# STC SA01185CH - Type: Supplemental type certificate - Status: Current, Amended - Holder: Wipaire Inc, United States - Description: Installation of Wipaire Model 3450 amphibian/seaplane floats, Hartzell Propeller model HC-F3YR-1RF/F8468A-2R, and Parts Kit No 12D1-7330. - Applied: February 7, 2000 - Status date: August 7, 2009 - Product: Aircraft, Single-Engine - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A4CE](https://openairdocs.org/tcds/A4CE) - Certificate PDF: https://openairdocs.org/files/sha256/a3/13/a3132d0be8646962d54eb318f3b602e00569501b65a467aba88787bd7e543618 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F67A7274BD97B3648625761F0055FA69.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA01185CH ## ADs that name it (0) None. ## Approved models (29) - Cessna Aircraft Company 206 ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company 206H ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company P206 ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company P206A ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company P206B ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company P206C ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company P206D ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company P206E ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company T206H ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TP206A ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TP206B ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TP206C ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TP206D ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TP206E ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TU206A ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TU206B ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TU206C ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TU206D ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TU206E ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TU206F ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TU206G ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206 ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206A ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206B ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206C ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206D ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206E ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206F ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206G ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. Part 23 of the Federal Aviation Regulations. (See Type Certificate Data Sheet No. A4CE for complete certification basis) 1. For Models 206H and T206H: Installation of Wipaire Model 3450 Amphibian/Seaplane Floats and Hartzell Propeller Model HC-F3YR-1RF/F8468A-2R, in accordance with Wipaire, Inc. Installation Drawing No. 12D1-7330, No Revision, dated October 28, 1999, or later FAA approved revisions. 2. For all other Models: Installation of Wipaire Model 3450 Amphibian/Seaplane Floats in accordance with Wipaire, Inc. Installation Drawing No. 12D1-7370, No Revision, dated April 20, 2000, or later FAA approved revisions. 1. The Installer must determine whether this design change is compatible with previously approved modifications. 2. For Models U206F and U206G, Teledyne Continental Motors IO-550-F engine with McCauley D3A34C402/90DFA-10 propeller is an approved option when installed as per STC SA1482GL. Propeller diameter is to be 80 inches. Wipaire Inc. 1700 Henry Ave South Saint Paul, MN 55075 A4CE Make : Cessna Model : 206; 206H; P206; P206A; P206B; P206C; P206D; P206E; T206H; TP206A; TP206B; TP206C; TP206D; TP206E; TU206A; TU206B; TU206C; TU206D; TU206E; TU206F; TU206G; U206; U206A; U206B; U206C; U206D; U206E; U206F; U206G Date of application : February 07, 2000 Date of issuance : February 25, 2000 Date amended : September 12, 2000; May 30, 2003; August 07, 2009 ( Signature) Gregory J. Michalik, Senior Aerospace. Engineer Airframe & Administrative Branch Chicago Aircraft Certification Office ( Title) Original signed by: Gregory J. Michalik FAA FORM 8110-2-1(10-69) PAGE 2 of 6 PAGES Number FAA FORM 8110-2-1(10-69) PAGE 3 of 6 PAGES Number SA01185CH Date of Issuance: February 25, 2000 Date Amended: August 07, 2009 3. For aircraft Models U206B, U206C, U206D, U206E, U206F, and U206G, the following engine/propeller/spinner combination is an approved option when installed per STC SA1482GL: Teledyne Continental Motors Engine Model IO-550-F and Hartzell Model PHC-J3YF-1RF/F8468A-6R, -8R, or PHC-C3yF-1RF/F8468A-6R, -8R propeller, and Hartzell Model C4582-P spinner. 4. For aircraft equipped with Teledyne Continental Motors Engine Model IO-520-A, or –F, the following propeller/spinner combinations are approved options when installed per STC SA397CH: a. Hartzell Propeller Model PHC-J3YF-1RF/F8468A-6R, -8R, and Hartzell C4582-() spinner. b. Hartzell Propeller Model PHC-C3YF-1RF/F8468A-6R, -8R, and Hartzell A2295-1() spinner. 