N562AU, cancelled May 17, 2006

Service difficulty reports · 65

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 = 'N562AU' AND deregistration_id = 'N562AU-2006-05-17'
  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 USAASB02067Coalescer Bag · contaminatedCLT - FLT 897 - AFTER TAKEOFF FROM EWR, EN ROUTE TO CLT, A FOUL ODOR WAS REPORTED COMING FROM THE AIR CONDITION PACKS. ODOR DISSIPATED WITHIN 10-15 MINUTES. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT AT CLT. MAINTENANCE REMOVED AND REPLACED THE LEMar 29, 2002 · N562AU · Boeing 737301 · Humidity Control SystemSDR USAASB01309Odor · detectedCLT - FLT 2135 - AFTER TAKEOFF FROM CLT, EN ROUTE TO MCO, THE FLIGHT ATTENDANTS AND PASSENGERS REPORTED A STRONG SMELL OF BURNING PLASTIC. FLIGHT ATTENDANT REPORTED THAT THE ODOR WAS INTENSIFYING. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INNov 6, 2001 · N562AU · Boeing 737301 · Air Distribution SystemSDR USAASB00181Structure · crackedPIT - FLT 9234 - EN ROUTE FROM ROC-CMH, CAPTAIN REPORTED AN AIRFRAME VIBRATION WHICH WAS FELT IN THE AFT GALLEY/LAVATORY AREA. VIBRATION WAS OF HIGH FREQUENCY AND MODERATE FROM 5,000 TO 31,000 FEET BETWEEN 220 TO 300 KNOTS. CAPTAIN ACCOMPLISHED TROUBLESHOOTIJun 29, 2000 · N562AU · Boeing 737301 · Elevator, Tab StructureSDR USAA000607Pan · corrodedCLT - FOUND FLOOR PAN CORRODED 4 INCHES BY 5 INCHES, STATION 1029, LBL 27 FLOOR PAN. FABRICATED NEW STRAP PER EA 67046. (M)Apr 26, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000608Strap · corrodedCLT - FOUND STRAP CORRODED 3 INCHES BY 6 INCHES, STATION 1016-1006, LBL 27 STRAP. REPAIRED FABRICATED STRAP PER EA 67046. (M)Apr 26, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000609Strap · corrodedCLT - FOUND STRAP CORRODED 6 INCHES BY 3 INCHES, STATION 1006-1016, BL 0, WL 208 STRAP. FABRICATED NEW H STRAP PER EA 67046. (M)Apr 26, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000599Keelbeam · corrodedCLT - FOUND KEELBEAM CORRODED 1 INCH BY 11 INCHES, STATION 500C PLUS 17 TO 500D PLUS 8 STRINGER 28R. INSTALLED DOUBLER PER EA66939. (M)Apr 25, 2000 · N562AU · Boeing 737301 · Fuselage Main, KeelSDR USAA000598Fitting · crackedCLT - FOUND FITTING CRACKED .375 INCH, LT MLG BEAM OUTBOARD ATTACH FITTING AT UPPER BOLT ON L/B. REPAIRED PER TR 57-40-13. (M)Apr 24, 2000 · N562AU · Boeing 737301 · Main Landing Gear Attach SectionSDR USAA000582Keelbeam · corrodedCLT - FOUND KEELBEAM CORRODED 2 INCHES BY 6 INCHES, RIGHT KEEL BEAM STATION 500C PLUS 17 TO 500D PLUS 8 STRINGER 28. INSTALLED SPLICE ANGLES PER EA 66939. (M)Apr 18, 2000 · N562AU · Boeing 737301 · Fuselage Main, KeelSDR USAA000575Strap · crackedCLT - FOUND SKIN AND BEARSTRAP CRACKED 2 INCHES, LOWER AFT CORNER OF FORWARD SERVICE DOOR CUTOUT. REPAIRED PER SRM 53-10-01. (M)Apr 17, 2000 · N562AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA000576Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 480, STRINGER 9L. REPAIRED DOUBLER INSTALLED PER SRM 53-00-07 AND SRM 51-30-01. (M)Apr 17, 2000 · N562AU · Boeing 737301 · Fuselage Main, FrameSDR USAA000577Skin · corrodedCLT - FOUND FUSELAGE SKIN CORRODED, .75 INCH BY .75 INCH, BS 500C PLUS 10, LBL 18. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M)Apr 17, 2000 · N562AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA000561Floorbeam · corrodedFOUND FLOORBEAM CORRODED .500 INCH, STATION 360 RBL 52 - RBL 72. INSTALLED T-CAP PER SRM 53-00-51 AND 51-70-11. CORROSION LEVEL 2 NR C53-107-01. (M)Apr 14, 2000 · N562AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA000562Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 3 INCHES BY 1 INCH, STATION 328, RBL 51 TOP SURFACE. INSTALLED T-CAP PER SRM 53-10-51. CORROSION LEVEL 2 NR C53-107-01. (M)Apr 14, 2000 · N562AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA000554Frame · crackedCLT - FRAME CRACKED .75 INCH CRACK, FS 907 JUST LEFT OF STRINGER 1 FRAME. INSTALLED FILLER AND DOUBLER PER EA 66974. (M)Apr 13, 2000 · N562AU · Boeing 737301 · Fuselage Main, FrameSDR USAA000555Beam · corrodedCLT - FOUND BEAM CORRODED .5 INCH, STATION 1016, LBL 6 AND LBL 10 SCREW HOLES. REPAIRED PER TR 53-20-10 AND EA 66954. (M)Apr 13, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000538Floorbeam · crackedCLT - FOUND FLOORBEAM WEB CRACKED 4 PLACES .25 INCH, BS 328, RBL 44, WL 202.5 RIVET HOLES. REMOVED DAMAGED PER EA 66993. (M)Apr 10, 2000 · N562AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA000539Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 727B, STRINGER 4L. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-02. (M)Apr 10, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000540Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 727B, STRINGER 5L. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-02. (M)Apr 10, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000541Frame · crackedCLT - FOUND FRAME CRACKED .500 INCH, BS 887, STRINGER 9L. REMOVED CRACK, INSTALLED DOUBLER PER TR 53-10-14. (M)Apr 10, 2000 · N562AU · Boeing 737301 · Fuselage Main, FrameSDR USAA000542Angle · crackedCLT - FOUND ANGLE CRACKED .5 INCH, BS 639, LBL 45, WL 203 VERT ATTACH ANGLE. REMOVED AND REPLACED ANGLE PER SRM 51-30-02 AND DWG 65-46540. (M)Apr 10, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000543Angle · corrodedCLT - FOUND ANGLE CORRODED 1 INCH BY 15 INCHES, AFT ENT Z-CHANNEL ANGLE. REMOVED AND REPLACED Z-ANGLE PER SRM 51-40-02. (M)Apr 10, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000537Frame · corrodedCLT - FOUND FRAME CORRODED 2 INCHES, STATION 500D, LBL 18 SKIN. INSTALLED DOUBLER, T-ANGLE AND SHIM PER SRM 53-00-07. (M)Apr 7, 2000 · N562AU · Boeing 737301 · Fuselage Main, FrameSDR USAA000531Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, STATION 178, BULKHEAD WEB RBL 4.75, WL 201. INSTALLED DOUBLER PER SRM 53-10-08. (M)Apr 7, 2000 · N562AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA000532Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD WEB LBL 4.75, WL 201. INSTALLED DOUBLER. (M)Apr 7, 2000 · N562AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA000533Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD WEB LBL 4.75, WL 198. INSTALLED DOUBLER PER SRM 53-10-08. (M)Apr 7, 2000 · N562AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA000534Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD WEB RBL 4.75, WL 198. INSTALLED DOUBLER PER SRM 53-10-08. (M)Apr 7, 2000 · N562AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA000535Stiffener · crackedCLT - FOUND VERTICAL STIFFENER CRACKED 1 INCH, STATION 178 BULKHEAD VERTICAL STIFFENER LBL 6, WL 184. INSTALLED DOUBLER AND ANGLES PER SRM 53-10-08. (M)Apr 7, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000536Bulkhead · crackedCLT - FOUND WEB CRACKED .25 INCH LONG, STATION 178 BULKHEAD WEB RBL 1, WL 206. INSTALLED DOUBLER PER SRM 53-10-08. (M)Apr 7, 2000 · N562AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA000528Web · crackedCLT - FOUND WEB CRACKED .25 INCH, BS 710-717, BBL 0, WL 203. INSTALLED DOUBLER PER SRM 51-70-13. (M)Apr 5, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000520Skin · crackedCLT - FOUND DOOR SKIN CRACKED 5 INCHES BY 5 INCHES, FORWARD SERVICE DOOR LOWER HINGE CUTOUT. INSTALLED DOUBLER PER SRM 52-00-01 FIG 203. (M)Apr 4, 2000 · N562AU · Boeing 737301 · Service DoorsSDR USAA000523Channel · corrodedCLT - FOUND Z-CHANNEL CORRODED, AFT SERVICE DOOR. REPLACED WITH NEW Z-CHANNEL PER SRM 51-4-02. (M)Apr 4, 2000 · N562AU · Boeing 737301 · Service DoorsSDR USAA000524Angle · corrodedCLT - FOUND DOOR Z-ANGLE CORRODED 6 FT BY 3 INCHES, STATION 947-1006, LBL 60, AFT ENTRY DOOR Z-ANGLE. INSTALLED