# Service difficulty reports: N215WE A list on [N215WE](https://openairdocs.org/aircraft/N215WE.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR VGCA20260917001](https://openairdocs.org/sdr/VGCA20260917001.md): Engine · making metal · Sep 17, 2026 · N215WE · Boeing 7272S2F · Engine (Turbine/Turboprop) > ENGINE OIL BYPASS INDICATION. METAL IN OIL FILTER - [SDR VGCA20251024009](https://openairdocs.org/sdr/VGCA20251024009.md): Skin Panel · damaged · Oct 24, 2025 · N215WE · Boeing 7272S2F · Elevator, Plate/Skin > R/H HORIZONTAL STABILIZER UPPER T/E DAMAGED PANEL 65-20659-24 BETWEEN ELEV. STA. 99.79 AND 173.21 - [SDR VGCA20251024020](https://openairdocs.org/sdr/VGCA20251024020.md): Frame · punctured · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame > FUSELAGE FRAME INNER CHORD SCREW DAMAGE AT BS 1110 BETWEEN STRINGER 25R AND 28R. - [SDR VGCA20251024019](https://openairdocs.org/sdr/VGCA20251024019.md): Frame · punctured · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame > FUSELAGE FRAME INNER CHORD SCREW DAMAGE AT BS 1090 BETWEEN STRINGER 26R AND 28R - [SDR VGCA20251024018](https://openairdocs.org/sdr/VGCA20251024018.md): Frame · dented · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame > FUSELAGE FRAME INNER CHORD DENT AT BS 1070 BETWEEN STRINGER 25R AND 29R - [SDR VGCA20251024017](https://openairdocs.org/sdr/VGCA20251024017.md): Frame · dented · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame > FUSELAGE FRAME INNER CHORD DENT AT BS 1050 BETWEEN STRINGER 26R AND 28R - [SDR VGCA20251024016](https://openairdocs.org/sdr/VGCA20251024016.md): Floorbeam · corroded · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Floor Beam > FUSELAGE FLOOR STABILIZER BEAM MULTIPLE SPOTS CORROSION AT BL 0 BETWEEN BS 449.94 AND BS 720+9.94 - [SDR VGCA20251024015](https://openairdocs.org/sdr/VGCA20251024015.md): Frame · gouged · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame > FUSELAGE FRAME INNER CHORD GOUGED AT BS 1130 BETWEEN STRINGER 26L AND 28L - [SDR VGCA20251024014](https://openairdocs.org/sdr/VGCA20251024014.md): Frame · gouged · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame > FUSELAGE FRAME INNER CHORD GOUGED AT BS 1110 BETWEEN STRINGER 26L AND 28L - [SDR VGCA20251024013](https://openairdocs.org/sdr/VGCA20251024013.md): Frame · punctured · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame > FUSELAGE FRAME INNER CHORD PUNCTURED AT BS 1090 BETWEEN STRINGER 26L AND 28L - [SDR VGCA20251024012](https://openairdocs.org/sdr/VGCA20251024012.md): Skin · dented · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Plate/Skin > FUSELAGE SKIN GOUGE/DENT REPAIRED BELOW MCD BETWEEN BS 460 AND BS 620, AND BETWEEN STRINGER 15L-20L - [SDR VGCA20251024011](https://openairdocs.org/sdr/VGCA20251024011.md): Frame · punctured · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame > FUSELAGE FRAME INNER CHORD PUNCTURED AT BS 1070 BETWEEN STRINGER 26L AND 29L - [SDR VGCA20251024010](https://openairdocs.org/sdr/VGCA20251024010.md): Shear Tie · corroded · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Internal Mounting Structure > FUSELAGE FRAME BOTTOM CHORD CORROSION DAMAGE AT BS 970 BETWEEN STRINGER 28R AND 29R. - [SDR