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Atlas / NTSB / CEN25LA043

NTSB CAROL · Event

Event CEN25LA043

2024-11-17 Seguin, Texas, United States Airport · 1TE4 None 1 aircraft Status: In work

Registry · N52B

FAA Aircraft Registry record.

Make / Model

ASBELL WILLIAM E PITTS S-1E

Year of manufacture

1988 · 36 years old at event

Engine

LYCOMING I0360 SER (180 hp)

Seats / Engines

1 seats · 1 engine

Last airworthiness date

19880518

ADS-B equipped

Yes — Mode-S A686AE

Registrant of record

RED BARON LLC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Factual narrative

On November 17, 2024, about 1415 central standard time, a Pitts Special S-1E airplane, N52B, was substantially damaged when it was involved in an accident near Seguin, Texas. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. According to the pilot, he was practicing the International Aerobatic Club Advanced Free Sequence maneuver nine, which consists of a left 1 and ½ rotation snap roll to inverted flight followed by a reverse direction ½ loop downward, when he felt the left rudder lose tension, go to the firewall, and lost rudder control. The airplane ceased the snap roll and entered an inverted spiraling descent. He regained control using aileron and elevator and stabilized the airplane in upright flight. He then found that while he had right rudder control, he was unable to center the rudder due to the unresponsive left rudder pedal. The pilot returned to Zuehl Airport (1TE4) but was unable to control the airplane’s lateral alignment with the runway until he found the broken left rudder cable and was able to manipulate the rudder flight control surface by grabbing the cable and centering the rudder. During the landing roll, the airplane veered to the right and the pilot attempted to correct with left rudder but was unable to overcome the friction of the tailwheel. The airplane ground looped, nosed over, and came to rest inverted which resulted in substantial damage to the vertical stabilizer, lower left wing, and upper wings. Postaccident examination by the pilot revealed that the left rudder cable had separated at the attachment linkage to the left rudder pedal (See figure 1). Figure 1. Broken Left Rudder Cable Additionally, according to the pilot the right rudder cable attachment loop showed evidence of frayed wires with possible corrosion of the thimble (see figure 2). Figure 2. Right Rudder Cable Attachment The airplane was retained for further examination. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2024_CEN25LA043.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

What the literature says.

Academic papers and agency reports matching this event's aircraft type or causal vocabulary (icing). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.

Browse the full corpus — academia portal ↗