NYC84FA240

NTSB accident investigation · MBB BO-105C · Rehobeth, MA · July 15, 1984

Accident · FatalField investigationFinal report
Date
July 14, 1984, 22:50 local (Jul 15, 1984, 02:50 UTC)
Place
Rehobeth, MA
Injuries
2 fatal, 2 serious
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N105CPMBB BO-105C
Weather
Visual (VMC) · Night/bright
Status
Completed
Report
Approved by Office Director
FAA report
19840714040609A
Case key
35356

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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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.

Loss of engine power(total) - nonmechanicalCruise - normal
Warning system(other) - disconnectedFactor
Fuel boost pump selector position - improperPilot in commandCause
Fluid,fuel - starvationCause
Fuel system - improper use ofPilot in commandCause
Aircraft performance,two or more engines - inoperative
Forced landingLanding
Autorotation - performedPilot in command
In flight collision with objectLanding - flare/touchdown
Light condition - nightFactor
Object - wire,transmissionFactor

Analysis

The messerschmitt-blohm-boelkow BO-105C was on an air ambulance flt with a plt, 2 additional crewmembers (doctor & nurse) & a passenger (patient) on board. During flt, the plt radioed that he had lost power in 1 eng, then about 14 sec later, he radioed that the other eng had also lost power. During a forced landing/autorotation to a road at night, the helicopter collided with power lines & crashed. No fuel was found in the right supply tank & only about 1 gal of fuel was found in the left supply tank. The main tank had 15.4 gal remaining, but the respective fuel boost pump switches were found in the 'off' position. The rear main fuel tank had only slightly over 1 gal remaining. Also, an electrical wire in the low fuel warning circuit was not connected. The fuel supply to each eng is from the fuel supply tanks, which are independent of each other.

Aircraft

Registration
N105CP
Reported as
MBB BO-105C
Category
Helicopter
Serial number
S190
Airframe hours
2,722
Engine
Allison 250-C20B, 420 horsepower, turbo shaft
Damage
Destroyed
Flight
Part 135
Registered owner
Omni Flight Airways Inc.
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · June 14, 1984 · 57 hours before
Departed
MVY · Martha'S Vineyd, MA
Destination
ORH · Worcester, MA
Airport
MVY · Marthas Vineyard

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
35
Certificate
Airline transport
Instrument ratings
Helicopter
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Right
Toxicology
Performed
Flight hours
4,728 total

Weather

Conditions
Visual (VMC) · Night/bright
Wind
260° at 9 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
75 °F, dew point 64 °F
Altimeter
30.00 inHg
Observed at
PVD

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.