STC SA5252SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Reissued
Status date
June 27, 1986
Applied
December 19, 1983
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS3A24

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-029.

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 Starts or Bepartmcnt of TCranfiportation —federal aoiation administration Supplemental ICgpc Certificate SA5252SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 «- 4fi& 4tite4>t4*4,n4j.-SWWCUAC** M>i£n ^Cin^^Ci/frti^a^e'e>n^t--M^va-Jcon^i^u>n^ Zn^t^Zt^ .^zJ1- Afttftfeca si£-**&7i -meedA. ^^-^z^?«<^*>*«^vx^i^4^y*«^E^^W^yi^*t^^^^t>/.»»«^' 3 ^>^n^ LI VI I Ml i 3 A2 4 CESSNA A185F Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-029, according to Bulletin No. 132, Revision 5, dated 6-24-86 and Master Drawing List No. 9228, Revision E, dated 6-24-86 and/or later FAA Approved revisions of the above data (28 Volt System).

1. Also eligible on the above Model when modified in accordance with STC SA2529WE (Internal Tip Tanks) and/or STC SA1441WE (Robertson STOL) Landplane or Floatplane.

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

&t^nj/rLa&^ Sx^frl-f^i^A^a/f^r- ^ 12-19-83 QLu*****^: 6-27-86, Revision 1 12-19-83 ^tta/c- ^a*n«nel6& .' (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW i - -- — /

This certificate may be transferred in accordance with FAR 21.17.

FAAfCKMSl 10-2(10-68)

United £tatti of SUncnra Bcpartmcnt of transportation— federal atiiation administration Supplemental t^pe Certificate(Continuation £heet) SA5252SW-D, Revision 1 Limitations and Conditions (con't)

2. FAA Approved Supplemental Flight Manual, P/N 8945-1, dated 12-19-83 is required for Cessna Model A185F, S/N 18503683 and below, and/or later FAA Approved revisions of the above supplement.

3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 8925-1, dated 12-19-83 is required for Cessna Model A185F, S/N 18503684 and on and/or later FAA Approved revisions of the above supplement.

4. FAA Approved Supplemental Flight Manual, P/N 8945-2, dated 6-27-86 is required for Cessna Model A185F, S/N 18503683 and below and/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 8925-2, dated 6-27-86 is required for Cessna Model A185F, S/N 18503684 and on and/or later FAA Approved revisions of the above supplement

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

. I'/; .illfTnlKin rif this certificate is punishable by a fine of not exceeding SI,000, or imprisonment not exceeding, -3 years, or /><>//.•.

' AA F ORM Biio-2-1 (10-69) 7his certificate may be tramjerrtd in accordance u-it/i i'AR I'/.-J.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 <7P code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and <7P 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 · 1

MakeModelData sheet
Cessna Aircraft CompanyA185F3A24