LAX07CA110
2007-03-16 · Barstow, California, United States · None · 1 aircraft · Status: Completed
Airport KDAG
Current FAA registration · N628TT
- Make / Model
- CESSNA T210N
- Year of manufacture
- 1978 · 29 years old at event
- Engine
- CONT MOTOR TSIO-520 SER (300 hp)
- Seats / Engines
- 6 seats · 1 engine
- Last airworthiness date
- 19781122
- ADS-B equipped
- Yes — Mode-S A835B0
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to properly execute the manual landing gear extension procedures.
Factual narrative
The pilot reported to the National Transpiration Safety Board investigator that he was cruising at 10,500 feet over Dagget, California, when his autopilot kicked off. He reset the autopilot and it kicked off again a few minutes later. He checked his instruments and found that the ammeter was discharging rapidly, dropping from 28 volts towards 20 volts. He notified ATC that he would descend into Dagget-Barstow Airport, reduced all nonessential electrical loads, and slowed the airplane down. The discharge was now about 12-14 volts, he setup an orbit over the Dagget airport, and attempted lowering the landing gear normally, which was not successful. He made numerous attempts to manually pump down the landing gear using the hand-operated hydraulic pump handle. The nose wheel extended; however, the main landing gear only extended 3 or 4 inches. After circling 30 to 45 minutes the pilot decided to land the airplane gear up. He landed on runway 26, slid about 1,000 feet, and veered off to its south side. Ground crews were able to pull the landing gear into the down and locked position. There was no evidence of a hydraulic fluid leak. The pilot reported that during a further examination of the airplane he determined that the landing gear motor malfunctioned, and that he had not properly engaged the emergency pump handle prior to attempting a manual extension of the landing gear. The single engine airplane made a gear up landing that resulted in substantial damage to the airplane. The pilot reported that he was cruising at 10,500 feet, when his autopilot kicked off. He reset the autopilot and it kicked off again a few minutes later. He checked his instruments and found that the ammeter was discharging, with the system voltage rapidly dropping from 28 volts towards 20 volts. He notified ATC that he would descend into a nearby airport, reduced all nonessential electrical loads, and slowed the airplane down. The system voltage was now about 12-14 volts. He setup an orbit over the airport, and attempted lowering the landing gear normally, which was not successful. He made numerous attempts to manually pump down the landing gear using the hand-operated emergency hydraulic pump handle. The nose wheel extended; however, the main landing gear only extended 3 or 4 inches. After circling 30 to 45 minutes, the pilot decided to land the airplane gear up. He landed on the runway, slid about 1,000 feet, and veered off to its south side. Ground crews were able to pull the landing gear into the down and locked position after putting the airplane on jacks. There was no evidence of a hydraulic fluid leak. The pilot reported that during a further examination of the airplane he determined that the landing gear motor malfunctioned, and that he had not properly engaged the emergency pump handle prior to attempting a manual extension of the landing gear. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2007_LAX07CA110.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
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Related research
Matched on aircraft type or causal vocabulary (autopilot). All research papers
- arXiv 2025 · arXiv preprint ROSflight 2.0: Lean ROS 2-Based Autopilot for Unmanned Aerial Vehicles
ROSflight is a lean, open-source autopilot ecosystem for unmanned aerial vehicles (UAVs). Designed by researchers for researchers, it is built to lower the barrier to entry to UAV research and acceler…
- arXiv 2025 · arXiv preprint ROSplane 2.0: A Fixed-Wing Autopilot for Research
Unmanned aerial vehicle (UAV) research requires the integration of cutting-edge technology into existing autopilot frameworks.
- arXiv 2024 · arXiv preprint A Data-Driven Autopilot for Fixed-Wing Aircraft Based on Model Predictive Control
Autopilots for fixed-wing aircraft are typically designed based on linearized aerodynamic models consisting of stability and control derivatives obtained from wind-tunnel testing.
- arXiv 2022 · arXiv preprint Experimental Flight Testing of a Fault-Tolerant Adaptive Autopilot for Fixed-Wing Aircraft
This paper presents an adaptive autopilot for fixed-wing aircraft and compares its performance with a fixed-gain autopilot.
- arXiv 2021 · arXiv preprint An Adaptive Digital Autopilot for Fixed-Wing Aircraft with Actuator Faults
This paper develops an adaptive digital autopilot for a fixed-wing aircraft and compares its performance with a fixed-gain autopilot.
- arXiv 2026 · arXiv preprint Robust Adaptive Sliding-Mode Control for Damaged Fixed-Wing UAVs
Many unmanned aerial vehicles (UAVs) can remain aerodynamically flyable after sustaining structural or control surface damage, yet insufficient robustness in conventional autopilots often leads to mis…