# STC SA2192CE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Avcon Division, Butler National Corporation
- Description: Installation of a cargo door and teardrop window aft of cargo door.
- Status date: March 31, 2016
- Data sheets: A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE
- Certificate PDF: https://openairdocs.org/files/sha256/7d/ca/7dca086f27f889fd6566a19758c31c9acaa49650fdd9836648012a4e1871db12
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FBCF6B29D88C2EFA86257F88005803CA.0001
- Page: https://openairdocs.org/stc/SA2192CE

## ADs that name it

None.

## Approved models (9)

- Beechcraft Corporation 200 (TCDS A24CE)
- Beechcraft Corporation 200T (TCDS A24CE)
- Beechcraft Corporation 300 (TCDS A24CE)
- Beechcraft Corporation 300LW (TCDS A24CE)
- Beechcraft Corporation A200 (C-12A) (TCDS A24CE)
- Beechcraft Corporation A200 (C-12C) (TCDS A24CE)
- Beechcraft Corporation B200 (TCDS A24CE)
- Beechcraft Corporation B200GT (TCDS A24CE)
- Beechcraft Corporation B200T (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.

FAA Form 8110-2 (5/14) Page 1 of

Part of the

Signature

Title 1965, plus amendments listed in the Type Certificate Data Sheet, and SFAR 41C (Model 300 only).

Avcon Division, Butler National Corporation 714 N. Oliver, Hangar M Newton, KS 67114 23 Federal Aviation Regulations effective February 1, 2 SA2192CE Installation of a cargo door and teardrop window aft of cargo door. Data required: Avcon Drawing List Number 1028, dated December 28, 1986, or later FAA Approved revisions.

Beechcraft 200, 200T, A200, B200, B200T, B200GT, 300, 300LW

1. Every airplane modified to a cargo door configuration shall be flight tested to verify that the flight handling characteristics have not been altered or degraded by the modification.

2. This approval should not be extended to other specific airplanes of these models on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of the other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane.

December 29, 1986, November 9, 1987, June 21, 1993, March 31, 2016 June 27, 1986 September 18, 1986 A24CE Grant E. Youngdahl Program Manager Wichita Aircraft Certification Office

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee)

From (Name and address of grantor)

2 SA2192CE

## Every issue (2)

- March 31, 2016: Amended, Current. [certificate](https://openairdocs.org/files/sha256/7d/ca/7dca086f27f889fd6566a19758c31c9acaa49650fdd9836648012a4e1871db12)
- June 21, 1993: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/1a/82/1a82c31115fc2b7af4673207b3992a8404ebaeb9415d81096cb9f4deaf556d78)

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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.