N252AU, cancelled Jul 18, 2002

Service difficulty reports · 83

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 = 'N252AU' AND deregistration_id = 'N252AU-2002-07-18'
  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 USAASB01108Charger · inoperativeMCO - THE FORWARD SECTION OF LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY/CHARGER. (M)Apr 25, 2001 · N252AU · Boeing 737201 · Emergency LightingSDR USAASB00361Charger · dischargedLGA - MAINTENANCE FOUND THE LOW LEVEL EMERGENCY PATH LIGHTS FROM SEAT ROWS 1 THROUGH 7 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (P/N 9008-3-5A) AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M)Dec 27, 2000 · N252AU · Boeing 737201 · Emergency LightingSDR USAASB00353Seal · failedBWI - FLT 2637 - ON CLIMB-OUT FROM BWI, AT FL230, A LOUD SQUEAL BEGAN COMING FROM THE FORWARD MAIN ENTRY DOOR. FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FORWARD MAIN Dec 21, 2000 · N252AU · Boeing 737201 · Passenger/Crew DoorsSDR USAA001925Skin · crackedCLT - FOUND SKIN CRACKED .5 INCH, UNDER STRINGER 5L, STATION 1138 LEFT STAB. INSTALLED DOUBLER PER EA 68315. (M)Nov 13, 2000 · N252AU · Boeing 737201 · Horizontal Stabilizer, Plate/SkinSDR USAA001959Web · crackedCRACKS UPPER RT & LT RADAR MOUNT BRACKET RBL 05 WL 198CORRECTIVE ACTION: DOUBLERS INSTALLED PER EA 68266Nov 13, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA002118Skin · crackedPIT - FOUND SKIN CRACKED .5 INCH, AFT ENTRY DOOR BELOW LOWER HINGE AREA. INSTALLED DOUBLER PER SRM 52-00-3. (M)Nov 11, 2000 · N252AU · Boeing 737201 · Service DoorsSDR USAA001917Angle · crackedCLT - FOUND ANGLE 1 INCH, RT STA 597 BELOW FLOOR LEVEL. REPLACED ANGLE PER SRM 51-10-1. (M)Nov 9, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001887Intercostal · corrodedCLT - FOUND INTERCOSTAL CORRODED 1 INCH BY 1 INCH, STATION 990, LBL 17 FLOORBEAM INTERCOSTAL. INSTALLED DOUBLER PER SRM 53-10-09 AND TR 53-60-02. CORROSION LEVEL 1 C53-107-02. (M)Nov 7, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001892Frame · crackedCRACK STA 490, STR 23R. SPLICED IN FRAME SECTION PER SRM 51-40-3 FIG 1Nov 7, 2000 · N252AU · Boeing 737201 · Fuselage Main, FrameSDR USAA001891Frame · crackedCRACK STA 597, R/W LWR SIDE OF FRAME. REPLACED WEB/FRAME PER SRM 51-10-01Nov 7, 2000 · N252AU · Boeing 737201 · Fuselage Main, FrameSDR USAA001890Floorbeam · corrodedCORROSION LEVEL 1 C 53-107-02 FLOORBEAM INTERCOASTAL STRAP STA 1016, LBL 17.5INSTALLED FLOORBEAM REPAIR ANGLE PER SRM 51-10-1Nov 7, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001889Intercostal · corrodedCORROSION LEVEL 1 C 53-107-02 FLOORBEAM INTERCOASTAL STRAP STA 1016, RBL 2.5.INSTALLED DOUBLER PER SRM 531009 & 536002Nov 7, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001888Floorbeam · corrodedFLOORBEAM CORRODED. INSTALLED DOUBLER PER SRM 53-10-09 & TR 53-60-02.Nov 7, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001877Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 2 INCHES AND 1 FT BY 2 INCHES, STATION 1006 TO 1016, LBL 5.5 TO 9. REMOVED AND REPLACED PER SRM 51-30-00. (M)Nov 3, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001859Frame · crackedCLT - FOUND CHORD CRACKED 2 INCH, BS 178, WL 195, LBL 24. INSTALLED NEW CHORD ANGLE. (M)Nov 2, 2000 · N252AU · Boeing 737201 · Fuselage Main, FrameSDR USAA001858Web · crackedCLT - FOUND WEB CRACKED, BS 178, RBL 5, WL 198. INSTALLED DOUBLER PER EA 68266. (M)Nov 2, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001857Web · crackedCLT - FOUND