CEN24LA014 · Cirrus SR22
Cirrus SR22 · Accident: system/component malfunction/failure (non-power) while taxiing
Event
- NTSB case
- CEN24LA014
- 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
- Event fatalities
- Unknown
- 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
Cirrus SR22
- Aircraft type
- Cirrus SR22
- 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
- N969JB
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From not recordedTo not recorded
- Aircraft age
- About 18 years (built 2005)
- 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
- Taxi · to runway
- 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 systems
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 taxiing from the fixed-base operator’s building to the runway. As he increased brake pressure to stop the airplane before the runway hold short line, it turned to the left and completed a full 360° turn before coming to rest. The passenger then offered to try his brake pedals but the airplane only turned to the left; the pilot and passenger concluded they had no control of the right brake. The passenger then observed a fire emanating from under the right wing. The airport’s aircraft rescue and firefighting personnel responded and extinguished a fire associated with the right brake assembly. The right wing’s lower surface sustained substantial thermal damage during the ground fire.
A postaccident examination revealed that the right brake linings had exceeded the manufacturer’s serviceable wear limit. The left brake linings were also significantly worn but within the serviceable wear limit. Additionally, the left brake assembly revealed a darkened temperature indicator sticker that indicated the left brake assembly had previously exceeded the manufacturer’s temperature limitation. The right brake assembly sustained significant thermal damage during the ground fire and its associated temperature indicator stickers were not observed.
The excessively worn brake linings would have resulted in increased brake temperatures being transferred to the brake pressure plate and pistons. The loss of right brake effectiveness and subsequent fire likely occurred when hydraulic fluid leaked past a thermally damaged O-ring installed on one of the right brake pistons, then caught fire when it contacted the hot brake assembly.
Probable cause
The failure of the right brake assembly due to excessive brake lining wear, which resulted in a thermally damaged piston O-ring, hydraulic fluid leak, and subsequent fire.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record CEN24LA014
- Event ID
- 20231016193247
- Case number
- CEN24LA014
- 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: a7820a93107db886e99c13cbf9e211b29194738d36dae7d556f9176152612e1e; retrieved 2026-09-16T18:13:19.046Z.