STC SA1070CE

This certificate issued to: Eaglejet Aviation Inc.

1600 Airport Road Wichita, KS 67209

Part 3 of the Civil Air Regulations. Dated May 15, 1956, as amended by 3-1 through 3-8.

Original Product - Type Certificate Number : A4CE Make : Cessna Model : TU206F, S/N U20602485, N1151V only

Installation of 50-gallon auxiliary fuel tank in aft cabin area in accordance with data listed on Drawing List PDA 5430 as revised December 10, 1974, or later FAA approved revisions. Data Required: (1) Copy of this certificate, including Continuation Sheets; and (2) Copy of FAA-approved Supplemental Airplane Flight Manual dated December 2, 1974; or later FAA-approved revisions.

The limitations and conditions of Aircraft Type Certificate Data Sheet A4CE apply except as outlined on pages 2 through 4 of this STC. Data used to approve this airplane for return to service are inadequate for production or duplication of installation/parts.

Date reissued : March 19, 1982; May 20, 2002;

September 20, 2002; February 28, 2003; June 23, 2006 Date amended :

Original signed by Dan Withers

(Signature) Dan Withers Program Manager Wichita Aircraft Certification Office (Title) Date of application : June 20, 1974 Date of issuance : January 28, 1975

FAA FORM 8110-2-1(10-69) PAGE 2 of 4 PAGES

Number SA1070CE

Date of Issuance: January 28, 1975 Date Reissued: March 19, 1982 Date Reissued: May 20, 2002 Date Reissued: September 20, 2002 Date Reissued: February 28, 2003 Date Reissued: June 23, 2006

X-Model TU206F, 6 PCL-SM (Normal Category), Approved October 26, 1971

C.G. Range Landplane (Note: Straight line variation between given points) (+33.0) to (+49.7) at 2500 lb. or less (+42.5) to (+49.7) at 3600 lb.

When STC SA1070CE 50-gallon auxiliary fuel system is installed and contains 10 or more gallons of fuel. (Note: Straight line variation between given points) (+33.0) to (+49.7) at 2500 lb. or less (+39.0) to (+49.7) at 3200 lb.

(+42.5) to (+48.7) to 3600 lb.

Floatplane Delete

Ski Plane Delete

No. of Seats (add) When STC SA1070CE 50-gallon auxiliary fuel system is installed:

2 at +34 to +48, right seat not approved as pilot station

Fuel Capacity 65 gal. (63.0 gal. Usable), two 32.5 gal. tanks in wings at +48 See NOTE 1 for data on system fuel.

See NOTE 2 for data on STC SA1070CE 50-gallon auxiliary fuel system

Serial Numbers U206F, S/N U20602485, only Eligibility

NOTE 1. (add) When STC SA1070CE 50-gallon auxiliary fuel system is installed, include unusable fuel of 6 lb. at +119.3.

FAA FORM 8110-2-1(10-69) PAGE 3 of 4 PAGES

Number SA1070CE

Date of Issuance: January 28, 1975 Date Reissued: March 19, 1982 Date Reissued: May 20, 2002 Date Reissued: September 20, 2002 Date Reissued: February 28, 2003 Date Reissued: June 23, 2006

NOTE 2. E. Applicable to model TU206F when STC SA1070CE 50-gallon auxilia ry fuel system is installed:

(1) On or adjacent fuel transfer filler cap:

“FUEL 100/130 OCT. MIN. 50 U.S. GAL. USABLE. WARNING: DETERMINE QUANTITY OF FUEL IN TANK PRIOR TO SERVICING. See loading and center of gravity section of supplemental flight manual prior to servicing.”

(2) On top of fuel transfer tank:

“No baggage is permitted when tank is serviced with fuel. Baggage allowable with no fuel in 50-gallon tank.”

(3) Above auxiliary fuel tank gauge and light:

“Fuel transfer pump on.”

(4) Adjacent to ci rcuit breakers:

“Fuel transfer pump 1 pump 2.”

(5) Adjacent to fuel transfer tank sump drains:

“Fuel transfer tank sump drain and cavity vent outlet.”

(6) Adjacent to fuel transfer line drain:

“Fuel transfer line drain.”

(7) Located above fuel selector valve:

“Fuselage Fuel Transfer System:

See loading and center of gravity limitations prior to servicing fuel transfer tank with fuel.

Transfer during level flight only.

Use left wing fuel first and burn to ¼ to ½ full.

FAA FORM 8110-2-1(10-69) PAGE 4 of 4 PAGES

Number SA1070CE

Date of Issuance: January 28, 1975 Date Reissued: March 19, 1982 Date Reissued: May 20, 2002 Date Reissued: September 20, 2002 Date Reissued: February 28, 2003 Date Reissued: June 23, 2006

NOTE 2 (continued):

Turn fuel transfer switches ON to transfer fuel to left wing tank.

Unless Flight Management dictates otherwise, burn right tank fuel during fuel transfer.

Use left tank as required to maintain lateral balance and to accept transfer fuel.

Monitor left wing fuel gauge to insure that tank does not overfill during fuel transfer.

Interrupt transfer as necessary.

Turn off transfer pump when transfer tank gauge reads empty (E) and fuel transfer low pressure light is on steady.”

(8) Adjacent to fuel tr ansfer quantity gauge:

“Fuselage fuel transfer tank gauge 50 U.S. Gal.”

“Light indicates NO fuel transfer or tank empty.”

(9) Adjacent to fuel transfer switches:

“ON – OFF pump #1, #2 fuel transfer.”

“Transfer system operation and limitations, see Supplemental Airplane Flight Manual.”

(10) Adjacent to original ident plate:

“Flo-Air, Inc., Wichita, Kansas. Modified per STC SA1070CE.

Date installed November 27, 1974.”

NOTE 3. Same.

NOTE 4: Same.

FAA FORM 8110-2-1(10-69) PAGE 5 of 4 PAGES

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