No fatalities

31 May 2018: THRUSH AIRCRAFT INC S2R-H80 NO SERIES (N6215P) — AIR AIDS INC — Parkin, AR

Parkin, AR, United States

On 31 May 2018, a THRUSH AIRCRAFT INC S2R-H80 NO SERIES (registration N6215P) operated by AIR AIDS INC was involved in an aviation accident near Parkin, AR. No fatalities were reported. Investigators recorded the probable cause as: The improper operation of the rudder pedal adjustment mechanism for an undetermined period of time, which led to the failure of the rudder pedal adjustment track, the detachment of the rudder pedal, and the pilot’s subsequent inability to maintain directional… 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 May 31, 2018, a Thrush S2R-H80 (N6215P) veered off runway 18 during takeoff from a private airstrip near Parkin, Arkansas, after the right rudder pedal moved fully forward. The pilot was uninjured. Examination revealed a worn rudder pedal adjustment mechanism.

Accident Details

On May 31, 2018, at approximately 1115 central daylight time, a Thrush Aircraft S2R-H80, registration N6215P, sustained substantial damage during a runway excursion while taking off from runway 18 at a private airstrip near Parkin, Arkansas. The aircraft was registered to Mid Continent Aircraft Corp and operated by Air Aids, Inc., under Title 14 Code of Federal Regulations Part 137 as an aerial application flight. Visual meteorological conditions prevailed, and the flight was conducted without a flight plan. The local flight was originating at the time of the accident. The pilot was not injured.

Pilot Report

According to the pilot, during the takeoff roll, the right rudder pedal moved all the way forward. Because the airplane was equipped with toe brakes, once the pedal was fully forward against the material hopper, directional control could not be maintained. The pilot attempted to stop the airplane by using reverse pitch on the propeller, but the airplane departed the east side of the runway and struck a ditch.

Aircraft Examination

Post-accident examination of the airplane revealed that the rudder pedal adjustment mechanism consisted of a track that allowed the rudder pedal shaft to move fore and aft, with a detent pin that engaged holes in the track. The track was fitted with a safety stop bolt to prevent the rudder pedal shaft from traveling too far forward and exiting the end of the track. The track assemblies for both the left and right rudder pedals showed wear on the track and the stop bolt located forward of the most forward detent position. The right adjustment track had a semi-circular section worn completely through, matching the shape of the rudder shaft. This was consistent with the rudder shaft being stopped by the stop bolt rather than being locked in the forward detent position. It could not be determined how long the rudder system had been used in this manner.

Maintenance Records

Review of the airplane's maintenance records indicated that the aircraft had accumulated 991 hours in service as of its most recent annual inspection, dated December 29, 2017. The "Before Starting Engines" checklist in use at the time of the accident included the instruction "Rudder Pedals – ADJUST and LOCK."

Manufacturer Service Letter

On June 11, 2018, the airplane manufacturer issued Service Letter SL-AG-126, entitled "Rudder Pedal Mechanism Inspection," which detailed proper use, rigging, and maintenance of the rudder system, including the rudder pedal adjustment mechanism.

Contributing factors

Causes

Rudder control system — FailureIncorrect use/operation

Other contributing factors

Contributed to outcome