# N951LF: Airbus Industrie A320-233, registration cancelled 2014-03-19

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 19, 2014
- Status when cancelled: Valid registration
- Airframe: [Airbus Industrie A320-233](https://openairdocs.org/model/airbus-industrie-a320-233) (registry code 3930329)
- Engine: [IAE V2527-A5](https://openairdocs.org/engine/iae-v2527-a5) (registry code 34604)
- Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM), [TCDS E40NE](https://openairdocs.org/tcds/E40NE) (OpenAirDocs)
- Serial number: 460
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 21, 1997
- Certificate issued: February 5, 2013
- Last registry action: February 5, 2013
- Mode S code: AD395E
- Owner when cancelled: [Acg Acquisition Xx LLC](https://openairdocs.org/faa-owner/ACG%20ACQUISITION%20XX%20LLC)
- Location: [Newport Beach, CA](https://openairdocs.org/faa-place/CA/Newport%20Beach)
- Owner type: Corporation
- Owner's area on the map: 33.6346° N, 117.8749° W: Placed by OpenAirDocs at the center of ZIP code 92660, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N951LF
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=951LF
- Page: https://openairdocs.org/deregistered/N951LF-2014-03-19

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 Industrie A320-233: https://openairdocs.org/model/airbus-industrie-a320-233.md

## Service difficulty reports (85, newest 50)

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

- [SDR 2004F00318](https://openairdocs.org/sdr/2004F00318), Jul 13, 2004: INLET. DEPARTED. AFTER TAKEOFF, NR 1 ENGINE INBOARD AND OUTBOARD FAN COWL DEPARTED AIRCRAFT. A SHUTTER WAS FELT BY THE AIRCREW AND THE NR 1 ENGINE INSTRUMENT LIGHTS FLASHED AMBE
- [SDR RYN2004F00001](https://openairdocs.org/sdr/RYN2004F00001), Feb 21, 2004: ENGINE. MALFUNCTIONED. ON TAKEOFF, THERE WAS A LOUD BANG AND ECAM WARNING INDICATED EGT OVERTEMP ON NR 2 ENGINE. ECAM PROCEDURES FOLLOWED AND EMERGENCY DECLARED. AIRCAFT RETURNED, AND
- [SDR RYN2004F00011](https://openairdocs.org/sdr/RYN2004F00011), Oct 19, 2003: FLOOR SUPPORT. CORRODED. AT (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 34 ABOVE STRINGER 34 IN FORWARD CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME
- [SDR RYN2004F00005](https://openairdocs.org/sdr/RYN2004F00005), Oct 19, 2003: FLOOR SUPPORT. CORRODED. AT (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT FROM FRAME 31 TO 34 AT STRINGER 34L IN FORWARD CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT FR
- [SDR RYN2004F00004](https://openairdocs.org/sdr/RYN2004F00004), Oct 19, 2003: FLOOR SUPPORT. CORRODED. A (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT FROM FRAME 28 TO 31 AT STRINGER 34R.
- [SDR RYN2004F00003](https://openairdocs.org/sdr/RYN2004F00003), Oct 19, 2003: FLOOR SUPPORT. CORRODED. AT (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT FROM FRAME 31 TO 33 AT STRINGER 34R IN FORWARD CARGO COMPARTMENT. FABRICATED NEW FLOORBOARD SUPPORT. TREATED
