# STC SA2160NM - Type: Supplemental type certificate - Status: Current, Amended - Holder: Precise Flight Inc, United States - Description: Installation of the Precise Flight stand-by vacuum system (SVS). - Applied: October 31, 1983 - Status date: November 7, 2003 - Product: Aircraft, Single-Engine - Certification basis: Part 3, Part 21, Part 23 - Data sheets: [TCDS A1CE](https://openairdocs.org/tcds/A1CE), [TCDS 3A15](https://openairdocs.org/tcds/3A15), [TCDS A-777](https://openairdocs.org/tcds/A-777), [TCDS 5A3](https://openairdocs.org/tcds/5A3), [TCDS A30CE](https://openairdocs.org/tcds/A30CE) - Certificate PDF: https://openairdocs.org/files/sha256/f6/31/f631e04eef1cfbee20ea5d8e8f8d18f507f0469a46be7f0fcff02194be8c7bd3 - Approved model list and other attachments: [SA2160NM AML .pdf](https://openairdocs.org/files/sha256/2f/6b/2f6b3559796c60c99c7e4aa1ed384f5aef5aad0c3c42371718eee2642f31f1fb) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/38390E1F54C652CA86256DF900505EB3.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA2160NM ## ADs that name it (2) - [AD 2005-11-05](https://openairdocs.org/ad/2005-11-05): Standby vacuum systems (SVS) · Precise Flight Vacuum Systems. Effective Jul 18, 2005. Cited in the text - [AD 99-24-10](https://openairdocs.org/ad/99-24-10): Standby Vacuum Systems · Precise Flight Vacuum Systems. Effective Jan 14, 2000. Named in the applicability ## Approved models (53, first 50) - Hawker Beechcraft Corporation 19A ([TCDS A1CE](https://openairdocs.org/tcds/A1CE)) - Hawker Beechcraft Corporation 23 ([TCDS A1CE](https://openairdocs.org/tcds/A1CE)) - Hawker Beechcraft Corporation 35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - 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 35R ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Hawker Beechcraft Corporation 36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation 45 (Military YT-34) ([TCDS 5A3](https://openairdocs.org/tcds/5A3)) - Hawker Beechcraft Corporation 77 ([TCDS A30CE](https://openairdocs.org/tcds/A30CE)) - Hawker Beechcraft Corporation A23 ([TCDS A1CE](https://openairdocs.org/tcds/A1CE)) - Hawker Beechcraft Corporation A23-19 ([TCDS A1CE](https://openairdocs.org/tcds/A1CE)) - Hawker Beechcraft Corporation A23-24 ([TCDS A1CE](https://openairdocs.org/tcds/A1CE)) - Hawker Beechcraft Corporation A23A ([TCDS A1CE](https://openairdocs.org/tcds/A1CE)) - Hawker Beechcraft Corporation A24 ([TCDS A1CE](https://openairdocs.org/tcds/A1CE)) - Hawker Beechcraft Corporation A24R ([TCDS A1CE](https://openairdocs.org/tcds/A1CE)) - Hawker Beechcraft Corporation A35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - 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 A45 (Military T-34A; B-45) ([TCDS 5A3](https://openairdocs.org/tcds/5A3)) - Hawker Beechcraft Corporation B19 ([TCDS A1CE](https://openairdocs.org/tcds/A1CE)) - Hawker Beechcraft Corporation B23 ([TCDS A1CE](https://openairdocs.org/tcds/A1CE)) - Hawker Beechcraft Corporation B24R ([TCDS A1CE](https://openairdocs.org/tcds/A1CE)) - Hawker Beechcraft Corporation B35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Hawker Beechcraft Corporation B36TC ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation C23 ([TCDS A1CE](https://openairdocs.org/tcds/A1CE)) - Hawker Beechcraft Corporation C24R ([TCDS A1CE](https://openairdocs.org/tcds/A1CE)) - 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 