# STC SA1998WE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Staggerwing Museum Foundation Inc. - Description: Installation of Bendix Model M-4C automatic flight control system. - Status date: September 3, 2004 - Data sheets: A-765, A-765, A-765, A-765, A-765, A-765, A-765, A-765, A-765, A-765, A-765 - Certificate PDF: https://openairdocs.org/files/sha256/1d/b9/1db9dde3a735650bb6317693ff5a682a59489fd1337cc373f886e408127a093f - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/36BDA63DA0BE0538862570C9006A3032.0001 - Page: https://openairdocs.org/stc/SA1998WE ## ADs that name it None. ## Approved models (11) - Raytheon Aircraft Company 3N (TCDS A-765) - Raytheon Aircraft Company 3NM (TCDS A-765) - Raytheon Aircraft Company 3TM (TCDS A-765) - Raytheon Aircraft Company C-45G (TCDS A-765) - Raytheon Aircraft Company C-45H (TCDS A-765) - Raytheon Aircraft Company D18S (TCDS A-765) - Raytheon Aircraft Company JRB-6 (TCDS A-765) - Raytheon Aircraft Company TC-45G (TCDS A-765) - Raytheon Aircraft Company TC-45H (TCDS A-765) - Raytheon Aircraft Company TC-45J (TCDS A-765) - Raytheon Aircraft Company UC-45J (SNB-5) (TCDS A-765) ## 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. This Certificate issued to Staggerwing Museum Foundation, Inc. 560 Old Shelbyville Highway Tullahoma, TN 37388 Part 3 of the Civil Air Regulations. 765 BEECH TC-45J(SNB-5), C45G, TC-45G, C-45H, TC-45H, JRB-6, D18S, 3N, 3NM, 3TM Description of Type Design Change: A Bendix Model M-4C Automatic Flight Control System is installed in accordance with FAA Sealed Hamilton Aircraft Company Drawing List 1123. AFM Supplement dated September 8, 1969, is required with this modification. *This modification pertains only to aircraft previously modified in accordance with STC SA1821WE. Limitations and Conditions: This approval should not be extended to other airplanes of those models on which other previously 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. 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 : July 11, 1969 Date of issuance : September 8, 1969 Date reissued April 28, 1977; September 3, 2004 ( Signature) Manager, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office ( Title) NOTE: **DO NOT DELETE THIS PAGE.** **DO NOT ADD ANY DATA TO THIS PAGE.** **THIS PAGE IS FOR PAGE NUMBERING PURPOSES, PLEASE DISCARD PRINTED COPY.** Number (STC No.) ## Every issue (1) - September 3, 2004: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/1d/b9/1db9dde3a735650bb6317693ff5a682a59489fd1337cc373f886e408127a093f) --- From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.