- [SDR RYN2004F00002](https://openairdocs.org/sdr/RYN2004F00002), Oct 19, 2003: FLOOR SUPPORT. CORRODED. A (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 34 AND STRINGERS 34R TO 34L IN FORWARD CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT AT
- [SDR 2004F00242](https://openairdocs.org/sdr/2004F00242), Oct 2, 2003: INTERCOSTAL. CORRODED. AT C-CHECK, OFUND AFT CARGO COMPARTMENT FLOOR INTERCOSTAL CORRODED AT FRAME 54 AND RBL 17. REMOVED CORROSION FROM INTERCOSTAL AT FRAME 54, RBL 17. NO MEASUREABL
- [SDR 2004F00383](https://openairdocs.org/sdr/2004F00383), Oct 2, 2003: INTERCOSTAL. CORRODED. AT C-CHECK, OFUND AFT CARGO FLOOR INTERCOSTAL IS CORRODED AT FRAME 56 AND RBL 22-24. REMOVED CORROSION FROM INTERCOSAL AT FRAME 56, RBL 22-24. NO MEASUREABLE MA
- [SDR 2004F00181](https://openairdocs.org/sdr/2004F00181), Oct 2, 2003: INTERCOSTAL. CORRODED. AT C-CHECK, FOUNDINTERCOSTAL AT FORWARD CARGO COMPARTMENT BETWEEN FRAME 51 AND 52 RBL 27 HAS SURFACE CORROSION. REMOVED AND REPLACED INTERCOSTAL AT AFT CARGO CO
- [SDR 2004F00094](https://openairdocs.org/sdr/2004F00094), Oct 2, 2003: FLOORBOARD. PUNCTURED. AT C-CHECK, FOUND AFT CABIN FLOORBOARD NR 261DF HAS MULTIPLE PUNCTURES. REPAIRED AFT CABIN FLOORBOARD PANEL NR 261DF. (M)
- [SDR 2004F00089](https://openairdocs.org/sdr/2004F00089), Oct 2, 2003: FLOOR SUPPORT. CORRODED. AT C-CHECK, FOUND AFT CABIN FLOOR SUPPORT HAS CORROSION AT STATION 3850 AND RBL 32. REMOVED LIGHT CORROSION AT NUT PLATE AT STATION 3850 AND RBL 32. FOUND TO BE
- [SDR 2004F00228](https://openairdocs.org/sdr/2004F00228), Sep 26, 2003: INTERCOSTAL. CORRODED. AT C-CHECK, FOUND INTERCOSTAL LOCATED BETWEEN FRAME 50 AND 51 RBL 27 AT AFT CARGO COMPARTMENT IS CORRODED AT FORWARD END. (M)
- [SDR 2004F00091](https://openairdocs.org/sdr/2004F00091), Sep 26, 2003: MOUNT. DAMAGED. AT C-CHECK, FOUND NR 1 ENGINE FORWARD MOUNT STOP SERIAL NR 0313-PTE HAS GOUGING IN BOLT HOLES. CLEANED NR 1 ENGINE FORWARD MOUNT STOP, S/N 0313. NO GOUGING NOTE
- [SDR 2004F00068](https://openairdocs.org/sdr/2004F00068), Sep 26, 2003: PLATE. CORRODED. AT C-CHECK, FOUND INTERCOSTAL AT AFT CARGO COMPARTMENT FRAME 48 TO 49, LBL 27 WITH SURFACE CORROSION. REMOVED AND REPLACED INTERCOSTAL PLATE AT AFT CARGO COMPAR
- [SDR 2004F00067](https://openairdocs.org/sdr/2004F00067), Sep 26, 2003: CROSSBEAM. DAMAGED. AT C-CHECK, FOUND NR 1 ENGINE FORWARD MOUNT CROSSBEAM HAS NICKS, SCRATCHES, AND GOUGING. INSPECTED AND CLEANED DAMAGED AREA. REPAIRED NR 1 ENGINE FORWARD MOUNT 
- [SDR 2004F00066](https://openairdocs.org/sdr/2004F00066), Sep 26, 2003: FITTING. CORRODED. AT C-CHECK, FOUND FLOOR SUPPORT FITTING AT AFT CARGO COMPARTMENT FRAME 56, LBL 12 IS CORRODED AROUND 2 EACH FASTENER HOLES. REMOVED AND REPLACED FLOOR SUPPORT F
- [SDR 2004F00065](https://openairdocs.org/sdr/2004F00065), Sep 26, 2003: FITTING. CORRODED. AT C-CHECK, FOUND FLOOR SUPPORT FITTING AT AFT CARGO COMPARTMENT FRAME 56 BL 0 IS CORRODED AROUND 2 EACH FASTENER HOLES. REMOVED AND REPLACED FLOOR SUPPORT FITT
