FlightGlobal.com
Home
Premium
Archive
Video
Images
Forum
Atlas
Blogs
Jobs
Shop
RSS
Email Newsletters
You are in:
Home
Aviation History
1934
1934 - 1473.PDF
1 ! r BRI T a oat y ft Maker and Type. Airspeed Courier Airspeed, Envoy Armstrong, Atalanta ... Avro, 642 Avro, 652 Avro, Commodore Blackburn, Feeder Boulton* Paul, P.64 ... Boulton & Paul, Feeder British Klemm, Eagle ... De Havilland, 86 De Havilland, 89 Airplane DevelopmentCorp., Vultee V.I. Douglas, D.C. I Lockheed, Alcor Lockheed, Altair 8E ... Lockheed, Electra Lockheed, Orion 9D ... Lockheed, Vega Northrop, Delta Northrop. Gamma Northrop, Victoria Dornter, Do. F Fokker, F. XX Heinkel, H.E.70A Pander, Postjager Col. 1 and 2 Power Plant 240 Lynx IVc. 2 x Wolseley A.R.9 11 203 at 2,420 r.p.m 4 x 400 Jaguar 2 x Jaguar VID460 at 2,000 r.p.m. 2 x Cheetah277 at 2,100 r.p.m. 215 Lynx 2 X Rapier VI805 at 3,500 at 10,000 ft. 2 X Pegasus I. M2 2 x Jaguar VIA450 h.p. 186/200 Gipsy Six 4 X Gipsv Six205 at 2,350 r.p.m 2 x Gipsv Six205 at 2,350 r.p.m. Cvclone F.2700 at'1,900 r.p.m. 2 x Cyclone710 at 1,950 at 7,000 ft. 2 x Menasco Buccaneer230 h.p. Wasp S.I.D.I.550 at 2,200 at 5,000 ft. 2 x Wasp Junior420 at 2,200 at 5,000 ft. Wasp S.I.D.I.550 at 2,200 at 5,000 it. Wasp S.C.I.450 at 2,100 at 6,000 ft. Cyclone SR.1820.F.3 Approx. 700 h.p. Cvclone SR.1820.F.3710 at 7,700 ft. Wasp S.I.D.I.525 at 5,000 ft. 2 x Siemens Jupiter550 h.p. 3 x Cyclone R.1820.F.3712 h.p. B.M.W. VI. 630 h.p. 3 x Whirlwind420 h.p. 3 HU 2—i^lLrUi Truss. PI nM n aM Q IXI-CXI f\LOW WING CANTILEVER MONO l>dk»ff><i f 1 DITTO m m o m o R M O Q R A m1 1 DITTO DITTO MI0-WINO SEMI-CANTILEVER m _ Fl•* 4 Weight lbs. Gross. 3,900 3,790 4,900 23,000 11,790 6,598 3,500 3.320 8,600 10,500 9,400 2,400 9,200 5,000 7,250 18,000 4,710 5,800 9,000 5,800 4,750 7,000 7,000 7,000 17.600 19,841) 7.380 ! 12,100 5 Tare. 2,210 2,100 3,077 13,600 7,450 4,192 2,225 4,740 6,125 6,000 1,510 5,5205,950 2,8513,102 4,275 11,87512,080 2,665 3,297 5,455 3,640 2,725 4,100 4,000 4,100 10,500 13,220 5.1905,410 6.655 6 IVltlJ Basic Load Wing Ib./sq.tt 15.6 15.15 14.55 17.7 16.2 16.1 11.410.82 18.3 13.0 13.1 12.0 14.3515.30 14.9 20.0 19.2 16.7 19.72 19.64 19.72 17.02 19.3 19.3 19.3 14.75 19.25 18.2 25.0 7 Data. ings. Power,b./h.p. 18.25 15.8 12.18 12.2 12.04 12.2410.8 15.45 12.3 8.4 9.6 11.7 11.2 12.2 10.2 12.7 10.2 10.55 10.71 10.55 10.55 9.86 9.86 13.6 16.1 9.25 11.7011.53 9.6 8 run ^i Spans. Upper,tt in. 47 0 52 4 90 0 71 3 56 6 37 4 58 4 54 0 54 0 39 3 64 6 