19980906022819A

Accident · Substantial damage

FAA accident report · Cessna 140 · Fairbanks, AK · September 6, 1998

Date
September 6, 1998 · 17:07 local
Place
Fairbanks, AK
Airport
Fairbanks International
Phase of flight
Normal Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N81045
NTSB investigation
NTSBANC98LA140
Reported as
Cessna 140
Reported engine
Continental C8512
People aboard
2
Fatal injuries
0
Pilot’s flight hours
433 total262 in this make and model29 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 6, 1998, at 1707 Alaska daylight time, a Cessna 140 airplane, N81045, sustained substantial damage when it nosed over during an emergency landing seven miles southeast of the Fairbanks International Airport, Fairbanks, Alaska. The private pilot owner and the sole passenger were not injured. The flight was conducted under 14 CFR part 91 as a personal flight. The flight departed clear creek butte, Alaska, at 1615, and was returning to Fairbanks from a camping trip. Visual meteorological conditions prevailed at the time of the accident, and no flight plan was filed. The pilot told the NTSB investigator-in-charge during a telephone interview on September 6, that while in cruise at 1,500 feet MSL, he heard a "clunk" and the engine RPM began to decrease. He stated that application of carburetor heat, and changing fuel tanks had no effect. The engine noise continued, and engine power continued to decrease. The pilot notified the Fairbanks air traffic control tower of his emergency, made a forced landing in tundra, and the airplane nosed over onto its back. (.4) while in cruise flight the pilot heard a 'clunk' and engine RPM immediately began to decrease. The engine noi se and RPM decrease continued, the pilot performed a forced landing in tundra, and the airplane nosed over onto its back. Postaccident inspection revealed that the exhaust valve stem of the number two cylinder had separated, and the valve was ingested into the cylinder. The engine had accumulated 4,555 hours since new, and 1,089 hours since overhaul.

As the FAA filed it

(.19) ON SEPTEMBER 6, 1998, AT 1707 ALASKA DAYLIGHT TIME, A CESSNA 140 AIRPLANE, N81045, SUSTAINED SUBSTANTIAL DAMAGE WHEN IT NOSED OVER DURING AN EMERGENCY LANDING SEVEN MILES SOUTHEAST OF THE FAIRBANKS INTERNATIONAL AIRPORT, FAIRBANKS, ALASKA. THE PRIVATE PILOT OWNER AND THE SOLE PASSENGER WERE NOT INJURED. THE FLIGHT WAS CONDUCTED UNDER 14 CFR PART 91 AS A PERSONAL FLIGHT. THE FLIGHT DEPARTED CLEAR CREEK BUTTE, ALASKA, AT 1615, AND WAS RETURNING TO FAIRBANKS FROM A CAMPING TRIP. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME OF THE ACCIDENT, AND NO FLIGHT PLAN WAS FILED. THE PILOT TOLD THE NTSB INVESTIGATOR-IN-CHARGE DURING A TELEPHONE INTERVIEW ON SEPTEMBER 6, THAT WHILE IN CRUISE AT 1,500 FEET MSL, HE HEARD A "CLUNK" AND THE ENGINE RPM BEGAN TO DECREASE. HE STATED THAT APPLICATION OF CARBURETOR HEAT, AND CHANGING FUEL TANKS HAD NO EFFECT. THE ENGINE NOISE CONTINUED, AND ENGINE POWER CONTINUED TO DECREASE. THE PILOT NOTIFIED THE FAIRBANKS AIR TRAFFIC CONTROL TOWER OF HIS EMERGENCY, MADE A FORCED LANDING IN TUNDRA, AND THE AIRPLANE NOSED OVER ONTO ITS BACK. (.4) WHILE IN CRUISE FLIGHT THE PILOT HEARD A 'CLUNK' AND ENGINE RPM IMMEDIATELY BEGAN TO DECREASE. THE ENGINE NOI SE AND RPM DECREASE CONTINUED, THE PILOT PERFORMED A FORCED LANDING IN TUNDRA, AND THE AIRPLANE NOSED OVER ONTO ITS BACK. POSTACCIDENT INSPECTION REVEALED THAT THE EXHAUST VALVE STEM OF THE NUMBER TWO CYLINDER HAD SEPARATED, AND THE VALVE WAS INGESTED INTO THE CYLINDER. THE ENGINE HAD ACCUMULATED 4,555 HOURS SINCE NEW, AND 1,089 HOURS SINCE OVERHAUL.

NTSB investigation

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