Accident Hughes 369A N98MP,
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ASN Wikibase Occurrence # 296818
 
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Date:Wednesday 7 August 2002
Time:09:26 LT
Type:Silhouette image of generic H500 model; specific model in this crash may look slightly different    
Hughes 369A
Owner/operator:Missouri State Highway Patrol
Registration: N98MP
MSN: 680542
Year of manufacture:1968
Total airframe hrs:3181 hours
Engine model:Allison 250-C18
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Springfield, Missouri -   United States of America
Phase: Unknown
Nature:Unknown
Departure airport:Springfield, MO (3DW)
Destination airport:
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The helicopter was substantially damaged during a forced landing shortly after takeoff. The pilot stated: "Approximately one minute after departure, I felt and heard a noise in the aircraft. We were approximately 200 to 300 feet above the ground and our airspeed was approximately 60 knots. The aircraft immediately began to yaw to the right. The anti-torque pedals immediately became ineffective. I lowered the collective to prevent the aircraft from yawing all the way around. This was effective, but resulted in a loss of altitude." The aircraft impacted immediately adjacent to an interstate highway, 1.25 statute miles from the departure airport. A post accident examination revealed the tail rotor transmission housing had failed and the tail rotor assembly had departed the aircraft. It was subsequently located approximately 3/8 statute mile prior to the main impact site, along the route of flight. The NTSB Materials Laboratory examined the tail rotor transmission housing and tail rotor assembly mounting bolt. Features of the fracture surfaces on both components were consistent with overload failures. No indications of fatigue were found.

Probable Cause: Overload failure of the tail rotor transmission housing (gearbox) for undetermined reasons, which resulted in an inability to adequately control the aircraft.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: CHI02TA239
Status: Investigation completed
Duration: 1 year and 3 months
Download report: Final report

Sources:

NTSB CHI02TA239

Revision history:

Date/timeContributorUpdates
14-Oct-2022 11:07 ASN Update Bot Added

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