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
CRACKED AT THE SLAT HOOK CUT-OUT IN THE AFT CORNER. AT WS 519 ON THE RIGHT WING
CORROSION ON FUSELAGE SKIN AT BS1028 TO 1055 AND S-29L TO S-29R
CORROSION ON RH HORIZONTAL STAB REAR SPAR UPPER CHORD AT STAB STATION 104.25 THRU 123.25 AND 141.5 THRU 160.5
BMS3-27 IS NO LONGER PROCURABLE. BOEING SR KFC-GUC-24-0105-09B APPROVED THE USE OF BMS3-38 AS AN ALTERNATE.
AFT UPPER FUSELAGE TRANSVERSE FLOOR BEAM UPPER CHORD CORROSION AT BS1148 FROM LBL45 TO LBL55
CORROSION AT MULTIPLE LOCATIONS AT A-NUT ATTACHMENTS. FORWARD LOWER FUSELAGE LONGITUDINAL STABILIZER LOWER CHORD REPAIRED AT BL0 FROM BS450-660
AFT UPPER FUSELAGE WINDOW FRAMES CORROSION FROM BS950A-950C AND S-10R TO S-14R
AFT LOWER FUSELAGE FRAME INNER CHORD PUNCTURE AT BS1148 FROM S-25R TO S-28R.
VERTICAL BEAM CORRODED AT LOWER END. REPAIRED AT BL 0 BS 1183.
AFT UPPER FUSELAGE TRANSVERSE FLOOR BEAM UPPER CHORD CORRODED AT BS1030 FROM LBL10 TO LBL20.
NON-PRODUCTION FASTENERS INSTALLED .AFT LOWER FUSELAGE FRAME REPAIRED AT BS1050 FROM S-25L TO S-28L
FORWARD UPPER FUSELAGE TRANSVERSE FLOOR BEAM UPPER AND LOWER CHORDS CORROSION AT BS720 FROM LBL65-RBL50
RIGHT OTBD END OF THE SIDELOAD BEAM CORRODED. CENTER FUSELAGE BULKHEAD SIDELOAD BEAM CORRODED AT BS740 FROM LBL30 TO RBL30
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
ELONGATED HOLE ON VERTICAL STIFFENER WEB IN CENTER FUEL TANK FRONT SPAR AT LBL40
NONPRODUCTION FASTENER INSTALLED @ AFT LOWER FUSELAGE FRAME REPAIRED AT BS1166 FROM S-25L TO S-28L
AFT LOWER FUSELAGE SKIN CORROSION FROM BS990-1010 AT S-26L
FORWARD LOWER FUSELAGE FRAME UPPER CHORD CRACKED AT BS700 FROM S-28L TO S-28R
CENTER FUSELAGE SECTION RH DELTA BEAM LOWER CHORD CORRODED FROM BS720F-755 AND S-27L TO S-27R
AFT LOWER FUSELAGE SKIN PANEL CORROSION FROM BS1148-1166 AND S-18L TO S-20L.
CRACK FOUND ON LEFT WING OUTBOARD TRAILING EDGE FLAP, OUTBOARD FLAP TRACK. CRACK WAS IN UPPER FLANGE INBOARD FLANGE.
WING CENTER BOX FRONT SPAR CORRODED IN MULTIPLE PLACES ON VERTICAL AND HORIZONTAL CHORD FLANGES AT BS740 FROM LBL70.5 TO RBL70.5
AFT UPPER FUSELAGE FLOOR SHEAR WEB CRACK NEAR BS1166-1176.9 AND RBL8 TO RBL17.87
FT LOWER FUSELAGE FRAME CRACKED AT BS1070 FROM S-26R TO S-28R
AFT LOWER FUSELAGE FRAME INNER CHORD PUNCTURE AT BS1130 FROM S-25L TO S-29L.
FRAME INNER CHORD PUNCTURE AT BS 1090 BETWEEN S26R AND S28R.
AFT LOWER FUSELAGE FRAME INNER CHORD PUNCTURE AT BS1090 FROM S-24L TO S-28L
KEEL BEAM BREATHER WEB CORRODED AT SEVERAL LOCATIONS ON THE UPPER SURFACE FROM BS740 TO 795 AND LBL13 TO RBL13
AFT LOWER FUSELAGE FRAME INNER CHORD DENTED AT BS1110 FROM S-24L TO S-28L
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
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.
HORIZONTAL STABILIZER LH SIDE LEADING EDGE PANEL #9122 REWORKED (BLEND OUT) DENT FOUND BEYOND ALLOWABLE DAMAGE, REPAIRED IN ACCORDANCE WITH B727-200 SRM
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.
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.
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
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.
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
WEB TANGS CRACKED AT BS. 600 AND BS 620 BETWEEN STR. 3L AND STR. 4L, ABOVE MAIN CARGO DOOR. PART REPLACEMENT REQUIRED.
COCKPIT EMER EXIT LIGHTS DIM. REPLACED EMER EXIT LIGHT UNIT.
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.
RIGHT HAND SLAT TE NR 5 DAMAGED.
INTERMITTENT FIRE WARNING.
DOOR SILL HAS CORROSION, REPAIRED.