N248US, cancelled Dec 18, 2003

Service difficulty reports · 120

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

Query with SQL
duckdb -csv -c "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 = 'N248US' AND deregistration_id = 'N248US-2003-12-18'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR USAASB01216Battery · dischargedBWI - THE EMERGENCY EXIT SIGN AT SEAT ROW 10 WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY SUPPLY ASSEMBLY. (M)Jul 30, 2001 · N248US · Boeing 737201 · Emergency LightingSDR USAASB0108Connector · damagedLGA-PBI - FLT 2693 - DURING A DESCENDING TURN THE CONTROL COLUMN SEIZED. NEITHER THE CAPT NOR THE F O COULD MOVE THE CONTROL COLUMN FOR SEVERAL SECONDS. AFTER A GO-AROUND THE AIRCRAFT LANDED W/O INCIDENT. MX REPLACED THE A/B AILERON PCUS, AUTOPILOT MODE CONMar 18, 2001 · N248US · Boeing 737201 · Flight Control SystemSDR USAASB01080Control Column · seizedLGA-PBI - FLT 2693 - DURING A DESCENDING TURN THE CONTROL COLUMN SEIZED. NEITHER THE CAPTAIN NOR THE FIRST OFFICER COULD MOVE THE CONTROL COLUMN FOR SEVERAL SECONDS. AFTER A GO-AROUND THE AIRCRAFT LANDED WITHOUT INCIDENT. (M)Mar 18, 2001 · N248US · Boeing 737201 · Control Column SectionSDR USAASB01051Duct · failedBWI - FLT 2639 - ON CLIMB-OUT FROM BWI, AT FL120, THE NR 2 ENG OVERHEAT LIGHT ILLUMINATED. CREW REDUCED POWER ON NR 2 ENG TO IDLE AND LIGHT EXTINGUISHED. CREW DECLARED AN EMERG AND RETURNED TO FIELD AT BWI. FLT LANDED W/O FURTHER INCIDENT. PRIOR TO LANDINGFeb 20, 2001 · N248US · Boeing 737201 · Engine Anti-Icing SystemSDR USAASB00366Duct · crackedBWI - FLT 2631 - EN ROUTE FROM FLL TO LGA, THE RIGHT WING-TO-BODY OVERHEAT LIGHT ILLUMINATED. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND CONTINUED FLIGHT ON ONE PACK, WHEREAS LIGHT EXTINGUISHED. FLIGHT DIVERTED TO BWI AND LANDED WITHOUT FURTHER INDec 31, 2000 · N248US · Boeing 737201 · Air Distribution SystemSDR USAASB00365Battery Pack · dischargedBWI - MAINTENANCE FOUND THE FORWARD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT THE FORWARD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT. OPERATIONAL CHECK GOOD. (M)Dec 30, 2000 · N248US · Boeing 737201 · Emergency LightingSDR USAA001962Skin · crackedCRACKS NR 5 SLAT INBD TRACK IN SLAT LWR SKIN AT SPAR. INSTALLED DOUBLER PER EA 68377Nov 17, 2000 · N248US · Boeing 737201 · Leading Edge DevicesSDR USAA001961Frame · crackedCRACK STA 663 BULKHD UPPER CHORD RBL 25, WBL 201.5. INSTALLED NEW CHORD SEGMENT & SPLICE ANGLES PER EA 68487Nov 17, 2000 · N248US · Boeing 737201 · Fuselage Main, FrameSDR USAA001972Floorbeam · crackedFLOORBEAM CRACKED. INSTALLED DOUBLER AND RADIUS BLOCKS INSTALLED PER EA68253Nov 17, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001971Floorbeam · crackedFLOORBEAM CRACKED. DOUBLER INSTALLED PER EA68253Nov 17, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001970Seat Track · crackedSEAT TRACK CRACKED. INSTALLED SEAT TRACK AND FLOOR SUPPORTSNov 17, 2000 · N248US · Boeing 737201 · Fuselage, Seat/Cargo Attach FittingsSDR USAA0001969Stringer Clip · crackedTEXTDRACKCORRECTIVE ACTION: DEFECTIVE PART REPLACED WITH IDENT. PART #Nov 17, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001968Frame · crackedFRAME CRACKED. CORRECTIVE ACTION: INSTALLED REPAIR ANGLE PER SRM 51-40-3Nov 17, 2000 · N248US · Boeing 737201 · Fuselage Main, FrameSDR USAA001967Fastener · crackedFASTENER CRACKED. CORRECTIVE ACTION:DEFECTIVE PART REPLACED WITH IDENT PART.Nov 17, 2000 · N248US · Boeing 737201 · Fuselage Main, StructureSDR USAA001966Floorbeam · crackedFLOORBEAM CRACKED. STOP DRILLED CRACK, HFEC VERIFIED CRACK REMOVED, INSTALLED REPAIR DBLRS PER EA 68328Nov 17, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001965Stringer