# N801FR: 2003 Airbus A318-111, registration cancelled 2013-01-07

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 7, 2013
- 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: 1939
- Year built: 2003
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 7, 2003
- Certificate issued: September 13, 2011
- Last registry action: March 29, 2012
- Mode S code: AAE621
- 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/N801FR
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=801FR
- Page: https://openairdocs.org/deregistered/N801FR-2013-01-07

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 (44)

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

- [SDR F3LA2012053000764](https://openairdocs.org/sdr/F3LA2012053000764), May 29, 2012: GIRT BAR. OUT OF ADJUST. L2 DOOR SLIDE DOES NOT SHOW ARMED IN FLIGHT SHOWS ARMED ON GROUND. FOUND L2 DOOR GIRT BAR FITTINGS OUT OF ADJUSTMENT. ADJUSTED GIRT BAR FITTINGS IAW AMM 52-13-2
- [SDR F3LA2012053000762](https://openairdocs.org/sdr/F3LA2012053000762), May 25, 2012: ACTUATOR. FAILED. STRONG ELECTRICAL/OIL ODOR FUMES IN COCKPIT AND CABIN ON CLIMB. RETURNED TO DEPARTURE. NR 1 PACK OVERHEAT FAULT. SHUTDOWN PACK, BLOWING VERY HOT AIR. REMOVE AND
- [SDR F3LA2012003080720](https://openairdocs.org/sdr/F3LA2012003080720), Mar 5, 2012: SHEAR PLATE. CRACKED. C-CHECK: FUSELAGE LT SIDE AT FRAME 68, STRINGER 23, LEFT LATERAL SHEAR PLATE CRACKED. R & R PLATE IAW SRM 51-42-11, PAR 6.B.
- [SDR F3LA2012003070719](https://openairdocs.org/sdr/F3LA2012003070719), Mar 5, 2012: FLOORBEAM. CORRODED. C-CHECK: MAIN CABIN FRAME 68 FLOOR PANEL FASTENER HOLES BETWEEN V1292, FLOORBEAM HAS CORROSION. BLENDED OUT CORROSION IAW SRM 51-73-00 PARAGRAPH 5. FOUND TO BE 
- [SDR F3LA2012003060717](https://openairdocs.org/sdr/F3LA2012003060717), Mar 5, 2012: FLOORBEAM. CORRODED. C-CHECK: MAIN CABIN FLOORBEAM HAS CORROSION AROUND FASTENER HOLES FRAME 66 TO FRAME 68, -Y765. R & R FLOORBEAM IAW SRM 51-42-11, PARAGRAPH 5.
- [SDR F3LA2012003060716](https://openairdocs.org/sdr/F3LA2012003060716), Mar 5, 2012: FRAME SPLICE. CORRODED. C-CHECK: AFT GALLEY AREA FRAME 70, -Y1292 SPLICE PLATE (SHEAR PLATE) HAS CORROSION. R & R AFT GALLEY SHEAR PLATE IAW SRM 51-42-11, PARAGRAPH 17-18 AND EO AO-53E
- [SDR F3LA2012022800712](https://openairdocs.org/sdr/F3LA2012022800712), Feb 23, 2012: BATTERY. FAILED. BATTIERY 10 WL FAILED CAPACITY TEST IAW CARD A332204-02. REPLACED EPSU BATTERY 10 WL IAW AMM33-51-38-400-002-A.
- [SDR F3LA2012020700705](https://openairdocs.org/sdr/F3LA2012020700705), Feb 2, 2012: ENGINE. MAKING METAL. ABORTED TAKEOFF. UNUSUAL VIBRATION NOTED ON START OF NR 2 ENGINE DURING TAXI. NO ECAMS NOTED. ON APPLICATION OF TAKE OFF THRUST, A LOUD COMPRESSOR STALL, FLAMES
- [SDR F3LA2010111400550](https://openairdocs.org/sdr/F3LA2010111400550), Nov 12, 2010: BATTERY PACK. DISCHARGED. BATTERY PACK 12W FAILED CAPACITY CHECK IAW TASK CARD A332204-02. REPLACED ESPU 12WL IAW AMM 33-51-38, PB 401.
