# N803FR: 2003 Airbus A318-111, registration cancelled 2014-01-22

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 22, 2014
- Status when cancelled: Valid registration
- Airframe: [Airbus A318-111](https://openairdocs.org/model/airbus-a318-111) (registry code 3940019)
- 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: 2017
- Year built: 2003
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 30, 2003
- Certificate issued: September 13, 2011
- Last registry action: April 3, 2012
- Mode S code: AAED8F
- Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%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: 40.8659° N, 112.0391° W: Placed by OpenAirDocs at the center of ZIP code 84116, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N803FR
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=803FR
- Page: https://openairdocs.org/deregistered/N803FR-2014-01-22

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 A318-111: https://openairdocs.org/model/airbus-a318-111.md

## Service difficulty reports (38)

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

- [SDR F3LA2013071700885](https://openairdocs.org/sdr/F3LA2013071700885), Jul 9, 2013: UNKNOWN. VIBRATION. AIR TURN BACK DUE TO SEVERE AIRFRAME VIBRATION. BEGAN AT 25,500 FT AND AROUND 330 KIAS. DID NOT STOP UNTIL SPEED MANUALLY FLOWN LESS THAN 300 KIAS. EMERGENY DEC
- [SDR F3LA2012041000740](https://openairdocs.org/sdr/F3LA2012041000740), Apr 6, 2012: PLATE. CORRODED. LATERAL SHEAR PLATE FRAME 69 TO FRAME 70, STRINGER 23 RT TO STRINGER 24 RT HAS CORROSION. R & R SHEAR PLATE IAW SRM 51 -42-11, PARA 6 B-18, D 1-5 AND EO AO-53EO
- [SDR F3LA2012041000739](https://openairdocs.org/sdr/F3LA2012041000739), Apr 6, 2012: PLATE. CORRODED. LATERAL SHEAR PLATE FRAME 69 TO FRAME 70, STRINGER 23 LT TO STRINGER 24 LT HAS CORROSION. R & R SHEAR PLATE IAW SRM 51-42-11 PARAGRAPH 6 B-1 B, 0 1-5 AND EO AO-
- [SDR F3LA2012041000738](https://openairdocs.org/sdr/F3LA2012041000738), Apr 6, 2012: FLOORBEAM. CORRODED. AFT CABIN FLOORBEAM FRAME 66 Y765 CORROSION. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5.
- [SDR F3LA2012041000737](https://openairdocs.org/sdr/F3LA2012041000737), Apr 6, 2012: FLOOR SUPPORT. CORRODED. AFT CABIN FRAME 66 TO FRAME 68, Y1292 FLOOR SUPPORT HAS CORROSION IN 3 AREAS. R & R FLOOR SUPPORT IAW SRM 51-42-11, PARA 5.
- [SDR F3LA2012041000734](https://openairdocs.org/sdr/F3LA2012041000734), Apr 6, 2012: FLOORBEAM. CORRODED. AFT CABIN FRAME 66 TO FRAME 68, Y1292 FLOORBEAM HAS CORROSION IN 3 AREAS. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5.
- [SDR F3LA2012041000736](https://openairdocs.org/sdr/F3LA2012041000736), Apr 6, 2012: FLOORBEAM. CORRODED. AFT CABIN FRAME 68, Y-1292 FLOORBEAM HAS CORROSION. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5.
- [SDR F3LA2012041000735](https://openairdocs.org/sdr/F3LA2012041000735), Apr 6, 2012: TRAY. CRACKED. SHEAR PLATE TRAY AT FRAME 68 TO FRAME 69. STRINGER 23 RT TO STRINGER 24, RT IS CRACKED. R & R SHEAR PLATE TRAY IAW SRM 51 -42-11, PARAGRAPH 5, 6, 7 AND 13.
- [SDR F3LA201204100734](https://openairdocs.org/sdr/F3LA201204100734), Apr 6, 2012: PLATE. CRACKED. C-CHECK, SHEAR PLATE TRAY AT FRAME 68 TO FRAME 69, S23-24L CRACKED. R & R SHEAR PLATE TRAY IAW SRM 51-42-11 PARAGRAPH 5, 6, 7 AND 13.
- [SDR F3LA2011080900665](https://openairdocs.org/sdr/F3LA2011080900665), Aug 5, 2011: BATTERY PACK. FAILED. ESPU LLWL (13WL) FAILED SYS TEST IAW A-CHECK CARD A332201-03. REPLACED BATTERY PACK ON ESPU LLWL(13WL) IAW AMM 33-51-38, PB 401.
- [SDR F3LA2011051800641](https://openairdocs.org/sdr/F3LA2011051800641), May 13, 2011: BATTERY. FAILED. ACFT LP 598021 I2M: EPSU TEST FAILED 11WL BATTERY. R & R EPSU BATTERY FOR 11WL IAW A318 AMM 33-51-38-000-002 AND 33-51-38-400-002. TEST OK.
