WPR23LA216 · Cessna 172R
Cessna 172R · Accident: system/component malfunction/failure (non-power) during landing
From Santa Monica Municipal Airport (SMO) to an unrecorded destination
Event
- NTSB case
- WPR23LA216
- 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
Cessna 172R
- 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
- N819KS
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Santa Monica Municipal Airport (SMO), Santa Monica, CATo not recorded
- Aircraft age
- About 23 years (built 2000)
- 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
- Landing · landing roll
- 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
- System/component malfunction/failure (non-power)
- 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 oper/perf/capability
- Aircraft › Aircraft systems
- Personnel issues › Task performance
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The pilot was completing a maintenance flight to determine that the airplane was airworthy after repairs following a collision with a fuel truck that had taken place one month before the accident. The high-speed taxi test and subsequent flight in the airport traffic pattern were uneventful. However, when the pilot landed the airplane, the nosewheel began a shimmy that intensified as the airplane slowed. The airplane began to veer left, and the pilot attempted to correct the movement with right rudder, aerodynamic braking, and then both brakes, but the airplane nosed over and came to rest inverted, which resulted in substantial damage to the rudder. A bolt from the upper portion of the nose torque link was found on the runway and a poastaccident material analysis revealed that the bolt had separated from shear overstress. The investigation also found that the bolt had been damaged and was not replaced as part of the repairs made to prepare the airplane for the ferry flight following the previous collision with the fuel truck. The accident was the result of a failure of the upper torque link during landing. The link failed due to a bolt that had unaddressed fractures originating from when the airplane collided with the truck. This resulted in a loss of steering control and a subsequent loss of directional control on the ground. A video provided by the airplane owner of the airplane showing the damage on the airplane following the collision with the fuel truck clearly shows the bent upper torque link bolt.
Probable cause
A failure of the nose wheel upper torque link bolt, which resulted in a loss of steering control. Contributing to the accident were maintenance personnel’s failure to inspect and replace the fractured bolt and the pilot’s oversight of the bolt during his preflight inspection.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record WPR23LA216
- Event ID
- 20230606192319
- Case number
- WPR23LA216
- 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, coordinates, 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: 3a57f7256a5bbeeeb65f26193b14a1667042ff4a460c23e6f85a436b39530d1f; retrieved 2026-09-16T17:41:51.432Z.