# Service difficulty reports: N248US, cancelled Dec 18, 2003 A list on [N248US, cancelled Dec 18, 2003](https://openairdocs.org/deregistered/N248US-2003-12-18.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 3 · 120 reports - [SDR USAASB01216](https://openairdocs.org/sdr/USAASB01216.md): Battery · discharged · Jul 30, 2001 · N248US · Boeing 737201 · Emergency Lighting > BWI - THE EMERGENCY EXIT SIGN AT SEAT ROW 10 WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY SUPPLY ASSEMBLY. (M) - [SDR USAASB0108](https://openairdocs.org/sdr/USAASB0108.md): Connector · damaged · Mar 18, 2001 · N248US · Boeing 737201 · Flight Control System > LGA-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 CON - [SDR USAASB01080](https://openairdocs.org/sdr/USAASB01080.md): Control Column · seized · Mar 18, 2001 · N248US · Boeing 737201 · Control Column Section > LGA-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) - [SDR USAASB01051](https://openairdocs.org/sdr/USAASB01051.md): Duct · failed · Feb 20, 2001 · N248US · Boeing 737201 · Engine Anti-Icing System > BWI - 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 LANDING - [SDR USAASB00366](https://openairdocs.org/sdr/USAASB00366.md): Duct · cracked · Dec 31, 2000 · N248US · Boeing 737201 · Air Distribution System > BWI - 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 IN - [SDR USAASB00365](https://openairdocs.org/sdr/USAASB00365.md): Battery Pack · discharged · Dec 30, 2000 · N248US · Boeing 737201 · Emergency Lighting > BWI - 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) - [SDR USAA001962](https://openairdocs.org/sdr/USAA001962.md): Skin · cracked · Nov 17, 2000 · N248US · Boeing 737201 · Leading Edge Devices > CRACKS NR 5 SLAT INBD TRACK IN SLAT LWR SKIN AT SPAR. INSTALLED DOUBLER PER EA 68377 - [SDR USAA001961](https://openairdocs.org/sdr/USAA001961.md): Frame · cracked · Nov 17, 2000 · N248US · Boeing 737201 · Fuselage Main, Frame > CRACK STA 663 BULKHD UPPER CHORD RBL 25, WBL 201.5. INSTALLED NEW CHORD SEGMENT & SPLICE ANGLES PER EA 68487 - [SDR USAA001972](https://openairdocs.org/sdr/USAA001972.md): Floorbeam · cracked · Nov 17, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor Beam > FLOORBEAM CRACKED. INSTALLED DOUBLER AND RADIUS BLOCKS INSTALLED PER EA68253 - [SDR USAA001971](https://openairdocs.org/sdr/USAA001971.md): Floorbeam · cracked · Nov 17, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor Beam > FLOORBEAM CRACKED. DOUBLER INSTALLED PER EA68253 - [SDR USAA001970](https://openairdocs.org/sdr/USAA001970.md): Seat Track · cracked · Nov 17, 2000 · N248US · Boeing 737201 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK CRACKED. INSTALLED SEAT TRACK AND FLOOR SUPPORTS - [SDR USAA0001969](https://openairdocs.org/sdr/USAA0001969.md): Stringer Clip · cracked · Nov 17, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous Structure > TEXTDRACKCORRECTIVE ACTION: DEFECTIVE PART REPLACED WITH IDENT. PART # - [SDR USAA001968](https://openairdocs.org/sdr/USAA001968.md): Frame · cracked · Nov 17, 2000 · N248US · Boeing 737201 · Fuselage Main, Frame > FRAME CRACKED. CORRECTIVE ACTION: INSTALLED REPAIR ANGLE PER SRM 51-40-3 - [SDR USAA001967](https://openairdocs.org/sdr/USAA001967.md): Fastener · cracked · Nov 17, 2000 · N248US · Boeing 737201 · Fuselage Main, Structure > FASTENER CRACKED. CORRECTIVE ACTION:DEFECTIVE PART REPLACED WITH IDENT PART. - [SDR USAA001966](https://openairdocs.org/sdr/USAA001966.md): Floorbeam · cracked · Nov 17, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor Beam > FLOORBEAM CRACKED. STOP DRILLED CRACK, HFEC VERIFIED CRACK REMOVED, INSTALLED REPAIR DBLRS PER EA 68328 - [SDR USAA001965](https://openairdocs.org/sdr/USAA001965.md): Stringer Clip · cracked · Nov 17, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous Structure > STRINGER CLIP IS CRACKED. DEFECTIVE PART REPLACED WITH IDENT. PART - [SDR USAA001964](https://openairdocs.org/sdr/USAA001964.md): Stringer Clip · cracked · Nov 17, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous Structure > STINGER CLIP IS CRACKED. DRILLED IDENTICAL REPLACEMENT PART & INSTALLED PER EO 