America's Fighters of the 1980s - F-16 & F-18 by Robert C. Stern

By Robert C. Stern

London released smooth Conflicts - Air

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Windshield Fairing 4. Windshield 5. Side Doors 6. Top Door 36 7. Rear Windows 8. Turtle Deck 9. Ventilation Scoop 10. Forward Cap 11. Handle 12. Screws 13. Rivets 14. AirScoop 16. Retaining Straps 17. Retaining Straps Left side cabane struts and trailing edge of wing centersection. Parabolic mirrors permit wide-field aft view. Modified centersection ofGene Soucy's one-off, two-seat aerial demonstation Ag-Cat. Visible is lowerportion of wng-walker support assembly. Cabane strut assembly mounted immediately undercentersection of upper wing.

Horizontal Tail Span: 13ft. 0 in. Landing Gear Track: 8 ft. 4 in. Empty Weight: 3,025 pounds Gross Weight: 6,075 pounds 32 -------~------. Grumman/Schweizer Model 450B Ag-Cat Length: 24 ft. 62 in. Wingspan: 42 ft. 39 in. Height: 11 ft. 9 in. Horizontal Tail Span: 13 ft. 0 in. Landing Gear Track: 8 ft. 0 in. Empty Weight: 3,625 pounds Gross Weight: 5,200 pounds Grumman/Schweizer Model G-164B Turbine Ag-Cat Length: 26 ft. 9 in. Wingspan: 42ft. 5 in. Height: 11 ft. 9 in. Horizontal Tail Span: 13 ft.

Oil Outlet Hose 13. Oil Cooler 14. Surge Valve 15. Fitting 16. "Y" Drain 17. Oil Tank Vent Hose 18. Oil Feed Line 19. Oil Cooler Pipe 20. Hose Engine mount forGarrett turboshaft engine. g. requirements. Center Section Assembly AnotherG-164A turboshaft engine modification utilized a Pratt & Whitney PT6A-34 (seen on G-164A N9889). 1 ~o',E~gineCOWling ~~ ~ ", \ r J ' I : , ®" ' . -:-'. ' . ~\' .. '" l , --- ~- ~~:"'" , ~~ Q Fuel System Vent Lines (48 Gallon) 4 1. Top Panel ~ 2. Channel ~ 3. Side Panel.

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