19990716009169A

Accident · Substantial damage

FAA accident report · Hiller UH-12C · Venice, FL · July 16, 1999

Date
July 16, 1999 · 08:10 local
Place
Venice, FL
Phase of flight
Pwr Off Vert Land/Autorotate
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N5317V
NTSB investigation
NTSBATL99LA108
Reported as
Hiller UH12C
Reported engine
Franklin O3355
People aboard
2
Fatal injuries
0
Pilot’s flight hours
1,276 total188 in this make and model101 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.

Power failure in flight. Aircraft soft landed in gulf of Mexico.(.19) on July 16, 1999, at 0812 eastern daylight time, a Hiller UH12-C, N5317V, ditched into the gulf of Mexico following a loss of engine power near Venice, Florida. 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 and one passenger were not injured and the helicopter sustained substantial damage. The helicopter departed Venice, Florida exact time unknown. Examination of the helicopter by the FAA found that the engine had sustained salt water contamination. Further examination established continuity throughout the engine and the drive train. Additionally, the mags sparked when rotated, there was oil/water in the crankcase, and there was fuel/water in the fuel tanks. (.4) according to the pilot, the helicopter lost power while flying at 50 knots and 100 feet above the ocean during a flight to record video footage of the area. The pilot made an auto-rotation into the water. Both the pilot and passenger were immediately rescued by a nearby boa t. examination of the helicopter by the FAA found that the engine had sustained salt water contamination. Further examination established continuity throughout the engine and the drive train. Additionally, the magnetos sparked when rotated, there was oil/water in the crankcase, and there was fuel/water in the fuel tanks.

As the FAA filed it

POWER FAILURE IN FLIGHT. AIRCRAFT SOFT LANDED IN GULF OF MEXICO.(.19) ON JULY 16, 1999, AT 0812 EASTERN DAYLIGHT TIME, A HILLER UH12-C, N5317V, DITCHED INTO THE GULF OF MEXICO FOLLOWING A LOSS OF ENGINE POWER NEAR VENICE, FLORIDA. 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 AND ONE PASSENGER WERE NOT INJURED AND THE HELICOPTER SUSTAINED SUBSTANTIAL DAMAGE. THE HELICOPTER DEPARTED VENICE, FLORIDA EXACT TIME UNKNOWN. EXAMINATION OF THE HELICOPTER BY THE FAA FOUND THAT THE ENGINE HAD SUSTAINED SALT WATER CONTAMINATION. FURTHER EXAMINATION ESTABLISHED CONTINUITY THROUGHOUT THE ENGINE AND THE DRIVE TRAIN. ADDITIONALLY, THE MAGS SPARKED WHEN ROTATED, THERE WAS OIL/WATER IN THE CRANKCASE, AND THERE WAS FUEL/WATER IN THE FUEL TANKS. (.4) ACCORDING TO THE PILOT, THE HELICOPTER LOST POWER WHILE FLYING AT 50 KNOTS AND 100 FEET ABOVE THE OCEAN DURING A FLIGHT TO RECORD VIDEO FOOTAGE OF THE AREA. THE PILOT MADE AN AUTO-ROTATION INTO THE WATER. BOTH THE PILOT AND PASSENGER WERE IMMEDIATELY RESCUED BY A NEARBY BOA T. EXAMINATION OF THE HELICOPTER BY THE FAA FOUND THAT THE ENGINE HAD SUSTAINED SALT WATER CONTAMINATION. FURTHER EXAMINATION ESTABLISHED CONTINUITY THROUGHOUT THE ENGINE AND THE DRIVE TRAIN. ADDITIONALLY, THE MAGNETOS SPARKED WHEN ROTATED, THERE WAS OIL/WATER IN THE CRANKCASE, AND THERE WAS FUEL/WATER IN THE FUEL TANKS.

NTSB investigation

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

Other reports on N5317V · 1

Matched to the same aircraft by N-number and date.