELETRICAL ODOR SYS INTEGRITY CHECK IAW LTV AMM 44-25-00
- [SDR F3LA2011080400663](https://openairdocs.org/sdr/F3LA2011080400663), Jul 29, 2011: FEEL UNIT. BINDING. REFERENCE PILOT REPORT LOG PAGE 615630 ITEM 1, UPON TOUCHDOWN PILOT NEEDED RIGHT RUDDER TO STRAIGHTEN NOSE BUT RUDDER FELT LOCKED IN CENTERED POSITION. AFTER AP
- [SDR F3LA2010111400548](https://openairdocs.org/sdr/F3LA2010111400548), Nov 14, 2010: MODULE. LOOSE. C-CHECK: NON ROUTINE N0694; EMERGENCY EXIT LIGHTS ON SEAT ROWS 16 AND 24 ARE INOP. RETERMINATED PINS ON EMERGENCY EXIT LIGHT CONNECTORS AT SEATS 16 LT AND 24 LT
- [SDR F3LA2010111400547](https://openairdocs.org/sdr/F3LA2010111400547), Nov 14, 2010: FLOORBEAM. CORRODED. C-CHECK: NON ROUTINE N0566; MAIN CABIN FLOORBEAM RT SIDE NR4 BETWEEN FRAME 67-69, CORROSION ON BOTTOM SIDE OF FLOORBEAM AT FASTENER HOLE. R & R FLOORBEAM IAW SR
- [SDR F3LA2010111400546](https://openairdocs.org/sdr/F3LA2010111400546), Nov 14, 2010: PLATE. CORRODED. C-CHECK: NON ROUTINE N0561; AFT GALLEY UNDERFLOOR STRUCTURE RT LATERAL SHEAR PLATE BETWEEN FRAME 69 AND 70, HAS CORROSION AT 8 IN AFT OF FRAME 69 (ABOUT 2 SQUAR
- [SDR F3LA2010111400545](https://openairdocs.org/sdr/F3LA2010111400545), Nov 14, 2010: SILL. CORRODED. C-CHECK: NON ROUTINE N0558; MAIN CABIN FLOOR AT FRAME 68L FLOOR SUPPORT HAS CORROSION APPROX 25 SQ IN AT THE FASTENER HOLES. CORROSION ON FLOOR SILL. REMOVED CO
- [SDR F3LA2010111400544](https://openairdocs.org/sdr/F3LA2010111400544), Nov 14, 2010: FLOORBEAM. CORRODED. C-CHECK: NON ROUTINE N0557; MAIN CABIN FLOORBEAM, NR 4 LT BETWEEN FRAME 67-68 HAS APPROX 2 SQ IN OF CORROSION AT THE FASTENER HOLES. R & R FLOORBEAM IAW SRM 51-
- [SDR F3LA2010111400543](https://openairdocs.org/sdr/F3LA2010111400543), Nov 14, 2010: FLOOR PANEL. DELAMINATED. C-CHECK: NON ROUTINE N0401; FLOORBOARD UNDER LAV E IS DELAMINATED. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REV G.
- [SDR F3LA2010111400542](https://openairdocs.org/sdr/F3LA2010111400542), Nov 14, 2010: TRANSITION PANEL. DEBONDED. C-CHECK: NON ROUTINE N0291; FWD CARGO TRANSITION PANEL 132FF UPPER SURFACE DEBONDED 6 SQ IN. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701, REV G.
- [SDR F3LA2010111400541](https://openairdocs.org/sdr/F3LA2010111400541), Nov 14, 2010: TRANSITION PANEL. DELAMINATED. C-CHECK: NON ROUTINE N0289; FWD CARGO TRANSITION PANEL 132GF UPPER SURFACE IS DELAMINATED IN 2 PLACES, 2 SQUARE IN, 4 SQUARE IN. FABRICATED REPLACEMENT PANEL IA
- [SDR F3LA2010111400540](https://openairdocs.org/sdr/F3LA2010111400540), Nov 14, 2010: FLOOR PANEL. CORRODED. C-CHECK: FWD CARGO PIT TRANSITION FLOOR PANEL 131BF UPPER SURFACE AFT END DISBOUNDED 8 SQUARE INCHES. FABRICATED TRANSITION PANEL IAW MCW IRM 9701 REV G.
- [SDR F3LA2010111400539](https://openairdocs.org/sdr/F3LA2010111400539), Nov 14, 2010: FLOOR PANEL. PUNCTURED. C-CHECK: NON ROUTINE N0286; FWD CARGO TRANSITION FLOOR PANEL 131BF HAS A 1 SQUARE IN PUNCTURE. FABRICATED REPLACEMENT PANEL IAW MCG 9701, REV G.
- [SDR F3LA2010111400538](https://openairdocs.org/sdr/F3LA2010111400538), Nov 14, 2010: COVER. GOUGED. C-CHECK: NON ROUTINE N0138; FWD CARGO DOOR INTERNAL SIDE HAS 2.5 INCHES ABOVE THE LOWER DOOR SEAL AND 26.5 INCHES FWD AFT DOOR SEAL IS GOUGED, THAT MEASURES 1/8
- [SDR F3LA2010111400537](https://openairdocs.org/sdr/F3LA2010111400537), Nov 14, 2010: SEAL. GOUGED. C-CHECK: NON ROUTINE N0134; AFT CARGO DOOR INTERNAL SIDE HAS 2 IN ABOVE THE LOWER SEAL AND 25 INCHES OF FWD SEAL IS GOUGED THAT MEASURES .3750 IN WIDE X .7500 I
- [SDR F3LA2010111400536](https://openairdocs.org/sdr/F3LA2010111400536), Nov 14, 2010: PANEL. GOUGED. C-CHECK: NON ROUTINE N0132; AFT CARGO DOOR INTERNAL SIDE HAS A 2.5 INCHES ABOVE THE LOWER DOOR SEAL AND 27 INCHES FWD OF AFT SEAL IS A GOUGE THAT MEASURES .7500
- [SDR F3LA2010071400466](https://openairdocs.org/sdr/F3LA2010071400466), Jul 13, 2010: BLEED VALVE. FAULTED. AIR TURNBACK DUE TO ENGINE NUMBER 1 CONTROL VALVE FAULT. REMOVED AND REPLACED TRANSIENT BLEED VALVE REFERENCE AMM 75-26-10-000-001 AND AMM 75-26-10-400-001. OPE
- [SDR F3LA2009120400241](https://openairdocs.org/sdr/F3LA2009120400241), Dec 4, 2009: RELAY. INOPERATIVE. REF LOG PAGE 492624. FLIGHT CREW MAD A BLOCK TURN BACK DUE TO THE F/A CIDS PANEL EMERGENCY LIGHTS ON AND COULD NOT BE RESTORED AND TURNED OFF. MX REMOVED AND RE
- [SDR F3LA2009042700081](https://openairdocs.org/sdr/F3LA2009042700081), Apr 24, 2009: OXYGEN MASK. NO TEST. DURING AIRCRAFT INDUCTION CHECK, THE FORWARD LAVATORY OXYGEN MASK WOULD NOT DROP DURING THE MANUAL MASK DROP TEST. MAINTENANCE REPACKED THE OXYGEN MASK AND PERF

## 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 20091006022169I](https://openairdocs.org/incident/20091006022169I), Oct 6, 2009: Airbus A320214 (N203FR), Denver, CO, Minor damage. Frontier flight 787 was scheduled for service between den and las on 6 October 2009. Pilot aborted takeoff on runway 25 due to faulty airspeed indications and…

---
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.