NEW Z-ANGLE PER SRM 51-40-02. (M)Apr 4, 2000 · N562AU · Boeing 737301 · Passenger/Crew DoorsSDR USAA000522Stringer · crackedCLT - FOUND STRINGER CRACKED .5 INCH, STRINGER 18 SHELF AT AFT END INBOARD RIVET IN WEB. REPLACED PER SRM 51-10-02. (M)Apr 4, 2000 · N562AU · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA000521Frame · crackedCLT - FOUND FRAME CRACKED .75 INCHES LONG, BOTTOM END OF STATION 616 INBOARD CHORD ANGLE RIGHT SIDE. FABRICATED ANGLE AND FILLER PER TR 53-62-01. (M)Apr 4, 2000 · N562AU · Boeing 737301 · Fuselage Main, FrameSDR USAA000508Stringer Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 727A, STRINGER 2R TIE CLIP AFT SIDE. REPLACED TIE CLIP PER SRM 51-10-02. (M)Mar 30, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000509Stringer Clip · crackedCLT - FOUND STRINGER TIE CLIP WITH TWO CRACKS .5 INCH LONG, STATION 639, STRINGER 4R FUSELAGE FRAME. REPLACED TIE CLIP PER SRM 51-10-02 AND 51-40-02. (M)Mar 30, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000510Door Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, FORWARD SERVICE DOOR FRAME LOWER FORWARD CORNER. INSTALLED DOUBLER AND FILLER PER SRM 51-10-11. (M)Mar 30, 2000 · N562AU · Boeing 737301 · Fuselage Main, StructureSDR USAA000512Bulkhead · crackedCLT - FOUND .5 INCH CRACK IN BULKHEAD, STATION 178, WEB LBL .75, WL 188. INSTALLED DOUBLER REPAIR PER SRM 53-10-08. (M)Mar 30, 2000 · N562AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA000507Frame · crackedCLT - FOUND FRAME CRACKED .250 INCH, STATION 827, STRINGER 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)Mar 30, 2000 · N562AU · Boeing 737301 · Fuselage Main, FrameSDR USAA000506Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 986, RBL 14 UPPER CHORD FLOORBEAM. REPLACED NEW T-CAP PER TR 53-10-05A. (M)Mar 30, 2000 · N562AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA000490Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 344 AT BL 0, LBL 22. CORROSION LEVEL 1. INSTALLED FLOORBEAM TOP CAP PER SRM 51-70-12. (M)Mar 29, 2000 · N562AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA000491Beam · corrodedCLT - FOUND BEAM CORRODED .5 INCH BY .5 INCH, BS 1006, LBL 10 BEAM SCREW HOLES. REPAIRED DOUBLER PER SRM 53-00-51. (M)Mar 29, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000492Seat Track · corrodedCLT - FOUND SEAT TRACK CORRODED 2 INCHES BY 2 INCHES, STATION 344, LBL 25. INSTALLED NEW SEAT TRACK PER SRM 53-00-52. (M)Mar 29, 2000 · N562AU · Boeing 737301 · Fuselage, Seat/Cargo Attach FittingsSDR USAA000464Stringer Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 727B, STRINGER 16. REMOVED AND REPLACED WITH NEW TIE CLIP PER SRM 51-10-02. (M)Mar 27, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000465Beam · corrodedCLT - FOUND BEAM CORRODED .5 INCH, STATION 967, LBL 5 UPPER CHORD SCREW HOLE BEAM. INSTALLED T-CAP PER SRM 53-00-51. CORROSION LEVEL 1. (M)Mar 27, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000469Frame · crackedCLT - FOUND CHORD CRACKED .5 INCH, BS 616, WL 202 RIGHT SIDE INNER FRAME CHORD AT LOWER FAST. REPAIRED DOUBLER PER TR 53-62-01. (M)Mar 27, 2000 · N562AU · Boeing 737301 · Fuselage Main, FrameSDR USAA000453Angle · crackedCLT - FOUND CHORD ANGLE CRACKED .350 INCH, BS 291.5 BETWEEN STRINGER 10R AND 11R. REPAIRED PER SRM 51-40-02. (M)Mar 24, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000454Stringer Clip · crackedCLT - FOUND TIE CLIP CRACKED .250 INCH, BS 663 STRINGER 10L. REPAIRED PER SRM 51-10-02. (M)Mar 24, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000455Stringer Clip · crackedCLT - FOUND TIE CLIP CRACKED .500 INCH, BS 887, STRINGER 1. REPAIRED PER SRM 51-40-02 AND 51-10-00. (M)Mar 24, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous Structure
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