STC SA00188SE

Number SA00188SE

This certificate, issued to AeroAcoustics Aircraft Systems, Inc.

9802 29 th Ave. W., Hangar B-104 Everett, WA 98204

Part 23 of the Federal Aviation Regulations.

Original Product⎯Type Certificate Number: A37CE Make: Cessna Model: 208B

Description of the Type Design Change: Installation of AeroAcoustics Aircraft Systems, Inc. Aircraft Payload Extender gross weight increase kit in accordance with Installation Manual AA1196, Revision A, dated June, 5, 1995, and Drawing List AA1195, Revision A, dated June 5, 1995, or later FAA-approved revisions.

Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to other aircraft on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including change in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this certificate, Continuation Sheets and FAA-approved Airplane Flight Manual Supplement listed on Page 3, dated July 5, 1995, must be maintained as part of the permanent records for the modified aircraft.

(See Continuation Sheets Pages 3 and 4)

This certificate and the supporting data which is the ba sis for approval shall remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of application: November 17, 1993 Date reissued: May 13, 2008 Date of issuance: April 14, 1995 Date amended: July 5, 1995; November 17, 2003

Any alteration of this certificat e is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both.

(Signature) Acting Manager, Seattle Aircraft Certification Office (Title)

United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA00188SE

AeroAcoustics Aircraft Systems, Inc.

Reissued: May 13, 2008 Amended: July 5, 1995; November 17, 2003

Limitations and Conditions: (cont’d)

This Continuation Sheet, which is part of STC No. SA00188, dated June 23, 1995, prescribes the conditions and limitations under which the product for which the STC was issued meets the airworthiness of the Federal Aviation Regulations.

The conditions and limitations of the Type Certificate Data Sheet No. A37CE apply, except where superseded by the following:

Applicability: This modification is limited to the following landplanes only:

Model Serial Numbers 208B without cargo pod 208B0001 through 208B0178 and 208B0180 through 208B0229 and aircraft modified by Cessna Kit SK208-84 208B 208B0179, 208B0230 and up and aircraft modified by Cessna Kit SK208-80

Flight Manual Supplement: Model 208B with PT6A-114 (600SHP) without cargo pod Document No. AFMS-C208-2, dated July 5, 1995, or later FAA approved revision

Model 208B with PT6A-114A(675 SHP) Document No. AFMS-C208-3, dated April 13, 1995, or later FAA approved R e v i s i o n

Airspeed Limits (IAS): Maneuvering Speed: at 8950 pounds.............148 knots

C.G. Range: Takeoff and flight +199.97 inches to +204.35 inches at 8950 pounds +199.15 inches to +204.35 inches at 8750 pounds +193.37 inches to +204.35 inches at 8000 pounds +179.60 inches to +204.35 inches at 5500 pounds or less Straight line variation between points given.

Placards: On each side of the nose strut fairing near the tow limit marking, and near the nose jacking point on the left side on the nose wheel strut fairing:

"DO NOT JACK OR TOW THIS AIRCRAFT AT GROSS WEIGHTS ABOVE 8785 POUNDS"

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

United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA00188SE

AeroAcoustics Aircraft Systems, Inc.

Reissued: May 13, 2008 Amended: July 5, 1995; November 17, 2003

Limitations and Conditions: (cont’d)

This Continuation Sheet, which is part of STC No. SA00188, dated June 23, 1995, prescribes the conditions and limitations under which the product for which the STC was issued meets the airworthiness of the Federal Aviation Regulations.

The conditions and limitations of the Type Certificate Data Sheet No. A37CE apply, except where superseded by the following:

Maximum Ramp 8985 pounds Weights: Takeoff 8950 pounds Landing 8500 pounds

Flight into known icing Model 208B with PT6A-114 (600 SHP):

Cargo pod removed 8450 pounds

Model 208B with PT6A-114A (675 SHP):

Cargo pod installed 8550 pounds Cargo pod removed 8750 pounds

Load Factors: Flaps Up +3.37g, -1.35g Flaps Down (all settings) +2.00g

- END -

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