- [SDR F3LA2010072500474](https://openairdocs.org/sdr/F3LA2010072500474), Jul 21, 2010: ENCODER. FAULTY. REFERENCE HEAVY MAINTENANCE NON ROUTINE N0526. EMERGENCY LIGHT OPERATIONAL TEST FAILED WITH A CLASS 1 MESSAGE EPSU (11WL) AND (12WL). FOUND HIGH AND LOW CODING 
- [SDR F3LA2010072500473](https://openairdocs.org/sdr/F3LA2010072500473), Jul 20, 2010: LIGHT. INOPERATIVE. REFERENCE HEAVY MAINTENANCE NON ROUTINE N0499. DURING TEST FORWARD EMERGENCY LIGHT 61WL WOULD NOT ILLUMINATE. TROUBLESHOT SYSTEM IAW A318 TSM 25-62-00-810-813. 
- [SDR F3LA2010072500472](https://openairdocs.org/sdr/F3LA2010072500472), Jul 12, 2010: FLAP. DAMAGED. REFERENCE HEAVY MAINTENANCE NON ROUTINE N0001. TEMPORARY REPAIR TO LIGHTNING STRIKE DAMAGE ON RIGHT WING OUTBOARD FLAP TRAILING EDGE 4.25 INCHES FROM OUTBOARD E
- [SDR F3LA2009042100078](https://openairdocs.org/sdr/F3LA2009042100078), Apr 20, 2009: COMPUTER. INOPERATIVE. PILOT REPORTED AFTER TAKEOFF THE AIRCRAFT DID NOT AUTO TRIM, CONSTANT FORWARD PRESSURE WAS REQUIRED TO MAINTAIN DESIRED PITCH. SAME RESULT ON BOTH STICKS. AIRCR
- [SDR F3LA2008111900718](https://openairdocs.org/sdr/F3LA2008111900718), Nov 18, 2008: FITTING. OUT OF ADJUST. DURING C4 C-CHECK, INSPECTION NOTED THE R2 DOOR ARMED HANDLE WAS SPONGY WHEN IN THE ARMED POSITION. MAINTENANCE ADJUSTED THE R2 GIRT BAR FITTING AND PERFORMED O
- [SDR F3LA2008111800717](https://openairdocs.org/sdr/F3LA2008111800717), Nov 18, 2008: BATTERY. FAILED. DURING C4 C-CHECK, INSPECTION NOTED THAT THE EMERGENCY LIGHT TEST THROUGH THE CENTRALIZED FAULT DISPLAY UNIT FAILED OPERATIONAL CHECK. MAINTENANCE REMOVED AND R
- [SDR F3LA2008111800716](https://openairdocs.org/sdr/F3LA2008111800716), Nov 17, 2008: HOOK. WORN. DURING C4 C-CHECK, INSPECTION NOTED THAT DURING INSTALLATION OF THE ESCAPE SLIDE THE L2 DOOR HANDLE WAS ABLE TO MOVE INTO THE CLOSED POSITION BEFORE THE DOOR WA
- [SDR F3LA2008111700713](https://openairdocs.org/sdr/F3LA2008111700713), Nov 15, 2008: HINGE FITTING. GOUGED. DURING C4 C-CHECK, INSPECTION NOTED THE RIGHT NR 4 SPOILER ANTI-ROTATION WEB FLAT WAS GOUGED. MAINTENANCE REPAIRED THE DAMAGE IN ACCORDANCE WITH ENGINEERING AUT
- [SDR F3LA2008111700712](https://openairdocs.org/sdr/F3LA2008111700712), Nov 15, 2008: HINGE FITTING. GOUGED. DURING C4 C-CHECK, INSPECTION NOTED THE RIGHT NR 3 SPOILER ANTI-ROTATION WEB FLAT WAS GOUGED. MAINTENANCE REPAIRED THE DAMAGE IN ACCORDANCE WITH ENGINEERING AUT
- [SDR F3LA200700379](https://openairdocs.org/sdr/F3LA200700379), Dec 24, 2007: BATTERY PACK. INOPERATIVE. FLIGHT CREW REPORTED EPSU "13WL" AFT LEFT MESSAGE. REPLACED EPSU BATTERY AT 13WL LOCATION IAW AMM 33-51-38-400-002. OPS CHECK GOOD. 
