19980325011989I

Incident · Minor damage

FAA incident report · Cndair CL6002B16 · Columbus, OH · March 25, 1998

Date: March 25, 1998 · 13:56 local
Place: Columbus, OH
Airport: Ohio State University
Phase of flight: Roll-Out (Fixed Wing)
Operating rules: Air taxi and commuter (Part 135)
Damage: Minor damage
Aircraft: N333MG
Reported as: Cndair CL6002B16
People aboard: 2
Fatal injuries: 0
Pilot’s flight hours: 10,000 total1,200 in this make and model150 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Narrative: departed (uny) in hard rain, destination (osu) cruise altitude FL 370 for 3 hours, outside temperature -50C. Landing arrival rwy 9 deployed thrust reversers, aircraft yawed slightly right with slight shudder heading correction made with flight controls. At 90 KIAS shudder intensified throughout deceleration. Exited runway, normal engine shutdown. Aircraft landed with suspected frozen brakes, deflating all main gear tires. Visual damage of the aircraft, but not limited to right wheel well door, close outpanel right flap hinge, tires and wheel assembly. Systems operation did not reveal any apparent mechanical failure.

As the FAA filed it

NARRATIVE: DEPARTED (UNY) IN HARD RAIN, DESTINATION (OSU) CRUISE ALTITUDE FL 370 FOR 3 HOURS, OUTSIDE TEMPERATURE -50C. LANDING ARRIVAL RWY 9 DEPLOYED THRUST REVERSERS, AIRCRAFT YAWED SLIGHTLY RIGHT WITH SLIGHT SHUDDER HEADING CORRECTION MADE WITH FLIGHT CONTROLS. AT 90 KIAS SHUDDER INTENSIFIED THROUGHOUT DECELERATION. EXITED RUNWAY, NORMAL ENGINE SHUTDOWN. AIRCRAFT LANDED WITH SUSPECTED FROZEN BRAKES, DEFLATING ALL MAIN GEAR TIRES. VISUAL DAMAGE OF THE AIRCRAFT, BUT NOT LIMITED TO RIGHT WHEEL WELL DOOR, CLOSE OUTPANEL RIGHT FLAP HINGE, TIRES AND WHEEL ASSEMBLY. SYSTEMS OPERATION DID NOT REVEAL ANY APPARENT MECHANICAL FAILURE.