N215WE
Registered owner: INTERNATIONAL TRADING COMPANY OF YUKON INC, OK (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
39 reports on file, 2012-05-21 – 2025-10-24.
Part: BEAM — CORRODED (ZONE 300) · corrosion level 2 · airframe 43,469 hrs · 25,021 cycles
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.
Part: SKIN PANEL — DAMAGED (ZONE 300) · airframe 43,469 hrs · 25,021 cycles
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
Part: FRAME — PUNCTURED (ZONE 100) · airframe 43,469 hrs · 25,021 cycles
FUSELAGE FRAME INNER CHORD PUNCTURED AT BS 1090 BETWEEN STRINGER 26L AND 28L
Part: FRAME — PUNCTURED (ZONE 100) · airframe 43,469 hrs · 25,021 cycles
FUSELAGE FRAME INNER CHORD PUNCTURED AT BS 1070 BETWEEN STRINGER 26L AND 29L
Part: FRAME — DENTED (ZONE 200) · airframe 43,469 hrs · 25,021 cycles
FUSELAGE FRAME INNER CHORD DENTS AT BS 1130 BETWEEN STRINGER 24R AND 28R
Part: SKIN PANEL — DAMAGED (ZONE 300) · airframe 43,469 hrs · 25,021 cycles
R/H HORIZONTAL STABILIZER UPPER T/E DAMAGED PANEL 65-20659-24 BETWEEN ELEV. STA. 99.79 AND 173.21
Part: FRAME — PUNCTURED (ZONE 200) · airframe 43,469 hrs · 25,021 cycles
FUSELAGE FRAME INNER CHORD SCREW DAMAGE AT BS 1110 BETWEEN STRINGER 25R AND 28R.
Part: FRAME — GOUGED (ZONE 100) · airframe 43,469 hrs · 25,021 cycles
FUSELAGE FRAME INNER CHORD GOUGED AT BS 1110 BETWEEN STRINGER 26L AND 28L
Part: FRAME — DENTED (ZONE 200) · airframe 43,469 hrs · 25,021 cycles
FUSELAGE FRAME INNER CHORD DENTED AT BS 1050 BETWEEN STRINGER 25L AND 28L
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,469 hrs · 25,021 cycles
FUSELAGE FLOOR STABILIZER BEAM MULTIPLE SPOTS CORROSION AT BL 0 BETWEEN BS 449.94 AND BS 720+9.94
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,469 hrs · 25,021 cycles
FUSELAGE TRANSVERSE FLOOR BEAM UPPER FLANGE CORROSION DAMAGE AT BS 740 BETWEEN LBL 45 AND LBL 62
Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,469 hrs · 25,021 cycles
FUSELAGE FRAME BOTTOM CHORD CORROSION DAMAGE AT BS 970 BETWEEN STRINGER 28R AND 29R.
Part: FRAME — DENTED (ZONE 200) · airframe 43,469 hrs · 25,021 cycles
FUSELAGE FRAME INNER CHORD DENT AT BS 1148 BETWEEN STRINGER 25R AND 28R
Part: FRAME — DENTED (ZONE 100) · airframe 43,469 hrs · 25,021 cycles
FUSELAGE FRAME INNER CHORD DENT AT BS 1070 BETWEEN STRINGER 25R AND 29R
Part: FRAME — CRACKED (ZONE 200) · airframe 43,469 hrs · 25,021 cycles
FUSELAGE FRAME INNER CHORD CRACK AT BS 640 BETWEEN STRINGER 28L AND 27R
Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,469 hrs · 25,021 cycles
FUSELAGE FRAME BOTTOM CHORD CORROSION DAMAGE AT BS 970 BETWEEN STRINGER 28R AND 29R
Part: FRAME — DENTED (ZONE 100) · airframe 43,469 hrs · 25,021 cycles
FUSELAGE FRAME INNER CHORD DENT AT BS 1050 BETWEEN STRINGER 26R AND 28R
Part: SKIN PANEL — DAMAGED (ZONE 300) · airframe 43,469 hrs · 25,021 cycles
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.
