STC SA1382WE

FAA Form 8110-2 (5/14) Page 1 of 6

Reissued on July 31, 2017 to supersede the original STC, which has been lost or misplaced.

Number: SA1382WE

Part 3 of the Civil Air Regulations, effective November 1, 1949, as amended by 3-1 through 3-12.

Original Product – Type Certificate Number: 3A13 Make: Cessna Model: 182 through 182R; R182, TR182, T182

Installation of flap actuated aileron droop system for all models. Additionally, for all models except the 182P, 182Q, 182R, R182, TR182, and T182, recontoured wing leading edge, flap actuated elevator trim system. All installations are accomplished per drawings shown on FAA sealed Robertson Aircraft Drawing List 10.

4/25/67; 12/5/68; 5/10/72; 11/5/73;

Date of Application: February 04, 1966 Date Reissued: 8/22/67; 2/12/68; 8/4/69; 4/20/70; 11/30/70;

11/8/84; 10/10/86; 7/21/05; 7/31/17 Date of Issuance: March 13, 1967 Date Amended: 5/10/72; 2/1/78; 2/15/78; 10/17/78; 11/27/78;

5/27/82; 10/20/82

Signature

Title Jim Grigg Manager, Fort Worth A CO Branch, Compliance & Airworthiness Division Sierra Industries, Ltd.

122 Howard Langford Drive Uvalde, TX 78801

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

Transfer the ownership of Supplemental Type Certificate Number: SA1382WE

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: SA1382WE

FAA Form 8110-2 (5/14) Page 3 of 6

Date of Issuance: March 13, 1967 Date Amended: October 20, 1982 Date of Reissuance: July 31, 2017

The approval of this change in type design applies basically to the above model aircraft only. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any other type design changes or previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate shall be maintained as part of the permanent records for the modified aircraft. The limitations and conditions of Type Certificate Data Sheet 3A13 apply except as follows:

This addendum which is part of Supplemental Type Certificate No. SA1382 prescribes conditions and limitations under which the produce 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: R/STOL SYSTEMS, INC.

I. MODEL 182 4PCLM (NORMAL CATEGORY)

Control Surface Movements

AILERONS

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

0° 0° ± 2° 20° ± 2° 14° ± 2° 10° 8° ± 2° 11° ± 2° 21° ± 2° 20° 13° ± 2° 6° ± 2° 25° ± 2° 30° 15° ± 2° 4° ± 2° 26° ± 2° 40° 12.5° ± 0° 6° ± 2° 24° ± 2°

II. MODEL 182A 4PCLM (NORMAL CATEGORY)

Control Surface Movement See Section I of this STC Addendum.

III. MODEL 182B 4PCLM (NORMAL CATEGORY)

Control Surface Movements See Section I of this STC Addendum.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1382WE

FAA Form 8110-2 (5/14) Page 4 of 6

Date of Issuance: March 13, 1967 Date Amended: October 20, 1982 Date of Reissuance: July 31, 2017

IV. MODEL 182C 4PCLM (NORMAL CATEGORY) MODEL 182D 4PCLM (NORMAL CATEGORY)

Control Surface Movements See Section I of this STC Addendum.

V. MODEL 182E 4PCLM (NORMAL CATEGORY) MODEL 182F 4PCLM (NORMAL CATEGORY) MODEL 182G 4PCLM (NORMAL CATEGORY)

Control Surface Movements See Section I of this STC Addendum.

VI. MODEL 182H 4PCLM (NORMAL CATEGORY) MODEL 182J 4PCLM (NORMAL CATEGORY) MODEL 182K 4PCLM (NORMAL CATEGORY) MODEL 182L 4PCLM (NORMAL CATEGORY)

Control Surface Movements See Section I of this STC Addendum.

VII. MODEL 182M 4PCLM (NORMAL CATEGORY)

Control Surface Movements See Section I of this STC Addendum.

VIII. MODEL 182N 4PCLM (NORMAL CATEGORY)

Control Surface Movements See Section I of this STC Addendum.

IX. MODEL 182P 4PCLM (NORMAL CATEGORY)

Control Surface Movements See Section I of this STC Addendum.

X. MODEL 182Q 4PCLM (NORMAL CATEGORY)

Control Surface Movements See Section I of this STC Addendum.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1382WE

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

Date of Issuance: March 13, 1967 Date Amended: October 20, 1982 Date of Reissuance: July 31, 2017

XI. MODEL 182R 4PCLM (NORMAL CATEGORY)

Control Surface Movements See Section I of this STC Addendum.

XII. MODEL R182 4PCLM (NORMAL CATEGORY)

Control Surface Movements See Section I of this STC Addendum.

XIII. MODEL TR182 4PCLM (NORMAL CATEGORY)

Control Surface Movements See Section I of this STC Addendum.

XIV. MODEL T182 4PCLM (NORMAL CATEGORY)

Control Surface Movements See Section I of this STC Addendum.

DATA PERTINENT TO ALL MODELS

NOTE 2.

C. Applicable to Models 182E, 182F, 182G, 182H, 182J, 182K, 182L and 182M

(5) For Models 182F, 182G, 182H, 182J, 182K, 182L and 182M, if optional electrical installatio n per Robertson Aircraft 10-800 has been accomplished, placard on pilot’s control wheel around push button switch to read:

“FLAPS UP – GROUND USE ONLY”

D. Applicable to Model 182N

(6) If optional electrical installation per Robertson Aircraft 10-800 has been accomplished, placard on pilot’s control wheel around push button switch to read: “FLAPS UP – GROUND USE ONLY”

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1382WE

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

Date of Issuance: March 13, 1967 Date Amended: October 20, 1982 Date of Reissuance: July 31, 2017

E. Applicable to All Models

Autopilot installations in all Model 182 airplanes are compatible with this STC.

The following additional limitation applies (this limitation must be a placard installed in full view of the pilot).

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: SA1382WE

FAA Form 8110-2 (5/14) Page 7 of 6