N321BJ

Substantial
None

BEECH 95 B55 (T42A)S/N: TC-925

Accident Details

Date
Wednesday, February 1, 2017
NTSB Number
WPR17LA061
Location
Cameron Park, CA
Event ID
20170203X42626
Coordinates
38.683612, -120.985832
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

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.

Aircraft Information

Registration
N321BJ
Make
BEECH
Serial Number
TC-925
Engine Type
Reciprocating
Year Built
1965
Model / ICAO
95 B55 (T42A)BE55
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Name
RAW A C INC
Address
3511 SILVERSIDE RD STE 105
Status
Deregistered
City
WILMINGTON
State / Zip Code
DE 19810-4902
Country
United States

Analysis

On February 1, 2017, about 1410 Pacific daylight time, a Beech 95-B55 airplane, 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. The pilot climbed the airplane to about 3,000 ft and saw 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. The pilot 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.

During a postaccident examination, the airplane was positioned on jacks and electrical power was supplied. The landing gear handle was put in the down position however, the gear would not extend normally as the landing gear motor did not respond and got hot. The emergency extension handle, and housing assembly was 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. In turn, the emergency gear handle lost contact with the pinion and rotated freely. The crank assembly exhibited signs of excessive wear and excessive pinion shaft end play resulting in the gear handle to disconnect 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.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR17LA061