# STC SA2162NM - 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: July 15, 2014 - Product: Aircraft, Small Airplane - Certification basis: Part 21 - Data sheets: [TCDS A-768](https://openairdocs.org/tcds/A-768), [TCDS 5A2](https://openairdocs.org/tcds/5A2), [TCDS 3A19](https://openairdocs.org/tcds/3A19), [TCDS A-799](https://openairdocs.org/tcds/A-799), [TCDS 3A12](https://openairdocs.org/tcds/3A12), [TCDS 3A17](https://openairdocs.org/tcds/3A17), [TCDS A13CE](https://openairdocs.org/tcds/A13CE), [TCDS A20CE](https://openairdocs.org/tcds/A20CE), [TCDS 5A6](https://openairdocs.org/tcds/5A6), [TCDS 3A13](https://openairdocs.org/tcds/3A13), [TCDS 3A24](https://openairdocs.org/tcds/3A24), [TCDS A9CE](https://openairdocs.org/tcds/A9CE), [TCDS A4CE](https://openairdocs.org/tcds/A4CE), [TCDS A16CE](https://openairdocs.org/tcds/A16CE), [TCDS 3A21](https://openairdocs.org/tcds/3A21), [TCDS 3A11](https://openairdocs.org/tcds/3A11), [TCDS 5A5](https://openairdocs.org/tcds/5A5), [TCDS 3A14](https://openairdocs.org/tcds/3A14) - Certificate PDF: https://openairdocs.org/files/sha256/b8/6b/b86b96863fa2fb087a2492769baaf0463a860b3189e9e2abb77d8668796fe7ac - Approved model list and other attachments: [SA2162NM_AML.pdf](https://openairdocs.org/files/sha256/21/35/2135bb56e83d21dfcdb707a0da0f896b3062dcefd4a001183b4128820151562f) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/CC8A9A6DABBD179F86257D18005FBEB4.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA2162NM ## 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 (167, first 50) - Cessna Aircraft Company 120 ([TCDS A-768](https://openairdocs.org/tcds/A-768)) - Cessna Aircraft Company 140 ([TCDS A-768](https://openairdocs.org/tcds/A-768)) - Cessna Aircraft Company 140A ([TCDS 5A2](https://openairdocs.org/tcds/5A2)) - Cessna Aircraft Company 150 ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150A ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150B ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150C ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150D ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150E ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150F ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150G ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150H ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150J ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150K ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150L ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 150M ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 152 ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 170 ([TCDS A-799](https://openairdocs.org/tcds/A-799)) - Cessna Aircraft Company 170A ([TCDS A-799](https://openairdocs.org/tcds/A-799)) - Cessna Aircraft Company 170B ([TCDS A-799](https://openairdocs.org/tcds/A-799)) - Cessna Aircraft Company 172 ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172A ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172B ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172C ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172D ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172E ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172F (USAF T-41A) ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172I ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172K ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172L ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172M ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172N ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172P ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172Q ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172RG ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) - Cessna Aircraft Company 175 ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) - Cessna Aircraft Company 175A ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) - Cessna Aircraft Company 175B ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) - Cessna Aircraft Company 175C ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) - Cessna Aircraft Company 177 ([TCDS