ERA24LA388 · Cessna 172K
Cessna 172K · Accident: loss of engine power (total) during initial climb
Event
- NTSB case
- ERA24LA388
- 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
- 0
- 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
Cessna 172K
- Aircraft type
- Cessna 172
- 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
- N7037G
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From not recordedTo not recorded
- Aircraft age
- About 55 years (built 1969)
- 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
- Initial climb
- Defining eventThe 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
- Loss of engine power (total)
- 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
- Aircraft › Aircraft power plant
- Personnel issues › Action/decision
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The pilot was conducting a local “break-in” flight for the airplane’s recently-installed engine. During the initial climb, the engine’s rpm started to decline, followed by a total loss of engine power. The pilot performed a forced landing to a field and the airplane nosed over during the landing roll, resulting in substantial damage to the airplane’s fuselage, wings, rudder, and vertical stabilizer. A postaccident examination of the airplane revealed that the engine’s crankshaft was not free to rotate. The engine’s front main bearing was discolored and exhibited rotational abrasion at its rear oil passage area and corresponding crankshaft surface. Additionally, insect-related debris, soil/clay/mud, and lubricating oil were obstructing the crankcase oil header and the front main bearing’s aft oil passage. The signatures of lubrication distress observed on the front main bearing were consistent with oil starvation as a result of the obstructions found within the engine’s lubrication system. Review of the engine’s maintenance records showed that crankcase was repaired nearly 12 years before the accident and that the engine was overhauled 2 years later. The engine did not accrue any time in service prior to its installation on the accident airplane about 1 month before the accident (about 10 years after the overhaul). The mechanic who performed the engine overhaul reported that the crankcase was stored in a hangar for several months before he acquired it and that he did not remember cleaning and verifying that the oil passages of the crankcase were unobstructed before assembly. According to the engine manufacturer’s overhaul manual, all oil passages should be cleaned with suitable brushes then flushed thoroughly with clean solvent and compressed air. Based on the available evidence, an insect likely infiltrated the crankcase and made a nest in the oil passages during the more than 2 years it was stored. Maintenance personnel then failed to clean and verify the oil passages were free of obstruction before assembly of the engine, which resulted in a lack of lubrication to the front main bearing and a subsequent total loss of engine power.
Probable cause
Maintenance personnel’s failure to follow the engine manufacturer’s maintenance guidance, which resulted in the assembly of the engine with an obstructed oil passage, a subsequent lack of lubrication to the front main bearing, and a total loss of engine power.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ERA24LA388
- Event ID
- 20240923195159
- Case number
- ERA24LA388
- Dataset
- full-current
- Source SHA-256
- 5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
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, cause areas. 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: 54c3067f2f525fb92a7f2519ee19318231559d3bbcdd84e76c2d2afd5b040964; retrieved 2026-09-16T19:17:39.788Z.