53936227 - [SDR USAA001963](https://openairdocs.org/sdr/USAA001963.md): Stringer Clip · cracked · Nov 17, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous Structure > STRINGER CLIP IS CRACKED. DEFECTIVE PART REPLACED WITH PART 693535214 - [SDR USAA001956](https://openairdocs.org/sdr/USAA001956.md): Skin · cracked · Nov 15, 2000 · N248US · Boeing 737201 · Fuselage Main, Plate/Skin > CRACK FUSELAGE SKIN STA 727A FWD SIDE STR 16R. CORRECTIVE ACTION: INSTALLED DOUBLER PER SRM 53-30-3 - [SDR USAA001957](https://openairdocs.org/sdr/USAA001957.md): Skin · cracked · Nov 15, 2000 · N248US · Boeing 737201 · Fuselage Main, Plate/Skin > CRACK FUSELAGE SKIN STA 727A FWD SIDE STR 16L. CORRECTIVE ACTION: INSTALLED DOUBLER PER SRM 53-30-3 - [SDR USAA001924](https://openairdocs.org/sdr/USAA001924.md): Keelbeam · corroded · Nov 13, 2000 · N248US · Boeing 737201 · Fuselage Main, Keel > CLT - 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) - [SDR USAA001923](https://openairdocs.org/sdr/USAA001923.md): Frame · corroded · Nov 13, 2000 · N248US · Boeing 737201 · Fuselage Main, Frame > CLT - 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) - [SDR USAA001922](https://openairdocs.org/sdr/USAA001922.md): Bulkhead · cracked · Nov 13, 2000 · N248US · Boeing 737201 · Fuselage Main, Bulkhead > CLT - FOUND BULKHEAD WEB CRACKED.125, BS 1016 BETWEEN STRINGER 5L AND 6L. INSTALLED REPAIR DOUBLER PER SRM 53-10-4 FIG 15. (M) - [SDR USAA001921](https://openairdocs.org/sdr/USAA001921.md): Crossbeam · cracked · Nov 13, 2000 · N248US · Boeing 737201 · Cargo/Baggage Doors > CLT - FOUND BEAM CRACKED 2 INCHES, LOWER CROSS BEAM OF FORWARD CARGO DOOR. INSTALLED DOUBLER PER EA 68360. (M) - [SDR USAA001916](https://openairdocs.org/sdr/USAA001916.md): Seat Track · cracked · Nov 9, 2000 · N248US · Boeing 737201 · Fuselage, Seat/Cargo Attach Fittings > CLT - 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) - [SDR USAA001915](https://openairdocs.org/sdr/USAA001915.md): Fitting · cracked · Nov 9, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - FOUND FITTING CRACKED.5 INCH, STATION 331.1 AFT SIDE STRINGER 8R. REMOVED AND INSTALLED PER SRM 51-10-01. (M) - [SDR USAA001914](https://openairdocs.org/sdr/USAA001914.md): Frame · cracked · Nov 9, 2000 · N248US · Boeing 737201 · Fuselage Main, Frame > CLT - FOUND FRAME CRACKED.5 INCH, FORWARD FRAME OF FORWARD SERVICE DOOR STATION 328. INSTALLED DOUBLER PER SRM 51-40-2. (M) - [SDR USAA001913](https://openairdocs.org/sdr/USAA001913.md): Attach Angle · cracked · Nov 9, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - FOUND ATTACH ANGLE CRACKED.25 INCH, STATION 290, STRINGER 10R. REPLACED PER SRM 51-30-0 AND 51-10-1. (M) - [SDR USAA001912](https://openairdocs.org/sdr/USAA001912.md): Stringer · cracked · Nov 9, 2000 · N248US · Boeing 737201 · Fuselage Main, Longeron/Stringer > CLT - FOUND STRINGER CRACKED 1 INCH, STATION 270, STRINGER 14R. FABRICATED NEW INTERCOSTAL PER SRM 53-10-2 FIG 1. (M) - [SDR USAA001911](https://openairdocs.org/sdr/USAA001911.md): Floorbeam · cracked · Nov 9, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor Beam > CLT - 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) - [SDR USAA001908](https://openairdocs.org/sdr/USAA001908.md): Floorbeam · cracked · Nov 8, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor Beam > CLT - FOUND FLOORBEAM CRACKED 1 INCH, BS 669, RBL 24 LONGITUDINAL UPPER CHORD. REPAIRED DOUBLER AND U-CHANNEL PER EA 68275. (M) - [SDR USAA001907](https://openairdocs.org/sdr/USAA001907.md): Floorbeam · cracked · Nov 8, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor Beam > CLT - FOUND FLOORBEAM CRACKED 1 INCH, BS 665, RBL 24 UPPER CHORD. REPAIRED DOUBLER AND U-CHANNEL PER EA 68275. (M) - [SDR USAA001906](https://openairdocs.org/sdr/USAA001906.md): Floorbeam · cracked · Nov 8, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor Beam > CLT - FOUND FLOORBEAM CRACKED.5 INCH, BS 663, RBL 24 UPPER CHORD. REPAIRED DOUBLERS AND U-CHANNEL PER EA 68275. (M) - [SDR USAA001905](https://openairdocs.org/sdr/USAA001905.md): Floorbeam · corroded · Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor