N995PM

Substantial
None

Bell 206-L4S/N: 52251

Accident Details

Date
Tuesday, August 28, 2001
NTSB Number
LAX01LA292
Location
Mesa, AZ
Event ID
20010829X01818
Coordinates
33.510284, -111.580421
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot's improper autorotation in that he failed to attain the proper descent rate resulting in a hard landing and subsequent airframe damage. A factor was the high temperature.

Aircraft Information

Registration
Make
BELL
Serial Number
52251
Engine Type
Turbo-shaft
Year Built
2000
Model / ICAO
206-L4B06
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
7
FAA Model
206-L4

Registered Owner (Current)

Name
5688C LLC
Address
24017 N 55TH AVE
City
GLENDALE
State / Zip Code
AZ 85310-3730
Country
United States

Analysis

On August 28, 2001, at 1030 hours mountain standard time, a Bell 206-L4, N995PM, was substantially damaged when the tail boom was bent after contacting the ground during a practice autorotation landing at Falcon Field, Mesa, Arizona. The airline transport pilot and one passenger were not injured. Visual meteorological conditions prevailed for the flight operated by Pacific Marine Leasing under 14 CFR Part 91. The helicopter departed Falcon Field about 1030 for the local flight, and no flight plan was filed.

The pilot was interviewed by an investigator from the National Transportation Safety Board shortly after the accident. He stated that he was doing a practice autorotation landing when the accident occurred. During the last landing, the helicopter "fell through" much faster than anticipated. In the resulting steep flare, the tail boom contacted the ground and was bent. The helicopter then touched down on the skids relatively softly and slid to a stop. The pilot accomplished a normal engine shutdown procedure and exited the helicopter. The temperature at the time of the accident was 100 degrees Fahrenheit. The pilot stated that no mechanical anomalies were experienced prior to or after the accident. The pilot stated that in the future he will allow a higher margin for autorotation power recovery in hot conditions.

According to an inspector from the Federal Aviation Administration, Scottsdale Flight Standards District Office, the damage was the result of the hard landing. According to the inspector, who examined the wreckage, the tail boom was broken prior to striking the ground due to a hard landing. He stated that the tail boom had ripped out at the aft bulkhead, and the landing skids were bent upward at the aft end. There was also damage to the nose of the helicopter. According to the inspector, the helicopter hit the ground hard enough to separate the tail boom from the fuselage and bend the skids, then rocked forward, damaging the nose. The helicopter then stopped upright on the skids. The main rotor blades were not damaged.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX01LA292