# STC SA4410SW

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Frakes Aviation, Inc, United States
- Description: Installation of 17 passenger configuration, seats, emergency exit, and floor modification.
- Applied: October 2, 1979
- Status date: December 10, 1984
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A-783](https://openairdocs.org/tcds/A-783)
- Certificate PDF: https://openairdocs.org/files/sha256/d2/d8/d2d83fc668b8648a22cb78b9e3d5d56f92c5ad1a7454c2aa7d8e1ab6c1299243
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2E9BFE3319701E0685256CC2000E3C4F.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA4410SW

## ADs that name it (0)

None.

## Approved models (1)

- Frakes Aviation G-73 ([TCDS A-783](https://openairdocs.org/tcds/A-783))

## 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.

ttnitrd .Starts of amrrita Bcpartmcnt of Transportation— Jpedcral 3toiation administration Supplemental t^pe Certificate SA4410SW T6931SW-D RAD-190 Aviation Route 3, Box 229-B Cleburne, Texas 76031 (!jr*a*rva/ Jvvctut/ —— • ^^Jfoj&6lc>u>t>n^ />*aMj/>^ni*n&4&iSMrJ L^ j^J/ie, Civil Air A— 783 Frakes Gulfatream American 6-73 Installation of 17 passenger configuration, seats, emergency exit, and floor modification according to Drawing List FA-5000-A, revised 5/11/81, or later FAA approved revision.

See Continuation Sheet October 2, 1979 July 6, 1981 So!cvrrivn*&&<a/&p'jpJ<n4' 12/10/84 Lsion 1 P. Wati Manager, Aircraft Certification Division Southwest Region (Title)

FAA Font tl 10-2 (10-68)

United £tatts of America Bcpartment of transportation—federal atriation administration Supplemental Itjipe Certificate(Continuation Sheet) SA4410SW Revision I Limitations and Conditions:

1. STC SA2323WE must be incorporated with this STC.

2. Flight operation is limited to Day VFR only. Day VFR limitation does not apply if aircraft has been modified to include an emergency interior lighting system according to Drawings FA5217, Revision A dated 11/27/84, FA5224 dated 8/28/84, FA5230 dated 12/5/84, and FA5142, Revision A dated 12/4/84, or later FAA approved revisions.

3. FAA Approved Airplane Flight Manual Supplement dated July 6, 1981, revised October 26, 1984, is required when emergency interior lighting system is not installed.

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

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

: AA F:ORM eno-2-1 (1O-69) This ceriijkate may be transferred in accordance with l:AR L'l.-f?

**PAGE 2 OF 2PAGES**

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 %IP code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (1)

- December 10, 1984: Amended, Current. [certificate](https://openairdocs.org/files/sha256/d2/d8/d2d83fc668b8648a22cb78b9e3d5d56f92c5ad1a7454c2aa7d8e1ab6c1299243)

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