NTSB CAROL · Event
Event ANC05LA093
Registry · N88110
FAA Aircraft Registry record.
Make / Model
BELLANCA 7GCBC
Year of manufacture
1974 · 31 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20010910
ADS-B equipped
Yes — Mode-S AC2420
Registrant of record
LOVAS THOMAS A
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain adequate airspeed during takeoff initial climb, which resulted in a loss of control and subsequent uncontrolled descent into a lake. A factor contributing to the accident was an inadvertent stall.
Factual narrative
On July 1, 2005, about 1935 Alaska daylight time, a float-equipped Bellanca 7GCBC airplane, N88110, sustained substantial damage when it collided with the waters of Lake Hood during initial climb after takeoff from the Lake Hood Seaplane Base, Anchorage, Alaska. The airplane was being operated as a visual flight rules (VFR) cross-country personal flight under Title 14, CFR Part 91, when the accident occurred. The airplane was operated by the pilot. The private certificated pilot, and the sole passenger, were not injured. Visual meteorological conditions prevailed. The flight was en route to Sterling, Alaska, and no flight plan was filed, nor was one required. During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC), on July 2, the pilot reported that he was performing a glassy water takeoff from the west waterlane of Lake Hood. He indicated that he lifted off the water at 45 mph, and began a climb at 55 mph. The airplane then rolled to the right and descended toward the water. The right wing and right float assembly struck the water and the airplane overturned. The pilot and passenger were both wearing inflatable jackets, and exited the airplane. A family pet did not escape from the airplane. The pilot said the engine was producing power during the accident sequence. A Federal Aviation Administration (FAA) operations inspector, Anchorage Flight Standards District Office (FSDO), responded to the accident scene, and reported that the airplane contained about 30 gallons of fuel. The float compartments contained additional fuel containers, an anchor, and rope. An FAA airworthiness inspector examined the airplane as it sat on a trailer on July 5, after the pilot recovered and partially disassembled the airplane. The inspector reported that the airplane's flap handle was set at 10 degrees. He did not indicate that he observed any mechanical malfunction. In the Pilot/Operator Aviation Accident Report (NTSB FORM 6120.1) submitted by the pilot, the pilot indicated that the water surface was glassy, with a variable wind from the north. During the takeoff run, the pilot stated that he lifted the left float out of the water, then the right float, and accelerated for a climb. He said that when the airplane reached about 50 feet, it began a "very fast uncommanded roll to the right, and control forces went to zero." The pilot also indicated there was no mechanical malfunction/failure. At 1957, an Aviation Routine Weather Report (METAR) at Lake Hood Seaplane Base was reporting, in part: Wind, calm; visibility, 10 statute miles; clouds and sky condition, few at 3,800 feet, 10,000 feet broken; temperature, 72 degrees F; dew point, 53 degrees F; altimeter, 29.71 inHg. The private certificated pilot was conducting a personal flight under Title 14, CFR Part 91, and was performing a glassy water takeoff toward the west from a lake in a float-equipped airplane. He reported variable winds from the north. The pilot said that during the takeoff, he lifted the left float out of the water, then the right float at 45 mph, and began a climb at 55 mph. He said that when the airplane reached about 50 feet, it began a "very fast uncommanded roll to the right, and control forces went to zero." The pilot also indicated there was no mechanical malfunction/failure, and the engine was producing power during the accident sequence. The airplane descended toward the water, and the right wing and right float assembly struck the water and the airplane overturned. The pilot and passenger were both wearing inflatable jackets, and exited the airplane. An FAA airworthiness inspector examined the airplane as it sat on a trailer, after the pilot recovered and partially disassembled the airplane. The inspector reported that the airplane's flap handle was set at 10 degrees. The inspector did not indicate that he observed any mechanical malfunction. A METAR from the accident site included calm winds, and a temperature of 72 degrees F. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2005_ANC05LA093.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Beyond the agency record
Search this event elsewhere.
Pre-filled searches into the sources where news + community discussion of aviation events lives. External sources are reported, not agency. Treat them as signal that something happened, not as fact about what happened.
Entity-clustered aviation events in the press — last 24 hr + 30-day archive.
Official agency record + docket.
Investigative docket: factual reports, photos, transcripts.
Long-running aviation incident database (Flight Safety Foundation).
Community NTSB synthesis blog — often has photos and witness reports.
Gold-standard aviation incident blog.
Aviation industry news search.
GA pilot forum — informed but rumor-prone.
GA pilot subreddit search.
Tail-number page — flight history (free tier limited).
AOPA Air Safety Institute search.
Mainstream press coverage. Recent events only.
Privacy-preserving news search.
External links open in a new tab. We don't ingest their content; we deep-link search queries.
Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (stall, loss of control). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Semantic Scholar 2016 · Article (Interacción)
Trajectory Recovery System: Angle of Attack Guidance for Inflight Loss of Control
This paper describes the design and development of an ecological display to aid pilots in the recovery of an In-Flight Loss of Control event due to a Stall (ILOC-S).
- NTSB Aircraft Accident Reports 2010 · Accident report
Loss of Control on Approach — Colgan Air Flight 3407
Colgan Air 3407 / Continental Connection (Q400) Buffalo NY, February 12, 2009 — 50 fatalities. Definitive investigation of the Colgan 3407 stall-stick-pusher crash on approach to Buffalo.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- 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…
- arXiv 2025 · arXiv preprint
Quadratic Programming Approach to Flight Envelope Protection Using Control Barrier Functions
Ensuring the safe operation of aerospace systems within their prescribed flight envelope is a fundamental requirement for modern flight control systems.
- 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.
Browse the full corpus — academia portal ↗