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June 20, 2026 · Zenith Aircraft 601 XL · N165TJ

O'Donnell, TX

Overview

Report Status
Factual report
Event Type
Accident
Date
June 20, 2026
Injury Outcomes
1 injury (1 serious injury)
Location
O'Donnell, TX
Aircraft
Zenith Aircraft 601 XL (2011)
Tail Number
N165TJ
Injuries
Serious
Aircraft Damage
Substantial
NTSB Number
CEN26LA230

On June 20, 2026, about 1147 central daylight time, an experimental Zodiac 601XL airplane, N165TJ, was substantially damaged when it was involved in an accident near O’Donnell, Texas. The pilot sustained serious injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 positioning flight. The pilot reported that she was relocating the airplane for the new owner, which was something she had previously done for this owner. During the preflight inspection, she did not find anything wrong with the airplane. About 15 minutes after departure, the canopy popped open about 2 inches, and she observed that the main canopy latch was no longer fully latched. As she initiated a right turn back to the airport, the latch broke and the canopy flew open. She grabbed the canopy rope and attempted to close the canopy but was unable. Due to the excessive drag, airplane’s descent increased so she executed a forced landing to a field. During the landing the airplane nosed over and came to rest inverted. The pilot added that she had accumulated about 20 to 30 hours in the same airplane model but had never flown this airplane before. Postaccident examination by the FAA revealed that the airplane landed in an agricultural field, perpendicular to the rows of crops. The airplane sustained substantial damage to the fuselage, empennage, and wings. The airplane was equipped with a forward hinging, tip-up canopy with gas struts that assisted in opening the canopy and supported the canopy when open. The main canopy latch was on the front left side near the instrument panel. The rear of the canopy frame featured a rope that locked into a cam cleat behind the pilot’s seat, which acted as a secondary canopy latch. A condition inspection was completed on May 18, 2026, at 388.6 hours airframe total time. The logbook entry noted that the canopy was clear with no distortion and recommended replacement of the canopy struts. The airplane has been retained for further examination.

Full Narrative

On June 20, 2026, about 1147 central daylight time, an experimental Zodiac 601XL airplane, N165TJ, was substantially damaged when it was involved in an accident near O’Donnell, Texas. The pilot sustained serious injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 positioning flight. The pilot reported that she was relocating the airplane for the new owner, which was something she had previously done for this owner. During the preflight inspection, she did not find anything wrong with the airplane. About 15 minutes after departure, the canopy popped open about 2 inches, and she observed that the main canopy latch was no longer fully latched. As she initiated a right turn back to the airport, the latch broke and the canopy flew open. She grabbed the canopy rope and attempted to close the canopy but was unable. Due to the excessive drag, airplane’s descent increased so she executed a forced landing to a field. During the landing the airplane nosed over and came to rest inverted. The pilot added that she had accumulated about 20 to 30 hours in the same airplane model but had never flown this airplane before. Postaccident examination by the FAA revealed that the airplane landed in an agricultural field, perpendicular to the rows of crops. The airplane sustained substantial damage to the fuselage, empennage, and wings. The airplane was equipped with a forward hinging, tip-up canopy with gas struts that assisted in opening the canopy and supported the canopy when open. The main canopy latch was on the front left side near the instrument panel. The rear of the canopy frame featured a rope that locked into a cam cleat behind the pilot’s seat, which acted as a secondary canopy latch. A condition inspection was completed on May 18, 2026, at 388.6 hours airframe total time. The logbook entry noted that the canopy was clear with no distortion and recommended replacement of the canopy struts. The airplane has been retained for further examination.

Flight

Event TypeAccident
Event Time11:47 CDT
Nearest Airport0nm
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftZenith Aircraft 601 XL
Tail NumberN165TJ
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Seats2

People & Injuries

Injury Summary1 injury (1 serious injury)
Fatal0
Serious1
Minor0
Uninjured0
Total1

Conditions

ConditionsVMC
LightDaylight
Wind190° @ 5 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point68 F
Altimeter30.00 inHg
Observation Time11:35
Weather SourceWFAC

Appendix: Source Data