Aircraft Accident/Incident Report

Hoover Dam, Arizona 86023
Monday, September 18, 2000 8:15 MST

NTSB Narrative Summary Released at Completion of Accident

The helicopter was being operated as a sightseeing flight to the Grand Canyon. The pilot reported that during cruise flight the rotor and engine noise suddenly decreased and the helicopter began a descent. During the ensuing forced landing, the helicopter landed hard. The helicopter was fabricated from an ex-military remanufactured and modified Sikorsky S-55 (UH-19D). The original radial reciprocating engine had been replaced with a Garrett Gas Turbine TPE 331 modified to a TSE 331 IOUA 511SW. It had a 6,000-hour time between overhaul. According to maintenance records dating back to July 3, 1985, the accident engine P-54083 operated in more than one Fairchild SA226 airplane in Australia, and several rotary wing S-55 aircraft during their certification in the United States. Following the accident the engine was shipped to the modifier for functional testing in a cell. The engine started and idled normally. Increasing the rpm to the certified operating specification of 101.5 percent revealed no abnormal conditions. The test propeller was moved from the start locks and increasing torque load was applied. As the torque was increased the engine responded normally until approximately 60 percent torque when the indicated engine rpm rapidly decreased and an emergency shutdown was initiated. The process was repeated through 12 cycles, during which the indicated rpm began a sudden rapid decrease when torque was increased. Test cell troubleshooting failed to identify or correct this condition. During manual rotation of the propeller following the final cycle some "slipping" was noted between the output shaft and the main rotating group. Subsequent examination of the gearbox revealed disengagement of the sun and bull gear assembly. Examination revealed fretting damage to the retaining nut and mating surfaces related to loss of specified torque. Visual examination of the sun and bull gears revealed severe damage to the mating splines of both gears. About 9 months before the accident the original manufacturer issued a service bulletin providing for the replacement of the affected components; the engine modifier recommended replacement of the components prior to further operation. Examination of past oil analysis samplings revealed increases of iron and magnesium over a period of time, with analysis report comments of "Alert" and "Iron Appears High."

NTSB Probable Cause Narrative

The failure of maintenance personnel to accomplish a service bulletin addressing the potential failure of engine drive gears, and the ignored oil analysis testing results that indicated an impending internal engine failure that subsequently resulted in the loss of engine drive to the main rotor during flight.

Event Information

Type of Event Accident
Event Date 9/18/2000
Event Day of the Week Monday
Time of Event 815
Event Time Zone Mountain Standard Time
Event City HOOVER DAM
Event State ARIZONA
Event Country --
Zipcode of the event site 86023
Event Date Year 2000
Event Date Month 9
MidAir Collision Indicator No
On Ground Collision occurred ? No
Event Location Latitude --
Event Location Longitude --
Event Location Airport --
Event Location Nearest Airport ID --
Indicates whether the acc/inc occurred off or on an airport Off Airport/Airstrip
Distance from airport in statute miles --
Degrees magnetic from airport --
Airport Elevation --
Weather Briefing Completeness Unknown
Investigator's weather source Weather Observation Facility
Time of the weather observation 756 Pacific Daylight Time
Direction of event from weather observation facility (degrees) 270
Weather Observation Facility ID LAS
Elevation of weather observation facility 2177
Distance of event from weather observation facility (units?) 30
Time Zone of the weather observation PDT
Lighting Conditions Day
Lowest Ceiling Height --
Lowest Non-Ceiling Height --
Sky/Lowest/Cloud Conditions Clear
Sky Condition for Lowest Ceiling None
Visibility Runway Visual Range (Feet) --
Visibility Runway Visual Value (Statute Miles) --
Visibility (Statute Miles) 10
Air Temperature at event time (in degrees celsius) 29
Dew Point at event time (in degress fahrenheit) 4
Wind Direction (degrees magnetic) 20
Variable Wind Indicator Wind direction could be determined
Wind Speed (knots) 8
Wind Velocity Indicator --
Wind Gust Indicator Unknown
Wind Gust (knots) --
Altimeter Setting at event time (in. Hg) 29.99
Density Altitude (feet) --
Intensity of Precipitation --
METAR weather report --
Event Highest Injury Minor
On Ground, Fatal Injuries 0
On Ground, Minor Injuries 0
On Ground, Serious Injuries 0
Injury Total Fatal --
Injury Total Minor 7
Injury Total None --
Injury Total Serious --
Injury Total All 7
Investigating Agency NTSB
NTSB Docket Number (internal use) 12341
NTSB Notification Source --
NTSB Notification Date Sep 18 2000 12:00AM
NTSB Notification Time 943
Fiche Number and/or location -used to find docket information DMS
Date of most recent change to record Oct 24 2002 3:20PM
User who most recently changed record NTSB\MONR
Basic weather conditions Visual Meteorological Cond
FAA District Office --

