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AIRFRAME
The basic airframe, except for a tubular steel engine mount, steel landing gear struts, and other miscellaneous steel parts, is of aluminum alloy construction. The extremities - the wing tips, the cowling, the tail surfaces - are of fiberglass or ABS thermoplastic. Aerobatics are prohibited in this airplane since the structure is not designed for aerobatic loads.
The semi-tapered wings have a laminar flow type NACA 652-415 airfoil. The wings are attached to each side of the fuselage by insertion of the butt ends of the respective main spars into a spar box carry-through which is an integral part of the fuselage structure, providing, in effect, a continuous main spar with splices at each side of the fuselage. There are also fore and aft attachments at the rear spar and at an auxiliary front spar.
👉 PIPER ARCHER III PA 28-181 HANDBOOK
👉 STARTING WITH EXTERNAL POWER
👉 WARM-UP
👉 TAXIING
👉 TAKEOFF
👉 SHORT FIELD, OBSTACLE CLEARANCE
👉 CLIMB
👉 CRUISING
👉 DESCENT
👉 MOORING
👉 ENGINE
👉 POWER PLANT INSTRUMENT MARKINGS
👉 AIRSPEEDS FOR SAFE OPERATION
👉 AIRFRAME
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