Clip · crackedSTRINGER CLIP IS CRACKED. DEFECTIVE PART REPLACED WITH IDENT. PARTNov 17, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001964Stringer Clip · crackedSTINGER CLIP IS CRACKED. DRILLED IDENTICAL REPLACEMENT PART & INSTALLED PER EO 53936227Nov 17, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001963Stringer Clip · crackedSTRINGER CLIP IS CRACKED. DEFECTIVE PART REPLACED WITH PART 693535214Nov 17, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001956Skin · crackedCRACK FUSELAGE SKIN STA 727A FWD SIDE STR 16R. CORRECTIVE ACTION: INSTALLED DOUBLER PER SRM 53-30-3Nov 15, 2000 · N248US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA001957Skin · crackedCRACK FUSELAGE SKIN STA 727A FWD SIDE STR 16L. CORRECTIVE ACTION: INSTALLED DOUBLER PER SRM 53-30-3Nov 15, 2000 · N248US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA001924Keelbeam · corrodedCLT - FOUND KEEL BEAM ANGLE .750 INCH BY 64 INCHES, LOWER KEEL BEAM RIGHT ANGLE STATION 727 TO 663. INSTALLED REPAIR STRAPS PER TR 53-10-22. (M)Nov 13, 2000 · N248US · Boeing 737201 · Fuselage Main, KeelSDR USAA001923Frame · corrodedCLT - FOUND CHORD CORRODED 5 INCHES, PRESSURE BULKHEAD RIGHT SIDE OF Y CHORD STATION 1016 BL 0. REPAIRED WEB PER EA 68373A AND SRM 51-30-0. (M)Nov 13, 2000 · N248US · Boeing 737201 · Fuselage Main, FrameSDR USAA001922Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED .125, BS 1016 BETWEEN STRINGER 5L AND 6L. INSTALLED REPAIR DOUBLER PER SRM 53-10-4 FIG 15. (M)Nov 13, 2000 · N248US · Boeing 737201 · Fuselage Main, BulkheadSDR USAA001921Crossbeam · crackedCLT - FOUND BEAM CRACKED 2 INCHES, LOWER CROSS BEAM OF FORWARD CARGO DOOR. INSTALLED DOUBLER PER EA 68360. (M)Nov 13, 2000 · N248US · Boeing 737201 · Cargo/Baggage DoorsSDR USAA001916Seat Track · crackedCLT - FOUND SEAT TRACK CRACKED TWO PLACES .25 INCH EACH, FORWARD OF STATION 520, BELOW LBL 45.5 SEAT TRACK. FABRICATED NEW WEB PER SRM 51-10-1. (M)Nov 9, 2000 · N248US · Boeing 737201 · Fuselage, Seat/Cargo Attach FittingsSDR USAA001915Fitting · crackedCLT - FOUND FITTING CRACKED .5 INCH, STATION 331.1 AFT SIDE STRINGER 8R. REMOVED AND INSTALLED PER SRM 51-10-01. (M)Nov 9, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001914Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, FORWARD FRAME OF FORWARD SERVICE DOOR STATION 328. INSTALLED DOUBLER PER SRM 51-40-2. (M)Nov 9, 2000 · N248US · Boeing 737201 · Fuselage Main, FrameSDR USAA001913Attach Angle · crackedCLT - FOUND ATTACH ANGLE CRACKED .25 INCH, STATION 290, STRINGER 10R. REPLACED PER SRM 51-30-0 AND 51-10-1. (M)Nov 9, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001912Stringer · crackedCLT - FOUND STRINGER CRACKED 1 INCH, STATION 270, STRINGER 14R. FABRICATED NEW INTERCOSTAL PER SRM 53-10-2 FIG 1. (M)Nov 9, 2000 · N248US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA001911Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED 4 INCHES, BL 0 LONGITUDINAL UPPER CHORD WEB WL 208, STATION 663. REMOVED DAMAGE INSTALLED DOUBLER PER SRM 51-10-02. (M)Nov 9, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001908Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED 1 INCH, BS 669, RBL 24 LONGITUDINAL UPPER CHORD. REPAIRED DOUBLER AND U-CHANNEL PER EA 68275. (M)Nov 8, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001907Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED 1 INCH, BS 665, RBL 24 UPPER CHORD. REPAIRED DOUBLER AND U-CHANNEL PER EA 68275. (M)Nov 8, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001906Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED .5 INCH, BS 663, RBL 24 UPPER CHORD. REPAIRED DOUBLERS AND U-CHANNEL PER EA 