No fatalities

18 Jun 2011: AEROVODOCHODY L-29 DELFIN (N37KF) — Ward Raju Mann — Reno, NV

Reno, NV, United States

On 18 Jun 2011, an AEROVODOCHODY L-29 DELFIN (registration N37KF) operated by Ward Raju Mann was involved in an aviation accident near Reno, NV. No fatalities were reported. Investigators recorded the probable cause as: The partial failure of the primary airframe structure supporting the rudder was due to melting from jet blast deflected by a failed engine support structure, which was part of a modification to install a higher thrust engine. This summary draws on records from NTSB; 2 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

An experimental Aerovodochody L-29 Delfin (N37KF) experienced partial failure of rudder support structure during landing roll at Reno-Stead Airport on June 18, 2011. Pilot not injured; aircraft sustained substantial damage. Failure traced to engine mount modification.

Event

On June 18, 2011, at approximately 1450 Pacific daylight time, an experimental Aerovodochody L-29 Delfin, registration N37KF, experienced a partial failure of the primary airframe structure that supports the airplane's rudder while in the air race pattern at Reno-Stead Airport, Reno, Nevada. The commercial pilot, who was the sole occupant, was not injured. The airplane, owned and operated by Raju Mann Ward, sustained substantial damage.

Aircraft and Flight

The local flight was conducted under 14 Code of Federal Regulations Part 91 as an air race qualification/training flight. It departed from Reno-Stead Airport approximately 20 minutes before the accident. Visual meteorological conditions prevailed, and no flight plan had been filed.

Failure and Damage

According to the Federal Aviation Administration (FAA) inspector who responded to the scene, while the airplane was in flight, part of the engine support structure—installed as part of a modification to accommodate a higher thrust engine—failed to hold the new engine in proper alignment. This failure allowed jet blast from the engine to be deflected onto a portion of the primary airframe structure. The melting of that structure affected the support and movement of the airplane's rudder.

Although the failure occurred in flight, it was not detected until the pilot was operating the rudder pedals during the landing roll. The pilot was able to keep the airplane on the runway by applying alternative or non-standard control inputs.

Investigation Findings

During the investigation, it was determined that at least five other L-29 airplanes had the same type of mounts, which were all designed and welded or manufactured by the same entity. According to the FAA inspector who examined these mounts, the welding was poor on some of them, and there was some degree of structural variation among a number of the mounts.

Probable cause

The partial failure of the primary airframe structure supporting the rudder was due to melting from jet blast deflected by a failed engine support structure, which was part of a modification to install a higher thrust engine.

Contributing factors

Capability exceededRudder misc structure — Failure