Aeronaves de Mexico Flight 111 Aftermath Footage @AirCrashDaily

Air Crash Daily | Aeronaves de Mexico Flight 111 Aftermath Footage @AirCrashDaily | Uploaded October 2024 | Updated October 2024, 3 hours ago.
Accident Description:
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𝗔𝗲𝗿𝗼𝗻𝗮𝘃𝗲𝘀 𝗱𝗲 𝗠𝗲𝘅𝗶𝗰𝗼 𝗙𝗹𝗶𝗴𝗵𝘁 𝟭𝟭𝟭 was a scheduled domestic passenger flight from Guadalajara to Mexico City, operated by a Lockheed L-749 Constellation (Reg. XA-MEV) on 𝗝𝘂𝗻𝗲 𝟮, 𝟭𝟵𝟱𝟴.

The Aeronaves de Mexico Constellation crew didn't follow the established climb-out procedure and crashed into the La Latilla Mountain, approximately 13 km from the radio beacon west of Guadalajara Airport, killing all persons aboard.

The flight made a routine take-off from runway 28. A turn to the left was made as though to perform the procedural tear drop turn prescribed by the Airports Manual for climb-out on instruments. Instead of completing the procedural turn, the pilot continued on a straight course for about two minutes in a southwesterly direction. Then, on making a right turn the plane crashed on the mountain peak.

𝗣𝗿𝗼𝗯𝗮𝗯𝗹𝗲 𝗖𝗮𝘂𝘀𝗲:
"The aircraft did not climb out in accordance with previously approved procedure - the provisions of which are set out in the Airports Manual."

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$Spantax Flight 995 Cabin Audio Recording Follow us on Instagram: https://www.instagram.com/aircrashdaily?igsh=aWdteWpkdm92enh1 Source: https://bmac.libs.uga.edu/index.php/Detail/objects/185485 (Credits: @DisasterBreakdown) Accident Description: https://www.instagram.com/p/Cicrs3qvRL3/?igsh=MTN6OGMxdXpvZGRo 𝗦𝗽𝗮𝗻𝘁𝗮𝘅 𝗙𝗹𝗶𝗴𝗵𝘁 𝟵𝟵𝟱 was an international charter flight from Madrid to New York with an intermediate stop in Málaga. The flight was being operated by a McDonnell Douglas DC-10 (Reg. EC-DEG) on 𝗦𝗲𝗽𝘁𝗲𝗺𝗯𝗲𝗿 𝟭𝟯, 𝟭𝟵𝟴𝟮. The plane departed Madrid at 09:36 and arrived at Málaga at 10:20. The crew then taxied to the threshold of runway 14. Takeoff clearance was received at 11:58. During takeoff the co-pilot called out the 80 knots and 100 knots speeds. A short time before reaching V1 (162 knots), pieces of tread of a nose wheel tire started to detach. As the captain tried to rotate by applying up elevator, the vibration was of such magnitude that he feared that the plane might become uncontrollable after takeoff. He decided to abort the takeoff. At that point, with a maximum speed attained of 184 knots, there was 4,250 feet of runway left. The captain retarded the throttles and tried to select reverse thrust. The no. 3 throttle slipped from his hands, causing a power asymmetry. The plane veered slightly to the left. The DC-10 overshot the runway at a speed of 110 knots, colliding with an ILS building, causing engine no. 3 to separate. The plane went through a fence and crossed a highway were it damaged 3 vehicles. It then collided with a farming construction, causing ¾ of the right wing to break off, as well as the right horizontal stabilizer. The plane stopped 1,475 feet past the end of runway 14. A fire erupted in the rear of the fuselage. 𝗣𝗿𝗼𝗯𝗮𝗯𝗹𝗲 𝗖𝗮𝘂𝘀𝗲: The Commission determines the cause of the accident to be the fractional detachment of the retread of the right wheel of the nose gear, originating a strong vibration which could not be identified by the captain, leading hime into the belief that the aircraft would become uncontrollable in flight, and thus deciding to abandon the take-off over VR. The decision of aborting the take-off, though not in accordance with the standard operation procedure, is in this case considered reasonable, on the base of the irregular circumstances that the crew had to face, the short period of time available to take the decision, the lack of training in case of wheel failure and the absence of take-off procedures when failure other than that of the engines occurs.$

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