N163DK

HAWKER BEECHCRAFT CORP HAWKER 900XP · 2008 · Valid Registration

Registered owner: HORIZONTAL VENTURES LLC, IN (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
GARY JET CENTER, INC. (YGJA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

O · 2019-12-02 Matched by certificate designator
ATA 5343

WHILE INSTALLING THE RIGHT MLG LEG WE NOTICED THAT THE FWD UPPER AND LOWER TRUNNION ATTACH POINTS, WHERE THE BARREL NUTS SLIDE INTO, BOTH HAD GROOVES WORN INTO THEM AND CHAFFED REALLY BAD ALL AROUND. TOP BARREL NUT HOLE HAD A GROOVE THAT MEASURED ABOUT .035" IN DEPTH AND BOTTOM HAD A GROOVE DEPTH OF ABOUT .025". THE GROOVE DOES NOT GO COMPLETELY AROUND THE CIRCUMFERENCE OF THE HOLE, MAYBE A 1/3 OF THE HOLE, ON TOP AND BOTTOM HOLE. BOTH BARREL NUT HOLES ALSO HAVE DEEP SCRATCHES THE RUN PERPENDICULAR TO THE CHAFFING. I'M NOT SURE HOW THIS AREA GETS CHAFFED THIS BAD BECAUSE THESE BOLTS GET TORQUED TO A SUBSTANTIAL AMOUNT, 72.0 TO 82.0 LB FT FOR TOP AND 160.0 TO 180.0 LB FT FOR THE BOTTOM. THERE IS ALSO NO RECORD OF THE LANDING GEAR EVER BEING OUT OF THIS AIRCRAFT SO THIS DAMAGE MAY HAVE BEEN CAUSED AT THE FACTORY.

Source: SDR 2GYR201912190007 · FAA SDRS
E · 2019-10-21 Matched by certificate designator
ATA 3210

WHEN THE AIRCRAFT TOUCHED DOWN ON LANDING, THE CREW NOTED A LARGE VIBRATION THROUGHOUT THE AIRFRAME. THE VIBRATION LESSENED IN INTENSITY AS THE AIRCRAFT SLOWED AND WENT AWAY WHEN STOPPED. TAXI TO THE RAMP WAS REPORTED AS NORMAL. IT WAS DISCOVERED THAT THE LEFT MAIN LANDING GEAR TORQUE LINK BOLT FAILED. THIS CAUSED THE LOWER GEAR ASSEMBLY TO ROTATE FREELY, CAUSING THE WHEELS TO SHIMMY. THIS IN TURN CAUSED THE UPPER TORQUE LINK TO CONTACT THE WHEELS, TIRES, AND OUTBOARD BRAKE ASSEMBLY. THE SHIMMY CAUSED THE WEIGHT ON WHEELS SWITCH NORMALLY ATTACHED TO THE LOWER TORQUE LINK TO DEPART THE AIRCRAFT. IT WAS LATER FOUND BY AIRPORT OPERATIONS DURING A FOD INSPECTION OF THE RUNWAY AFTER THE INCIDENT.

Source: SDR 2GYR201910240001 · FAA SDRS
E · 2019-10-21 Matched by certificate designator
ATA 3210

UPON LANDING AT KGYY AT APPROX. 8:00 P.M. ON THE NIGHT OF OCTOBER 21, 2019 AIRCRAFT N163DK FELT A ABNORMAL VIBRATION FORM THE LEFT MLG. THE AIRCRAFT TAXIED TO THE JET CENTER AND DISCOVERED THAT THE LEFT MLG UPPER AND LOWER TORQUE LINKS WERE SEPARATED FROM EACH OTHER. UPON INVESTIGATION WE DISCOVERED THAT THE BOLT THAT HOLDS THE TORQUE LINKS TOGETHER HAD SHEARED. THIS ALLOWED THE INNER STRUT AND LEFT MLG WHEELS TO BECOME INDEPENDENT FROM THE OUTER STRUT. WHEN THAT HAPPENED THE MLG WHEELS BEGIN TO VIBRATE AND THE INNER WHEEL HALVES BEGIN TO CONTACT THE UPPER TORQUE LINK CAUSING SEVERE DAMAGE TO THE WHEELS AND OUTER BRAKE ASSEMBLY. ALSO THE WEIGHT ON WHEELS SWITCH WAS RIPPED OUT OF THE LOWER TORQUE LINK.

Source: SDR 2GYR20191023004 · FAA SDRS