Summary
On August 26, 2001, a Hughes 269B (N9390F) was involved in an incident near Pontiac, MI. All 2 people aboard were uninjured. The aircraft sustained substantial damage.
The National Transportation Safety Board determined the probable cause of this incident to be: The checklist not compiled with by the operator and not verified by the operator’s pilot and the operator's flight instructor. An additional cause was the improper autorotation by the pilot in command. The out of calibration engine idle speed was a contributing factor.
On August 26, 2001, at 1530 eastern daylight time, a Hughes 269B, N9390F, operated by Oakland Helicopters Incorporated, was substantially damaged during a simulated autorotation on runway 27R (5,000 feet by 100 feet, asphalt) at the Oakland County International Airport near Pontiac, Michigan. Visual meteorological conditions prevailed at the time of the accident. The 14 CFR Part 91 instructional flight was not operating on a flight plan. The airline transport pilot and instructor pilot were uninjured. The local flight originated at 1430.
The pilot reported in a written statement, "Engine failed during power-recovery phase of autorotational descent.
This incident is documented in NTSB report CHI01LA293. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N9390F.
Accident Details
Probable Cause and Findings
the checklist not compiled with by the operator and not verified by the operator’s pilot and the operator's flight instructor. An additional cause was the improper autorotation by the pilot in command. The out of calibration engine idle speed was a contributing factor.
Aircraft Information
Registered Owner (Current)
Analysis
On August 26, 2001, at 1530 eastern daylight time, a Hughes 269B, N9390F, operated by Oakland Helicopters Incorporated, was substantially damaged during a simulated autorotation on runway 27R (5,000 feet by 100 feet, asphalt) at the Oakland County International Airport near Pontiac, Michigan. Visual meteorological conditions prevailed at the time of the accident. The 14 CFR Part 91 instructional flight was not operating on a flight plan. The airline transport pilot and instructor pilot were uninjured. The local flight originated at 1430.
The pilot reported in a written statement, "Engine failed during power-recovery phase of autorotational descent. After touchdown, (1) main rotor blade contacted tailboom..."
Inspection of the engine idle speed by a mechanic revealed that the engine idle speed was 700-800 rpm. The Schweizer 269C Pilot's Flight Manual (PFM) states under Normal Procedures, Pilot's Check of Idle Mixture, Idle Speed, and Fuel Boost Pump, "NOTE: This check of idle mixture, idle speed, and fuel boost pump shall be accomplished at the end of the last flight each day, prior to shutdown." According to the Federal Aviaiton Administration, this check was not being conducted by the operator. The PFM also states, ...NOTE: The first check (throttle into full override) should produce an idle speed no less than 1400 rpm. The second check (throttle at normal idle stop) should produce an idle speed no greater than 1600 rpm."
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI01LA293