# STC SA269WE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Brittain Industries, Inc, United States - Description: Installation of Brittain/Beech Pneumatic Pitch Assist Model PC-1 - Applied: October 29, 1962 - Status date: November 19, 2013 - Product: Aircraft, Small Airplane - Certification basis: Part 3, Part 21 - Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15), [TCDS A-777](https://openairdocs.org/tcds/A-777) - Certificate PDF: https://openairdocs.org/files/sha256/e7/dd/e7ddb6191805fbf8f155ed8cb2473f33c1319d1917567debe0b6b2e1a1fb5055 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D2A308AB592CA5B486257DCB00520788.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA269WE ## ADs that name it (0) None. ## Approved models (24) - Beechcraft Corporation 35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Beechcraft Corporation 35-33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Beechcraft Corporation 35-A33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Beechcraft Corporation 35-B33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Beechcraft Corporation 35-C33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Beechcraft Corporation 35-C33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Beechcraft Corporation 35R ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Beechcraft Corporation A35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Beechcraft Corporation B35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Beechcraft Corporation C35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Beechcraft Corporation D35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Beechcraft Corporation E35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Beechcraft Corporation F35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Beechcraft Corporation G35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Beechcraft Corporation H35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Beechcraft Corporation J35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Beechcraft Corporation K35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Beechcraft Corporation M35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Beechcraft Corporation N35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Beechcraft Corporation P35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Beechcraft Corporation S35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Beechcraft Corporation V35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Beechcraft Corporation V35A ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Beechcraft Corporation V35B ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) ## 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. Number SA269WE This certificate issued to: Brittain Industries, Inc. 3266 N. Sheridan Road Tulsa, Oklahoma 74115 Part 3of the Civil Air Regulations. Original Product – Type Certificate Number: 777, 3A15 Make: Beech Model: 35 Series see Limitations and Conditions Description of Type Design Change: Installation of Brittain/Beech Pneumatic Pitch Assist Model PC-1 in accordance with Brittain Industries, Inc. Installation Manual 11905-3 and Altitude Hold Model AH-1 (Optional Installation) in accordance with Brittain Industries, Inc. Installation Manual 11905-5 and Drawings No. 11393 and 11398. Brittain/Beechcraft Autopilot per STC SA4-1260 or SA136WE (P35 Only) or Tactair Model B101 Autopilot (Brittain Industries, Inc. Installaiton Instructions No. 11905-3-TI) is required with this installation. Date of application: October 29, 1962 Date reissued: November 19, 2013; 12/21/62; 2/4/63; 2/27/63; 9/20/63; 11/10/64; 11/10/69; 11/2/72 Revision 7 Date of issuance: December 13, 1962 Date amended: Signature S. Frances Cox Title Manager, Special Certification Office, Southwest Region FAA Form 8110-2 (8/13) Page 1 Number: SA269WE Date of Issuance: December 13, 1962 Reissuance Date: November 19, 2013 Applicable eligible aircraft models and FAA approved Airplane Flight Manual Supplements listed on sealed Master Drawing List DP-20 and DP-20-TI or later FAA approved revision. The installer must determine whether this design change is compatible with previously approved modifications. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission. -END- FAA Form 8110-2 (8/13) Page 3 **SUPPLEMENTAL TYPE CERTIFICATE, FAA FORM 8110-2 (CONTINUED)** To (Name of transferee) (Address of transferee) (Number and street) (City, State, and ZIP Code) From (Name of grantor) (Address of grantor) (Number and street) (City, State, and ZIP Code) FAA Form 8110-2 (8/13) Page 2 ## Every issue (1) - November 19, 2013: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/e7/dd/e7ddb6191805fbf8f155ed8cb2473f33c1319d1917567debe0b6b2e1a1fb5055) --- From OpenAirDocs.org, an independent open copy of FAA and NTSB data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.