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Aviation History
1985
1985 - 0026.PDF
cfl^l mruh 1 Upward lifting one-piece Kevlar reinforced avionics bay cover. 2 Weather, radar and glideslope aerials 3 Avionics bay and battery stowage (two 24amp/hr ni cad batteries) 4 Emergency oxygen stowage 5 Avionics cooling air intake 6 Electrically heated pilot head (both sides) 7 Forward retracting, fully steering, hydraulically actuated nose undercarriage (16in X 4.4in tyres) all doors made from Kevlar 8 Forward pressure bulkhead 9 Electrically driven windscreen wipers 10 Electrically heated birdproof windscreen (warm air demisted) 11 Direct vision DV panel 12 Fully adjustable crew-seats 13 Fuliy shrouded flight and engine instrument panel 14 Overhead electrical panel (engine start, systems control) 15 Centre console (engine controls, autopilot) 18 Control columns with trim switches and stick-shaker fitted 17 Rudder pedals with toe-brakes 18 Overhead clearview panels 19 Sliding door to flightdeck 20 Folding plug-type integral door and steps (48in X 26in) 21 Seven-passenger seat configuration shown (max nine seats): overall cabin length 22ft 6in between pressure bulkheads 22 Galley and refreshment unit 23 Foldaway tables 24 Sunken aisle 25 Cabin telephone 26 Cabin roof heightened by blending in new roof structure to existing Westwind 2 cross section 27 Continuous extruded longeron 28 Separate window frames 29 Emergency overwing exits (19inx27in) both sides 30 Chemically etched fuselage skin panels 31 Toilet and cloakroom vanity unit on rear bulkhead 32 First-aid box, axe, and fire extinguisher stowage 33 Rear pressure bulkhead and flying control seals 34 Fuselagefueltank(upperandlower), total fuel capacity 392 Imp gal 35 Gravity filler, pressure refuel/defuel lower down on right side 36 Long-range fuel tanks, mounted on bulkhead (crashproof), 85 Imp gal approx 37 Reinforced rearfloorstructure over undercarriage bay 38 External door to heated baggage compartment (55ft3) 39 Engine fire extinguisher (see detail) 40 Access to air conditioning and hydraulic bay (see detail) 41 Carry through frontand rear engine mounting beam and engine pylons 42 Glassfibre moulded ram-air inlet 43 Three-spar fin torsion box covered with chemically etched skin panels 44 Fin/fuselage multi lug attachment fittings 45 Detachable leading edge 46 Glassfibre fin tip and fuselage tail fairing 47 Rear fuselage venting panels (both sides) 48 Rudder and geared trim tab (22* either side) 49 Rudder bellcrank and torque tube 50 Two-spar carry through variable incidence tailplane 51 Tailplane actuator (triple electric motors+1°-12*) 52 Tailplane pivot point 53 Elevator and geared tab 54 Elevator bellcrank and torque tube (adjustable stops+22.5"-12') 55 Chemically etched, extruded stringer stiffened tailplane skin panels, provision for "logo lights" on upper surface 56 Detachable glassfibre tips 24 FLIGHT International, 5 January 1985
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