Wednesday, May 14, 2025

D'Apuzzo D-295 Senior Aero Sport, N321WC, accident occurred on April 19, 2025, near Phoenix Deer Valley Airport (DVT/KDVT), Phoenix, AZ

 This is preliminary information, subject to change, and may contain errors. Any errors in this report will be corrected when the final report has been completed.

Aviation Accident Preliminary Report - National Transportation Safety Board

The National Transportation Safety Board did not travel to the scene of this accident.

Investigator In Charge (IIC): Nepomuceno, Eleazar

Additional Participating Entities:

Scott Boek; Federal Aviation Administration; Scottsdale, AZ 

Mark Platt; Lycoming; Phoenix, AZ 

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N321WC

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200044/pdf

N321 Whiskey Charlie LLC

  • Location: Phoenix, AZ 
  • Accident Number: WPR25LA136 
  • Date & Time: April 19, 2025, 11:06 Local 
  • Registration: N321WC 
  • Aircraft: D'Apuzzo Senior Aero Sport 
  • Injuries: 1 None 
  • Flight Conducted Under: Part 91: General aviation - Personal 

On April 19, 2025, about 1106 Pacific daylight time, an experimental amateur built D'Apuzzo Senior Aero Sport, N321WC, was substantially damaged when it was involved in an accident near Phoenix, Arizona. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported after completing a thorough preflight inspection and adding fuel to the main saddle tanks. The pilot departed runway 7R at Phoenix Deer Valley Airport, Phoenix, Arizona, with the intention of staying in the airport traffic pattern, to “exercise the airplane.” During an approach for a third touch and go takeoff and landing, the pilot initiated a go-around at the direction of the air traffic control tower controller. As he turned onto the downwind leg for runway 7R, about 1,000 ft above the ground (agl), the engine RPM surged multiple times followed by a total loss of engine power. The pilot turned the electric fuel boost pump on (both high and low speed settings) and cycled the throttle and mixture lever settings, but the engine did not restart.

About 700 ft agl, the pilot turned towards the airport and declared an emergency, in which he was immediately cleared by a tower controller to land on runway 25R. The pilot realized that he would not be able to make it to the airport and initiated a forced landing onto a road. During the off-airport landing sequence, the pilot the pilot maneuvered from the road to avoid a vehicle, and the airplane impacted a carport roof. Subsequently the airplane came to rest nose down in a parking lot. Postaccident examination of the airplane revealed that both lower wings were substantially damaged.

The airplane was recovered to a secure location for further examination.

Tuesday, May 13, 2025

Cessna 560 Citation V, N611VG, fatal accident occurred on June 4, 2023, near Montebello, Virginia

The National Transportation Safety Board travelled to the scene of this accident.

Investigator In Charge (IIC): Gerhardt, Adam

Additional Participating Entities:

  • Mitch A. Mitchell; FAA/AVP; Washington, DC 
  • Helen Tsai; Transportation Safety Board of Canada; Gatineau , OF 
  • Ricardo J. Asensio; Textron Aviation; Wichita, KS 
  • David Studtmann; Honeywell Aerospace; Phoenix, AZ 
  • Randolph W. Rushworth; Department of the United States Air Force; Washington, DC

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/192300/pdf

https://data.ntsb.gov/Docket?ProjectID=192300

http://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=611VG

Encore Motors of Melbourne Inc

Location: Montebello, Virginia 
Accident Number: ERA23FA256 
Date & Time: June 4, 2023, 15:23 Local 
Registration: N611VG 
Aircraft: Cessna 560 Aircraft 
Damage: Destroyed 
Defining Event: Unknown or undetermined 
Injuries: 4 Fatal 
Flight Conducted Under: Part 91: General aviation - Personal 

On June 4, 2023, at 1523 eastern daylight time, a Cessna Citation 560 airplane, N611VG, was destroyed when it was involved in an accident near Montebello, Virginia. The airline transport pilot and three passengers were fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot and three passengers departed on a cross-country flight. Shortly after the airplane climbed through 26,600 ft, the pilot stopped responding to air traffic control instructions. According to ADS-B data, the airplane continued climbing to 34,000 ft, then flew at that altitude along its flight plan waypoints, turning southwest to overfly the intended destination about 1 hour later. The airplane continued flying for about another hour along a relatively constant track and altitude before entering a spiraling descent and impacting terrain.

United States Air Force (USAF) pilots intercepted the airplane about 2 minutes before it began the spiraling descent. They observed no breaches of the airplane structure or doors, no smoke in the cockpit or passenger cabin, and no oxygen masks deployed in the cabin. One occupant was observed slumped over in the pilot seat and no movement or other occupants were observed in the cabin.

Based on the lack of response to air traffic control communications, ADS-B data showing the airplane following its flight plan waypoints at the altitude last assigned by air traffic control, and the USAF pilot observations, it is likely that the pilot of the accident airplane became incapacitated during the climb to cruise altitude. It is also likely the airplane trajectory was then directed by the autopilot until a point at which it was no longer able to maintain control.

