# STC SA00773DE - Type: Supplemental type certificate - Status: Current, Issued - Holder: Lee Products Engineering Services, Inc., United States - Description: Installation of Engine Cowl Access Panel - Applied: December 12, 2013 - Status date: August 1, 2014 - Product: Aircraft, Small/Large Airplane - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) - Certificate PDF: https://openairdocs.org/files/sha256/d9/be/d9be3f0f75b2bc28cb118d29824bae3816d4dd12348847a895f47a5b9392faf5 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8CCA865FD6E0A13786257D400061AC8D.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA00773DE ## ADs that name it (0) None. ## Approved models (3) - Beechcraft Corporation 1900C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Beechcraft Corporation 1900C (C-12J) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Beechcraft Corporation 1900D ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) ## 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 N umber SA00773DE This certificate, issued to Lee Products Engineering Services, Inc. 16748 E. Smoky Hill Road, 9C-Suite 337 Centennial, Colorado 80015 P art 23 of th e F ederal A viation R egulations . (See Page 3 for complete certification basis) Original Product Type Certificate N umber: A24CE M ake: Hawker Beechcraft M odel: 1900C, 1900C (C-12J) and 1900D Description of the Type Design Change: Installation of Engine Cowl Access Panel in accordance with Lee Products Engineering Services Master Data List Document No. 223-MDL-001, Revision IR, dated July 16, 2014, FAA approved August 01, 2014, or later FAA approved revision. 1. The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configurations will not introduce any adverse effect upon the airworthiness of the aircraft. 2. Instructions for Continued Airworthiness, Document Number 223-ICA-001, Revision A, FAA accepted March 13, 2014, or later FAA accepted revision is required for this installation. 3. 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: December 12, 2013 Date reissued: Date of issuance: August 01, 2014 Date amended: B y direction of the A dministrator (Signature) Gregory K. Johnson, Acting Manager Denver Aircraft Certification Office Northwest Mountain Region (Title) United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet 3) N umber SA00773DE Certification B asis: Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the design change to the Hawker Beechcraft 1900 series aircraft is as follows: • The type certification basis for Hawker Beechcraft 1900 series airplanes is shown on TCDS A24CE for parts not changed or not affected by the change. • The certification basis for the parts changed or affected by this change since the reference date of application, December 12, 2013, is shown in TCDS A24CE. -END- ## Every issue (1) - August 1, 2014: Issued, Current. [certificate](https://openairdocs.org/files/sha256/d9/be/d9be3f0f75b2bc28cb118d29824bae3816d4dd12348847a895f47a5b9392faf5) --- 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.