STC SA5251SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
December 16, 1983
Applied
December 2, 1983
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 manual electric trim system Model ST-154.

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.

Unfed £tatu of anmca Btpartmcnt of 'Crarsportation— Jfedcral atriation administration Supplemental t^pe Certificate SA5251SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex :

Mineral Wells, TX 76067 anf^J&t'fcituxtfvrbajhfixiuf^JviJn ^fLe,JtmjSa/ismiL mnftfj*n-r/</i'*nA *ef4*»erru*iA,^'&»»i 3 y^ ClVl'l Air

•Slta4i/a£ 3A15 BEECH 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, E33C, F33, F33C, G33 AND F33A Installation of S-TEC Manual Electric Trim System, Model ST-154, according to Bulletin No. 254, dated 11-30-83 and Master Drawing List No. 92266, dated 11-30-83 and/or later FAA Approved revisions of the above data, (14 Volt System).

1. Eligible only on Model F33A, S/N CE-315 and below.

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89381, dated 12-16-83 is required and/or later FAA Approved revisions of the above Supplement.

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

£Xdrru/njA&<i/ci^*xJA* 12-2-83 12-16-83 (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (Till*)

This artificatt may tt traxtftrnd in •cordkjicr Ljith FAR 21.47.

ttitittfl £tatta of amcrira Bepartment of transportation— federal 2toiation administration Supplemental ICgpe Certificate(Continuation &heet) SA5251SW-D Limitations and Conditions (con't)

3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89382, dated 12-16-83 is required and/or later FAA Approved revisions of the above Supplement.

4. Compatability of this modification with other previously installed modifications must be determined by the installer.

.•!«v alteration of this certificate is punishable by a fine of not exceeding SI, OOP, or imprisonment not exceeding 3 years, or both.

FAA FORM siio-2-1 (1O-69) This certificate may be transjcrred in accordance with FAR L'i.-)'.

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

Signature of grantor (In ink):

U.S. GOVERNMENT PRINTING OFFICE : 1966 OF —205-579

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 · 12

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