Loss of control Accident Enstrom Helicopter Corp 280C N51683,
ASN logo
ASN Wikibase Occurrence # 290694
 
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:Tuesday 21 January 2014
Time:17:35 LT
Type:Silhouette image of generic EN28 model; specific model in this crash may look slightly different    
Enstrom Helicopter Corp 280C
Owner/operator:Private
Registration: N51683
MSN: 1110
Year of manufacture:1977
Total airframe hrs:1285 hours
Engine model:Lycoming HIO-360 SER
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Showlow, Arizona -   United States of America
Phase: Take off
Nature:Private
Departure airport:Show Low Airport, AZ (SOW/KSOW)
Destination airport:Glendale Municipal Airport, AZ (KGEU)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot reported that just after takeoff he hovered the helicopter about two feet above the ground before starting a northwesterly takeoff run over an area of grass-covered, uneven terrain. The pilot noted that during the takeoff run, the main rotor RPM began to decay, so he added engine throttle to correct for the RPM decline. The helicopter subsequently descended and during touchdown, the left main landing gear skid collapsed. The helicopter rolled to the left, and the main rotor blades struck the ground. The helicopter sustained substantial damage to the main rotor drive system, tail boom, and fuselage.

The pilot reported that the estimated gross weight of the helicopter at takeoff was 2,300 pounds, or approximately 50 pounds under the maximum gross weight of 2,350 pounds. The density altitude was calculated to be 7,015 feet mean sea level.

The pilot reported no preaccident mechanical malfunctions or failures with the helicopter that would have precluded normal operation.

Probable Cause: The pilot's failure to maintain main rotor RPM during the takeoff run in a high density altitude environment, which resulted in a loss of aircraft control and collision with terrain.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: WPR14CA101
Status: Investigation completed
Duration: 4 months
Download report: Final report

Sources:

NTSB WPR14CA101

Location

Revision history:

Date/timeContributorUpdates
06-Oct-2022 18:15 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