# Service difficulty reports: N951LF, cancelled Mar 19, 2014 A list on [N951LF, cancelled Mar 19, 2014](https://openairdocs.org/deregistered/N951LF-2014-03-19.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 85 reports - [SDR 2004F00318](https://openairdocs.org/sdr/2004F00318.md): Inlet · departed · Jul 13, 2004 · N951LF · Airbus A320233 · Engine Air Intake System > 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 AMBER AND THEN WENT TO NORMAL. THE NR 1 ENGINE OIL QUANTITY LIGHT REMAINED AMBER. AN EMERGENCY WAS DEC - [SDR RYN2004F00001](https://openairdocs.org/sdr/RYN2004F00001.md): Engine · malfunctioned · Feb 21, 2004 · N951LF · Engine (Turbine/Turboprop) > 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 LANDED WITHOUT INCIDENT. - [SDR RYN2004F00011](https://openairdocs.org/sdr/RYN2004F00011.md): Floor Support · corroded · Oct 19, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous Structure > 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 34 JUST ABOVE 34L IN FORWARD CARGO COMPARTMENT. - [SDR RYN2004F00005](https://openairdocs.org/sdr/RYN2004F00005.md): Floor Support · corroded · Oct 19, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous Structure > 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 FROM FRAME 31 TO 34, STRINGER 34L IN FORWARD PIT. - [SDR RYN2004F00004](https://openairdocs.org/sdr/RYN2004F00004.md): Floor Support · corroded · Oct 19, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous Structure > A (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT FROM FRAME 28 TO 31 AT STRINGER 34R. - [SDR RYN2004F00003](https://openairdocs.org/sdr/RYN2004F00003.md): Floor Support · corroded · Oct 19, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous Structure > 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, PRIMED, TOP COATED AND INSTALLED FLOORBOARD SUPPORT FROM FRAME 31 TO 33 AT STRINGER 34R. - [SDR RYN2004F00002](https://openairdocs.org/sdr/RYN2004F00002.md): Floor Support · corroded · Oct 19, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous Structure > 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 FRAME 34 FROM STRINGER 34R TO 34L IN FORWARD PIT. - [SDR 2004F00242](https://openairdocs.org/sdr/2004F00242.md): Intercostal · corroded · Oct 2, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous Structure > 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 MEASUREABLE MATERIAL LOSS. TREATED, PRIMED AND APPLIED TOPCOAT. (M) - [SDR 2004F00383](https://openairdocs.org/sdr/2004F00383.md): Intercostal · corroded · Oct 2, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous Structure > 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 MATERIAL LOSS. TREATED, PRIMED AND APPLIED TOPCOAT. (M) - [SDR 2004F00181](https://openairdocs.org/sdr/2004F00181.md): Intercostal · corroded · Oct 2, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous Structure > 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 COMPARTMENT BETWEEN FRAME 51 AND FRAME 52, RBL 27. (M) - [SDR 2004F00094](https://openairdocs.org/sdr/2004F00094.md): Floorboard · punctured · Oct 2, 2003 · N951LF · Airbus A320233 · Fuselage Floor Panel > 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.md): Floor Support · corroded · Oct 2, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous Structure > 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 WITHIN LIMITS. TREATED, PRIMED AND TOPCOAT APPLIED. (M) - [SDR 2004F00228](https://openairdocs.org/sdr/2004F00228.md): Intercostal · corroded · Sep 26, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous Structure > 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.md): Mount · damaged · Sep 26, 2003 · N951LF · Airbus A320233 · Engine Mount Section > 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 NOTED. DIMENSIONS CHECKED AND FOUND TO BE WITHIN LIMITS. (M) - [SDR 2004F00068](https://openairdocs.org/sdr/2004F00068.md): Plate · corroded · Sep 26, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous Structure > 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 COMPARTMENT, FRAME 48 TO FRAME 49, LBL 27. (M) - [SDR 2004F00067](https://openairdocs.org/sdr/2004F00067.md): Crossbeam · damaged · Sep 26, 2003 · N951LF · Airbus A320233 · Engine Mount Section > 