N8930N Aviation Accident 2025-04-11: Difference between revisions

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Created page with "= Accident Summary = === '''Fatal Accident (2) - Piper PA-60-601P Aerostar, D-ICEL, Salzgitter, Germany, April 13, 2025.''' === == Interactive Map == <html><iframe src="https://wiki.alsresume.com/maps/d-icel.html" width="800" height="450" frameborder="0" scrolling="no"></iframe></html> == Accident Information == {| class="wikitable" |+ ! Approx. Avalanche Location ! Aircraft Fatalities ! Ground Fatalities ! Injured ! ASN Entry |- | [https://g.co/kgs/TVWRwjJ 52°9'10.4..."
 
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[[File:N8930N.jpg|thumb|right|Cessna 310R, N8930N|333x333px]]
= Accident Summary =
= Accident Summary =


=== '''Fatal Accident (2) - Piper PA-60-601P Aerostar, D-ICEL, Salzgitter, Germany, April 13, 2025.''' ===
=== '''Fatal Accident (3) - ReProp LLC 310 Series' Cessna 310R, N8930N, Boca Raton, FL, April 11, 2025''' ===


== Interactive Map ==
== Interactive Map ==
<html><iframe src="https://wiki.alsresume.com/maps/d-icel.html" width="800" height="450" frameborder="0" scrolling="no"></iframe></html>
<html><iframe src="https://wiki.alsresume.com/maps/n8930n.html" width="800" height="450" frameborder="0" scrolling="no"></iframe></html>


== Accident Information ==
== Accident Information ==
{| class="wikitable"
{| class="wikitable"
|+
|+
! Approx. Avalanche Location
! Approx. Accident Location
! Aircraft Fatalities
! Aircraft Fatalities
! Ground Fatalities
! Ground Fatalities
Line 15: Line 16:
! ASN Entry
! ASN Entry
|-
|-
| [https://g.co/kgs/TVWRwjJ 52°9'10.48"N, 10°24'43.43"E]
| [https://g.co/kgs/muUrWU9 26°22'3.42"N, 80° 7'14.93"W]
| style="color:red; font-weight:bold;" | 2
| style="color:red; font-weight:bold;" | 3
| 0
| 0
| 0
| 0
| [https://asn.flightsafety.org/wikibase/497968 Aviation Safety Network]
| [https://asn.flightsafety.org/wikibase/496232 Aviation Safety Network]
|}
|}


Line 31: Line 32:
! Manufacture Date
! Manufacture Date
|-
|-
| [https://wiki.alsresume.com/index.php?title=Piper_Aerostar Piper PA-60-601P Aerostar]
| [https://wiki.alsresume.com/index.php?title=Cessna_310 Cessna 310R]
| Private
| ReProp LLC 310 Series
| D-ICEL
| [https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8930N N8930N]
| 61P-0577-79632
| [https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8930N 310R0986]
| [https://www.flightradar24.com/data/aircraft/d-icel?utm_source=chatgpt.com 1978]
| [https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8930N 1977]
|}
|}


== Gallery ==
== Gallery ==
<html>
<html>
<iframe src="https://asxgalleries.alsresume.com/d-icel/" width="800px" height="400px" frameborder="0" scrolling="yes" style="text-align: left;"></iframe>
<iframe src="https://asxgalleries.alsresume.com/n8930n/" width="800px" height="400px" frameborder="0" scrolling="yes" style="text-align: left;"></iframe>
</html>
</html>


== YouTube Video(s) ==
== YouTube Video(s) ==
<table>
<table>
<tr>
<td><embedvideo service="youtube" dimensions="395x222" alignment="right">lmy_w1QibKE</embedvideo></td><td><embedvideo service="youtube" dimensions="395x222" alignment="right">v=rpBg63EzKDA</embedvideo></td>
<tr>
<td><embedvideo service="youtube" dimensions="395x222" alignment="right">MTtNtlpp708</embedvideo></td><td><embedvideo service="youtube" dimensions="395x222" alignment="right">MikOezAdtfU</embedvideo></td><td></td></tr>


