Low-Altitude Maneuvering · NTSB ERA10LA266
AEROSTAR S A YAK-52 — Jensen Beach, FL
| Date | May 15, 2010 |
| Location | Jensen Beach, FL |
| Aircraft | AEROSTAR S A YAK-52 |
| Purpose of flight | Personal |
| Conditions | Day · Visual Meteorological Cond |
| Phase / occurrence | Maneuvering-aerobatics Low altitude operation/event |
| Pilot age | 60 |
| Pilot total time | 442 hrs · Building experience |
| Time in type | 160 hrs |
| Fatalities | 2 |
Probable cause
NTSB findings
- Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Altitude-Incorrect use/operation - C
- Aircraft-Aircraft oper/perf/capability-Performance/control parameters-(general)-Not attained/maintained - C
- Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot - C
- Aircraft-Aircraft systems-Landing gear system-(general)-Incorrect use/operation - F
What happened
After takeoff from a nearby airport, the pilot of the accident airplane commenced a series of aerobatic maneuvers at low altitude along a beach. Witnesses observed the airplane flying along the beach about 100 yards offshore in a northerly direction, descending from approximately 300 feet to approximately 50 feet above the water. It next entered a very abrupt and steep turn to the northeast, then went straight up while continuing to turn until it rolled out on a westerly heading toward a cluster of condominiums that lined the beach. The airplane once again made a sharp turn to the right (northbound), then pitched up sharply until it was upside down. It then pitched down, rolled about its longitudinal axis, and impacted the water nose first.
A postaccident examination of the wreckage revealed no evidence of any preimpact failure or malfunction of the airplane or engine. Both the Federal Aviation Administration and the International Aerobatic Club consider the minimum altitude for aerobatic maneuvers to be 1,500 feet, which the pilot was well below when he commenced the maneuvers. Examination of a landing gear down light bulb revealed filament stretching, which indicated that the light bulb was energized prior to the airplane's impact with the water. Review of photographs taken of the airplane a few minutes prior to the accident and moments before it impacted the water, confirmed that the landing gear was extended. Review of the airplane’s pilot operating handbook revealed that the landing gear was supposed to be raised after takeoff and that the pilot was supposed to check for a landing gear up indication. The extended landing gear would have affected the airplane's performance and would have made the airplane slower to respond to the pilot's inputs. This, in combination with his decision to commence the aerobatic maneuvers at low altitude, resulted in his inability to recover prior to impacting the water.