Atlantic Southeast Airlines (ASA) Flight 2311 ATC Recording @AirCrashDaily

Air Crash Daily | Atlantic Southeast Airlines (ASA) Flight 2311 ATC Recording @AirCrashDaily | Uploaded May 2024 | Updated October 2024, 1 hour ago.
Credit(s)/Source(s): @elsopaipilla315 & CONUS Archive

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Accident Description:
instagram.com/p/CqqMbayvQZA/?igsh=MTcyMGJiYnk3bWVzMQ==

𝗔𝘁𝗹𝗮𝗻𝘁𝗶𝗰 𝗦𝗼𝘂𝘁𝗵𝗲𝗮𝘀𝘁 𝗔𝗶𝗿𝗹𝗶𝗻𝗲𝘀 𝗙𝗹𝗶𝗴𝗵𝘁 𝟮𝟯𝟭𝟭 was a scheduled domestic passenger flight from Atlanta to Brunswick, operated by an Embraer EMB-120 Brasilia (Reg. N270AS) on 𝗔𝗽𝗿𝗶𝗹 𝟱, 𝟭𝟵𝟵𝟭.

The flight was initially scheduled to depart Atlanta at 13:24 EST and be operated by an EMB-120 Brasilia (Reg. N228AS). Because of mechanical problems an airplane change was made to N270AS. The flight departed Atlanta at 13:47 and arrived in the Brunswick area about 14:44. At 14:48 the flight was cleared for a visual approach to runway 07. The plane had just turned from base leg to final approach when the plane was seen to pitch up about 5° and roll to the left. The plane then nosed down into the ground, 9,975 feet short of the runway.

Examination of the left propeller components indicated a blade angle of about 3°, while the left PCU ballscrew position was consistent with a commanded blade angle of 79.2°. Extreme wear on the PCU quill spline teeth, which normally engaged the titanium-nitrided splines of the propeller transfer tube, was found. The titanium-nitrided surface was much harder and rougher than the nitrided surface of the quill. Therefore, the transfer tube splines acted like a file and caused abnormal wear of the gear teeth on the quill. Wear of the quill was not considered during the certification of the propeller system.

𝗣𝗿𝗼𝗯𝗮𝗯𝗹𝗲 𝗖𝗮𝘂𝘀𝗲:
"The loss of control in flight as a result of a malfunction of the left engine propeller control unit which allowed the propeller blade angles to go below the flight idle position. Contributing to the accident was the deficient design of the propeller control unit by Hamilton Standard and the approval of the design by the Federal Aviation Administration. The design did not correctly evaluate the failure mode that occurred during this flight, which resulted in an uncommanded and uncorrectable movement of the blades of the airplane's left propeller below the flight idle position."

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$Avianca Flight 052 ATC Recording CHAPTERS 0:00 New York ARTCC 1:48 New York APPROACH 5:05 New York TOWER 5:55 New York APPROACH Source/Credit: https://youtu.be/2VyxqNZjcBQ?si=4_RLiQUT1mjsNnUR / @engineergaming4333 Accident Description: https://www.instagram.com/p/Cn1o0fpvyn5/?igshid=OGQ2MjdiOTE= 𝗔𝘃𝗶𝗮𝗻𝗰𝗮 𝗙𝗹𝗶𝗴𝗵𝘁 𝟬𝟱𝟮 was a scheduled international passenger flight from Bogotá to New York with an intermediate stop in Medellín. The flight was being operated by a Boeing 707 (Reg. HK-2016) on 𝗝𝗮𝗻𝘂𝗮𝗿𝘆 𝟮𝟱, 𝟭𝟵𝟵𝟬. The plane departed Medellín at 15:08. When arriving near New York, the plane had to enter 3 holding patterns. The first for 19 minutes over Norfolk, the second for 29 minutes over New Jersey, and the third pattern over the CAMRN intersection for 29 minutes. At 20:44:43, while holding at CAMRN for 26 minutes, the New York ARTCC radar controller advised AVA052 to expect further clearance at 21:05. At that moment the crew advised ATC that they could only hold for 5 more minutes and that their alternate Boston couldnt be reached anymore due to the low state of fuel. The flight left the holding pattern at 20:47 and the crew contacted the New York TRACON who guided AV052 for a runway 22L ILS approach. On finals, at 21:15 the crew contacted JFK Tower and they were cleared to land 4 minutes later. Due to the bad weather (300 feet ceiling, 400 m visibility, RVR of 2,400 feet and wind shear of ca. 10 knots) the crew had to carry out a missed approach at 21:23. ATC vectored the crew for another approach. About 21:32, at 12 miles SE of JFK Airport, engines no. 3 and 4 ran down. Shortly afterwards followed by the remaining two. At 21:34, heading 250° and flaps at 14° and gear up, the plane impacted on a hillside in a wooded residential area on the north shore of Long Island. The starboard side of the forward fuselage impacted and fractured the wooden deck of a residential home. 𝗣𝗿𝗼𝗯𝗮𝗯𝗹𝗲 𝗖𝗮𝘂𝘀𝗲: The failure of the flight crew to adequately manage the airplanes fuel load, and their failure to communicate an emergency fuel situation to air traffic control before fuel exhaustion occurred. Contributing to the accident was the flight crews failure to use an airline operational control dispatch system to assist them during the international flight into a high-density airport in poor weather. Also contributing to the accident was inadequate traffic flow management by the FAA and the lack of standardized understandable terminology for pilots and controllers for minimum and emergency fuel states. The Safety Board also determines that windshear, crew fatigue and stress were factors that led to the unsuccessful completion of the first approach and thus contributed to the accident.$

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