# STC SA6090SW-D

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: S-TEC Corporation
- Description: Installation of S-TEC yaw damper system Model ST-072.
- Status date: April 16, 2002
- Data sheets: 3A15, 3A15, 3A15, 3A15
- Certificate PDF: https://openairdocs.org/files/sha256/d6/20/d6209f5e2f3ace4f98afb48769f08e6dc9d4b2cc976033af6281d29224175e2f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/994C7C30FA60073485256CC200569E86.0001
- Page: https://openairdocs.org/stc/SA6090SW-D

## ADs that name it

None.

## Approved models (4)

- Raytheon Aircraft Company S35 (TCDS 3A15)
- Raytheon Aircraft Company V35 (TCDS 3A15)
- Raytheon Aircraft Company V35A (TCDS 3A15)
- Raytheon Aircraft Company V35B (TCDS 3A15)

## 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.

®f (America of transportation - Jifebcral Rotation ^hmtntstration (Eerttftcate SA6090SW-D S-TEC Corporation One S-TEC Way Mineral Wells Municipal Airport Mineral Wells, TX 76067-9236 3A15 Beech S35, V35, V35A, and V35B Installation of S-TEC Yaw Damper System, Model ST-072, according to Bulletin No. 175, Revision 9, dated 3-18-02 and Master Drawing List No. 9279, Revision I, dated 3-18-02 or later FAA Approved revisions of the above data (14 Volt System).

(See Continuation Sheet, Page 2, 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.

b <x/M$<Mfo and the ±«/i//<j>/ftia data wAieh «i the 4aM jot, aMvuwat' <*hatt' lamain in effect untilr //a ill f/ date & othetwilte ebtaMibhed' fy the <yldmm*{dhafoi of the 9-30-86 10-13-86 .- 10-03-90,7-12-91,4-16-02 (Signature) Michael Keirnan DAS Staff Coordinator. DAS 5 SW (Title)

PJniteb ^tates ®f .America bpartnumt of 'CEransptfrlatton - JJfehcral OLerttftcate SA6090SW-D Limitations and Conditions (con't.)

1. Also eligible on Beech models S35, V35, V35A, and V35B when modified by STC SA1035WE (turbocharged engine) or STC SA5223NM (turbo normalizing system) and any combination of the following STCs: STC SA09074SC (vortex generators), STC SA4-1629 (tip tanks).

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 8988-1, dated 10-13-86 is required and/or later FAA Approved revisions of the above supplement.

3. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 8988, Revision 2, dated 4-16-02 is required for Beech models S35, V35, V35A, and V35B and Beech models S35, V35, V35A, and V35B when modified by STC SA1035WE (turbocharged engine) or STC SA5223NM (turbo normalizing system) and any combination of the following STCs: STC SA09074SC (vortex generators), STC SA4-1629 (tip tanks) or later FAA Approved revisions of the above supplement.

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

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

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) ( Xumter tnJ strut) (Ctty.SWt,, from (Name of grantor) (Print or type) —_—— (Address of grantor) tXumktr tnj tttttt) . Suit, Extent of Authority (if licensing agreement):.

Signature of grantor (In ink):

## Every issue (1)

- April 16, 2002: Amended, Current. [certificate](https://openairdocs.org/files/sha256/d6/20/d6209f5e2f3ace4f98afb48769f08e6dc9d4b2cc976033af6281d29224175e2f)

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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.