No fatalities

1 Feb 2017: BEECH 95 B55 (T42A) A (N321BJ) — Cameron Park, CA

Cameron Park, CA, United States

On 1 Feb 2017, a BEECH 95 B55 (T42A) A (registration N321BJ) was involved in an aviation accident near Cameron Park, CA. No fatalities were reported. Investigators recorded the probable cause as: Failure of the landing gear to extend as a result of excessive wear within the landing gear gearbox and motor, which resulted in a gear-up landing. 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 February 1, 2017, a Beech 95-B55 (N321BJ) sustained substantial damage during a gear-up landing near Cameron Park, California. The pilot was uninjured; postaccident examination revealed a shorted landing gear motor and worn gearbox components.

Accident Description

On February 1, 2017, about 1410 Pacific daylight time, a Beech 95-B55 airplane, registration N321BJ, sustained substantial damage when it was involved in an accident near Cameron Park, California. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that when he raised the landing gear shortly after takeoff, he heard a loud crunch as the gear entered the gear wells. He climbed the airplane to about 3,000 ft and observed that the landing gear circuit breaker was popped and the alternator was off. The pilot attempted to extend the landing gear normally several times after resetting the circuit breaker; however, the circuit breaker popped each time and the gear remained retracted. He also attempted to use the emergency gear extension to no avail, and subsequently landed with the landing gear retracted, which resulted in substantial damage to the lower fuselage.

Postaccident Examination

During a postaccident examination, the airplane was positioned on jacks and electrical power was supplied. When the landing gear handle was placed in the down position, the gear would not extend normally as the landing gear motor did not respond and became hot. The emergency extension handle and housing assembly were removed to extend the landing gear. During the removal, the bearing retaining ring was not secured and fell out. The gear motor was subsequently removed, which allowed the landing gear extension to the down and locked position. The landing gear motor was function tested by applying 28 volts to both the clockwise and counterclockwise wires; it was determined that the motor was shorted out internally.

The gearbox was disassembled; the gearbox sector gear contacted the internal stop when retracted, and the emergency gear handle lost contact with the pinion, causing it to rotate freely. The crank assembly exhibited signs of excessive wear and excessive pinion shaft end play, resulting in the gear handle disconnecting from the pinion gear when the sector gear was against the internal up stop.

The American Bonanza Society Air Safety Foundation’s Landing Gear Inspection Checklist and Repair Guide stated: "There should be 1/8 to 1/4 turn counterclockwise remaining to the stop when you crank the emergency handcrank down… If the sector gear hits the stop in either the extended or retracted position, the gearbox and motor should be removed and overhauled. The most common cause of this condition is a gear motor that is due for overhaul."

Probable Cause

The source did not provide a stated probable cause.

Contributing factors

Fatigue/wear/corrosionGear extension and retract sys — Failure