SPECIFICATION AND DESCRIPTION STATIONAIR TC December 2015 Revision B Units T206-9215 to TBD CESSNA STATIONAIR TC SPECIFICATION AND DESCRIPTION UNITS T206-9215 TO TBD DECEMBER 2015 REVISION B Cessna Aircraft Company P.O. Box 7706 Wichita, Kansas 67277-7706 CESSNA STATIONAIR TC INTRODUCTION This document is published for the purpose of provid- This document supersedes all previous Specification and ing general information for the evaluation of design, per- Description documents and describes only the Turbo Sta- formance and equipment of the Cessna Turbo Stationair. tionair Model T206H, its powerplant and equipment. Also Should more information be required, please contact: included are the warranties applicable to the Turbo Station- air Model T206H aircraft, the Textron Lycoming TIO-540- AJ1A engine, the McCauley propeller and the OEM-installed Cessna Aircraft Company Garmin avionics. In the event of any conflict or discrepancy between this document and the basic purchase agreement, Single Engine Piston Aircraft the basic purchase agreement language shall govern. Due to the time span between the date of this Specification and 2625 S. Hoover Rd. Description and the scheduled delivery date of the aircraft, Wichita, Kansas 67215 Seller reserves the right to revise the “Specification” when- ever occasioned by product improvements, government 1-800-4-CESSNA regulations or other good cause. www.se.cessna.com December 2015, Revision B 1 CESSNA STATIONAIR TC TABLE OF CONTENTS CESSNA STATIONAIR TC SPECIFICATION AND DESCRIPTION SECTION PAGE 1. General Description ........................................................................................................................................................... 3 1.1 Certification.......................................................................................................................................................... 3 1.2 Approximate Dimensions ................................................................................................................................. 6 1.3 Design Weights and Capacities ...................................................................................................................... 7 2. Performance .......................................................................................................................................................................... 8 3. Powerplant & Accessories ................................................................................................................................................. 8 4. Stationair Equipment List ................................................................................................................................................... 9 5. Instrument Panel .................................................................................................................................................................. 10 6. Electrical Power .................................................................................................................................................................... 11 7. Engine Indicating System .................................................................................................................................................. 11 8. Environmental ....................................................................................................................................................................... 11 9. Exterior .................................................................................................................................................................................... 12 10. Exterior Lights ....................................................................................................................................................................... 12 11. Flight Controls ....................................................................................................................................................................... 12 12. Fuel System ........................................................................................................................................................................... 12 13. Interior .................................................................................................................................................................................... 13 14. Interior Lighting .................................................................................................................................................................... 13 15. Exterior ................................................................................................................................................................................... 14 16. Training ................................................................................................................................................................................... 14 17. Limited Warranties .............................................................................................................................................................. 14 17.1 Cessna’s Limited Warranty - Single Engine Piston Aircraft ...................................................................... 14 17.2 Aircraft Paint and Graphics - Single Engine Piston Aircraft ..................................................................... 15 17.3 Textron Lycoming Warranty (Limited) New Reciprocating Aircraft Engines ......................................... 15 17.4 McCauley Propeller Systems Standard Limited Warranty ........................................................................ 17 17.5 Garmin Avionics Installed in Single Engine Aircraft ................................................................................... 18 FIGURE I — CESSNA STATIONAIR EXTERIOR DIMENSIONS ................................................................................................. 4 FIGURE II — CESSNA STATIONAIR INTERIOR DIMENSIONS ................................................................................................. 5 FIGURE III — CESSNA STATIONAIR INSTRUMENT PANEL ..................................................................................................... 10 2 December 2015, Revision B CESSNA STATIONAIR TC 1. GENERAL DESCRIPTION 1. GENERAL DESCRIPTION All information herein applies to the Turbo Stationair (Model T206H). The Stationair is an all-metal, six-place, high-wing, fixed gear, single-engine piston aircraft de- signed for general utility purposes. 1.1 CERTIFICATION The Model 206H is certified to the requirements of U.S. FAA Federal Aviation Regulation Part 23 through amend- ment 23-6, including day, night, VFR and IFR. December 2015, Revision B 3 CESSNA STATIONAIR TC 1. GENERAL DESCRIPTION (CONTINUED) 36 ft 0 in 8 ft 1 in 13 ft 0 in 28 ft 3 in 9 ft 3.5 in FIGURE I — CESSNA STATIONAIR EXTERIOR DIMENSIONS 4 December 2015, Revision B CESSNA STATIONAIR TC 1. GENERAL DESCRIPTION (CONTINUED) Baggage Shelf Rear Wall of Cabin Firewall 24.00 36.00 49.50 44.00 45.50 42.00 21.00 35.00 24.00 47.00 65.00 Forward Doorpost Tiedown Rings Bulkhead (10 Standard) Face of Instrument Panel *14.00 *36.00 *40.00 *34.00 **40.00 **43.50 **42.00 *28.50 *29.00 *35.50 **30.00 **34.50 *38.50 *28.50 *37.50 **42.50 **44.00 **36.00 **42.00 *14.00 Firewall Code *Cabin **Lower Window Line FIGURE II — CESSNA STATIONAIR INTERIOR DIMENSIONS December 2015, Revision B 5 CESSNA STATIONAIR TC 1. GENERAL DESCRIPTION (CONTINUED) 1.2 APPROXIMATE DIMENSIONS Overall Height ........................................................................................................................................................................ 9 ft 3.5 in (2.83 m) Overall Length .......................................................................................................................................................................... 28 ft 3 in (8.61 m) WING Span (overall) ................................................................................................................................................................................. 36 ft (10.97 m) Area ................................................................................................................................................................................................. 174 ft2 (16.2 m2) CABIN INTERIOR Height (maximum) ....................................................................................................................................................................... 49.5 in (1.26 m) Width (trim to trim) ............................................................................................................................................................................ 44 in (1.12 m) Length (firewall to aft baggage bulkhead) ............................................................................................................................. 145 in (3.68 m) CABIN DOOR Height (front) ..................................................................................................................................................................................... 41 in (1.04 m) Height (rear) ..................................................................................................................................................................................... 39 in (1.00 m) Width (top) ...................................................................................................................................................................................