NTSB CAROL · Event
Event ANC18LA049
Aircraft involved
Probable cause & findings
The flight crew’s failure to fully disengage the parking brake before taxi, which resulted in a brake fire.
Factual narrative
On June 26, 2018, about 0850 mountain daylight time (MDT), a Bombardier Learjet 60 airplane, N57Z, sustained substantial damage when it was involved in an accident at Salt Lake City International Airport (KSLC), Salt Lake City, Utah. The two pilots and one technician were uninjured. The airplane was operated as a Title 14 Code of Federal Regulations Part 135 flight. The mission-specific modified airplane was registered to and operated by the Federal Aviation Administration (FAA) and was used to perform flight inspections of the National Airspace navigational systems. The captain was the pilot flying at the time of the accident. According to the flight crew, while taxiing to the runway for departure, the nose wheel steering seemed unusually sensitive and the airplane pulled slightly to the right. As they neared the runway threshold, they smelled what they thought was overheated brakes. The crew confirmed the position of the parking brake handle and the airplane moved more freely. The crew then cancelled their takeoff clearance and taxied the airplane to the runup area to allow the brakes to cool. Shortly thereafter, the control tower notified the crew that the airplane was on fire. The crew secured and then evacuated the airplane. The cockpit voice recorder (CVR) recorded the captain’s and first officer’s comments and revealed that, as the airplane taxied, both pilots felt that the airplane’s movement was jerky and they could hear a squealing noise that was not audible on the CVR. The captain indicated that the airplane wanted to pull to the right and that it seemed like more power was required to taxi. The first officer indicated that it felt like the captain was "riding" the brakes. Shortly thereafter, the captain realized the parking brake was not completely released. Examination of the airplane by an FAA inspector revealed that the right tire and landing gear were fire-damaged, and that the underside of the fuselage and right wing was substantially damaged due to the fire. A detailed examination of the airplane’s brake system revealed no pre-accident mechanical failures or malfunctions that would have precluded normal operation. The parking brake handle was located on the pedestal below the thrust levers and labeled PARKING BRAKE. The parking brake was operated by depressing and holding the toe brakes and pulling the parking brake handle to set the brakes. The parking brake was released by returning the handle to the off, or in, position. Whenever the parking brake handle was not fully in, the PARK BRAKE light would illuminate. A review of the Lear 60 Single Card Checklist, Revision 1, dated June 4, 2017, revealed that the Before Taxi, Taxi and Before Takeoff, Quick Turnaround, and Taxi checklists did not contain a line item for the release of the parking brake. The pilots reported that, while taxiing to the runway for departure, the nose wheel steering seemed unusually sensitive and the airplane pulled slightly to the right. As they neared the runway threshold, they smelled what they thought to be overheated brakes. The crew confirmed the position of the parking brake handle, which had not been fully stowed, and once the handle was completely stowed (parking brake OFF position), the airplane moved more freely. The crew then cancelled their takeoff clearance and taxied the airplane to the runup area to allow the brakes to cool. Shortly thereafter, the control tower notified the flight crew that the airplane was on fire. Examination of the airplane revealed substantial damage to the underside of the fuselage and right wing due to fire that originated at the right main landing gear. A detailed examination of the airplane’s brake system revealed no preaccident mechanical failures or malfunctions that would have precluded normal operation. A review of the cockpit voice recorder information confirmed that the crew did not completely release the parking brake before taxi. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- — Personnel issues-Task performance-Use of equip/info-Use of equip/system-Pilot
- — Personnel issues-Task performance-Use of equip/info-Use of equip/system-Copilot
- — Aircraft-Aircraft systems-Landing gear system-Brake-Incorrect use/operation
Verbatim from NTSB's published report. Source file
NTSB_2018_ANC18LA049.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type. Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2024 · Conference Paper
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- NASA NTRS 2024 · Presentation
Al6061-RAM2 Development and Hot-Fire Testing using Additive Manufacturing Laser Powder Directed Energy Deposition for Liquid Rocket Engine Channel-Cooled Nozzles
Aluminum 6061-RAM2 is a high-strength aluminum feedstock developed for additive manufacturing (AM)processes. This alloy leverages Reactive Additive Manufacturing (RAM) technology.
- arXiv 2022 · arXiv preprint
Zero Touch Coordinated UAV Network Formation for 360° Views of a Moving Ground Target in Remote VR Applications
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- NTSB Aircraft Accident Reports 2022 · Accident report
Loss of Control on Takeoff in Icing Conditions — Citation 560XL
Cessna Citation 560XL fatal takeoff icing accident, March 2018. Investigation of a Citation 560XL loss-of-control takeoff accident in icing conditions.
- NASA NTRS 2019 · Technical Memorandum (TM)
Fidelity assessment of a UH-60A simulation on the NASA Ames vertical motion simulator
Helicopter handling qualities research requires that a ground-based simulation be a high-fidelity representation of the actual helicopter, especially over the frequency range of the investigation.
- NASA NTRS 2019 · Other
Differential Pressures on a Pitot-venturi and a Pitot-static Nozzle over 360 Degrees Pitch and Yaw
Measurements of the differential pressures on two navy air-speed nozzles, consisting of a Zahm type Pitot-Venturi tube and a SQ-16 two-pronged Pitot-static tube, in a tunnel air stream of fixed speed …
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