# NTSB GAA18CA060: Hughes 300, N9685F, Woodlawn, VA, November 22, 2017

- Type: NTSB accident investigation
- Classification: Accident · No injuries · Data collection · Final report
- Date: November 22, 2017, 11:00 local (16:00 UTC)
- Place: Woodlawn, VA
- Coordinates: 36.771945, -80.89833 (estimated)
- Nearby events: https://openairdocs.org/map.md?lat=36.7719&lon=-80.8983&mi=10
- Phase of flight: [Landing](https://openairdocs.org/ntsb-phases/550) (OpenAirDocs' grouping)
- Defining event: [Landing: Loss of control in flight](https://openairdocs.org/ntsb-events/240)
- Highest injury: No injuries
- Injuries: 2 uninjured
- Status: Completed, report February 21, 2018
- Report: Approved by Office Director
- NTSB office: General Aviation Accidents
- Parties: FAA
- NTSB case key (mKey): 96388
- NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=GAA18CA060
- NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/96388/pdf
- NTSB docket: https://data.ntsb.gov/Docket?ProjectID=96388
- Page: https://openairdocs.org/ntsb/GAA18CA060

## Probable cause

The pilot’s inappropriate descent profile during landing with a quartering gusting tailwind, which resulted in a loss of main rotor rpm.

## Findings

NTSB's coded findings; those marked are part of the probable cause.

- [Performance/control parameters: descent/approach/glide path](https://openairdocs.org/ntsb-findings/01062040): Aircraft › Aircraft oper/perf/capability · Not attained/maintained (probable cause); cases with it: [Hughes 269C, 1 case](https://openairdocs.org/ntsb-findings/01062040/cases.md?model=4470504), [All aircraft, 809 cases](https://openairdocs.org/ntsb-findings/01062040/cases.md)
- [Use of equip/info: aircraft control](https://openairdocs.org/ntsb-findings/02063040): Personnel issues › Task performance · Pilot (probable cause); cases with it: [Hughes 269C, 11 cases](https://openairdocs.org/ntsb-findings/02063040/cases.md?model=4470504), [All aircraft, 9,295 cases](https://openairdocs.org/ntsb-findings/02063040/cases.md)
- [Wind: tailwind](https://openairdocs.org/ntsb-findings/03034015): Environmental issues › Conditions/weather/phenomena · Effect on operation; cases with it: [Hughes 269C, 1 case](https://openairdocs.org/ntsb-findings/03034015/cases.md?model=4470504), [All aircraft, 594 cases](https://openairdocs.org/ntsb-findings/03034015/cases.md)
- [Wind: gusts](https://openairdocs.org/ntsb-findings/03034045): Environmental issues › Conditions/weather/phenomena · Effect on operation; cases with it: [Hughes 269C, 2 cases](https://openairdocs.org/ntsb-findings/03034045/cases.md?model=4470504), [All aircraft, 1,199 cases](https://openairdocs.org/ntsb-findings/03034045/cases.md)

## Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event best describes what happened.

- [Landing: Miscellaneous/other](https://openairdocs.org/ntsb-events/900); cases with it: [Hughes 269C, 1 case](https://openairdocs.org/ntsb-events/900/sequence.md?model=4470504), [All aircraft, 1,556 cases](https://openairdocs.org/ntsb-events/900/sequence.md)
- [Landing: Loss of control in flight](https://openairdocs.org/ntsb-events/240) (defining event); cases with it: [Hughes 269C, 8 cases](https://openairdocs.org/ntsb-events/240/sequence.md?model=4470504), [All aircraft, 5,002 cases](https://openairdocs.org/ntsb-events/240/sequence.md)
- [Landing: Attempted remediation/recovery](https://openairdocs.org/ntsb-events/060); cases with it: [Hughes 269C, 2 cases](https://openairdocs.org/ntsb-events/060/sequence.md?model=4470504), [All aircraft, 1,422 cases](https://openairdocs.org/ntsb-events/060/sequence.md)
- [Landing: Settling with power/vortex ring state](https://openairdocs.org/ntsb-events/244); cases with it: [Hughes 269C, 2 cases](https://openairdocs.org/ntsb-events/244/sequence.md?model=4470504), [All aircraft, 52 cases](https://openairdocs.org/ntsb-events/244/sequence.md)
- [Landing: Landing area undershoot](https://openairdocs.org/ntsb-events/370); cases with it: [Hughes 269C, 1 case](https://openairdocs.org/ntsb-events/370/sequence.md?model=4470504), [All aircraft, 201 cases](https://openairdocs.org/ntsb-events/370/sequence.md)
- [Landing: Collision with terr/obj (non-CFIT) ](https://openairdocs.org/ntsb-events/470); cases with it: [Hughes 269C, 10 cases](https://openairdocs.org/ntsb-events/470/sequence.md?model=4470504), [All aircraft, 10,189 cases](https://openairdocs.org/ntsb-events/470/sequence.md)
- [Landing: Roll over](https://openairdocs.org/ntsb-events/097); cases with it: [Hughes 269C, 3 cases](https://openairdocs.org/ntsb-events/097/sequence.md?model=4470504), [All aircraft, 261 cases](https://openairdocs.org/ntsb-events/097/sequence.md)

