NTSB CAROL · Event
Event ANC15LA008
Registry · N2580D
FAA Aircraft Registry record.
Make / Model
CESSNA 170B
Year of manufacture
1952 · 63 years old at event
Engine
CONT MOTOR C145 SERIES (145 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19560418
ADS-B equipped
Yes — Mode-S A27792
Registrant of record
PLACE ASHLEY K
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s loss of directional control during takeoff, which resulted in a runway excursion.
Factual narrative
On January 21, 2015 at 1142 Alaska standard time, a tailwheel-equipped, Cessna 170B airplane, N2580D, sustained substantial damage following a loss of control during takeoff from Lake Hood Seaplane Base (Z41), Anchorage, Alaska. The private pilot and three passengers were not injured. The airplane was registered to a private individual and operated by the pilot under the provisions of 14 Code of Federal Regulations (CFR) Part 91 as a personal flight. Visual meteorological conditions prevailed and a visual flight rules (VFR) flight plan had been filed. During an interview with an investigator from the National Transportation Safety Board (NTSB) on January 21, 2015, the pilot stated that during the takeoff roll, after the brakes were released and full power was applied, the airplane began to veer to the left. The pilot applied right rudder and right brake in an effort to correct for the veer, but the airplane continued to the left, struck a runway edge light, and departed the runway into the snow covered median between the runway and an adjacent taxiway, sustaining substantial damage to the right wing. A post accident examination of the airplane by the NTSB, along with a Federal Aviation Administration (FAA) aviation safety inspector from the Anchorage Flight Standards District Office revealed no mechanical irregularities that would have precluded normal operation. A post-accident weight and balance was accomplished by the NTSB using fuel load, passenger weights and seating location provided by the pilot. The aircraft was found to be about 82 pounds over the approved maximum gross weight of 2,200 pounds. The estimated center of gravity at the time of the accident was positive 43.53 inches. The center of gravity range at 2,200 pounds (maximum gross weight) is positive 40.8 inches to positive 46.4 inches. The closest weather reporting facility is Anchorage International Airport, Anchorage Alaska, less than one mile from the accident site. At 1153, an aviation routine weather report (METAR) from the Anchorage Airport was reporting in part: wind from 120 degrees at 8 knots; sky condition, clear; visibility, 10 statute miles; temperature 12 degrees F; dew point 9 degrees F; altimeter 29.34inHG. The pilot stated that, during the takeoff roll, after he released the brakes and applied full power, the airplane began to veer left. The pilot applied right rudder and right brake in an effort to correct the veer, but the airplane continued to veer left. The airplane then struck a runway edge light and departed the runway into the snow-covered median between the runway and an adjacent taxiway, which resulted in substantial damage to the right wing. A postaccident examination revealed no evidence of any preaccident mechanical anomalies. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
Verbatim from NTSB's published report. Source file
NTSB_2015_ANC15LA008.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (loss of control, runway excursion). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Embry-Riddle Scholarly Commons 2017 · Conference paper
Energy Safety Management: Mitigating Loss of Control Inflight
Under the new Airman Certification Standards (ACS), the Federal Aviation Administration (FAA) has mandated for the first time that private and commercial pilot candidates demonstrate understanding of …
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- SKYbrary (Eurocontrol) 2024 · SKYbrary article
Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
SKYbrary comprehensive knowledge-base entry on Loss of Control In-Flight — definitions, contributing factors, accident case studies (Air France 447, Colgan 3407), and prevention strategies.
- SKYbrary (Eurocontrol) 2024 · SKYbrary article
Runway Excursion — SKYbrary Knowledge Base
SKYbrary runway excursion review — RE-OE (overruns) + RE-LO (lateral). Risk drivers: long landing, high approach speed, contaminated surface, tailwind, mis-set autobrakes.
- NTSB Aircraft Accident Reports 2022 · Accident report
Loss of Control on Takeoff in Icing Conditions — Citation 560XL
Cessna Citation 560XL fatal takeoff icing accident, March 2018. Investigation of a Citation 560XL loss-of-control takeoff accident in icing conditions.
- Semantic Scholar 2021 · Article (Aviation)
ANALYSIS OF GENERAL AVIATION FIXED-WING AIRCRAFT ACCIDENTS INVOLVING INFLIGHT LOSS OF CONTROL USING A STATE-BASED APPROACH
Inflight loss of control (LOC-I) is a significant cause of General Aviation (GA) fixed-wing aircraft accidents. The United States National Transportation Safety Board’s database provides a rich source…
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