# N916FR: 2002 Airbus Industrie A319-112, registration cancelled 2009-04-13

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 13, 2009
- Exported to: Bermuda
- Status when cancelled: Valid registration
- Airframe: [Airbus Industrie A319-112](https://openairdocs.org/model/airbus-industrie-a319-112) (registry code 3930323)
- Engine: [CFM International CFM56-5B5/P series](https://openairdocs.org/engine/cfm-international-cfm56-5b5-p-series) (registry code 13016)
- Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM) (OpenAirDocs)
- Serial number: 1876
- Year built: 2002
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 9, 2008
- Certificate issued: December 9, 2008
- Last registry action: December 9, 2008
- Mode S code: ACAD82
- 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: 40.7558° 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/N916FR
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=916FR
- Page: https://openairdocs.org/deregistered/N916FR-2009-04-13

From the FAA registry file of November 4, 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 A319-112: https://openairdocs.org/model/airbus-industrie-a319-112.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 F3LA200800196](https://openairdocs.org/sdr/F3LA200800196), Apr 21, 2008: LAMP. BURNED OUT. DURING C4 S1 C CHECK INSPECTION NOTED LIGHT OUT IN AFT LEFT OVERWING EXIT. MAINTENANCE REMOVED AND REPLACED LAMP IN AFT LEFT EMERGENCY OVERWING LIGHT 63WL IN AC
- [SDR F3LA200800195](https://openairdocs.org/sdr/F3LA200800195), Apr 20, 2008: BRACKET. CORRODED. DURING C4 S1 C CHECK INSPECTION NOTED L2 DOOR SLIDE UPPER AFT MOUNT BRACKET HAD CORROSION. MAINTENANCE REMOVED AND REPLACED L2 DOOR SLIDE UPPER AFT MOUNT BRACKE
- [SDR F3LA200800194](https://openairdocs.org/sdr/F3LA200800194), Apr 20, 2008: BRACKET. CORRODED. DURING C4 S1 C CHECK INSPECTION NOTED R2 DOOR SLIDE UPPER AFT MOUNT BRACKET HAD CORROSION. MAINTENANCE REMOVED AND REPLACED R2 DOOR SLIDE UPPER AFT MOUNT BRACKE
- [SDR F3LA200800183](https://openairdocs.org/sdr/F3LA200800183), Apr 19, 2008: SEAT. CORRODED. DURING C4 S1 C CHECK INSPECTION NOTED CORROSION AT MOUNTING HOLES AFT LEFT FLIGHT ATTENDANT SEAT. MAINTENANCE REMOVED AND REPLACED AFT LEFT FLIGHT ATTENDANT SEA
- [SDR F3LA200800191](https://openairdocs.org/sdr/F3LA200800191), Apr 16, 2008: FLOORBOARD. PUNCTURED. DURING C4 S1 C CHECK INSPECTION NOTED FORWARD GALLEY FLOORBOARD 222EF HAS TWO PUNCTURES IN TOP RIGHT EDGE OF FLOORBOARD. MAINTENANCE REPAIRED PUNCTURES IN GALLE
- [SDR F3LA200800189](https://openairdocs.org/sdr/F3LA200800189), Apr 15, 2008: FLOOR PANEL. DAMAGED. DURING C4 S1 C CHECK INSPECTION NOTED FLOOR PANEL 232MF HAS HOLE IN FACE 1/4 INCH DIAMETER, 3 INCHES FROM INBOARD EDGE AND 3 FEET FROM FORWARD EDGE. MAINTENANCE
