N246US, cancelled Mar 25, 2002

Service difficulty reports · 79

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 = 'N246US' AND deregistration_id = 'N246US-2002-03-25'
  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 USAA010396Skin · crackedTPA - FOUND SKIN CRACKED BS 727A PLUS 1 INCH BELOW STRINGER 17L, BS 727A PLUS 18 INCHES ABOVE STRINGER 18L. REMOVED EXISTING REPAIR, INSTALLED REPAIR DOUBLER AND TRIPLER, SRM 53-30-03 FIG 1. (M)Apr 16, 2001 · N246US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA010394Skin · crackedTPA - FOUND SKIN CRACKED 1.5 INCH, BS 727B PLUS 12 INCHES, STRINGER 17L. INSTALLED REPAIR DOUBLE, SRM 53-30-3, FIG 1. (M)Apr 16, 2001 · N246US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB01098Power Supply · inoperativeCLE - THE AFT SERVICE DOOR AND AFT ENTRY DOOR EMERGENCY EXIT SIGNS AND ENTRY DOOR LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK. (M)Apr 7, 2001 · N246US · Boeing 737201 · Emergency LightingSDR USAA010395Skin · crackedTPA - FOUND SKIN CRACKED 4 INCHES, BS 747 PLUS 3 INCHES, STRINGER 18R. INSTALLED REPAIR DOUBLER, SRM 53-30-3 FIG 1. (M)Apr 1, 2001 · N246US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA010164Skin · crackedBOS - FOUND SKIN CRACKED 2 INCHES, BS 727A STRINGER 15L. INSTALLED DOUBLER PER SRM 53-30-3 PP 2E, FIG 1. (M)Jan 16, 2001 · N246US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB00260Control Unit · failedFLL - FLT 2995 - EN ROUTE FROM LGA-FLL, AT FL310, THE PASSENGERS OXYGEN DROPPED TO ZERO PSI. CREW ACCOMPLISHED PROCEDURES AND DESCENDED TO FL100. BEFORE LANDING, THE PASSENGER OXYGEN PRESSURE RETURNED TO NORMAL. MAINTENANCE REMOVED AND REPLACED THE PASSENGESep 17, 2000 · N246US · Boeing 737201 · Passenger Oxygen SystemSDR USAA000736Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 30 INCHES, STATION 328, LBL 28, AND RBL 20 - RBL 50. T-CAP REPLACEMENT PER SRM 53-10-2. (M)May 24, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000735Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED, 1 INCH BY 8 INCH, BS 259 FLOORBEAM. INSTALLED DOUBLER AND NEW T-CAP PER TR 53-10-16 AND EA 67170. CORROSION LEVEL 2. (M)May 24, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000726Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 344 UPPER CHORD LBL 15 TO LBL 50. REPAIRED T-CAP PER TR 53-10-13. (M)May 23, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000725Fitting · crackedCLT - FOUND .5 INCH CRACK IN FITTING, OUTBOARD SUPPORT FITTING MLG BEAM AT CUTOUT, REMOVED AND REPLACED. (M)May 23, 2000 · N246US · Boeing 737201 · Main Landing Gear Attach SectionSDR USAA000715Fitting · crackedCLT - Q-1, EXPANSION BEAM FITTING CRACKED 1.5 INCHES, BS 520, RBL 25. INSTALLED DOUBLER AND NEW CHANNEL PER EA 67143. (X)May 16, 2000 · N246US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000711Beam · crackedCLT - Q-1, BEAM WEB HAD 2 EACH .75 INCH CRACKS, BL ZERO, STA 706 TO STA 713, WL 203 BEAM WEB. INSTALLED DOUBLER PER EA 67224. (X)May 15, 2000 · N246US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000710Fitting · crackedCLT - Q-1, EXPANSION BEAM FITTING HAD .50 INCH CRACK, STA 520, LBL 25 EXPANSION BEAM FITTING . INSTALLED DOUBLER AND REPAIR ANGLES PER EA 67143. (X)May 15, 2000 · N246US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000704Floorbeam · corrodedCLT - FLOORBEAM HAD LEVEL 2 CORROSION, 3 INCHES BY 15 INCHES, BS 986.5 LBL 14 TO RBL 16. INSTALLED T-CAP PER TR 53-60-1. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000694Beltframe · corrodedCLT - BELT FRAME HAD LEVEL 2 CORROSION, .250 INCH BY .250 INCH, BS 727B, RBL 04. INSTALLED DOUBLER PER SRM 53-10-4. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, StructureSDR USAA000692Floorbeam · corrodedCLT - FLOORBEAM HAD LEVEL 2 CORROSION, 1 INCH BY 1 INCH, BS 986.5 LBL 43. INSTALLED T-CAP PER TR 53-60-01. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000690Floorbeam · corrodedCLT - FLOORBEAM HAD LEVEL 2 CORROSION, 1 INCH BY 6 INCH, AT BS 986.5, RBL 27, RBL 33. INSTALLED T-CAP PER TR 53-60-1. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000688Floorbeam · corrodedCLT - FLOORBEAM HAD LEVEL 2 CORROSION, 1 INCH BY 2 INCH, BS 986.5, RBL 40 TO RBL 42. INSTALLED T-CAP PER TR 53-60-1. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000687Skin · crackedCLT - SKIN CRACKED 2.7 INCHES, STR 19L, STA 726 - STA 765, STR 18L 765-780. REPAIRED FILLER AND DOUBLER PER SRM 53-30-03 FIGURE 17. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000686Floorbeam · crackedCLT - FLOORBEAM CRACKED .50 INCH, UPPER FLANGE STA 520, LBL 45. INSTALLED DOUBLER AND PIVOT LINK PER EA 67143. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000685Attach Angle · crackedCLT - ATTACH ANGLE CRACKED 1.50 INCHES, AT FRAME TO STRINGER ATTACH ANGLE STA 360, STR 20R. INSTALLED DOUBLER PER SRM 51-40-3. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Attach FittingsSDR USAA000684Frame · crackedCLT - FRAME HAD A 4 INCH CRACK AT STA 360, JUST ABOVE STR 20R. INSTALLED DOUBLER PER SRM 51-40-3. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, FrameSDR USAA000683Floorbeam · corrodedCLT- FLOORBEAM HAD LEVEL 1 CORROSION, .250 INCH BY .250 INCH, BS 312, LBL 08 TO RBL 08. INSTALLED NEW T-CAP PER TR 53-10-13. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000682Floorbeam · corrodedCLT- FLOORBEAM HAS LEVEL 1 CORROSION, 1 INCH BY 2 INCH, BS 986.5, RBL 37 TO RBL 45. INSTALLED T-CAP PER TR 53-60-1. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000681Floorbeam · corrodedCLT - FLOORBEAM HAD LEVEL 1 CORROSION, 1 INCH BY 1 INCH, BL 1006, LBL 19. REPAIRED ANGLE, INSTALLED PER EA67218 AND SRM 51-10-6. (X)May 11, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000679Angle · crackedCLT - WEB AND ANGLE HAD 6 EACH CRACKS, 4 EACH AT .50 INCH AND 2 EACH AT .1250 INCH, BL ZERO FROM BS 927 TO BS 947. FABRICATED AND INSTALLED NEW ANGLE PER DWG 6936656. (X)May 9, 2000 · N246US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000678Floorbeam · corrodedCLT - FLOORBEAM HAD LEVEL 1 CORROSION, 1 INCH BY 1 INCH, BS 947, LBL 18. REPLACED T-CAP PER SRM 53-10-2. (X)May 8, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000677Floorbeam · corrodedCLT - FLOORBEAM HAD LEVEL 1 CORROSION, 1 INCH BY 1 INCH, BS 947, LBL 14. REPLACED T-CAP PER SRM 53-10-2. (X)May 8, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000676Floorbeam · corrodedCLT - FLOORBEAM HAD LEVEL 1 CORROSION, 2 INCHES BY 3 INCHES, BS 947, LBL 4.5, RBL 5. REPLACED T-CAP PER SRM 53-10-2. (X)May 8, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000675Beam · crackedCLT - WEB CRACKED 1 INCH, AT LT SIDE CREASE BEAM, STA 663.75. (X)May 8, 2000 · N246US · Boeing 737201 · Fuselage Main, StructureSDR USAA000673Tie Clip · crackedCLT - TIE CLIP CRACKED 0.500 INCH, BS 986.5, STR 25R. INSTALLED TIE CLIP PER SRM 51-10-01. (X)May 8, 2000 · N246US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000672Beam · crackedCLT - LEFT CREASE BEAM WEB HAD .50 INCH CRACK. REPLACED WEB PER TR 53-10-02. (X)May 8, 2000 · N246US · Boeing 737201 · Fuselage Main, StructureSDR USAA000671Web · crackedCLT - WEB CRACKED, 1 INCH, STR 25R, BS 847. INSTALLED NEW WEB PER SRM 51-10-02. (X)May 