N9483F

Destroyed
None

HUGHES 269B S/N: 1260289

Accident Details

Date
Saturday, July 22, 1995
NTSB Number
NYC95LA170
Location
HONESDALE, PA
Event ID
20001207X04070
Coordinates
41.569568, -75.250106
Aircraft Damage
Destroyed
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

Corrosion and subsequent failure of the attaching lugs for the left (4H) shock strut assembly, which resulted in collapse of the landing gear/skid.

Aircraft Information

Registration
N9483F
Make
HUGHES
Serial Number
1260289
Model / ICAO
269B

Registered Owner (Historical)

Name
KITTNER ERNEST F
Address
RR 4 BOX 635
Status
Deregistered
City
HONESDALE
State / Zip Code
PA 18431-9426
Country
United States

Analysis

On July 22, 1995, about 1730 eastern daylight time, a Hughes 269B, helicopter, N9483F, was destroyed after the landing gear skid collapsed while standing with the engine operating, at a private heliport (P48), near Honesdale, Pennsylvania. The private pilot was not injured. Visual meteorological conditions prevailed, and no flight plan had been filed. The local, personal flight was being conducted under 14 CFR Part 91.

The pilot stated that after take off from the heliport he, "felt a low frequency vibration." He thought this was associated with the main rotor, so he elected to return to the heliport to determine the cause of the vibration. He landed on the helipad and tried to make radio contact with his instructor to advise him of the problem.

According to the pilot's statement on the NTSB Form 6120.1/2:

...the machine was completely on the ground with the pitch stick in the full down position. Rotor and engine RPM's were at operating range. I reached my cyclic hand to adjust the radio, and no sooner returned it [to the cyclic] to pull [the] trigger and talk...the helicopter began a violent forward and aft gyration and pounding...it proceeded to self destruct around me....

The examination of the landing skids, revealed that the left (4H) shock strut assembly had separated from the landing skid.

According to the FAA Inspector's statement:

...severe exfoliation corrosion was noticed at both attaching lugs. The lugs had failed due to corrosion. All three (3) remaining shock struts were attached.

At the time of the accident, the pilot had 224 total flight hours, 80 hours as a student pilot, rotorcraft, and 10 flight hours in this make and model helicopter.

The reported winds, at the time of the accident, were calm.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC95LA170