N524AS

Service difficulty reports · 66

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 = 'N524AS' AND registry_match = 'registration'
  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 ASAA2015083013054Intercostal · crackedMAIN CABIN, INTERCOSTAL AT BS 340-360, BL 0 HAS A CRACKED NUTPLATE HOLE. ACFT GROUNDED. REMOVED CRACKED INTERCOSTAL, LOCATED AND DRILLED NEW INTERCOSTAL AND INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02, 51-40-05 AND DWG 141A5400, REV REMOVED DOT.Aug 30, 2015 · N524AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015083013053Intercostal · crackedMAIN CABIN, INTERCOSTAL AT BS 340-360, LBL 11 HAS A CRACKED NUTPLATE HOLE. ACFT GROUNDED. REMOVED CRACKED WEB, LOCATED AND DRILLED NEW WEB, INSTALLED NEW WEB IAW SRM 51-40-02 AND DWG 141A5400. REMOVED DOT.Aug 30, 2015 · N524AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015082813065Skin · corrodedCORROSION AT FWD SIDE OF DOOR 311BL ON FUSELAGE. ACFT GROUNDED. REMOVED CORRROSION FROM FUSELAGE FWD OF DOOR 311BL ORIGINAL MATERIAL THICKNESS WAS .080 WITH .005 REMOVED .075 REMAINING FOUND TO BE IN LIMITS IAW SRM 53-80-01-1A-5 TREATED, PRIMED AND TOP COATEDAug 28, 2015 · N524AS · Boeing 737890 · Fuselage Main, Plate/SkinSDR ASAA2015082813049Stop Fitting · gougedL2 DOOR CUTOUT FWD UPPER DOOR STOP FITTING GOUGED, NR G556189 WRITTEN TO CHECK DOOR ADJUSTMENT. ACFT GROUNDED. R & R STOP FITTING IAW AMM 52-13-01 AND DWG 144A8101 REV A ADJUSTMENT CHECK ACCOMPLISHED ON CARD NR NRG556189 DOT REMOVED.Aug 28, 2015 · N524AS · Boeing 737890 · Fuselage Main, StructureSDR ASAA2015021710692Skin · crackedRT HORIZONTAL LOWER SKIN HAS 2 CRACKS AT STA 129.5, APPROXIMATELY 10' AND 18' FROM THE AFT SPAR. ACFT GROUNDED. REPAIRED CRACKED SKIN AT RT HORIZONTAL LOWER SKIN AT STAB STA 129.5, 10" AND 16" FROM AFT SPAR IAW SRM 55-10-01-2R-11.Feb 17, 2015 · N524AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2015021710691Skin · crackedLT HORIZONTAL LOWER SKIN CRACKED AT STA. 101.9 APPROXIMATELY 10' FROM AFT SPAR. ACFT GROUNDED. REPAIRED CRACKED SKIN AT LT HORIZONTAL STAB STA 101.9 APPROXMATELY 10" FROM AFT SPAR IAW SRM 55-10-01-2R11.Feb 17, 2015 · N524AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2015021710690Skin · crackedRT HORIZONTAL LOWER SKIN CRACKED AT STA 101.9, APPROXIMATELY 11' FROM THE AFT SPAR. ACFT GROUNDED. REPAIRED CRACKED SKIN IAW SRM 55-10-01-2R-11.Feb 17, 2015 · N524AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2015012510422Sign · brokenEMERGENCY LIGHT EXIT LOCATOR SIGN AT L-2 DOOR IS BROKEN. ACFT GROUNDED. REMOVED, REPLACED, AND TESTED THE SIGN IAW MM 33-51-01-960-802. OPS NORMAL.Jan 25, 2015 · N524AS · Boeing 737890 · Emergency LightingSDR ASAA2015012510421Lens · damagedEMERGENCY LIGHT EXIT LOCATOR SIGN AT RT FORWARD OVERWING EXIT HAS DAMAGED LENS. ACFT GROUNDED. R & R LENS AND TESTED IAW MM 33-51-01-960-801. OPS NORMAL.Jan 25, 2015 · N524AS · Boeing 737890 · Emergency LightingSDR ASAA2014050607803Web · corrodedAFT CARGO FLOOR SUPPORT FWD "SHIELD" CORRODED AT FASTENERS BS 765-794, STRINGER 25R. ACFT GROUNDED. R & R SHIELD.May 6, 2014 · N524AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2014042807626Guide · lack of lubeL1 DOOR DIFFICULT TO CLOSE. ACFT GROUNDED. CLEANED AND LUBRICATED DOOR GUIDES. CHECKED FWD ENTRY DOOR IAW AMM 52-11-00-200-801. NO DEFECTS NOTED, NO HISTORY LAST 90 DAYS. OK TO CONTINUE IN SERVICE.Apr 28, 2014 · N524AS · Boeing 737890 · Passenger/Crew DoorsSDR ASAA2013121396893Housing · gougedFWD CARGO DOOR HANDLE HOUSING GOUGED. ACFT GROUNDED. REPLACED HOUSING ASSY IAW NG-52EO-06500-1.Dec 13, 2013 · N524AS · Boeing 737890 · Cargo/Baggage DoorsSDR ASAA2013100296222Engine · malfunctionedDURING CLIMB, THROUGH APPROX FL 320, NR 2 ENGINE PARAMETERS BEGAN FLUCTUATING. N1 VARIED /- 3-5 . TURNED AUTO THROTTLES OFF, REDUCED THRUST, FLUCTUATIONS CONTINUED. LEVELED OFF FL 350 FLUCTUATIONS SLOWLY DISSIPATED TO NORMAL WITHIN ABOUT 30 SECONDS. FIRST FOct 2, 2013 · N524AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2013082695883Nut · looseCATERING REPORTED UNABLE TO OPEN THE R1 DOOR. ACFT GROUNDED. FOUND R1 DOOR GUIDE ARM ADJUSTMENT JAMB NUT LOOSE, ADJUSTED GUIDE ARM, TIGHTENED JAMB AND INSTALLED LOCK CHANNEL, REF AMM 52-11-00-820-801, STEP H. R-1 DOOR TESTED GOOD, REF AMM 52-11-00-700-804, Aug 26, 2013 · N524AS · Boeing 737890 · Passenger/Crew DoorsSDR ASAA12511644Battery Pack · no testBATTERY PACK, M1673, FAILED CAPACITANCE TEST (15 MINUTE MINIMUM). REPLACED POWER SUPPLY M1673.May 31, 2012 · N524AS · Boeing 737890 · Emergency LightingSDR ASAA1159720Skin · puncturedFOUND A PUNCTURE IN FUSELAGE SKIN AT APPROX BS 881 BETWEEN STR 16 AND 17 LT. CUT OUT DAMAGED AREA AND INSTALLED EXTERNAL REPAIR DOUBLER IAW B737 800 SRM 53 00 01 REPAIR 3 AND EA 800 53EA 05484.May 25, 2011 · N524AS · Boeing 737890 · Fuselage Main, Plate/Skin
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