A13CE](https://openairdocs.org/tcds/A13CE)) - Cessna Aircraft Company 177A ([TCDS A13CE](https://openairdocs.org/tcds/A13CE)) - Cessna Aircraft Company 177B ([TCDS A13CE](https://openairdocs.org/tcds/A13CE)) - Cessna Aircraft Company 177RG ([TCDS A20CE](https://openairdocs.org/tcds/A20CE)) - Cessna Aircraft Company 180 ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180A ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180B ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180C ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180D ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180E ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180F ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) All 167: https://openairdocs.org/stc/SA2162NM/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 SA2162NM 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. SA2162NM 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 AML No. SA2162NM, dated April 14, 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 December 28, 1982, 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. SA2162NM, and the appropriate FAA approved Airplane Flight Manual Supplement (AFMS) listed on AML No. SA2162NM 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; 7/25/90; 4/14/00; 11/7/03 (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ### SA2162NM_AML.pdf **FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA2162NM FOR** INSTALLATION OF PRECISE FLIGHT STANDBY VACUUM SYSTEM ISSUE DATE: May 23, 1988 Page 1 of 10 **ITEM AIRCRAFT MAKE** **AIRCRAFT MODEL ORIGINAL TC NUMBER** **CERTIFICATION** **BASIS FOR** **ALTERATION** **FAA APPROVED** **AIRCRAFT FLIGHT MANUAL** **SUPPLEMENT** **FAA APPROVED MASTER** **DRAWING LIST** AML REV DATE Number Drawing Revision* 1. Cessna 120, 140 A-768 CAR 4a Supplemental Flight Manual for SA2162NM 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 4/14/2000 2. Cessna 120, 140 A-768 CAR 4a 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 4/14/2000 3. Cessna 140A 5A2 CAR 3, (CAR 4a) Supplemental Flight Manual for SA2162NM 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 4/14/2000 4. Cessna 140A 5A2 CAR 3, (CAR 4a) 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 4/14/2000 **FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA2162NM FOR** INSTALLATION OF PRECISE FLIGHT STANDBY VACUUM SYSTEM ISSUE DATE: May 23, 1988 Page 2 of 10 **ITEM AIRCRAFT MAKE** **AIRCRAFT MODEL ORIGINAL TC NUMBER** **CERTIFICATION** **BASIS FOR** **ALTERATION** **FAA APPROVED** **AIRCRAFT FLIGHT MANUAL** **SUPPLEMENT** **FAA APPROVED MASTER** **DRAWING LIST** AML REV DATE Number Drawing Revision* 5. Cessna 150, 150A, 150B, 150C, 150D, 150E, 150F, 150G, 150H, 150J, 150K, 150L, 150M, A150K, A150L, A150M, 152, A152 3A19 CAR Part 3 Supplemental Flight Manual for SA2162NM 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 4/14/2000 6. Cessna 150, 150A, 150B, 150C, 150D, 150E, 150F, 150G, 150H, 150J, 150K, 150L, 150M, A150K, A150L, A150M, 152, A152 3A19 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. 08074 Rev.-, dated 3/10/2000 Rev.-, dated 12/22/1999 4/14/2000 7. Cessna 170, 170A, 170B A-799 CAR Part 3 Supplemental Flight Manual for SA2162NM 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 4/14/2000 8. Cessna 170,170A, 170B A-799 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 4/14/2000 **FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA2162NM FOR** INSTALLATION OF PRECISE FLIGHT STANDBY VACUUM SYSTEM ISSUE DATE: May 23, 1988 Page 3 of 10 **ITEM AIRCRAFT MAKE** **AIRCRAFT MODEL ORIGINAL TC NUMBER** **CERTIFICATION** **BASIS FOR** **ALTERATION** **FAA APPROVED** **AIRCRAFT FLIGHT MANUAL** **SUPPLEMENT** **FAA APPROVED MASTER** **DRAWING LIST** AML REV DATE Number Drawing Revision* 9. Cessna 172, 172A, 172B, 172C, 172D, 172E, 172F (USAF T-41A) 172I, 172K, 172L, 172M, 172N, 172P, 172Q 3A12 Part 23 Supplemental Flight Manual for SA2162NM 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 4/14/2000 10. Cessna 172, 172A, 172B, 172C, 172D, 172E, 172F (USAF T-41A) 172I, 172K, 172L, 172M, 172N, 172P, 172Q 3A12 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 