<tr>
<td><embedvideo service="youtube" dimensions="395x222" alignment="right">MikOezAdtfU</embedvideo></td>
</tr>
</table>
</table>


== Other Video(s) ==
== Other Video(s) ==
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== ASX Accident Report ==
== ASX Accident Report ==
On the morning of Sunday, April 13, 2025, a [https://wiki.alsresume.com/index.php?title=Piper_Aerostar Piper PA-60-601P Aerostar] registered as D-ICEL departed from [https://wiki.alsresume.com/images/thumb/0/04/Salzgitter-Dr%C3%BCtte_Airfield_%28EDVS%29.png/797px-Salzgitter-Dr%C3%BCtte_Airfield_%28EDVS%29.png?20250414163616 Salzgitter-Drütte Airfield (EDVS)] in Lower Saxony, Germany. The aircraft was privately owned and operated, and its planned destination was Hildesheim Airfield (EDVM), located approximately 35 kilometers southeast. On board were two occupants: a 55-year-old pilot and a 56-year-old co-pilot, both residents of Salzgitter. The aircraft took off around 09:40 local time under clear weather conditions, with the METAR reports indicating calm wind and CAVOK visibility.


Shortly after takeoff, eyewitnesses observed the aircraft pitching sharply upward before descending uncontrollably. Within approximately one kilometer of flight distance from the departure point, the Aerostar impacted the grounds of the Salzgitter AG steel production complex, specifically crashing into a narrow six-meter-wide corridor between two large industrial halls. The crash resulted in a post-impact fire, with the aircraft completely consumed in flames. Emergency services responded rapidly with over 90 personnel including the plant's internal fire brigade, city fire units, medical responders, and trauma support staff.
On April 11, 2025, at approximately 10:23 AM local time, a 1977 Cessna 310R registered as N8930N and operated by ReProp LLC was involved in a fatal accident near Boca Raton, Florida. The aircraft had departed Boca Raton Public Airport (KBCT) and was en route to Tallahassee International Airport (KTLH) with three individuals on board. The occupants, all members of the Stark family, were identified as 81-year-old Robert Stark, 54-year-old Stephen Stark, and 17-year-old Brooke Stark. All three occupants sustained fatal injuries. One individual on the ground, Pablo Tafur, was injured but survived with non-life-threatening injuries when his vehicle was impacted as a result of the post-crash fire and subsequent debris.
 
The accident occurred shortly after takeoff from Runway 05 at KBCT. ADS-B flight tracking data and eyewitness reports indicate that the aircraft exhibited erratic behavior in flight, including a continuous series of left-hand turns and difficulty in maintaining altitude, with the aircraft failing to climb above approximately 600 feet above ground level. Multiple witnesses reported seeing the aircraft flying low and unsteady, and some described a circling motion before the aircraft appeared to return toward the airport, likely in an attempted emergency return-to-field maneuver.
 
The Cessna 310R impacted terrain near the intersection of Military Trail and Glades Road, with significant portions of wreckage strewn across the roadway and adjacent railroad tracks. The impact resulted in a post-crash fire, which consumed most of the aircraft. Video and photographic evidence showed both engines operating at the time of the crash and the landing gear in the down position. This aligns with the possibility that the pilot was preparing for a forced landing. Recorded ATC and witness reports indicated the pilot had declared or relayed a mechanical issue—specifically rudder difficulties—prior to the crash.
 
Preliminary analysis from accident observers and aviation analysts indicates that a rudder hard-over condition likely occurred, which would have severely limited the aircraft’s controllability. The Cessna 310R features a large rudder designed to counteract asymmetric thrust, and a hard-over condition would require substantial compensatory aileron and asymmetric engine power management to avoid an uncontrollable yaw and roll. This scenario is consistent with the observed left-turning flight path, side-slip flight profile, and inability to maintain stable airspeed and altitude. The aircraft’s airspeed was recorded fluctuating between 96 and 148 knots ground speed, further highlighting the instability.
 
