Cessna T-207 Turbo Stationair 7 Airplane Flight Manual
CESSNA T-207 Turbo Stationair 7 · Flight Manual
Overview
This Airplane Flight Manual (AFM) is specifically designed for the Cessna T-207 Turbo Stationair 7. It serves as a comprehensive guide for pilots, providing essential information on the aircraft's operation, performance, and safety procedures. The manual includes detailed sections on aircraft specifications, operating limitations, emergency procedures, and performance data, ensuring that pilots have the necessary information to operate the aircraft safely and efficiently. The AFM is an essential resource for both new and experienced pilots flying the T-207, offering insights into the aircraft's systems and best practices for operation.
- Maximum takeoff weight: 3,600 lbs (1,633 kg)
- Maximum horsepower: 300 hp
- Stall speed in landing configuration: approximately 60 knots
- Takeoff distance at sea level: approximately 1,600 feet
- Climb rate: about 1,000 feet per minute
Document
Source
Originally published by www.aeroelectric.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Flight Manual
- Pages
- 8
- File size
- 671 KB
- Publisher
- www.aeroelectric.com
Common. Rarer than 2% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the CESSNA T-207 Turbo Stationair 7.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Aircraft Specifications
The Cessna T-207 Turbo Stationair 7 features a maximum takeoff weight of 3,600 lbs (1,633 kg) and a maximum payload capacity of 1,200 lbs (544 kg). The aircraft is powered by a Lycoming IO-540-U4A5 engine, providing a maximum horsepower of 300 hp. The stall speed in landing configuration is approximately 60 knots.
Operating Limitations
Pilots must adhere to specific operating limitations, including a maximum altitude of 20,000 feet and a maximum speed of 140 knots. The aircraft should not be flown in icing conditions, and pilots must ensure that fuel levels are maintained above 10 gallons in each tank during flight.
Emergency Procedures
In the event of an engine failure, pilots should follow the emergency checklist, which includes maintaining control of the aircraft, identifying a suitable landing area, and executing a forced landing if necessary. The manual provides detailed steps for handling various emergency scenarios.
Performance Data
The T-207 Turbo Stationair 7 has a takeoff distance of approximately 1,600 feet at sea level under standard conditions. The climb rate is about 1,000 feet per minute, and the aircraft has a range of approximately 600 nautical miles with full fuel.
Weight and Balance
Proper weight and balance calculations are crucial for safe flight operations. The manual includes charts and formulas to assist pilots in determining the center of gravity and ensuring that the aircraft is loaded within its limits.
Safety notes
- Do not operate in icing conditions.
- Ensure fuel levels are above 10 gallons in each tank during flight.
Full document text
CESSNA 206 TRAINING MANUAL History The Cessna aircraft company has a long and rich history. Founder Clyde Cessna built his first aeroplane in 1911, and taught himself to fly it! He went on to build a number of innovative aeroplanes, including several race and award winning designs. In 1934, Clyde's nephew, Dwane Wallace, fresh out of college, took over as head of the company. During the depression years Dwane acted as everything from floor sweeper to CEO, even personally flying company planes in air races (several of which he won!). Under Wallace's leadership, the Cessna Aircraft Company eventually became the most successful general aviation company of all time. The Cessna 205, 206, and 207, known variously as the Super Skywagon, Super Skylane and Stationair, are a family of single engine, general aviation aircraft with fixed landing gear and may be used in commercial air service or for personal use. The family was originally developed from the popular retractable-gear Cessna 210. The Cessna 206 family is best known for the powerful engine, rugged construction, large cabin