# STC SE1779NM - Type: Supplemental type certificate - Status: Current, Amended - Holder: Precise Flight Inc, United States - Description: Installation of Precise Flight, Inc. Standby Vacuum System SVS III - Applied: December 13, 1982 - Status date: November 7, 2003 - Product: Engine - Certification basis: Part 21 - Data sheets: [TCDS 1E10](https://openairdocs.org/tcds/1E10), [TCDS E-228](https://openairdocs.org/tcds/E-228), [TCDS E-275](https://openairdocs.org/tcds/E-275), [TCDS E-276](https://openairdocs.org/tcds/E-276), [TCDS E-284](https://openairdocs.org/tcds/E-284), [TCDS 1E11](https://openairdocs.org/tcds/1E11), [TCDS 1E7](https://openairdocs.org/tcds/1E7), [TCDS 1E12](https://openairdocs.org/tcds/1E12), [TCDS 1E4](https://openairdocs.org/tcds/1E4), [TCDS E-286](https://openairdocs.org/tcds/E-286), [TCDS E14EA](https://openairdocs.org/tcds/E14EA), [TCDS E26EA](https://openairdocs.org/tcds/E26EA), [TCDS E-223](https://openairdocs.org/tcds/E-223), [TCDS E-274](https://openairdocs.org/tcds/E-274), [TCDS E-277](https://openairdocs.org/tcds/E-277), [TCDS E-295](https://openairdocs.org/tcds/E-295), [TCDS E-285](https://openairdocs.org/tcds/E-285), [TCDS E19EA](https://openairdocs.org/tcds/E19EA), [TCDS E16EA](https://openairdocs.org/tcds/E16EA), [TCDS E10EA](https://openairdocs.org/tcds/E10EA) and 5 more - Certificate PDF: https://openairdocs.org/files/sha256/9e/39/9e399b9c8a614d1714255271c678107576db8304a48d68ce5d54c6feb1208978 - Approved model list and other attachments: [SE1779NM_AML.pdf](https://openairdocs.org/files/sha256/59/fb/59fb0c9b51c34540aa3929bba28c12cddf9ff8fa8ca6caf1f13dcf8155834a19) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A7ECC72F6023B8C086256DF9004DA5A8.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SE1779NM ## ADs that name it (1) - [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 ## Approved models (575, first 50) - Lycoming Engines AEIO-360-A1A ([TCDS 1E10](https://openairdocs.org/tcds/1E10)) - Lycoming Engines AEIO-360-A1B ([TCDS 1E10](https://openairdocs.org/tcds/1E10)) - Lycoming Engines AEIO-360-A1B6 ([TCDS 1E10](https://openairdocs.org/tcds/1E10)) - Lycoming Engines AEIO-360-A1C ([TCDS 1E10](https://openairdocs.org/tcds/1E10)) - Lycoming Engines AEIO-360-A1D ([TCDS 1E10](https://openairdocs.org/tcds/1E10)) - Lycoming Engines AEIO-360-A1E ([TCDS 1E10](https://openairdocs.org/tcds/1E10)) - Lycoming Engines AEIO-360-A1E6 ([TCDS 1E10](https://openairdocs.org/tcds/1E10)) - Lycoming Engines AEIO-360-A2A ([TCDS 1E10](https://openairdocs.org/tcds/1E10)) - Lycoming Engines AEIO-360-A2B ([TCDS 1E10](https://openairdocs.org/tcds/1E10)) - Lycoming Engines AEIO-360-A2C ([TCDS 1E10](https://openairdocs.org/tcds/1E10)) - Lycoming Engines AEIO-360-B1B ([TCDS 1E10](https://openairdocs.org/tcds/1E10)) - Lycoming Engines AEIO-360-B1D ([TCDS 1E10](https://openairdocs.org/tcds/1E10)) - Lycoming Engines AEIO-360-B1F ([TCDS 1E10](https://openairdocs.org/tcds/1E10)) - Lycoming Engines AEIO-360-B1F6 ([TCDS 1E10](https://openairdocs.org/tcds/1E10)) - Lycoming