NTSB CAROL · Event
Event SEA03LA202
Registry · N2869D
FAA Aircraft Registry record.
Make / Model
NORTH AMERICAN/AERO CLASSICS P-51D
Year of manufacture
1944 · 59 years old at event
Engine
AMA/EXPR UNKNOWN ENG
Seats / Engines
1 seats · 1 engine
Last airworthiness date
20230830
ADS-B equipped
Yes — Mode-S A2E7DC
Registrant of record
ACV GROUP LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The malfunction of the cooling system pressure relief valve and the pilot's failure to follow procedures. An engine over temperature, a coolant leak as a result of a relief valve failure, an obstructed windshield which was covered with coolant fluid, and an improper flare resulting in a hard landing were factors.
Factual narrative
On a date on or about July 3, 2003, about 1100 mountain daylight time, a North American P-51D, N2869D, registered to and operated by the pilot as a 14 CFR Part 91 personal flight, experienced a loss of engine power shortly after takeoff from Jerome County Airport, Jerome, Idaho. During the return for landing, the aircraft landed hard and slid off the side of the runway. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft was substantially damaged and the commercial pilot and his passenger were not injured. During a telephone interview with the pilot on December 4, 2003, the pilot reported that shortly after takeoff, the engine overheated and then lost coolant. The coolant covered the windshield and he had a hard time seeing in front of him for the return landing to runway 8. During the touchdown, the aircraft landed hard and slid off the side of the runway. The pilot could not recall the actual date of the accident. He further stated that he was not aware that he needed to report this accident to the NTSB. The accident was reported to the NTSB on December 3, 2003. A telephone conversation with the mechanic who was accomplishing the repairs to the aircraft reported that the left wing spar was bent. As a result of this damage, which adversely affected the structural strength of the spar, it was being replaced. The mechanic also reported that he believed that the accident occurred just before the fourth of July weekend. The mechanic reported that the relief valve to the aftercooling system header tank failed, subsequently releasing the coolant. Section IV of the P-51D, Maintenance Manual states, "The system is of the low pressure type, incorporating a relief valve which relieves at approximately 18 to 20 pounds per square inch." The Mustang Flight Handbook indicates for engine starting and for all ground operations, oil and coolant flaps should be fully opened to prevent overheating. A caution is noted indicating that if coolant temperature exceeds 100 degrees C, the coolant radiator air control switch should be placed in the open position until airborne. Restricted ground operations during hot-weather is recommended to prevent overheating, and to maintain a constant check on carburetor air and coolant temperature. The Handbook instructions further state that "If the engine overheats in flight (indicated by coolant relief valve pop-off, maximum coolant temperature being exceeded, or white smoke coming from exhaust stacks), move coolant radiator air control switch to OPEN and hold." Two letters with the National Transportation Safety Board Pilot/Operator Aircraft Accident Report Form 6120.1/2 were sent to the pilot on December 4, 2003, and then on January 15, 2004, with instructions to complete the form and return to the NTSB. The pilot's response to the first letter was that he needed more time to complete the form. When the pilot did not return the 6120.1/2, the second letter was mailed with another 6120.1/2 form attached. The pilot's response to the second letter stated that he just had a hard landing and did not consider this an accident because there were no injuries and no damage on the airport. To date, the pilot has not returned Form 6120.1/2. The pilot reported that shortly after takeoff, the engine overheated, then lost coolant. The coolant covered the windshield and he had a hard time seeing in front of him for the return to the airport for landing. During the touchdown, the aircraft landed hard and slid off the side of the runway. During an inspection by maintenance personnel, it was found that the left wing spar was bent and required replacement. It was also found that the relief valve to the aftercooling system header tank failed, subsequently releasing the coolant. The aftercooling system is of the low pressure type, incorporating a relief valve which relieves at approximately 18 to 20 pounds per square inch. The flight manual states in several areas for start, ground operations and takeoff to closely monitor coolant temperatures to prevent overheating. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_SEA03LA202.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 or causal vocabulary (maintenance). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Embry-Riddle Scholarly Commons 2026 · Journal article (IJAAA)
From Reactive to Predictive: A hybrid Trust-Mediated Adoption Framework for Data-Driven Maintenance in Distributed-Authority Aviation Environments
Modern aviation maintenance operates within increasingly data-intensive technological environments, yet the operational integration of predictive maintenance into routine decision-making remains incon…
- Semantic Scholar 2025 · Article (Applied Sciences)
Decision-Making Framework for Aviation Safety in Predictive Maintenance Strategies
The implementation of predictive maintenance (PM) in aviation presents unique challenges due to strict safety requirements, complex operational environments, and regulatory constraints.
- Embry-Riddle Scholarly Commons 2024 · Journal article (JAAER)
Low-Resource Automatic Speech Recognition Domain Adaptation – A Case-Study in Aviation Maintenance
With timeliness and efficiency being critical in the aviation maintenance industry, the need has been growing for smart technological solutions that optimize and streamline the different underlying ta…
- Embry-Riddle Scholarly Commons 2024 · Journal article (JAAER)
A New Trajectory in UAV Safety: Leveraging Reinforcement Learning for Distance Maintenance Under Wind Variations
In the field of aviation, safety is a critical cornerstone, and the operation of Unmanned Aerial Vehicle (UAV) systems is deeply connected with this principle.
- Embry-Riddle Scholarly Commons 2024 · Journal article (IJAAA)
Just Culture in Aviation: A Metaphorical Study on Aircraft Maintenance Students
Just Culture, a sub-dimension of safety culture, has been a prominent and debated topic in aviation safety in recent years.
- Embry-Riddle Scholarly Commons 2024 · Journal article (IJAAA)
Performance PRISM: A Comprehensive Framework For Performance Measurement In Aircraft Maintenance
Aircraft maintenance is governed by rigorous safety requirements and high operational complexity, demanding robust performance measurement frameworks to ensure optimal maintenance practices.
Browse the full corpus — academia portal ↗