NYC92GA089

NTSB accident investigation · Mcdonnell Douglas 500E · Mount Zion, KY · April 30, 1992

Accident · No injuriesFinal report
Date
April 30, 1992, 13:25 local (17:25 UTC)
Place
Mount Zion, KY
Injuries
3 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N97BRMcdonnell Douglas 500E
Weather
Visual (VMC) · Day
Status
Completed · report May 26, 1993
Report
Approved by Office Director
Case key
37075

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

An in-flight separation of the tail rotor assembly as the result of the loss of an abrasion strip from the leading edge of one of the tail rotor blades, which induced vibrational stresses high enough to initiate fatigue failure in the tail rotor gear box mounting studs.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Airframe/component/system failure/malfunctionCruise - normal
Rotor system,tail rotor blade abrasion strip - disconnectedCause
Material inadequateCompany maintenance personnelFactor
Rotor drive system,tail rotor gearbox(90 deg) - separationCause
Aircraft control - not possiblePilot in command
Forced landingDescent - emergency
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - ground

Analysis

While flying in a cruise configuration at 1500 feet mean sea level, and about 10 minutes into the flight the helicopter started to vibrate. The pilot elected to make a forced landing in the most suitable area available. During the descent the vibration continued to worsen. At about 5 feet above the selected landing site the pilot heard a loud bang, the helicopter yawed to the right and pitched nose down. The pilot lowered the collective and put the helicopter on the ground. Metallurgical examination determined that the loss of the abrasion strip from the leading edge of tail rotor blade s/n 5086 induced vibrational stresses that were high enough to initiate fatigue failure in the tail rotor gear box mounting studs which resulted in the separation of the gear box assembly from the helicopter.

Aircraft

Registration
N97BR
Reported as
Mcdonnell Douglas 500E
Category
Helicopter
Serial number
145E
Airframe hours
1,350
Engine
Allison 250-C-20D, 420 horsepower, turbo shaft
Damage
Substantial damage
Flight
Public aircraft · Part 91
Operator
US Customs Service
Registered owner
US Customs Service
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · January 2, 2000 · 59 hours before
Departed
CVG · Cincinnati, OH
Destination
CVG
Flight plan
Company VFR

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
37
Certificates
Flight instructor, Airline transport, Commercial
Airplane ratings
Single-engine sea, Multi-engine sea, Single-engine land, Multi-engine land
Instrument ratings
Helicopter, Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
5,750 total · 500 in this make and model · 4,700 as pilot in command · 150 in the last 90 days · 50 in the last 30 days · 6 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
25 statute miles
Lowest ceiling
None
Temperature
75 °F
Altimeter
30.00 inHg