# STC SA27SO - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Staggerwing Museum Foundation Inc. - Description: Increase in landing weight to 9800 lbs. and extension of Aft. C.G. limits to +120.5. These limitations applicable to Beech D18S, C45H, TC45G, TC45H when modified to Airline Training Inc. CONRAD 9800 D. - Status date: October 6, 2006 - Data sheets: A-765, A-765, A-765, A-765, A-765 - Certificate PDF: https://openairdocs.org/files/sha256/81/84/81847149b279e3c38b7602f0b028d6db278727eeaa2c5c02082aaa2606067922 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4049CE0BE7BAB4F0862574F100743070.0001 - Page: https://openairdocs.org/stc/SA27SO ## ADs that name it None. ## Approved models (5) - Hawker Beechcraft Corporation C-45G (TCDS A-765) - Hawker Beechcraft Corporation C-45H (TCDS A-765) - Hawker Beechcraft Corporation D18S (TCDS A-765) - Hawker Beechcraft Corporation TC-45G (TCDS A-765) - Hawker Beechcraft Corporation TC-45H (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 Hwy Tullahoma, TN 37388 Part * of the Civil Air Regulations. * CAR 03 effective 11/13/45 and 3.242 of CAR 3 effective 11/01/49 as amended by 3-14. Original Product - Type Certificate Number : 765 Make : Beech Model : D18S, C-45G/H, and TC-45G/H Increase in landing weight to 9800 lbs. and extension of Aft. C.G. limits to +120.5. These limitations applicable to Beech D18S, C-45G, C-45H, TC-45G, TC-45H when modified to Airline Training, Inc. “CONRAD 9800 D” in accordance with STC SA2-820, and as follows: (1) Elevator Down Spring installed in accordance with Airline Training, Inc. Dwg. No. 2203 dated 07/22/61; and (2) Extended Tail Wheel installed in accordance with STC SA2-1230. Airline Training, Inc. revisions #1 dated 06/01/61 and #2 dated 07/24/62 to Airplane Flight Manual Supplement for CONRAD 9800D issued 01/14/60 required. Airworthiness compatibility of this STC with all other major changes to the standard original model(s) shown above should be confirmed prior to installation of this STC. 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 reissued : December 9, 1966; August 15, 1968; February 26, 1990; October 6, 2006 Date amended : Original signed by Robert D. Adamson ( Signature) Robert D. Adamson Program Manager Wichita Aircraft Certification Office (Title) Date of application : March 8, 1962 Date of issuance : July 24, 1962 ## Every issue (1) - October 6, 2006: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/81/84/81847149b279e3c38b7602f0b028d6db278727eeaa2c5c02082aaa2606067922) --- 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.