Engines AEIO-360-B1G6 ([TCDS 1E10](https://openairdocs.org/tcds/1E10)) - Lycoming Engines AEIO-360-B1H ([TCDS 1E10](https://openairdocs.org/tcds/1E10)) - Lycoming Engines AEIO-360-B2F ([TCDS 1E10](https://openairdocs.org/tcds/1E10)) - Lycoming Engines AEIO-360-B2F6 ([TCDS 1E10](https://openairdocs.org/tcds/1E10)) - Lycoming Engines AEIO-360-B4A ([TCDS 1E10](https://openairdocs.org/tcds/1E10)) - Lycoming Engines AEIO-360-H1A ([TCDS 1E10](https://openairdocs.org/tcds/1E10)) - Lycoming Engines AEIO-360-H1B ([TCDS 1E10](https://openairdocs.org/tcds/1E10)) - Lycoming Engines GO-435 ([TCDS E-228](https://openairdocs.org/tcds/E-228)) - Lycoming Engines GO-435-C2 (O-435-17) ([TCDS E-228](https://openairdocs.org/tcds/E-228)) - Lycoming Engines GO-435-C2A ([TCDS E-228](https://openairdocs.org/tcds/E-228)) - Lycoming Engines GO-435-C2A2 ([TCDS E-228](https://openairdocs.org/tcds/E-228)) - Lycoming Engines GO-435-C2B ([TCDS E-228](https://openairdocs.org/tcds/E-228)) - Lycoming Engines GO-435-C2B1 ([TCDS E-228](https://openairdocs.org/tcds/E-228)) - Lycoming Engines GO-435-C2B2 ([TCDS E-228](https://openairdocs.org/tcds/E-228)) - Lycoming Engines GO-435-C2C ([TCDS E-228](https://openairdocs.org/tcds/E-228)) - Lycoming Engines GO-435-C2D ([TCDS E-228](https://openairdocs.org/tcds/E-228)) - Lycoming Engines GO-435-C2E ([TCDS E-228](https://openairdocs.org/tcds/E-228)) - Lycoming Engines GO-435-D1 ([TCDS E-228](https://openairdocs.org/tcds/E-228)) - Lycoming Engines GO-480 ([TCDS E-275](https://openairdocs.org/tcds/E-275)) - Lycoming Engines GO-480-A1A ([TCDS E-275](https://openairdocs.org/tcds/E-275)) - Lycoming Engines GO-480-B ([TCDS E-275](https://openairdocs.org/tcds/E-275)) - Lycoming Engines GO-480-B1 ([TCDS E-275](https://openairdocs.org/tcds/E-275)) - Lycoming Engines GO-480-B1A6 ([TCDS E-275](https://openairdocs.org/tcds/E-275)) - Lycoming Engines GO-480-B1B ([TCDS E-275](https://openairdocs.org/tcds/E-275)) - Lycoming Engines GO-480-B1C ([TCDS E-275](https://openairdocs.org/tcds/E-275)) - Lycoming Engines GO-480-B1D ([TCDS E-275](https://openairdocs.org/tcds/E-275)) - Lycoming Engines GO-480-C1B6 ([TCDS E-275](https://openairdocs.org/tcds/E-275)) - Lycoming Engines GO-480-C1D6 ([TCDS E-275](https://openairdocs.org/tcds/E-275)) - Lycoming Engines GO-480-C2C6 ([TCDS E-275](https://openairdocs.org/tcds/E-275)) - Lycoming Engines GO-480-C2D6 ([TCDS E-275](https://openairdocs.org/tcds/E-275)) - Lycoming Engines GO-480-C2E6 ([TCDS E-275](https://openairdocs.org/tcds/E-275)) - Lycoming Engines GO-480-C3A6 ([TCDS E-275](https://openairdocs.org/tcds/E-275)) - Lycoming Engines GO-480-D1A ([TCDS E-275](https://openairdocs.org/tcds/E-275)) - Lycoming Engines GO-480-E1A6 ([TCDS E-275](https://openairdocs.org/tcds/E-275)) - Lycoming Engines GO-480-F1A6 ([TCDS E-275](https://openairdocs.org/tcds/E-275)) - Lycoming Engines GO-480-F2A6 ([TCDS E-275](https://openairdocs.org/tcds/E-275)) All 575: https://openairdocs.org/stc/SE1779NM/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 SE1779NM 