# STC SA1775GL

- Type: Supplemental type certificate
- Status: Current, Surrendered
- Holder: ABX Air Incorporated, United States
- Description: Incorporate maximum permissible quick turn-around landing weight (flaps 35º)
- Applied: June 30, 1992
- Status date: December 2, 2014
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 4A25](https://openairdocs.org/tcds/4A25)
- Certificate PDF: https://openairdocs.org/files/sha256/d3/d2/d3d2496e56089a855d050c7b6a250aa2a0cc6e22f0e387f90eac8c3aa8379dcd
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D2C761E4A7A471D386257DC60073BA8E.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1775GL

## ADs that name it (0)

None.

## Approved models (4)

- The Boeing Company DC-8-62 ([TCDS 4A25](https://openairdocs.org/tcds/4A25))
- The Boeing Company DC-8-62F ([TCDS 4A25](https://openairdocs.org/tcds/4A25))
- The Boeing Company DC-8-63 ([TCDS 4A25](https://openairdocs.org/tcds/4A25))
- The Boeing Company DC-8-63F ([TCDS 4A25](https://openairdocs.org/tcds/4A25))

## What the certificate says

The certificate is a scan without a text layer; open the PDF to read it.

## Every issue (1)

- December 2, 2014: Surrendered, Current. [certificate](https://openairdocs.org/files/sha256/d3/d2/d3d2496e56089a855d050c7b6a250aa2a0cc6e22f0e387f90eac8c3aa8379dcd)

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