Part: FRAME — GOUGED (ZONE 100) · airframe 43,469 hrs · 25,021 cycles
FUSELAGE FRAME INNER CHORD GOUGED AT BS 1130 BETWEEN STRINGER 26L AND 28L
Part: FRAME — CRACKED (ZONE 200) · airframe 43,469 hrs · 25,021 cycles
FUSELAGE FRAME INNER CHORD CRACK AT BS 660 BETWEEN STRINGER 27L AND 27R
Part: FRAME — PUNCTURED (ZONE 200) · airframe 43,469 hrs · 25,021 cycles
FUSELAGE FRAME INNER CHORD SCREW DAMAGE AT BS 1090 BETWEEN STRINGER 26R AND 28R
Part: SKIN — DENTED (ZONE 100) · airframe 43,469 hrs · 25,021 cycles
FUSELAGE SKIN GOUGE/DENT REPAIRED BELOW MCD BETWEEN BS 460 AND BS 620, AND BETWEEN STRINGER 15L-20L
Earlier reports · 2012–2023 · 17 reports
2023
Part: GEARBOX — LEAKING (ZONE 400) · airframe 42,019 hrs · 24,326 cycles
#2 ENGINE PRECAUTIONARY SHUTDOWN DUE TO LOW OIL PRESSURE. FOUND LOOSE FASTENER ON MAIN ACCESORY GEARBOX CAUSING OIL LOSS.
Part: STUB FRAME — DAMAGED (ZONE 200) · airframe 41,938 hrs · 24,287 cycles
MISSDRILLED HOLES IN VERTICAL FLANGE OF LEFT STUB BEAM LOWER CHORD PART NUMBER 65-86355-3 AT STATION 783.95
Part: FRAME — SCRATCHED (ZONE 200) · airframe 41,938 hrs · 24,287 cycles
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
2020
Part: PROXIMITY SENSOR — INTERMITTENT (MLG) · airframe 40,456 hrs · 23,562 cycles
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 MECHANICAL POINTER.
Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 40,401 hrs · 23,528 cycles
CORROSION ON WING CENTER SECTION FRONT SPAR LOWER CHORD BETWEEN LBL 3.25 AND RBL 10.25.
Part: FLOORBEAM — CORRODED (BS 950D) · corrosion level 2 · airframe 40,401 hrs · 23,528 cycles
CORROSION ON FLOOR BEAM LOWER FLANGE AT STATION 950D LBL 20.
2018
Part: LOCKING PLATE — CORRODED (HORIZONTAL STAB) · airframe 38,795 hrs · 22,691 cycles
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.
2015
Part: WEB — CRACKED (ELEVATOR) · airframe 37,173 hrs · 21,772 cycles
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.
Part: A/C PACK — OVERHEATED (AC BAY) · airframe 37,127 hrs · 21,743 cycles
AIR CONDITIONING PACK OVERHEAT.
2014
Part: SKIN — DENTED (FUSELAGE) · airframe 36,217 hrs · 21,245 cycles
FUSELAGE SKIN DENTED BETWEEN STATIONS 344 & 351 LT ABOVE STRINGER 19L.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 36,217 hrs · 21,245 cycles
SUSPECTED LIGHTNING STRIKE ON RIVET AT STATION 680, STRINGER 3L RESULTING IN FUSELAGE SKIN DAMAGE.
2012
Part: SILL — CORRODED (BS 500-520) · airframe 34,162 hrs · 22,936 cycles
CORROSION ON MAIN CARGO DOOR SILL.
Part: KEELBEAM — CORRODED (BS 740 S28L/R) · airframe 34,162 hrs · 22,936 cycles
CORROSION ON LWR INBD FLANGE OF STR 28R AND 28L FWD OF DELTA KEEL AT STA 740.
Part: FLOORBEAM — CORRODED (BS 537) · airframe 34,162 hrs · 22,936 cycles
CORROSION ON FWD CARGO PIT FLOOR SUPPORT STA 537 RBL8 AND RBL13.
Part: FRAME — CORRODED (BS 228) · airframe 34,162 hrs · 22,936 cycles
CORROSION ON FRAME BS 228 RBL 4 - LBL 4 INSIDE FWD ACCESS FOUND BEYOND LIMITS.
Part: WEB — DAMAGED (BS 1130) · airframe 34,162 hrs · 22,936 cycles
DAMAGED FLOOR WEB AT BS 1130, RBL 24 UNDER SEAT TRACK ON MAIN CARGO DECK.
Part: KEEL — CORRODED (BS 740) · airframe 34,162 hrs · 22,936 cycles
CORROSION ON KEEL LT SIDE BESIDE STA 740.