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. SE1779NM for list of approved airplane models Model: and applicable airworthiness regulations Description of the Type Design Change: Installation of Precise Flight, Inc. Standby Vacuum System SVS III, in accordance with Engineering Drawing 000V0000, Revision -, dated March 10, 2000, and Installation Report No. 50050, Revision 25, dated August 26, 1999, or later approved revision. Or Installation of Precise Flight, Inc. SVS V, in accordance with Precise Flight, Inc. Engineering Drawing 000V0000, Revision -, dated March 10, 2000 and Installation Instructions 08072, Revision -, dated December 12, 1999, or later FAA approved revision. 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, Continuation Sheet, and FAA approved AML No. SE1779NM, dated December 30, 1983, or later FAA approved revision, 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. (See Continuation Sheet Page 3) This certificate and the supporting data which is the ba sis for approval shall remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration. Date of application: December 13, 1982 Date reissued: Date of issuance: December 28, 1982 Date amended: 12/30/83; 1/31/85; 7/25/90; 1/31/91; 4/21/00; 11/7/03 (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) Number SE1779NM Precise Flight, Inc. Reissued: Amended: 12/30/83; 1/31/85; 7/25/90; 1/31/91; 4/21/00; 11/4/03 Limitations and Conditions: (cont’d) The conditions and limitations of Type Certificate Data sheet as listed in the attached AML apply except where superseded by the following: This Supplemental Type Certificate Data Sheet, which is part of STC SE1779NM, prescribes the conditions and limitations under which the product for which the STC was issued meets the airworthiness requirements of the Federal Aviation Regulations: Engines Lycoming Fuel: See Type Certificate Data Sheet Engine Limits: See Type Certificate Data Sheet Placards: Placards and Operating Limits on appropriate Type Certificate Data Sheet apply except as noted herein: The following placard is mandatory on aircraft that are required to have POH/AFM's and must be located near instrument suction gauge in full view of the pilot. NOTE: This STC covers modification of the engine only. Installation of this system in an aircraft requires aircraft installations approval and associated Airplane Flight Manual and Pilot Operating Handbook Supplement for the installation. For those airplanes which do not have an AFM/POH, the placards provided in each Precise Flight, Inc. Installation Kit must be installed with the modification. - END - FAA FORM 8110-2- 1 (10-69) PAGE 3 OF 3 PAGES STANDBY VACUUM SYSTEM: FOR OPERATING INSTRUCTIONS AND LIMITATIONS SEE SUPPLEMENT IN OWNER’S MANUAL OR PILOT’S OPERATNG HANDBOOK ### SE1779NM_AML.pdf **PRECISE FLIGHT, INC.