- [SDR F3LA200800188](https://openairdocs.org/sdr/F3LA200800188), Apr 13, 2008: FITTING. CORRODED. DURING C4 S1 C CHECK INSPECTION NOTED GIRT BAR FITTING WAS REMOVED ON R1 DOOR DUE TO CORROSION UNDER SPACERS. MAINTENANCE FABRICATED NEW NUT CLIP PLATES IN ACCO
- [SDR F3LA200800202](https://openairdocs.org/sdr/F3LA200800202), Apr 12, 2008: SUPPORT FITTING. CORRODED. DURING C4 S1 C CHECK INSPECTION, NOTED CENTER FLOORBEAM SUPPORT FITTING BETWEEN C59 AND C60 CORRODED. MAINTENANCE REMOVED CORROSION ON SUPPORT FITTING AND REINS
- [SDR F3LA200800163](https://openairdocs.org/sdr/F3LA200800163), Apr 11, 2008: FLOOR PANEL. DELAMINATED. DURING C4 S1 C CHECK INSPECTION REPORTED FLOOR PANEL 261CG HAD DELAMINATION FROM ONE SCREW HOLE. MAINTENANCE REPAIRED FLOOR PANEL 261CG IN ACCORDANCE WITH SRM 5
- [SDR F3LA200800162](https://openairdocs.org/sdr/F3LA200800162), Apr 11, 2008: FLOORBEAM. CORRODED. DURING C4 S1 C CHECK INSPECTION REPORTED CORROSION WAS FOUND ON NUT CLIP HOLE FLOORBEAM Y1292 AT FRAME 67 AND WAS FOUND UNSERVICEABLE. MAINTENANCE REMOVED AND R
- [SDR F3LA200800161](https://openairdocs.org/sdr/F3LA200800161), Apr 11, 2008: FLOOR SUPPORT. CORRODED. DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION AT NUT PLATES FWD CARGO PIT RIGHT SIDE FLOOR SUPPORT PLATE FRAME 28 TO FRAME 31. MAINTENANCE REMOVED AND REP
- [SDR F3LA200800160](https://openairdocs.org/sdr/F3LA200800160), Apr 11, 2008: FLOOR SUPPORT. CORRODED. DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE AFT BULKHEAD FLOOR SUPPORT PLATE, IN THE FORWARD CARGO PIT, AT FRAME 31, BETWEEN STRINGERS 
- [SDR F3LA200800159](https://openairdocs.org/sdr/F3LA200800159), Apr 11, 2008: FLOOR SUPPORT. CORRODED. DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND AROUND THE NUT PLATE HOLES OF THE FLOOR SUPPORT PLATE ON THE LEFT SIDE OF THE FORWARD CARGO COMPAR
- [SDR F3LA200800158](https://openairdocs.org/sdr/F3LA200800158), Apr 11, 2008: DUMMY RAIL. CORRODED. DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON DUMMY RAIL Y503.2 AT FRAME 16. MAINTENANCE REMOVED AND REPLACED THE DUMMY RAIL IN ACCORDANCE WI
- [SDR F3LA200800157](https://openairdocs.org/sdr/F3LA200800157), Apr 11, 2008: FLOOR SUPPORT. CORRODED. DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON FLOOR SUPPORT-Y1292, BETWEEN FRAMES 16 AND 20. MAINTENANCE REMOVED AND REPLACED THE CORRODED FL
- [SDR F3LA200800190](https://openairdocs.org/sdr/F3LA200800190), Apr 10, 2008: FLOORBEAM. CORRODED. DURING C4 S1 C CHECK INSPECTION NOTED CORROSION AT NUT PLATES AFT PIT LEFT FLOORBEAM UNDER COVER PROFILE AT FRAME 56 LOCATED FROM STRINGER 38 LEFT TO 38 RIGHT. 
