N216WE
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.
43 reports on file, 2012-01-09 – 2025-08-05.
Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles
CENTER FUSELAGE SECTION RH DELTA BEAM LOWER CHORD CORRODED FROM BS720F-755 AND S-27L TO S-27R
Part: SKIN PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles
AFT LOWER FUSELAGE SKIN PANEL CORROSION FROM BS1148-1166 AND S-18L TO S-20L.
Part: SKIN PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles
AFT LOWER FUSELAGE SKIN CORROSION FROM BS990-1010 AT S-26L
Part: FRAME — CRACKED (ZONE 100) · airframe 44,542 hrs · 25,488 cycles
FT LOWER FUSELAGE FRAME CRACKED AT BS1070 FROM S-26R TO S-28R
Part: FRAME — PUNCTURED (ZONE 100) · airframe 44,542 hrs · 25,488 cycles
AFT LOWER FUSELAGE FRAME INNER CHORD PUNCTURE AT BS1090 FROM S-24L TO S-28L
Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles
CORROSION AT MULTIPLE LOCATIONS AT A-NUT ATTACHMENTS. FORWARD LOWER FUSELAGE LONGITUDINAL STABILIZER LOWER CHORD REPAIRED AT BL0 FROM BS450-660
Part: SKIN — CRACKED (ZONE 600) · airframe 44,542 hrs · 25,488 cycles
CRACKED AT THE SLAT HOOK CUT-OUT IN THE AFT CORNER. AT WS 519 ON THE RIGHT WING
Part: FRAME — DENTED (ZONE 100) · airframe 44,542 hrs · 25,488 cycles
AFT LOWER FUSELAGE FRAME INNER CHORD DENTED AT BS1110 FROM S-24L TO S-28L
Part: FRAME — PUNCTURED (ZONE 100) · airframe 44,542 hrs · 25,488 cycles
AFT LOWER FUSELAGE FRAME INNER CHORD PUNCTURE AT BS1130 FROM S-25L TO S-29L.
Part: FRAME — PUNCTURED (ZONE 100) · airframe 44,542 hrs · 25,488 cycles
AFT LOWER FUSELAGE FRAME INNER CHORD PUNCTURE AT BS1148 FROM S-25R TO S-28R.
Part: SPAR WEB — ELONGATED (ZONE 500) · airframe 44,542 hrs · 25,488 cycles
ELONGATED HOLE ON VERTICAL STIFFENER WEB IN CENTER FUEL TANK FRONT SPAR AT LBL40
Part: FRAME — MISREPAIRED (ZONE 100) · airframe 44,542 hrs · 25,488 cycles
NON-PRODUCTION FASTENERS INSTALLED .AFT LOWER FUSELAGE FRAME REPAIRED AT BS1050 FROM S-25L TO S-28L
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles
AFT UPPER FUSELAGE TRANSVERSE FLOOR BEAM UPPER CHORD CORROSION AT BS1148 FROM LBL45 TO LBL55
Part: VERTICAL BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles
VERTICAL BEAM CORRODED AT LOWER END. REPAIRED AT BL 0 BS 1183.
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles
CORROSION ON FUSELAGE SKIN AT BS1028 TO 1055 AND S-29L TO S-29R
Part: FLAP TRACK — CRACKED (ZONE 500) · airframe 44,542 hrs · 25,488 cycles
CRACK FOUND ON LEFT WING OUTBOARD TRAILING EDGE FLAP, OUTBOARD FLAP TRACK. CRACK WAS IN UPPER FLANGE INBOARD FLANGE.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles
AFT UPPER FUSELAGE TRANSVERSE FLOOR BEAM UPPER CHORD CORRODED AT BS1030 FROM LBL10 TO LBL20.
Part: FASTENER — WRONG PART (ZONE 100) · airframe 44,542 hrs · 25,488 cycles
NONPRODUCTION FASTENER INSTALLED @ AFT LOWER FUSELAGE FRAME REPAIRED AT BS1166 FROM S-25L TO S-28L
Part: NONE — NONE (NONE) · airframe 44,542 hrs · 25,488 cycles
BMS3-27 IS NO LONGER PROCURABLE. BOEING SR KFC-GUC-24-0105-09B APPROVED THE USE OF BMS3-38 AS AN ALTERNATE.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles
FORWARD UPPER FUSELAGE TRANSVERSE FLOOR BEAM UPPER AND LOWER CHORDS CORROSION AT BS720 FROM LBL65-RBL50
Part: FRAME — CRACKED (ZONE 100) · airframe 44,542 hrs · 25,488 cycles
FORWARD LOWER FUSELAGE FRAME UPPER CHORD CRACKED AT BS700 FROM S-28L TO S-28R
Part: BEAR STRAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles
CORROSION ON BEAR STRAP, DOUBLER, AND FUSLAGE EXTERNAL SKIN AT AFT CONER OF AFT CARGO DOOR FROM FS965 TO FS1010 AND STR S-21R TO S-29L
Part: SPAR — CORRODED (ZONE 300) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles
CORROSION ON RH HORIZONTAL STAB REAR SPAR UPPER CHORD AT STAB STATION 104.25 THRU 123.25 AND 141.5 THRU 160.5
Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles
KEEL BEAM BREATHER WEB CORRODED AT SEVERAL LOCATIONS ON THE UPPER SURFACE FROM BS740 TO 795 AND LBL13 TO RBL13
Part: SHEAR WEB — CRACKED (ZONE 100) · airframe 44,542 hrs · 25,488 cycles
AFT UPPER FUSELAGE FLOOR SHEAR WEB CRACK NEAR BS1166-1176.9 AND RBL8 TO RBL17.87
Part: SPAR — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles
WING CENTER BOX FRONT SPAR CORRODED IN MULTIPLE PLACES ON VERTICAL AND HORIZONTAL CHORD FLANGES AT BS740 FROM LBL70.5 TO RBL70.5
Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles
AFT UPPER FUSELAGE WINDOW FRAMES CORROSION FROM BS950A-950C AND S-10R TO S-14R
Part: FRAME — PUNCTURED (ZONE 100) · airframe 44,542 hrs · 25,488 cycles
FRAME INNER CHORD PUNCTURE AT BS 1090 BETWEEN S26R AND S28R.
Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles
RIGHT OTBD END OF THE SIDELOAD BEAM CORRODED. CENTER FUSELAGE BULKHEAD SIDELOAD BEAM CORRODED AT BS740 FROM LBL30 TO RBL30
Earlier reports · 2012–2021 · 14 reports
2021
Part: NONE — NONE · airframe 43,030 hrs · 24,721 cycles
DURING CLIMB WHILE PASSING THROUGH FL250 THE AIRCRAFT EXPERIENCED A RAPID DECOMPRESSON THAT WAS NOT CONTROLLABLE FROM THE FLIGHT DECK. EMERGENCY DECENT WAS INITATED AND AIRCRAFT RETURNED WITHOUT FURTHER INCIDENT
2020
Part: CABIN PRESSURE — ABNORMAL · airframe 41,953 hrs · 24,219 cycles
LOST CABIN PRESSUURIZATION AT FLIGHT LEVEL 30000, CABIN ALTITUDE WARNING HORN SOUNDED AT 10000 FEET CABIN PRESSURE. UNABLE TO CONTROL CABIN PRESSURE WITH OUTFLOW VALVE CLOSED.
Part: PANEL — DENTED (HORIZ STAB) · airframe 41,829 hrs · 24,161 cycles
HORIZONTAL STABILIZER LH SIDE LEADING EDGE PANEL #9122 REWORKED (BLEND OUT) DENT FOUND BEYOND ALLOWABLE DAMAGE, REPAIRED IN ACCORDANCE WITH B727-200 SRM
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 41,829 hrs · 24,161 cycles
SEAT TRACK FLANGE GOUGED IN MAIN CARGO DECK FLOOR AT BS. 870, LBL 45.5. FOUND BEYOND ALLOWABLE DAMAGE. SEAT TRACK SEGMENT REPLACED IN ACCORDANCE WITH B727 SRM.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 41,829 hrs · 24,161 cycles
SEAT TRACK GOUGED IN MAIN CARGO DEK FLOOR AT BS. 625, RBL 62.5. FOUND BEYOND ALLOWABLE DAMAGE. SEGEMENT OF SEAT TRACK REPLACED IN ACCORDANCE WITH B727 SRM
Part: WEB — CRACKED (FUSELAGE) · airframe 41,829 hrs · 24,161 cycles
WEB TANGS CRACKED AT BS. 600 AND BS 620 BETWEEN STR. 3L AND STR. 4L, ABOVE MAIN CARGO DOOR. PART REPLACEMENT REQUIRED.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 41,829 hrs · 24,161 cycles
SEAT TRACK FLANGE CRACKED IN MAIN CARGO DECK FLOOR AT BS. 870, LBL, 62.5. FOUND BEYOND ALLOWABLE DAMAGE. SEAT TRACK SEGMENT REPLACED IN ACCORDANCE WITH B727 SRM.
Part: PRESSURE PANEL — PUNCTURED (FUSELAGE) · airframe 41,829 hrs · 24,161 cycles
PRESSURE PAN WEB PUNCHTURED BETWEEN BS. 880 - 890 AND LBL. 48 - 68 AT MAIN CARGO DECK FLOOR. REPLACED WITH PART IN ACCORDANCE WITH B727 SRM.
Part: PRESSURE PANEL — PUNCTURED (FUSELAGE) · airframe 41,829 hrs · 24,161 cycles
PRESSURE PAN WEB PUNCTURED BETWEEN BS. 880 - 890 AND RBL. 48 - 68 AT MAIN CARGO DECK FLOOR. REPLACED WITH NEW PART IN ACCORDANCE WITH B727 SRM
2015
Part: LIGHT — DIM (CABIN) · airframe 38,616 hrs · 22,454 cycles
COCKPIT EMER EXIT LIGHTS DIM. REPLACED EMER EXIT LIGHT UNIT.
2014
Part: SERVICE PANEL — DEPARTED (ZONE 100) · airframe 37,496 hrs · 21,823 cycles
NUMBER 1 ENG VIBRATION IN FLIGHT, AFTER LANDING PERFORMED WALK AROUND AT WHICH POINT DISCOVERED THE LT HYD ACCESS PANEL MISSING & DENT IN LT INLET COWLING RESULTING IN SUSPECTED FOD DAMAGE.
Part: SLAT — DAMAGED (RT WING) · airframe 37,386 hrs · 21,762 cycles
RIGHT HAND SLAT TE NR 5 DAMAGED.
2012
Part: FIRE LOOP — SHORTED (ZONE 400) · airframe 35,348 hrs · 20,597 cycles
INTERMITTENT FIRE WARNING.
Part: SILL — CORRODED (BS 570-610) · airframe 35,092 hrs · 20,451 cycles
DOOR SILL HAS CORROSION, REPAIRED.