FLINT AERO, INC.1942 Joe Crosson Dr.EI Cajon, CA 92020

FAP.APPROVEDSUPPLEMENTAL AI'~PLANE FLIGHT MANUAL #1

CESSNA MODELS U~~06F,U206G, TU206F, TU206G

Thismanual provides information pertaining to the operation of the aircraft when Flint Aero wing tip transfer fueltanks are installed in accordance with STC SA436EWE.

For limitations, procedures, and performance information not contained in this manual, refer to the FAA-approvedmarkings, placards and manuals.

I. LIMITATIONS AND PLACARDS:

Limitations:

(a) Ailiandplane and floatplane versions, the TU206G amphibian, the U206F skiplane and the TU206Fskiplane are cleared as follows: Maximum takeoff gross weight 3,800 lb. Forward and aft limits of CGand moment diagrams are extended with straiqnt lines to 3800 lb.

Maximum landing gross weight is unchanged.

Placards:

Placards shall be provided as follows in the location given:

(b) On instrument panel in clear view of the Pilot:"Total wing tip transfer tank fuel 30 U.S. gal. (29.8 U.S. gal. usable). Transfer fuel during level flight.Transfer fuel when each main tank is 15 to :20gallons below full and when main tank is not supplyingengine. Wing tip fuel transfer pump switch must be off during takeoff, landing, filling, and when empty.Monitor main fuel tank gauge while transferring wing tip fuel to prevent over filling."

(c) Adjacent to the airspeed indicator:"Reduce VNE 5 mph per 1,000 ft. above 18,000 ft." (Turbocharged models only.)

(d) Adjacent to each wing tip tank filler:"'15 U.S. Gallons (14.9 U.S. Gallons usable) ** minimum grade aviation gasoline." Insert for the doubleasterisk ** Grade number on placards for main tanks.

PROCEDURES: CAUTION: If the flight plan requires wing tip fuel to complete the flight, test both wing tipfuel tank transfer pumps early in the flight to assure fuel transfer.

PERFORMANCE: Stall speeds for the airplane modified with the wing tip tanks at 3800 LBGW are thesame as those of the unmodified airplane at 3600 LBGW. Takeoff distances for the modified airplane at3800 LBGW should be increased 10% over the distances in the Cessna AFM for a 3600 LBGW airplane.Rate of climb for the modified airplane at 3HOO LBGW is the same as that of the unmodified airplane at3600 LBGW.

FAA APPROVED ~~....L4J=:~====::±'-.4?;'~~:..·=~x:A:::c::='/:::' =====Manager, FI~ Testl8ranch, ANM-160LFederal Avj.q.tlonAdministrationLos AngelKs Aircraft Certification OfficeTransport Airplane Directorate

II.

III.

Revision B

Date ...•.•£~ Il, z.eiTRevision A approved July 20, 1998

gross weight inoreased to 3800 100.

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Loaded Aircraft Moment/lOOO - (Pound - Inches)

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Loaded Aircraft Mornent/rooo - (Pound - Inches)

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3/25/9~1Flint Aero Inc.

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