STC SA5197SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Amended
Status date
February 15, 1999
Applied
August 19, 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 6, 2025.

What it approves

Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-024.

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.

JHutieb States (M of tftranspCTrtattrm - (Sf^beral jA&tattrm (Certificate SA5197SW-D S-TEC Corporation One S-TEC Way Mineral Wells Municipal Airport Mineral Wells, TX 76067-9236 /tie ffSt's/,t/f> ^f.f iv 5 A6 Cessna 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, andlSOK Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-024, according to Bulletin No. 127, Revision 11, dated 2-10-99 and Master Drawing List No. 9224, Revision K, dated 2-10-99 with Optional Flight Director/Steering Horizon or later FAA Approved revisions of the above data (14 Volt System).

1. Also eligible on the above models (floatplane or amphibian) when modified per STC SA1705WE (internal tip tanks) and/or STC SA1435WE (Robertson STOL).

(See Continuation Sheets, Pages 2, 3, and 4, a part of this STC.)

If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

s^^t»/ti>M' irft/fr wd/rSi ' d /dt? ti/rM/%> t sr frfrw/r/r/tbtf a6r/<? fj v 8-19-83 8-29-83 10-26-83, 7-16-84, 3-03-86, 12-01-87, 2-15-99, Revisions (Signature) Michael Keirnan DAS Staff Coordinator. DAS 5 SW (Title)

nf 'CEraitspGrtattott - JifefrBral J^&taium (Ahmtmstraltort QLerttficnte SA5197SW-D, Revisions Limitations and Conditions (con't.)

2. Also eligible on the above models (landplane) when modified per STC SA649NW (gross weight increase), STC SA09132SC (engine conversion), STC SA09030SC (Hartzell propeller), STC SA1603SO (speed kit), STC SA1705WE (internal tip tanks) and STC SA1435WE (Robertson STOL) or any combination of the above.

3. FAA Approved Supplemental Flight Manual, P/N 8927-1, dated 8-29-83 is required for Cessna Models 180G, 180H, 180J, 180K, S/N 18053000 and Below, Landplane Only 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 8935-1, dated 8-29-83 is required for Cessna Model 180K, S/N 18053001 and On or later FAA Approved revisions of the above supplement, (Landplane Only).

5. FAA Approved Supplemental Flight Manual, P/N 8927-2, dated 10-26-83 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) 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 8935-2, dated 10-26-83 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) or later FAA Approved revisions of the above supplement.

7. FAA Approved Supplemental Flight Manual, P/N 8927-3, dated 7-16-84 is required for Cessna Models 180G, 180H, 180J, 180K, S/N 18053000 and Below, Landplane or Floatplane Configurations and the above models when modified by STC SA1705WE (Internal Tip Tanks) and/or STC SA1435WE (Robertson STOL Conversion) or later FAA Approved revisions of the above supplement.

8. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 8935-3, dated 7-16-84 is required for Cessna Model 180K, S/N 18053001 and On, Landplane or Floatplane Configurations and the above model when modified by STC SA1705WE (Internal Tip Tanks) and/or STC SA1435WE (Robertson STOL Conversion) or later FAA Approved revisions of the above supplement.

9. FAA Approved Supplemental Flight Manual, P/N 89481, dated 7-16-84 is required for Cessna Models 180, 180A, 180B, 180C, 180D, 180E, 180F 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) or later FAA Approved revisions of the above supplement.

FAA Form 8110-2-1(10-69) Page 2 of 4 This certificate may be transferred in accordance with FAR 21-47.

JHixiteb JitaicB (©f Jkmerica of tKraitspnriattcm - (Herttftcate (donttnuatton SA5197SW-D, Revisions Limitations and Conditions (con't.)

10. FAA Approved Supplemental Flight Manual, P/N 8927-4, dated 3-03-86 is required for Cessna Models 180G, 180H, 180J, 180K, S/N 18053000 and Below, (Landplane or Floatplane Configurations) and the above models when modified by STC SA1705WE (Internal Tip Tanks) and/or STC SA1435WE (Robertson STOL Conversion) or later FAA Approved revisions of the above supplement.

11. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 8935-4, dated 3-03-86 is required for Cessna Model 180K, S/N 18053001 and On (Landplane or Floatplane Configurations) and the above models when modified by STC SA1705WE (Internal Tip Tanks) and/or STC SA1435WE (Robertson STOL Conversion) or later FAA Approved revisions of the above supplement.

12. FAA Approved Supplemental Flight Manual, P/N 89481-1, dated 3-03-86 is required for Cessna Models 180, 180 A, 180B, 180C, 180D, 180E, 180F 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) or later FAA Approved revisions of the above supplement.

13. FAA/DAS Approved Supplemental Flight Manual, P/N 8927, Revision 5, dated 2-15-99 is required for

1. Cessna models 180G, 180H, 180J; and 180K, S/N 18053000 and below (floatplane or amphibian) and the above models when modified per STC SA1705WE (internal tip tanks) and/or STC SA1435WE (Robertson STOL) 2. Cessna models 180G, 180H, 180J; and 180K, S/N 18053000 and below (landplane) and the above models when modified per STC SA649NW (gross weight increase), STC SA09132SC (engine conversion), STC SA09030SC (Hartzell propeller), STC SA1603SO (speed kit), STC SA1705WE (internal tip tanks), and STC SA1435WE (Robertson STOL) or any combination of the above or later FAA Approved revisions of the above supplement.

14. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 8935, Revision 5, dated 2-15-99 is required for 1. Cessna model 180K, S/N 18053001 and on (floatplane or amphibian) and the above model when modified per STC SA1705WE (internal tip tanks) and/or STC SA1435WE (Robertson STOL) 2. Cessna model 180K, S/N 18053001 and on (landplane) and the above model when modified per STC SA649NW (gross weight increase), STC SA09132SC (engine conversion), STC SA09030SC (Hartzell propeller), STC SA1603SO (speed kit), STC SA1705WE (internal tip tanks), and STC SA1435WE (Robertson STOL) or any combination of the above or later FAA Approved revisions of the above supplement.

FAA Form 8110-2-1(10-69) Page 3 of 4 This certificate may be transferred in accordance with FAR 21.4?.

•Mmteh ^iatcB ®f .America of tErattspnriatum - ^eheral ^frtatton J\.bmmtstratimt OLerttftcate SA5197SW-D, Revisions Limitations and Conditions (con't.)

15. FAA/DAS Approved Supplemental Flight Manual, P/N 89481, Revision 2, dated 2-15-99 is required for

1. Cessna model 180, 180 A, 180B, 180C, 180D, 180E, and 180F (floatplane or amphibian) and the above models when modified per STC SA1705WE (internal tip tanks) and/or STC SA1435WE (Robertson STOL) 2. Cessna models 180, 180A, 180B, 180C, 180D, 180E, and 180F (landplane) and the above models when modified per STC SA649NW (gross weight increase), STC SA09132SC (engine conversion), STC SA09030SC (Hartzell propeller), STC SA1603SO (speed kit), STC SA1705WE (internal tip tanks), and STC SA1435WE (Robertson STOL) or any combination of the above or later FAA Approved revisions of the above supplement.

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

FAA Form 8110-2-1(10-69) Page 4 of 4

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