N555SJ

Substantial
None

Bell 206A S/N: 308

Accident Details

Date
Friday, January 3, 1997
NTSB Number
NYC97LA041
Location
LINDEN, NJ
Event ID
20001208X07348
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 allowing the rotor RPM to decay and his failure to take remedial action in time to recover the autorotation.

Aircraft Information

Registration
Make
BELL
Serial Number
308
Engine Type
Turbo-shaft
Year Built
1968
Model / ICAO
206A B06
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
4
FAA Model
206A

Registered Owner (Current)

Name
APEX59 LLC
Address
1041 GRAND AVE # 261
City
SAINT PAUL
State / Zip Code
MN 55105-3002
Country
United States

Analysis

On January 3, 1997, at 1330 eastern standard time, a Bell 206A, N555SJ, sustained substantial damage from a hard landing while performing a practice touchdown autorotation at the Linden Airport (LDJ) near Linden, New Jersey. The airline transport rated pilot and the private pilot rated copilot, the sole occupants, reported no injuries. Visual meteorological conditions prevailed at the time of the accident and no flight plan was filed. The local instructional flight was conducted under 14 CFR Part 91 and originated at the Linden Airport at approximately 1300.

The pilot reported, "While practicing full autorotations I attempted to demonstrate a 180 degree autorotation to the ground to the owner of the aircraft, who is himself a private helicopter pilot. While turning to the touchdown spot I noticed the RPM decaying, I attempted to recover the RPM by entering the flare early and prior to completing the turn, however the helicopter mushed through the flare and impacted the ground at a high rate of descent, and caused damage to the rear cross tube. After the immediate impact the helicopter became airborne again and collective application was used to conclude the auto with the helicopter in an upright position."

The copilot reported, "While practicing full touchdown autos with my instructor ... he asked to demonstrate a 180 degree auto. With [the instructor] at the controls, he entered the auto and began his turn to the touchdown zone. As we completed the 180 degree turn to touchdown, I noticed that the aircraft's sink rate was unusually high. As he entered the flare, the aircraft did not respond very well to the flare and as he pulled collective to cushion the touchdown, the aircraft impacted the ground very hard. The aircraft came to rest about 100 yards from the touchdown spot after which we secured the aircraft and exited normally."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC97LA041