- [SDR F3LA200700108](https://openairdocs.org/sdr/F3LA200700108), May 4, 2007: OXYGEN MASK. NO TEST. WHILE PERFORMING MASK DROP TEST, ROWS 15 AND AFT ON BOTH SIDES, 7, 8, AND 9 RT SIDE, R2 DOOR AND C LAV DID NOT DROP COMPLETELY. RESET MASKS AND PERFORMED TEST A
- [SDR F3LA200700101](https://openairdocs.org/sdr/F3LA200700101), Apr 27, 2007: SHEAR PLATE. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED LT SIDE OF CABIN FLOOR WEB 69 AND 70 HAD VERY LIGHT CORROSION AT NUT PLATES, MOSTLY ON LWR SIDE. REPLACED SHEAR PLATE IAW 
- [SDR F3LA200700091](https://openairdocs.org/sdr/F3LA200700091), Apr 27, 2007: WEB. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED RT SIDE CABIN FLOOR WEB 69 AND 70 HAD VERY LIGHT CORROSION AT NUT PLATES, MOSTLY ON LWR SIDE. REPLACED SHEAR PLATE IAW SRM
- [SDR F3LA200700107](https://openairdocs.org/sdr/F3LA200700107), Apr 25, 2007: FLOORBEAM. DAMAGED. DURING C-3 CHECK, INSPECTION REPORTED FWD SPLICE OF R2 DOOR SILL HAD TWO DOUBLE DRILLED HOLES, ONE COMPLETELY THROUGH THE FWD FLOORBEAM. REPLACED DAMAGED FLOORB
- [SDR F3LA200700106](https://openairdocs.org/sdr/F3LA200700106), Apr 25, 2007: FLOOR PANEL. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED FLOOR PANEL 262FF AT R-2 DOOR CORRODED ON BOTTOM OF PANEL. REPLACED FLOORBOARD 262FF IAW AMM 53-42-12-400-001.
- [SDR F3LA200700098](https://openairdocs.org/sdr/F3LA200700098), Apr 25, 2007: RIB. SCRATCHED. DURING C-3 CHECK, INSPECTION REPORTED LE OF VERTICAL STAB FIN HAD DEEP SCRATCH MARKS (TOOL MARKS) BETWEEN PANELS NR 322BL AND 322CL ON ATTACHMENT BRACKET WHERE 
- [SDR F3LA200700099](https://openairdocs.org/sdr/F3LA200700099), Apr 24, 2007: LATCH. MISSING. DURING C-3 CHECK, INSPECTION REPORTED AFT OTBD NUTPLATE FOR THE AFT FILLER PLATE AROUND THE L2 DOOR GIRT BAR LATCH MISSING. REPLACED L2 DOOR SILL IAW SRM 51-42-
- [SDR F3LA200700097](https://openairdocs.org/sdr/F3LA200700097), Apr 24, 2007: SPLICE. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON OTBD UPPER ANGLE AFT ATTACHMENT HOLE UPON REMOVAL OF L2 DOOR SILL SPLICE ANGLES FWD OF FR66. REPLAC
- [SDR F3LA200700096](https://openairdocs.org/sdr/F3LA200700096), Apr 24, 2007: SILL. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION IN NUTPLATE HOLE UNDER THE FWD GIRT FITTING ON THE L2 DOOR SILL. REPLACED L2 DOOR SILL IAW SRM 51-42-11, FIG 6 A
- [SDR F3LA200700095](https://openairdocs.org/sdr/F3LA200700095), Apr 24, 2007: SILL. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION IN NUTPLATE HOLES ON THE L2 DOOR SILL PLATE AT FR66. REPLACED L2 DOOR SILL IAW SRM 51-42-11, FIG 6 AND 7.
- [SDR F3LA200700094](https://openairdocs.org/sdr/F3LA200700094), Apr 24, 2007: SILL. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR SILL PLATE HAD CORROSION FWD OF FR66. REPLACED L2 DOOR SILL IAW 51-42-11, FIG 6 AND 7.
- [SDR F3LA200700093](https://openairdocs.org/sdr/F3LA200700093), Apr 24, 2007: SILL. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR SILL THRESHOLD HAD CORROSION AROUND SEVERAL NUTPLATE HOLES. REPLACED L2 DOOR SILL IAW SRM 51-42-11, FIG 6 AND 7.
- [SDR F3LA200700092](https://openairdocs.org/sdr/F3LA200700092), Apr 24, 2007: FLOORBOARD. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED FLOORBOARD 222FF (R1 ENTRY) CORRODED. REPLACED FLOORBOARD 222FF IAW AMM 53-12-12-400-001.
- [SDR F3LA200700100](https://openairdocs.org/sdr/F3LA200700100), Apr 21, 2007: SILL. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED R2 DOOR SILL PLATE CORRODED FWD OF FR66. REPLACED R2 DOOR SILL IAW SRM 51-42-11.