VGC2025F00000](https://openairdocs.org/sdr/VGC2025F00000.md): Frame · corroded · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame > FUSELAGE FRAME BOTTOM CHORD CORROSION DAMAGE AT BS 970 BETWEEN STRINGER 28R AND 29R - [SDR VGCA202511254009](https://openairdocs.org/sdr/VGCA202511254009.md): Skin Panel · damaged · Oct 24, 2025 · N215WE · Boeing 7272S2F · Horizontal Stabilizer, Plate/Skin > R/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 03.2025 - [SDR VGCA202511254008](https://openairdocs.org/sdr/VGCA202511254008.md): Skin Panel · damaged · Oct 24, 2025 · N215WE · Boeing 7272S2F · Elevator, Plate/Skin > RIGHT 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 VGCA20251024007](https://openairdocs.org/sdr/VGCA20251024007.md): Beam · corroded · Oct 24, 2025 · N215WE · Boeing 7272S2F · Horizontal Stabilizer Miscellaneous Structure > R/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 VGCA20251024006](https://openairdocs.org/sdr/VGCA20251024006.md): Floorbeam · corroded · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Floor Beam > FUSELAGE TRANSVERSE FLOOR BEAM UPPER FLANGE CORROSION DAMAGE AT BS 740 BETWEEN LBL 45 AND LBL 62 - [SDR VGCA20251024005](https://openairdocs.org/sdr/VGCA20251024005.md): Frame · dented · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame > FUSELAGE FRAME INNER CHORD DENTED AT BS 1050 BETWEEN STRINGER 25L AND 28L - [SDR VGCA20251024004](https://openairdocs.org/sdr/VGCA20251024004.md): Frame · cracked · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame > FUSELAGE FRAME INNER CHORD CRACK AT BS 660 BETWEEN STRINGER 27L AND 27R - [SDR VGCA20251024003](https://openairdocs.org/sdr/VGCA20251024003.md): Frame · cracked · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame > FUSELAGE FRAME INNER CHORD CRACK AT BS 640 BETWEEN STRINGER 28L AND 27R - [SDR VGCA20251024002](https://openairdocs.org/sdr/VGCA20251024002.md): Frame · dented · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame > FUSELAGE FRAME INNER CHORD DENT AT BS 1148 BETWEEN STRINGER 25R AND 28R - [SDR VGCA20251024001](https://openairdocs.org/sdr/VGCA20251024001.md): Frame · dented · Oct 24, 2025 · N215WE · Boeing 7272S2F · Fuselage Main, Frame > FUSELAGE FRAME INNER CHORD DENTS AT BS 1130 BETWEEN STRINGER 24R AND 28R - [SDR VGCA20230323001](https://openairdocs.org/sdr/VGCA20230323001.md): Gearbox · leaking · Mar 23, 2023 · N215WE · Boeing 7272S2F · Engine Oil Pressure > #2 ENGINE PRECAUTIONARY SHUTDOWN DUE TO LOW OIL PRESSURE. FOUND LOOSE FASTENER ON MAIN ACCESORY GEARBOX CAUSING OIL LOSS. - [SDR VGCA20230213002](https://openairdocs.org/sdr/VGCA20230213002.md): Stub Frame · damaged · Feb 13, 2023 · N215WE · Boeing 7272S2F · Fuselage Main, Frame > MISSDRILLED HOLES IN VERTICAL FLANGE OF LEFT STUB BEAM LOWER CHORD PART NUMBER 65-86355-3 AT STATION 783.95 - [SDR VGCA20230213001](https://openairdocs.org/sdr/VGCA20230213001.md): Frame · scratched · Feb 13, 2023 · N215WE · Boeing 7272S2F · Fuselage Main, Frame > DAMAGED HOLE / DEEP SCRATCH AT THE LOWEST HOLE OF THE INBOARD CHORD OF THE LH FRAME PART NUMBER 65-16326-139 AT STATION 783.95 - [SDR VGCA20201028001](https://openairdocs.org/sdr/VGCA20201028001.md): Proximity Sensor · intermittent · Oct 28, 2020 · N215WE · Boeing 7272S2F · Landing Gear Position and Warning > DURING 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 MECHANIC - [SDR VGCA202009098302](https://openairdocs.org/sdr/VGCA202009098302.md): Floorbeam · corroded · Aug 31, 2020 · N215WE · Boeing 7272S2F · Fuselage Main, Floor Beam > CORROSION ON FLOOR BEAM LOWER FLANGE AT STATION 950D LBL 20. - [SDR VGCA2020090983101](https://openairdocs.org/sdr/VGCA2020090983101.md): Spar · corroded · Aug 31, 2020 · N215WE · Boeing 7272S2F · Wing Spar > CORROSION ON WING CENTER SECTION FRONT SPAR LOWER CHORD BETWEEN LBL 3.25 AND RBL 10.25. - [SDR VGCA20180108001](https://openairdocs.org/sdr/VGCA20180108001.md): Locking Plate · corroded · Jan 8, 2018 · N215WE · Boeing 7272S2F · Horizontal Stabilizer Structure > WHILE 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 VGCA20150526001](https://openairdocs.org/sdr/VGCA20150526001.md): Web · cracked · May 26, 2015 · N215WE · Boeing 7272S2F · Elevator Miscellaneous Structure > DURING 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 VGCA20150413001](https://openairdocs.org/sdr/VGCA20150413001.md): A/C Pack · overheated · Apr 13, 2015 · N215WE · Boeing 7272S2F · Cabin Cooling System > AIR CONDITIONING PACK OVERHEAT. - [SDR VGCA20140609001](https://openairdocs.org/sdr/VGCA20140609001.md): Skin · dented · Jun 9, 2014 · N215WE · Boeing 7272S2F · Fuselage Main, Plate/Skin > FUSELAGE SKIN DENTED BETWEEN STATIONS 344 & 351 LT ABOVE STRINGER 19L. - [SDR VGCA20140605001](https://openairdocs.org/sdr/VGCA20140605001.md): Skin · damaged · Jun 5, 2014 · N215WE · Boeing 7272S2F · Fuselage Main, Plate/Skin > SUSPECTED LIGHTNING STRIKE ON RIVET AT STATION 680, STRINGER 3L RESULTING IN FUSELAGE SKIN DAMAGE. - [SDR VGCA20120521006](https://openairdocs.org/sdr/VGCA20120521006.md): Keelbeam · corroded · May 21, 2012 · N215WE · Boeing 7272S2F · Fuselage Main, Keel > CORROSION ON LWR INBD FLANGE OF STR 28R AND 28L FWD OF DELTA KEEL AT STA 740. - [SDR VGCA20120521005](https://openairdocs.org/sdr/VGCA20120521005.md): Floorbeam · corroded · May 21, 2012 · N215WE · Boeing 7272S2F · Fuselage Main, Floor Beam > CORROSION ON FWD CARGO PIT FLOOR SUPPORT STA 537 RBL8 AND RBL13. - [SDR VGCA20120521004](https://openairdocs.org/sdr/VGCA20120521004.md): Keel · corroded · May 21, 2012 · N215WE · Boeing 7272S2F · Fuselage Main, Keel > CORROSION ON KEEL LT SIDE BESIDE STA 740. - [SDR VGCA20120521003](https://openairdocs.org/sdr/VGCA20120521003.md): Web · damaged · May 21, 2012 · N215WE · Boeing 7272S2F · Fuselage Miscellaneous Structure > DAMAGED FLOOR WEB AT BS 1130, RBL 24 UNDER SEAT TRACK ON MAIN CARGO DECK. - [SDR VGCA20120521002](https://openairdocs.org/sdr/VGCA20120521002.md): Frame · corroded · May 21, 2012 · N215WE · Boeing 7272S2F · Fuselage Main, Frame > CORROSION ON FRAME BS 228 RBL 4 - LBL 4 INSIDE FWD ACCESS FOUND BEYOND LIMITS. - [SDR VGCA20120521001](https://openairdocs.org/sdr/VGCA20120521001.md): Sill · corroded · May 21, 2012 · N215WE · Boeing 7272S2F · Fuselage Miscellaneous Structure > CORROSION ON MAIN CARGO DOOR SILL. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/aircraft/N215WE/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.