N243US, cancelled Sep 13, 2004

Service difficulty reports · 100

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 = 'N243US' AND deregistration_id = 'N243US-2004-09-13'
  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 USAA010751Bulkhead · crackedCLT - FOUND BULKHEAD WEB WITH NUMEROUS CRACKS RANGING FROM .125 INCH TO .75 INCH, BS 178 WL 207 TO 234, LBL 12.6 TO RBL 11.7. DAMAGE REMOVED, REPAIR DOUBLER INSTALLED PER EO 5300V153, EA 69807 AND 69774. (M)Jun 16, 2001 · N243US · Boeing 737201 · Fuselage Main, BulkheadSDR USAA010752Frame · crackedCLT - FOUND VERTICAL CHORD WITH TWO CRACKS EACH 1 INCH LONG, BS 178 WL 181 AT RBL 5.7 AND WL 184 AT LBL 5.7. DAMAGE REMOVED, INSTALLED REPAIR ANGLES ADN STRAPS PER EO 5300V155. (M)Jun 16, 2001 · N243US · Boeing 737201 · Fuselage Main, FrameSDR USAA010753Frame · crackedCLT - FOUND SIDE CHORDS WITH TWO CRACKS .25 INCH AT RBL 26, 1 INCH AT LBL 24, BS 178 WL 195 AT LBL 24 AND WL 207 AT RBL 26. DAMAGED SECTION REMOVED, INSTALLED CHORD SPLICE REPAIR PER EO 5300V157. (M)Jun 16, 2001 · N243US · Boeing 737201 · Fuselage Main, FrameSDR USAASB01086Duct · failedPBI - FLT 2990 - EN ROUTE FROM LGA TO PBI, APPROXIMATELY ONE HOUR INTO FLIGHT, THE FLIGHT ATTENDANT ADVISED THE CREW OF AN ELECTRICAL SMELL IN MID-CABIN. CREW COOLED DOWN CABIN AND SMELL DISSIPATED. FLIGHT ATTENDANT ADVISDED THAT ONLY A FAINT ODOR REMAINED. Mar 23, 2001 · N243US · Boeing 737201 · Air Distribution SystemSDR USAASB01085Bleed Valve · faultyLGA - FLT 2721 - ON TAKEOFF FROM LGA, EN ROUTE TO FLL, THE AUTO THROTTLE DISENGAGED AND THE NR 1 ENGINE EPR PULLED BACK TO 1.88. THERE WAS NO RESPONSE TO THROTTLE MOVEMENT. CONDITIONS WERE A BLEEDS-OFF NON-PRESSURIZED TAKEOFF. THEN ON CLIMB-OUT, AFTER BLEEDMar 22, 2001 · N243US · Boeing 737201 · Compressor Bleed ValveSDR USAASB00351Engine · failedFLL - FLT 2828 - ON CLIMB-OUT FROM FLL, EN ROUTE TO BOS, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL AND HIGH EGT. CAPTAIN SHUTDOWN THE NR 2 ENGINE, DECLARED AN EMERGENCY AND ADVISED THE FLIGHT ATTENDANTS THEY WERE RETURNING TO FIELD AT FLL. CAPTAIN FIRED Dec 18, 2000 · N243US · Boeing 737201 · Engine (Turbine/Turboprop)SDR USAA002076Stringer · corrodedTPA - FOUND STRINGER CORRODED 2 INCHES BY 3 INCHES, STATION 965, STRINGER 27R. CORROSION LEVEL 2. SPLICED IN SECTION PER SRM 53-10-3 PAGE 4 FIG 1. (M)Dec 6, 2000 · N243US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAASB00270Gyro · faultyBWI - FLT 2821 - ON CLIMB-OUT FROM BWI, THE HEADING COMPARATOR LIGHT ILLUMINATED. CAPTAINS AND FIRST OFFICERS COMPASS SYSTEM SPLIT 30 DEGREES APART AND REMAINED THAT WAY FOR 10 MINUTES. CAPTAINS ADVISED BWI THAT HE WAS RETURNING TO FIELD. JUST PRIOR TO LANDSep 22, 2000 · N243US · Boeing 737201 · Directional Gyro and Indicating SystemSDR USAASB00214Handle · failedBOS - FLT 2602 - CAPTAIN REPORTED THAT AFTER TAKEOFF, THE LANDING GEAR HANDLE WOULD NOT MOVE PAST THE OFF POSITION TO RETRACT THE LANDING GEAR. CREW ACCOMPLISHED ABNORMAL PROCEDURES AND RETURNED TO FIELD AT BOS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMAug 10, 2000 · N243US · Boeing 737201 · Landing Gear SelectorSDR USAA000188Frame · crackedCLT - FOUND 1 INCH CRACK, STATION 727 STRINGER 24R CHORD ANGLE. INSTALLED NEW CHORD AND DOUBLER PER EA 66451 AND SRM 51-40-2. (M)Feb 11, 2000 · N243US · Boeing 737201 · Fuselage Main, FrameSDR USAA000137Floorbeam · corrodedCLT - Q-1, BS 1016 LT LENGTH OF FLOORBEAM HAS CORROSION LEVEL 1. REPLACED WEB, T-CAP PER TR 53-60-02 AND SRM 51-40-02. (M)Feb 3, 2000 · N243US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000136Seat Track · corrodedCLT - Q-1, FOUND CORROSION AT RBL 39 STATION 1000 TO 1014 FLOOR SEAT TRACK 1 INCH BY 14 INCH CORROSION LEVEL 1. INSTALLED NEW SEAT TRACK PER SRM 51-10-2 AND 51-30-03. (M)Feb 3, 2000 · N243US · Boeing 737201 · Fuselage, Seat/Cargo Attach FittingsSDR USAA000135Skin · crackedCLT - Q-1, FOUND .25 INCH CRACK, LOWER FORWARD CORNER AFT ENTRY DOOR CUTOUT. REPLACED PARTS PER SRM 53-30-3 FIG 24. (M)Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000134Fitting · crackedCLT - Q-1, FOUND .5 INCH CRACK, LOWER DOOR STOP FITTING. REPLACED FITTING PER DRAWING 6517685. (M)Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000133Tie Clip · crackedCLT - Q,1, FOUND .1 INCH CRACK STATION 578, STRINGER 7R TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-1 AND EO 5393G227. (M)Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000132Strap · crackedCLT - Q-1, FOUND 1 INCH CRACK, STRINGER 5A JUST AFT STATION 1138. INSTALLED REPAIR DOUBLER PER EA66501 AND SRM 53-00-1. (M)Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000131Tie Clip · crackedCLT - Q-1, STRINGER 17 TIE CLIP AT STATION 1138, HAS 1 INCH CRACK. REPLACED TIE CLIP PER SRM 51-10-1. (M)Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000130Tie Clip · crackedCLT - Q-1, STRINGER 161 TIE CLIP AT STATION 1138, HAS A .75 INCH CRACK. REPLACED TIE CLIP PER SRM 51-40-1. (M)Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000129Shear Tie · crackedCLT - Q-1, STATION 1104 STRINGER 161 INBOARD SIDE FRAME SHEAR TIE HAS A .5 INCH CRACK. INSTALLED SHEAR TIE PER SRM 51-10-1. (M)Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000128Tie Clip · crackedCLT - Q-1, STRINGER 21 AT FRAME 616 TIE CLIP HAS A .5 INCH CRACK. REPLACED TIE CLIP PER EO5393G227 PART 3. (M)Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000127Floorbeam · crackedCLT - Q-1, STATION 707, LBL 25, WL 202.5 FLOORBEAM WEB HAS A 1.5 INCH CRACK. REPLACED PARTS PER SRM 51-40-2. (M)Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000126Frame · crackedCLT - Q-1, STATION 663 BULKHEAD UPPER FRAME RBL 23, WL 201.5 HAS A .5 INCH CRACK. REPLACED VERTICAL ANGLES AND CHORD PER BOEING 65C37732. (M)Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Main, FrameSDR USAA000125Crease Beam · crackedCLT - Q-1, STRINGER 17R CREASE BEAM 8 INCH AFT STATION 639 FRAME CREASE BEAM WEB HAS A .375 INCH CRACK AT WL 208. REPLACED WEB PER SRM 51-10-02. (M)Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000124Shear Tie · crackedCLT - Q-1, STATION 520 FORWARD CARGO PIT BULKHEAD STRINGER 24R SHEAR TIE HAS A .375 INCH CRACK. INSTALLED CLIP PER SRM 51-10-02 AND BOEING 6551298. (M)Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000123Crease Beam · crackedCLT - Q-1, FOUND STRINGER 17R STATION 639 FRAME WL 208 CREASE BEAM WEB HAS A 1 INCH CRACK. REPLACED WEB AND ANGLE PER SRM 51-10-01 AND 51-40-04. (M)Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000122Tie Clip · crackedCLT - Q-1, STATION 597 STRINGER 8R TIE CLIP HAS A .1 INCH CRACK. REPLACED STRINGER CLIP PER EO5393G227 PART 3. (M)Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000121Frame · crackedCLT - Q-1, STRINGER 15R AT SKIN FASTENER FORWARD STATION 540 FRAME HAS A .25 INCH CRACK. INSTALLED REPAIR SPLICE PER EA66436 AND SRM 53-10-3 FIG 1. (M)Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Main, FrameSDR USAA000120Frame · crackedCLT - Q-1, STATION 726, S18AL AT L/B CHORD FRAME HAS A .5 INCH CRACK. REPLACED SHELF PER EO5393G256 AND SRM 51-10-9. (M)Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Main, FrameSDR USAA000114Angle · crackedCLT - Q-1, BS 178, LBL 5, WL 184 ANGLE HAS A 1.5 INCH CRACK. INSTALLED REPAIR ANGLE AND STRAP PER EA 66497. (M)Jan 27, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000113Beam · crackedCLT - Q-1, STATION 178, LBL 5.25, WL 188 BEAM HAS A 1 INCH CRACK. INSTALLED REPAIR ANGLE AND FILLER PER EA 66497. (M)Jan 27, 2000 · N243US · Boeing 737201 · Fuselage Main, StructureSDR USAA000092Stringer · crackedCLT - Q-1 - BS 533.5 AND 532.5, STR 151, STRINGER HAS 2 EACH .25 INCH CRACKS. SPLICED NEW STRINGER PER EACH 66436 AND SRM 53-10-3 FIG 1. (X)Jan 26, 2000 · N243US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA000090Bulkhead · crackedCLT - Q-1 - STA 727, LBL 23, WL 202, BULKHEAD HAS A .50 INCH CRACK. INSTALLED REPAIR DOUBLER PER TR 53-10-03. (X)Jan 26, 2000 · N243US · Boeing 737201 · Fuselage Main, BulkheadSDR USAA000089Bulkhead · crackedCLT - Q-1 - STA 727, RBL 23, WL 202. BULKHEAD HAS A .50 INCH CRACK. INSTALLED REPAIR DOUBLER PER TR 53-10-03. (X)Jan 26, 2000 · N243US · Boeing 737201 · Fuselage Main, BulkheadSDR USAA000088Beam · corrodedCLT - Q-1 - BS236, RBL 6, WL189, TRANSVERSE BEAM HAS 1 INCH BY .50 INCH OF CORROSION. REPAIRED PER SRM 51-10-1. (X)Jan 26, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000068Angle · crackedANGLE CRACKED AT BS 727, RT BUTTLINE 1 WATERLINE 202. INSTALLED REPAIR ANGLE PER TR 53-10-03 A. (M)Jan 19, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000049Web · crackedWEB CRACKED AT BS 350, STRINGER 15 LT. INSTALLED NEW WEB SKIN PER SRM 51-10-01. (M)Jan 18, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000048Bulkhead · crackedBULKHEAD CRACKED AT BS 663, LT BUTTLINE 23, WATERLINE 201.5. INSTALLED SPLICE ANGLE PER TR 57-10-03. (M)Jan 18, 2000 · N243US · Boeing 737201 · Fuselage Main, BulkheadSDR USAA000047Floorbeam · corrodedFLOORBEAM CORRODED AT BS 986, RT BUTTLINE 47, LT BUTTLINE 12. INSTALLED NEW T-CAP PER TR 53-60-1 AND EA 66459. (M)Jan 18, 2000 · N243US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000034Splice · corrodedSPLICE CORRODED AT BS 359, STRINGER 27L. REPLACED STRINGER SPLICE PER SRM 53-10-3. (M)Jan 14, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000031Web · crackedWEB FOUND CRACKED AT BS 578, LBL 58, 59, 60, 60.5, WL 205.5. INSTALLED DOUBLER PER SRM 51-40-2. (M)Jan 13, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000030Frame · crackedFOUND FRAME CRACKED AT BS 400, STRINGER 25L. INSTALLED DOUBLER PER SRM 51-40-3. (M)Jan 13, 2000 · N243US · Boeing 737201 · Fuselage Main, FrameSDR USAA000029Stringer · crackedFOUND STRINGER 15 RIGHT CRACKED AT BBS 533.5.. REPAIRED PER EA 66436 AND SRM 53-10-3 FIG 1. (M)Jan 13, 2000 · N243US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA000028Web · crackedFOUND WEB CRACKED AT BS 639, WL 208, RBL 63. REPLACED WEBPER SRM 51-10-1. (M)Jan 13, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000027Intercostal · crackedINTERCOSTAL FOUND CRACKED AT BS 278, STRINGER 14R. REPLACED PART PER SRM 51-10-1. (M)Jan 13, 2000 · N243US · Boeing 737201 · Fuselage Main, StructureSDR USAA000026Angle · crackedFOUND ANGLE CRACKED AT BS 350, WL 216, RBL 65. REPAIRED PER SRM 51-30-2. (M)Jan 13, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000025Fitting · crackedFOUND FITTING CRACKED AT BS 348.2, WL 216, RBL 61. REPAIRED PER SRM 51-30-2. (M)Jan 13, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000024Web · crackedWEB FOUND CRACKED AT BS 350, LBL 61, WL 216. REPAIRED PERSRM 51-30-2. (M)Jan 13, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000023Angle · crackedFOUND ANGLE CRACKED AT BS 727, WL 202, RBL 8..5. REPAIREDPER SRM 51-30-2. (M)Jan 13, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000022Bulkhead · crackedFOUND BULKHEAD CRACKED. INSTALLED REPAIR KIT PER DWG 65C37732. (M)Jan 13, 2000 · N243US · Boeing 737201 · Fuselage Main, BulkheadSDR USAA991480Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FUOND A .125 INCH CRACK FORWARD SERVICE DOOR FORWARD CUTOUT STUB FRAME BETWEEN STRINGER 11R AND 12R OUTBOARD CHORD ANGLE STATION 290. REMOVED AND REPLACED ANGLE PER REPAIR DOCUMENT 51-10-01. (M)Jan 12, 2000 · N243US · Boeing 737201 · Fuselage Main, Frame
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