5. For aircraft Model TU206F, Teledyne Continental Motors Engine Model TSIO-520-M and McCauley Propeller Model D3A34C402/90DFA-10 is an approved option when installed as per STC SA1588GL. 6. For Models U206F and U206G (both with STC SA1482GL installed) and Model TU206F (with STC SA1588GL installed) and TU206G: a. AIRSPEED LIMITS: Never Exceed (V NE) 158 KIAS Maximum Structural Cruising (V NO) 142 KIAS Maneuvering (V A) at 3800 lbs. 121 KIAS at 3000 lbs. 114 KIAS at 2500 lbs. 104 KIAS b. MAXIMUM WEIGHT: 3800 lbs. (S/N U20601701 through U20604649) 3792 lbs. (S/N U20604650 and up). c. C.G. RANGE: S/N U20601701 through U20604649 (+34.0) to (+47.4) at 2600 lbs. or less. (+40.0) to (+47.4) at 3800 lbs. Straight line variation between points given. S/N U20604650 and up (+34.0) to (+47.4) at 2600 lbs. or less. (+39.7) to (+47.4) at 3792 lbs. Straight line variation between points given. FAA FORM 8110-2-1(10-69) PAGE 4 of 6 PAGES Number SA01185CH Date of Issuance: February 25, 2000 Date Amended: August 07, 2009 7. For Models U206F and U206G (without STC SA1482GL installed): a. AIRSPEED LIMITS: Never Exceed (V NE) 158 KIAS Maximum Structural Cruising (V NO) 142 KIAS Maneuvering (V A) at 3650 lbs. 120 KIAS at 3000 lbs. 111 KIAS at 2500 lbs. 100 KIAS b. MAXIMUM WEIGHT: 3650 lbs. c. C.G. RANGE: (+34.0) to (+47.4) at 2600 lbs. or less. (+39.2) to (+47.4) at 3650 lbs. Straight line variation between points given. 8. For Models U206G, TU206G, 206H, and T206H with Soloy Turbine Pac installed (STC SA2353NM): a. AIRSPEED LIMITS: Maximum Operating Speed (V mo) 150 KIAS Maneuvering (V A) at 3800 lbs. 126 KIAS at 3200 lbs. 118 KIAS at 2800 lbs. 110 KIAS b. MAXIMUM WEIGHT: 3800 lbs. (Models U206G/TU206G (S/N U20603522 through U20604649)) 3792 lbs. (Models U206G/TU206G (S /N U20604650 and up), 206H and T206H). c. C.G. RANGE: Models U206G /TU206G (S/N U20603522 through U20604649) (+34.0) to (+45.5) at 2600 lbs. or less. (+40.0) to (+45.5) at 3800 lbs. Straight line variation between points given. Models U206G/TU206G (S/N U 20604650 and up), 206H and Model T206H (+34.0) to (+45.5) at 2600 lbs. or less. (+40.0) to (+45.5) at 3792 lbs. Straight line variation between points given. d. CONTROL SURFACE Floatplane/Amphibian MOVEMENTS: Rudder: Right 20 ° +0°, -1° Left 20 ° +0°, -1° (measured parallel to O.O.W.L.) FAA FORM 8110-2-1(10-69) PAGE 5 of 6 PAGES Number SA01185CH Date of Issuance: February 25, 2000 Date Amended: August 07, 2009 9. For Models 206H and T206H with Soloy Mark II Turbine Pac installed (STC SA01878SE): a. AIRSPEED LIMITS: Maximum Operating Speed (V mo) 150 KIAS Maneuvering (V A) at 3792 lbs. 128 KIAS at 3200 lbs. 118 KIAS at 2800 lbs. 110 KIAS b. MAXIMUM WEIGHT: Maximum Ra mp Weight: 3808 lbs. Maxi mum Takeoff Weight: 3792 lbs. Maximum Landing Weight: 3792 lbs. c. C.G. RANGE: (+34.0) to (+45.5) at 2600 lbs. or less. (+39.96) to (+45.5) at 3792 lbs. Straight line variation between points given. 10. For Models 206H and T206H: a. AIRSPEED LIMITS: Never Exceed (V NE) 159 KIAS Maximum Structural Cruising (V NO) 142 KIAS Maneuvering (V A) at 3792 lbs. 122 KIAS at 3300 lbs. 114 KIAS at 2800 lbs. 104 KIAS b. MAXIMUM WEIGHT: 3792 lbs. c. C.G. RANGE: (+34.0) to (+47.4) at 2600 lbs. or less. (+39.6) to (+47.4) at 3792 lbs. Straight line variation between points given. 11. For all other Models: a. AIRSPEED LIMITS: Never Exceed (V NE) 158 KIAS Maximum Structural Cruising (V NO) 142 KIAS Maneuvering (V A) at 3600 lbs. 120 KIAS at 3000 lbs. 111 KIAS at 2500 lbs. 100 KIAS b. MAXIMUM WEIGHT: 3600 lbs. c. C.G. RANGE: (+34.0) to (+47.4) at 2600 lbs. or less. (+39.0) to (+47.4) at 3600 lbs. Straight line variation between points given. 12. For Models 206H (S/N 20608060 through 20608091) and T206H (S/N T20608101 through T20608158), the inspection/modification called out in Cessna Accomplishment Instructions AI206-57-01, Revision A, dated September 11, 2000, entitled “Wing Spar Cap Inspection/Replacement for Float Planes Only” must be complied with. 13. For Models 206H and T206H, the appropriate Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement, dated February 25, 2000, or a later FAA approved revision, is required. FAA FORM 8110-2-1(10-69) PAGE 6 of 6 PAGES Number SA01185CH Date of Issuance: February 25, 2000 Date Amended: August 07, 2009 14. For all other Models, the appropriate FAA Approved Airplane Flight Manual/Pilot's Operating Handbook Supplement, dated August 21, 2000, or a later FAA approved revision, is required. 15. If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission. - END - ## Every issue (1) - August 7, 2009: Amended, Current. [certificate](https://openairdocs.org/files/sha256/a3/13/a3132d0be8646962d54eb318f3b602e00569501b65a467aba88787bd7e543618) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.