20000825011539A

Accident · No damage

FAA accident report · Hughes 369E · Coolin, ID · August 25, 2000

Date
August 25, 2000 · 14:15 local
Place
Coolin, ID
Airport
Cavanaugh Bay Airport
Operating rules
General operating rules (Part 91)
Operator
GMUA
Damage
No damage
Aircraft
N570CA
NTSB investigation
NTSBSEA00LA170
Reported as
Hughes 369E

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) The aircraft was departing with 2 passengers on board and lost power at about 15 to 20 feet altitude. A hard landing was made with substantial damage to the helicopter. There were no injures to the passengers. A safety recommendation is bing considered to address the inspector of the tot indicating gage on similar make and model helicopters. Upon investigation of the accident aicraft, there were indications and evidence of excessive engine temperatures above beyond the limits for the aircraft engine as specified in the rfm. The actual cause of the power loss is yet to be determined, pending a teardown inspection of the engine at the rolls-royce facility a t indianapolis, IN.

As the FAA filed it

(-23) THE AIRCRAFT WAS DEPARTING WITH 2 PASSENGERS ON BOARD AND LOST POWER AT ABOUT 15 TO 20 FEET ALTITUDE. A HARD LANDING WAS MADE WITH SUBSTANTIAL DAMAGE TO THE HELICOPTER. THERE WERE NO INJURES TO THE PASSENGERS. A SAFETY RECOMMENDATION IS BING CONSIDERED TO ADDRESS THE INSPECTOR OF THE TOT INDICATING GAGE ON SIMILAR MAKE AND MODEL HELICOPTERS. UPON INVESTIGATION OF THE ACCIDENT AICRAFT, THERE WERE INDICATIONS AND EVIDENCE OF EXCESSIVE ENGINE TEMPERATURES ABOVE BEYOND THE LIMITS FOR THE AIRCRAFT ENGINE AS SPECIFIED IN THE RFM. THE ACTUAL CAUSE OF THE POWER LOSS IS YET TO BE DETERMINED, PENDING A TEARDOWN INSPECTION OF THE ENGINE AT THE ROLLS-ROYCE FACILITY A T INDIANAPOLIS, IN.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.