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Cockpit Voice Recorder Inoperable In Philadelphia Jet Crash

AV Web

31, revealing that the cockpit voice recorder (CVR) was not operational at the time of the crash and likely hadn’t captured audio for several years. The data ended one minute later, with the plane at 1,275 feet and traveling at 242 knots. The NTSB report also highlighted that both pilots held a type rating for the Learjet 55.

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Adam’s Profile Reports: Air and Space Exhibits at the Museum of Science and Industry, Chicago

Vintage Aviation News

The aircraft had to land into a 15-knot crosswind, and the plane landed at a speed of 115 mph, well below the standard landing speed of between 150-175 mph. The cockpit is protected by a transparent panel, while sections have been cut into the fuselage to allow for easier access for people with disabilities.

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Are There Consequences for Declaring an Emergency in Flight?

Flying Magazine

The aircraft was equipped with a cockpit camera that captured the entire instrumentation for both the left and right seats, as well as the center pedestal and overhead panel. READ MORE: Pattern Operations Require the Right Technique The pilot was trying to fly by looking at the instrument on the other side of the cockpit, said Sedor.

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Preliminary Reports and Key Updates on Recent Aviation Incidents

Fear of Landing

Analysts confirmed that they had the data from the Cockpit Voice Recorder but last week, there was concern about the fire damage from the Flight Data Recorder. Both cockpit voice recorders were overwritten, so the primary information is crew interviews and ADS-B data. The descent profile matches what we saw from the ADSB data.

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NTSB Releases Preliminary Report on San Diego Crash

Flying Magazine

The weather at the time of the accident included an AIRMET active for IFR conditions with ceilings below 1,000 feet and visibility less than 3 miles due to fog and mist. The LPV has lower weather minimums of the two, as it requires a ceiling of 673 feet versus 750 for the LNAV. The pilot answered, “I think we’ll be alright.”

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Accident Briefs—June 2025

Plane and Pilot

A spring switch in the cockpit controlled the turbocharger wastegate, to select whether the turbocharger was engaged or bypassed (or midrange). Weather at the destination airport at the time of the accident included a 300 feet ceiling, quarter mile visibility in fog, and calm wind.

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Challenger 300 Fatal Upset Wasn’t Turbulence

Fear of Landing

During the take-off roll, the first officer noticed that although the Challenger 300 was accelerating normally, the right-side primary flight control had stopped showing acceleration above 40 knots. The captain slowed the aircraft from 104 knots and exited the runway onto a taxiway. He called out that he had no airspeed.