- [SDR 2004F00064](https://openairdocs.org/sdr/2004F00064), Sep 26, 2003: SKIN. DAMAGED. AT C-CHECK, FOUND UPPER FUSELAGE CROWN AREA BETWEEN FRAMES 52 AND 53 STRINGER 1 LT AND 1 RT VHF ANTENNA MOUNT SURFACE HAS TOOL MARKS AROUND PERIPHERY. UPON FURT
- [SDR 2004F00063](https://openairdocs.org/sdr/2004F00063), Sep 26, 2003: STRINGER. CORRODED. AT C-CHECK, FOUND AFT CABIN FUSELAGE STRINGER FLOOR LEVER UPPER SURFACE CORRODED BETWEEN FRAMES 68-69 AT STATION 3280. REMOVED AND REPLACED STRINGER 21L BETWEEN
- [SDR 2004F00138](https://openairdocs.org/sdr/2004F00138), Sep 17, 2003: SILL. CORRODED. AT C-CHECK, FOUND CORROSION AT L2 DOOR INBOARD OF AFT GIRT BAR ATTACH PLATE AT FRAME 68 AND LBL 50. REMOVED AND REPLACED L2 DOOR SILL, LOWER FORWARD CORNER FITT
- [SDR 2004F00137](https://openairdocs.org/sdr/2004F00137), Sep 17, 2003: FLOORBOARD. CORRODED. AT C-CHECK, FOUND CORROSION ON MAIN CABIN FLOORBOARD PANEL NR 222FF. REPAIRED MAIN CABIN FLOORBOARD NR 222FF. (M)
- [SDR 2004F00135](https://openairdocs.org/sdr/2004F00135), Sep 17, 2003: FLOORBOARD. CORRODED. AT C-CHECK, FOUND CORROSION ON MAIN CABIN FLOORBOARD PANEL NR 221FF. REMOVED SURFACE CORROSION FROM FLOORBOARD 221FF. MATERIAL LOSS FOUND TO BE WITHIN LIMITS. T
- [SDR 2004F00123](https://openairdocs.org/sdr/2004F00123), Sep 17, 2003: PAN. CORRODED. AT C-CHECK, FOUND CORROSION ON LEFT AFT LAVATORY FLOOR PAN ASSEMBLY ATTACH POINTS FOR BLOW-OUT DOOR FRAME, 8 PLACES. AFTER EVALUATION, FOUND NO CORROSION ON LEF
- [SDR 2004F00120](https://openairdocs.org/sdr/2004F00120), Sep 17, 2003: FLOORBEAM. CORRODED. AT C-CHECK, FOUND CORROSION AT R2 DOOR FLOORBEAM 8 INCHES INBOARD OF DOOR CUT OUT FROM FRAMES 66 TO 68 RBL 50. REPAIRED CORRODED AREA AT R2 DOOR FLOORBEAM, 8 IN
- [SDR 23431924](https://openairdocs.org/sdr/23431924), Sep 17, 2003: SILL. CORRODED. AT (C) CHECK, FOUND L2 DOOR SILL HAS RIVET HEADS THAT HAVE EXFOLIATED CORROSION BETWEEN FR 66 AND FR 68. REMOVED AND REPLACED L2 DOOR SILL, LOWER FORWARD CORNER
- [SDR 2004F00139](https://openairdocs.org/sdr/2004F00139), Sep 16, 2003: FITTING. CORRODED. AT C-CHECK, FOUND CORROSION ON FITTING AT FRAME 59 AND STRINGER 41R IN AFT CARGO BAY. FITTING AT FRAME 59, RIGHT STRINGER 41 OF FLOOR STRUCTURE REMOVED AND REPL
- [SDR 2004F00134](https://openairdocs.org/sdr/2004F00134), Sep 16, 2003: FLOOR SUPPORT. CORRODED. AT C-CHECK, FOUND FLOORBOARD SUPPORT CORRODED AT RIGHT STRINGER 38 BETWEEN FRAME 58 AND 59 ON AFT LOWER CARGO BAY FLOOR. REMOVED AND REPLACED FLOOR SUPPORT FRAM
- [SDR 2004F00133](https://openairdocs.org/sdr/2004F00133), Sep 16, 2003: FLOOR SUPPORT. DAMAGED. AT C-CHECK, FOUND 5 DAMAGED AREAS ON FLOORBOARD SUPPORT AT FRAME 59 BETWEEN STRINGER 42R AND 43L IN AFT CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPO
- [SDR 2004F00132](https://openairdocs.org/sdr/2004F00132), Sep 16, 2003: SEAT TRACK. CORRODED. AT C-CHECK, FOUND SEAT TRACK CORRODED BETWEEN FRAMES 20 AND 21 AT RBL 32. REMOVED AND REPLACED SEAT TRACK FROM RBL 32, FRAME 12 TO 24. (M)
