N261AU, cancelled Jun 6, 2002

Service difficulty reports · 73

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 = 'N261AU' AND deregistration_id = 'N261AU-2002-06-06'
  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 USAASB01181Battery · dischargedBOS - THE PASSENGER CABIN CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)Jun 20, 2001 · N261AU · Boeing 737201 · Emergency LightingSDR USAASB01102Power Supply · inoperativeMCO - THE CENTER OVERHEAD EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE CENTER OVERHEAD EMERGENCY EXIT LIGHT POWER SUPPLY. (M)Apr 17, 2001 · N261AU · Boeing 737201 · Emergency LightingSDR USAASB01107Power Supply · failedLGA - THE CENTER EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT POWER SUPPLY. (M)Apr 4, 2001 · N261AU · Boeing 737201 · Emergency LightingSDR USAA010201Skin · crackedBOS - FOUND SKIN CRACKED .75 INCH, BETWEEN STATION 787/807 STRINGER 19L. INSTALLED DOUBLER INCORPORATED PREVIOUS PATCH PER SRM 53-30-3 FIG 1. (M)Feb 9, 2001 · N261AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB00293Accessory Unit · faultyBDL - FLT 2708 - ON FINAL APPROACH TO BDL FROM MCO, CREW RECEIVED THREE GREEN GEAR DOWN LIGHTS AND THREE RED GEAR UNSAFE LIGHTS WHEN GEAR WAS EXTENDED. CREW RECYCLED GEAR SEVERAL TIMES AND RED LIGHTS EXTINGUISHED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAIOct 16, 2000 · N261AU · Boeing 737201 · Landing Gear Position and WarningSDR USAA001728Stringer · crackedCLT - FOUND STRINGER CRACKED .250 INCHES, BS 360, STRINGER 15L. INSTALLED NEW PART PER SRM 51-10-01. (M)Oct 12, 2000 · N261AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA001729Wedge · crackedCLT - FOUND SLAT TRAILING EDGE WEDGE CRACKED 12.5 INCHES, ENTIRE WIDTH OF THE WEDGE. REMOVED DAMAGED CORE PER EA 68081 AND SRM 51-40-10 AND 51-70-10. (M)Oct 12, 2000 · N261AU · Boeing 737201 · Leading Edge DevicesSDR USAA001698Angle · crackedCLT - FOUND CHORD ANGLE CRACKED 2 INCHES, STATION 695 AT RBL 48. REPAIRED PER EA 68082. (M)Oct 9, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001697Angle · crackedCLT - FOUND CHORD ANGLE CRACKED 2 INCHES, STATION 695 AT LBL 48. REPAIRED PER EA 68082. (M)Oct 9, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001696Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .500 INCH, STRINGER TIE CLIP FS 500B, STRINGER 22L. INSTALLED TIE CLIP PER SRM 51-10-1 AND 51-30-3. (M)Oct 9, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001648Floorbeam · crackedCLT - FOUND CHORD ANGLE CRACKED 1 INCH, AT FLOORBEAM CHORD BS 344, RBL 12. REPLACED ANGLE PER SRM 51-10-2. (M)Oct 2, 2000 · N261AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001649Floorbeam · crackedCLT - FOUND FLOORBEAM CHORD CRACKED 1 INCH, AT SEAT TRACK BS 344, WL 208. REPLACED BEAM PER TR 53-10-13. (M)Oct 2, 2000 · N261AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001650Attach Angle · crackedCLT - FOUND ATTACH ANGLE CRACKED 1 INCH, STATION 350, STRINGER 15L, WL 221. REPLACED ANGLE PER SRM 51-10-01. (M)Oct 2, 2000 · N261AU · Boeing 737201 · Fuselage Main, Attach FittingsSDR USAA001651Stringer · crackedCLT - FOUND STRINGER CRACKED .75 INCH, STRINGER 16L CRACKED AT FS 787. INSTALLED DOUBLER PER SRM 53-10-3. (M)Oct 2, 2000 · N261AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA001631Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, BS 967, RBL 44 - LBL 12. CORROSION LEVEL 1 C 53-107-02. REPAIRED PER T-CAP SPLICE PER SRM 53-10-9. (M)Sep 29, 2000 · N261AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001630Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, BS 