** **FAA APPROVED MODEL LIST (AML) NO. SE1779NM FOR** INSTALLATION OF STANDBY VACUUM SYSTEM (SVS) Issue Date: October 31, 1999 **LIST OF ACTIVE PAGES** **PAGE AMMENDMENT DATE** 1 08/22/99 2 12/28/82 3 12/28/82 FAA APROVED: Acting Manager, Special Certification Branch S e a t t l e A i r c r a f t C e r t i f i c a t i o n O f f i c e Ammendment Date: September 09, 1999 **PRECISE FLIGHT, INC.** **FAA APPROVED MODEL LIST (AML) NO. SE1779NM FOR** INSTALLATION OF STANDBY VACUUM SYSTEM (SVS) Issue Date: October 31, 1999 1 of 3 Item Engine Make Engine Model Original Type Certificate Number Certification Basis For Alteration FAA Approved Drawing No. Revision No. and Date AFM Supplement Number/Date AML Amendment Date LYCOMING O-235 Series E-223 CAR 13 and T.C. E-223 **LYC. SVS 0010 12/28/82 04/11/83** 2 O-290 E-229 CAR 13 and T.C. E-223 LYC. SVS 0010 3 0-320 E-274 CAR13 and T.C. E-274 LYC. SVS 0010 4 IO-320 1E12 CAR 13 and T.C. 1E12 LYC. SVS 0010 5 0-340 E-277 CAR 13 and T.C. E-277 LYC. SVS 0010 6 0-350 227 CAR13 and T.C. 227 LYC. SVS 0010 7 0360, LO-360, IO-360, LIO360 E-286 1W10 CAR 13 and T.C. E-286 LYC. SVS 0010 05/10/85 8 AEIO-360 E1CE CAR 13 and T.C. E1CE LYC. SVS 0010 08/22/90 **PRECISE FLIGHT, INC.** **FAA APPROVED MODEL LIST (AML) NO. SE1779NM FOR** INSTALLATION OF STANDBY VACUUM SYSTEM (SVS) Issue Date: October 31, 1999 2 of 3 Item Engine Make Engine Model Original Type Certificate Number Certification Basis For Alteration FAA Approved Drawing No. Revision No. and Date AFM Supplement Number/Date AML Amendment Date 9 LYCOMING TIO-360 E-16EA CAR13 and T.C. E-16EA LYC. SVS 0010 10 TO-360 LTO-360 E26EA CAR 13 and T.C. E-26EA LYC. SVS 0010 11 O-43E GO-435 E-228 CAR 13 and T.C. E-228 LYC. SVS 0010 12/28/82 12 GSO-435 E-276 CAR13 and T.C. E-276 LYC. SVS 0010 13 GO-480, IGO-480, GSO-480, O480 E-275 CAR 13 and T.C. E-275 LYC. SVS 0010 14 IGSO-480 E-284 CAR 13 and T.C. E284 LYC. SVS 0010 15 O-540 E-295 CAR13 and T.C. E-295 LYC. SVS 0010 16 IO-540 1E4 CAR 13 and T.C. 1E4 LYC. SVS 0010 17 IGO-540 1E11 CAR 13 and T.C. 1E11 LYC. SVS 0010 **PRECISE FLIGHT, INC.** **FAA APPROVED MODEL LIST (AML) NO. SE1779NM FOR** INSTALLATION OF STANDBY VACUUM SYSTEM (SVS) Issue Date: October 31, 1999 3 of 3 Item Engine Make Engine Model Original Type Certificate Number Certification Basis For Alteration FAA Approved Drawing No. Revision No. and Date AFM Supplement Number/Date AML Amendment Date 18 LYCOMING IGSO-540 1E7 CAR 13 and T.C. 1E7 LYC. SVS 0010 19 O-540-9 E-304 CAR 13 and T.C. E-304 LYC. SVS 0010 20 TIO-540 LTIO-540 E14EA CAR 13 and T.C. E14EA LYC. SVS 0010 12/28/82 21 TIO-541 E10EA CAR 13 and T.C. E10EA LYC. SVS 0010 22 TIGO-541 E19EA CAR 13 and T.C. E19EA LYC. SVS 0010 23 GSO-580 E-256 CAR13 and T.C. E-256 LYC. SVS 0010 24 SO-580 E-285 CAR 13 and T.C. E-285 LYC. SVS 0010 25 IO-720 1E15 CAR 13 and T.C. 1E15 LYC. SVS 0010 ## Every issue (1) - November 7, 2003: Amended, Current. [certificate](https://openairdocs.org/files/sha256/9e/39/9e399b9c8a614d1714255271c678107576db8304a48d68ce5d54c6feb1208978), [SE1779NM_AML.pdf](https://openairdocs.org/files/sha256/59/fb/59fb0c9b51c34540aa3929bba28c12cddf9ff8fa8ca6caf1f13dcf8155834a19) --- 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.