# STC SA2307CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Metrea Special Aerospace ISR Inc., United States
- Description: Incorporation of STCs and associated modifications identified by Commuter Air Transport drawing list.
- Applied: August 27, 1987
- Status date: May 6, 2025
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/85/ad/85ad18fb91c5c7fdb0fdb3b07c5fc55cde6c963468e78e2e0a35e526dc1f75cd
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195277257520250711152234.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2307CE

## ADs that name it (0)

None.

## Approved models (2)

- Textron Aviation Inc. 200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. B200 ([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.

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SA2307CE Metrea Special Aerospace, ISR Inc.

1100 N. Broadway Ave, Suite 200 Oklahoma City, OK 73103 Part 23 Federal Aviation Regulations A24CE Textron Aviation (Beechcraft) 200, B200 Incorporation of Supplemental Type Certificates (STC) and associated modifications. Data required:

1. FAA Approved Drawing List No. CAT 2307-1, dated November 23, 1987, or later FAA Approved revision.

When modified, the airplane is in compliance with the requirements of FAR Part 135, Appendix A, for the maximum seating capacity of 13 passengers plus a crew of two. This is identified as CATPASS 200-15 and CATPASS 1300 configurations.

1. One of the following FAA Approved Airplane Flight Manual Supplement (AFMS) is required when the modification is installed: (continued on page 3) August 27, 1987 1/25/1988, 6/14/1993, 4/3/2008, 4/27/2021, 5/6/2025 November 23, 1987 1/27/1989, 9/25/1992 for Paul Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 3

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Too (Name and address of transferee):

Date oI transfer:

SA2307CE 3

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nited States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA2307CE Date Reissued: May 6, 2025 *Airworthiness requirements:

Effective February 1, 1965, plus amendments listed in the Type Certificate Data Sheet (TCDS) and FAR Part 135, Appendix A.

a. AFMS Document No. CATPASS 1011, dated November 23, 1987, including Rev. 1, dated January 27, 1989, or later FAA Approved revision. Required when STC SA2300CE (external baggage compartment (40 cubic foot cargo pod)) is installed.

b. AFMS Document No. CATPASS 1011A, dated January 27, 1989, or later FAA Approved revision. Required when STC SA2451CE 'Super 60 Pod' (external 60 foot lower fuselage baggage/cargo carrier) is installed.

c. AFMS Document No. CATPASS 1200, dated September 25, 1992, or later FAA Approved revision. Required when SA2451CE 'Super 60 Pod' (external 60 foot lower fuselage baggage/cargo carrier) is installed and the airplane is also equipped or installed with the following:

1) High Flotation Landing Gear (Goodyear wheel P/N 500-2460 and brakes P/N 500-2256).

2) STC SA4378WP, AVIADESIGN hydraulic landing gear retraction system.

3) STC SA2698NM, Hartzell/Raisbeck quiet Turbofan Propellers.

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

-------- END -------- 33

## Every issue (3)

- May 6, 2025: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/85/ad/85ad18fb91c5c7fdb0fdb3b07c5fc55cde6c963468e78e2e0a35e526dc1f75cd)
- April 27, 2021: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/bb/bc/bbbc822d2bf25a2568ff107c1d2976e0949b7335328312b2f3ee19fdf8f74129)
- June 3, 2008: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/64/3e/643e51761c882aaabf1ac5c5d355a3ca060f1bb4948de27e662e6f6a7bae44a0)

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