and loading capacity. These features have made the aircraft popular 'bush planes' and for aerial work such as skydiving or photography, they can also be equipped with amphibious floats and skis. The combined total number of Cessna 205, 206 and 207 produced so far is over 8500. Cessna 205 In its initial form the 205 (originally 210-5) was essentially a fixed undercarriage derivative of the 210 Centurion. Although designated as a 1963 model the 205 was introduced to the Cessna lineup late in 1962, followed by the C205A in 1964. The C205 is powered by the same 260hp IO-470 engine as the 210B and featured an additional small cargo door on the left side of the fuselage. The 205 retained the early 210's engine cowling bulge, originally where the 210 stowed its nose wheel on retraction (the space where the nose wheel would have retracted was used for radio equipment in the 205). This distinctive cowling was made more streamlined on the later Cessna 206. There were only 577 Cessna 205's produced, before being replaced by the popular Cessna 206. by D. Bruckert & O. Roud © 2010 Page 11 CESSNA 206 TRAINING MANUAL Cessna 206 The six-seat Cessna 206 was introduced as a 1964 model and was built until 1986, when Cessna halted production of its single-engine product. It was then re-introduced in 1998 and remains in production at the time of publication. The total number of Cessna 206's produced is now over 6500. Unlike the C210, from which it is based, the C206 has had relatively few changes over the years. The main changes include the engine (1964 and 1998), electrical system (1965 and 1973) and maximum weight (1967). Cessna U206 The original 1964 model was the U206, powered by a 285hp Continental IO- 520-A. The "U" designation indicated "utility" and this model was equipped with a pilot side door and two opposing rear doors, permitting more convenient access to the back two rows of seats, and permitting easy loading of over-sized cargo. The TU206 offered a turbocharged version of the U206, powered by the Continental TSIO-520-C engine producing 285hp. In 1967 the turbo TU206 was powered by a TSIO-520-F providing 300hp. The additional 15hp was available at a higher rpm, but was limited to 5 minutes for takeoff and produced a significant noise penalty. From 1964 to 1969 the U206 was known as the "Super Skywagon". From 1970 it was named the "Stationair", a contraction of "Station Wagon of the Air", which is a good description of the aircraft's intended role. In 1977 the U206 had its engine upgraded to a Continental IO-520-F of 300 hp (continuous rating, obtained at a more reasonable rpm speed than the previous IO-520-F) and the TU206 engine was changed to the TSIO-520-M producing 310hp. Production of all versions of the U206 was halted in 1986 when Cessna stopped manufacturing all piston engine aircraft. A total of 5208 U206's had been produced. Cessna P206 1965 saw the P206 added to the line. In this case the "P" stood for "people", as the P206 had passenger doors on both sides, similar to the Cessna 210 from which it originated. The P206 was produced from 1965 to 1970 and was powered by a Continental IO-520-A of 285hp. There was a turbocharged model designated TP206 which was powered by a Continental TSIO-520-A also of 285hp. by D. Bruckert & O. Roud © 2010 Page 12 CESSNA 206 TRAINING MANUAL 647 P206's were produced under the name "Super Skylane" which incorrectly made it sound like a version of the Cessna 182. Cessna 206H After a production break of twelve years, Cessna started manufacturing a new version of the 206 in 1998, with the introduction of the 206H. The "H" model is generally similar to the previous U206 configuration, with a pilot entry door and double rear doors for access to the middle and back seats. The C206H is marketed under the name "Stationair", and Cessna aptly portrays it as the "Sport Utility Vehicle of the air". The 206H is powered by a Lycoming IO-540-AC1A powerplant producing 300hp. The turbocharged T206H is powered by a Lycoming TSIO-540-AJ1A engine of 310hp. Both the 206H