# STC SA2352CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Metrea Special Aerospace ISR Inc., United States
- Description: Increase maximum zero fuel weight from 10,400 lbs. To 11,000 lbs.
- Applied: December 23, 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/sha256/86/f7/86f78c3d6ec59ee808a7c6887692fe7887c07fa409ce4c05be034d514946fa6f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139684229120250711152448.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2352CE

## ADs that name it (0)

None.

## Approved models (4)

- Textron Aviation Inc. 200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. 200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. 200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. A200C (UC-12B) ([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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SA2352CE 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, 200C, A200C, 200T Increase Maximum Zero Fuel Weight from 10,400 lb. to 11,000 lb. Data required:

1. Drawing No. CE115W1032/CAT-001, dated January 27, 1988, or Drawing No. CAT 2352-001, Rev. 2, dated March 15, 1992, or later FAA Approved revision.

2. Beechcraft Model 200T only: Drawing No. CAT 11000, dated November 22, 1993, or later FAA Approved revision.

1. Beechcraft Model 200/200C/A200C only: AFMS No. CAT 88-1 or CAT 88-1A, dated January 27, 1988, or later FAA Approved revision. Drawing No. CE115W1032/CAT-001 includes required modifications as follows:

(continued on page 3) December 23, 1987 6/14/1993, 4/27/2021, 5/6/2025 January 27, 1988 4/6/1992, 11/22/1993 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:

SA2352CE 3

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nited States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA2352CE 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. STC SA1602CE, AVIADESIGN Wing Front Spar Reinforcement Kit.

b. Airspeed Indicator Markings change: barber pole limit Vmo should be 239 KIAS, or as limited by Mmo of 0.48.

c. STC SA2352CE: Fuel Management Placard, 'Auxiliary Fuel Tanks must be empty if Zero Fuel Weight exceeds 10,000 lb.' (located on or near the fuel panel).

2. Additional requirements for Beechcraft Model 200 only:

a. STC SA1783NM: Western Mark IV System, or

b. STC SA3831NM: Raisbeck Short-Field Enhancement System, and

c. STC SA3366NM: Raisbeck Ram Air Recovery System.

3. Beechcraft Model 200T only: AFMS No. CAT 88-2, dated November 22, 1993, or later FAA Approved revision.

Drawing No. CAT-11000 includes required modifications as follows:

a. STC SA1602CE, AVIADESIGN Wing Front Spar Reinforcement Kit.

b. Airspeed Indicator Markings change: barber pole limit Vmo should be 239 KIAS, or as limited by Mmo of 0.48.

c. STC SA2352CE: Fuel Management Placard, 'Auxiliary Fuel Tanks must be empty if Zero Fuel Weight exceeds 10,000 lb.' (located on or near the fuel panel).

d. Beech Kit P/N 101-9028 Fuel Filler Plates must be installed on the tip tank configuration to preclude 544 gallons maximum usable fuel; or remove tip tanks and replace with standard Beechcraft Model 200 wing tips in accordance with approved procedure.

4. 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/sha256/86/f7/86f78c3d6ec59ee808a7c6887692fe7887c07fa409ce4c05be034d514946fa6f)
- April 27, 2021: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/50/ff/50ff1a4ef366c00813d691ae7da4eac07e46eceb7d8dc24a8114e822d3c20bb6)
- April 6, 1992: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/ea/0b/ea0b514bbd904471f7e461b6efc94de2199f5378f36535ca28f5cad8e9eb031d)

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