N97168

Substantial
None

Stinson 108S/N: 168

Accident Details

Date
Thursday, July 31, 2003
NTSB Number
NYC03LA175
Location
White Post, VA
Event ID
20030808X01291
Coordinates
39.062500, -78.091392
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot/ mechanic's improper annual inspection including his rigging of the elevator flight control, and his subsequent inadequate preflight inspection of the airplane prior to flight, when he failed to detect the improperly rigged elevator flight control, both of which resulted in restricted up elevator control during the flare.

Aircraft Information

Registration
N97168
Make
STINSON
Serial Number
168
Engine Type
Reciprocating
Year Built
1946
Model / ICAO
108S108
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
PERKINS JAMES H
Address
805 LAKEVIEW DR
Status
Deregistered
City
CROSS JNCT
State / Zip Code
VA 22625
Country
United States

Analysis

On July 31, 2003, about 1605 eastern daylight time, a Stinson 108, N97168, was substantially damaged while landing at White Post Airport, White Post, Virginia. The certificated commercial pilot was not injured. Visual meteorological conditions prevailed for the personal flight. No flight plan had been filed for the local flight that was conducted under 14 CFR Part 91.

The pilot owned the airplane, and held a mechanic's certificate with airframe and powerplant ratings. In addition, he held "Inspection Authorization" on his mechanic's certificate. The pilot stated he had just completed an annual inspection of the airplane, and also overhauled the engine. The accident flight was the first flight following the maintenance.

The pilot stated:

"Departed 3VA7 at 1600 EDT. A/C flew normally, flew one LH pattern, at about 1605 EDT, making normal approach at 75 mph, added full flaps and heard a "ting" noise. When about 12-15 feet above runway, chopped power and A/C immediately dove at runway - no up elevator. A/C hit runway at approx 65 - 70 mph and flipped upside down."

An inspector from the Federal Aviation Administration examined the airplane. The vertical stabilizer was crushed, and the right wing strut was bent. In addition, the trusses adjacent to the right main cabin door were bent and broken. When the control yoke was exercised through its full range of motion, sometimes it would contacted the side of the radio rack, which restricted its rearward motion. However contact was not made every time the yoke was moved. The radio rack appeared tight and there was no evidence that it had shifted, or was loose.

Measurements were taken with a protractor revealed the up elevator movement was 12 degrees, and the down movement was 33 degrees. According to the type certificate data sheet, the elevator movement allowed was 20 degrees down for all flap configuration. The elevator up movement was 17 degrees for flaps up, or 25.5 degrees with flaps extended.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC03LA175