and the T206H remain in production in 2008. By the end of 2004 Cessna had produced 221 206H's and 505 T206H's, for a total production of 726 "H" models. Cessna 207 The Model 207 was a seven and later eight seat development of the 206, achieved by stretching the design further to allow space for more seats. The nose section was extended 18" by adding a constant-section nose baggage compartment between the passenger compartment and the engine firewall; the aft section was extended by 44" by inserting a constant-area section in the fuselage area just aft of the aft wing attach point. Thus the propeller's ground clearance was unaffected by the change (the nose wheel had moved forward the same distance as the propeller), but the tail moved aft relative to the main wheel position, which made landing (without striking the tail
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skid on the runway) a greater challenge. The move gave that aircraft a larger turning radius, since the distance between main wheels and nose wheel increased by 18 inches but the nose wheel's maximum allowed deflection was not increased. The 207 was introduced as a 1969 model featuring a Continental IO-520-F engine of 300hp. A turbocharged version was equipped with a TSIO-520-G of the same output. At the beginning of production the model was called a Cessna 207 "Skywagon", but in 1977 the name was changed to "Stationair 7". 1977 also saw a change in engine on the turbocharged version to a Continental TSIO- 520-M producing 310hp – the same engine used in the TU206 of the same vintage. - by D. Bruckert & O. Roud © 2010 Page 13 CESSNA 206 TRAINING MANUAL The 207 added a seat in 1980 and was then known as the "Stationair 8". Production of the 207 was completed in 1984, just two years before U206 production halted. A total of 788 Cessna 207's were manufactured. The Cessna Model 207 has been popular with air taxi companies, particularly on short runs where its full seating capacity could be used. Very few of these aircraft have seen private use. Models Differences Table A brief outline of the models by year with major changes is outlined in the table below. During practical training, reference should be made to the flight manual of the aeroplane you will be flying to ensure that the limitations applicable for that aeroplane are adhered to. Likewise when flying different models it should always be remembered that MAUW, flap limitations, engine limitations and speeds may vary between models and with modifications. Before flying different models, particularly if maximum performance is required, the POH of the aircraft you are flying should be reviewed to verify differences. TYPE NAME YEAR MODEL C205 C205A 1963 205 0001-0480 1964 205 0481-0577 1964 206 0001-0275 C206 Super Skywagon U206 Super Skywagon 1965 206 0276-0437 (Utility Cargo Door) P206 Super Skywagon 1965 (Passenger Door) P206 0001-0160 P206 Super Skylane 1965 MAJOR DIFFERENCES 3300lbs maximum takeoff weight, IO470 engine; essentially a C210B with fixed gear and electric flap Engine changed to IO520 First cargo door version, 14V Alternator replaces Generator First C206 to come out with 6 seats as a standard (not optional) fitting by D. Bruckert & O. Roud © 2010 Page 14 CESSNA 206 TRAINING MANUAL TYPE NAME U206A Super Skywagon (Utility Cargo Door) U206B U206C TU206A Turbo-System Super YEAR MODEL MAJOR DIFFERENCES weight increased to 3600lbs 1966 U206 0438-0656 Maximum takeoff 1967 U206 0657-0914 1968 U206 0915 1966 U206 0438-0656 1967 U206 0657-0914 1968 U206 0915 TU206B Skywagon (Utility Cargo Door) TU206 P206A Super Skylane 1966 P206 0161-0306 TP206A Turbo-System Super 1966 P206 0161-0306 Skylane P206A Super Skylane 1966 P206 0161-0306 P206B P206C 1967 P206 0307-0419 1968 P206-0420 TP206A Turbo-System Super TP206B Skylane 1966 P206 0161-0306 1967 P206 0307-0419 TP206C TU206D Super Skywagon U206D Turbo-System Super Skywagon P206D Super Skylane TP206D Turbo-System Super Skylane U206E Super Skywagon TU206E Turbo-System Super Skywagon P206E Super Skylane 1968 P206-0420 