- [SDR 2004F00124](https://openairdocs.org/sdr/2004F00124), Sep 16, 2003: FLOORBEAM. CORRODED. AT C-CHECK, FOUND CORROSION ON FLOORBEAM AT FRAME 20 AT RBL 12. REMOVED AND REPLACED FLOORBEAM AND SPLICE AT FRAME 20, RBL 12. (M)
- [SDR 2004F00113](https://openairdocs.org/sdr/2004F00113), Sep 15, 2003: STRUCTURE. CORRODED. AT C-CHECK, OFUND CORROSION ON AFT CABIN FLOOR STRUCTURE AT FRAME 67 PLUS 13 INCHES TO FRAME 67 AT LBL 45. REMOVED AND REPLACED AFT CABIN FLOOR STRUCTURE AT FRA
- [SDR 2004F00112](https://openairdocs.org/sdr/2004F00112), Sep 15, 2003: STRUCTURE. CORRODED. AT C-CHECK, FOUND CORROSION ON FLOOR STRUCTURE AT FRAME 69 PLUS 3 INCHES TO 69 PLUS 10 INCHES AND LBL 50 IN CABIN. REMOVED AND REPLACED AFT CABIN FLOOR STRUCTUR
- [SDR 2004F00060](https://openairdocs.org/sdr/2004F00060), Sep 15, 2003: PLATE. WORN. AT C-CHECK, FOUND R2 DOOR CAM PLATE FOR DOOR HANDLE BACK MECHANISM ROLLER HAD WEAR MARKS. REMOVED AND REPLACED FITTING ON R2 DOOR, DOOR HANDLE BACK MECHANISM. (
- [SDR 2004F00059](https://openairdocs.org/sdr/2004F00059), Sep 15, 2003: FITTING. GOUGED. AT C-CHECK, FOUND GOUGES ON THE LATCHES OF THE LOWER FITTING OF THE RT FORWARD EMERGENCY EXIT DOOR. REMOVED AND REPLACED LOWER LATCH FITTINGS ON RT FORWARD EMER
- [SDR RYN2004F00009](https://openairdocs.org/sdr/RYN2004F00009), Sep 15, 2003: ATTACH FITTING. CORRODED. AT (C) CHECK FOUND AFT CABIN NR 2 RT DOORWAY, FORWARD GIRT BAR ATTACH FITTING PLATE, WITH CORROSION. REMOVED AND REPLACED FORWARD GIRT BAR ATTACH FITTING PLATE 
- [SDR RYN2004F00008](https://openairdocs.org/sdr/RYN2004F00008), Sep 15, 2003: ATTACH FITTING. CORRODED. AT (C) CHECK FOUND AFT CABIN NR 2 RT DOORWAY AFT GIRT BAR ATTACH FITTING PLATE WITH CORROSION. REMOVED AND REPLACED AFT GIRT BAR ATTACH FITTING PLATE ON AFT CAB
- [SDR RYN2004F00006](https://openairdocs.org/sdr/RYN2004F00006), Sep 15, 2003: LATCH. DAMAGED. AT (C) CHECK, FOUND GOUGE ON FORWARD LT EMERGENCY EXIT DOOR LOWER AFT FITTING LATCH. REMOVED AND REPLACED FORWARD LT EMERGENCY EXIT DOOR, LOWER AFT LATCH FITTIN
- [SDR 2004F00227](https://openairdocs.org/sdr/2004F00227), Sep 13, 2003: FLOOR SUPPORT. BENT. AT C-CHECK, FOUND FLOOR PANEL SUPPORT FOR FLOOR PANEL 232WF IS BENT. FORMED FLOOR PANEL SUPPORT AT FLOOR PANEL NR 232WF BACK TO ORIGINAL CONTOUR. (M)
- [SDR 2004F00136](https://openairdocs.org/sdr/2004F00136), Sep 12, 2003: PAN. CORRODED. AT C-CHECK, FOUND CORROSION ON LEFT AFT LAVATORY FLOOR PAN ASSEMBLY ATTACH POINTS FOR BLOW-OUT DOOR FRAME, 8 PLACES. AFTER EVALUATION, FOUND NO CORROSION ON LEF
- [SDR 2004F00116](https://openairdocs.org/sdr/2004F00116), Sep 12, 2003: FLOOR PANEL. CORRODED. AT C-CHECK FOUND EXFOLIATED CORROSION AT AFT CARGO COMPARTMENT FLOOR PANEL 151DF. FABRICATED AND INSTALLED FLOOR PANEL NR 151DF, AFT CARGO COMPARTMENT. (M)
- [SDR 2004F00111](https://openairdocs.org/sdr/2004F00111), Sep 12, 2003: FLOOR PANEL. CORRODED. AT C-CHECK, FOUND CORROSON ON FLOOR PANEL NR 152BF IN AFT CARGO COMPARTMENT. FABRICATED, PRIMED AND INSTALLED AFT CARGO FLOOR PANEL NR 152BF. (M)
