# NTSB NYC04LA142: Schweizer 269C, N2065T, Norfolk, VA, June 15, 2004 - Type: NTSB accident investigation - Classification: Accident · No injuries · Limited investigation · Final report - Date: June 15, 2004, 18:20 local (22:20 UTC) - Place: Norfolk, VA - Coordinates: 36.781387, -76.448608 - Nearby events: https://openairdocs.org/map.md?lat=36.7814&lon=-76.4486&mi=10 - Phase of flight: [Landing](https://openairdocs.org/ntsb-phases/550) (OpenAirDocs' grouping) - Highest injury: No injuries - Injuries: 1 uninjured - Status: Completed, report April 28, 2005 - Report: Approved by Office Director - Parties: FAA Richmond FSDO - NTSB case key (mKey): 59472 - NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=NYC04LA142 - NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/59472/pdf - Page: https://openairdocs.org/ntsb/NYC04LA142 ## Probable cause The student pilot's failure to maintain control of the helicopter, which resulted ground resonance. Contributing to the accident was the improperly serviced landing gear dampers. ## Sequence of events In NTSB's coding before 2008 (https://www.ntsb.gov/GILS/Documents/codman.pdf). - Loss of control - on ground/water, landing - landing gear,main gear shock absorbing strut - improperly serviced (contributing factor) - ground resonance - encountered (cause) - aircraft control - not maintained, pilot in command (cause) ## Analysis The student pilot was conducting his third supervised solo flight, and had completed two takeoffs and landings. During his third landing attempt, after the helicopter contacted the ground, it began to vibrate violently. The student pilot was not able to stop the vibration, before the helicopter began to break apart. The accident was witnessed by the student pilot's flight instructor, who stated he utilized a hand-held radio to tell the student to pick up the helicopter, in order to recover. Examination of the landing skid dampers revealed that they were improperly charged. The helicopter had been operated for 371 hours since it's most recent annual inspection, which was performed about 6 months prior to the accident. The helicopter had been operated for 85 hours since it's most recent 100-hour inspection. The student pilot had accumulated 22 hours of total flight experience, all in the same make and model as the accident helicopter. ## Factual narrative On June 15, 2004, about 1820 eastern daylight time, a Schweizer 269C, N2065T, was substantially damaged while landing at Hampton Roads Executive Airport, Norfolk, Virginia. The certificated student pilot was not injured. Visual meteorological conditions prevailed and no flight plan had been filed for the solo instructional flight conducted under 14 CFR Part 91. According to a Federal Aviation Administration (FAA) inspector, the student pilot was conducting his third supervised solo flight, and had completed two takeoffs and landings. During his third landing attempt, after the helicopter contacted the ground, it began to vibrate violently. The student pilot was not able to stop the vibration, before the helicopter began to break apart. The accident was witnessed by the student pilot's flight instructor, who stated he utilized a hand-held radio to tell the student to pick up the helicopter, in order to recover. Examination of the landing skid dampers conducted by Schweizer Aircraft Corporation revealed that they were improperly charged. Three of the four dampers had maximum travel compression values in excess of that specified for their part number. According to a Schweizer representative, the improperly charged dampers would have effected their attenuation capability. The helicopter had been operated for 371 hours since it's most recent annual inspection, which was performed on December 23, 2003. The helicopter had been operated for 85 hours since it's most recent 100-hour inspection. The student pilot had accumulated 22 hours of total flight experience, all in the same make and model as the accident helicopter. According to FAA publication FAA-H-8083-21, "Rotorcraft Flying Handbook:" "Ground resonance is an aerodynamic phenomenon associated with fully-articulated rotor systems. It develops when rotor blades move out of phase with each other and cause the rotor disc to become unbalanced. This condition can cause a helicopter to self-destruct in a matter of seconds....If the rpm is low, the corrective action to stop ground resonance is to close the throttle immediately and fully lower the collective to place the blades in low pitch. If the rpm is in the normal range, you should fly the helicopter off the ground, and allow the blades to automatically realign themselves. You can then make a normal touchdown...." ## Aircraft - Registration: [N2065T](https://openairdocs.org/deregistered/N2065T-2018-01-02), registration cancelled 2018-01-02, S/N 0146 (OpenAirDocs) - Reported make and model: Schweizer 269C - Registry model: [Schweizer 269C-1](https://openairdocs.org/model/schweizer-269c-1) (registry code 8059504) (OpenAirDocs) - Category: Helicopter - Serial number: 146 - Airframe hours: 1404 - Engines: Lycoming HIO-360-D1A 190 horsepower reciprocating - Damage: Substantial damage - Flight: Instructional, Part 91 - Registered owner: Aerial Resources LLC. - Airworthiness certificate: Standard, Normal - Last inspection: Annual, December 23, 2003, 371 hours before - Departed: PVG, Norfolk, VA - Destination: PVG, Norfolk, VA - Airport: PVG, Hampton Roads Executive ## Flight crew As NTSB recorded them. NTSB leaves out names. - Student pilot; age 31; injuries: none; medical: class 2, valid medical--w/ waivers/lim; seat: right; flight hours: 22 total, 22 in this make and model ## Weather - Conditions: Visual (VMC), Day - Wind: 200° at 7 knots - Visibility: 7 statute miles - Lowest ceiling: 12,000 ft broken - Temperature: 86 °F, dew point 72 °F - Altimeter: 30.07 inHg - Observed at: NGU, 12 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 20040615023179A](https://openairdocs.org/incident/20040615023179A), Jun 15, 2004: Hughes 269C1, Portmouth, VA, Destroyed. (-23) Student pilot landed from a hover with a low RPM (2600 RPM). Aircraft entered ground resonance and destroyed itself. 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.