19991102043059A

Accident · No damage

FAA accident report · Hiller UH-12E · Stites, ID · November 2, 1999

Date
November 2, 1999 · 11:18 local
Place
Stites, ID
Operating rules
General operating rules (Part 91)
Damage
No damage
Aircraft
N5388V
NTSB investigation
NTSBSEA00TA013
Reported as
Hiller UH12E
Fatal injuries
0

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) Pilot reported loss of control of helicopter when control rotor tube assembly separated from helicopter. Helicopter fell through electrical power lines before impacting terrain causing substantial damage. Pilot and one passenger sustained minor injuries. Second passenger did not sustain any injuries. Preliminary inspection of failed part, Hiller part number 36124, indicated that a crack formed at the inboard attachment bolt hole and eventually continued along the circumference of the part before the outer portion of part (cuff) separated from the helicopter. Failed control rotor assemblyhas been sent to the NTSB for metallurgical analysis.

As the FAA filed it

(-23) PILOT REPORTED LOSS OF CONTROL OF HELICOPTER WHEN CONTROL ROTOR TUBE ASSEMBLY SEPARATED FROM HELICOPTER. HELICOPTER FELL THROUGH ELECTRICAL POWER LINES BEFORE IMPACTING TERRAIN CAUSING SUBSTANTIAL DAMAGE. PILOT AND ONE PASSENGER SUSTAINED MINOR INJURIES. SECOND PASSENGER DID NOT SUSTAIN ANY INJURIES. PRELIMINARY INSPECTION OF FAILED PART, HILLER PART NUMBER 36124, INDICATED THAT A CRACK FORMED AT THE INBOARD ATTACHMENT BOLT HOLE AND EVENTUALLY CONTINUED ALONG THE CIRCUMFERENCE OF THE PART BEFORE THE OUTER PORTION OF PART (CUFF) SEPARATED FROM THE HELICOPTER. FAILED CONTROL ROTOR ASSEMBLYHAS BEEN SENT TO THE NTSB FOR METALLURGICAL ANALYSIS.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.