The Marathon I (M.60) is an all-metal, short/medium-range aeroplane capable of carrying a maximum of 22 passengers or, by simple adaptation, freight and mixed cargo. Two flight crew (first pilot and second pilot/navigator) are carried; radio is installed immediately aft of the cockpit on the starboard side while directly opposite this location provision is made for a forward freight compartment or a seat for a third crew member. A toilet can be fitted on the left-hand side of the passenger cabin just aft of the entrance door and a space at the rear on the-right hand side can be utilized as a wardrobe.
Aircraft Engineering Reference Sheet
7—Handley Page Marathon I
Aircraft Engineering and Aerospace Technology ; 23 , 1 ; 15-18
1951-01-01
4 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Aircraft Engineering Reference Sheet
Emerald Group Publishing | 1949
|Aircraft Engineering Reference Sheet
Emerald Group Publishing | 1949
|Aircraft Engineering Reference Sheet
Emerald Group Publishing | 1950
|Aircraft Engineering Reference Sheet
Emerald Group Publishing | 1949
Aircraft Engineering Reference Sheet
Emerald Group Publishing | 1949
|