STC SA5102SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Amended
Status date
February 7, 1996
Applied
August 2, 1982
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS3A15

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of S-TEC yaw damper system, Model ST-118.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

£001 Btpartmtnt of transportation—Jfotaal atriation Administration Supplemental 'Cgpc Certificate SA5102SW-D S-TEC Corporation 946 Pegram Mineral Wells, Texas 76067 ^ 3 y^ C 1 V i 1 Air 3A1 5 Beech 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33 E33A, E33C, F33, F33A, F33C, 633, 36, and A36 Installation of S-TEC Yaw Damper System, Model ST-118, according to Bulletin No.

221, Revision 6, dated 1-23-96 and Master Drawing List No. 92128, Revision F, dated 1-23-96 or later FAA Approved revisions of the above data (14 Volt System).

1. Only eligible on Beech Model F33A, S/N CE-290 through S/N CE-771.

2. Only eligible on Beech Model F33C, S/N CJ-26 through S/N CJ-148.

(See Continuation Sheet, Page 2, a part of this STC.)

^2e>r~m4^^^ SZcJmMii/ra&v^jb 8-02-82 <%-'- —*—-'• 8-18-82 3Le*~~-J~i: 9-22-82, 1-13-87, 1-25-91, 2-07-96, Revision 4 \A)M,etiir*£&0t*jit'2ne'£&arn£n& William J. Thomas DAS Staff ConrdJaatar^ DAS(Till*) fine of not exceeding tl ,000, or imprisonment not exceeding 3 years, or both.

Tkit etrtijitatt may bt traiufemj in tenrJtua m'(A FAR 21.47.

ttniad Statrs of Sntnra Btpartmtnt of Transportation— federal Station administration Supplemental t^pe Certificate(Continuation SA5102SW-D, Revision 4 Limitations and Conditions (con't.)

3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89152, dated 8-18-82 is required for Beech Models 36 and A36 or later FAA Approved revisions of the above supplement.

4. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89152-1, dated 1-13-87 is required for Beech Models 36 and A36 or later FAA Approved revisions of the above supplement.

5. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89903, dated 1-25-91 is required for Beech Model F33A, S/N CE-290 through S/N CE-771 or later FAA Approved revisions of the above supplement.

6. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891235, dated 2-07-96 is required for Beech Models 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, E33C, F33; F33C, S/N CJ-26 through S/N CJ-148; and 633 or later FAA Approved revisions of the 'above supplement.

7. Compatibility of this modification with other previously approved modifications must be determined by the installer.

HI alteration of thu certificate is punishable by a fine of not exceeding Si,OOP, or imprisonment not exceeding 3 years, or hnth.

AA FOBM »ii*2-l (tO-M> TAu catiftati may be transftrriJ in accordant! with 1'Ali .'1.1?.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name oj transferee) (Address of transferee) (lumber and street) (City, State, and £IP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, Stale, and <7/> code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 14

MakeModelData sheet
Beechcraft Corporation35-333A15
Beechcraft Corporation35-A333A15
Beechcraft Corporation35-B333A15
Beechcraft Corporation35-C333A15
Beechcraft Corporation35-C33A3A15
Beechcraft Corporation363A15
Beechcraft CorporationA363A15
Beechcraft CorporationE333A15
Beechcraft CorporationE33A3A15
Beechcraft CorporationE33C3A15
Beechcraft CorporationF333A15
Beechcraft CorporationF33A3A15
Beechcraft CorporationF33C3A15
Beechcraft CorporationG333A15