N48RW

Substantial
None

Columbia XJ-7 S/N: 31399

Accident Details

Date
Thursday, March 13, 1997
NTSB Number
LAX97LA122
Location
CAMP PENDELTON, CA
Event ID
20001208X07576
Coordinates
33.390369, -117.439491
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

loss of engine power due to an undetermined cause or causes.

Aircraft Information

Registration
Make
COLUMBIA
Serial Number
31399
Engine Type
Reciprocating
Year Built
1954
Model / ICAO
XJ-7 H46
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
XJL

Registered Owner (Current)

Name
YANKS AIR MUSEUM
Address
13470 DALEWOOD ST
City
BALDWIN PARK
State / Zip Code
CA 91706-5834
Country
United States

Analysis

On March 12, 1997, at 1625 hours Pacific standard time, a Columbia XJ-7, N48RW, collided with soft terrain and nosed over while attempting an off airport forced landing at Camp Pendelton, California. The aircraft sustained substantial damage; however, the pilot and mechanic were not injured. The aircraft was being operated as a maintenance test flight by R. W. Martin, Inc., when the accident occurred. The flight originated in Carlsbad, California, at 1605. Visual meteorological conditions prevailed and no flight plan was filed.

The pilot stated that he experienced a partial engine failure about 20 minutes after takeoff. He notified McClellan-Palomar tower that he was making a forced landing near Las Pulgas Road, west of Interstate 5. After touching down in an open grassy area, the hull dug into rain-softened terrain and the aircraft nosed over onto its back. The accident site was located within a restricted area of Camp Pendelton Marine Base at 33 degrees 18 minutes north latitude by 117 degrees 28 minutes west longitude. This was the aircraft's first flight after an annual safety condition inspection.

An inspection of the aircraft by FAA inspectors revealed throttle movement in the cockpit did not produce corresponding movement of the butterfly valve in the carburetor throat. The throttle linkage did not show evidence of impact damage. The operator reported that the carburetor is designed to automatically go to 80 percent power in the event there is a mechanical separation in the throttle linkage. A review of the aircraft logbooks did not reveal any discrepancies.

A final attempt by the operator to diagnose the cause of the engine failure was unsuccessful.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX97LA122