19980725017549A

Accident · Substantial damage

FAA accident report · Enstrm F-28F · Skwentna, AK · July 25, 1998

Date
July 25, 1998 · 14:00 local
Place
Skwentna, AK
Phase of flight
Pwr On Vertical Ldng/Rtrcrft
Operating rules
Air taxi and commuter (Part 135)
Operator
EMVC
Damage
Substantial damage
Aircraft
N8622U
NTSB investigation
NTSBANC98LA109
Reported as
Enstrm F28F
Reported engine
Lycoming HIO360*
People aboard
2
Fatal injuries
0
Pilot’s flight hours
11,000 total1,200 in this make and model200 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.

Crashed en route, anchoragae, AK. (-23) on July 25, 1998, at approximately 1400, Alaska daylight time, an Enstrom F28F, N8622U helicopter landed hard after experiencing a loss of power, while counting fish for the department of fish and game on the upper talachulitna river. There were no injuries. The commercial certificated pilot was operating the flight in visual meteorological conditions. The pilot stated, during a telephone conversation, that after landing, he an exhaust gasket completely "completely blow out." The heat from the blown gasket apparently heated a bolt on the intake manifold and caused it to break and cause the intake manifold to come loose. The helicopter would not maintain operating RPM and the pilot was forced to land the helicopter. He also stated that the landing he made was a little downwind with low RPM, as he was unable to regain full RPM due to the mechanical failure. The helicopter sustained substantil damage to the main rotor blades and the tail rotor gear box during landing. (.4) the certificated commercial helicopter pilot was conducting a salmon survey for the state of Alaska, department of fish & game. This operation required him to hover the helicopter over the stream while the passenger, a wildlife biologist employed by the state of Alaska, noted the number of fish. The pilot stated that while in a hover above the stream, he felt a slight vibration followed by a partial loss of engine power. He said that while hover taxiing the helicopter to a suitable landing area, the engine continued to lose power, and he was forced to make a downwind autorotation. He said that as the helicopter touched down, the main rotor blades flexed downward, and struck the tail boom. The helicopter's tail boom, and tail rotor gearbox sustained substantial damage. The operator reported that during a postaccident inspection of the engine, a fractured intake manifold flange was discovered on the number three cylinder assembly.

As the FAA filed it

CRASHED EN ROUTE, ANCHORAGAE, AK. (-23) ON JULY 25, 1998, AT APPROXIMATELY 1400, ALASKA DAYLIGHT TIME, AN ENSTROM F28F, N8622U HELICOPTER LANDED HARD AFTER EXPERIENCING A LOSS OF POWER, WHILE COUNTING FISH FOR THE DEPARTMENT OF FISH AND GAME ON THE UPPER TALACHULITNA RIVER. THERE WERE NO INJURIES. THE COMMERCIAL CERTIFICATED PILOT WAS OPERATING THE FLIGHT IN VISUAL METEOROLOGICAL CONDITIONS. THE PILOT STATED, DURING A TELEPHONE CONVERSATION, THAT AFTER LANDING, HE AN EXHAUST GASKET COMPLETELY "COMPLETELY BLOW OUT." THE HEAT FROM THE BLOWN GASKET APPARENTLY HEATED A BOLT ON THE INTAKE MANIFOLD AND CAUSED IT TO BREAK AND CAUSE THE INTAKE MANIFOLD TO COME LOOSE. THE HELICOPTER WOULD NOT MAINTAIN OPERATING RPM AND THE PILOT WAS FORCED TO LAND THE HELICOPTER. HE ALSO STATED THAT THE LANDING HE MADE WAS A LITTLE DOWNWIND WITH LOW RPM, AS HE WAS UNABLE TO REGAIN FULL RPM DUE TO THE MECHANICAL FAILURE. THE HELICOPTER SUSTAINED SUBSTANTIL DAMAGE TO THE MAIN ROTOR BLADES AND THE TAIL ROTOR GEAR BOX DURING LANDING. (.4) THE CERTIFICATED COMMERCIAL HELICOPTER PILOT WAS CONDUCTING A SALMON SURVEY FOR THE STATE OF ALASKA, DEPARTMENT OF FISH & GAME. THIS OPERATION REQUIRED HIM TO HOVER THE HELICOPTER OVER THE STREAM WHILE THE PASSENGER, A WILDLIFE BIOLOGIST EMPLOYED BY THE STATE OF ALASKA, NOTED THE NUMBER OF FISH. THE PILOT STATED THAT WHILE IN A HOVER ABOVE THE STREAM, HE FELT A SLIGHT VIBRATION FOLLOWED BY A PARTIAL LOSS OF ENGINE POWER. HE SAID THAT WHILE HOVER TAXIING THE HELICOPTER TO A SUITABLE LANDING AREA, THE ENGINE CONTINUED TO LOSE POWER, AND HE WAS FORCED TO MAKE A DOWNWIND AUTOROTATION. HE SAID THAT AS THE HELICOPTER TOUCHED DOWN, THE MAIN ROTOR BLADES FLEXED DOWNWARD, AND STRUCK THE TAIL BOOM. THE HELICOPTER'S TAIL BOOM, AND TAIL ROTOR GEARBOX SUSTAINED SUBSTANTIAL DAMAGE. THE OPERATOR REPORTED THAT DURING A POSTACCIDENT INSPECTION OF THE ENGINE, A FRACTURED INTAKE MANIFOLD FLANGE WAS DISCOVERED ON THE NUMBER THREE CYLINDER ASSEMBLY.

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 N8622U · 1

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