NTSB CAROL · Event
Event DEN06LA041
Registry · N7743Y
FAA Aircraft Registry record.
Make / Model
PIPER PA-30
Year of manufacture
1965 · 41 years old at event
TCDS
A1EA · PIPER AIRCRAFT INC
Engine
LYCOMING IO-320 SERIES (150 hp)
Seats / Engines
6 seats · 2 engines
Last airworthiness date
19650428
ADS-B equipped
Yes — Mode-S AA7ABB
Registrant of record
SCHROEDER DAVID C
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's flight into adverse weather conditions, the airframe ice, and the wheels up landing. Factors contributing to the accident were the icing conditions, the frozen landing gear, the frozen alternate gear extension system, and the runway sign.
Factual narrative
On February 17, 2006, approximately 1410 mountain standard time, a Piper PA-30, N7743Y, piloted by an airline transport pilot, sustained substantial damage during a wheels up landing at the Greeley-Weld County Airport (GXY), Greeley, Colorado. Instrument meteorological conditions prevailed at the time of the accident. The personal cross-country flight from Sioux City, Iowa (SUX), to GXY was operating on an instrument flight rules flight plan under the provisions of Title 14 CFR Part 91. The pilot sustained minor injuries. The passenger on board the airplane was not injured. The flight originated at 1110 central standard time The pilot was cleared for the ILS approach to runway 34 (10,000 feet by 100 feet, dry asphalt) and instructed to contact Greeley UNICOM. The pilot performed a missed approach, contacted Denver Approach Control and informed them that he went missed approach for a "no gear indication." The airplane subsequently circled over the airport in an attempt to get the landing gear to come down. Finally, the pilot performed a wheels up landing on runway 34. During the landing, the airplane's right wing struck a runway sign. The pilot said that about half way to GXY, they heard something vibrate. After 5 minutes the vibration stopped. The pilot said the vibration occurred again later. On the ILS approach into GXY, the pilot said the wheels failed to come down. "I advised approach control and said I intended to circle the field and extend the landing gear manually." The pilot said he "was not successful lowering the wheels. They wouldn't budge." The pilot said that Greeley personnel requested he continue to circle until emergency equipment was in place. "I did, and continued trying to lower the wheels. When the airport people were ready, we landed with the wheels up." The pilot said the temperature en route was "about minus 5 [degrees]." An examination of the airplane showed that it sustained skin scrapes to the nose gear doors and the bottom fuselage. Both propellers' blades were curled and showed chordwise scratches. The right outboard wing bottom skin showed a triangular-shaped tear, located approximately 3 feet outboard of the right engine nacelle. The tear was approximately 1-foot long, chordwise, and 4-5 inches wide. It began just below the leading edge and ran aft. Several stringers were broken and bent aft in the area of the tear. Flight control continuity was confirmed. A post-accident examination of the landing gear system showed no anomalies. A witness that assisted in recovering the airplane following the accident reported that the airframe was covered with ice that measured approximately 3/4 inch thick. At 1355, the weather at GXY was reported as ceilings 400 broken, 5,500 broken, 7,500 overcast, 1-1/2 mile visibility, temperature 2 degrees Fahrenheit (F), dew point -2 degrees F, winds 040 at 16 knots, and altimeter 30.32 inches. The pilot was cleared for the ILS approach to runway 34 (10,000 feet by 100 feet, dry asphalt) and was instructed to change radio frequency to the airport UNICOM. The pilot performed a missed approach, contacted approach control and informed them that he was executing a missed approach for a "no gear indication." The airplane subsequently circled over the airport in an attempt to get the landing gear to come down. Finally, the pilot performed a wheels up landing. During the landing, the airplane's right wing struck a runway sign. The pilot said that about half way to their destination, they heard something vibrate. After 5 minutes the vibration stopped. The pilot said the vibration occurred again later. On the ILS approach, the pilot said the wheels failed to come down. "I advised approach control and said I intended to circle the field and extend the landing gear manually." The pilot said he "was not successful lowering the wheels. They wouldn't budge." The pilot said that airport personnel requested he continue to circle until emergency equipment was in place. "I did, and continued trying to lower the wheels. When the airport people were ready, we landed with the wheels up." The pilot said the temperature en route was "about minus 5 [degrees]." Responders to the airplane reported that it was covered with ice that measured approximately 3/4 inch thick. An examination of the airplane's systems showed no anomalies. The weather at the airport was reported as ceilings 400 broken, 5,500 broken, 7,500 overcast, 1-1/2 mile visibility, temperature 2 degrees Fahrenheit (F), dew point -2 degrees F, winds 040 at 16 knots, and altimeter 30.32 inches. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2006_DEN06LA041.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 (icing). 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 2026 · Contractor Report (CR)
Icing Physics Studies Using the 3D SIDRM Test Article: 2023 Icing Tests Analysis
In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation…
- arXiv 2025 · arXiv preprint
Multi-Agent Deep Reinforcement Learning for UAV-Assisted 5G Network Slicing: A Comparative Study of MAPPO, MADDPG, and MADQN
The growing demand for robust, scalable wireless networks in the 5G-and-beyond era has led to the deployment of Unmanned Aerial Vehicles (UAVs) as mobile base stations to enhance coverage in dense urb…
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Mathematical Model on the Temporal Dynamics of Aviation Competitive Pricing
This study investigates the competitive dynamics of airport pricing using U.S. airport data to validate the findings. It employs linear and nonlinear ordinary differential equation models to analyze t…
- NASA NTRS 2025 · Presentation
NASA Icing Update – March 2025
This NASA Icing Update was prepared for presentation to the SAE International AC-9C Inflight Icing Technology Committee. This update includes the following topics: planned Rotational Icing Scaling tes…
- arXiv 2024 · arXiv preprint
An energy-stable phase-field model for droplet icing simulations
A phase-field model for three-phase flows is established by combining the Navier-Stokes (NS) and the energy equations, with the Allen-Cahn (AC) and Cahn-Hilliard (CH) equations and is demonstrated ana…
- NASA NTRS 2024 · Presentation
NASA Icing Update – Oct 2024
This presentation provides a status update on select NASA icing research activities for the SAE AC-9C Icing Technical Committee Meeting on Oct 21, 2024.
Browse the full corpus — academia portal ↗