N215WE
Service difficulty reports · 40
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 = 'N215WE' 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.
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 = 'N215WE' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR VGCA20260917001Engine · making metalENGINE OIL BYPASS INDICATION. METAL IN OIL FILTERSDR VGCA20251024009Skin Panel · damagedR/H HORIZONTAL STABILIZER UPPER T/E DAMAGED PANEL 65-20659-24 BETWEEN ELEV. STA. 99.79 AND 173.21SDR VGCA20251024020Frame · puncturedFUSELAGE FRAME INNER CHORD SCREW DAMAGE AT BS 1110 BETWEEN STRINGER 25R AND 28R.SDR VGCA20251024019Frame · puncturedFUSELAGE FRAME INNER CHORD SCREW DAMAGE AT BS 1090 BETWEEN STRINGER 26R AND 28RSDR VGCA20251024018Frame · dentedFUSELAGE FRAME INNER CHORD DENT AT BS 1070 BETWEEN STRINGER 25R AND 29RSDR VGCA20251024017Frame · dentedFUSELAGE FRAME INNER CHORD DENT AT BS 1050 BETWEEN STRINGER 26R AND 28RSDR VGCA20251024016Floorbeam · corrodedFUSELAGE FLOOR STABILIZER BEAM MULTIPLE SPOTS CORROSION AT BL 0 BETWEEN BS 449.94 AND BS 720+9.94SDR VGCA20251024015Frame · gougedFUSELAGE FRAME INNER CHORD GOUGED AT BS 1130 BETWEEN STRINGER 26L AND 28LSDR VGCA20251024014Frame · gougedFUSELAGE FRAME INNER CHORD GOUGED AT BS 1110 BETWEEN STRINGER 26L AND 28LSDR VGCA20251024013Frame · puncturedFUSELAGE FRAME INNER CHORD PUNCTURED AT BS 1090 BETWEEN STRINGER 26L AND 28LSDR VGCA20251024012Skin · dentedFUSELAGE SKIN GOUGE/DENT REPAIRED BELOW MCD BETWEEN BS 460 AND BS 620, AND BETWEEN STRINGER 15L-20LSDR VGCA20251024011Frame · puncturedFUSELAGE FRAME INNER CHORD PUNCTURED AT BS 1070 BETWEEN STRINGER 26L AND 29LSDR VGCA20251024010Shear Tie · corrodedFUSELAGE FRAME BOTTOM CHORD CORROSION DAMAGE AT BS 970 BETWEEN STRINGER 28R AND 29R.SDR VGC2025F00000Frame · corrodedFUSELAGE FRAME BOTTOM CHORD CORROSION DAMAGE AT BS 970 BETWEEN STRINGER 28R AND 29RSDR VGCA202511254009Skin Panel · damagedR/H HORIZONTAL STABILIZER UPPER T/E DAMAGED PANELS 65-20659-24 BETWEEN ELEV. STA. 99.79 AND 173.21 REPAIRED AND INSTALLED I.A.W. V1 AEROSPACE DOC. NO. R24-02464-001, REVISION 6 ,DATE OCTOBER 03.2025SDR VGCA202511254008Skin Panel · damagedRIGHT HORIZONTAL STABILIZER UPPER T/E DAMAGED PANELS 65-20658-24 BETWEEN ELEV. STA. 99.79 AND 173.21 REPAIRED AND INSTALLED IAW. R24-02464-001, REVISION 6 ,DATE OCTOBER 03.2025.SDR VGCA20251024007Beam · corrodedR/H SIDE H-STAB. TRAILING EDGE BEAM UPPER SURFACE CORROSION REPAIRED BY REPLACEMENT OF R/H TRAILING EDGE UPPER BEAM ENTIRE LENGTH BETWEEN ELEVATOR STATION 10 AND ELEVATOR STATION 209.90 I.A.W BOEING DRAWING 65-22987, SHEET 5, REVISION C.SDR VGCA20251024006Floorbeam · corrodedFUSELAGE TRANSVERSE FLOOR BEAM UPPER FLANGE CORROSION DAMAGE AT BS 740 BETWEEN LBL 45 AND LBL 62SDR VGCA20251024005Frame · dentedFUSELAGE FRAME INNER CHORD DENTED AT BS 1050 BETWEEN