# STC SA181SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Signature Flight Support Corporation
- Description: Installation of oxygen system.
- Status date: August 31, 2000
- Data sheets: A-723
- Certificate PDF: https://openairdocs.org/files/sha256/71/36/7136aae97188683eec5ec94125bd36daffda854d9f4cd10c10a84cf9628f36e1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/209B267C9503E54B86257D5600545C67.0001
- Page: https://openairdocs.org/stc/SA181SW

## ADs that name it

None.

## Approved models (1)

- Lockheed Martin Aeronautics Company 18 (TCDS A-723)

## 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.

JSmtfb ^latta t&f of 'tEransporlatton - Ji (E^rttftc&te SA181SW Signature Flight Support Corporation, a Delaware Corporation 7511 Lemmon Avenue, Hangar C Dallas, TX 75209 t&3£&ati,&m 723 Lockheed 18 Civil Air Installation of oxygen system in accordance with Drawing List SD413000-2D dated 4/27/64, or later FAA approved revision.

(See continuation sheet 3 of 3) .-January 15, 1963 January 30, 1963 ; 12/21/98; 8/31/00 '.- June 30, 1982 Rev. 10 / £_i / ' / (Signature) fr S. Frances Cox // Manager, Special Certification Office, Southwest Region (Title) Any flCfrttlon o£ tills certificate by p lifif of rtot i/ig $1,000, or irtpflaennfnt not vxceedin? 3 ysers. or both.

FAA Forn 611D-2(10-68) Page 1 of 3 Thlj ccrtlflc*c* aay b* transferred in tfcc-ordanc* with FAR 21.47.

Peparhnent nf "(SranBpnrtatum - Jljehpral : (Eerttftcate sAieisw Date of Issuance: January 30, 1963 Date Amended: June 30, 1982 Reissuance Date: August 31, 2000 iead- (Continued):

1. A minimum crew of two (2) is required with this system installed.

2. FAA Approved AFM Supplement dated 1/11/63 is required for L-18 aircraft.

3. Placard in accordance with Dwg. SD413019 dated 1/10/63 for non-SR407 is required.

4. FAA Approved AFM Supplement dated 5/19/65 is required for H-250 aircraft-

5. This STC is part of the basic H250 Tri-Gear configuration, and flight manual for that model covers this system.

6. Compatibility of this modification with other previously approved modifications must be determined by the installer.

-END- Any #j terdt.l<?n of this certificate is punishable by a fine of noc exeee41ng $1,000, ar IqprJdanvent not fxcetdlng 3 years, or both* FAA Form 8110-2-1(10-69) Page 3 of 3 Thl* certificate may £# transferred In *acard*nce vjth FAR 21-47.

INSTRUCTIONS: I he transfcrcndorsemcnt below may be used to notify the appropriate FAA Regional Office of [he transfer of this Supplemental Type Certificate.

The FAA will reissue the certificate in the name of the transferee and forward ii to him.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and ifr/el) t City, Stall, and ZIP i from (Name of grantor) (Print or type) (Address of grantor) f Nvmbtr and itrtel) ( Cltf.StaU, and ZIP'<"**> Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

**C FAA AC 69-SS36**

## Every issue (1)

- August 31, 2000: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/71/36/7136aae97188683eec5ec94125bd36daffda854d9f4cd10c10a84cf9628f36e1)

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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.