STC SA1513WE

FAA Form 8110-2 (5/14) Page 1 of 8

Reissued on July 14, 2017 to supersede the original STC, which has been lost or misplaced.

Number: SA1513WE

Part 3 of the Civil Air Regulations and Part 23 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: A4CE Make: Cessna Model: 206 (See STC Addendum No. SA1513WE) Description of Type Design Change:

Installation of flap actuated aileron droop system recontoured wing leading edge (except TU206F, U206F, U206E, U206G, TU206G, 206H and T206H) and flap actuated elevator trim system in accordance with Sierra Industries, Ltd. Master Drawing List No. 13, Rev. B dated 01/20/2006, or later FAA approved revision.

Compatibility of this design change with previously approved modifications must be determined by the installer. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. A copy of this Certificate and Addendum No. SA1513WE shall be maintained as part of the permanent records for the modified aircraft.

Date of Application: May 12, 1967 Date Reissued: 11/8/84; 10/10/86; 7/21/05; 7/14/17 Date of Issuance: September 15, 1967 Date Amended: 3/31/77; 5/18/79; 6/13/80 3/14/06

Signature

Title James A. Grigg Manager, Fort Worth Aircraft Certification Office , Southwest Region Sierra Industries, Ltd.

122 Howard Langford Drive Uvalde, TX 78801

FAA Form 8110-2 (5/14) Page 2 of 8

Transfer the ownership of Supplemental Type Certificate Number: SA1513WE

To (Name and address of transferee)

From (Name and address of grantor)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1513WE

FAA Form 8110-2 (5/14) Page 3 of 8

Date of Issuance: September 15, 1967 Date Amended: March 14, 2006 Date of Reissuance: July 14, 2017

Description of Type Design Change (Continued):

Addendum No. SA1513WE

CESSNA 206 TU206C TP206C Landplane & U206 Landplane & TU206D TP206D Skiplane P206 Floatplane TU206E Landplane, TP206E U206G TU206F Floatplane & TU206G Landplane & Floatplane U206A P206A Skiplane 206H U206B Landplane P206B T206H U206C Floatplane & TP206A U206D Skiplane TP206B Floatplane as approved on TC U206E P206C Data Sheet A4CE) U206F P206D Landplane TU206A P206E Skiplane TU206B

NOTE: These are the basic landing gear options approved on Type Certificate Data Sheet A4CE, Revision 20, dated July 15, 1976.

The limitations and conditions of Type Certificate Data Sheet A4CE apply except as follows:

This Addendum which is part of Supplemental Type Certificate No. SA1513WE prescribes conditions and limitations under which the product for which the STC was issued meets the airworthiness requirements of the Civil Air Regulations. A copy of this Addendum shall be maintained as part of the modified aircraft permanent records.

Supplemental Type Certificate Holder: Sierra Industries, LTD.

1. MODEL 206, 6PCL-SM (NORMAL CATEGORY)

C.G. Range LANDPLANE Straight line variation (+36.0) to (+47.4) at 2250 lb. or less between points given (+40.5) to (+47.4) at 3300 lb.

FLOATPLANE (EDO 582-3430) (+35.0) to (+47.4) at 2600 lb. or less (+38.5) to (+47.4) at 3500 lb.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1513WE

FAA Form 8110-2 (5/14) Page 4 of 8

Date of Issuance: September 15, 1967 Date Amended: March 14, 2006 Date of Reissuance: July 14, 2017

Description of Type Design Change (Continued):

Control Surface Movements

AILERON

Flap Droop from Setting Neutral ±2° Up ±2° Down ±2°

0° 0° 20° 14° 25° 16° 3° 28° 30° 15° 4° 28° (Sea) 40° 13 5° 25° (Land)

II. MODEL U206, 6PCL-SM (NORMAL CATEGORY)

C. G. Range See Section I of this STC Addendum

Control Surface See Section I of this STC Addendum.

Movements

III. MODEL P206, 6PCL-SM (NORMAL CATEGORY)

C. G. Range See Section I of this STC Addendum

Control Surface See Section I of this STC Addendum.

Movements

IV. MODEL U206A, 6PCL-SM (NORMAL CATEGORY)

C. G. Range LANDPLANE Straight Line Variation between points given (+36.0) to (+47.4) at 2500 lb. or less (+42.5) to (+47.4) at 3600 lb.

FLOATPLANE (EDO 582-3430)

(+35.0) to (+47.4) at 2600 lb. or less (+38.5) to (+47.4) at 3500 lb.

