# STC SA2167NM - 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 21 - Data sheets: [TCDS TC 760](https://openairdocs.org/tcds/TC%20760), [TCDS A-797](https://openairdocs.org/tcds/A-797), [TCDS A-780](https://openairdocs.org/tcds/A-780), [TCDS 2A8](https://openairdocs.org/tcds/2A8), [TCDS A-800](https://openairdocs.org/tcds/A-800), [TCDS 1A1](https://openairdocs.org/tcds/1A1), [TCDS A-805](https://openairdocs.org/tcds/A-805), [TCDS 1A2](https://openairdocs.org/tcds/1A2), [TCDS 1A4](https://openairdocs.org/tcds/1A4), [TCDS 1A6](https://openairdocs.org/tcds/1A6), [TCDS 1A15](https://openairdocs.org/tcds/1A15), [TCDS 2A13](https://openairdocs.org/tcds/2A13), [TCDS A3SO](https://openairdocs.org/tcds/A3SO), [TCDS A9SO](https://openairdocs.org/tcds/A9SO), [TCDS A18SO](https://openairdocs.org/tcds/A18SO), [TCDS A25SO](https://openairdocs.org/tcds/A25SO) - Certificate PDF: https://openairdocs.org/files/sha256/b8/5c/b85c9b8ef5fd958eaf4f6990aa61a34a549dd5edbdeeb1aad095367f6ec45536 - Approved model list and other attachments: [SA2167NM AML .pdf](https://openairdocs.org/files/sha256/6d/df/6ddfbfc28a7016008b3313da3664c384caa5d09a7980f109cfb41199f71024df) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3D349E68BAF0E12886256DF900500AB3.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA2167NM ## 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 (76, first 50) - FS 2000 Corp. L-14 ([TCDS TC 760](https://openairdocs.org/tcds/TC%20760)) - FS 2002 Corp. PA-14 ([TCDS A-797](https://openairdocs.org/tcds/A-797)) - FS 2003 Corp. PA-12 ([TCDS A-780](https://openairdocs.org/tcds/A-780)) - FS 2003 Corp. PA-12S ([TCDS A-780](https://openairdocs.org/tcds/A-780)) - Lavia Argentina S.A. (Laviasa) PA-25 ([TCDS 2A8](https://openairdocs.org/tcds/2A8)) - Lavia Argentina S.A. (Laviasa) PA-25-235 ([TCDS 2A8](https://openairdocs.org/tcds/2A8)) - Lavia Argentina S.A. (Laviasa) PA-25-260 ([TCDS 2A8](https://openairdocs.org/tcds/2A8)) - Piper Aircraft Inc. PA-15 ([TCDS A-800](https://openairdocs.org/tcds/A-800)) - Piper Aircraft Inc. PA-16 ([TCDS 1A1](https://openairdocs.org/tcds/1A1)) - Piper Aircraft Inc. PA-16S ([TCDS 1A1](https://openairdocs.org/tcds/1A1)) - Piper Aircraft Inc. PA-17 ([TCDS A-805](https://openairdocs.org/tcds/A-805)) - Piper Aircraft Inc. PA-18 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18-105 (Special) ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18-125 (Army L-21A) ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18-135 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18-150 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18A ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18A-135 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18A-150 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18AS-125 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18AS-135 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18AS-150 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S-105 (Special) ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S-125 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S-150 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-19 (Army L-18C) ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-19S ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-20 ([TCDS 1A4](https://openairdocs.org/tcds/1A4)) - Piper Aircraft Inc. PA-20-115 ([TCDS 1A4](https://openairdocs.org/tcds/1A4)) - Piper Aircraft Inc. PA-20-135 ([TCDS 1A4](https://openairdocs.org/tcds/1A4)) - Piper Aircraft Inc. PA-20S ([TCDS 1A4](https://openairdocs.org/tcds/1A4)) - Piper Aircraft Inc. PA-20S-115 ([TCDS 1A4](https://openairdocs.org/tcds/1A4)) - Piper Aircraft Inc. PA-22 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) - Piper Aircraft Inc. PA-22-108 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) - Piper Aircraft Inc. PA-22-135 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) - Piper Aircraft Inc. PA-22-150 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) - Piper Aircraft Inc. PA-22-160 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) - Piper