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SEA07LA210

2007-07-17 · Laurel, Montana, United States · None · 1 aircraft · Status: Completed

Airport 6S8

Current FAA registration · N7927R

Make / Model
BEECH E33C
Year of manufacture
1969 · 38 years old at event
Engine
CONT MOTOR IO 520 SERIES (285 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20020627
ADS-B equipped
Yes — Mode-S AAC2D0

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The overload failure of the nose gear retract brace (drag link) during the landing roll.

Factual narrative

On July 17, 2007, approximately 1445 mountain daylight time, a Beech E-33C, N7927R, experienced a collapse of the nose gear during the landing roll at Laurel Municipal Airport, Laurel, Montana. The Certified Flight Instructor and his student where not injured, but the airplane, which is owned by Rocky Mountain College, sustained substantial damage. The local 14 CFR Part 91 instructional flight, which departed the same airport about 20 minutes earlier, was being operated in visual meteorological conditions. No flight plan had been filed, and there was no report of an ELT activation. According to the instructor and the student, the touchdown was uneventful, but during the landing roll the nose gear collapsed. A post-accident inspection of the gear system revealed that the nose gear retract brace (drag-link) had failed. The fracture surface of the brace was analyzed by the NTSB Materials Laboratory, and it was determined that it had failed in a manner consistent with a twisting overload. No preexisting damage or indication of fatigue was found. The reason for the twisting overload failure could not be determined. The failure of the brace resulted in structural damage to the area around the nose gear wheel well. The nose gear collapsed during the landing roll after an uneventful touchdown. An inspection of the gear system revealed that the nose gear retract brace (drag-link) had failed. The fracture surface of the brace was determined to have failed in a twisting overload. No preexisting damage or indication of fatigue was found. The reason for the twisting overload failure could not be determined. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2007_SEA07LA210.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.