LAX87FA112

NTSB accident investigation · Hughes 369D · Honolulu, HI · February 9, 1987

Accident · FatalField investigationFinal report
Date
February 8, 1987, 15:30 local (Feb 9, 1987, 01:30 UTC)
Place
Honolulu, HI
Injuries
1 fatal, 2 serious, 2 minor
Damage
Destroyed
Phase of flight
Initial climb
Aircraft
N1102UHughes 369D
Weather
Visual (VMC) · Day
Status
Completed · report February 20, 1989
Report
Approved by Office Director
Safety recommendations
Yes
FAA report
19870208050329A
Case key
25378

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.

Airframe/component/system failure/malfunctionTakeoff - initial climb
Rotor system,main rotor hub - corrodedCause
Maintenance,service of aircraft/equipment - inadequateCompany maintenance personnelFactor
Rotor system,main rotor hub - fatigueCause
Maintenance,inspection - improperCompany maintenance personnelCause
Maintenance,recordkeeping - inadequateFactor
Maintenance,service bulletin/letter - not followedCompany maintenance personnelFactor
Rotor system,main rotor blade - separationCause
Fuselage - vibration
Misc rotorcraft,tail boom - overload
Loss of control - in flightTakeoff - initial climb
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - water,rough

Analysis

Drg tkof clb, a loud noise occurred as 1 of 5 main rotors (mrb's) & the tail boom sepd fm the helicopter (hel). The hel then crashed & hit a submerged reef aprx 200' fm the heliport. An exam of the failed mrb showed its retention strap assy(rsa), pn 369D21210-501, failed fm fatigue in an area of corrosion; 11 of the mrb's 16 strap laminates had preexisting cracks. Corrosion was fnd on 78 of 80 laminates. The maint hndbk reqd the rsa's be inspected at 25, 100 & 600 hr inter- vals. Svc info notice (sin) DN-77.1 rdmdd a 300 hr inspn if any crack or laminate failure was fnd drg a 100 hr inspn. Ad's 77-15-09R1 & 81-10-08 reqd inspn w/i (but not outbrd of) the pitch housing. Drg 100 hr/ad inspns after 1768 & 1839 hrs of opn, up to 3 cracks were fnd in laminate legs, but their lctns were not documented for ltr inspn. However, drg 2 subsequent 100 hr inspns by another mech, no cracked laminates were noted. The hel had 2135 hrs of opn when the acdnt occurred. Svc info ltr DL-54 rcmdd a tri-flow wash proc after the last flt of each day when opng in a marine environment

Aircraft

Registration
N1102U
Reported as
Hughes 369D
Category
Helicopter
Serial number
100820D
Airframe hours
2,135
Engine
Allison 250-C20B, 375 horsepower, turbo shaft
Damage
Destroyed
Flight
Part 91
Registered owner
Royal Helicopter Inc.
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · January 13, 1987 · 94 hours before
Flight plan
Company VFR
Airport
Z06 · Ala Wai Heliport

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
44
Certificates
Commercial, Private
Airplane ratings
Single-engine land
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Toxicology
Performed
Flight hours
8,518 total · 4,078 in this make and model · 7,950 as pilot in command · 134 in the last 90 days · 36 in the last 30 days · 7 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
220° at 8 knots
Visibility
20 statute miles
Lowest ceiling
None
Temperature
81 °F, dew point 64 °F
Altimeter
29.00 inHg
Observed at
HNL, 6 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.