Aircraft Inc. PA-22S-135 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) - Piper Aircraft Inc. PA-22S-150 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) - Piper Aircraft Inc. PA-22S-160 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) - Piper Aircraft Inc. PA-24 ([TCDS 1A15](https://openairdocs.org/tcds/1A15)) - Piper Aircraft Inc. PA-24-250 ([TCDS 1A15](https://openairdocs.org/tcds/1A15)) - Piper Aircraft Inc. PA-24-260 ([TCDS 1A15](https://openairdocs.org/tcds/1A15)) - Piper Aircraft Inc. PA-24-400 ([TCDS 1A15](https://openairdocs.org/tcds/1A15)) - Piper Aircraft Inc. PA-28-140 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-150 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-151 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-160 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-161 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) All 76: https://openairdocs.org/stc/SA2167NM/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 SA2167NM 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. SA2167NM 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. SA2167NM, dated May 4, 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. SA2167NM, and the appropriate FAA approved Airplane Flight Manual Supplement (AFMS) listed on AML No. SA2167NM 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; 8/17/89; 5/4/00; 11/7/03 (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ### SA2167NM AML .pdf **FAA APPROVED MODEL LIST (AML) NO. SA2167NM PRECISE FLIGHT, INC.** For INSTALLATION OF PRECISE FLIGHT STANDBY VACUUM SYSTEM Issue Date: December 7, 1984 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 Piper Aircraft Corp. L-14 760 CAR 4a Supplemental Flight Manual for SA2167NM 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 5/4/2000 2 Piper Aircraft Corp. L-14 760 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 5/4/2000 PA-12, -12S 780 CAR 3 PA-14 797 CAR 3 PA-15 800 CAR 3 PA-16, -16S 1A1 CAR 3 3 Piper Aircraft Corp. PA-17 805 CAR 3 Supplemental Flight Manual for SA2167NM 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 5/4/2000 PA-12, -12S 780 CAR 3 PA-14 797 CAR 3 PA-15 800 CAR 3 PA-16, -16S 1A1 CAR 3 4 Piper Aircraft Corp. PA-17 805 CAR 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 5/4/2000 * or later FAA Approved Revision Page 1 of 7 FAA APPROVED MODEL LIST (AML) NO. SA2167NM **PRECISE FLIGHT, INC.** For INSTALLATION OF PRECISE FLIGHT STANDBY VACUUM SYSTEM Issue Date: December 7, 1984 Item Aircraft Make Aircraft Model Original Type Certificate Number Certificatio n Basis for Alteration FAA Approved Airplane Flight Manual Supplement* FAA Approved Drawing* ____________________________________________ Number REV AML Amdt. Date 5 Piper Aircraft Corp. PA-18, -18A, -18S, -18-105 (SPECIAL), -18S-105 (SP), -18-125 (ARMY L- 21A), -18AS-125, -18S-125, -18-135, -18A-135, -18AS-135, -18-150, -18A- 150, -18AS-150, -18S-150, -19 (ARMY L-18C), -19S 1A2 CAR 3 Supplemental Flight Manual for SA2167NM 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 5/4/2000 6 Piper Aircraft Corp. PA-18, -18A, -18S, -18-105 (SPECIAL), -18S-105 (SP), - 18-125 (ARMY L- 21A), -18AS-125, -18S-125, -18-135, -18A-135, -18AS-135, -18-150, -18A- 150, -18AS-150, -18S-150, -19 (ARMY L-18C), -19S 1A2 CAR 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 5/4/2000 * or later FAA Approved Revision Page 2 of 7 **FAA APPROVED MODEL LIST (AML) NO. SA2167NM PRECISE FLIGHT, INC.** For INSTALLATION OF PRECISE FLIGHT STANDBY VACUUM SYSTEM Issue Date: December 7, 1984 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 Piper Aircraft Corp. PA-20, -20S, -20-115, -20S-115, -20-135 1A4 CAR 3 Supplemental Flight Manual for SA2167NM 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 5/4/2000 8 Piper Aircraft Corp. PA-20, -20S, -20-115, -20S-115, -20-135 1A4 CAR 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 5/4/2000 9 Piper Aircraft Corp. PA-22, -22-108, -22-135, -22S-135, -22-150, -22S-150, -22-160, -22S-160 1A6 CAR 3 Supplemental Flight Manual for SA2167NM 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 5/4/2000 10 Piper Aircraft Corp. PA-22, -22-108, -22-135, -22S-135, -22-150, -22S-150, -22-160, -22S-160 1A6 CAR 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 5/4/2000 * or later FAA Approved Revision **PAGE 3 OF 7 FAA APPROVED MODEL LIST (AML) NO. SA2167NM** **PRECISE FLIGHT, INC.