Overall shape of Fokker F.28 Fellowship is to large extent determined by required airfield performance, i.e., economical operation from runways of less than 4500 ft; aerodynamics, research and wind tunnel tests which preceded choice of wing shape; structural design and basic principles applied to aircraft having five-abreast seating for 60 passengers; aircraft is powered by two Rolls-Royce RB.183-2 Mk 555-15 Spey Junior turbofans of 9850 lb thrust each; description of systems and equipment, flight control, operational and economic performance; two-page cutaway drawing is included.
Fokker Fellowship
Flight
Flight International ; 91 , n 3040
1967
8 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1967
Online Contents | 1995
Introduction to the Fokker F.28 Fellowship
Emerald Group Publishing | 1967
Fokker F.28 Fellowship Ground Handling and Maintenance
Emerald Group Publishing | 1967
Fokker F.28 fellowship -- Ground handling and maintenance
Engineering Index Backfile | 1967