Cessna 172 Skyhawk — Supplemental Type Certificate

This document is an exam for pilots training on the Cessna 172 aircraft, specifically focusing on the M, N, and P models. It includes a series of questions that cover general knowledge, limitations, normal procedures, performance, and airplane systems. The exam is designed to test the understanding of key operational aspects of the Cessna 172, including fuel capacity, weight limits, flap settings, and emergency procedures. Pilots are expected to refer to the appropriate manuals and supplemental type certificates to answer the questions accurately.

• Cessna 172P can hold 43 gallons of fuel with 40 gallons usable; long-range tanks hold 54 gallons with 50 gallons usable.
• Maximum takeoff weight for C-172P is 2550 lbs; maximum landing weight is 2100 lbs.
• Maximum flap extended speed (Vfe) for C-172P is 110 KIAS; never exceed speed (Vne) is 158 KIAS.
• Best glide speed for C-172P is 65 knots; stall warning horn activates 5-10 knots above stall.
• The C-172P has 2 spark plugs per cylinder and 2 engine-driven magnetos.