SKIPLANE (Fluidyne R210)

(35.0) to (+47.4) at 2250 lb. or less

(40.5) to (+47.4) at 3300 lb. or less

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1513WE

FAA Form 8110-2 (5/14) Page 5 of 8

Date of Issuance: September 15, 1967 Date Amended: March 14, 2006 Date of Reissuance: July 14, 2017

Description of Type Design Change (Continued):

Control Surface Movements

WING FLAPS Up Down +1°-2°

Land 0° 40° Sea 0° 30° Ski 0° 30°

AILERON Flap Droop from Setting Neutral ±2° Up ±2° Down ±2°

0° 0° 20° 14° 25° 16° 3° 28° 30° 15° 4° 28° (Ski, Sea) 40° 13° 5° 25° (Land)

V. MODEL P206A, 6PCL-SM (NORMAL CATEGORY) MODEL P206B, 6PCL-SM (NORMAL CATEGORY)

C. G. Range See Section IV of this STC Addendum

Control Surface See Section IV of this STC Addendum.

Movements

VI. MODEL TU206A, 6PCL-SM (NORMAL CATEGORY) MODEL TU206B, 6PCL-SM (NORMAL CATEGORY)

C. G. Range LANDPLANE Straight line variation between points +36.0) to (+47.4) at 2500 lb. or less (+42.5) to (+47.4) at 3600 lb.

FLOATPLANE (EDO 582-3430) (+35.0) to (+47.4) at 2600 lb. or less (+39.0) to (+47.4) at 3600 lb.

SKIPLANE (Fluidyne R210) (+35.0) to (+47.4) at 2250 lb. or less (+40.5) to (+47.4) at 3300 lb.

Control Surface See Section I of this STC Addendum.

Movements

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1513WE

FAA Form 8110-2 (5/14) Page 6 of 8

Date of Issuance: September 15, 1967 Date Amended: March 14, 2006 Date of Reissuance: July 14, 2017

Description of Type Design Change (Continued):

VII. MODEL TP206A, 6PCL-SM (NORMAL CATEGORY) MODEL TP206B, 6PCL-SM (NORMAL CATEGORY)

C. G. Range See Section I of this STC Addendum

Control Surface See Section IV of this STC Addendum.

Movements

VIII. MODEL U206B, 6PCL-SM (NORMAL CATEGORY)

C. G. Range LANDPLANE Straight line variation between points given (See Section VI of this STC Addendum)

FLOATPLANE

(+35.0) to (+47.4) at 2600 lb. or less (+39.0) to (+47.4) at 3500 lb.

SKIPLANE (Fluidyne R210)

(See Section VI of this STC Addendum)

Control Surface See Section IV of this STC Addendum.

Movements

IX. MODEL P206C/TP206C, 6PCLM (NORMAL CATEGORY) MODEL P206D/TP206D, 6PCLM (NORMAL CATEGORY) MODEL P206E/TP206E, 6PCLM (NORMAL CATEGORY)

Control Surface See Section IV of this STC Addendum.

Movements for data on the Landplane and Skiplane.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1513WE

FAA Form 8110-2 (5/14) Page 7 of 8

Date of Issuance: September 15, 1967 Date Amended: March 14, 2006 Date of Reissuance: July 14, 2017

Description of Type Design Change (Continued):

X. MODEL U206C/TU206C, 6PCL-SM (NORMAL CATEGORY) MODEL U206D/TU206D, 6PCL-SM (NORMAL CATEGORY) MODEL U206E/TU206E, 6PCL-SM (NORMAL CATEGORY) MODEL U206F/TU206F, 6PCL-SM (NORMAL CATEGORY)

Airspeed Limits Flap Extended: (S/N U206-0915 through U206-1444, U206-1445 through U206-01700) (S/N U206-01701 and up) 110 MPH (96 Knots CAS)

Control Surface See Section IV of this STC Addendum.

Movements

XI. MODEL U206G/TU206G, 6PCL-SM (NORMAL CATEGORY)

Airspeed Limits Flaps Extended See Section X of this STC Addendum

Control Surface Movements See Section IV of this STC Addendum.

XII. MODEL 206H/T206H, 6PCL-SM (NORMAL CATEGORY)

Airspeed Limits Flaps Extended See Section X of this STC Addendum

Control Surface Movements See Section IV of this STC Addendum.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1513WE

FAA Form 8110-2 (5/14) Page 8 of 8

Date of Issuance: September 15, 1967 Date Amended: March 14, 2006 Date of Reissuance: July 14, 2017

Description of Type Design Change (Continued):

DATA PERTINENT TO ALL MODELS

NOTE 2.B.

(10) On the flap control indicator for the following models U206F, TU206F, U206G and TU206G

(a) 0° to 10°

(b) 0° to 20° - Full (indices at these positions with white color code and 110 mph callout; also mechanical detent at 20°)”

POHS 13-4 required for U206G/TU206G serial numbers U20604650 and on.

AFMS 13-5, dated March 14, 2006, or later FAA approved revision is required for 206H/T206H S/N 20608001/T206 8001 and on.

Previously approved autopilot installations in all Model 206 airplanes are compatible with this STC when the flaps are fully retracted. The following placard must be displayed in full view of the pilot on airplanes equipped with an autopilot.

“AUTOPILOT MUST BE OFF FOR ALL OPERATIONS WITH FLAPS EXTENDED”

-END-

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1513WE

FAA Form 8110-2 (5/14) Page 9 of 8