- [SDR F3LA200800185](https://openairdocs.org/sdr/F3LA200800185), Apr 10, 2008: FLOORBEAM. CORRODED. DURING C4 S1 C CHECK INSPECTION NOTED CORROSION AT NUT PLATES AFT PIT LEFT HAND FLOORBEAM UNDER COVER PROFILE AT FRAME 58 LOCATED FROM STRINGER 38 LEFT TO 38 RI
- [SDR F3LA200800184](https://openairdocs.org/sdr/F3LA200800184), Apr 10, 2008: MOUNT. CORRODED. DURING C4 S1 C CHECK INSPECTION NOTED RIGHT WIND SCREEN LOWER ATTACH MOUNTS WERE CORRODED. MAINTENANCE REMOVED AND REPLACED RIGHT WINDSCREEN LOWER ATTACH MOUNTS
- [SDR F3LA200800173](https://openairdocs.org/sdr/F3LA200800173), Apr 10, 2008: FITTING. CORRODED. DURING C4 S1 C CHECK INSPECTION NOTED R2 FORWARD GIRT BAR FITTING PLATE CORODDED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED FITTING PLATE. OKAY TO INST
- [SDR F3LA200800171](https://openairdocs.org/sdr/F3LA200800171), Apr 10, 2008: FITTING. CORRODED. DURING C4 S1 C CHECK INSPECTION NOTED R1 FORWARD GIRT BAR FITTING PLATE WAS CORRODED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED FITTING PLATE. OKAY TO 
- [SDR F3LA200800198](https://openairdocs.org/sdr/F3LA200800198), Apr 9, 2008: SUPPORT. CORRODED. DURING C4 S1 C CHECK INSPECTION NOTED FRAME 59 COVER PROFILE NUT PLATE HOLES WERE CORRODED FROM STRINGER 38 RIGHT TO 38 LEFT. MAINTENANCE BLENDED OUT CORROSION 
- [SDR F3LA200800152](https://openairdocs.org/sdr/F3LA200800152), Apr 7, 2008: PLATE. CRACKED. DURING C4 S1 C CHECK, INSPECTION REPORTED A CRACK WAS FOUND IN THE MOULLION PLATE LOCATED AFT OF THE L2 DOOR FRAME AT THE JOINT SHEET ATTACH POINT. MAINTENANCE 
- [SDR F3LA200800203](https://openairdocs.org/sdr/F3LA200800203), Apr 6, 2008: FLOOR PANEL. DELAMINATED. DURING C4 S1 C CHECK INSPECTION NOTED FLOOR PANEL 222EF DELAMINATED AT EDGE. MAINTENANCE REPAIRED FLOOR PANEL 222EF IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9
- [SDR F3LA200800201](https://openairdocs.org/sdr/F3LA200800201), Apr 6, 2008: FLOORBEAM. CORRODED. DURING C4 S1 C CHECK INSPECTION NOTED AFT CARGO PIT CENTER FLOORBEAM BETWEEN C58 AND C59 NUT PLATES HAVE SIGNS OF CORROSION. MAINTENANCE REMOVED OLD FLOORBEAM A
- [SDR F3LA200800187](https://openairdocs.org/sdr/F3LA200800187), Apr 6, 2008: FLOOR PANEL. CORRODED. DURING C4 S1 C CHECK INSPECTION NOTED FLOOR PANEL 221PF LAV A HAS CORROSION ON BOLT HOLES. MAINTENANCE RECEIVED NEW FLOOR PANEL 221PK, OKAY TO INSTALL AND INSTA
- [SDR F3LA200800186](https://openairdocs.org/sdr/F3LA200800186), Apr 6, 2008: STRIP. CORRODED. DURING C4 S1 C CHECK INSPECTION NOTED BOTH LEFT 1 AND RIGHT 1 GAP STRIPS CORRODED ON LOWER SURFACE. MAINTENANCE REMOVED AND REPLACED LEFT 1 AND RIGHT 1 GAP STRI
- [SDR F3LA200800172](https://openairdocs.org/sdr/F3LA200800172), Apr 6, 2008: FLOOR SUPPORT. CORRODED. DURING C4 S1 C CHECK INSPECTION NOTED CORROSION AROUND NUT PLATES AFT CARGO PIT FLOOR PROFILE BETWEEN C55 AND C56. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED 
