19990810047199A

Accident · Substantial damage

FAA accident report · Beech H35 · Swanlake, MT · August 10, 1999

Date
August 10, 1999 · 17:30 local
Place
Swanlake, MT
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N7975D
NTSB investigation
NTSBSEA99FA138
Reported as
Beech H35
Reported engine
Continental O470G
Fatal injuries
0
Pilot’s flight hours
2,158 total700 in this make and model65 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.

(-23) On August 10, 1999, a BE-35 operated by paul wells crashed into the water of spotted bear river approximately 5 miles east of spotted bear ranger station during a pleasure flight. The flight originated at tom sand's airfield with an intended destination of benchmark (3UY) airfield. No flight plan was filed and VFR conditions prevailed. The aircraft was substantially damaged and an ambulance helicopter transported pilot and single passenger to hospital in serious condition. Air ambulance medic reported that pilot indicated an engine overtemperature condition/prop vibration at 7000 feet AGL and attempted to land a spotted bear airport. (.4) the pilot observed a RPM overspeed with oil temperature rise. Throttling back relieved the overspeed situation; however, he observed a rapid loss of remaining power after turning back toward a potential emergency landing airstrip. He stated that the propeller had continued windmilling until impact. Pistons 1, 2, 4, 5, and 6 had few combustion deposits on their combustion faces. Piston 3 exhibited evidence of detonation, including a hole of about 1 inch diameter, and a combustion surface with the appearance of er osion. As originally manufactured, minimum octane requirement for this engine fuel was 91/96 octane. Teledyne Continental motors amended the recommended fuel to 100 octane after 91/96 octane fuel became obsolete. Placards on the airplane fuel tanks stated that minimum fuel required was 100 octane. No evidence was found of a supplemental type certificate for use of automotive gasoline in the subject airplane or engine. A sample of the automotive fuel removed from the airplane after the accident was tested: research octane number was 94, motor octane number was 83.8, and anti-knock index was 88.9. The pilot stated that he had been using automotive gasoline in the airplane for approximately 700 hours.

As the FAA filed it

(-23) ON AUGUST 10, 1999, A BE-35 OPERATED BY PAUL WELLS CRASHED INTO THE WATER OF SPOTTED BEAR RIVER APPROXIMATELY 5 MILES EAST OF SPOTTED BEAR RANGER STATION DURING A PLEASURE FLIGHT. THE FLIGHT ORIGINATED AT TOM SAND'S AIRFIELD WITH AN INTENDED DESTINATION OF BENCHMARK (3UY) AIRFIELD. NO FLIGHT PLAN WAS FILED AND VFR CONDITIONS PREVAILED. THE AIRCRAFT WAS SUBSTANTIALLY DAMAGED AND AN AMBULANCE HELICOPTER TRANSPORTED PILOT AND SINGLE PASSENGER TO HOSPITAL IN SERIOUS CONDITION. AIR AMBULANCE MEDIC REPORTED THAT PILOT INDICATED AN ENGINE OVERTEMPERATURE CONDITION/PROP VIBRATION AT 7000 FEET AGL AND ATTEMPTED TO LAND A SPOTTED BEAR AIRPORT. (.4) THE PILOT OBSERVED A RPM OVERSPEED WITH OIL TEMPERATURE RISE. THROTTLING BACK RELIEVED THE OVERSPEED SITUATION; HOWEVER, HE OBSERVED A RAPID LOSS OF REMAINING POWER AFTER TURNING BACK TOWARD A POTENTIAL EMERGENCY LANDING AIRSTRIP. HE STATED THAT THE PROPELLER HAD CONTINUED WINDMILLING UNTIL IMPACT. PISTONS 1, 2, 4, 5, AND 6 HAD FEW COMBUSTION DEPOSITS ON THEIR COMBUSTION FACES. PISTON 3 EXHIBITED EVIDENCE OF DETONATION, INCLUDING A HOLE OF ABOUT 1 INCH DIAMETER, AND A COMBUSTION SURFACE WITH THE APPEARANCE OF ER OSION. AS ORIGINALLY MANUFACTURED, MINIMUM OCTANE REQUIREMENT FOR THIS ENGINE FUEL WAS 91/96 OCTANE. TELEDYNE CONTINENTAL MOTORS AMENDED THE RECOMMENDED FUEL TO 100 OCTANE AFTER 91/96 OCTANE FUEL BECAME OBSOLETE. PLACARDS ON THE AIRPLANE FUEL TANKS STATED THAT MINIMUM FUEL REQUIRED WAS 100 OCTANE. NO EVIDENCE WAS FOUND OF A SUPPLEMENTAL TYPE CERTIFICATE FOR USE OF AUTOMOTIVE GASOLINE IN THE SUBJECT AIRPLANE OR ENGINE. A SAMPLE OF THE AUTOMOTIVE FUEL REMOVED FROM THE AIRPLANE AFTER THE ACCIDENT WAS TESTED: RESEARCH OCTANE NUMBER WAS 94, MOTOR OCTANE NUMBER WAS 83.8, AND ANTI-KNOCK INDEX WAS 88.9. THE PILOT STATED THAT HE HAD BEEN USING AUTOMOTIVE GASOLINE IN THE AIRPLANE FOR APPROXIMATELY 700 HOURS.

NTSB investigation

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