# STC SA5259SW-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: S-TEC Corporation
- Description: Installation of S-TEC System 40/50 single and two axis automatic flight guidance systems Model ST-210-40/50.
- Status date: February 13, 1985
- Data sheets: A16CE, A16CE, A16CE, A16CE
- Certificate PDF: https://openairdocs.org/files/sha256/60/ec/60ec3af347cac316f6877e625d2a73bac80c7b7a8fa06c07fe05f64eccefd950
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/44A8E5A5BEE839DF86257ECB004E845D.0001
- Page: https://openairdocs.org/stc/SA5259SW-D

## ADs that name it

None.

## Approved models (4)

- Cessna Aircraft Company 207 (TCDS A16CE)
- Cessna Aircraft Company 207A (TCDS A16CE)
- Cessna Aircraft Company T207 (TCDS A16CE)
- Cessna Aircraft Company T207A (TCDS A16CE)

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

* .sltaa/a Uiritrd £tatu of anrrica Bcpartmcnt of transportation — jftderal atriation administration Supplemental l^gpe (Certificate isutmv&r SA5259SW-D S-TEC Corporation Rt, 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 M>^^ reuerai Aviation A16CE CESSNA : 207, 207A, T207 AND T207A Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems, Model ST-210-40/50, according to Bulletin No, 310;1 Revision 2, dated 1-17-85 and Master Drawing List No, 92230, Revision Bt dated 1-17-85 and/or later FAA Approved revisions of the above data, (28 Volt System), 1, FAA Approved Supplemental Flight Manual, P/N 89294, dated 1-13-84, is required for S-TEC System 40 for Cessna Models 207A and T207A, S/N 20700363 through S/N 20700482 and/or later "FAA Approved revisions of the above supplement, (See Continuation Sheet, Page 2, a part of this STC), 9-23-83 1-13 "84 ^ertL7riiAiji&0n Sola(rrivnA&fo<z/&p-jyJ£ : 10-15-84, 2-13-85, Revision 2 *^^J*£i*AC&&ri'4&Jl/t&£tfldn^^ yf^-^^j^C^^- (Signature ) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (Title)

TtiLt crrtijicate may be tramfirrid in accordance with FAR 21.47.

FAA fo«- 8II0-2 (! 0-48]

ttnitrd States of amenta Btpartmcnt of transportation— federal a&iation administration Supplemental t:gpe Certificate(Continuation £hcet) SA5259SWJD',' Revision 2 Limitations and Conditions (con't)

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89295, dated 1-13-84 is required for S-TEC System 40 for Cessna Models 207A and T207A, S/N 20700483 and upy and/or later FAA Approved revisions of the above supplement,

3. FAA Approved Supplemental Flight Manual, P/N 89296, dated "1.13 -84 is required for S-TEC System 50 for Cessna Models 207A and T207A, S/N 20700363 through S/N 20700482 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 89297, dated 1-13-84 is required for S-TEC System 50 for Cessna Models 207A and T207Ai' S/N 20700483 and up, and/or later FAA Approved revisions of the above supplement,

5. FAA Approved Supplemental Flight Manual, P/N 89294-1, dated 10-15.84 is required for S-TEC System 40 for Cessna Models 207, 207A, T207. and T207A, S/N 20700363 through S/N 20700482 and/or later FAA Approved revisions of the above supplement,

6. FAA Approved Supplemental Flight Manual, P/N 89296-1, dated 10-15-84 is required for S-TEC System 50 for Cessna Models 207, 207A, T207 and T207A, S/N 20700363 through S/N 20700482 and/or later FAA Approved revisions of the above supplement,

7. FAA Approved Supplemental Flight Manual, P/N 89294-2, dated 2-13-85 is required for S-TEC System 40 for Cessna Models 207, T207 and 207A, T207A, S/N 20700363 through S/N 20700482 and/or later FAA Approved revisions of the above supplement,

8. FAA Approved Supplemental Flight Manual, P/N 89296-2, dated 2-13-85 is required for S-TEC System 50 for Cessna Models 207, T207 and 207A, T207A, S/N 20700363 through S/N 20700482 and/or later FAA Approved revisions of the above supplement.

9. Compatabil ity of this modification with other previously approved modifications must be determined by the installer, . i •., .i!'.:r,i!ii,n nj this certificate is pumshahle by a fine nj nnt exceeding, SI, 000, or imfrisnrcm'nt nnt exceeding 3 \f/iri, <•' ' ••'• ' A.-. ( GRM 8iiy-2-l (10-69) This certificate may be twujerrej in accordance :t itfi i'.\R .7 / PAGE 2 op 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 ^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):.

## Every issue (1)

- February 13, 1985: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/60/ec/60ec3af347cac316f6877e625d2a73bac80c7b7a8fa06c07fe05f64eccefd950)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.