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NTSB Report

August 4, 1993 · Bell 206B · N16814

Pearland, TX

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
August 4, 1993
Injury Outcomes
No injuries (2 uninjured)
Location
Pearland, TX
Aircraft
Bell 206B
Tail Number
N16814
Injuries
None
Aircraft Damage
Substantial
NTSB Number
FTW93LA228

DURING A MAINTENANCE FLIGHT CHECK FOLLOWING A TURBINE REPLACEMENT, A TOTAL LOSS OF ENGINE POWER OCCURRED. AS THE PILOT BEGAN TO CUSHION WITH COLLECTIVE DURING THE AUTOROTATION THE HELICOPTER TOUCHED DOWN, ROCKED FORWARD AND THEN BACK. THE MAIN ROTORS SEVERED THE TAILBOOM. EXAMINATION OF THE ENGINE REVEALED A LACK OF OIL TO THE NUMBER EIGHT BEARING ASSEMBLY.

NTSB Probable Cause

PILOT'S FAILURE TO MAINTAIN PROPER ROTOR RPM, THE DELAYED FLARE, AND IMPROPER TOUCHDOWN. FACTORS WERE TOTAL FAILURE OF THE POWER TURBINE DUE TO OIL STARVATION TO THE #8 BEARING ASSEMBLY.

Full Narrative

On August 4, 1993, at 1400 central daylight time, a Bell 206B, N16814, sustained substantial damage during a forced landing near Pearland, Texas. The airline transport rated pilot and a mechanic aboard the helicopter were not injured. Visual meteorological conditions prevailed for the local maintenance check flight. The Pilot/Operator report and statement submitted by the pilot reported that he performed the preflight, and after a 10 minute ground run was cleared for takeoff. During initial climbout, at approximately 200 to 280 feet above the ground (AGL), the engine made a noise and decelerated. An autorotation was initiated to an open field. The pilot stated that "at about 30 to 40 feet I began a gentle deceleration and reduced my ground speed to about 0 at about 4 feet and waited for the aircraft to settle, then I began to cushion with collective." He further stated "the aircraft touched down and rocked forward and then back." During the backward movement, the pilot heard a loud bang. Damage to the helicopter included a severed outboard portion of the tailboom. The mechanic reported in the enclosed statement that he was aboard the helicopter for a maintenance operational flight check following a turbine replacement. He further reported that the engine "seized at about 300 feet" above the ground. Examination of the engine by the operator and FAA inspectors (enclosed statement) indicated a lack of lubrication to the number eight bearing. The representative of the engine manufacturer (enclosed report) examined the engine and found that the #8 bearing was "not fully engaged with the groove in the G. P. Support and the bearing had partially failed."

Flight

Event TypeAccident
Event Time14:00 CDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 206B
Tail NumberN16814
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · 250-C20B · Turboshaft · 420
Seats5

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 44 · Second Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility10 sm
CeilingNone
Temperature / Dew Point0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data