N7504Y

Substantial
None

PIPER PA-30S/N: 30-566

Accident Details

Date
Wednesday, July 22, 2009
NTSB Number
WPR09LA372
Location
Walla Walla, WA
Event ID
20090727X81723
Coordinates
46.094722, -118.288887
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

A tripped landing gear motor circuit breaker, which prevented the gear from fully locking in the down position, and subsequent collapse during landing. Contributing to the accident was the disabled landing gear warning horn.

Aircraft Information

Registration
N7504Y
Make
PIPER
Serial Number
30-566
Engine Type
Reciprocating
Year Built
1964
Model / ICAO
PA-30PA30
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Name
SALE REPORTED
Address
14 MARS DR
Status
Deregistered
City
HOLLISTER
State / Zip Code
CA 95023-2518
Country
United States

Analysis

On July 22, 2009, about 1400 Pacific daylight time, a Piper PA-30, N7504Y, experienced a landing gear collapse during the landing roll at Walla Walla, Washington. Walla Walla University was operating the airplane under the provisions of 14 Code of Federal Regulations (CFR) Part 91. The certificated commercial pilot, with a certified flight instructor (CFI) certificate, and one passenger were not injured. The airplane sustained substantial damage to the airframe. The local maintenance test flight departed Walla Walla about 1345. Visual meteorological conditions prevailed, and no flight plan had been filed.

The pilot reported that he had remained in the airport traffic pattern, and completed one takeoff and landing. The pilot stated that, prior to the second landing, the landing gear was down, and all indications appeared normal. After reducing power for landing, he did not hear an audible alert warning horn. As the airplane touched down, the gear collapsed. He noticed smoke coming from the circuit breaker panel on the floor, and exited the airplane.

The air traffic control tower personnel reported that they thought that the landing gear appeared to be down prior to touchdown.

The operator reported that they had previously been having trouble with the landing gear circuit breaker popping during landing gear extension and retraction. Six flight hours prior to the accident, they had replaced the right main landing gear push/pull retraction/extension cable, the gear motor control contactor, and the gear motor circuit breaker. Ground and flight tests had been successfully completed without a recurrence. The operator stated that the airplane had about 8 to 10 landing gear cycles prior to the accident flight with no anomalies noted, which led them to believe that the situation had been resolved.

Post accident examination revealed that the landing gear motor circuit breaker tripped. The landing gear warning horn circuit is powered by the gear motor circuit, and would not activate with the circuit breaker tripped.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR09LA372