D45 (Military T-34B) ([TCDS 5A3](https://openairdocs.org/tcds/5A3)) - 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 M19A ([TCDS A1CE](https://openairdocs.org/tcds/A1CE)) - 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)) All 53: https://openairdocs.org/stc/SA2160NM/models.md ## 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 SA2160NM 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. SA2160NM for list of approved airplane models Model: and applicable airworthiness regulations Description of the Type Design Change: Installation of Precise Flight, Inc. Stand-By Vacuum System (SVS) in accordance with the appropriate Precise Flight, Inc. Engineering Drawing listed on FAA Approved Model List No. SA2160NM, dated April 28, 2000, or later FAA approved revision. NOTE: As a prerequisite to this change, the engine must be modified in accordance with Precise Flight, Inc. STC No. SE1779NM or SE1780NM, dated April 21, 2000, or later FAA approved revision. Also, modified aircraft must be equipped with a vacuum indicator. Limitations and Conditions: 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 by the installer 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, AML No. SA2160NM and the appropriate FAA Approved Flight Manual Supplement (AFMS) listed on AML No. SA2160NM 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: October 31, 1983 Date reissued: Date of issuance: November 7, 1983 Date amended: 12/16/83; 12/7/84; 4/28/00; 11/7/03 (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ### SA2160NM AML .pdf **FAA APPROVED MODEL LIST (AML) NO. SA2160NM PRECISE FLIGHT, INC.** For INSTALLATION OF PRECISE FLIGHT STANDBY VACUUM SYSTEM Issue Date: October 31, 1989 Item Aircraft Make Aircraft Model Original Type Certificate Number Certification Basis for Alteration FAA Approved Airplane Flight Manual Supplement* FAA Approved Drawing* ____________________________________________ Number REV AML Amdt. Date 1 Beech Aircraft Corp. 23, A23, A23A, A23-19, 19A, B19, M19A, A23- 24, B23, C23, A24, A24R, B24R, C24R A1CE CAR Part 3 Supplemental Flight Manual for SA2160NM dated 8/11/99. (SVS III) SVS III Engineering Drawing 000V0000 And Installation Report No. 50050 Rev.-, dated 3/10/2000 Rev. 25, dated 8/26/99 4/28/2000 2 Beech Aircraft Corp. 23, A23, A23A, A23-19, 19A, B19, M19A, A23- 24, B23, C23, A24, A24R, B24R, C24R A1CE CAR Part 3 Supplemental Flight Manual for Push Operated Cable Valve dated 2/4/2000. (SVS V) OR Supplemental Flight Manual for Pull Operated Cable Valve dated 2/4/2000. (SVS V) SVS V Engineering Drawing 000V0000 And Installation Report No. 08072 Rev.-, dated 3/10/2000 Rev.-, dated 12/22/1999 4/28/2000 3 Beech Aircraft Corp. 35, A35, B35, C35, D35, E35, F35, G35, 35R 777 CAR Part 3 Supplemental Flight Manual for SA2160NM dated 8/11/99. (SVS III) SVS III Engineering Drawing 000V0000 And Installation Report No. 50050 Rev.-, dated 3/10/2000 Rev. 25, dated 8/26/99 4/28/2000 4 Beech Aircraft Corp. 35, A35, B35, C35, D35, E35, F35, G35, 35R 777 CAR Part 3 Supplemental Flight Manual for Push Operated Cable Valve dated 2/4/2000. (SVS V) OR Supplemental Flight Manual for Pull Operated Cable Valve dated 2/4/2000. (SVS V) SVS V Engineering Drawing 000V0000 And Installation Report No. 08072 Rev.-, dated 3/10/2000 Rev.-, dated 12/22/1999 4/11/2000 * or later FAA Approved Revision Page 1 of 3 FAA APPROVED MODEL LIST (AML) NO. SA2160NM **PRECISE FLIGHT, INC.