# STC SA915SW

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Bendix Corporation
- Description: Installation of Bendix P/N 19E138-2A flexible drive shaft in lieu of Dana P/N 26567 universal joint shaft on Pratt & Whitney Model JT3D-1 engine gear box and CSD.
- Status date: October 1, 1971
- Data sheets: 4A25, 4A25, 4A25, 4A25, 4A25, 4A25, 4A25, 4A25, 4A25, 4A25, 4A25, 4A25, 4A25
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/BBB7F772F4749B7E85256CC20058EA52.0001
- Page: https://openairdocs.org/stc/SA915SW

## ADs that name it

None.

## Approved models (13)

- McDonnell Douglas Corporation DC-8-21 (TCDS 4A25)
- McDonnell Douglas Corporation DC-8-31 (TCDS 4A25)
- McDonnell Douglas Corporation DC-8-32 (TCDS 4A25)
- McDonnell Douglas Corporation DC-8-33 (TCDS 4A25)
- McDonnell Douglas Corporation DC-8-41 (TCDS 4A25)
- McDonnell Douglas Corporation DC-8-42 (TCDS 4A25)
- McDonnell Douglas Corporation DC-8-43 (TCDS 4A25)
- McDonnell Douglas Corporation DC-8-51 (TCDS 4A25)
- McDonnell Douglas Corporation DC-8-52 (TCDS 4A25)
- McDonnell Douglas Corporation DC-8-53 (TCDS 4A25)
- McDonnell Douglas Corporation DC-8-55 (TCDS 4A25)
- McDonnell Douglas Corporation DC-8F-54 (TCDS 4A25)
- McDonnell Douglas Corporation DC-8F-55 (TCDS 4A25)

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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.