NTSB CAROL · Event
Event GAA17CA074
Registry · N600RV
FAA Aircraft Registry record.
Make / Model
BEECH 58
Year of manufacture
1998 · 18 years old at event
Engine
CONT MOTOR IO-550 SERIES (300 hp)
Seats / Engines
6 seats · 2 engines
Last airworthiness date
19980608
ADS-B equipped
Yes — Mode-S A7C8CA
Registrant of record
AERO-TECH SERVICES INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
A collision with deer on the runway during the takeoff roll.
Factual narrative
The pilot of the multiengine retractable landing gear airplane reported that during takeoff, two deer ran onto the runway as the airplane became airborne and that he heard and felt one of the deer hit the left main landing gear. He further reported that he diverted to an airport with an operating control tower, where he performed two passes in front of the tower, and was informed by tower personnel that it "appeared" that the left main landing gear was no longer "attached to the airplane". The pilot reported that he decided the best course of action was to land with the landing gear retracted, and on short final he moved the mixture controls to idle cut off, feathered the propellers, and turned both fuel selectors off. The airplane landed gear up and all persons on board evacuated immediately. The airplane sustained substantial damage to the fuselage. In an email exchange with the Director of Operations of the flight company, he reported that there were no reported mechanical anomalies with the airframe or engine prior to the deer impact. The Federal Aviation Administration Chart Supplement airport page for the departure airport in part states: "Deer and large flocks of geese on and invof [in the vicinity of] arpt." The pilot of the multiengine retractable landing gear airplane reported that during takeoff, two deer ran onto the runway as the airplane became airborne and that he heard and felt one of the deer hit the left main landing gear. He further reported that he diverted to an airport with an operating control tower, where he performed two passes in front of the tower, and was informed by tower personnel that it "appeared" that the left main landing gear was no longer "attached to the airplane". The pilot reported that he decided the best course of action was to land with the landing gear retracted, and on short final he moved the mixture controls to idle cut off, feathered the propellers, and turned both fuel selectors off. The airplane landed gear up and all persons on board evacuated immediately. The airplane sustained substantial damage to the fuselage. In an email exchange with the Director of Operations of the flight company, he reported that there were no reported mechanical anomalies with the airframe or engine prior to the deer impact. The Federal Aviation Administration Chart Supplement airport page for the departure airport in part states: "Deer and large flocks of geese on and invof [in the vicinity of] arpt." 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 Environmental issues-Physical environment-Object/animal/substance-Animal(s)/bird(s)-Effect on operation - C
- C Environmental issues-Physical environment-Object/animal/substance-Animal(s)/bird(s)-Ability to respond/compensate - C
Verbatim from NTSB's published report. Source file
NTSB_2016_GAA17CA074.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. Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2011 · Conference Paper
Joint thunderstorm operations using the NASA F-106B and FAATC/AFWAL Convair 580 airplanes
During the 1985 thunderstorm season, three joint thunderstorm research flights were conducted within 100 n.mi. of NASA Langley by the NASA Storm Hazards F-106B and the FAA/USAF CV-580 research airplan…
- NTSB Aircraft Accident Reports 2004 · Accident report
In-Flight Separation of Vertical Stabilizer — American Airlines Flight 587
American Airlines 587 (A300-605R) Belle Harbor, NY, November 12, 2001 — 265 fatalities. Investigation of the post-takeoff in-flight breakup of American 587 over Belle Harbor.
- NASA NTRS 2024 · Presentation
American Airlines Flight 587 Crash Investigation: NASA Langley Research Center Participation and Perspective
- NASA NTRS 2019 · Other
Documentation for Three Wake Vortex Model Data Sets from Simulation of Flight 587 Wake Vortex Encounter Accident Case
This document contains a general description for data sets of a wake vortex system in a turbulent environment. The turbulence and thermal stratification of the environment are representative of the co…
- NASA NTRS 2016 · Conference Paper
An overview of SAE ARP 1587: Aircraft gas turbine engine monitoring system guide
A systematic approach to developing an engine monitoring system (EMS) is outlined. An extensive shopping list of EMS capabilities and benefits are included.
- arXiv 2025 · arXiv preprint
Numerical Investigation of Discontinuous Ice Effects on Swept Wings
This study investigates the aerodynamic performance and flow structures of infinite swept wings with artificially simulated discontinuous ice using an enhanced delayed detached-eddy simulation.
Browse the full corpus — academia portal ↗