Aircraft Involved

Aircraft #1

Aircraft Registration Number N17754
NTSB Number LAX00FA342
Missing Aircraft Indicator N
Federal Aviation Reg. Part Part 135: Air Taxi & Commuter
Type of Flight Plan filed Company VFR
Flight plan Was Activated? No
Damage Substantial
Aircraft Fire None
Aircraft Explosion None
Aircraft Manufacturer's Full Name Sikorsky/Orlando
Aircraft Model S-55
Aircraft Series Identifier S-55
Aircraft Serial Number V55-398T
Certified Max Gross Weight 7700
Aircraft Category Helicopter
Aircraft Registration Class U.S. Registered/U.S. Soil
Aircraft is a homebuilt? No
Flight Crew Seats --
Cabin Crew Seats --
Passenger Seats --
Total number of seats on the aircraft 7
Number of Engines 1
Fixed gear or retractable gear Fixed
Aircraft, Type of Last Inspection 100 Hour
Date of Last Inspection Apr 19 2000 12:00AM
Airframe hours since last inspection 91
Airframe Hours 487
ELT Installed No
ELT Activated No
ELT Aided Location of Event Site No
ELT Type --
Aircraft Owner Name Foxtrot Inc.
Aircraft Owner Street Address 12515 Willows Rd. NE Ste 200
Aircraft Owner City Kirkland
Aircraft Owner State WA
Aircraft Owner Country --
Aircraft Owner Zipcode 98034
Operator is an individual? No
Operator Name PAPILLON HELICOPTERS INC.
Operator Same as Owner? No
Operator Is Doing Business As --
Operator Address Same as Owner? No
Operator Street Address P.O.BOX 455/HWY 64
Operator City GRAND CANYON
Operator State AZ
Operator Country --
Operator Zip code 86023
Operator Code PG9A
Owner has at least one certificate --
Other Operator of large aircraft? --
Certified for Part 133 or 137 Operation --
Operator Certificate Number --
Indicates whether an air carrier operation was scheduled or not Non-scheduled
Indicates Domestic or International Flight Domestic
Operator carrying Pax/Cargo/Mail Passenger Only
Type of Flying (Per_Bus / Primary) --
Second Pilot on Board No
Departure Point Same as Event No
Departure Airport Code LAS
Departure City LAS VEGAS
Departure State NV
Departure Country USA
Departure Time 730
Departure Time Zone PDT
Destination Same as Local Flt --
Destination Airport Code GCN
Destination City GRAND CANYON
Destination State AZ
Destination Country USA
Specific Phase of Flight Cruise
Report sent to ICAO? --
Evacuation occurred No
Date of most recent change to record May 11 2004 2:21PM
User who most recently changed record NTSB\HAMG
Since inspection or accident Time of Accident
Event Location Runway Number and Location --
Runway Length --
Runway Width --
Sight Seeing flight Yes
Air Medical Flight No
Medical Flight --