N5596C

Substantial
None

CESSNA 170S/N: 19650

Accident Details

Date
Thursday, July 27, 2017
NTSB Number
GAA17CA445
Location
San Andreas, CA
Event ID
20170727X81021
Coordinates
38.146667, -120.648612
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’s improper landing flare during an aborted go-around in gusting wind conditions, which resulted in a hard landing.

Aircraft Information

Registration
Make
CESSNA
Serial Number
19650
Engine Type
Reciprocating
Year Built
1950
Model / ICAO
170C170
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
170A

Registered Owner (Current)

Name
FIELDGROVE MATT L
Address
PO BOX 20
City
SOMERTON
State / Zip Code
AZ 85350-0020
Country
United States

Analysis

The pilot of the tailwheel-equipped airplane reported that, he landed on the main wheels, and while waiting for the tailwheel to drop, the "tailwheel jammed." He added, that when the tailwheel touched down, the airplane was difficult to control, and veered to the left. He corrected for the veer, but the airplane veered to the right. He then did a go-around, however, once airborne the airplane "did not appear to be producing proper power." He then aborted the go-around, and opted to land on the remaining runway. About 25 ft. above the runway, he set the airplane up for a wheel landing and descended. When the airplane was about 5-10 ft. above the runway, the airplane "abruptly" sank, landed hard and collapsed the main landing gear. Subsequently, the airplane came to rest nose down on the runway.

The airplane sustained substantial damage to the fuselage.

During a telephone interview, the pilot reported that he believed the tailwheel had jammed prior to touchdown, and that he had previously re-designed and altered the tailwheel. Further, the airplane produced insufficient power during the go-around. He reported that, the tailwheel was mechanically "okay" when inspected after the accident.

Additionally, an airframe and powerplant mechanic reported that he inspected the tailwheel assembly after the accident, and found no defects and no binding.

The pilot reported the weather at the accident airport, about the time of the accident to be, wind from 320° at 10 knots, gusting to 12 knots. The pilot landed on runway 31.

Photographs taken at the accident site showed torsional twisting of the propeller, consistent with the engine producing power at the time of impact. The National Transportation Safety Board did not examine the engine.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# GAA17CA445