Beech K35 accident near Newberry Spring, California, August 14, 2000
On August 14, 2000 at about 7:55 pm local time, a Beech K35, registered N878R, was destroyed in an accident near Newberry Spring, California. It was a personal flight under general aviation rules (Part 91). 1 person was killed. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The crankshaft's fatigue failure at the site of an electrical arc mark stress riser, during cruise flight. Contributing factors were the pilot's inadequate preflight inspection, improper decision, and maintenance.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- August 14, 2000 · about 7:55 pm local time
- Place
- Newberry Spring, California · map
- Type
- Accident
- Injuries
- 1 person was killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Beech K35 · all K35s on the register
- Registration
- N878R · no longer on the register · serial D-6059
- Damage
- Destroyed
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
At 1247, during cruise flight, the pilot advised the radar controller that he had a little oil leak on his windshield. The severity of the leak increased, and 5 minutes later oil had covered the front windshield thus precluding visibility. One minute later, the pilot announced that he had "totally lost oil pressure." Prior to the engine seizing, the pilot attempted to make a forced landing on an interstate freeway. During flare, the airplane impacted three automobiles, cartwheeled, and came to rest upside down. Three days before the accident, the pilot had flown his airplane from Torrance, California, to Bullhead City, Arizona. En route, an engine oil leak became evident, which inhibited the pilot's ability to see through the front windshield. The pilot believed that engine oil was leaking past the engine's crankcase nose seal, aft of the propeller, and that replacing the seal would resolve the leakage problem. (Seepage had been documented in this crankshaft area during the last annual inspection that was completed 21 engine operational hours earlier.) The pilot flew 16 miles to near Needles, California, where repair services were available. Upon arrival, oil was dripping off the engine, and the pilot was advised by an engine shop to have the engine removed and repaired. The pilot declined indicating that he had insufficient funds. Instead, the pilot purchased the nose seal parts from the engine shop, and he hired a local independent mechanic to install them in his airplane. Upon completion of the maintenance, the mechanic requested that the pilot perform a ground run-up to check for leaks. The pilot declined and took off. The accident occurred about 40 minutes later, 92 miles from Needles. In 1986, about 537 engine operational hours earlier, the airplane's landing gear collapsed and the propeller was damaged. The crankcase was found cracked on its front, right side, and the engine was overhauled. The case was repaired, according to the maintenance records. During the last annual inspection, oil seepage was noted on the front, right side of the case. During the accident investigation, a weld was noted on the front, right side of the case, and electrical arc marks were noted about 2.3 inches inside the crankshaft bore. The crankshaft was found to have fractured, and the fracture had originated at the site of the arc marks creating a stress riser in the crankshaft. As the fracture progressed, it provided an avenue for oil to escape from the crankshaft and propagate through the nose seal.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
Pilot
- Certificate: flight instructor, commercial pilot
- Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
- Flight time: 2,000 hours in all; 580 in this make and model; 1,800 as pilot in command; 400 on instruments
- Last flight review: January 27, 1999
- Medical certificate: Class 2 (valid medical--w/ waivers/lim.)
- Seat: left
- Injury: fatal
The aircraft
- Airframe total time: 4,757 hours
- Last inspection: annual inspection, May 1, 2000; 21 hours since
- Maximum gross weight: 2,950 lb
- Seats: 4
- Landing gear: retractable
- Engine: Continental IO-470-C (piston); 0 hours total
The flight
- Departed from: A09 Needles AZ at 7:15 pm
- Destination: TOA Torrance CA
- Flight plan: none
Weather at the time
- Light: daylight
- Wind: from 080° at 7 knots
- Visibility: 35 statute miles
- Sky: scat at 7,000 ft
- Temperature: 104°F (40°C), dew point 45°F (7°C)
- Altimeter: 29.00 inHg
- Observation at 7:52 pm from DAG, 16 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
