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Last updated: 16 December 2018
Statuts:Enquête Officielle
Date:jeudi 9 mars 1967
Type/Sous-type:Silhouette image of generic DC91 model; specific model in this crash may look slightly different
Douglas DC-9-15
Compagnie:Trans World Airlines - TWA
Immatriculation: N1063T
Numéro de série: 45777/80
Année de Fabrication: 1967
Moteurs: 2 Pratt & Whitney JT8D-7
Equipage:victimes: 4 / à bord: 4
Passagers:victimes: 21 / à bord: 21
Total:victimes: 25 / à bord: 25
Victime de la collision:victimes: 1
Dégats de l'appareil: Perte Totale
Conséquences: Written off (damaged beyond repair)
Lieu de l'accident:près de Urbana, OH (   Etats-Unis d'Amérique)
Phase de vol: En vol (ENR)
Nature:Transport de Passagers Nat.
Aéroport de départ:Pittsburgh International Airport, PA (PIT/KPIT), Etats-Unis d'Amérique
Aéroport de destination:Dayton-James Cox Dayton International Airport, OH (DAY/KDAY), Etats-Unis d'Amérique
Numéro de vol:TW553
TWA 553 operated on a flight from New York to Chicago via Harrisburgh, Pittsburgh, and Dayton. The aircraft operated on an IFR flight plan in visual flight conditions and had been cleared to descend from FL200 to 3000 feet. While descending through 4525 feet the DC-9 collided with a Beechcraft 55 (N6127V operated by the Tann Comp.) which was on a flight to Springfield. The descending DC-9, overtaking and converging from the left, struck the level Beechcraft from the left rear quarter. The collision angle between longitudinal axes of the two aircraft was approx. 47deg in the horizontal plane and 10deg down in the vertical plane. The collision destroyed the Beechcraft by causing it to disintegrate; portions of the Beech penetrated the forward fuselage section of the DC-9 and destroyed the integrity of the flight control system. The DC-9 entered a descending left turn, crashed and burned. The Beechcraft was not under control of, or in radio contact with any FAA traffic facility. Weather at the time of the collision was thin broken clouds with 6-7 miles visibility in haze.

Probable Cause:

PROBABLE CAUSE: "The failure of the DC-9 crew to see and avoid the Beechcraft. Contributing to this cause were physiological and environmental conditions and the excessive speed of the DC-9 which reduced visual detection capabilities under an air traffic control system which was not designed or equipped to separate a mixture of controlled and uncontrolled traffic."

» ICAO Accident Digest Circular 107-AN/81 (38-54)

Opérations de secours
The NTSB suggested some changes in the air traffic control system . Also, the Board recommended the development of a practical Collision Avoidance System (CAS).
Following this accident the FAA issued Advisory Circular 90-32 titled 'Air traffic control and general operations, radar capabilities and limitations'. Also a rule was adopted establishing that all aircraft flying below 10,000ft msl will be limited to a maximum speed of 250kts effective December 15, 1967 to provide a more realistic 'see and avoid' environment.


photo of Douglas DC-9-15 N1063T
Photographed on departure for the accident flight.
Add your photo of this accident or aircraft

Ce plan montre l'aéroport de départ ainsi que la supposée destination du vol. La ligne fixe reliant les deux aéroports n'est pas le plan de vol exact.
La distance entre Pittsburgh International Airport, PA et Dayton-James Cox Dayton International Airport, OH est de 342 km (214 miles).
Accident location: Approximate; accuracy within a few kilometers.

Les informations ci-dessus ne représentent pas l'opinion de la 'Flight Safety Foundation' ou de 'Aviation Safety Network' sur les causes de l'accident. Ces informations prélimimaires sont basées sur les faits tel qu'ils sont connus à ce jour.
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