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Atlas / NTSB / NYC07CA016

NTSB CAROL · Event

Event NYC07CA016

2006-10-31 Farmingdale, New Jersey, United States Airport · BLM None 1 aircraft Status: Completed

Registry · N916R

FAA Aircraft Registry record.

Make / Model

SLING AIRCRAFT (PTY) LTD SLING HW

Seats / Engines

4 seats · 1 engine

ADS-B equipped

Yes — Mode-S ACAE6C

Registrant of record

AIRPLANE FACTORY INC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

A loss of engine power due to a disconnected throttle/power lever linkage. A contributingfactor was the owner/builder's improper installation of the throttle linkage.

Factual narrative

According to the pilot, the builder/owner of the amateur built RV-7 hired the pilot, who was also a designated airworthiness representative, to inspect the airplane and to perform its first test flight. During the preflight inspection, the pilot did not remove the cowling to inspect the engine compartment. The pilot completed the test flight and returned to the airport for landing. On final approach, he adjusted the throttle, but the engine did not respond and he could not increase or decrease power. He then extended the flaps and "slipped" the airplane, but was "going too fast and was too high" to land. He turned the airplane to land on another runway, but during the turn, the airplane "lost altitude" and impacted the ramp area. An inspection of the airplane following the accident revealed that throttle control was disconnected from the fuel servo. The throttle linkage connecting bolt and several washers were found loose inside the engine cowling. The corresponding castellated retaining nut and respective cotter key were not located. During an interview, the owner/builder stated that he "may have forgotten to install the cotter key." The builder/owner of the amateur built RV-7 hired the pilot, who was also a designated airworthiness representative, to inspect the airplane and to perform its first test flight. During the preflight inspection, the pilot did not remove the cowling to inspect the engine compartment. The pilot completed the test flight and returned to the airport for landing. On final approach, he adjusted the throttle, but the engine did not respond and he could not increase or decrease power. He then extended the flaps and "slipped" the airplane, but was "going too fast and was too high" to land. He turned the airplane to land on another runway, but during the turn, the airplane "lost altitude" and impacted the ramp area. An inspection of the airplane following the accident revealed that throttle control was disconnected from the fuel servo. The throttle linkage connecting bolt and several washers were found loose inside the engine cowling. The corresponding castellated retaining nut and respective cotter key were not located. During an interview, the owner/builder stated that he "may have forgotten to install the cotter key." Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2006_NYC07CA016.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

What the literature says.

Academic papers and agency reports matching this event's aircraft type or causal vocabulary (stall). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.

Browse the full corpus — academia portal ↗