GRUMMAN AMERICAN AVN. CORP. AA 5B

Willow Park, TX, January 21, 2014

Event Information

DateJanuary 21, 2014
Event TypeACC
LocationWillow Park, TX
CountryUSA
Coordinates32.75079, -97.77094
Highest InjuryNONE
NTSB NumberCEN14LA118
Event ID20140122X64032

Aircraft

MakeGRUMMAN AMERICAN AVN. CORP.
ModelAA 5B
Registration #N28578
OperatorJack E Barnett
OwnerTerry L Melton
CategoryAIR
FAR Part091
Aircraft DamageSUBS

Conditions

Light ConditionDAYL
WeatherVMC

Injuries

Fatal0
Serious0
Minor0
None1
Total Injured0

Event Location

Probable Cause

The improper reinstallation of the propeller assembly, which resulted in the subsequent in-flight separation of the propeller.

Full Narrative

On January 21, 2014, about 1500 central standard time, a Grumman American AA-5B airplane, N28578, was substantially damaged during a forced landing following an in-flight separation of the propeller near Willow Park, Texas. The pilot was not injured. The airplane was substantially damaged. The airplane was registered to a private individual and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed for the flight, which was not operated on a flight plan. The local flight originated from the Lake Whitney State Park Airport (F50), Whitney, Texas, about 1445.

The pilot reported that he heard 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. The airplane encountered a drainage ditch during the landing, which caused the nose and right main landing gears to collapse.

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.

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 Federal Aviation Administration 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.

About This NTSB Record

This aviation event was investigated by the National Transportation Safety Board (NTSB). NTSB investigates all U.S. civil aviation accidents to determine probable cause and issue safety recommendations to prevent future accidents.

All Aviation Events More in TX