STC SA5263SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Reissued
Status date
August 12, 1986
Applied
November 4, 1983
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS3A13

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of S-TEC System 60 two axis Automatic Flight Guidance System, Model ST-011 with optional automatic electric trim system

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.

United Stotis of antrica Bcpartmcnt of transportation —federal 2toiation administration Supplemental 'Cuje Certificate tXufm&er' SA5263SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 a<e i 3 j^^Ae Civil Air

• ./ItaAt f^iatn^u t^foauf/ —— I/'U^if ~fze>r&fi<M£e><yi'um/ivr- : oAlo CESSNA 182P AND 182Q . *y •Is/uA.t —/ ^e&i&n ^3SiJzn,a* :

Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-011, with Optional Automatic Electric Trim System according to Bulletin No.

Ill, Revision 8, dated 6-10-86 and Master Drawing List No. 9216, Revision H, dated 6-10-86 and/or later FAA Approved revisions of the above data, (14 Volt System)

1. FAA Approved Supplemental Flight Manual, P/N 8912-3, dated 1-20-84 is required for Cessna Models 182P and 182Q, S/N 18266590 and below and/or later FAA Approved revisions of the above supplement.

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

&^ 11-4-83 ~£*~**~J: 8-12-86, Revision 1 1-20-84 (Signature) Harold W. Holdeman HAS Staff r.nnrHirmtnr^ DAS 5 SW (THU)

Tkii crrtificati may kt trantftrrtJ in tceorJanet with FAR 21.47.

PAA fomm (110-2 (10-««)

ttnittd £»tatc» of amcrica Bepartmcnt of transportation— Jftdcral aoiation administration Supplemental HTjipe Certificate(Continuation &heet) _ SA5263SW-D, Revision 1 Limitations and Conditions (Con't)

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 8973-1, dated 1-20-84 is required for Cessna Model 182Q, S/N 18266591 and up and/or later FAA Approved revisions of the above supplement.

3. FAA Approved Supplemental Flight Manual, P/N 8912-4, dated 8-12-86 is required for Cessna Models 182P and 182Q, S/N 18266590 and below and/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 8973-2, dated 8-12-86 is required for Cessna Model 182Q, S/N 18266591 and up and/or later FAA Approved revisions of the above supplement.

5. Compatability of this modification with other previously approved modifications must be determined by the installer.

.I'n tilli-rnlum (if this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 tears, nr hnth.

i AA ( ORM 8110-2-1 (1O-69) This certificate may be transferred in accordance wit/i i.\R -A-/.7 PAGE 2 OF 2 PAGES

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee)_ (Address of transferee). (Number and street) (City, State, and <JP code) from (Name of grantor) (Print or type) .

(Address of grantor) (Number and street) (City, State, and 2JP 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 · 2

MakeModelData sheet
Textron Aviation Inc.182P3A13
Textron Aviation Inc.182Q3A13