19990911026809A

Accident · Substantial damage

FAA accident report · Hiller UH-12A · Satartia, MS · September 11, 1999

Date
September 11, 1999 · 17:30 local
Place
Satartia, MS
Phase of flight
Final Approach
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N212W
NTSB investigation
NTSBATL99LA131
Reported as
Hiller UH12A
Fatal injuries
0
Pilot’s flight hours
7,644 total76 in this make and model250 in the last 90 days

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.

(.19) On September 11, 1999, at 1800 central daylight time, a Hiller UH-12A helicopter, N212W, collided with the ground while on approach to land, in Satartia, Mississippi. The helicopter was operated by the commercial pilot under the provisions of title 14 CFR part 91, and visual flight rules. Visual meteorological conditions prevailed and no flight plan was filed for the local flight. The pilot was not injured, however, the unauthorized passenger received minor injuries and the helicopter sustained substantial damage. The flight had originated about 1745. According to the pilot, he decided to land in an open area next to a soy bean field to relieve himself. He stated that during the approach to the selected landing site, he heard a loud "bang" behind him followed by the control stick moving forcefully in all directions. He stated that he had lost complete control of the helicopter resulting in a hard impact with the ground followed by the helicopter rolling onto its right side, substantially damaging the helicopter. (-23)during landing approach pilot stated he lost all cyclic control including anti torque loss. A/c landed on skids with side movement and rolled over on right side. Pilot escaped with no injuries. A passenger however sustained minor injuries. (.4)the pilot decided to land in an open area next to a soybean field due to a physical urgency. He stated that during the approach, a 'loud noise occurred' and the helicopter became 'uncontrollable,' with the control stick moving forcefully in all directions. Upon impact, the helicopter rolled onto its right side, sustaining damage to the main rotor blades, the tail boom, the skids, and the fuselage. Examination of the helicopter disclosed that the forward engine/transmission mounts had separated from the airframe. Examination of the engine mounts, however, revealed the fracture surface was consistent with overstress separation.

As the FAA filed it

(.19) ON SEPTEMBER 11, 1999, AT 1800 CENTRAL DAYLIGHT TIME, A HILLER UH-12A HELICOPTER, N212W, COLLIDED WITH THE GROUND WHILE ON APPROACH TO LAND, IN SATARTIA, MISSISSIPPI. THE HELICOPTER WAS OPERATED BY THE COMMERCIAL PILOT UNDER THE PROVISIONS OF TITLE 14 CFR PART 91, AND VISUAL FLIGHT RULES. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND NO FLIGHT PLAN WAS FILED FOR THE LOCAL FLIGHT. THE PILOT WAS NOT INJURED, HOWEVER, THE UNAUTHORIZED PASSENGER RECEIVED MINOR INJURIES AND THE HELICOPTER SUSTAINED SUBSTANTIAL DAMAGE. THE FLIGHT HAD ORIGINATED ABOUT 1745. ACCORDING TO THE PILOT, HE DECIDED TO LAND IN AN OPEN AREA NEXT TO A SOY BEAN FIELD TO RELIEVE HIMSELF. HE STATED THAT DURING THE APPROACH TO THE SELECTED LANDING SITE, HE HEARD A LOUD "BANG" BEHIND HIM FOLLOWED BY THE CONTROL STICK MOVING FORCEFULLY IN ALL DIRECTIONS. HE STATED THAT HE HAD LOST COMPLETE CONTROL OF THE HELICOPTER RESULTING IN A HARD IMPACT WITH THE GROUND FOLLOWED BY THE HELICOPTER ROLLING ONTO ITS RIGHT SIDE, SUBSTANTIALLY DAMAGING THE HELICOPTER. (-23)DURING LANDING APPROACH PILOT STATED HE LOST ALL CYCLIC CONTROL INCLUDING ANTI TORQUE LOSS. A/C LANDED ON SKIDS WITH SIDE MOVEMENT AND ROLLED OVER ON RIGHT SIDE. PILOT ESCAPED WITH NO INJURIES. A PASSENGER HOWEVER SUSTAINED MINOR INJURIES. (.4)THE PILOT DECIDED TO LAND IN AN OPEN AREA NEXT TO A SOYBEAN FIELD DUE TO A PHYSICAL URGENCY. HE STATED THAT DURING THE APPROACH, A 'LOUD NOISE OCCURRED' AND THE HELICOPTER BECAME 'UNCONTROLLABLE,' WITH THE CONTROL STICK MOVING FORCEFULLY IN ALL DIRECTIONS. UPON IMPACT, THE HELICOPTER ROLLED ONTO ITS RIGHT SIDE, SUSTAINING DAMAGE TO THE MAIN ROTOR BLADES, THE TAIL BOOM, THE SKIDS, AND THE FUSELAGE. EXAMINATION OF THE HELICOPTER DISCLOSED THAT THE FORWARD ENGINE/TRANSMISSION MOUNTS HAD SEPARATED FROM THE AIRFRAME. EXAMINATION OF THE ENGINE MOUNTS, HOWEVER, REVEALED THE FRACTURE SURFACE WAS CONSISTENT WITH OVERSTRESS SEPARATION.

NTSB investigation

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