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Aviation safety reports, made easier to study

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NTSB Report

September 18, 1995 · Mbb BO-105C · N91070

Lafayette, LA

Overview

Report Status
Final with probable cause
Event Type
Incident
Date
September 18, 1995
Injury Outcomes
No injuries (2 uninjured)
Location
Lafayette, LA
Aircraft
Mbb BO-105C
Tail Number
N91070
Injuries
None
NTSB Number
FTW95IA397

While over 'Fast Lane,' a visual check point on the highway approach to the Lafayette Regional Airport, the helicopter 'abruptly and violently pitched nose down.' It took both pilots pulling aft on the cyclic to level the helicopter. Once control was re-established, the PIC saw that the 'hyd block' light was illuminated and the Mast Moment Indicator (MMI) limit light was on steady. The helicopter was landed without further incident. Examination and testing of the Tandem Hydraulic Unit found the System 1 hydraulic pump leaking internally. A nick and an abrasion were found in the edge of its longitudinal control slider. Metallic chips were found in the hydraulic high and low pressure filters, and one chip was found in a groove of the longitudinal control slider. The electrical portion of the 'jam-proof system,' which should activate the back-up hydraulic system two in case of a control slider jamming, only worked randomly. The connector was heavily corroded and the magnetic core of the solenoid valve had an internal short circuit.

NTSB Probable Cause

a short in the 'jam proof system' solenoid valve which prevented activation of the backup hydraulic system and resulting in a cyclic hardover. Factors were the contaminated hydraulic fluid and the resulting jammed actuator (longitudinal control slider).

Full Narrative

On September 18, 1995, at 0940 central daylight time, a MBB BO-105C, N91070, registered to, and operated by Petroleum Helicopters, Inc., as a 14 CFR Part 91 flight, experienced an in- flight uncommanded pitch down near Lafayette, Louisiana. Visual meteorological conditions prevailed and a company flight plan was filed. The helicopter was not damaged and the commercial pilots were not injured. The flight originated from Lafayette, Louisiana, about 2 hours 10 minutes before the incident. The pilots reported that, while over "Fast Lane," a visual check point on the highway approach to the Lafayette Regional Airport, Lafayette, Louisiana, the helicopter "abruptly and violently pitched nose down." It took both pilots pulling aft on the cyclic to level the helicopter. The pilot-in-command estimates the helicopter pitched down 90 degrees; however, less than 100 feet of altitude was lost. Once control was re-established, the pilot-in-command saw that the "hyd block" light was illuminated and the Mast Moment Indicator (MMI) limit light was on steady. The helicopter was landed at the Petroleum Helicopters, Inc., heliport on the Lafayette Regional Airport, without further incident. An examination of the Tandem Hydraulic Unit (THU) by Petroleum Helicopter maintenance personnel revealed that, the hydraulic system had switched to the number 2 system. After rotating the main rotor blades, the hydraulic system switched back to the number 1 system. The THU was removed and sent to the manufacturer for examination and testing. An examination and testing of the THU was accomplished on November 2, 1995. The number 1 hydraulic system did not function properly. The hydraulic pump had a loss of pressure and the hydraulic pressure switch did not indicate a loss of pressure. The hydraulic pump was found to be leaking internally. A nick and an abrasion were found in the edge of the longitudinal control slider. This control slider controls the oil flow from the actuator to the return line. Metallic chips were found in the hydraulic high and low pressure filters. A metallic chip was also found in one of the grooves of the longitudinal control slider. The electrical portion of the "jam-proof system," which should activate the back-up number 2 hydraulic system in case of a control slider jamming, only worked randomly. The connector was heavily corroded and the magnetic core of the solenoid valve had an internal short circuit. See enclosed manufacturer's report.

Flight

Event TypeIncident
Event Time09:40 CDT
Nearest Airport0nm
Runway0
Flight Plan FiledCvfr
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftMbb BO-105C
Tail NumberN91070
Aircraft CategoryHeli
Operating RulePart 91
Engines2
Engine TypeTurboshaft
Engine DetailsAllison · 250-C20 · Turboshaft · 400
Seats6

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 / 0 C
Altimeter0
Weather SourceWIT

Appendix: Source Data