# STC SA2310SW

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Braniff Airways, Inc
- Description: Installation of wheel and brake advisory system.
- Status date: May 17, 1976
- Data sheets: 4A25
- Certificate PDF: https://openairdocs.org/files/sha256/8f/26/8f26f9413896102eaf3ab89f0732443bbd046024093bee5e6ad96a2bb2fb0317
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7E7831C5C4735DF685256CC200015C6C.0001
- Page: https://openairdocs.org/stc/SA2310SW

## ADs that name it

None.

## Approved models (1)

- The Boeing Company DC-8-62 (TCDS 4A25)

## 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.

Hmtri £nta of Starta ©tpartmcnt of transportation — Jftdtral Situation administration Supplemental TCpe Certificate iSUtmw*' SA2310SH Project T3411SW-S

• JDL-213 Eraniff Airways, Incorporated P. 0. Box 35001 Dallas, Texas 75235 rfr<ifi<A M Jn*<i^6tr^^AAfr^^dA*^j>n'rti^&&t.ait^xfi^i^ 4b ^*54c/ Civil Air ^/Ifafttti&ttnA 4A25 FcDonnell Douglas DC-8-62 Installation of wheel and brake advisory system according to Braniff Engineering Authorizations 6-32-41, I<ev. 2 dated 5/7/76, and 6-32-42S dated 4/20/76, or later FAA approved revision.

FAA Approved Airplane Flight Manual Supplement dated May 17, 1976, Is required, u,t, • March 3, 1976 9 May 17, 1976 ^ ;% (Signature ) Don ?. Watson Chief, Engineering and Manufacturing Branch alteration of this certificate is punishable by a fine of not exceeding H,000, or imprisonment not exceeding 3years, ^ This cirltficatt may bi Iraiuferred in accordance with FAR 21.47.

FAA fou II 10-1110-tt) .

## Every issue (1)

- May 17, 1976: Issued, Current. [certificate](https://openairdocs.org/files/sha256/8f/26/8f26f9413896102eaf3ab89f0732443bbd046024093bee5e6ad96a2bb2fb0317)

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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.