STC SA2202WE

FAA Form 8110-2 (5/14) Page 1 of 4

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

Number: SA2202WE

Part 3 of the Civil Air Regulations, dated 15 May 1956 and Amendments 1 and 2 and paragraphs 3.304 and 3.705 of Amendment 3-7 effective May 3, 1962.

Original Product – Type Certificate Number: 2A13 Make: Piper Model: PA-28R-180 PA-28R-200 S/N 28R-35001 thru 28R-7135329 PA-28R-200 S/N 28-R7235001 and up

Installation of recontoured leading edge, drooped ailerons in flaps down mode, fuselage flap, stabilator trim spring, wing stall fences, raked wing tips and dorsal fin (optional) in accordance with sealed Robertson Aircraft Drawing List

17. Installation of S/N 28R-7235001 and up same as above except stabilator trim spring is not required. A Robertson Aircraft FAA Approved Airplane Flight Manual Supplement is required for each model.

Date of Application: May 19, 1970 Date Reissued: 11/8/84; 10/10/86; 9/8/05; 7/31/17 Date of Issuance: July 13, 1970 Date Amended: 1/27/71; 6/26/73

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 4

Transfer the ownership of Supplemental Type Certificate Number: SA2202WE

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: SA2202WE

FAA Form 8110-2 (5/14) Page 3 of 4

Date of Issuance: July 13, 1970 Date Amended: June 26, 1973 Date of Reissuance: July 31, 2017

The approval of this change in type design applied basically to the above model aircraft only. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those previously approved modifications will introduce no adverse effect upon the airworthiness of these aircraft. Supplemental Type Certificate Addendum No. SA2202WE is a part of this STC. A copy of this Certificate and Addendum is required to be maintained as part of the modified aircrafts permanent records.

The conditions and limitations of Type Certificate Data Sheet No. 2A13 apply except as follows:

This STC Addendum, which is a part of Supplemental Type Certificate No. SA2202WE 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 STC Addendum is required to be maintained as part of the modified aircraft’s permanent records.

SUPPLEMENTAL TYPE CERTIFICATE HOLDER: R/STOL SYSTEMS, INC.

IX. Model PA-28R-180 (Normal Category) Airspeed Limits:

Never exceed 209 mph (181 knots) CAS Flaps extended 100 mph (87 knots) CAS Control Surface Movements:

Ailerons Aileron Droop Flaps from Neutral Up Down 0° 0° + 0° 30° + 2° 15° + 2°

- 2° - 2° - 2° 10° 2° + 2° 30° + 2° 15° + 2°

- 1° - 2° - 2° 25° 19° + 1° 27° + 2° 20° + 2°

- 2° - 2° - 2° 40° 15° + 1° 28° + 2° 20° + 2°

X. Model PA-28R-200 (Normal Category) S/N 28R-35001 thru 28R-7135329 Same conditions and limitations as IX above.

XI. Model PA-28R-200 (Normal Category) S/N 28R-7235001 & Up Same conditions and limitations as IX above.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA2202WE

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

Date of Issuance: July 13, 1970 Date Amended: June 26, 1973 Date of Reissuance: July 31, 2017

Data Pertinent To All Models:

Equipment – The following airplane flight manual supplements are required:

PA-28R-180 – Robertson Aircraft FAA approved Airplane Flight Manual Supplement, dated January 27, 1971.

PA-28R-200 S/N 28R-35001 through 28R-7135329 – Robertson Aircraft Corporation FAA Approved Airplane Flight Manual Supplement No. 17-6 dated June 26, 1973.

PA-28R-200 S/N 28R-7235001 and up – Robertson Aircraft FAA Approved Airplane Flight Manual Supplement No. 17-12 dated June 26, 1973.

NOTE 1: The Weight and Balance Report must be revised as follows:

PA-28R-180, PA-28R-200 S/N 28R-35001 through 28R-7135329, add 24 pounds at Station 114.8 or add 26 pounds at Station 120.7 with addition of dorsal fin.

PA-28R-200, S/N 28R-7235001 and up, add 22 pounds at Station 115 or add 24 pounds at Station 121 with addition of dorsal fin.

NOTE 2: The placards specified in the FAA Approved Piper Airplane Flight Manuals must be displayed plus the following changes made by the FAA Approved Robertson Aircraft Flight Manual Supplements:

ALL MODELS -- FLAP SET (100 MPH)

PA-28R-200, S/N 28R-7235001 and up, “Demonstrated Crosswind Component” deleted.

-END-

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA2202WE

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