N9299D

Substantial
None

PIPER PA-18-150 S/N: 18-6606

Accident Details

Date
Monday, June 5, 1995
NTSB Number
ANC95LA065
Location
MANLEY HOT SPRI, AK
Event ID
20001207X03578
Coordinates
64.650955, -150.899932
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 FAILURE TO CORRECTLY COMPENSATE FOR THE EXISTING WIND CONDITIONS. THE GUSTING WIND CONDITION WAS A FACTOR.

Aircraft Information

Registration
N9299D
Make
PIPER
Serial Number
18-6606
Engine Type
Reciprocating
Year Built
1958
Model / ICAO
PA-18-150 PA18
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
HILL DAVID R
Address
PO BOX 771696
Status
Deregistered
City
EAGLE RIVER
State / Zip Code
AK 99577-1696
Country
United States

Analysis

On June 4, 1995, at 1745 Alaska daylight time, a wheel equipped Piper PA-18-150 airplane, N9299D, registered to and operated by the pilot, landed hard and veered off the runway into the trees at Manley Hot Springs, Alaska. The personal flight, operating under 14 CFR Part 91, departed Fairbanks, Alaska, and the destination was Manley Hot Springs. No flight plan was filed and visual meteorological conditions prevailed. The pilot, the sole occupant, was not injured and the airplane was substantially damaged.

According to the pilot, the wind was gusting during her final approach and she was planning on making a "wheel landing." When the airplane was 10 feet above the runway's surface, she stated the wind stopped and the airplane hit the ground hard. It bounced into the air and when it touched down a second time it veered to the right. The pilot stated she applied left rudder but it would not move. It felt like it was against the stop or jammed.

A subsequent interview between the pilot and the Federal Aviation Administration (FAA), Flight Standards Inspector, revealed that the tail of the airplane hit the ground first, then the main landing gear.

According to the FAA Inspector who examined the airplane wreckage, when the tailwheel struck the ground it bent the lower right longeron and shifted the left rudder stop toward the right side of the airplane. This reduced the left rudder's range of travel.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC95LA065