FTW88IA145

NTSB incident investigation · Bell 222UT · Cameron, LA · August 7, 1988

Incident · No injuriesIncident investigationFinal report
Date
August 6, 1988, 19:30 local (Aug 7, 1988, 00:30 UTC)
Place
Cameron, LA
Injuries
2 uninjured
Damage
Minor damage
Phase of flight
Enroute
Aircraft
N3190KBell 222UT
Weather
Visual (VMC) · Day
Status
Completed · report June 11, 1990
Report
Approved by Office Director
FAA report
19880806071059I
Case key
22577

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

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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.

Airframe/component/system failure/malfunctionCruise - normal
Horizontal stabilizer surface - fatigueCause
Horizontal stabilizer surface - failure,total
Maintenance,inspection - inadequateCompany maintenance personnelCause

Analysis

Plt stated that the acft pitched 20 deg nose down without warning while in cruise flt at 1,200' and 120 KTS. Following recovery, the acft required additional rt pedal to stay in trim and it flew about 10 deg nosed down in lvl flt. Flt diverted to the opr's base and landed successfully. Examination revealed that the rt horz stab had separated just outboard of the tailboom. Metallurgical examination of the separation revealed multiple fatigue origins in the areas of both the forward and aft top spar cap rivet holes and that the crack in the aft spar had been present for some time. Previous failures in this area had been attributed to working rivets causing stress concentrations in the rivet holes. Prevention of this type failure is effected by replacing the affected rivets in a timely manner. Maintenance records revealed that the left horizontal stabilizer had been repaired on 3 prior occasions, but there were no records of repairs on the rt stabilizer.

Aircraft

Registration
N3190K
Reported as
Bell 222UT
Category
Helicopter
Serial number
47531
Airframe hours
2,712
Engine
Lycoming LT5-101-750C1, 700 horsepower, turbo shaft
Damage
Minor damage
Flight
Part 135
Operator
Petroleum Helicopters, Inc.
Registered owner
Textron Financial Corp.
Airworthiness certificate
Standard, Normal
Last inspection
Continuous airworthiness · August 3, 1988 · 9 hours before
Departed
EC · East Cameron245, GM
Destination
LCH · Lake Charles, LA
Flight plan
Company VFR
Airport
Private

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
49
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Right
Flight hours
8,491 total · 958 in this make and model · 7,774 as pilot in command · 93 in the last 90 days · 46 in the last 30 days · 6 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
160° at 8 knots
Visibility
6 statute miles
Lowest ceiling
2,500 ft broken
Temperature
79 °F, dew point 73 °F
Altimeter
29.00 inHg
Observed at
PHI, 10 nm away

FAA reports on this event · 1

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