NTSB Releases Images Of Fatigue Cracks In Chalk's Wreckage | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-06.23.25

Airborne-NextGen-06.24.25

AirborneUnlimited-06.25.25

Airborne-AffordableFlyers-06.26.25

AirborneUnlimited-06.27.25

Thu, Dec 22, 2005

NTSB Releases Images Of Fatigue Cracks In Chalk's Wreckage

Accident Claimed 20 Lives

(Editor's Note: The following is the unedited text of the National Transportation Safety Board's latest release concerning the December 19 accident involving a Chalk's Ocean Airways Grumman seaplane. While the probable cause of the accident has yet to be released, it appears increasingly likely fatigue cracks in the aircraft's main spar caused the right wing to separate from the aircraft, sending the plane into the waters of Miami's Government Cut shortly after takeoff.)

The National Transportation Safety Board has released photos depicting fatigue cracks found on the separated wing of the Chalk’s Ocean Airways plane that crashed into the water near Miami Beach on Monday.

On Tuesday afternoon, the right wing of the aircraft was recovered. The wing had separated at the inboard section, at the wing/fuselage juncture. Safety Board engineers and metallurgists agree that the signatures are consistent with fatigue fractures. Portions of the wing are at the NTSB metallurgy laboratory in Washington, DC.

As part of the investigation of this accident, which claimed 20 lives, the Safety Board will extensively examine the wing and other structures in the coming days. The probable cause of this accident has not been determined.

IMAGE 1: Overall view of the inboard end of the right wing as it was recovered from the water. An unlabeled arrow indicates the lower spar cap of the rear spar where fatigue features were observed.

IMAGE 2: Closer view of the fracture surface at the inboard end of the lower spar cap of the right wing rear spar. Unlabeled arrows indicate the location of two offset drilled holes.

IMAGE 3: Closer view of the fatigue region in the horizontal leg of the lower spar cap of the rear spar. Unlabeled brackets indicate fatigue origin areas at the surfaces of the fastener hole, and dashed lines indicate the extent of the fatigue region visible on the fracture surface.

FMI: www.ntsb.gov

Advertisement

More News

TikToker Arrested After Landing His C182 in Antarctica

19-Year-Old Pilot Was Attempting to Fly Solo to All Seven Continents On his journey to become the first pilot to land solo on all seven continents, 19-year-old Ethan Guo has hit a >[...]

Classic Aero-TV: Versatile AND Practical - The All-Seeing Aeroprakt A-22 LSA

From 2017 (YouTube Edition): A Quality LSA For Well Under $100k… Aeroprakt unveiled its new LSA at the Deland Sport Aviation Showcase in November. Dennis Long, U.S. Importer>[...]

ANN's Daily Aero-Term (06.27.25): Hazardous Weather Information

Hazardous Weather Information Summary of significant meteorological information (SIGMET/WS), convective significant meteorological information (convective SIGMET/WST), urgent pilot>[...]

ANN's Daily Aero-Linx (06.27.25)

Aero Linx: Historic Aircraft Association (HAA) The Historic Aircraft Association (HAA) was founded in 1979 with the aim of furthering the safe flying of historic aircraft in the UK>[...]

Aero-News: Quote of the Day (06.27.25)

"We would like to remember Liam not just for the way he left this world, but for how he lived in it... Liam was fearless, not necessarily because he wasn't afraid but because he re>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2025 Web Development & Design by Pauli Systems, LC