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 CROSSBEAM BY REMOVING AND REPLACING BUSHING. (M) - [SDR 2004F00066](https://openairdocs.org/sdr/2004F00066.md): Fitting · corroded · Sep 26, 2003 · N951LF · Airbus A320233 · Fuselage Main, Attach Fittings > 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 FITTING AT FRAME 56, LBL 12, IN AFT CARGO PIT. (M) - [SDR 2004F00065](https://openairdocs.org/sdr/2004F00065.md): Fitting · corroded · Sep 26, 2003 · N951LF · Airbus A320233 · Fuselage Main, Attach Fittings > 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 FITTING AT FRAME 56, BL 0 IN AFT CARGO PIT. (M) - [SDR 2004F00064](https://openairdocs.org/sdr/2004F00064.md): Skin · damaged · Sep 26, 2003 · N951LF · Airbus A320233 · Fuselage Main, Plate/Skin > 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 FURTHER EVALUATION OF UPPER FUSELAGE CROWN AREA BETWEEN FRAME 52 AND FRAME 53, STRINGER 1L AND 1R, VHF - [SDR 2004F00063](https://openairdocs.org/sdr/2004F00063.md): Stringer · corroded · Sep 26, 2003 · N951LF · Airbus A320233 · Fuselage Main, Longeron/Stringer > 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 FRAMES 68 AND 69 STATION 3280. (M) - [SDR 2004F00138](https://openairdocs.org/sdr/2004F00138.md): Sill · corroded · Sep 17, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous Structure > 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 FITTING, DRAINS AND ANGLE AT FRAME 67, LEFT LOWER, UNDER SILL. (M) - [SDR 2004F00137](https://openairdocs.org/sdr/2004F00137.md): Floorboard · corroded · Sep 17, 2003 · N951LF · Airbus A320233 · Fuselage Floor Panel > 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.md): Floorboard · corroded · Sep 17, 2003 · N951LF · Airbus A320233 · Fuselage Floor Panel > 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. TREATED AND PRIMED. (M) - [SDR 2004F00123](https://openairdocs.org/sdr/2004F00123.md): Pan · corroded · Sep 17, 2003 · N951LF · Airbus A320233 · Fuselage Floor Panel > 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 LEFT AFT LAVATORY FLOOR PAN ASSEMBLY, ATTACHMENT POINTS FOR BLOW OUT DOOR FRAME. (M) - [SDR 2004F00120](https://openairdocs.org/sdr/2004F00120.md): Floorbeam · corroded · Sep 17, 2003 · N951LF · Airbus A320233 · Fuselage Main, Floor Beam > 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 INCHES INBOARD OF DOOR CUTOUT FROM FRAMES 66 TO 68, RBL 50. (M) - [SDR 23431924](https://openairdocs.org/sdr/23431924.md): Sill · corroded · Sep 17, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous Structure > 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 FITTING, DRAINS AND ANGLE AT FRAME 67, LT LOWER UNDER SILL. (SDR NR 23431924) - [SDR 2004F00139](https://openairdocs.org/sdr/2004F00139.md): Fitting · corroded · Sep 16, 2003 · N951LF · Airbus A320233 · Fuselage Main, Attach Fittings > 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 REPLACED. (M) - [SDR 2004F00134](https://openairdocs.org/sdr/2004F00134.md): Floor Support · corroded · Sep 16, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous Structure > 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 FRAME BETWEEN FRAME 58 AND 59. (M) - [SDR 2004F00133](https://openairdocs.org/sdr/2004F00133.md): Floor Support · damaged · Sep 16, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous Structure > 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 SUPPORT AT FRAME 59 ON RIGHT SIDE. (M) - [SDR 2004F00132](https://openairdocs.org/sdr/2004F00132.md): Seat Track · corroded · Sep 16, 2003 · N951LF · Airbus A320233 · Fuselage, Seat/Cargo Attach Fittings > 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.md): Floorbeam · corroded · Sep 16, 2003 · N951LF · Airbus A320233 · Fuselage Main, Floor Beam > 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.md): Structure · corroded · Sep 15, 2003 · N951LF · Airbus A320233 · Fuselage Main, Structure > 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 FRAME 67 PLUS 13 INCHES TO FRAME 67 AT LBL 45. (M) - [SDR 2004F00112](https://openairdocs.org/sdr/2004F00112.md): Structure · corroded · Sep 15, 2003 · N951LF · Airbus A320233 · Fuselage Main, Structure > 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 STRUCTURE AT FRAME 69 PLUS 3 INCHES TO FRAME 69 PLUS 10 INCHES, LBL 50. (M) - [SDR 