- [SDR 2004F00118](https://openairdocs.org/sdr/2004F00118), Sep 12, 2003: FLOOR PANEL. CORRODED. AT C-CHECK, FOUND DAMAGE ON UPPER SKIN AND CORROSION ON FLOOR PANEL NR 151BF IN AFT CARGO BAY. FABRICATED AND INSTALLED NEW AFT CARGO COMPARTMENT, FLOOR PANEL N
- [SDR RYN2004F00007](https://openairdocs.org/sdr/RYN2004F00007), Sep 12, 2003: FLOOR PANEL. CORRODED. AT (C) CHECK FOUND AFT LAV FLOOR PANEL WITH CORROSION AT NUMEROUS LOCATIONS AT ATTACHMENT POINTS FOR BLOW OUT DOOR FRAME. REPAIRED AFT LAV FLOOR PANEL, CORROSIO
- [SDR 2004F00114](https://openairdocs.org/sdr/2004F00114), Sep 11, 2003: FLOOR PANEL. CORRODED. AT C-CHECK, FOUND CORROSION ON FLOOR PANEL NR 152EF IN AFT CARGO BAY. FABRICATED, TREATED, PRIMED AND INSTALLED AFT CARGO COMPARTMENT FLOOR PANEL NR 152EF. (M)
- [SDR 2004F00141](https://openairdocs.org/sdr/2004F00141), Sep 10, 2003: FLOOR SUPPORT. CORRODED. AT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 63 ABOVE STRINGER 38L IN AFT CARGO BAY. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 63 ABOVE STR
- [SDR 2004F00131](https://openairdocs.org/sdr/2004F00131), Sep 10, 2003: FLOOR SUPPORT. CORRODED. AT C-CHECK, FOUND FLOORBOARD SUPPORT CORRODED AT FRAME 58 BETWEEN STRINGER 38R AND 40R IN AFT LOWER CARGO COMPARTMENT. REMOVED FLOORBOARD SUPPORT, FABRICATED AN
- [SDR 2004F00130](https://openairdocs.org/sdr/2004F00130), Sep 10, 2003: FLOOR SUPPORT. CORRODED. AT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 59 ABOVE STRINGER 40L IN AFT LOWER CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT CHANNEL
- [SDR 2004F00129](https://openairdocs.org/sdr/2004F00129), Sep 10, 2003: FLOOR SUPPORT. CORRODED. AT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FASTENER HOLE BETWEEN FRAME 60 AND 61 ABOVE STRINGER 43L IN AFT LOWER CARGO BAY. REMOVED AND REPLACED FLOOR
- [SDR 2004F00128](https://openairdocs.org/sdr/2004F00128), Sep 10, 2003: FLOOR SUPPORT. CORRODED. AT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT BETWEEN FRAME 58 AND 59 ABOVE STRINGER 38R IN AFT LOWER CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUP

All 85: https://openairdocs.org/deregistered/N951LF-2014-03-19/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ATL04IA156](https://openairdocs.org/ntsb/ATL04IA156), Jul 13, 2004: Airbus Industrie A320-233 (N951LF), Atlanta, GA, incident, minor damage. Probable cause: The failure of company maintenance personnel to secure the nacelle/cowl doors, which resulted in a separation of the doors during takeoff initial climb.

## 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 20040713030279I](https://openairdocs.org/incident/20040713030279I), Jul 13, 2004: Airbus A320233 (N951LF), Atlanta, GA, Minor damage. (-23) Per pilot line report (on take-off, a passenger notified a flight attendant that something had come off of the #1 engine. The flight attendant notified…

---
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.