## Analysis

The helicopter pilot reported that he was landing on a pad in a confined area. He added that, as he approached the landing pad, he slowed the helicopter to transition to a hover. The main rotor rpm began to drop, and he applied full throttle, but the rpm continued to decline. The helicopter was unable to maintain altitude and slowly settled into the trees on the hillside about 20 ft short of the landing pad. Subsequently, the helicopter struck the trees and rolled onto its right side. The helicopter sustained substantial damage to the fuselage and main rotor system. The pilot reported that there were no preaccident mechanical failures or malfunctions with the helicopter that would have precluded normal operation. The pilot reported that, after the accident, he noticed there was a significant right quartering tailwind, which required the application of more left pedal than anticipated. He further explained that the increased application of antitorque pedal lessened the available power to maintain the main rotor rpm. He concluded that the approach could have been completed safely with a steeper and faster approach to better manage engine power.

## Factual narrative

The helicopter pilot reported that, he was landing on a pad in a confined area. He added that, as he approached the landing pad, he slowed the helicopter to transition to a hover. The main rotor RPM began to drop and he applied full throttle, but the RPM continued to decline. The helicopter was unable to maintain altitude and slowly settled into the trees on the hillside about 20 ft. short of the landing pad. Subsequently, the helicopter struck the trees, and rolled onto its right-side. The helicopter sustained substantial damage to the fuselage and main rotor system. The pilot reported that there were no preaccident mechanical failures or malfunctions with the helicopter that would have precluded normal operation. The pilot reported that, after the accident, he noticed there was a significant right quartering tailwind, which required the application of more left pedal than anticipated. He further explained that the increased application of anti-torque pedal lessened the available power to maintain the main rotor RPM. He concluded the approach could have been completed safely with a steeper and faster approach to better manage engine power.

## Aircraft

- Registration: [N9685F](https://openairdocs.org/deregistered/N9685F-2020-05-08), registration cancelled 2020-05-08, S/N 620147, built 1972 (OpenAirDocs)
- Reported make and model: HUGHES 300 (C)
- Registry model: [Hughes 269C](https://openairdocs.org/model/hughes-269c) (registry code 4470504) (OpenAirDocs)
- Registry engine: [Lycoming I0360 series](https://openairdocs.org/engine/lycoming-i0360-series) (registry code 41515, reciprocating) (OpenAirDocs)
- Category: Helicopter
- Serial number: 620147
- Year built: 1972
- Airframe hours: 5598
- Engines: Lycoming HIO-360-D1A 190 horsepower reciprocating
- Damage: Substantial damage
- Fire: On-Ground
- Flight: Personal, Part 91
- Airworthiness certificate: Standard, Normal
- Last inspection: Annual, August 8, 2017
- Departed: HLX, GALAX HILLSVILLE, VA
- Destination: Woodlawn, VA
- Equipment: Handheld GPS

## Flight crew

As NTSB recorded them. NTSB leaves out names.

- Pilot; age 64; injuries: none; flight instructor, airline transport; airplane ratings: single-engine sea, single-engine land, multi-engine land; instrument ratings: airplane; medical: basicmed; last flight review July 26, 2017; seat: left; restraint: 4-point; flight hours: 4,241 total, 127 in this make and model, 4,173 as pilot in command, 34 in the last 90 days, 9 in the last 30 days, 1 in the last 24 hours

## Weather

- Conditions: Visual (VMC), Day
- Wind: 320° at 17 knots, gusting 25
- Visibility: 10 statute miles
- Lowest ceiling: none
- Temperature: 45 °F, dew point 28 °F
- Altimeter: 30.05 inHg
- Observed at: KHLX, 4 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 20171122019709A](https://openairdocs.org/incident/20171122019709A), Nov 22, 2017: Hughes 269C, Woodlawn, VA, Destroyed. While on a short final approach to a landing area, the pilot attempted to enter into a hover while out of ground effect. Due to gusty winds and being out of…

## Other investigations on N9685F (1)

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.

- [NTSB CHI76DEM24](https://openairdocs.org/ntsb/CHI76DEM24), Jan 5, 1976: Hughes 269C (N9685F), Saginaw, MI, substantial damage

## Docket (2 files)

The files NTSB released with the investigation on January 25, 2018, on NTSB's docket system: https://data.ntsb.gov/Docket?ProjectID=96388. 1.5 MB in all.

- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1 (item 1, .PDF, 895 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40459550&FileExtension=.PDF&FileName=Pilot%2FOperator%20Aircraft%20Accident%20Report,%20NTSB%20Form%206120.1-Master.PDF
- Accident Photo (Courtesy of FAA) (item 2, .PDF, 1 photo, 587 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40459551&FileExtension=.PDF&FileName=Accident%20Photo%20(Courtesy%20of%20FAA)-Master.PDF

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.

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