The pilot had medical conditions, including high blood pressure and high cholesterol, that represented some increased risk of an impairing or incapacitating cardiovascular event. In addition, the pilot had prior prescriptions for medications that could be impairing if used too recently before flight. However, there was no evidence of the pilot being at exceptionally high incapacitation risk, or of using medications inappropriately. Based on the accident circumstances, it is likely that all the airplane occupants were incapacitated due to a common environmental condition, such as loss of cabin pressurization.

Maintenance records indicated that, at the time of the accident flight, five items were overdue for inspection, including the co-pilot oxygen mask. About 4 weeks before the accident flight, maintenance personnel noted 26 discrepancies that the owner declined to address, including several related to the pressurization and environmental control system. Furthermore, 2 days before the accident flight, maintenance personnel noted that the pilot-side oxygen mask was not installed, and the supplementary oxygen was at its minimum serviceable level. At that level, oxygen would not have been available to the airplane occupants and passenger oxygen masks would not have deployed in the event of a loss of pressurization. No evidence was found to indicate that the oxygen system was serviced or that the pilot-side oxygen mask was reinstalled before the accident flight.

Altitude-related hypoxia, although not verifiable from forensic medical evidence, likely explains the incapacitation of the airplane occupants. According to the FAA Pilot’s Handbook of Aeronautical Knowledge, impairing effects from hypoxia are often vague and are experienced differently by different individuals; they include confusion, disorientation, diminished judgment and reactions, worsened motor coordination, difficulty communicating and performing simple tasks, a false sense of well-being, diminished consciousness, and, if conditions aren’t remedied or mitigated, death.

Between 30,000 and 35,000 ft, the time of useful consciousness for a pilot to take protective action against hypoxia, including donning an oxygen mask and descending, is about 1/2 to 2 minutes. These times depend on multiple variables, including medical factors, with substantial variation among individuals. The times are decreased by about half when depressurization is rapid. However, gradual depressurization can be as dangerous or more dangerous than rapid depressurization because of its potential to insidiously impair a pilot’s ability to recognize and respond to the developing emergency until the pilot is no longer effectively able to do so. Cognitive impairment from hypoxia makes it harder for affected individuals to recognize their own impairment.

Based on the available information, it is likely that the airplane occupants became hypoxic due to a lack of oxygen during the flight and became incapacitated. However, the reason for the loss of pressurization, and whether it was rapid or progressed over time, could not be determined.

- Probable Cause: 

Pilot incapacitation due to loss of cabin pressure for undetermined reasons. Contributing to the accident was the pilot’s and owner/operator’s decision to operate the airplane without supplemental oxygen.

Sunday, May 11, 2025

Ryan Navion A, N2341, accident occurred on November 19, 2024, at Aero Estates Airport (7IS2), Belleville, Illinois


The National Transportation Safety Board did not travel to the scene of this accident.

Investigator In Charge (IIC): Abraham, Laura

Additional Participating Entities:

  • Klarann Voegelle; FAA
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/195394/pdf

https://data.ntsb.gov/Docket?ProjectID=195394

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=2341

Location: Belleville, Illinois 
Accident Number: CEN25LA032 
Date & Time: October 19, 2024, 14:00 Local 
Registration: N2341 Aircraft: Ryan NAVION A 
Aircraft Damage: Substantial 
Defining Event: Loss of control in flight 
Injuries: 1 None 
Flight Conducted Under: Part 91: General aviation - Personal

Analysis:
An airport surveillance video showed the airplane in a takeoff roll become airborne in a nosehigh attitude, settle back down to the runway, and bounce hard on the main landing gear. The airplane went through this cycle twice and on the final bounce, the right wheel separated from the airplane and the left horizontal stabilizer struck the ground, which resulted in substantial damage.

Attempts were made to contact the pilot for a statement, and a National Transportation Safety Board Form 6120.1 Pilot/Operator Aircraft Accident/Incident Report was mailed to the pilot’s address via certified mail. The pilot did not return phone calls, and the accident report form was returned as “undeliverable.”

An examination of the airplane revealed no mechanical anomalies that would have precluded normal operations. 

Probable Cause: 

The pilot’s failure to maintain airplane control during the takeoff.

Saturday, May 10, 2025

Aqua-Bee, N799RX, accident on February 25, 2025, at Miami–Opa Locka Executive Airport (OPF/KOPF), Miami Gardens, Florida

Aviation Investigation Final Report - National Transportation Safety Board

The National Transportation Safety Board did not travel to the scene of this accident.