STRINGER 25L AND 28LSDR VGCA20251024004Frame · crackedFUSELAGE FRAME INNER CHORD CRACK AT BS 660 BETWEEN STRINGER 27L AND 27RSDR VGCA20251024003Frame · crackedFUSELAGE FRAME INNER CHORD CRACK AT BS 640 BETWEEN STRINGER 28L AND 27RSDR VGCA20251024002Frame · dentedFUSELAGE FRAME INNER CHORD DENT AT BS 1148 BETWEEN STRINGER 25R AND 28RSDR VGCA20251024001Frame · dentedFUSELAGE FRAME INNER CHORD DENTS AT BS 1130 BETWEEN STRINGER 24R AND 28RSDR VGCA20230323001Gearbox · leaking#2 ENGINE PRECAUTIONARY SHUTDOWN DUE TO LOW OIL PRESSURE. FOUND LOOSE FASTENER ON MAIN ACCESORY GEARBOX CAUSING OIL LOSS.SDR VGCA20230213002Stub Frame · damagedMISSDRILLED HOLES IN VERTICAL FLANGE OF LEFT STUB BEAM LOWER CHORD PART NUMBER 65-86355-3 AT STATION 783.95SDR VGCA20230213001Frame · scratchedDAMAGED HOLE / DEEP SCRATCH AT THE LOWEST HOLE OF THE INBOARD CHORD OF THE LH FRAME PART NUMBER 65-16326-139 AT STATION 783.95SDR VGCA20201028001Proximity Sensor · intermittentDURING APPROACH WITH THE GEAR SELECTED DOWN, LEFT GEAR UNSAFE LIGHT ILLUMINATED WITH NO GREEN LIGHT. NOSE AND RIGHT GEAR INDICATE SAFE. DOORS LIGHT INDICATES NORMAL. MANUAL CRANKING OF THE LEFT GEAR WAS NORMAL AND INDICATED DOWN AND LOCKED WITH THE MECHANICSDR VGCA202009098302Floorbeam · corrodedCORROSION ON FLOOR BEAM LOWER FLANGE AT STATION 950D LBL 20.SDR VGCA2020090983101Spar · corrodedCORROSION ON WING CENTER SECTION FRONT SPAR LOWER CHORD BETWEEN LBL 3.25 AND RBL 10.25.SDR VGCA20180108001Locking Plate · corrodedWHILE GAINING ACCESS TO PERFORM AD 2008-22-12F, FOUND THE HORIZONTAL STABILIZER HINGE BEARING RETAINER LOCKING PLATE HAD A BROKEN BOLT. REMOVED THE STABILIZER TO REPLACE THE BROKEN BOLT, DISCOVERED SURFACE CORROSION ON RH ATTACH FITTING.SDR VGCA20150526001Web · crackedDURING THE UNRELATED ACCOMPLISHMENT OF AD 2014-21-09 PARAGRAPH H DISCOVERED BOTH LT & RT WEB OF ELEVATOR QUADRANT ASSEMBLIES CRACKED. R & R BOTH WEBS.SDR VGCA20150413001A/C Pack · overheatedAIR CONDITIONING PACK OVERHEAT.SDR VGCA20140609001Skin · dentedFUSELAGE SKIN DENTED BETWEEN STATIONS 344 & 351 LT ABOVE STRINGER 19L.SDR VGCA20140605001Skin · damagedSUSPECTED LIGHTNING STRIKE ON RIVET AT STATION 680, STRINGER 3L RESULTING IN FUSELAGE SKIN DAMAGE.SDR VGCA20120521006Keelbeam · corrodedCORROSION ON LWR INBD FLANGE OF STR 28R AND 28L FWD OF DELTA KEEL AT STA 740.SDR VGCA20120521005Floorbeam · corrodedCORROSION ON FWD CARGO PIT FLOOR SUPPORT STA 537 RBL8 AND RBL13.SDR VGCA20120521004Keel · corrodedCORROSION ON KEEL LT SIDE BESIDE STA 740.SDR VGCA20120521003Web · damagedDAMAGED FLOOR WEB AT BS 1130, RBL 24 UNDER SEAT TRACK ON MAIN CARGO DECK.SDR VGCA20120521002Frame · corrodedCORROSION ON FRAME BS 228 RBL 4 - LBL 4 INSIDE FWD ACCESS FOUND BEYOND LIMITS.SDR VGCA20120521001Sill · corrodedCORROSION ON MAIN CARGO DOOR SILL.
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