68275. (M)Nov 8, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001905Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .5 INCH, 360 AND RBBL 53. INSTALLED REPAIR DOUBLER PER EA 68400. (M)Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001904Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .5 INCH BY .5 INCH, STATION 986, LBL 30 TO RBL 45. INSTALLED T-CAP TR 53-60-01 REV A. (M)Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001903Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 2 INCHES BY 1.5 INCHES, BS 957-1006. CORROSION LEVEL 1 C53-107-02. REPLACED Z-ANGLE PER SRM 51-10-01. (M)Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001901Frame · crackedCLT - FOUND FRAME CRACKED 1 INCH BY 3 INCHES, STATION 767 FRAME BL 0. FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 51-40-3. (M)Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Main, FrameSDR USAA001900Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 500 AND STRINGER 21L. FABRICATED AND INSTALLED DOUBLER PER SRM 53-10-4. (M)Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Main, FrameSDR USAA001899Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED 1 INCH, BL 0 LONGITUDINAL WEB STATION 706 TO 714, WL 203. INSTALLED REPAIR DOUBLER AND WEB PER EA 68300 AND SRM 53-60-51. (M)Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001898Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED .25 INCH, LBL 25 LONGITUDINAL WEB STATION 706 TO 710, WL 203. INSTALLED WEB REPAIR PER EA 68300. (M)Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001897Beam · crackedCLT - FOUND BEAM CRACKED 3 INCHES, STATION 695 STUB BEAM WEB LBL 62, WL 206. FABRICATED STUB BEAM WEB AND INSTALLED PER SRM 51-10-1. (M)Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Main, StructureSDR USAA001896Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED 1.5 INCHES, LBL 24 LONGITUDINAL AT AILERON QUADRANT STATION 677. INSTALLED DOUBLER AND U-CHANNEL PER EO 5791G632. (M)Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001895Angle · crackedCLT - FOUND FRAME CHORD ANGLE CRACKED .50 INCH, INBOARD CHORD ANGLE OF FRAME AT STATION 639 STRINGER 16L. REMOVED AND REPLACED PER SRM 51-10-1. (M)Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001894Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED 1.5 INCH, RBL 24 LONGITUDINAL FLOORBEAM STATION 677, WL 206. INSTALLED DOUBLER AND U-CHANNEL PER EA 68275. (M)Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001893Skin · crackedCLT - FOUND SKIN CRACKED .5 INCH, STATION 322, FORWARD ENTRY DOOR SILL. EXTERIOR. INSTALLED REPAIR STRAP AND DOUBLER PER EA 68364. (M)Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA001876Stringer · crackedCLT - FOUND SHELF 18A CRACKED .5 INCH, LEFT MOST INBOARD HOLE. INSTALLED NEW PART PER SRM 51-30-1. (M)Nov 3, 2000 · N248US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA001871Web · crackedCLT - FOUND WEB CRACKED .75 INCH, BS 178, WL 213, LBL 5. INSTALLED DOUBLER PER SRM 53-10-11 AND EA 68167. (M)Nov 2, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001870Web · crackedCLT - FOUND WEB CRACKED 2 INCHES, BS 178 LBL 5, WL 201/197. INSTALLED DOUBLER PER SRM 53-10-11. (M)Nov 2, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001869Web · crackedCLT - FOUND WEB CRACKED .5 INCH, BS 178, WL 190, 194, 196 AT RBL 5. INSTALLED DOUBLER PER SRM 53-10-11 AND EA 68167. (M)Nov 2, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001868Web · crackedCLT - FOUND WEB CRACKED .5 INCH, BS 178, LBL 5, WL 190, 193, 194. INSTALLED DOUBLER PER EA 68167 AND SRM 53-10-11. (M)Nov 2, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous Structure
Back to N248US, cancelled Dec 18, 2003