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Atlas / NTSB / SEA07CA159

NTSB CAROL · Event

Event SEA07CA159

2007-06-14 Roche Harbor, Washington, United States Airport · WA09 Serious 1 aircraft Status: Completed

Registry · N623AM

FAA Aircraft Registry record.

Make / Model

BELLANCA 17-30A

Year of manufacture

1979 · 28 years old at event

Engine

CONT MOTOR IO 520 SERIES (285 hp)

Seats / Engines

4 seats · 1 engine

Last airworthiness date

20010710

ADS-B equipped

Yes — Mode-S A8216E

Registrant of record

MELGAR ALBERT T

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The jamming of the left brake during landing. A factor was the kit manufacturer's design of the brake system.

Factual narrative

The pilot said he was landing on runway 07 with a 5-knot right crosswind. He said that shortly after touchdown, the aircraft started a slight drift to the right. The pilot said he applied left rudder to compensate and felt a "thunk" as the left rudder pedal locked forward, over center, underneath the brake pedal, which prevented the use of the left brake. The aircraft briefly lurched to the left. He applied hard right rudder, but with no apparent effect. He next applied right brake and intentionally ground looped the aircraft to prevent going down an embankment on the south side of the runway. The airplane's left main landing gear collapsed, followed by the left wing, left aileron, and forward fuselage being wrinkled and bent. The pilot said that the rudder/brake pedal assembly has only one master cylinder for the braking system and it is located on the right hand side. He said there is a mechanical linkage from the right to the left, which is prone to jamming in certain rudder pedal deflections. He said that other pilot's have reported this problem with their homebuilt airplanes manufactured from the same kit. The pilot said he was landing on runway 07 with a 5-knot right crosswind. He said that shortly after touchdown, the aircraft started a slight drift to the right. The pilot said he applied left rudder to compensate and felt a "thunk" as the left rudder pedal locked forward, over center, underneath the brake pedal, which prevented the use of the left brake. The aircraft briefly lurched to the left. He applied hard right rudder, but with no apparent effect. He next applied right brake and intentionally ground looped the aircraft to prevent going down an embankment on the south side of the runway. The airplane's left main landing gear collapsed, followed by the left wing, left aileron, and forward fuselage being wrinkled and bent. The pilot said that the rudder/brake pedal assembly has only one master cylinder for the braking system and it is located on the right hand side. He said there is a mechanical linkage from the right to the left, which is prone to jamming in certain rudder pedal deflections. He said that other pilot's have reported this problem with their amateur-built airplanes manufactured from the same kit. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2007_SEA07CA159.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.