4/14/2000 11. Cessna 175, 175A, 175B, 175C, P172D, R172E (USAF T-41B, USAF T41-C and D) R172F (USAF T-41D), R172G (USAF T-41C or D), R172H (USAF T-41D), R172J, R172K, 172RG 3A17 CAR Part 3 Supplemental Flight Manual for SA2162NM 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 7/15/2014 12. Cessna 175, 175A, 175B, 175C, P172D, R172E (USAF T-41B, USAF T41-C and D) R172F (USAF T-41D), R172G (USAF T-41C or D), R172H (USAF T-41D), R172J, R172K, 172RG 3A17 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 7/15/2014 **FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA2162NM FOR** INSTALLATION OF PRECISE FLIGHT STANDBY VACUUM SYSTEM ISSUE DATE: May 23, 1988 Page 4 of 10 **ITEM AIRCRAFT MAKE** **AIRCRAFT MODEL ORIGINAL TC NUMBER** **CERTIFICATION** **BASIS FOR** **ALTERATION** **FAA APPROVED** **AIRCRAFT FLIGHT MANUAL** **SUPPLEMENT** **FAA APPROVED MASTER** **DRAWING LIST** AML REV DATE Number Drawing Revision* 13. Cessna 177,177A,177B 177RG A13CE A20CE FAR 23 Supplemental Flight Manual for SA2162NM 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 4/14/2000 14. Cessna 177, 177A, 177B 177RG A13CE A20CE FAR 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 4/14/2000 15. Cessna 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 180K 5A6 CAR Part 3 Supplemental Flight Manual for SA2162NM 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 4/14/2000 16. Cessna 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 180K 5A6 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 4/14/2000 **FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA2162NM FOR** INSTALLATION OF PRECISE FLIGHT STANDBY VACUUM SYSTEM ISSUE DATE: May 23, 1988 Page 5 of 10 **ITEM AIRCRAFT MAKE** **AIRCRAFT MODEL ORIGINAL TC NUMBER** **CERTIFICATION** **BASIS FOR** **ALTERATION** **FAA APPROVED** **AIRCRAFT FLIGHT MANUAL** **SUPPLEMENT** **FAA APPROVED MASTER** **DRAWING LIST** AML REV DATE Number Drawing Revision* 17. Cessna 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, R182, T182, TR182, T182T 3A13 CAR Part 3 Supplemental Flight Manual for SA2162NM 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 7/15/2014 18. Cessna 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, R182, T182, TR182, T182T 3A13 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 7/15/2014 19. Cessna 185, 185A, 185B, 185C, 185D, 185E, A185E, A185F 3A24 CAR Part 3 Supplemental Flight Manual for SA2162NM 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 4/14/2000 20. Cessna 185, 185A, 185B, 185C, 185D, 185E, A185E, A185F 3A24 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 4/14/2000 **FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA2162NM FOR** INSTALLATION OF PRECISE FLIGHT STANDBY VACUUM SYSTEM ISSUE DATE: May 23, 1988 Page 6 of 10 **ITEM AIRCRAFT MAKE** **AIRCRAFT MODEL ORIGINAL TC NUMBER** **CERTIFICATION** **BASIS FOR** **ALTERATION** **FAA APPROVED** **AIRCRAFT FLIGHT MANUAL** **SUPPLEMENT** **FAA APPROVED MASTER** **DRAWING LIST** AML REV DATE Number Drawing Revision* 21. Cessna 188, 188A, 188B, A188A, A188B, T188C A9CE FAR Part 21 Supplemental Flight Manual for SA2162NM 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 4/14/2000 22. Cessna 188, 188A, 188B, A188A, A188B, T188C A9CE FAR Part 21 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 4/14/2000 23. Cessna 206, U206B, TP206D, P206, U206C, TP206E, P206A, U206D, TU206A, P206B, U206E, TU206B, P206C, U206F, TU206C, P206D, U206G, TU206D, P206E, TP206A, TU206E, U206, TP206B, TU206F, U206A, TP206C, TU206G, 206H, T206H A4CE CAR Part 3 Supplemental Flight Manual for SA2162NM 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 7/15/2014 **FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA2162NM FOR** INSTALLATION OF PRECISE FLIGHT STANDBY VACUUM SYSTEM ISSUE DATE: May 23, 1988 Page 7 of 10 **ITEM AIRCRAFT MAKE** **AIRCRAFT MODEL ORIGINAL TC NUMBER** **CERTIFICATION** **BASIS FOR** **ALTERATION** **FAA APPROVED** **AIRCRAFT FLIGHT MANUAL** **SUPPLEMENT** **FAA APPROVED MASTER** **DRAWING LIST** AML REV DATE Number Drawing Revision* 24. Cessna 