ANC18LA048 · Cessna 180
Cessna 180 · Accident: system/component malfunction/failure (non-power) during landing
From Fairbanks International Airport (FAI) to Gold King Creek Airport (AK7)
Narrative check · The NTSB narrative appears to contradict this record's location. Values are shown as recorded, not corrected; compare with the narrative.
Event
- NTSB case
- ANC18LA048
- 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 180
- Aircraft type
- Cessna 180
- 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
- N3125D
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Fairbanks International Airport (FAI), Fairbanks, AKTo Gold King Creek Airport (AK7), Fairbanks, AK
- Aircraft age
- About 63 years (built 1955)
- 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 systems
- Personnel issues › Task performance
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
According to the pilot, he was landing with a right crosswind, and after touchdown, as the airplane began to decelerate, he applied left brake to maintain directional control. He stated that the left brake pedal was "soft" and traveled to its full forward limit. The airplane weathervaned and skidded sideways before the left main wheel went off the landing area and into brush. The left wing and left horizontal stabilizer impacted terrain, which resulted in substantial damage. The pilot noted in a postflight examination that the brake line had separated at the compression fitting near the brake caliper where the brake line transitioned from a rigid line to a flexible line.
A laboratory examination of the brake line and its components revealed that the interior surface of the failed end had circumferential marks consistent with formation of a flared end with a flaring tool. The sleeve was trapped within the nut from the failed end, and deposits of gray metal appearing consistent with deformed brake tube material were observed deposited on internal threads of the nut.
According to Federal Aviation Administration Advisory Circular AC 43-13-1B, "Acceptable Methods, Techniques, and Practices – Aircraft Inspection and Repair," a double flare is used on soft aluminum tubing having a 3/8-inch outside diameter or less. No evidence of folded walls consistent with a double flare was noted at either end of the brake line tube.
No records could be found that showed the manufacture or assembly date of the fractured brake line components.
Probable cause
The failure of the brake line tube due to an improper flare.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ANC18LA048
- Event ID
- 20180625X23720
- Case number
- ANC18LA048
- 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: local date, investigation status. Values present in the bulk record are kept.
- The date is the local date; the NTSB stores the UTC date 2018-06-23.
- API snapshot SHA-256: 0914bc3a7acf823f65a990a705889647a57e587f17fca2c8db8d1dc3a10b36ad; retrieved 2026-09-16T07:39:40.209Z.