Accident Overview
On January 21, 2014, at about 1500 central standard time, a Grumman American AA-5B airplane, registration N28578, was substantially damaged during a forced landing following an in-flight separation of the propeller near Willow Park, Texas. The pilot, who was the sole occupant, was not injured. The aircraft was registered to a private individual and operated by the pilot under 14 CFR Part 91 as a personal flight. Visual meteorological conditions prevailed, and the flight was not operated on a flight plan. The local flight had originated from Lake Whitney State Park Airport (F50), Whitney, Texas, about 1445.
Pilot Report
The pilot reported hearing a loud noise during cruise flight at 2,000 feet mean sea level. He was unable to maintain altitude and subsequently executed a forced landing to the infield of a horse racing track. During the landing, the airplane encountered a drainage ditch, causing the nose and right main landing gears to collapse.
Postaccident Examination
A postaccident examination revealed that the two-blade, fixed-pitch propeller assembly had separated from the engine propeller flange. The propeller was recovered about three days later from a pasture located about 8 miles east-southeast of the accident site. The propeller bolts, which were retained by the spinner, were recovered. Four of the bolts were intact, with no apparent damage to either the bolt threads or the propeller flange insert threads. The remaining two bolts had failed, with the threaded portion of the bolt retained by the propeller flange insert. The appearance of portions of the fracture surfaces appeared consistent with fatigue failure. Safety wire remnants were recovered with the bolts.
Maintenance Records
Airplane maintenance records indicated that an annual inspection was completed on January 14, 2013. The airframe and engine had accumulated about 32,055 hours total time, with about 14 hours since the annual inspection. The engine had accumulated about 412 hours since overhaul. The pilot informed FAA inspectors that the propeller assembly had been removed and reinstalled during the most recent annual inspection. However, the maintenance logbook entry did not include a notation regarding the removal of the propeller.