# NTSB NYC02LA184: Graham Mini-500, N373TG, Renfrew, PA, September 7, 2002 - Type: NTSB accident investigation - Classification: Accident · Fatal · Limited investigation · Final report - Date: September 7, 2002, 14:00 local (18:00 UTC) - Place: Renfrew, PA - Coordinates: 40.806388, -79.964447 - Nearby events: https://openairdocs.org/map.md?lat=40.8064&lon=-79.9644&mi=10 - Phase of flight: [Enroute](https://openairdocs.org/ntsb-phases/400) (OpenAirDocs' grouping) - Highest injury: Fatal - Injuries: 1 fatal - Status: Completed, report July 23, 2003 - Report: Approved by Office Director - Parties: FAA\FSDO - NTSB case key (mKey): 55645 - NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=NYC02LA184 - NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/55645/pdf - Page: https://openairdocs.org/ntsb/NYC02LA184 ## Probable cause Failure of the main transmission. ## Sequence of events In NTSB's coding before 2008 (https://www.ntsb.gov/GILS/Documents/codman.pdf). - Airframe/component/system failure/malfunction, cruise - rotor drive system,main gearbox/transmission - failure (cause) - Loss of control - in flight, descent - uncontrolled - In flight collision with terrain/water, descent - uncontrolled - terrain condition - grass ## Analysis The amateur built helicopter was reported missing, and then located the following day. No information regarding the en route portion of the flight was available. No witnesses reported seeing the accident, and the pilot was not in radio contact with any air traffic control facilities, or automated flight service stations. The helicopter had a total of 25.6 hours of operation since construction. Examination of the wreckage revealed minor damage to both main rotor blades. Flight control continuity was confirmed from the cockpit to the main rotor and tailrotor. The transmission chip detector had metal fragments on it, the transmission oil contained suspended metal particles, and small pieces of metal were retrieved, with a magnet, from within the transmission. Examination of the engine revealed no preimpact failures or malfunctions. ## Factual narrative On September 7, 2002, about 1400 eastern daylight time, a Mini-500 homebuilt helicopter, N373TG, was substantially damaged when it impacted terrain near Renfrew, Pennsylvania. The certificated private pilot was fatally injured. Visual meteorological conditions prevailed for the personal flight that departed the Butler Farm Show Airport (3G9), Butler, Pennsylvania, destined for the Zelienople Municipal Airport (8G7), Zelienople, Pennsylvania. A flight plan was not filed, and the flight was conducted under 14 CFR Part 91. The helicopter was reported missing on September 7, 2002, and was located on September 8, 2002. No information regarding the en route portion of the flight was available. No witnesses reported seeing the accident, and the pilot was not in radio contact with any air traffic control facilities, or automated flight service stations. The accident time was approximated by using the time of departure, the distance from the departure airport to the accident site, and the amount of fuel estimated to be at the accident site. The pilot held a private pilot certificate with an airplane single engine land rating, and a helicopter rating. On his last Federal Aviation Administration (FAA) third-class medical certificate, which was dated June 7, 2001, he reported a total flight experience of 520 hours. The pilot's logbook was not located at the accident site and follow on attempts to find it were unsuccessful. According to an FAA inspector, the helicopter had a total of 25.6 hours of operation since construction. Examination of the wreckage revealed minor damage to both main rotor blades. The No. 1 tailrotor blade was bent and broken mid span, and opposite the direction of rotation. The No. 2 tailrotor blade displayed minor impact damage. Flight control continuity was confirmed from the cockpit to the main rotor and tailrotor. The transmission chip detector was removed, and metal fragments were observed. The transmission oil contained suspended metal particles, and small pieces of metal were retrieved, with a magnet, from within the transmission. Examination of the engine revealed no preimpact failures or malfunctions. The only entry in the maintenance records was date April 4, 1998, and was for certification. An autopsy was performed on the pilot at the Butler Memorial Hospital, Butler, Pennsylvania, on September 8, 2002. The FAA Toxicology and Accident Research Laboratory in Oklahoma City, Oklahoma, performed a toxicological test on the pilot on October 15, 2002. A weather observation was taken about 10 minutes before the accident at the Beaver County Airport (BVI), Beaver Falls, Pennsylvania, which was located approximately 21 miles to the west of the accident site. According to the observation, the wind was 360 degrees at 8 knots, visibility was 10 miles, ceiling was 4,000 feet broken, temperature was 73 degrees Fahrenheit, dew point was 50 degrees Fahrenheit, and the altimeter setting was 30.23 inches of mercury. According to FAA Advisory Circular AC 20-27D, Certification and Operation of Amateur-Built Aircraft, "the amateur-built program was designed to permit person(s) to build an aircraft solely for educational or recreational purposes. The FAA has always permitted amateur builders freedom to select their own designs. The FAA does not formally approve these designs since it is not practicable to develop design standards for the multitude of unique design configurations generated by kit manufacturers and amateur builders." It also stated, "Since 1983, FAA inspections of amateur-built aircraft have been limited to ensuring the use of acceptable workmanship methods, techniques, practices, and issuing operating limitations necessary to protect persons and property not involved in this activity." ## Aircraft - Registration: [N373TG](https://openairdocs.org/deregistered/N373TG-2003-10-31), registration cancelled 2003-10-31, S/N 373, built 2001 (OpenAirDocs) - Reported make and model: Graham Mini-500 - Registry model: [Graham Thomas E MINI 500](https://openairdocs.org/model/graham-thomas-e-mini-500) (registry code 05605QS) (OpenAirDocs) - Registry engine: [Bombardier ROTAX (ALL)](https://openairdocs.org/engine/bombardier-rotax-all) (registry code 09050, reciprocating) (OpenAirDocs) - Category: Helicopter, amateur-built - Serial number: 373 - Airframe hours: 25.6 - Engines: Rotax 582 67 horsepower reciprocating - Damage: Substantial damage - Flight: Personal, Part 91 - Registered owner: Thomas Graham - Airworthiness certificate: Special, Experimental (Special) - Departed: 3GN, Butler, PA - Destination: 8G7, Zelienople, PA ## Flight crew As NTSB recorded them. NTSB leaves out names. - Pilot; age 51; injuries: fatal; private; airplane ratings: single-engine land; medical: class 3, valid medical--w/ waivers/lim; seat: right; toxicology performed; flight hours: 520 total ## Weather - Conditions: Visual (VMC), Day - Wind: 360° at 8 knots - Visibility: 10 statute miles - Lowest ceiling: 4,000 ft broken - Temperature: 73 °F, dew point 50 °F - Altimeter: 30.22 inHg - Observed at: BVI, 21 nm away ## FAA reports on this event (1) The FAA's own accident and incident reports, matched to the aircraft by N-number and date (OpenAirDocs). - [Accident 20020907026789A](https://openairdocs.org/incident/20020907026789A), Sep 7, 2002: Amtr MINI500, Renfrew, PA, Destroyed, 1 fatal. (-23) On September 7, 2002 at 14:00E while enroute from butler farm show airport, butler pa. To zelienople airport, zelienople pa. N373TG an experimental… From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.