- [SDR F3LA200800178](https://openairdocs.org/sdr/F3LA200800178), Apr 6, 2008: PROFILE. CORRODED. DURING C4 S1 C CHECK INSPECTION NOTED CORROSION AROUND NUT PLATES AFT CARGO PIT LEFT FLOOR PROFILE AT C 58. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDAN
- [SDR F3LA200800177](https://openairdocs.org/sdr/F3LA200800177), Apr 6, 2008: FLOORBEAM. CORRODED. DURING C4 S1 C CHECK INSPECTION REPORTED NUT PLATE CORRODED OUTBOARD OF CENTER FLOORBEAM AFT CARGO PIT C 56 1. MAINTENANCE REMOVED AND REPLACED NEW C 56 PROFILE
- [SDR F3LA200800174](https://openairdocs.org/sdr/F3LA200800174), Apr 6, 2008: FLOORBEAM. CORRODED. DURING C4 S1 C CHECK INSPECTION REPORTED FLOORBEAM Y1292 SHOWS SIGNS OF CORROSION AT FRAME 16. MAINTENANCE REPLACED ONE SECTION OF THE BEAM IN ACCORDANCE WITH T
- [SDR F3LA200800136](https://openairdocs.org/sdr/F3LA200800136), Apr 6, 2008: DUMMY RAIL. CORRODED. DURING C4 S1 C-CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON DUMMY RAIL Y503.2 AT FRAME 16. MAINTENANCE REMOVED AND REPLACED DUMMY RAIL IN ACCORDANCE WITH T
- [SDR F3LA200800199](https://openairdocs.org/sdr/F3LA200800199), Apr 5, 2008: FLOOR PANEL. DELAMINATED. DURING C4 S1 C CHECK INSPECTION NOTED FLOOR PANEL 261HG HAS DELAMINATION AROUND EDGES. MAINTENANCE REPAIRED FLOOR PANEL 261HG IN ACCORDANCE WITH THE REQUIREMENT
- [SDR F3LA200800156](https://openairdocs.org/sdr/F3LA200800156), Apr 5, 2008: FLOOR PANEL. CORRODED. DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE UNDERSIDE OF FLOOR PANEL 222FF. MAINTENANCE REMOVED THE CORRODED PANEL. THE NEW PANEL WAS I
- [SDR F3LA200800155](https://openairdocs.org/sdr/F3LA200800155), Apr 5, 2008: FLOOR PANEL. CORRODED. DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE UNDERSIDE OF FLOOR PANEL 221FF. MAINTENANCE REMOVED CORRODED PANEL. THE NEW PANEL WAS INSTA
- [SDR F3LA200800204](https://openairdocs.org/sdr/F3LA200800204), Apr 4, 2008: SILL. CORRODED. DURING C4 S1 C CHECK INSPECTION NOTED R2 DOOR SILL HAS CORROSION AROUND NUT CLIP HOLE AT FRAME 66. MAINTENANCE FABRICATED REPAIR ANGLE IN ACCORDANCE WITH THE RE
- [SDR F3LA200800154](https://openairdocs.org/sdr/F3LA200800154), Apr 4, 2008: FLOOR PANEL. CORRODED. DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THREE INSERTS ON FLOOR PANEL 261PF. MAINTENANCE REMOVED THE CORRODED PANEL. THE NEW PANEL WAS I
- [SDR F3LA200800153](https://openairdocs.org/sdr/F3LA200800153), Apr 4, 2008: FLOORBEAM. CORRODED. DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE FORWARD LAVATORY FLOOR ANGLE BRACKET, ON ITS UNDERSIDE. MAINTENANCE REMOVED AND REPLACED TH
- [SDR F3LA200800151](https://openairdocs.org/sdr/F3LA200800151), Apr 4, 2008: FLOOR SUPPORT. CORRODED. DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND AROUND THE NUT CLIP HOLES ON FLOOR BEAM Y1292 BETWEEN FRAMES 68 AND 69. MAINTENANCE REMOVED AND RE