947, RBL 50 - LBL 44. REPAIRED T-CAP PER SRM 53-10-09. (M)Sep 29, 2000 · N261AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001629Angle · crackedCLT - FOUND ANGLE CRACKED 1.5 INCH, FORWARD SERVICE DOOR Z-ANGLE STATION 296.5, WL 208. FABRICATED NEW ANGLE PER DWG 65-45807. (M)Sep 29, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001628Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 827, STRINGER 9R. REPAIRED PER EO 5393G227. (M)Sep 29, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001627Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 663.75, STRINGER 10R. REPAIRED PER EO 5393G227. (M)Sep 29, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001626Angle · crackedCLT - FOUND ANGLE CRACKED .25 INCH, AFT LOWER CORNER ANGLE ASSEMBLY THRESHOLD. REPAIRED PER SRM 51-30-02. (M)Sep 29, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001613Bulkhead · crackedCLT - FOUND THE BULKHEAD WEB CRACKED .5 INCH, STATION 178 RBL 6.75, WL 198. ENLARGED CUTOUT OF DAMAGE (3 INCHES BY 5 INCHES) AND INSTALLED DOUBLERS PER SRM 53-10-11 FIG 1. (M)Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA001619Tie Clip · crackedCLT - FOUND TIE CLIP CARCKED .25 INCH, AT FS 727B-582. MODIFIED PART INSTALLED PER EO 5393G227. (M)Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001618Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED, .572 INCH BS 663-510L. MODIFIED PART INSTALLED PER EO 5393G227. (M)Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001617Tie Clip · crackedCLT - FOUND STRINGER TIE CLIP CRACKED .25, STRINGER 10L B STATION 500A. REPLACED CLIP PER EO 5393G227. (M)Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001622Web · crackedCLT - FOUND WEB CRACKED .25 INCH, AT FORWARD END OF STRINGER 14R AT STATION 277. ROUTED OUT CRACK PER 51-10-1 FIG 1. (M)Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001621Stiffener · crackedCLT - FOUND VERTICAL STIFFENER CRACKED 1 INCH, INBOARD FLANGE LBL 5.7 VERT STIFFENER STATION 178 WL 184. INSTALLED 1/2 HARD SS ANGLES PER SRM 53-10-11. (M)Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001620Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, STATION 597 STRINGER 9R. MODIFIED PART INSTALLED PER EO 53936227. (M)Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001616Tie Clip · crackedCLT - FOUND STRINGER TIE CLIP CRACKED, FS 727B-S7L. MODIFIED PART INSTALLED PER EO 5393G227. (M)Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001615Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, STATION 639 STRINGER 2R. MODIFIED PART INSTALLED PER EO 5393G227. (M)Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001614Splice · crackedCLT - FOUND STRINGER END SPLICE CRACKED .5 INCH, STATION 360 STRINGER 14L. REPLACED SPLICE PER SRM 51-10-01. (M)Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001610Skin · crackedCLT - FOUND DOOR CUTOUT CRACKED 3 INCHES, LEFT AFT ENTRY DOOR LOWER FORWARD CORNER. INSTALLED DOUBLER PER SRM 53-30-03 AND EA 68158. (M)Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA001609Bulkhead · crackedCLT - FOUND AFT NOSE W/W BULKHEAD CRACKED 1.5 INCHES, ACT SUPPORT BEAM WEB STATION 228, WL 185.5, BL 0. INSTALLED FILLER AND DOUBLER PER SRM 51-40-2. (M)Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA001599Angle · crackedCLT - FOUND VERTICAL ANGLE CRACKED .25 INCH, AFT SIDE STATION 727, BULKHEAD RBL 6.5. REPLACED ANGLE PER SRM 51-10-01 AND EA 68132. (M)Sep 28, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001570Skin · crackedCLT - FOUND SKIN CRACKED .25 INCH, BS 339, STRINGER 17LT. REPAIRED PER DWG 65C27257 