Cessna Aircraft Differences Training

Objectives / Content Summarize key differences among models in CAP’s Cessna aircraft fleet in terms of: General Description Aerodynamics (speeds) Weight Limitations Training Requirements General Differences Techniques

The information in this briefing is intended to serve as a departure point for discussion during CAP flight evaluations and transition training. It should not be interpreted or used as a substitute for the detailed information provided in the Airplane Flying Manual or Pilot’s Operating Handbook for each aircraft model.

General Description Aircraft Information C172P C182T C185F C206 Horsepower 180 230 300 Propeller Fixed Controllable Cowl Flaps No Yes Usable Fuel Capacity 40/50/62* 87 gal 84 gal Electrical 24 volts Landing Gear Tricycle Floats Seating Capacity 4 6 *Standard Tanks-40 Gal / Long Range-50 Gal / Integral-62 Gal

Aerodynamics KIAS C172P C182T C185F C206 Rotation 55 59 ?? 56 Vx 62 65 76 70 Vy 73 80 90 86 Va 105 110 (3100#) 117 (3350#) 125 (3600 #) Vno 127 140 149 Vne 158 175 184 180 Landing-Flaps Up 65-75 70-80 75-85 Landing-Flaps Down 60-70 Xwind (knots) 15 20

Weight Limitations Weights* C172P C182T C185F C206 Take Off 2550 3100 3350 3600 Landing 2950 Nominal Useful Load* 905 1052 1400 1300 * Useful load varies, check the aircraft’s weight and balance for specific data

Training Requirements Qualifications C172P C182T C185F C206 Form 5 Yes Yes* Complex Endorsement No High Performance Endorsement *CAPR 70-1 7.1.4. requires an initial CAPF 5 in each aircraft type (e.g., make/model, endorsement). Thereafter, a pilot my renew qualifications as follows: 7.1.4.1. High-Performance: Pass the CAPF 5 in a high performance airplane 7.1.4.2. Complex: Pass the CAPF 5 in a complex airplane or show evidence of equivalent check ride in military or under Part 61.58, 121.439/441, or 135.293/297 in the past 12 calendar months 7.1.4.3. G1000: Pass the CAPF 5 in a G1000-equipped airplane Equivalent Aircraft: C182QSP counts for C182 C206SP counts for C206. C205, and C207

General Differences – C182 Heavier on the controls then the C-172 Normally configured with flaps at 10 degrees for takeoff – – allows for easier rotation and less “pull” on the yoke Considerably more “nose heavy,” thus requiring more back pressure on landing. Takeoff weight can be higher than maximum landing weight Slips are to be avoided in varied C-172/185 models in certain flap settings – check the specific POH.

General Differences – C206 Heavier controls: Similar in feel to the 182, but larger, heavier Longer nose: Limited visibility over the nose in the landing flare Landing attitude: Far more tail low than 172 or 182 - tendency is to land nose wheel first or three point

General Differences – C206 Engine: Discuss engine operation for turbocharger Fuel injection vs carbureted engines Flaps: Flap interrupt switch How to open cargo door if flaps are extended Gear: Spring steel gear tends to vibrate in flight

Technique – C206 Taxi: Landing: Keep taxi speeds low in gusty/crosswinds Minimize use of flaps while taxiing Landing: Proper technique for recovery from a bounce is imperative Use caution on landing rollout to maintain directional control and avoid over braking Avoid configuration changes during the landing rollout: wait until clear of the runway before retracting wing flaps and opening cowl flaps to reduce distractions during a critical phase