48 0 48 0 85 0 42 0 42 9 55 0 42 9 41 0 48 0 48 0 48 0 91 10 90 2 48 6 54 5 9 Lower.tt in. - — — — 37 4 — 54 0 54 0 — 64 6 48 0 — — — — — — — — — — — — — — 10 Vll^ AE 8peeds. High. Speed 162 170 165 160 175 130 196 195 175 170 170 165 225 210 183 230 221 225 195 221 215 200 155 202 234 224 11 Heighttt. S.L. S.L. 4,000 S.L. S.L. S.L. 10,000 5,000 S.L. S.L. S.L. 1,000 3,000 7,000 S.L. 5,000 5,000 5,000 6,000 7,700 7,700 5,000 S.L. 5900 S.L.7,200 S.L. 12 M.P.H. Low. Land- ing. 48 55 — 56 64 50 63 60 62 48 72 66» — 65 61 57 63 63 63 60 58 63 58 62 59 59 60 13 Stall- ing. 55 63 — 64 — — — — — — — 63 — — — — — — — — — — — — — — 14 Weigh t Ratio . 1.77 1.59 1.69 1.58 1.58 1.571.49 1.82 1.72 1.57 1.59 1.671.55 1.751.61 1.70 1.521.49 1.77 1.76 1.65 1.59 1.74 1.71 1.75 1.71 1.68 1.50 1.421.36 1.82 15 Figures of Speed Range Ratio. S.38 3.09 — 2.86 2.74 2.60 3.11 3.25 2.82 3.54 2.3fi 2.57 2.62 3.46 3.44 3.21 3.65 3.51 3.57 3.25 3.81 3.41 3.45 2.50 3.43 3.97 3.73 16 Win g Power . 0.96 1.20 1.45 1.34 1.32 1.49 0.74 0.70 1.49 1.66 1.36 1.03 1.28 1.37 1.22 1.96 1.51 1.64 1.87 1.83 1.87 1.62 1.95 1.95 1.42 0.92 2.08 1.56 1.58 2.60 17 Merit Spa n Loading . .07 .5« .56 .35 .43 .48 .40 .42 .39 .28 .31 .64 .45 .46 .32 .40 .37 .32 .34 .32 .35 .33 .33 .33 AH .41 .32 24 18 Hig h 8pee d Fig . 30.1 27.8 18.7 21.4 20.8 27.6 24.4 20.2 21.3 25.4 26.2 26.8 32.9 26.3 24.4 25.0 36.134.3 33.8 32.1 25.4 24.1 38.136.2 34.6 32.9 35.7 33.9 26.0 24.7 29.8 27.4 26.0 33.0 31.4 27.5 25.0 25.3 24.0 55.8 44.3 29.1 27.9 19 * 1.32 0.94 — 1.01 0.77 0.89 0.85 0.90 0.76 0.67 1.02 0.65 0.69 0.74 0.92 1.01 1.00 0.97 0.97 0.97 0.93 1.12 0.95 1.12 0.75 1.12 1.03 1.36 20 Source of Basic Data and Speeds. Jane's 1933 Aeroplane Jane's 1933 Flight 5.4.34 Flight 7.6.34 Flight 31.5.34 Flight 7.6.34 Flight 6.4.33 Flight 7.6.34 Aeroplane25.7.34 Flight 22.2.34 Flight 26.4.34 Flight 22.3.34 Flight 1.3.34 Flight 6.7.34 Flight 16.8.34 Aeroplane11.4.34 Flight 16.8.34 Flight 16.8.34 Flight 8.2.34 Jane's 1933 Flight 8.2.S4 Flight 22.2.34 Jane's 1933 Jane's 1933 Jane's 1933 21 Remarks. W FWing Flap* V.P.A. -Variable PitchAirscrews. — • — — — — — — — — — •Corrected byCapt. Broad. — R.P. V.P.A. R.P.—W.F. 4V.P.A. R.P. V.P.A. R.P.—W.F. &V.P.A. R.P.- -W.F. &V.P.A. R.P.—W.F. & V.P.A. R.P. V.P.A. R.P.—W.F. & V.P.A. R.P.—W.F. &V.P.A. R.P —W.F. &V.P.A. N.P. R.P. W.F W.F R.P. W.F. 22 I M ts w I-H > H w o c rE
Sign up to
Flight Digital Magazine
Flight Print Magazine
Airline Business Magazine
E-newsletters
RSS
Events