- [SDR F3LA200700090](https://openairdocs.org/sdr/F3LA200700090), Apr 21, 2007: FLOORBEAM. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE HOLE ON FLOORBEAM -Y1292, AFT OF FR68. REPLACED FLOORBEAM AT FR68 STATION -Y1292 IAW SRM 51-42-
- [SDR F3LA200700088](https://openairdocs.org/sdr/F3LA200700088), Apr 21, 2007: FLOORBEAM. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE HOLE ON FLOORBEAM Y1292 FWD OF FR68. REPLACED FLOORBEAM AT Y1292 FWD OF FR68 IAW SRM 51-42-11, 
- [SDR F3LA200700087](https://openairdocs.org/sdr/F3LA200700087), Apr 21, 2007: FLOORBEAM. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE ON FLOORBEAM Y1292, AFT OF FR66. REPLACED FLOORBEAM AT Y1292 AFT OF FR66 IAW SRM 51-42-11, FIG 
- [SDR F3LA200700089](https://openairdocs.org/sdr/F3LA200700089), Apr 21, 2007: FLOORBEAM. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE HOLE ON FLOORBEAM Y1292 AFT OF FR68. REPLACED FLOORBEAM AT Y1292 AFT OF FR68 IAW 51-42-11, FIG 
- [SDR F3LA200700086](https://openairdocs.org/sdr/F3LA200700086), Apr 21, 2007: BUSHING. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED NLG UPPER TORSION LINK FROM STRUT CORRODED INSIDE ATTACH LUG. REMOVED CORROSION UNDER BUSHINGS OF NLG UPPER TORSION LINK A
- [SDR F3LA200700085](https://openairdocs.org/sdr/F3LA200700085), Apr 21, 2007: BOLT. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED WINGLET ATTACH HARDWARE RUSTY. REPLACED WINGLET ATTACH HARDWARE (MILD SURFACE CORROSION ON BOLT HEADS) ON LT WING IAW AMM 
- [SDR F3LA200600048](https://openairdocs.org/sdr/F3LA200600048), Jun 8, 2006: COMPUTER. FAILED. AIR TURNBACK. FLIGHT CREW REPORTED AILERON SERVO ECAM ON CLIMB. NORMAL LAW WAS LOST. RETURNED TO DEN AND PERFORMED AN OVERWEIGHT LANDING WITHOUT INCIDENT. REPLA
- [SDR F3LA200500042](https://openairdocs.org/sdr/F3LA200500042), Sep 17, 2005: COMPUTER. FAILED. FLIGHT CREW REPORTED A BURNING ELECTRICAL ODOR 20 MIN OUT FROM DEN FL390. APPROXIMATELY 20 SEC AFTER ODOR BEGAN, ECAM ANTI-ICE CAPT L & R STAT ILLUMINATED. REPL
- [SDR F3LA200500037](https://openairdocs.org/sdr/F3LA200500037), Aug 12, 2005: COOLING FAN. FAILED. FLIGHT CREW REPORTED LIVE TV SMOKE DETECTION WARNING HORN SOUNDED DURING FLIGHT. LIVE TV FAN C/B 2000VU POPPED AND WOULD NOT RESET. REPLACED AFT RACK COOLING FA
- [SDR F3LA200400070](https://openairdocs.org/sdr/F3LA200400070), Jul 19, 2004: SLEEVE. DAMAGED. FLIGHT CREW REPORTED NOSE WHEEL VIBRATION ON GEAR RETRACTION. FOUND NOSE WHEEL LT BEARING AND SLEEVE DAMAGED. REMOVED SLEEVE AND INSPECTED AXLE FOR DAMAGE. NO D
- [SDR F3LA200400005](https://openairdocs.org/sdr/F3LA200400005), Feb 4, 2004: WINDSHIELD. CRACKED. AIR TURNBACK, FLIGHT CREW REPORTED FIRST OFFICER'S WINDSHIELD CRACKED. DECLARED AN EMERGENCY, AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED FIRST OFFICER'S WINDSHI

## 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 20040108000709I](https://openairdocs.org/incident/20040108000709I), Jan 8, 2004: Airbus A318111 (N801FR). (-23) Aircraft encountered turbulence @ FL 270 enroute den to lax. Flight crew had just extinguished fasten seat belt sign and "b" flight attendant arose to…

---
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.