N951AT

Service difficulty reports · 209

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 = 'N951AT' 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 ZZDA2010188Bracket · corrodedRIGHT FLOOR WEB BRACKET, STA 565, LONG L18R, CORROSION. ACCOMPLISHED FLOOR WEB BRACKET REPLACEMENT PER B717 SRM 51-41-02.Jan 21, 2010 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR ZZDA2010029Floor Support · corrodedCABIN FLOOR SUPPORT BEAM, STA 1022 TO 1053, RBL 16, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM BLENDING WITHIN LIMITS PER B717 SRM 51-10-04.Jan 21, 2010 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR ZZDA2010028Floor Support · corrodedCABIN FLOOR SUPPORT BEAM, STA 1022 TO 1053, LBL 16, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM BLENDING WITHIN LIMITS PER B717 SRM 51-10-04.Jan 21, 2010 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR ZZDA2010182Splice · unknownFWD CARGO DOOR SEAL DEPRESSOR SPLICES. ACCOMPLISHED SEAL DEPRESSOR SPLICES REPLACEMENT PER B717 SRM 51-41-01.Jan 19, 2010 · N951AT · Boeing 717200 · Cargo/Baggage DoorsSDR AT0700079Sill · corrodedFWD CARGO PIT DOOR SILL AREA, HAS AREA'S OF SURFACE CORROSION AND CHIPPED/CRACKED PAINT. INSTALLED FWD CARGO DOOR CUTOUT LOWER JAMB PAN REPAIR IAW B717 SRM 53-20-15 REPAIR 6.May 22, 2006 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR AT0700077Vent · crackedAFT FUSELAGE RIGHT HAND VENT BOX REPAIR IS CRACKED. INSTALLED REPAIR OF AFT FUSELAGE RIGHT SIDE VENT BOX DRAIN PAN IAW T/C 17-5320-0223 FIG 1.May 22, 2006 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR AT0700076Frame · crackedAFT FUSELAGE CANTED FRAME AT F/A 1178 CRACKED AT LONGERON 16 LEFT. INSTALLED DOUBLER REPAIR AT LEFT HAND CANTED FRAME AT STA 1178 LONGERON 18L IAW B717 SRM 51-70311 FIG 201 PAGE 203. MATERIAL USED 0.080" 7075-0, 13 X 2.5 INCHES. HEAT TREATED TO T6 IAW AVBORMay 22, 2006 · N951AT · Boeing 717200 · Fuselage Main, FrameSDR AT0700078Skin · damagedFS 248 AT L18L HAS SMOOTH DENT WITH NO INTERNAL DAMAGE, NO LOOSE OR PULLED FASTENERS. MEASURES 2.5 X 2.5 X .048 INCH. CONDITION 2 WITH D/X 52.08. DENT IS ON L18L, PER RES 05-1279 REQUIRES HFEC OR DYE PENATRENT EVERY 500 HRS. INSTALLED DOUBLER REPAIR AT FS 2Oct 24, 2005 · N951AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR AT0200070Eec · failedIN CRUISE AT FL330 .771 M RIGHT ENGINE WENT TO IDLE - ENG R SYS FAIL ILLUMINATED, SELECT FADEC ALT DISPLAY, SELECTED NO CHANGE SHUT ENGINE DOWN. ALL OTHER INDICATIONS NORMAL. EPR INDICATION DISPLAYED A -X-. DIVERTED TO SAV. REMOVED AND REPLACED NR 2 ENGINEJul 9, 2002 · N951AT · Boeing 717200 · Fuel Control/Turbine Engines
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