- [SDR F3LA2011032100618](https://openairdocs.org/sdr/F3LA2011032100618), Mar 17, 2011: WINDSHIELD. CRACKED. F/O FRONT WINDSHIELD CRACKED, ANTI-ICE RT WINDSHIELD ECAM. R & R THE F/O FRONT WINDSHIELD IAW AMM 56-11-11-400-000-001.
- [SDR F3LA2011022100605](https://openairdocs.org/sdr/F3LA2011022100605), Feb 16, 2011: ENGINE. OVERTEMP. AIR TURN BACK DUE TO BIRDSTRIKE ON NR 1 ENGINE. ENGINE SHUTDOWN, INVESTIGATION FOR ENGINE SHUTDOWN SHOWS THE EGT WAS EXCEEDED AT 1015 DEGREES CELCIUS FOR 21 SEC
- [SDR F3LA2010100600529](https://openairdocs.org/sdr/F3LA2010100600529), Oct 17, 2010: LENS. CRACKED. C-CHECK: NON ROUTINE N0616; L-1 ENTRY LOWER EXIT LIGHT, THE LENS IS ILLEGIBLE. R & R LENS ASSY ON L-1 DOOR LOWER EXIT LIGHT IAW AMM 33-51-13-400-001 PAGE 3 STEP
- [SDR F3LA2010100600528](https://openairdocs.org/sdr/F3LA2010100600528), Oct 17, 2010: FLOOR PANEL. DELAMINATED. C-CHECK: NON ROUTINE N0613; AFT CARGO FLOOR PANEL 161DF EDGE DELAMINATED AND EDGE FILLER DAMAGED 10 INCH. FABRICATED REPLACEDMENT FLOOR PANEL IAW MCG IRM 9701, 
- [SDR F3LA2010100600527](https://openairdocs.org/sdr/F3LA2010100600527), Oct 17, 2010: LENS. CRACKED. C-CHECK: NON ROUTINE N0610; EMERGENCY LIGHT ABOVE L-1 DOOR, THE LENS IS CRACKED. R & R EMERGENCY LIGHT ASSY IAW AMM 33-51-11-020-050B AND AMM 33-51-11-420-050A.
- [SDR F3LA2010100600526](https://openairdocs.org/sdr/F3LA2010100600526), Oct 17, 2010: POWER SUPPLY. NO TEST. C-CHECK: NON ROUTINE N0607; NUMEROUS EMERGENCY PATH LIGHTS INOP ON SEATS AND CEILING PANELS. PERFORMED OPS TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00-710-059A. E
- [SDR F3LA2010100600525](https://openairdocs.org/sdr/F3LA2010100600525), Oct 17, 2010: FITTING. GOUGED. C-CHECK: NON ROUTINE N0124; FWD CARGO LOWER FWD CORNER SEALING SECTION FITTING GOUGED .1250 IN X .2500 IN X .040 INCH. R & R FWD LOWER SEALING SECTION FITTING I
- [SDR F3LA2010100600524](https://openairdocs.org/sdr/F3LA2010100600524), Oct 17, 2010: CONNECTOR. MISINSTALLED. C-CHECK: NON ROUTINE N0033, EMERGENCY EXIT LIGHT AT ROW 13ABC INOP. FOUND CONNECTOR AT LIGHT ASSEMBLY TO BE INPROPERLY CONNECTED. RE-SEATED CONNECTOR IAW AIRBUS
- [SDR F3LA200700193](https://openairdocs.org/sdr/F3LA200700193), Aug 3, 2007: FLOOR PANEL. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR THRESHOLD CORRODED ON SURFACE OF PANEL 261FF. REPLACED FLOOR PANEL 261FF IAW AMM 53-42-12-400-002.
- [SDR F3LA200700190](https://openairdocs.org/sdr/F3LA200700190), Aug 3, 2007: FLOOR SUPPORT. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT AT FR 66 TO FR 70 AT Y1292, FWD INBD FASTENER LOCATIONS. REPLACED FLOOR SUPPORT BETWEEN FR 66 A
- [SDR F3LA200700192](https://openairdocs.org/sdr/F3LA200700192), Aug 1, 2007: PLATE. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR FWD AND AFT GIRT BAR FITTING BLANKING PLATES CORRODED. REPLACED L2 DOOR FWD AND AFT GIRT BAR FITTING BLANKING PLAT
- [SDR F3LA200700191](https://openairdocs.org/sdr/F3LA200700191), Jul 31, 2007: GIRT BAR. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON L2 DOOR SEAL NUT PLATE HOLE AFT OF AFT GIRT BAR FITTING PLATE. REPAIRED PER EA A8-53R-12044.
- [SDR F3LA200700188](https://openairdocs.org/sdr/F3LA200700188), Jul 30, 2007: PLATE. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR FWD AND AFT GIRT BAR FITTING BLANKING PLATES CORRODED. REPLACED BLANKING PLATES IAW A318 SRM 51-42-11 AND AMM 52-1
- [SDR F3LA200700187](https://openairdocs.org/sdr/F3LA200700187), Jul 28, 2007: FLOOR PANEL. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED L1 DOOR THRESHOLD FLOOR PANEL 221FF CORRODED. REPLACED FLOOR PANEL 221FF IAW AIRBUS AMM 53-12-12-400-001.