WEB CRACKED .5 INCH IN TWO PLACES, BS 178, LBL 5 AND 6 UPPER RADAR MOUNT BRACKET. INSTALLED DOUBLER PER EA 68266. (M)Nov 2, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001856Frame · crackedCLT - FOUND SIDE CHORD CRACKED 1 INCH, BS 178, WL 207, LBL 26. INSTALLED NEW CHORD ANGLE PER EA 68295. (M)Nov 2, 2000 · N252AU · Boeing 737201 · Fuselage Main, FrameSDR USAA001855Web · crackedCLT - FOUND WEB CRACKED 1 INCH, BS 178, WL 207, LBL 27. INSTALLED NEW CHORD ANGLE PER EA 68295. (M)Nov 2, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001854Web · crackedCLT - FOUND WEB CRACKED .250 INCH, BS 178, LBL .05, WL 197-201. INSTALLED DOUBLER PER EA 68266. (M)Nov 2, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001853Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH IN SIX AREAS, UPPER T-CAP FLOORBEAM STATION 1006, LBL 9, 11, 15, 28.5. INSTALLED NEW T-CAP SECTION PER SRM 53-10-9 FIG 2. (M)Nov 2, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001842Web · crackedCLT - FOUND WEB CRACKED 1 INCH, BS 676, RBL 25. INSTALLED DOUBLER AND V CHANNEL PER EO 5791G632. (M)Nov 1, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001841Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED .250 INCH, BS 668 - BS 680, LBL 23.5. REMOVED AND REPLACED BEAM PER DWG 65-45410. (M)Nov 1, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001840Stiffener · crackedCLT - FOUND VERTICAL CHORD CRACKED .25 INCH, BS 178, AFT SIDE LBL 5-7, WL 184. FOUND DOUBLER STRAP/REPAIR ANGLES PER SRM 53-10-11. (M)Nov 1, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001839Stiffener · crackedCLT - FOUND VERTICAL CHORD (STIFFENER) CRACKED .25 INCH, BS 178, AFT SIDE RBL 5-7, WL 184. FOUND DOUBLER STRAP/REPAIR ANGLES PER SRM 53-10-11. (M)Nov 1, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001835Tie Clip · crackedCLT - FOUND STRINGER TIE CLIP CRACKED .25 INCH, STATION 578 STRINGER 5L. REPLACED TIE CLIP PER EO 5393G227 REV A. (M)Oct 31, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001833Web · crackedCLT - FOUND WEB CRACKED .250 INCH, BS 706-710, LBL 24. INSTALLED NEW WEB PER EA 68267. (M)Oct 27, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001832Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 3 INCHES, LOWER SURFACE CREASEBEAM WEB AFT SERVICE DOOR. INSTALLED DOUBLER AND REPAIR ANGLE PER SRM 51-10-1. CORROSION LEVEL 1 C53-107-02. (M)Oct 27, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001826Stringer · corrodedCLT - FOUND STRINGER CORRODED 1 INCH BY 1 INCH AREA, BS 948 STRINGER 27L. CORROSION LEVEL 1. INSTALLED NEW SECTION PER SRM 53-10-3. (M)Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA001825Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH IN FOUR PLACES, STATION 947.5 RBL 4, 5, 10.5 AND LBL 5. CORROSION LEVEL 1. SPLICED T-CAP PER SRM 53-10-2. (M)Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001824Angle · corrodedCLT - FOUND TRANSITION ANGLE CORRODED 32 INCHES BY 1 INCH, STATION 344 TO 312. INSTALLED NEW Z-ANGLE PER SRM 51-10-2 AND 51-30-3. (M)Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001823Floorbeam · corrodedCLT - FOUND FLOOBEAM CORRODED 12 INCHES BY 5 INCHES, STATION 344, BL 0 TO BL 12L. CORROSION LEVEL 1. REPLACED PER TR 53-10-13. (M)Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001822Web · crackedCLT - FOUND WEB CRACKED .250 INCH, BS 715. REPAIRED PER TR 57-10-05. (M)Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001821Web · crackedCLT - FOUND LONGITUDINAL WEB CRACKED 1 INCH, BS 706-710, RBL 