The NTSB began their on-scene investigation the same afternoon, focusing on three investigative areas: the aircraft, the pilot, and the environment. The investigative team collected flight tracking data, maintenance records, weather data, pilot credentials, and electronic media. The METAR at the time of the accident reported clear conditions with visibility of 10 statute miles and wind from 350° at 5 knots, indicating that environmental factors were unlikely to have been a significant contributor. The aircraft was manufactured in 1977 and had a history of ownership under Robert Stark, an experienced aerobatic pilot and multi-engine, instrument-rated private pilot.
 
Although definitive causal findings await the NTSB’s final report, all current evidence supports the conclusion that a mechanical failure involving the rudder system led to a progressive loss of control shortly after departure. Despite the apparent efforts by the pilot(s) to manage the situation through asymmetric thrust and emergency maneuvering, the aircraft was unable to maintain a safe flight envelope and ultimately impacted a populated area. The severity of the mechanical issue, combined with low altitude and urban terrain, limited recovery options, leading to the fatal outcome for all on board.
 
</div>


The aircraft was destroyed on impact, and both occupants were fatally injured. According to multiple reports, the airframe fragmented on impact, and only a charred steel frame remained once the fire was extinguished. There were no injuries to people on the ground and only minor damage to the buildings. The ongoing operations of Salzgitter AG were not interrupted by the crash. Aerial photos and video taken by news outlets confirmed scattered debris and burn marks along a confined area on the factory premises.


Initial investigative efforts were led by the German Federal Bureau of Aircraft Accident Investigation (BFU), which secured the wreckage for forensic examination. The aircraft’s engines may be transported to Braunschweig for further analysis. No definitive cause has yet been identified, but reports suggest possible engine failure or mechanical anomaly shortly after takeoff. Witnesses mentioned seeing the aircraft enter a yawing or unstable attitude prior to its descent. The BFU indicated that a full investigation could take up to a year, with a preliminary report expected within several weeks.


The Piper PA-60-601P Aerostar is a twin-engine, high-performance light aircraft known for its speed and pressurization capabilities. The specific airframe involved, serial number 61P-0577-79632, had previously operated under registrations N8091J and C-FDNJ before becoming D-ICEL. Records indicate the pilot was considered experienced and active within a local flying club. However, due to the lack of immediate data from onboard recording devices and the total destruction of the aircraft, determining the chain of events leading to the accident will rely heavily on mechanical analysis, witness accounts, and reconstructed flight data.


== Tracking and Social Media ==
== Tracking and Social Media ==
* '''Flight Tracking:''' [https://www.flightradar24.com/data/aircraft/d-icel?utm_source=chatgpt.com Flightradar24], FlightAware, ADS-B Exchange
* '''Flight Tracking:''' [https://www.flightradar24.com/data/aircraft/n8930n Flightradar24], [https://www.flightaware.com/live/flight/N8930N FlightAware], [https://globe.adsbexchange.com/?icao=ac52de&lat=26.370&lon=-80.126&zoom=14.8&showTrace=2025-04-11&trackLabels ADS-B Exchange]
* '''Social Media:''' Facebook, Instagram, X (formerly Twitter)
* '''Social Media:''' Facebook, Instagram, [https://x.com/HEXJUMPER293949 X (formerly Twitter)]


== Sources and References ==
== Sources and References ==
* [https://www.ndr.de/nachrichten/niedersachsen/braunschweig_harz_goettingen/Kleinflugzeug-stuerzt-ueber-Gelaende-der-Salzgitter-AG-ab-zwei-Tote,salzgitter1284.html NDR]
* [https://www.nbcnews.com/news/us-news/small-plane-crashes-boca-raton-airport-florida-rcna200854 NBC News]
* [https://www.bild.de/news/salzgitter-kleinflugzeug-stuerzt-in-stahlwerk-zwei-tote-67fb8b0d3ceb7108c48fc2bb Bild]
* [https://bocanewsnow.com/2025/04/11/plane-crashes-in-boca-raton-two-reported-dead/ Boca News Now]
* [https://www.jetphotos.com/registration/D-ICEL JetPhotos]
* [https://www.jetphotos.com/registration/D-ICEL JetPhotos]
* LiveATC
* [https://www.msn.com/en-us/news/us/small-plane-crashes-in-boca-raton-florida-all-3-on-board-killed/vi-AA1CKSJL?ocid=socialshare MSN]
 