Beam > CLT - FOUND FLOORBEAM CORRODED.5 INCH, 360 AND RBBL 53. INSTALLED REPAIR DOUBLER PER EA 68400. (M) - [SDR USAA001904](https://openairdocs.org/sdr/USAA001904.md): Floorbeam · corroded · Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor Beam > CLT - 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) - [SDR USAA001903](https://openairdocs.org/sdr/USAA001903.md): Angle · corroded · Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA001901](https://openairdocs.org/sdr/USAA001901.md): Frame · cracked · Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Main, Frame > CLT - FOUND FRAME CRACKED 1 INCH BY 3 INCHES, STATION 767 FRAME BL 0. FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 51-40-3. (M) - [SDR USAA001900](https://openairdocs.org/sdr/USAA001900.md): Frame · cracked · Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Main, Frame > CLT - FOUND FRAME CRACKED.5 INCH, STATION 500 AND STRINGER 21L. FABRICATED AND INSTALLED DOUBLER PER SRM 53-10-4. (M) - [SDR USAA001899](https://openairdocs.org/sdr/USAA001899.md): Floorbeam · cracked · Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor Beam > CLT - 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) - [SDR USAA001898](https://openairdocs.org/sdr/USAA001898.md): Floorbeam · cracked · Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor Beam > CLT - FOUND FLOORBEAM CRACKED.25 INCH, LBL 25 LONGITUDINAL WEB STATION 706 TO 710, WL 203. INSTALLED WEB REPAIR PER EA 68300. (M) - [SDR USAA001897](https://openairdocs.org/sdr/USAA001897.md): Beam · cracked · Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Main, Structure > CLT - 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) - [SDR USAA001896](https://openairdocs.org/sdr/USAA001896.md): Floorbeam · cracked · Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor Beam > CLT - FOUND FLOORBEAM CRACKED 1.5 INCHES, LBL 24 LONGITUDINAL AT AILERON QUADRANT STATION 677. INSTALLED DOUBLER AND U-CHANNEL PER EO 5791G632. (M) - [SDR USAA001895](https://openairdocs.org/sdr/USAA001895.md): Angle · cracked · Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA001894](https://openairdocs.org/sdr/USAA001894.md): Floorbeam · cracked · Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Main, Floor Beam > CLT - FOUND FLOORBEAM CRACKED 1.5 INCH, RBL 24 LONGITUDINAL FLOORBEAM STATION 677, WL 206. INSTALLED DOUBLER AND U-CHANNEL PER EA 68275. (M) - [SDR USAA001893](https://openairdocs.org/sdr/USAA001893.md): Skin · cracked · Nov 7, 2000 · N248US · Boeing 737201 · Fuselage Main, Plate/Skin > CLT - FOUND SKIN CRACKED.5 INCH, STATION 322, FORWARD ENTRY DOOR SILL. EXTERIOR. INSTALLED REPAIR STRAP AND DOUBLER PER EA 68364. (M) - [SDR USAA001876](https://openairdocs.org/sdr/USAA001876.md): Stringer · cracked · Nov 3, 2000 · N248US · Boeing 737201 · Fuselage Main, Longeron/Stringer > CLT - FOUND SHELF 18A CRACKED.5 INCH, LEFT MOST INBOARD HOLE. INSTALLED NEW PART PER SRM 51-30-1. (M) - [SDR USAA001871](https://openairdocs.org/sdr/USAA001871.md): Web · cracked · Nov 2, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - FOUND WEB CRACKED.75 INCH, BS 178, WL 213, LBL 5. INSTALLED DOUBLER PER SRM 53-10-11 AND EA 68167. (M) - [SDR USAA001870](https://openairdocs.org/sdr/USAA001870.md): Web · cracked · Nov 2, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - FOUND WEB CRACKED 2 INCHES, BS 178 LBL 5, WL 201/197. INSTALLED DOUBLER PER SRM 53-10-11. (M) - [SDR USAA001869](https://openairdocs.org/sdr/USAA001869.md): Web · cracked · Nov 2, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA001868](https://openairdocs.org/sdr/USAA001868.md): Web · cracked · Nov 2, 2000 · N248US · Boeing 737201 · Fuselage Miscellaneous Structure > CLT - FOUND WEB CRACKED.5 INCH, BS 178, LBL 5, WL 190, 193, 194. INSTALLED DOUBLER PER EA 68167 AND SRM 53-10-11. (M) Next page: https://openairdocs.org/deregistered/N248US-2003-12-18/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 = 'N248US' AND deregistration_id = 'N248US-2003-12-18' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N248US-2003-12-18/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.