# STC SA1992SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Air Freighters Intl Inc, United States
- Description: Installation of Aft cargo door between F.S. 549 and 658 between floorline and stringer 26 and associated modification
- Applied: February 3, 1975
- Status date: February 20, 1980
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A-793](https://openairdocs.org/tcds/A-793)
- Certificate PDF: https://openairdocs.org/files/sha256/e0/9e/e09e7ee36bbffaff6cb5b861549d69dd15192f7015abbf31a381bd388d899257
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0F29ADD25D83EDC486257D7A0066E558.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1992SW

## ADs that name it (0)

None.

## Approved models (1)

- Kelowna Flightcraft R & D Ltd. 240 Series ([TCDS A-793](https://openairdocs.org/tcds/A-793))

## 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.

Urartd Starts or ©tpartmcnt of Transportation -Jpedtral atriatton administration Supplemental 'Cgpe Certificate *SMMn>V€4t' SA1992SW Air Freighters International P. 0. Box 2 15808 Addiaon Road Addlson, Texas 75001 4b

•Jt&a*eta&&r Civil Air 793 General Dynamics /Convalr 600(240D), and 240 Series Inatallatlon of Aft Cargo Door between FS 549 and 658 between floorllne and stringer 26 and associated modification according to Data List Report 75-3 through Revision "A" dated 6/15/79 or later FAA approved revision.

1. The Presaurization System must be completely removed.

2. An approved cargo restraint system is not included with this STC.

3. FAA approved Airplane Flight Manual Supplement dated June 6, 1975, is required for the Model 600(240D).4. FAA approved Airplane Flight Manual Supplement dated February 20, 1980, is required for the Model 24Q Series. ... - , ..... ... _5. Compatibility of this modification with other previously approved modifications must be determined by the installer.

'^^ w February 3, 1973 D* iy/5 a/f si ff r Don P. WatsonChief, Engineering and Manufacturing Branch ^_ (7 "It!

FA* Fou 8110-2 (10-48)

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) : t"tbe7 and street) ICtty, Stall, and £IP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and strret) , Stall, ana ?JP ,odt/ Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

**C FAA AC 69-5536**

## Every issue (1)

- February 20, 1980: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/e0/9e/e09e7ee36bbffaff6cb5b861549d69dd15192f7015abbf31a381bd388d899257)

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