** For INSTALLATION OF PRECISE FLIGHT STANDBY VACUUM SYSTEM Issue Date: October 31, 1989 Item Aircraft Make Aircraft Model Original Type Certificate Number Certification Basis for Alteration FAA Approved Airplane Flight Manual Supplement* FAA Approved Drawing* ____________________________________________ Number REV AML Amdt. Date 5 Beech Aircraft Corp. H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, E33C, F33, F33A, F33C, G33, 36, A36, A36TC, B36TC 3A15 CAR Part 3 Supplemental Flight Manual for SA2160NM dated 8/11/99. (SVS III) SVS III Engineering Drawing 000V0000 And Installation Report No. 50050 Rev.-, dated 3/10/2000 Rev. 25, dated 8/26/99 4/28/2000 6 Beech Aircraft Corp. H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, E33C, F33, F33A, F33C, G33, 36, A36, A36TC, B36TC 3A15 CAR Part 3 Supplemental Flight Manual for Push Operated Cable Valve dated 2/4/2000. (SVS V) OR Supplemental Flight Manual for Pull Operated Cable Valve dated 2/4/2000. (SVS V) SVS V Engineering Drawing 000V0000 And Installation Report No. 08072 Rev.-, dated 3/10/2000 Rev.-, dated 12/22/1999 4/28/2000 * or later FAA Approved Revision Page 2 of 3 FAA APPROVED MODEL LIST (AML) NO. SA2160NM PRECISE FLIGHT, INC. For INSTALLATION OF PRECISE FLIGHT STANDBY VACUUM SYSTEM Issue Date: October 31, 1989 Item Aircraft Make Aircraft Model Original Type Certificate Number Certification Basis for Alteration FAA Approved Airplane Flight Manual Supplement* FAA Approved Drawing* ____________________________________________ Number REV AML Amdt. Date 7 Beech Aircraft Corp. 4S(YT-34), A45(T034A, B045), D45 (T-34B) 5A3 CAR Part 3 Supplemental Flight Manual for SA2160NM dated 8/11/99. (SVS III) SVS III Engineering Drawing 000V0000 And Installation Report No. 50050 Rev.-, dated 3/10/2000 Rev. 25, dated 8/26/99 4/28/2000 8 Beech Aircraft Corp. 4S(YT-34), A45(T034A, B045), D45 (T-34B) 5A3 CAR Part 3 Supplemental Flight Manual for Push Operated Cable Valve dated 2/4/2000. (SVS V) OR Supplemental Flight Manual for Pull Operated Cable Valve dated 2/4/2000. (SVS V) SVS V Engineering Drawing 000V0000 And Installation Report No. 08072 Rev.-, dated 3/10/2000 Rev.-, dated 12/22/1999 4/28/2000 9 Beech Aircraft Corp. 77 Series A29CE-2 Part 23 Supplemental Flight Manual for SA2160NM dated 8/11/99. (SVS III) SVS III Engineering Drawing 000V0000 And Installation Report No. 50050 Rev.-, dated 3/10/2000 Rev. 25, dated 8/26/99 4/28/2000 10 Beech Aircraft Corp. 77 Series A29CE-2 Part 23 Supplemental Flight Manual for Push Operated Cable Valve dated 2/4/2000. (SVS V) OR Supplemental Flight Manual for Pull Operated Cable Valve dated 2/4/2000. (SVS V) SVS V Engineering Drawing 000V0000 And Installation Report No. 08072 Rev.-, dated 3/10/2000 Rev.-, dated 12/22/1999 4/28/2000 * or later FAA Approved Revision FAA Approved: ________________________________ Acting Manager, Seattle Aircraft C e r t i f i c a t i o n O f f i c e Amended: _April 28, 2000 _ Page 3 of 3 ## Every issue (1) - November 7, 2003: Amended, Current. [certificate](https://openairdocs.org/files/sha256/f6/31/f631e04eef1cfbee20ea5d8e8f8d18f507f0469a46be7f0fcff02194be8c7bd3), [SA2160NM AML .pdf](https://openairdocs.org/files/sha256/2f/6b/2f6b3559796c60c99c7e4aa1ed384f5aef5aad0c3c42371718eee2642f31f1fb) --- 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.