No fatalities

4 Apr 2015: CESSNA 206H H (N245RB) — Honolulu, HI

Honolulu, HI, United States

On 4 Apr 2015, a CESSNA 206H H (registration N245RB) was involved in an aviation accident near Honolulu, HI. No fatalities were reported. Investigators recorded the probable cause as: A blown nose landing gear tire during landing, which resulted in the pilot’s inability to maintain directional control. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On April 3, 2015, a Cessna 206H veered off runway 4R during landing at Honolulu International Airport, striking an arrester gear assembly and sustaining substantial damage to the right wing strut. No injuries occurred.

Incident

On April 3, 2015, about 2115 Hawaiian standard time, a Cessna 206H, registration N245RB, was substantially damaged during landing at Honolulu International Airport (HNL), Honolulu, Hawaii. The airplane was registered to and operated by Worldwide Aircraft Leasing Corporation under Part 91 of Title 14 Code of Federal Regulations. The commercial pilot and one passenger were not injured. Visual meteorological conditions prevailed and an instrument flight rules flight plan had been filed. The flight originated from Kona International Airport at Keahole (HKO) in Kailua/Kona, Hawaii, about 1945.

Pilot and Passenger Reports

The pilot reported that shortly after landing on runway 4R, he experienced difficulties controlling the airplane during the landing roll. He stated that the airplane initially drifted slightly to the left. When he applied aileron and rudder to correct the drift, the airplane yawed suddenly to the right, and he was unable to counteract it. Subsequently, the airplane exited the runway surface and struck an arrester gear assembly, used by military fighter and trainer aircraft for emergencies. The passenger stated that the landing was normal and on the centerline. She further stated that shortly after landing, the pilot struggled to maintain control of the airplane.

Postaccident Examination

Postaccident examination by a Federal Aviation Administration Inspector revealed that the right wing strut was bent about mid-span. Flight control and braking continuity was established with the cockpit controls. The main tires were examined and appeared to be properly inflated with no anomalies observed. The nose wheel tire remained on its hub, but a hole approximately 1/2-inch in diameter was observed on the side wall of the inner tube. No additional pre-accident mechanical malfunctions or failures were observed that would have precluded normal operations.

Damage

The airplane sustained substantial damage to the right wing strut during the accident sequence.

Contributing factors

PilotDamaged/degraded