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Aviation History
1950
1950 - 0574.PDF
376 FLIGHT Engines : Four Bristol Hercules 7*1 of 2,010 Span 162ft Length 99ft 2in Heifht ... 33ft Wing area 2,916 sq ft Aspect ratio 9 Dihedral 54min 31 sec Incidence S dec 30 min T/C ratio, root 21.6 per cent tip ... 12.6 per cent Tailplane span (projected) ... ... ... 42ft 1.7in T/p and elevator area, gross (projected) ... 527 sq ft Fin and rudder area, gross 388 sq ft Undercarriage track ... 36ft C.G. range, per cent of S.M.C., front limit ... 17 aft limit 28 neutral point 40 Estimated Performance at I OS ,0001b A.U.W. Max all out speed 225 m.p.h. T.A.S. Max cont. cruise 216 m.p.h. T.A.S. Recomm. econ. cruise ... ... 168 m.p.h. T.A.S. Recomm. cruise, 2 engines dead ... ... 139 m.p.h. Climb speed and rate 120 m.p.h. T.A.S. at S.L. = . . .. . . 620ft/min ' The very size of the Universal Freighter makes it difficult to show the structural detail; nevertheless, in this special cut-away drawing, our artist has succeeded in por- tray i ngnotonlythe essential structu ral form of the aircraft, but also a very considerable amount of the airframe detail design. h.p. each, driving 14ft diameter Rotol airscrews 83 m.p.h. 100 m.p.h. Stalling speed, flaps down flaps up UNIVERSAL FREIGHT Service ceiling Take-off distance to clear 50ft, zero windDistance to stop from clearing 50ft, zero wind, 19,400ft 970 yd braking airscrews Payload 31,6501b 28.7001b 21.8001b 12,9001b Range 700 miles 1,000 miles 1.600 miles 2,465 miles Speed 169 m.p.h. 171 m.p.h. 172 m.p.h. 173 m.p.h. 700 yd Altitude 8.000ft 8,000ft 8.000ft 8,000ft Loading Data All-up weight 105,0001b Max landing weight 100,0001b Percentage structure weight ' 37.25 Wing loading 36.1 Ib/sq ft Power loading (T-O) 13.32 Ib/h.p. Passenger capacity ... ... 18 seats ,, cabin area and volume 237 sq ft and 910 cu ft Toilets, etc 77 sq ft and 410 cu ft Baggage and mail ... 80 sq ft and 540 cu ft Flight-deck 180 sq ft and 850 cu ft Freight ... 360 sq ft and 3,600 cu ft POUT WING DE-ICING COMBUSTION HEATERS |2) 1. TWIN INTAKES 2. COMBUSTION EXHAUST (li OTHER ABOVE WING 3 WING DUCT FREE EXIT COWLING 6 AIR FROM CUINDE. 7. AIR FROM CVUN AUTOPILOT SERVO MOTORS CARBURETTOR AIR TRUNK FIREPROOF BULKHEAC CABIN HEATER (PORT) 4. INTAKE 5. COMBUSTION EXHAUST CONTROL RUNS 10. AILERON 11. ELEVATOR 12. RUDDER TRANSPORT JOINT RADIO OPERATOR i NOSEWHEEL STEERING I. SELECTOR CABLES ?. JACK STARTER BATTERY SOCKET ENTRANCE TO WING CRAWL -WAY (STARB.Dl »r.4>-.<.->-'---.-.::. •••:--.. 7 PRESSURE WELLING POINTS (PORT) TRANSPORT JOINTDE- fUELUNGPOINT
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