** For INSTALLATION OF PRECISE FLIGHT STANDBY VACUUM SYSTEM Issue Date: December 7, 1984 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 11 Piper Aircraft Corp. PA-24, -24-250, -24-260, -24-400 1A15 CAR 3 Supplemental Flight Manual for SA2167NM 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 5/4/2000 12 Piper Aircraft Corp. PA-24, -24-250, -24-260, -24-400 1A15 CAR 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 5/4/2000 13 Piper Aircraft Corp. PA-25, -25-235, -25-260 2A8 CAR 3 Supplemental Flight Manual for SA2167NM 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 5/4/2000 14 Piper Aircraft Corp. PA-25, -25-235, -25-260 2A8 CAR 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 5/4/2000 * or later FAA Approved Revision Page 4 of 7 FAA APPROVED MODEL LIST (AML) NO. SA2167NM PRECISE FLIGHT, INC. For INSTALLATION OF PRECISE FLIGHT STANDBY VACUUM SYSTEM Issue Date: December 7, 1984 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 15 Piper Aircraft Corp. PA-32-260, -32RT-300, -32RT-301T, -32-300, -32RT-300T, -32-301, -32S-300, -32R-301, -32-301T, -32R-300, -32R-301T A3SO CAR 3 Supplemental Flight Manual for SA2167NM 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 5/4/2000 16 Piper Aircraft Corp. PA-32-260, -32RT-300, -32RT-301T, -32-300, -32RT-300T, -32-301, -32S-300, -32R-301, -32-301T, -32R-300, -32R-301T A3SO CAR 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 5/4/2000 * or later FAA Approved Revision Page 5 of 7 FAA APPROVED MODEL LIST (AML) NO. SA2167NM PRECISE FLIGHT, INC. For INSTALLATION OF PRECISE FLIGHT STANDBY VACUUM SYSTEM Issue Date: December 7, 1984 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 17 Piper Aircraft Corp. PA-28-140, -28-141, -28-150, -28-151, -28-160, -28-180, -28R-180, -28S-180, -28-235, -28-181, -28-161, -28R-200, -28R-201, -28R-201T, -28-236, -28RT-201, -28RT-201T, -28-201T 2A13-38 CAR 3 Supplemental Flight Manual for SA2167NM 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 5/4/2000 18 Piper Aircraft Corp. PA-28-140, -28-141, -28-150, -28-151, -28-160, -28-180, -28R-180, -28S-180, -28-235, -28-181, -28-161, -28R-200, -28R-201, -28R-201T, -28-236, -28RT-201, -28RT-201T, -28-201T 2A13-38 CAR 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. A, dated 12/22/1999 5/4/2000 * or later FAA Approved Revision Page 6 of 7 FAA APPROVED MODEL LIST (AML) NO. SA2167NM PRECISE FLIGHT, INC. For INSTALLATION OF PRECISE FLIGHT STANDBY VACUUM SYSTEM Issue Date: December 7, 1984 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 19 Piper Aircraft Corp. PA-36-285, -36-300, -36-375 A9SO FAR 23 Supplemental Flight Manual for SA2167NM 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 5/4/2000 20 Piper Aircraft Corp. PA-36-285, -36-300, -36-375 A9SO 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 5/4/2000 PA-38-112 A18SO FAR 23 21 Piper Aircraft Corp. PA-46-310P A25SO FAR 23 Supplemental Flight Manual for SA2167NM dated8/11/99. (SVS III) SVS III Engineering Drawing 000V0000 And Installation Report No. 50050 Rev.-, dated 3/10/2000 Rev. 25, dated 8/26/99 5/4/2000 PA-38-112 A18SO FAR 23 22 Piper Aircraft Corp. PA-46-310P A25SO 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 5/4/2000 * 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: _May 4, 2000 _ Page 7 of 7 ## Every issue (1) - November 7, 2003: Amended, Current. [certificate](https://openairdocs.org/files/sha256/b8/5c/b85c9b8ef5fd958eaf4f6990aa61a34a549dd5edbdeeb1aad095367f6ec45536), [SA2167NM AML .pdf](https://openairdocs.org/files/sha256/6d/df/6ddfbfc28a7016008b3313da3664c384caa5d09a7980f109cfb41199f71024df) --- 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.