Accident Piper PA-28-140 N6183J,
ASN logo
ASN Wikibase Occurrence # 295280
 
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. If you feel this information is incomplete or incorrect, you can submit corrected information.

Date:Friday 5 September 2003
Time:15:35 LT
Type:Silhouette image of generic P28A model; specific model in this crash may look slightly different    
Piper PA-28-140
Owner/operator:Somerset Air Service
Registration: N6183J
MSN: 28-7625228
Year of manufacture:1976
Engine model:Lycoming O-320
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Somerville, New Jersey -   United States of America
Phase: Unknown
Nature:Training
Departure airport:Readington, NJ (N51)
Destination airport:Somerville-Somerset Airport, NJ (KSMQ)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
According to the pilot of the accident airplane, while he was on the downwind leg of the traffic pattern, he heard a helicopter announce over the UNICOM frequency that he was "inbound...5 miles to the northeast." The pilot continued in the pattern, and when he was at an altitude of 100 feet on final approach, he obtained visual contact with the helicopter, which was descending towards the taxiway adjacent to runway 30, about 1/3 down the runway. The pilot then decided to initiate a go-around; however, the airplane had already "lost its lift," and only climbed to about 20-30 feet before it was blown "by the propwash of the helicopter" to the left of the runway. The right wing dropped, impacted the runway, and the airplane "cartwheeled," coming to rest on the grassy area between the runway and taxiway. A review of FAA Advisory Circular (AC) 90-23E, Wake Turbulence, revealed: "A hovering helicopter generates a downwash from its main rotor(s) similar to the "prop wash" of a conventional aircraft. However, in forward flight, this energy is transformed into a pair of strong, high-speed trailing vortices similar to wing-tip vortices of larger fixed-wing aircraft. Pilots should avoid helicopter vortices since helicopter forward flight airspeeds are often very low which generate exceptionally strong wake turbulence."


Probable Cause: The pilot's delay in executing a go-around, which resulted in an encounter with wake turbulence from a helicopter. A factor in the accident was the wake turbulence.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: NYC03LA195
Status: Investigation completed
Duration: 1 year 1 month
Download report: Final report

Sources:

NTSB NYC03LA195

History of this aircraft

Other occurrences involving this aircraft
5 September 1991 N6183J Somerset Air Service Inc. 0 Somerville, NJ sub

Revision history:

Date/timeContributorUpdates
13-Oct-2022 06:35 ASN Update Bot Added

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org