# STC SA01075SE - Type: Supplemental type certificate - Status: Current, Amended - Holder: Precise Flight Inc - Description: Installation of the Precise Flight, Inc., SpeedBrake 2000 System. - Status date: July 19, 2006 - Data sheets: 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, A-777, A-777, A-777, A-777, A-777, A-777, A-777, A-777, A-777 - Certificate PDF: https://openairdocs.org/files/sha256/14/25/14258edc173e216350b15b055271de400d69bca3b46bb0b1ef58196e1a6c8da6 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F2D58733777B584F862571C3006E06C7.0001 - Page: https://openairdocs.org/stc/SA01075SE ## ADs that name it None. ## Approved models (33) - Raytheon Aircraft Company 35 (TCDS A-777) - Raytheon Aircraft Company 35-33 (TCDS 3A15) - Raytheon Aircraft Company 35-A33 (TCDS 3A15) - Raytheon Aircraft Company 35-B33 (TCDS 3A15) - Raytheon Aircraft Company 35-C33 (TCDS 3A15) - Raytheon Aircraft Company 35-C33A (TCDS 3A15) - Raytheon Aircraft Company 35R (TCDS A-777) - Raytheon Aircraft Company 36 (TCDS 3A15) - Raytheon Aircraft Company A35 (TCDS A-777) - Raytheon Aircraft Company A36 (TCDS 3A15) - Raytheon Aircraft Company A36TC (TCDS 3A15) - Raytheon Aircraft Company B35 (TCDS A-777) - Raytheon Aircraft Company C35 (TCDS A-777) - Raytheon Aircraft Company D35 (TCDS A-777) - Raytheon Aircraft Company E33 (TCDS 3A15) - Raytheon Aircraft Company E33A (TCDS 3A15) - Raytheon Aircraft Company E35 (TCDS A-777) - Raytheon Aircraft Company F33 (TCDS 3A15) - Raytheon Aircraft Company F33A (TCDS 3A15) - Raytheon Aircraft Company F33C (TCDS 3A15) - Raytheon Aircraft Company F35 (TCDS A-777) - Raytheon Aircraft Company G33 (TCDS 3A15) - Raytheon Aircraft Company G35 (TCDS A-777) - Raytheon Aircraft Company H35 (TCDS 3A15) - Raytheon Aircraft Company J35 (TCDS 3A15) - Raytheon Aircraft Company K35 (TCDS 3A15) - Raytheon Aircraft Company M35 (TCDS 3A15) - Raytheon Aircraft Company N35 (TCDS 3A15) - Raytheon Aircraft Company P35 (TCDS 3A15) - Raytheon Aircraft Company S35 (TCDS 3A15) - Raytheon Aircraft Company V35 (TCDS 3A15) - Raytheon Aircraft Company V35A (TCDS 3A15) - Raytheon Aircraft Company V35B (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. United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate Number SA01075SE This certificate, issued to Precise Flight, Inc. 63354 Powell Butte Road Bend, OR 97701 Part 3 of the Civil Air Regulations. Original Product⎯Type Certificate Number: A-777 3A15 Make: Beech Beech Model: A35, B35, C35, D35, 35-33, 35-A33, 35-B33, E35, F35, G35, 35R 35-C33, 35-C33A, E33, E33A, F33, F33A, F33C, G33, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, 36, A36, A36TC Description of the Type Design Change: Installation of the Precise Flight, Inc. SpeedBrake 2000 System. Manufactured in accordance with Precise Flight Engineering Drawing List 010S0000, Revision AD, dated April 27, 2006, or later FAA approved revision. Installed in accordance with Precise Flight, Inc. Engineering Drawing List 121S0000, Revision G, dated May 8, 2006, or later FAA approved revision. Maintained in accordance with Precise Flight, Inc. Instructions for Continued Airworthiness as stated in FAA Approved Aircraft Flight Manual Supplement, dated June 19, 2003, or later FAA approved revision. Limitations and Conditions : This installation requires the installation of the following stall warning STC’s SA177EA or SA361EA, or equivalent for models A35, B35, C35, D35, E35, F35, G35, and 35R. Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate and FAA approved Airplane Flight Manual Supplement (AFMS) 121SMAN0001, Revision A, dated June 19, 2003, or later FAA approved revision, must be maintained as part of the permanent records for the modified airplane. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. Date of application: October 30, 2001 Date reissued: Date of issuance: April 25, 2002 Date amended: 5/24/02; 1/24/03; 6/19/03; 11/7/03 7/19/06 (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ## Every issue (1) - July 19, 2006: Amended, Current. [certificate](https://openairdocs.org/files/sha256/14/25/14258edc173e216350b15b055271de400d69bca3b46bb0b1ef58196e1a6c8da6) --- 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.