1969 U206-1235 U206-1444 1969 P206-0520 P206-0603 1970 U20601445- U20601587 1970 1970 P20600604-647 TP206E Turbo-System Super Skylane 1970 P20600604-647 U206E Stationair 1971 U20601588-1700 Turbo Stationair U206F Stationair 1972 U20601701-1874 Flap toggle switch Turbo Stationair changed to pre- select lever by D. Bruckert & O. Roud © 2010 1973 U20601875-2199 12V battery changed to 24V Page 15 CESSNA 206 TRAINING MANUAL TYPE NAME YEAR MODEL MAJOR DIFFERENCES U206F Stationair 1974 U20602200-2579 Turbo Stationair U206G Stationair Turbo Stationair Stationair II Turbo Stationair II U206G Stationair 6 Turbo Stationair 6 Stationair 6 II Turbo Stationair 6 II U206G Stationair Turbo Stationair Stationair With Value Group A Turbo Stationair II 1975- U20602580-3021 76 1977 U20603522-4074 1978 U20604075-4649 In 1979 the 1979 U20604650-5309 bladder tanks 1980 U20605310-5919 were changed to 1981 U20605920-6439 integral wet wing 1982 U20606440-6699 tanks. 1983 U20606700-6788 1984 U20606789-6846 1985 U20606847-6920 1986 U20606921-7020 With Value Group A 207 Skywagon 207 1969 20700001-0414 1977 T207 Turbo Skywagon 207 1969- 20700415-0562 1977 207 Stationair 7 1978-20700563-0788 Turbo Stationair 7 1979 Stationair 7 II Turbo Stationair 7 II C207 Stationair 8 1980- New model C207 introduced, 3800lbs Gross weight, 300 or 310hp IO520 series engine Wing span 432- 439", length 381" 7 or 8 place seating Turbo Stationair 8 1984 Stationair 8 II 206H Turbo Stationair 8 II Stationair 1998 20608001 on On T206H Stationair TC 1998 T20608001 on On Lycoming IO/TIO- 540 engine, annunciator systems. From 2005, G1000 glass avionics optional, from 2007 standard. by D. Bruckert & O. Roud © 2010 Page 16 CESSNA 206 TRAINING MANUAL Modifications Common modifications include the famous cargo pod, floats, most of the common STOL kits (eg. Robertson and Sportsman), additional fuel tanks and various engine modifications including a turbine version. Details on common modifications available are outlined in the table on the following page. At present there is no 'RG' (retractable gear) version of the C206, as offered with the 100 series Cessnas This is presumably because of the similarity and success of the retractable C210 on which the C206 was based. Illustration 1b C206 with Cargo Pod by D. Bruckert & O. Roud © 2010 STS NG SERVICE Illustration 1c C206 on Floats Page 17 CESSNA 206 TRAINING MANUAL Common Modification's Table TYPE NAME and MANUFACTURER Any Cargo Pod Any Skis / Floats Any Soloy Any Engine Conversion, Bonaire Any Engine Conversion, Atlantic Aero Any Low Fuel Warning System, DIFFERENCES and FEATURES (Various) Extra cargo/luggage room, small speed penalty (Various) Turbine Engine Installation, 418 SHP Allison C20S engine Conversion to IO550 engine, 300hp maximum continuous Conversion to IO550 engine, 300hp maximum continuous Warns when fuel remaining is less than approximately 7USG O & N Aircraft Modifications F, G, H Engine Conversion, Thielert Any 300 or 310hp V8 diesel engine installation Fuel Cap Monarch Air Umbrella style fuel caps which fix problems with leaks, predominantly occurring in older flush mounted caps, (available for most Cessna types) Any Wing Tip Tanks, Flint Aero Any Horton STOL Any Robertson STOL Two auxiliary tip tanks of 16.5USG in each, used with an electrical transfer pump to each main tank. Higher MTOW (3800lbs) is permitted if tanks are half full. Wing length is also increased by 26 inches. Tip and wing surface modifications to permit lower stall speed, take-off and landing speeds and distances Increased lift, more speed, added stability, and lower stall speed, take-off and landing speeds and distances. ? Note: The table above is included for interest and awareness, as there are many C206s operating with the modifications installed, some modifications may no longer be available for installation. by D. Bruckert & O. Roud © 2010 Page 18
What's in the CESSNA T-207 Turbo Stationair 7 TCDS
A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.
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