N527AS

Service difficulty reports · 59

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 = 'N527AS' 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 ASAA2015030310867Skin · crackedCRACK FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN. CRACK IS JUST INBD OF STABILIZER STA 147.9, APPROXIMATELY 9.25' FWD OF REAR SPAR AND IS APPROXIMATELY 0.875' LONG. NOTE: CRACKS .875, .906, .5. ACFT GROUNDED. FABRICATED & INSTALLED REPAIR ON LOWER STABMar 3, 2015 · N527AS · Boeing 737890 · Horizontal Stabilizer, Spar/RibSDR ASAA2015030310853Skin · crackedCRACK FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN. CRACK IS JUST INBD OF STABILIZER STA 101.9, APPROX 19.5' FWD OF REAR SPAR AND IS APPROXIMATELY 1' LONG. ACFT GROUNDED. REPAIRED CRACKED SKIN AT STAB STA 101.9, 19.5" FWD OF AFT SPAR AND 10.25" FWD OF AFT Mar 3, 2015 · N527AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2015030310852Skin · crackedCRACK FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN JUST INBD OF STABILIZER STA 129.5 APPROXIMATELY 8.75' AFT OF FWR SPAR. CRACK IS APPROX 0.765' LONG. ACFT GROUNDED. REPAIRED CRACKED SKIN AT LT STABILIZER LOWER SKIN STABILIZER STA 12935, 8.75" AFT OF FWD SPMar 3, 2015 · N527AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2014082709071Plate · corrodedFORWARD CARGO BAY AFT BULKHEAD LT SIDEPLATE CORRODED. BS 500H- 500I, S23-24L. ACFT GROUNDED. CORROSION REMOVED IAW SRM 53-00-53-2R-5. FOUND OUT OF LIMITS AND WAS REMOVED IAW SRM 51-40-02. FABRICATED NEW SIDEPLATE AND REPAIR DOUBLER IAW DWG BAC1496-444Aug 27, 2014 · N527AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2014082609086Transition Panel · corrodedAFT CARGO BAY TRANSITION PANEL CORRODED BS 727-727D, RBL 24. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE TRANSITION PANEL IAW SRM 53-00-53-2R-5.Aug 26, 2014 · N527AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2014072308666Skin · crackedRT HORIZONTAL STABILIZER LWR SURFACE HAS ONE CRACK IN SKIN. ACFT GROUNDED. VERIFIED 1EA CRACK RT HORIZONTAL STABILIZER HFEC NDT PART 6 51-00-00 PROCEED 23. 23 ENDS OF CRACK MARKED. REMOVED RT HORIZ L/E AND TIP CAP REF MM 27-21-000-801. REMOVED FASTENERS INJul 23, 2014 · N527AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2014072308665Skin · crackedLEFT HORIZONTAL STABILIZER LWR SURFACE HAS TWO CRACKS IN SKIN. ACFT GROUNDED. VERIFIED 2 EA CRACKS LT HS HFEC PART 6 -51-00-00 PROCEED 23 ENDS OF CRACK MARKED. LT STAB L/E REMOVED IAW MM 27-41-21-000-801. REPAIRED LT HORIZONTAL STABILIZER LWR SURFACE IAW 55Jul 23, 2014 · N527AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2014022807041Starter · failedBLINKING NR 1 ENGINE OIL QTY READ 3, NR 2 NORMAL, NO LOW OIL PRESS LT ON MASTER CAUTION. WENT TO CHECKLIST, RETARDED THROTTLE AFTER 5-10 MIN OIL QTY WENT TO 2, OIL PRESSURE DROPPED, OIL TEMP ROSE. SHUTDOWN ENGINE WITH 2 QTS ON OIL QTY. ACFT GROUNDED. REMOVEDFeb 28, 2014 · N527AS · Boeing 737890 · Engine StarterSDR ASAA12511045Guide Arm · out of adjustFWD SERVICE DOOR (R1) WILL NOT PROPERLY CLOSE. ADJUSTED (R1) DOOR GUIDE ARM REF MM 52 41 00 820 801 STEP I. (1). DOOR OPERATION NORMAL REF MM 52 41 00 700 801.Feb 4, 2012 · N527AS · Boeing 737890 · Passenger/Crew Doors
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