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Aviation History
1943
1943 - 0347.PDF
Designers To relieve the airframe of unnecessary shock when landing and taxi-ing, for greatly improved directional stability, and for absolute freedom from shimmy. fsigned f atic load of • %000 lbs. SPECIFY TAIL WHEEL STRUTS BRITISH LANDING GEARS LIMITED In association with THE BRITISH SYPHON CO. LTD. MILNER SQUARE, LONDON, N.I Telephone: NORTH 2431 wneers m x articulation
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