Investigator In Charge (IIC): Mccarter, Lawrence

Additional Participating Entities:

  • Michael H. Torrent; FAA/FSDO; Miramar, FL
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/199777/pdf

https://data.ntsb.gov/Docket?ProjectID=199777

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N799RX

Location: Miami, Florida 
Accident Number: ERA25LA131 
Date & Time: February 25, 2025, 15:30 Local 
Registration: N799RX Aircraft: MALLORY HORTON AQUA-BEE 
Aircraft Damage: Substantial Defining 
Event: Landing gear not configured 
Injuries: 1 None 
Flight Conducted Under: Part 91: General aviation - Flight test 

At the conclusion of the local test flight of the experimental amateur-built amphibious airplane, the pilot arrived back in the airport traffic pattern for landing. After receiving clearance to land, he arrived over the runway, reduced power and flared for landing, realizing that he had not extended the landing gear when he heard the hull contact the runway. The airplane skidded to a stop resulting in substantial damage to the fuselage/hull. The pilot reported that there were no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation.

Probable Cause:
The pilot’s failure to lower the landing gear before touchdown.

Eurocopter EC 130T2 (Airbus Helicopters H130), N3WL, accident occurred on February 13, 2025, at Canyonlands Regional Airport (CNY/KCNY), Moab, Utah






Aviation Investigation Final Report - National Transportation Safety Board

The National Transportation Safety Board did not travel to the scene of this accident.

Investigator In Charge (IIC): Swick, Andrwe

Additional Participating Entities:

  • James Hill; FAA-FSDO; Salt Lake City, UT

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/199715/pdf

https://data.ntsb.gov/Docket?ProjectID=199715

Well Lived Mt LLC

https://registry.faa.gov/aircraftinquiry/Search/NNumberResult?NNumberTxt=N3WL

Location: Moab, Utah 
Accident Number: WPR25LA093 
Date & Time: February 13, 2025, 10:50 Local 
Registration: N3WL
Aircraft: Airbus Helicopters EC 130 T2 Aircraft 
Damage: Substantial 
Defining Event: Collision with terr/obj (non-CFIT) 
Injuries: 7 None 
Flight Conducted Under: Part 91: General aviation - Unknown 

Analysis:

The pilot reported that shortly after he lifted off from a helipad, a window dislodged from a nearby hangar door and impacted the helicopter’s main rotor blade from behind, which in a loss of lift and an excessive vibration. The pilot initiated an emergency landing and subsequently landed hard. One of the main rotor blades was substantially damaged. The pilot reported that there were no preimpact mechanical malfunctions or failures with the helicopter that would have precluded normal operation.

Probable Cause:

The inflight collision with debris during takeoff.

Amazon MK30, N265PA, accident occurred on February 21, 2025, at Pendleton UAS Range, Pendleton, Oregon

Aviation Investigation Final Report - National Transportation Safety Board

The National Transportation Safety Board did not travel to the scene of this accident.

Investigator In Charge (IIC): Gutierrez, Eric

Additional Participating Entities:

  • Christopher Painter; FAA; Portland, OR

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/199746/pdf

https://data.ntsb.gov/Docket?ProjectID=199746

Amazon.com Services LLC

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N265PA

Location: Pendleton, Oregon
Accident Number: WPR25LA103
Date & Time: February 21, 2025, 10:33 Local
Registration: N265PA
Aircraft: AMAZON.COM SERVICES LLC MK30 Aircraft
Damage: Substantial Defining Event: Collision with terr/obj (non-CFIT)
Injuries: 1 None
Flight Conducted Under: Part 91: General aviation - Flight test

Analysis:

The operator of the unmanned aircraft system (UAS) reported that, the purpose of the flight was to test the Safe Contingent Land (SCL) during a flight test operation, vertical ascent following a delivery. An obstacle (cart) was intentionally placed in the delivery area. As the UAS hovered over the delivery location, a commercial drone piloted by another employee, intentionally flew above the UAS. The UAS detected the drone and descended. During the descent the UAS struck the cart and came to a stop on the ground near the cart. After landing, the UAS performed an unplanned vertical ascent, started to oscillate, and descended into the ground.

The UAS sustained substantial damage to the upper wing struts and fuselage.

The operator reported that there were no preaccident mechanical failures or malfunctions with the UAS that would have precluded normal operation.

Probable Cause: 

The unmanned aircraft system’s failure to maintain clearance from an obstacle, which resulted in a loss of control and impact with terrain.

Piper PA-18-150 Super Cub, N82065, accident occurred on August 15, 2024, near Arctic Village, Alaska

Aviation Investigation Final Report - National Transportation Safety Board

The National Transportation Safety Board did not travel to the scene of this accident.

Investigator In Charge (IIC): Rasmussen, Mitchell

Additional Participating Entities:

  • Kyle Weinzirl; FAA FSDO Fairbanks; Fairbanks, AK

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/194992/pdf

https://data.ntsb.gov/Docket?ProjectID=194992

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=
N82065

Analysis:

The pilot reported that, shortly after takeoff, the airplane encountered a strong gust of wind that lifted the left wing and pushed the airplane to the right of the remote, off airport site. The right wingtip struck the ground, and the airplane ground looped which resulted in substantial damage to the right wing and horizontal stabilizer. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation.

Probable Cause:

The pilot’s failure to maintain directional control of the airplane during takeoff in gusting wind conditions.