206, U206B, TP206D, P206, U206C, TP206E, P206A, U206D, TU206A, P206B, U206E, TU206B, P206C, U206F, TU206C, P206D, U206G, TU206D, P206E, TP206A, TU206E, U206, TP206B, TU206F, U206A, TP206C, TU206G, 206H, T206H A4CE 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 7/15/2014 25. Cessna 207, 207A, T207, T207A A16CE Part 23 Supplemental Flight Manual for SA2162NM 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 4/14/2000 26. Cessna 207, 207A, T207, T207A A16CE 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 4/14/2000 **FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA2162NM FOR** INSTALLATION OF PRECISE FLIGHT STANDBY VACUUM SYSTEM ISSUE DATE: May 23, 1988 Page 8 of 10 **ITEM AIRCRAFT MAKE** **AIRCRAFT MODEL ORIGINAL TC NUMBER** **CERTIFICATION** **BASIS FOR** **ALTERATION** **FAA APPROVED** **AIRCRAFT FLIGHT MANUAL** **SUPPLEMENT** **FAA APPROVED MASTER** **DRAWING LIST** AML REV DATE Number Drawing Revision* 27. Cessna 210, 210K, 210A, T210K, 210B, 210L, 210C, T210L, 210D, 210M, 210E, T210M, 210F, 210N, T210F, P210N, 210G, T210N, T210G, 210R, 210H, P210R, T210H, T210R, 210J, 210-5 (205), T210J, 210-5A (205A) 3A21 CAR Part 3 Supplemental Flight Manual for SA2162NM 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 7/15/2014 28. Cessna 210, 210K, 210A, T210K, 210B, 210L, 210C, T210L, 210D, 210M, 210E, T210M, 210F, 210N, T210F, P210N, 210G, T210N, T210G, 210R, 210H, T210H, 210J, T210J 3A21 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 7/15/2014 29. Cessna P210R, 205U, T210R, 210-5, 210-5A 3A21 CAR Part 3 Supplemental Flight Manual for SA2162NM 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 4/14/2000 30. Cessna P210R, 205U, T210R, 210-5, 210-5A 3A21 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 4/14/2000 **FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA2162NM FOR** INSTALLATION OF PRECISE FLIGHT STANDBY VACUUM SYSTEM ISSUE DATE: May 23, 1988 Page 9 of 10 **ITEM AIRCRAFT MAKE** **AIRCRAFT MODEL ORIGINAL TC NUMBER** **CERTIFICATION** **BASIS FOR** **ALTERATION** **FAA APPROVED** **AIRCRAFT FLIGHT MANUAL** **SUPPLEMENT** **FAA APPROVED MASTER** **DRAWING LIST** AML REV DATE Number Drawing Revision* 31. Cessna (USAF 0-1A) 305A (USAF 0-1E) 305C (USAF 0-1G) 305D 305F 5A5 Part 23 Supplemental Flight Manual for SA2162NM 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 7/15/2014 32. Cessna (USAF 0-1A) 305A (USAF 0-1E) 305C (USAF 0-1G) 305D 305F 5A5 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 7/15/2014 33. Cessna 305B (USAF TO-1D, O1-D, OR O1-F), 305 3A14 CAR Part 3 Supplemental Flight Manual for SA2162NM 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 7/15/2014 34. Cessna 305B (USAF TO-1D, O1-D, OR O1-F), 305 3A14 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 7/15/2014 **FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA2162NM FOR** INSTALLATION OF PRECISE FLIGHT STANDBY VACUUM SYSTEM ISSUE DATE: May 23, 1988 Page 10 of 10 **ITEM AIRCRAFT MAKE** **AIRCRAFT MODEL ORIGINAL TC NUMBER** **CERTIFICATION** **BASIS FOR** **ALTERATION** **FAA APPROVED** **AIRCRAFT FLIGHT MANUAL** **SUPPLEMENT** **FAA APPROVED MASTER** **DRAWING LIST** AML REV DATE Number Drawing Revision* 35. Cessna 321 (NAVY OE-2) 3A11 Part 23 Supplemental Flight Manual for SA2162NM 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 4/14/2000 36. Cessna 321 (NAVY OE-2) 3A11 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 4/14/2000 * Or later FAA Approved Revision FAA Approved: Manager, Seattle Aircraft Certification Office AMENDED: 4/14/2000; 7/15/2014 REISSUED: ## Every issue (2) - July 15, 2014: Amended, Current. [certificate](https://openairdocs.org/files/sha256/b8/6b/b86b96863fa2fb087a2492769baaf0463a860b3189e9e2abb77d8668796fe7ac), [SA2162NM_AML.pdf](https://openairdocs.org/files/sha256/21/35/2135bb56e83d21dfcdb707a0da0f896b3062dcefd4a001183b4128820151562f) - November 7, 2003: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/b8/6b/b86b96863fa2fb087a2492769baaf0463a860b3189e9e2abb77d8668796fe7ac), [SA2162NM AML .pdf](https://openairdocs.org/files/sha256/21/4b/214b8d87ce227823582c580c12d7727f4a19a8cabbefa6ff7cd6037ca0026d2b) --- 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.