- [SDR F3LA200700185](https://openairdocs.org/sdr/F3LA200700185), Jul 24, 2007: TORQUE LINK. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED PITTING AND CORROSION ON NLG UPPER TORQUE LINK ATTACH POINT. REMOVED PITS AND CORROSION AND CADMIUM PLATED INNER BORE IAW 
- [SDR F3LA200700184](https://openairdocs.org/sdr/F3LA200700184), Jul 24, 2007: PLATE. DAMAGED. DURING C-3 CHECK, INSPECTION REPORTED HOLES ON JOINT PLATE COMMON TO FLOORBEAM AT -Y1292 BETWEEN FR68 AND FR69 DAMAGED. FABRICATED AND INSTALLED REPLACEMENT JOI
- [SDR F3LA200700183](https://openairdocs.org/sdr/F3LA200700183), Jul 24, 2007: SKATE ANGLE. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED MODERATE CORROSION IN NUT PLATE MOUNT HOLES OF SKATE ANGLE AFT OF R2 DOOR GIRT BAR CUTOUTS. REMOVED AND REPLACED SKATE ANG
- [SDR F3LA200700182](https://openairdocs.org/sdr/F3LA200700182), Jul 24, 2007: SKATE ANGLE. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED MODERATE CORROSION IN NUT PLATE MOUNT HOLES OF SKATE ANGLE AFT OF L2 DOOR GIRT BAR CUT OUTS. REMOVED AND REPLACED SKATE AN
- [SDR F3LA200700181](https://openairdocs.org/sdr/F3LA200700181), Jul 24, 2007: FLOORBEAM. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED AFT GALLEY RT FLOORBEAM -Y1292, FR 68 TO FR69 CORRODED AT NUT PLATE FASTENER LOCATIONS.
- [SDR F3LA200700180](https://openairdocs.org/sdr/F3LA200700180), Jul 24, 2007: FLOORBEAM. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM INBD OF R2 DOOR GIRT BAR CUTOUTS HAD LIGHT TO MODERATE CORROSION AT ALL NUT PLATE ATTACH POINTS. REPLACED FLOORB
- [SDR F3LA200700179](https://openairdocs.org/sdr/F3LA200700179), Jul 24, 2007: FLOORBEAM. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM INBD OF L2 DOOR GIRT BAR CUTOUTS HAD LIGHT TO MODERATE CORROSION AT ALL NUT PLATE ATTACH POINTS. REPLACED FLOORB
- [SDR UPS07449033](https://openairdocs.org/sdr/UPS07449033), Jul 24, 2007: FLOORBEAM. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED AFT GALLEY RT FLOORBEAM -Y1292, FR 68 TO FR69 CORRODED AT NUT PLATE FASTENER LOCATIONS.
- [SDR F3LA200700084](https://openairdocs.org/sdr/F3LA200700084), Apr 27, 2007: CONTACTOR. DAMAGED. AIR RETURN AT 0130Z FOR MULTIPLE ECAMS ASSOCIATED W/AC ESS BUSS. DEPARTURE OUT OF KDEN, LEVELING AT 35,000 FT, RECEIVED ECAM ENG 1 IGN A AND ENG 2 IGN A, C/B TR
- [SDR F3LA200600063](https://openairdocs.org/sdr/F3LA200600063), Jun 30, 2006: LINE. LEAKING. DURING CRUISE, FLIGHT CREW REPORTED -Y- HYDRAULIC SYSTEM LEVEL LOW. AS A PRECAUTIONARY MEASURE, AN EMERGENCY WAS DECLARED UPON LANDING AT PDX. REPLACED NR 2 ENG
- [SDR F3LA200500032](https://openairdocs.org/sdr/F3LA200500032), Jul 15, 2005: CONTROLLER. UNSERVICEABLE. FLT CREW REPORTED CABIN PRESSURIZATION FLUCTUATING FOLLOWED BY NR 2 CONTROLLER FAILURE. ECAM EXCESS CABIN ALT. AT APPROX 30,000 FT & CLIMBING. NOTICED CABIN ALT
- [SDR F3LA200400065](https://openairdocs.org/sdr/F3LA200400065), Jun 6, 2004: CONTROL UNIT. ODOR. IN CRUISE CREW REPORTED SMOKE COMING FROM FLIGHT CONTROL UNIT. NO ECAMS NOTED, SMOKE/AVNCS SMOKE. QRH PROCEDURE APPLIED, EMERGENCY DECLARED. DIVERTED TO OKC & L
- [SDR F3LA200300136](https://openairdocs.org/sdr/F3LA200300136), Sep 15, 2003: POWER SUPPLY. INOPERATIVE. FLIGHT CREW REPORTED SEAT BELT/NO SMOKING LIGHTS AND FWD GALLEY EXIT SIGNS INOPERATIVE. REPLACED EPSU IAW MM 33-51-13-04.

## 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 20110214002309I](https://openairdocs.org/incident/20110214002309I), Feb 14, 2011: Airbus A318-111 (N803FR), Denver, CO, No damage. Frontier airlines flight 226 a Airbus 318-111, aircraft N803FR departed rwy 34L. On climb out reported a bird strike to number one engine . Engine loss power…

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