FlightGlobal.com
Home
Premium
Archive
Video
Images
Forum
Atlas
Blogs
Jobs
Shop
RSS
Email Newsletters
You are in:
Home
Aviation History
1962
1962 - 1498.PDF
276 FLIGHT International, 23 August 1% BEAGLE M.218 Structure 1 Wing torsion box: I5in chord, 18 s.w.g. skin 2 Flanged light-alloy sheet spars 3 Six doublers, decreasing pro gressively to nil at mid-span 4 Pressed light-alloy ribs 5 Single Reduxcd stiffen er on top and bottom skins 6 Flap hinge brackets 7 Flap and aileron hinge brackets 8 Box-spar fork fittings 9 Light-alloy leading edge inboard of engines 10 Engine-bearer box-beams 11 Glass-fibre integrally-ribbed lead ing edge 12 Glass-fibre flap spar and skin: balsa insert at trailing edge 13 Glass-fibre flap-shrouds 14 Moulded clearance in flaps for retracted wheel 15 Single forged member carrying undercarriage fulcrum and actu ating linkage 16 Glass-fibre ailerons and shrouds 17 Centre-section box-spar 18 Rolled-angle longerons 19 22 s.w.g. light-alloy side-panels 20 Top decking and bottom skin of 22 s.w.g. light-alloy sheet with longitudinal swaged stiff en ers 21 Corrugated floor to baggage space: 12^ cu ft 22 Corrugated shelf for light per sonal baggage 23 Light-alloy frames 24 Glass-fibre single-piece mould ing: cabin roof, fuselage top- fairing, and dorsal fin 25 Double-skinned glass-fibre doors with moulded arm-rests 26 Glass-fibre roof structure with moulded wells for switch panels 27 Light-alloy windscreen frame, and instrument panel cross- member 28 Perspex centre-stiffener 29 Glass-fibre scuttle structure 30 Glass-fibre nose structure with integral side-boxes 31 Glass-fibre nose-cap hinged for access 32 Tubular keel truss from centre- section to front bulkhead 33 Tubular structure carrying nose- wheel 34 Four-point attachment of (33) to (32) 35 0.25in Perspex all round 36 Cross-member at front of rear seats 37 Forward limit of metal primary structure 38 Light-alloy fin spars riveted to back-face of frames 39 Light-alloy ribs 40 Glass-fibre fin skin 41 Foam-filled glass-fibre skin stiff ened 42 Glass-fibre fin leading-edge and top fairing 43 Rudder-spar: light-alloy tube of changing section 44 Glass-fibre rudderskin 45 Light-alloy all-moving tailplane, some spot-welding 46 Tailplane fulcrum 47 Light-alloy anti-balance tab 48 Glass-fibre taitplane tips 49 Tail bumper C Flying Controls CI Control wheels C2 Tee-type control column C3 Endless-chain aileron circuit C4 Aileron torque-tube driven by C3 CS Double sprockets for chain and cable aileron actuation C6 Aileron cables and push-rods C7 Tailplane cables attached to C8 C8 Tailplane mass-balance arm C9 Adjustable rudder-pedal units CIO Rudder cables CI I Tailplane tab control-wheel C11 Tab screw-jack CI3 Cable and chain to CI2 CI4 CI5 CI6 CI7 Flap lever Flap Servodyne Cables to port and starboard flaps Rudder mass-balance (proto type only) Electrics El E2 E3 E4 E5 E6 E7 E8 integrally d.c. generator on each engine Dagenite 12V, 24A-hr light weight battery moulded tray Navigation lights Beacon Switch panel: boost pumps, engine starting Rear-seat overhead light Cigar lighter on panel Fi»<-tro-hydraulic power pack F Fuel system Fl 35 Imp gal each wing Fuel tank end-ribs Polypenco plastics along rear spar Fillers, two each wn Fuel cocks „ Contents units (• in each wing Pump and filter t root P Powerplant PI 145 b.h.p. Ro"5"1 Spec 8 engines PI 72in Hartzcil t propellers F2 F3 F4 F5 F6
Sign up to
Flight Digital Magazine
Flight Print Magazine
Airline Business Magazine
E-newsletters
RSS
Events
