ATL05CA083 · Rand Robinson Engineering KR-2
Rand Robinson Engineering KR-2 · Accident: airframe, component or system failure en route
From Cobb County International Airport-McCollum Field (RYY) to Valdosta Regional Airport (VLD)
Event
- NTSB case
- ATL05CA083
- Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
- Accident
- InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
- Completed
- API-reported fatalities
- 0 · all aircraft and ground
- Ground fatalities
- Unknown
- OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
- General aviation
- WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
- Visual Meteorological Cond
Rand Robinson Engineering KR-2
- Aircraft type
- Rand Robinson Engineering KR-2
- Category
- Airplane
- RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
- N1701L
- Operator
- Robert E. Lester · private individual
- Onboard fatalities
- Unknown
- Route
- From Cobb County International Airport-McCollum Field (RYY), Marietta, GATo Valdosta Regional Airport (VLD), Valdosta, GA
- Aircraft age
- Not recorded
- Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
- Part 91: General Aviation
- Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
- En route · cruise
- First occurrenceThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
- Airframe, component or system failure
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Substantial
Cause areas
- Engine assembly, crankshaft › Fractured
- Engine assembly, crankshaft › Overload
- Owner/pilot mechanic › Maintenance, balancing, inadequate
- Owner/pilot mechanic › Maintenance, modification, inadequate
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
While flying at 3,500 feet the pilot noticed that the engine was losing power and vibrating. The pilot stated that he shut the engine off and decided to make an emergency landing. The pilot first attempted to make it to a crop duster airstrip, but could not, and decided to attempt a landing on the highway. The airplane landed on a westerly heading, veered off the highway, hit an embankment and rotated 180-degrees to the left and came to rest on an easterly heading. Examination of the engine revealed the crankshaft was broken just behind the front main bearing before the crankshaft exits the engine and attaches to the propeller. The post-accident examination revealed that the crankshaft had an extension between it and the propeller in order for it to clear the cowling. Maintenance records showed that on May 3, 2005, the propeller extension was found to be out of true and the shaft, propeller and spinner combination were balanced. At the accident site, it was observed that washers were affixed to the back of the propeller spinner and the propeller spinner contained voids in the fiberglass. It was also noted that the crankshaft broke approximately 8.2 hours after the shaft, propeller and spinner combination were balanced.
Probable cause
A loss of engine power due to the owner/pilot mechanic's improper balancing of the modification to engine crankshaft which resulted in an overload failure.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ATL05CA083
- Event ID
- 20050616X00780
- Case number
- ATL05CA083
- Dataset
- historical-pre2008
- Source SHA-256
- 89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
Source notes (4)
- Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
- Filled from the NTSB case API where the bulk record had no value: investigation status, coordinates. Values present in the bulk record are kept.
- The date is the local date, which is the same as the UTC date the NTSB stores.
- API snapshot SHA-256: 398bda41cf4478416ef263eb555593d64eba0064de3a25f8f518be2494de8bcb; retrieved 2026-09-21T19:01:31.780Z.