STC SA5245SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Reissued
Status date
March 18, 1986
Applied
November 21, 1983
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS5A6

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 single axis automatic flight guidance system Model ST-023.

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 dates of 9arrica Bepartmcnt of Transportation —federal dotation Administration Supplemental TCpe Certificate SA5245SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wo Hers Industrial Complex Mineral Wells, TX 76067 ria* * ClVll Air

• .'i£<aAi£ &ria* 'rut/ \JrocuicS —— •-/•ySi* ~Gie<r&fica£e'<yu4rrvv0r- : 5A6 CESSNA 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J AND 180K Installation of S-TEC System 60 Single Axis Automatic Flight Guidance System, Model ST-023, according to Bulletin No. 126, Revision 4, dated 1-15-86 and Master Drawing List No. 9223, Revision D, dated 1-15-86 and/or later FAA Approved revisions of the above data (14 Volt System).

1. Eligible on the above listed models when modified in accordance with STC SA1705WE (Wing Tip Tanks-Internal) and/or STC SA1435WE (Robertson STOL Conversion) (Landplane and Floatplane).

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

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•&*^nimjtfa>wda&Afa'0£n*i**f€teJeA£a>0&Art4djpy'£ne' Sxdm4*uA£t>a/*»r-JtJj&f 11-21-83 SLu*****^: 7-18-84, 3-18-86, Revision 2 11-29-83 ^^^C (Slfnalurt) Harold W. Holdeman DAS Staff Coordinator. DAS 5 SW (Title)

This artificatt may kt Iraiuftmd in tcctrjanct with FAR 21.47.

United &tatu of SUncnra Bepartmcnt of ^transportation— .federal Station administration Supplemental HCjipe Certificate(Continuation £hett) SA5245SW-D, Revision 2 Limitations and Conditions (con't)

2. FAA Approved Supplemental Flight Manual, P/N 8926-1, dated 11-29-83 is required for Cessna Models 180G, 180H, 180J, 180K, S/N 18053000 and below and the above Models when modified in accordance with STC SA1705WE (Wing Tip Tanks- Internal ) and/or STC SA1435WE Robertson STOL Conversion (Landplane and Floatplane Configuration) 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 8934-1, dated 11-29-83 is required for Cessna Model 180K, S/N 18053001 and on and the above Model when modified in accordance with STC SA1705WE (Wing Tip Tanks-Internal) and/or STC SA1435WE Robertson STOL Conversion (Landplane and Floatplane Configuration) and/or later FAA Approved revisions of the above supplement.

4. FAA Approved Supplemental Flight Manual, P/N 89482, dated 7-18-84 is required for Cessna Models 180, 180A, 180B, 180C, 180D, 180E and 180F and the above Models when modified in accordance with STC SA1705WE (Internal Tip Tanks) and/or STC SA1435WE (Robertson STOL) (Landplane and Floatplane) and/or later FAA Approved revisions of the above supplement.

5. FAA Approved Supplemental Flight Manual, P/N 8926-2, dated 3-18-86 is required for Cessna Models 180G, 180H, 180J, 180K, S/N 18053000 and below and the above -Models when modified in accordance with STC SA1705WE (Wing Tip Tanks-Internal) and/or STC SA1435WE Robertson STOL Conversion (Landplane and Floatplane Configuration) and/or later FAA Approved revisions of the above supplement,

6. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 8934-2, dated 3-18-86 is required for Cessna Model 180K, S/N 18053001 and on and the above Model when modified in accordance with STC SA1705WE (Wing Tip Tanks-Internal) and/or STC SA1435WE Robertson STOL Conversion (Landplane and Floatplane Configuration) and/or later FAA Approved revisions of the above supplement.

7. FAA Approved Supplemental Flight Manual, P/N 89482-1, dated 3-18-86 is required for Cessna Models 180, 180A, 180B, 180C, 180D, 180E and 180F and the above Models when modified in accordance with STC SA1705WE (Internal Tip Tanks) and/or STC SA1435WE (Robertson STOL) (Landplane and Floatplane) and/or later FAA Approved revisions of the above supplement.

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

.I'D alteration of this certificate is punishable by a fine of not exceeding SI, 000, or imprisonment not exceeding 3 years, or both.

' A A FORM ai io-2-i (1O-69) This certificate may be transferred in accordance with I'.Mt i'1.1?

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee).

(Address of transferee). (Number and street) (City, Slate, and ^IP code) from (Name of grantor) (Print or type) .

(Address of grantor) (Number and street) (City, State, and ^IP 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 · 11

MakeModelData sheet
Cessna Aircraft Company1805A6
Cessna Aircraft Company180A5A6
Cessna Aircraft Company180B5A6
Cessna Aircraft Company180C5A6
Cessna Aircraft Company180D5A6
Cessna Aircraft Company180E5A6
Cessna Aircraft Company180F5A6
Cessna Aircraft Company180G5A6
Cessna Aircraft Company180H5A6
Cessna Aircraft Company180J5A6
Cessna Aircraft Company180K5A6