# STC SA1782NM - Type: Supplemental type certificate - Status: Current, Amended - Holder: Precise Flight Inc, United States - Description: Installation of Precise speedbrake system. - Applied: September 3, 1982 - Status date: November 7, 2003 - Product: Aircraft, Single-Engine - Certification basis: 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/a7/e4/a7e4f762bf133d8b4598a36e93711c99b3bcf9c6423f3915b26f32b8fcbbf1ac - Approved model list and other attachments: [SA1782NM_AML.pdf](https://openairdocs.org/files/sha256/03/62/03626fc6e4fe7c00b52fd921492ffa947820b27c29482a5688990d0f77a5e9db) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/BCA381BA9D1ED95186256DF9004EC6FE.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA1782NM ## ADs that name it (0) None. ## Approved models (31) - Hawker Beechcraft Corporation 35-33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation 35-A33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation 35-B33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation 35-C33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation 35-C33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation 36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation A36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation A36TC ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation B36TC ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation C35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Hawker Beechcraft Corporation D35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Hawker Beechcraft Corporation E33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation E33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation E33C ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation E35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Hawker Beechcraft Corporation F33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation F33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation F33C ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation F35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Hawker Beechcraft Corporation G33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation G35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Hawker Beechcraft Corporation H35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation J35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation K35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation M35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation N35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation P35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation S35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation V35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation V35A ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker 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. United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate Number SA1782NM This certificate, issued to Precise Flight, Inc. 63354 Powell Butte Road Bend, OR 97701 Part * of the * Regulations. Original ProductType Certificate Number: *See attached FAA Approved Model List (AML) Make: No. SA1782NM for list of approved airplane Model: models and applicable airworthiness regulations. Description of the Type Design Change: Installation of Precise Flight Hydraulic or Electric Speedbrake System in accordance with the provisions of FAA AML No. SA1782NM, dated July 29, 2002, or later FAA approved revision. Limitations and Conditions: Approval of this change in type design applies to the airplane models listed on the AML 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. Aircraft modified per this STC must be operated in accordance with the appropriate Precise Flight, Inc. Airplane Flight Manual Supplement (AFMS), per FAA Approved Model List (AML) No. SA1782NM. A copy of this Certificate, Continuation Sheet, AML, and the appropriate Precise Flight, Inc. AFMS must be maintained as part of the permanent records for the modified aircraft. 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: September 3, 1982 Date reissued: Date of issuance: December 28, 1982 Date amended: 5/24/84; 9/27/84; 9/17/90; 1/31/91; 12/24/91; 7/29/02; 11/7/03 (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) Number SA1782NM Precise Flight, Inc. Reissued: Amended: 5/24/84; 9/27/84; 9/17/90; 1/31/91; 12/24/91; 7/29/02 11/7/03 Limitations and Conditions(cont’d): The conditions and limitations of the original Type Certificate No.’s A-777 and 3A15 apply except as follows: This addendum, which is part of Supplemental Type Certificate No. SA1782NM, prescribes the conditions and limitations under which the STC was issued and meets the airworthiness requirements of the Civil Air Regulations. EQUIPMENT: Beech Owner’s Manual or Pilot’s Operating Handbook and AFMS for the Speedbrake System must be maintained in the airplane at all times. Note 1: Current weight and balance report, including list of equipment in the certified empty weight, must be in the aircraft. Note 2: In addition to the Placards and Markings required by Type Certificate Data Sheets A-777 and 3A15, Note 2, apply the following: a. The following placard is to be located at the circuit breaker panel: **SPEED BRAKE** b. The following placard is to be near the Speedbrake Control Switch: **SPEED BRAKE** c. The following placard is to be placed in front and in full view of the pilot: SPEEDBRAKE EQUIPPED: FOR OPERATING INSTRUCTIONS AND LIMITATIONS - SEE AFM SUPPLEMENT IN OWNER’S MANUAL OR PILOT’S OPERATING HANDBOOK Note 3: With the described Speedbrake System installation, performance will be at least equal to or better than that given in the Owner’s Manual or Pilot’s Operating Handbook for the Piper airplane. - END - **FAA FORM 8110-2- 1 (10-69) PAGE 3 OF 3 PAGES** ### SA1782NM_AML.pdf **FAA APPROVED MODEL LIST (AML) NO. SA1782NM PRECISE FLIGHT, INC.** for SPEEDBRAKE INSTALLATION Issue Date: June 17, 2002 Item Aircraft Make Aircraft Model Original Type Certificate Number Certification Basis for Alteration *FAA Approved Flight Manual Supplement *FAA Approved Drawing ______________________________________________ Number Revision AML Amdt. Date 1 Beech C35, D35, E35, F35, G35 A-777 CAR 3 and Type Certificate A-777 Hydraulic Speedbrakes, dated November 19, 1986 OR Electric Speedbrakes, dated December 24, 1991 Drawing List B33-035-040H and Installation Manual 136 OR Drawing List B33-DL-036 and Installation Manual 136 OR Drawing List B33-DL-026 and Installation Manual 136 OR Drawing List 120S0001 and Drawing List 010S0000 and Drawing List 005S0000 and Installation Manual 08042 Revision -, dated 2/20/85 Revision 10, dated 6/11/87 Revision -, dated 7/19/90 Revision 11, dated 5/15/90 Revision 4, dated 2/5/96 Revision 11, dated 5/15/90 Revision B, dated 9/18/97 Revision V, dated 3/25/02 Revision A, dated 4/26/99 Revision -, dated 12/01/97 IR 2 Beech 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, E33C, F33, F33A, F33C, G33, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, 36, A36, A36TC, B36TC 3A15 CAR 3 and Type Certificate 3A15 PF-02, Revision A, dated July 27, 1999 Drawing List B33-035-040H and Installation Manual 136 OR Drawing List B33-DL-036 and Installation Manual 136 OR Drawing List B33-DL-026 and Installation Manual 136 OR Drawing List 120S0001 and Drawing List 010S0000 and Drawing List 005S0000 and Installation Manual 08042 Revision -, dated 2/20/85 Revision 10, dated 6/11/87 Revision -, dated 7/19/90 Revision 11, dated 5/15/90 Revision 4, dated 2/5/1996 Revision 11, dated 5/15/1990 Revision B, dated 9/18/97 Revision V, dated 3/25/02 Revision A, dated 4/26/99 Revision -, dated 12/01/97 IR * or later FAA Approved Revision Issue Date: _______________________ FAA Approved: ________________________________ Acting Manager, Seattle Aircraft Certification Office Page 1 of 1 ## Every issue (1) - November 7, 2003: Amended, Current. [certificate](https://openairdocs.org/files/sha256/a7/e4/a7e4f762bf133d8b4598a36e93711c99b3bcf9c6423f3915b26f32b8fcbbf1ac), [SA1782NM_AML.pdf](https://openairdocs.org/files/sha256/03/62/03626fc6e4fe7c00b52fd921492ffa947820b27c29482a5688990d0f77a5e9db) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.