N7150A

Destroyed
Fatal

Aero Vodochody Aero. Works L-29 S/N: 591318

Accident Details

Date
Friday, October 11, 1996
NTSB Number
SEA97LA011
Location
TILLAMOOK, OR
Event ID
20001208X06977
Coordinates
45.459579, -123.710609
Aircraft Damage
Destroyed
Highest Injury
Fatal
Fatalities
2
Serious Injuries
0
Minor Injuries
0
Uninjured
0
Total Aboard
2

Probable Cause and Findings

failure of the pilot to maintain control of the aircraft, while maneuvering behind an F4F aircraft. The lack of altitude for a recovery was a related factor.

Aircraft Information

Registration
N7150A
Make
AERO VODOCHODY AERO. WORKS
Serial Number
591318
Engine Type
Turbo-jet
Model / ICAO
L-29 L29
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
ERICKSON GROUP LTD
Address
4900 SW GRIFFITH DR STE 133
Status
Deregistered
City
BEAVERTON
State / Zip Code
OR 97005
Country
United States

Analysis

On October 11, 1996, approximately 1617 Pacific daylight time, an Aero Vodochody L-29 Delfin, N7150A, registered to the Erickson Group Ltd. of Beaverton, Oregon, collided with terrain following a loss of control while maneuvering at low altitude in the vicinity of Tillamook Airport, Tillamook, Oregon. The commercial pilot and a passenger were fatally injured, and the experimental-category airplane, a Czechoslovakian-manufactured two-seat military jet trainer retrofitted with a Pratt & Whitney J60-5 engine, was destroyed. The 14 CFR 91 flight was planned as a local flight out of Tillamook. Visual meteorological conditions prevailed and no flight plan had been filed.

A representative of the operator stated that the passenger was a photojournalist for an aviation publication and that the flight was being conducted as a photographic mission for the passenger. At the time of the accident, the aircraft was maneuvering into position to photograph an F4F Wildcat aircraft. Witnesses reported that the aircraft took off and maneuvered to overtake the Wildcat. They stated that as the L-29 crossed behind the F4F's flight path, it initiated a roll to the right, rolling approximately 1 1/4 turns, and that the L-29's nose then pitched up, then dropped to an extremely nose-low position, and that the aircraft subsequently impacted the ground in a near level attitude with a steep flight path angle. The witnesses reported that the sequence took place at an estimated airspeed between 120 and 150 knots and about 500 feet above ground level. The witnesses also reported that the two aircraft did not collide. A guide to world military trainers published in the magazine of the Air Force Association (John W.R. Taylor & Kenneth Munson, "World Gallery of Trainers", Air Force Magazine, December 1995) gives the L-29's flaps-down stall speed as 81 MPH (70 knots) at 7,165 pounds gross weight.

FAA investigators conducted an on-site examination of the aircraft wreckage on the day after the crash. They reported that they did not find any evidence of malfunction in either the airframe or the engine.

The operator, Erickson Group Ltd., failed to return a completed NTSB Form 6120.1/2, Pilot/Operator Aircraft Accident Report.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA97LA011