AND 65C27297. (M)Sep 27, 2000 · N261AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA001569Frame · crackedCLT - FOUND SIDE CHORD CRACKED 2 INCHES, BS 178, WL 207, LBL 25. INSTALLED REPAIR ANGLE PER SRM 53-10-11 AND EA 68032. (M)Sep 27, 2000 · N261AU · Boeing 737201 · Fuselage Main, FrameSDR USAA001598Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD WEB LBL 6.75 WL 201. ENLARGED CUT OUT OF DAMAGE (3 INCHES BY 5 INCHES) AND INSTALLED DOUBLERS. (M)Sep 27, 2000 · N261AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA001575Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, BS 986, RBL 46, LBL 12. CORROSION LEVEL 1, C53-107-02. INSTALLED FABRICATED T-CAP AND SPLICE DOUBLER PER TR 53-60-01 REV A. (M)Sep 27, 2000 · N261AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001574Web · crackedCLT - FOUND WEB CRACKED TWO PLACES .25 INCH EACH, 2 INCHES AND 3 INCHES AFT OF BS 706 AT BL 0. INSTALLED FILLER, DOUBLER AND TRIPLER PER TR 57-10-05. (M)Sep 27, 2000 · N261AU · Boeing 737201 · Wing Miscellaneous StructureSDR USAA001573Angle · crackedCLT - FOUND CHORD ANGLE CRACKED 1 INCH, STATION 663, RBL 25, WL 201.5 ON L/B SIDE. INSTALLED REPAIR ANGLE AND SPLICES PER EA 68031. (M)Sep 27, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001572Torque Box · crackedCLT - FOUND TORQUE BOX CRACKED .5 INCH, FS 947 PLUS 1, STRINGER 10L. INSTALLED FILLER AND REPAIR STRAP PER TR 53-30-07A. (M)Sep 27, 2000 · N261AU · Boeing 737201 · Fuselage Main, StructureSDR USAA001571Web · crackedCLT - FOUND WEB CRACKED 3 INCHES, IN RADIUS OF NLG ACT BEAM WEB. REPLACED WEB PER SRM 51-10-02. (M)Sep 27, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001565Skin · crackedCLT - FOUND SKIN CRACKED 3 INCHES, BS 962, STRINGER 17 LEFT. INSTALLED DOUBLER PER SRM 53-30-3 FIG 24. (M)Sep 26, 2000 · N261AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA001544Floorbeam · corrodedCLT - FOUND FLOORBEAM 2 INCHES BY 10 INCHES, BS 1016, LBL 5 - LBL 15. CORROSION LEVEL 1. REPAIRED T-CAP PER TR 53-60-02. (M)Sep 25, 2000 · N261AU · Boeing 737201 · Fuselage Main, Floor BeamSDR SAA001543Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 827, STRINGER 9RT. REPAIRED PER EO 5393G227. (M)Sep 25, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001539Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED 3 INCHES, STATION 178, LBL 5.7, WL 211-214. INSTALLED DOUBLER PER SRM 53-10-11. (M)Sep 25, 2000 · N261AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA001538Frame · crackedCLT - FOUND CHORD ANGLE CRACKED 1 INCH, STATION 663, LBL 25, WL 201.5 ON L/B SIDE. INSTALLED DOUBLER PER EA 68031. (M)Sep 25, 2000 · N261AU · Boeing 737201 · Fuselage Main, FrameSDR USAA001507Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED 2 INCHES, BS 178, WL 195, RBL 24. INSTALLED NEW INTERCOSTAL PER TR 53-10-15. (M)Sep 12, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001506Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED 2 INCHES, BS 178, WL 195, LBL 24. INSTALLED NEW INTERCOSTAL PER TR 53-10-15. (M)Sep 12, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001505Floorbeam · corrodedCLT - FOUND T-CAP CORRODED 6 PLACES 1 INCH BY 1 INCH EACH, BS 344 LBL 24 TO RBL 24, WL 208. CORROSION LEVEL 1 C53-46-53501C. INSTALLED T-CAP PER TR 53-10-13. (M)Sep 12, 2000 · N261AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001504Strap · crackedCLT - FOUND STABILIZER STRAP CRACKED .5 INCH, BS 328 AT RBL 33. INSTALLED DOUBLER PER SRM 53-10-9 FIG 4. (M)Sep 12, 2000 · N261AU · Boeing 737201 · Fuselage Miscellaneous Structure
Back to N261AU, cancelled Jun 6, 2002