# STC SA289NE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Textron Aviation Inc, United States - Description: Installation of a Turbomach (Solar) T-62T-40C3A auxiliary power unit. - Applied: April 17, 1984 - Status date: April 27, 2017 - Product: Aircraft, Large Multi-Engine - Certification basis: Part 21 - Data sheets: [TCDS A9NM](https://openairdocs.org/tcds/A9NM) - Certificate PDF: https://openairdocs.org/files/sha256/66/5c/665c27658375710066bb0d9439e3bc23761469e623135d513041803731f6a1c0 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/96AA20FFE7CA38CC8625817D004D9C94.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA289NE ## ADs that name it (0) None. ## Approved models (1) - The Cessna Aircraft Company 650 ([TCDS A9NM](https://openairdocs.org/tcds/A9NM)) ## 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. FAA Form 8110-2 (5/14) Page 1 of Part of the Signature Title SA289NE Textron Aviation Inc. One Cessna Boulevard Wichita, KS 67215 25 Federal Aviation Regulations. Cessna 650 3 A9NM Installation of Turbomach (Solar) T-62T-40C3A Auxiliary Power Unit in accordance with the data listed in PATS, Inc, Installation Drawing List Report No.: 1. 282, dated July 19, 1984, or later FAA approved revision, or 2. 334, Revision A, dated August 22, 1986, or later FAA approved revision, or 3. In accordance with data listed in Cessna Drawing 6200483, Revision A, or later FAA approved revision. 1. a. For Citation III airplanes up to and including Serial Number 0104: PATS, Inc. Flight Manual Supplement No. 1, approved September 5, 1984, or later FAA approved revision, or Cessna Citation III Flight Manual Supplement No. 65, Revision 1, approved August 19, 1992, or later FAA approved revision is required. (see continuation sheet 3 of 3) December 12, 1986; April 27, 2017 April 17, 1984 September 14, 1984 12/7/84; 9/11/85; 1/21/86; 8/26/86; 11/5/86; 12/8/87; 7/9/90; 1/29/92; 9/24/92 Mark Fuller STC ODA administrator ODA-100129-CE FAA Form 8110-2 (5/14) Page 2 of To (Name and address of transferee) From (Name and address of grantor) FAA Form 8110-2 (5/14) Page 3 of Date of Issuance: September 14, 1984 Date Amended: September 24, 1992 Date Reissued: April 27, 2017 1. b. For Citation III airplanes Serial Numbers 0105 through 0178: PATS, Inc. Flight Manual Supplement No. 2, approved August 28, 1986, or later FAA approved revision, or Cessna Citation III Flight Manual Supplement No. 65, approved October 22, 1991, or later FAA approved revision, is required. c. For Citation III airplanes Serial Numbers 0105 through 0178 without hydraulic pump: PATS, Inc. Flight Manual Supplement No. 5 approved November 12, 1987, or later FAA Approved revision, or Cessna Citation III Flight Manual Supplement No. 66 approved October 22, 1991, or later FAA approved revision, is required. d. For Citation III airplanes Serial Numbers 0179 through 7000: Cessna Citation III Flight Manual Supplement No. 56 approved January 22, 1990, or later FAA Approved revision, is required. e. For Citation VI airplanes Serial Numbers 0200 through 7000: Cessna Citation VI Flight Manual Supplement No. 14 approved April 12, 1991, or later FAA approved revision, is required. f. For Citation VII airplanes Serial Numbers 7001 and on: Cessna Citation VII Flight Manual Supplement No. 17 approved January 15, 1992, or later FAA approved revision, is required. 2. a. PATS, Inc. Installation Report No. 282 applies to airplanes up to and including Serial Number 0104. b. PATS, Inc. Installation Report No. 334 applies to airplanes Serial Number 0105 through Serial Number 0169. c. Cessna Drawing 6200483 applies to airplanes Serial Number 0170 and on. 3. This approval should not be extended to other specific aircraft of this model on which other approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane. -- END -- 3 SA289NE ## Every issue (1) - April 27, 2017: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/66/5c/665c27658375710066bb0d9439e3bc23761469e623135d513041803731f6a1c0) --- 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.