2004F00060](https://openairdocs.org/sdr/2004F00060.md): Plate · worn · Sep 15, 2003 · N951LF · Airbus A320233 · Service Doors > 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. (M) - [SDR 2004F00059](https://openairdocs.org/sdr/2004F00059.md): Fitting · gouged · Sep 15, 2003 · N951LF · Airbus A320233 · Emergency Exits > 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 EMERGENCY EXIT DOOR. (M) - [SDR RYN2004F00009](https://openairdocs.org/sdr/RYN2004F00009.md): Attach Fitting · corroded · Sep 15, 2003 · N951LF · Airbus A320233 · Escape Slide > 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 ON AFT CABIN NR 2 RT DOORWAY. - [SDR RYN2004F00008](https://openairdocs.org/sdr/RYN2004F00008.md): Attach Fitting · corroded · Sep 15, 2003 · N951LF · Airbus A320233 · Passenger/Crew Doors > 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 CABIN NR 2 RT DOORWAY. - [SDR RYN2004F00006](https://openairdocs.org/sdr/RYN2004F00006.md): Latch · damaged · Sep 15, 2003 · N951LF · Airbus A320233 · Emergency Exits > 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 FITTING. - [SDR 2004F00227](https://openairdocs.org/sdr/2004F00227.md): Floor Support · bent · Sep 13, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous Structure > 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.md): Pan · corroded · Sep 12, 2003 · N951LF · Airbus A320233 · Fuselage Floor Panel > 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 LEFT AFT LAVATORY FLOOR PAN ASSEMBLY, ATTACHMENT POINTS FOR BLOW OUT DOOR FRAME. (M) - [SDR 2004F00116](https://openairdocs.org/sdr/2004F00116.md): Floor Panel · corroded · Sep 12, 2003 · N951LF · Airbus A320233 · Fuselage Floor Panel > 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.md): Floor Panel · corroded · Sep 12, 2003 · N951LF · Airbus A320233 · Fuselage Floor Panel > 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.md): Floor Panel · corroded · Sep 12, 2003 · N951LF · Airbus A320233 · Fuselage Floor Panel > 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 NR 151BF. (M) - [SDR RYN2004F00007](https://openairdocs.org/sdr/RYN2004F00007.md): Floor Panel · corroded · Sep 12, 2003 · N951LF · Airbus A320233 · Fuselage Floor Panel > 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, CORROSION AT ATTACHMENT POINTS FOR BLOW OUT DOOR FRAME. REMOVED AND REPLACED INSERTS. - [SDR 2004F00114](https://openairdocs.org/sdr/2004F00114.md): Floor Panel · corroded · Sep 11, 2003 · N951LF · Airbus A320233 · Fuselage Floor Panel > 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.md): Floor Support · corroded · Sep 10, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous Structure > 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 STRINGER 38L. (M) - [SDR 2004F00131](https://openairdocs.org/sdr/2004F00131.md): Floor Support · corroded · Sep 10, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous Structure > AT C-CHECK, FOUND FLOORBOARD SUPPORT CORRODED AT FRAME 58 BETWEEN STRINGER 38R AND 40R IN AFT LOWER CARGO COMPARTMENT. REMOVED FLOORBOARD SUPPORT, FABRICATED AND INSTALLED NEW FLOORBOARD SUPPORT AT FRAME 58 BETWEEN STRINGER 38R AND 40R. (M) - [SDR 2004F00130](https://openairdocs.org/sdr/2004F00130.md): Floor Support · corroded · Sep 10, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous Structure > 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 AT FRAME 59 ABOVE STRINGER 40L. (M) - [SDR 2004F00129](https://openairdocs.org/sdr/2004F00129.md): Floor Support · corroded · Sep 10, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous Structure > 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 FLOORBOARD SUPPORT BETWEEN FRAME 60 AND 61 ABOVE STRINGER 43L. (M) - [SDR 2004F00128](https://openairdocs.org/sdr/2004F00128.md): Floor Support · corroded · Sep 10, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous Structure > 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 SUPPORT BETWEEN FRAME 58 AND 59 ABOVE STRINGER 38R. (M) Next page: https://openairdocs.org/deregistered/N951LF-2014-03-19/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N951LF' AND deregistration_id = 'N951LF-2014-03-19' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N951LF-2014-03-19/reports --- 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.