24. INSTALLED DOUBLER AND WEB PER EA 67997-A, EA 68267 AND TR 57-10-05. (M)Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001820Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED 2 INCHES, BS 178, WL 195, RBL 24. REPAIRED PER EO 5300V152. (M)Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001819Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED 2 INCHES, BS 178 WL 195, LBL 24. INSTALLED NEW INTERCOSTAL PER SRM 51-10-1. (M)Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001818Beam · crackedCLT - FOUND LONGITUDINAL BEAM 2 INCH CRACK, BS 663, OBL. INSTALLED DOUBLER, NEW WEB PER TR 57-10-04 AND EA 68369. (M)Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Main, StructureSDR USAA001817Tie Clip · crackedCLT - FOUND TIE CLIP .5 INCH, STATION 400 STRINGER 28L. REPAIRED PER SRM 51-10-1. (M)Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001816Stringer Clip · crackedCLT - FOUND STRINGER TIE CRACKED .5 INCH, BS 360, STRINGER 16L. REPAIRED PER SRM 51-30-2. (M)Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001815Angle · crackedCLT - FOUND INTERCOSTAL ANGLE CRACKED 2 INCHES, BS 178, WL 195 LBL 25. INSTALLED DOUBLER PER SRM 51-40-4. (M)Oct 26, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001797Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED 2 INCHES, STATION 957 FORWARD LOWER CORNER AFT RIGHT SERVICE DOOR CUTOUT. INSTALLED 3 DOUBLERS AND FILLERS PER SRM 53-30-3. (M)Oct 23, 2000 · N252AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA001798Skin · corrodedCLT - FOUND CORROSION ON SKIN 8 INCHES BY 3 INCHES, STATION 767-787. CORROSION LEVEL 1. INSTALLED DOUBLER AND FILLER PER SRM 53-30-3. (M)Oct 23, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001778Frame · crackedCLT - FOUND FRAME CRACKED 3 INCHES, LOWER END OF FORWARD SERVICE DOOR FORWARD FRAME WL 209. FABRICATED REPAIR PARTS PER SRM 51-40-03. (M)Oct 19, 2000 · N252AU · Boeing 737201 · Fuselage Main, FrameSDR USAA001779Floorbeam · corrodedCLT - FOUND FLOORBEAM 38 INCHES, STATION 328, BL 12L TO BL 50L. CORROSION LEVEL 1. REPLACED FLOORBEAM PER SRM 53-10-9. (M)Oct 19, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001772Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORRODED 1 INCH BY 1 INCH EACH, STATION 987, LBL 5, 6, 16, 17, 39.5 AND RBL 5, 14.5, 23.5. INSTALLED NEW T-CAP PER TR 53-60-01 REV A. (M)Oct 18, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001771Floorbeam · crackedCLT - FOUND FLOORBEAM ANGLE CRACKED 1 INCH, BS 520, RBL 45. REPLACED ANGLE PER REPAIR DOCUMENT 51-10-02. (M)Oct 18, 2000 · N252AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA001759Floor Support · crackedCLT - FOUND FLOOR SUPPORT CRACKED 1 INCH, BS 727, LBL 46. FABRICATED ANGLE PER SRM 51-10-03. (M)Oct 16, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA001758Bulkhead · crackedCLT - FOUND WEB CRACKED, BS 178, RBL 10.5, WL 234. INSTALLED DOUBLER PER SRM 53-10-11. (M)Oct 16, 2000 · N252AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA001757Bulkhead · crackedCLT - FOUND WEB CRACKED .25 INCH IN TEN PLACES, BS 178, WL 234 BETWEEN LT AND RBL 7 TO 12 AFT SIDE. INSTALLED DOUBLER PER SRM 53-10-11. (M)Oct 16, 2000 · N252AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA001707Splice · crackedCLT - FOUND STRINGER SPLICE CRACKED .375 INCH, STATION 908, STRINGER 4L CIRCUMFERENTIAL SPLICE. REPAIRED PER SRM 51-10-01. (M)Oct 10, 2000 · N252AU · Boeing 737201 · Fuselage Miscellaneous Structure
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