STC SA1400NW

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: SA1400NW

Part 3 of the Civil Air Regulations, as amended to May 15, 1956 including Amendment 3-8.

Original Product – Type Certificate Number: 3A15 Make: Beechcraft Model: Bonanza 36 and A36

Removal of ailerons and installation of full span flaps, spoiler roll control system and elevator downspring compensator in accordance with FAA Sealed Robertson Aircraft Drawing List No. 36.

Date of Application: July 08, 1980 Date Reissued: 11/8/84; 10/10/86; 9/8/05; 7/31/17 Date of Issuance: September 18, 1981 Date Amended:

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: SA1400NW

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: SA1400NW

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

Date of Issuance: September 18, 1981 Date of Reissuance: July 31, 2017

The approval of this change in type design applies basically to the above model aircraft only. Th is approval should not be extended to other aircraft of this model on which other previously approved modification 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 3A15 apply except as follows:

The Addendum which is part of Supplemental Type Certificate No. SA1400NW 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: R/STOL SYSTEMS, INC.

MODEL Bonanza 36 and A36

Airspeed Limits: Remain the same, except for:

Flaps extended 15° 124 KIAS (143 MPH IAS) 120 KCAS (138 MPH CAS) Flaps extended 30° 104 KIAS (120 MPH IAS) 100 KCAS (115 MPH CAS)

C. G. Limits: Remain the same except for:

AFT CG Limits: 87.7 inches aft of datum at 3500 lbs or less with straight line variation to 87.2 inches at 3600 lbs.

Control Surface Movements: Remain the same except for:

SPOILER:

FLAP POSITION CONTROL WHEEL LEFT SPOILER RIGHT SPOILER

Neutral *0° *0° Up Left 61° ± 2° -6.5° ± 2° Right -6.5° ± 2° 61° ± 2° Takeoff Neutral 0° ± 1° 0° ± 1° 15° +2° Left N/A N/A

- 1° Right N/A N/A Landing Neutral 0° ± 1° 0° ± 1° 30° + 2° Left 55° ± 2° -15 ± 2°

- 0° Right -15° ± 2° 55° ± 2°

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1400NW

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

Date of Issuance: September 18, 1981 Date of Reissuance: July 31, 2017

*Left Spoiler travels must be within 1° of the right spoiler. Spoiler control cable tension same as original aileron equipped aircraft. (Ref.) 70°F – 38 lbs. to 48 lbs.

ELEVATOR AND ELEVATOR TAB

FLAP POSITION ELEVATOR ELEVATOR TAB

Up Up 23° ± 1° Down 20° ± 1° Up 5° ± Down 15° ± 1°

Takeoff Up 30° ± 1° Down 20° ± 1° N/A 15° + 2°

Landing Up 30° ± 1° Down 20° ± 1° N/A 30° + 2°

PILOTS OPERATING HANDBOOK SUPPLEMENT: POHS 36-1

Required for Models 36 and A 36.

King KFC 200 Autopilot per STC SA1145 CE is compatible with this modification with the following additional limitations:

1. Servo clutches must be set to the following values:

A. Roll Servo: 36 ± 3 lbs.

B. Pitch Servo: No Change.

C. Pitch Trim Servo: No Change.

2. No limitation on flap settings with autopilot engaged.

-END-

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1400NW

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