- [SDR F3LA200800140](https://openairdocs.org/sdr/F3LA200800140), Apr 4, 2008: SHEAR PLATE. CORRODED. DURING C4 S1 CHECK INSPECTION REPORTED CORROSION WAS FOUND ON SHEAR PLATE AT FLOORBEAM Y1732 AFT OF FRAME 69. MAINTENANCE REMOVED AND REPLACED SHEAR PLATE IN AC
- [SDR F3LA200800139](https://openairdocs.org/sdr/F3LA200800139), Apr 4, 2008: SHEAR PLATE. CORRODED. DURING C4 S1 C-CHECK INSPECTION REPORTED CORROSION WAS FOUND ON SHEAR PLATE AT FLOORBEAM Y1732 AFT OF FRAME 69. MAINTENANCE REMOVED AND REPLACE SHEAR PLATE IN A
- [SDR F3LA200800138](https://openairdocs.org/sdr/F3LA200800138), Apr 4, 2008: SUPPORT. CORRODED. DURING C4 S1 C-CHECK, INSPECTION REPORTED CORROSION WAS FOUND AT FRAME SUPPORT OF FLOORBEAM Y1732 AFT OF FRAME 69. MAINTENANCE REMOVED AND REPLACED FRAME SUPPOR
- [SDR F3LA200800137](https://openairdocs.org/sdr/F3LA200800137), Apr 4, 2008: SUPPORT. CORRODED. DURING C4 S1 C-CHECK, INSPECTION REPORTED CORROSION WAS FOUND AT FRAME SUPPORT OF FLOORBEAM Y1732 AFT OF FRAME 69. MAINTENANCE REMOVED AND REPLACED FRAME SUPPOR
- [SDR F3LA200800200](https://openairdocs.org/sdr/F3LA200800200), Apr 3, 2008: SUPPORT BRACKET. CORRODED. DURING C4 S1 C CHECK INSPECTION NOTED THE NOSE LANDING GEAR DECORATIVE DOOR LOWER ATTACH POINTS ON STRUT WERE CORRODED AND WORN. MAINTENANCE REMOVED AND REPLACE
- [SDR F3LA200700277](https://openairdocs.org/sdr/F3LA200700277), Oct 8, 2007: BATTERY. DISCHARGED. FLIGHT CREW REPORTED EMERGENCY LIGHTS "ON" CAUSING LOW VOLTAGE ON AIRCRAFT BATTERY. REMOVED AND REPLACED NR 1 MAIN BATTERY IAW AMM 24-38-37 PB401. OPS CHECKED G
- [SDR F3LA200600158](https://openairdocs.org/sdr/F3LA200600158), Nov 6, 2006: CABLE. BROKEN. DURING C-3 CHECK, INSPECTION REPORTED RT EMERGENCY EXIT SLIDE INFLATION CABLE BROKEN. REPLACED RESERVOIR IAW AMM 25-62-46.
- [SDR F3LA200600107](https://openairdocs.org/sdr/F3LA200600107), Sep 8, 2006: LINE. LEAKING. DURING CRUISE, FLIGHT CREW REPORTED ECAM READING: HYD GREEN RSVR LO LVL G ENG 1 NR 1 PUMP LO PRESS. FOUND NR 1 ENG HYD LOW PRESSURE SWITCH LINE LEAKING. REPLACE
- [SDR F3LA200600040](https://openairdocs.org/sdr/F3LA200600040), Jun 7, 2006: FILTER. DIRTY. ON SHORT FINAL, A PLASTIC-TYPE BURNING ODOR, WHICH DISSIPATED ON LANDING, NO SMOKE. PERFORMED VISUAL INSP OF CABIN LIVE TV SYSTEM. FOUND SYSTEM OPERATIONAL. PER
- [SDR F3LA200500014](https://openairdocs.org/sdr/F3LA200500014), Mar 22, 2005: FAN. INOPERATIVE. FLIGHT CREW REPORTED VENT EXTRACT FAULT. NOTICED AIRCRAFT VIBRATION, FRONT RIGHTSIDE, AND SMELL OF ELECTRICAL SMOKE FRONT TO BACK OF AIRCRAFT. DECLARED AN EMERG

## 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 20041223034819I](https://openairdocs.org/incident/20041223034819I), Dec 23, 2004: Airbus A319112 (N916FR), Chicago, IL, Substantial damage. (-23) "Industrial incident-no intent to fly" at 2330L on 23 December 04, frontier airlines aircraft N916FR was parked at gate A2, at Chicago Midway Airport,…

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