19970914026909A

Accident · Substantial damage

FAA accident report · Piper PA-12 · Healy River, AK · September 14, 1997

Date
September 14, 1997 · 08:30 local
Place
Healy River, AK
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N7894H
NTSB investigation
NTSBANC97LA137
Reported as
Piper PA12
Reported engine
Lycoming O235C
People aboard
1
Fatal injuries
0
Pilot’s flight hours
3,700 total50 in this make and model

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.

Aircraft crashed on landing. (.4) on September 14, 1997, at 0830 Alaska daylight time, a Piper PA-12 airplane, N7894H, sustained substantial damage when it nosed over during a precautionary landing on an 800 foot long gravel strip on the moody River, about 20 miles east of Healy, Alaska. The airline transport certificated pilot was uninjured. The flight was conducted under 14 CFR part 91 as a personal, local flight, and departed the Healy River airport, Healy, at 0800. Visual meteorological conditions prevailed at the time of the accident, and no flight plan was filed. The pilot stated in an interview with the NTSB investigator, that during climb to cruise, the engine RPM began to decrease. He said that application of carburetor heat, and switching magnetos did not correct the problem. The pilot indicated that he was making a precautionary landing at an 800 foot landing strip, and that horses were on the strip. After flying over the horses, the airplane landed on the remaining strip and bounced. The pilot attempted to abort the landing, the landing gear contacted a berm, and the airplane nosed over. The NTSB investigator interviewed the persons who recovered the airplane. They reported an unknown quantity of water in the fuel, and worn fuel tank cap gaskets. The engine was tested at an engine shop in anchorage, Alaska, and witnessed by an FAA airworthiness inspector. The engine produced a static RPM of 1,900 RPM, which is the minimum required by the type certificate. The inspector stated that cylinder compression was low, and the engine was "tired."

As the FAA filed it

AIRCRAFT CRASHED ON LANDING. (.4) ON SEPTEMBER 14, 1997, AT 0830 ALASKA DAYLIGHT TIME, A PIPER PA-12 AIRPLANE, N7894H, SUSTAINED SUBSTANTIAL DAMAGE WHEN IT NOSED OVER DURING A PRECAUTIONARY LANDING ON AN 800 FOOT LONG GRAVEL STRIP ON THE MOODY RIVER, ABOUT 20 MILES EAST OF HEALY, ALASKA. THE AIRLINE TRANSPORT CERTIFICATED PILOT WAS UNINJURED. THE FLIGHT WAS CONDUCTED UNDER 14 CFR PART 91 AS A PERSONAL, LOCAL FLIGHT, AND DEPARTED THE HEALY RIVER AIRPORT, HEALY, AT 0800. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME OF THE ACCIDENT, AND NO FLIGHT PLAN WAS FILED. THE PILOT STATED IN AN INTERVIEW WITH THE NTSB INVESTIGATOR, THAT DURING CLIMB TO CRUISE, THE ENGINE RPM BEGAN TO DECREASE. HE SAID THAT APPLICATION OF CARBURETOR HEAT, AND SWITCHING MAGNETOS DID NOT CORRECT THE PROBLEM. THE PILOT INDICATED THAT HE WAS MAKING A PRECAUTIONARY LANDING AT AN 800 FOOT LANDING STRIP, AND THAT HORSES WERE ON THE STRIP. AFTER FLYING OVER THE HORSES, THE AIRPLANE LANDED ON THE REMAINING STRIP AND BOUNCED. THE PILOT ATTEMPTED TO ABORT THE LANDING, THE LANDING GEAR CONTACTED A BERM, AND THE AIRPLANE NOSED OVER. THE NTSB INVESTIGATOR INTERVIEWED THE PERSONS WHO RECOVERED THE AIRPLANE. THEY REPORTED AN UNKNOWN QUANTITY OF WATER IN THE FUEL, AND WORN FUEL TANK CAP GASKETS. THE ENGINE WAS TESTED AT AN ENGINE SHOP IN ANCHORAGE, ALASKA, AND WITNESSED BY AN FAA AIRWORTHINESS INSPECTOR. THE ENGINE PRODUCED A STATIC RPM OF 1,900 RPM, WHICH IS THE MINIMUM REQUIRED BY THE TYPE CERTIFICATE. THE INSPECTOR STATED THAT CYLINDER COMPRESSION WAS LOW, AND THE ENGINE WAS "TIRED."

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 N7894H · 1

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