 
 
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Latest revision as of 09:27, 7 May 2025

Cessna 310R, N8930N

Accident Summary

Fatal Accident (3) - ReProp LLC 310 Series' Cessna 310R, N8930N, Boca Raton, FL, April 11, 2025

Interactive Map

Accident Information

Approx. Accident Location Aircraft Fatalities Ground Fatalities Injured ASN Entry
26°22'3.42"N, 80° 7'14.93"W 3 0 0 Aviation Safety Network

Aircraft Information

Type Operator Registration Serial Number Manufacture Date
Cessna 310R ReProp LLC 310 Series N8930N 310R0986 1977

Gallery

YouTube Video(s)

Other Video(s)

ASX Accident Report

On April 11, 2025, at approximately 10:23 AM local time, a 1977 Cessna 310R registered as N8930N and operated by ReProp LLC was involved in a fatal accident near Boca Raton, Florida. The aircraft had departed Boca Raton Public Airport (KBCT) and was en route to Tallahassee International Airport (KTLH) with three individuals on board. The occupants, all members of the Stark family, were identified as 81-year-old Robert Stark, 54-year-old Stephen Stark, and 17-year-old Brooke Stark. All three occupants sustained fatal injuries. One individual on the ground, Pablo Tafur, was injured but survived with non-life-threatening injuries when his vehicle was impacted as a result of the post-crash fire and subsequent debris.

The accident occurred shortly after takeoff from Runway 05 at KBCT. ADS-B flight tracking data and eyewitness reports indicate that the aircraft exhibited erratic behavior in flight, including a continuous series of left-hand turns and difficulty in maintaining altitude, with the aircraft failing to climb above approximately 600 feet above ground level. Multiple witnesses reported seeing the aircraft flying low and unsteady, and some described a circling motion before the aircraft appeared to return toward the airport, likely in an attempted emergency return-to-field maneuver.

The Cessna 310R impacted terrain near the intersection of Military Trail and Glades Road, with significant portions of wreckage strewn across the roadway and adjacent railroad tracks. The impact resulted in a post-crash fire, which consumed most of the aircraft. Video and photographic evidence showed both engines operating at the time of the crash and the landing gear in the down position. This aligns with the possibility that the pilot was preparing for a forced landing. Recorded ATC and witness reports indicated the pilot had declared or relayed a mechanical issue—specifically rudder difficulties—prior to the crash.

Preliminary analysis from accident observers and aviation analysts indicates that a rudder hard-over condition likely occurred, which would have severely limited the aircraft’s controllability. The Cessna 310R features a large rudder designed to counteract asymmetric thrust, and a hard-over condition would require substantial compensatory aileron and asymmetric engine power management to avoid an uncontrollable yaw and roll. This scenario is consistent with the observed left-turning flight path, side-slip flight profile, and inability to maintain stable airspeed and altitude. The aircraft’s airspeed was recorded fluctuating between 96 and 148 knots ground speed, further highlighting the instability.

The NTSB began their on-scene investigation the same afternoon, focusing on three investigative areas: the aircraft, the pilot, and the environment. The investigative team collected flight tracking data, maintenance records, weather data, pilot credentials, and electronic media. The METAR at the time of the accident reported clear conditions with visibility of 10 statute miles and wind from 350° at 5 knots, indicating that environmental factors were unlikely to have been a significant contributor. The aircraft was manufactured in 1977 and had a history of ownership under Robert Stark, an experienced aerobatic pilot and multi-engine, instrument-rated private pilot.

Although definitive causal findings await the NTSB’s final report, all current evidence supports the conclusion that a mechanical failure involving the rudder system led to a progressive loss of control shortly after departure. Despite the apparent efforts by the pilot(s) to manage the situation through asymmetric thrust and emergency maneuvering, the aircraft was unable to maintain a safe flight envelope and ultimately impacted a populated area. The severity of the mechanical issue, combined with low altitude and urban terrain, limited recovery options, leading to the fatal outcome for all on board.



Tracking and Social Media

Sources and References