# STC SA01474AT

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Corporate Flight Management, Inc., United States
- Description: Install actuator links for existing oil cooper flap.
- Status date: March 18, 1998
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A21EU](https://openairdocs.org/tcds/A21EU), [TCDS A56EU](https://openairdocs.org/tcds/A56EU)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0CDB8CA446C1264285256CC1007F3868.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01474AT

## ADs that name it (0)

None.

## Approved models (2)

- British Aerospace (Scotland) HP Jetstream Model 3101 ([TCDS A21EU](https://openairdocs.org/tcds/A21EU))
- British Aerospace (Scotland) Jetstream Model 3201 ([TCDS A56EU](https://openairdocs.org/tcds/A56EU))

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