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GAA18CA154

2018-02-25 · Newtok, Alaska, United States · None · 1 aircraft · Status: Completed

Airport EWU

Current FAA registration · N1658U

Make / Model
CESSNA 207
Year of manufacture
1974 · 44 years old at event
Engine
CONT MOTOR IO 520 SERIES (285 hp)
Seats / Engines
6 seats · 1 engine
Last airworthiness date
19740930
ADS-B equipped
Yes — Mode-S A107C4

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot’s failure to maintain directional control during takeoff. Contributing to the accident was the pilot’s failure to properly check that the flight controls were correctly configured before takeoff.

Factual narrative

The pilot reported that during a return flight, he elected to fly from the right pilot seat, to allow a cargo-handler to sit in the left pilot seat. The taxi to the runway was short and required little rudder input. However, during takeoff, as he added power, he "did not seem" to have full right rudder authority and he was unable to maintain the runway centerline. Subsequently, the airplane exited the left side of the runway, struck a small ridge, and came to rest nose down. The airplane sustained substantial damage to the fuselage and left-wing. The pilot further reported that, after the accident, he realized the airplane had stow-able rudder pedals on the right side, and that they had been placed in the "stowed" position. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The pilot reported that, during a return flight, he chose to fly from the right pilot seat to allow a cargo-handler to sit in the left pilot seat. The taxi to the runway was short and required little rudder input. However, during takeoff, as he added power, he "did not seem" to have full right rudder authority, and he was unable to maintain the runway centerline. Subsequently, the airplane exited the left side of the runway, struck a small ridge, and came to rest nose down. The airplane sustained substantial damage to the fuselage and left wing. The pilot further reported that, after the accident, he realized the airplane had stowable rudder pedals on the right side and that they had been placed in the "stowed" position. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Attain/maintain not possible - C
  • C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
  • F Personnel issues-Action/decision-Action-Lack of action-Pilot - F
  • — Aircraft-Aircraft structures-Empennage structure-Rudder-Inadequate inspection

Verbatim from NTSB's published report. Source file NTSB_2018_GAA18CA154.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.