8, 2000 · N246US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000670Floorbeam · crackedCLT - FLOORBEAM CRACKED0 .500 INCH BY 2 INCH, BS 967, RBL 17.5, CORROSION LEVEL 1. REPLACED ANGLE PER EA67156. (X)May 8, 2000 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA000669Skin · crackedCLT - SKIN CRACKED .250 INCH, FORWARD SERVICE DOOR CUT OUT AFT CORNER. REPAIRED FILLER AND DOUBLER PER SRM 53-30-3. (X)May 8, 2000 · N246US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000653Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, BS 597, STRINGER 4L. INSTALLED NEW TIE CLIP PER EO5393G227. (M)May 1, 2000 · N246US · Boeing 737201 · Fuselage Main, StructureSDR USAA000652Beam · crackedCLT - FOUND BEAM WEB CRACKED .5 INCH, RIGHT CREASE BEAM WEB STATIN 647. REPLACED WEB PER TR 53-10-02. (M)May 1, 2000 · N246US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000651Beam · crackedCLT - FOUND BEAM WEB CRACKED .375 INCH, FRAME 663.75 RT CREASE BEAM FORWARD WEB. REPLACED WEB PER TR 53-10-02. (M)May 1, 2000 · N246US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000650Beam · crackedCLT - FOUND BEAM WEB CRACKED .5 INCH, STATION 616 RIGHT CREASE BEAM WEB. REPLACED NEW WEB PER TR 53-10-02. (M)May 1, 2000 · N246US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000641Clip · crackedCLT - FOUND TIE CLIP CRACKED .250 INCH, STATION 767, STRINGER 5 LEFT. REMOVED AND REPLACED PER EO 5393G227. (M)Apr 28, 2000 · N246US · Boeing 737201 · Fuselage Main, StructureSDR USAA000640Clip · crackedCLT - FOUND TIE CLIP CRACKED .250 INCH, BS 747, STRINGER 10 RIGHT. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M)Apr 28, 2000 · N246US · Boeing 737201 · Fuselage Main, StructureSDR USAA000639Clip · crackedCLT - FOUND TIE CLIP CRACKED .250 INCH, BS 747, STRINGER 7 LEFT. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M)Apr 28, 2000 · N246US · Boeing 737201 · Fuselage Main, StructureSDR USAA000638Clip · crackedCLT - FOUND TIE CLIP CRACKED .500 INCH, BS 747, STRINGER 5 LEFT. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M)Apr 28, 2000 · N246US · Boeing 737201 · Fuselage Main, StructureSDR USAA000637Clip · crackedCLT - FOUND TIE CLIP CRACKED .500 INCH, BS 727B, STRINGER 5 LEFT. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M)Apr 28, 2000 · N246US · Boeing 737201 · Fuselage Main, StructureSDR USAA000636Clip · crackedCLT - FOUND TIE CLIP CRACKED .250 INCH, BS 727B, STRINGER 8 LEFT. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M)Apr 28, 2000 · N246US · Boeing 737201 · Fuselage Main, StructureSDR USAA000635Clip · crackedCLT - FOUND TIE CLIP CRACKED .50 INCH, BS 727B, STRINGER 6 LEFT. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M)Apr 28, 2000 · N246US · Boeing 737201 · Fuselage Main, StructureSDR USAA000634Clip · crackedCLT - FOUND TIE CLIP CRACKED .250 INCH, BS 727A, STRINGER 5R. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M)Apr 28, 2000 · N246US · Boeing 737201 · Fuselage Main, StructureSDR USAA000633Clip · crackedCLT - FOUND TIE CLIP CRACKED, BS 706, STRINGER 10 LEFT. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M)Apr 28, 2000 · N246US · Boeing 737201 · Fuselage Main, StructureSDR USAA000632Clip · crackedCLT - FOUND TIE CLIP CRACKED, .250 INCH, BS 706 STRINGER 3 RIGHT. REPAIRED PER EO 5393G227. (M)Apr 28, 2000 · N246US · Boeing 737201 · Fuselage Main, StructureSDR USAA000631Clip · crackedCLT - FOUND TIE CLIP CRACKED .250 INCH, BS 706, STRINGER 2 RIGHT. REPAIRED PER EO 5393G227. (M)Apr 28, 2000 · N246US · Boeing 737201 · Fuselage Main, Structure
Back to N246US, cancelled Mar 25, 2002