# STC ST00065MC

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Erickson Incorporated, United States
- Description: Installation of a Ballistic Protection System (BPS)
- Applied: December 21, 2010
- Status date: April 3, 2024
- Product: Aircraft, Large Airplane
- Certification basis: Part 25
- Data sheets: [TCDS A43EU](https://openairdocs.org/tcds/A43EU)
- Certificate PDF: https://openairdocs.org/files/sha256/fc/62/fc62f3843ea55540eb930298a7ebb6389ae6e50c91ef538acede65271c3d5584
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171907303220240404133528.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/ST00065MC

## ADs that name it (0)

None.

## Approved models (7)

- EADS CASA C-212-CB ([TCDS A43EU](https://openairdocs.org/tcds/A43EU))
- EADS CASA C-212-CC ([TCDS A43EU](https://openairdocs.org/tcds/A43EU))
- EADS CASA C-212-CD ([TCDS A43EU](https://openairdocs.org/tcds/A43EU))
- EADS CASA C-212-CE ([TCDS A43EU](https://openairdocs.org/tcds/A43EU))
- EADS CASA C-212-CF ([TCDS A43EU](https://openairdocs.org/tcds/A43EU))
- EADS CASA C-212-DE ([TCDS A43EU](https://openairdocs.org/tcds/A43EU))
- EADS CASA C-212-DF ([TCDS A43EU](https://openairdocs.org/tcds/A43EU))

## 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.

ST00065MC Erickson Incorporated 3100 Willow Springs Rd.

Central Point, OR 97502 PT 25 Federal Aviation Regulations A43EU

EADS CASA C-212-CB, C-212-CC, C-212-CD, C-212-CE, C-212-CF, C-212-DF, and C-212-DE Installation of a Ballistic Protection System (BPS) in accordance with FAA Approved Master Drawing List for the Installation of the Ballistic Protection System in the EADS CASA C-212 Series Aircraft, C212-0-1100-MCM11, Revision A, dated June 23, 2011 or later FAA approved revision. FAA Approved Airplane Flight Manual Supplement No. C212-12-1100-MCM11, Revision IR, dated July 27, 2011, or later FAA approved revision is required as part of this installation.

The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft.

*** See continuation sheet 3. *** December 21, 2010 June 6, 2017; April 3, 2024 July 27, 2011 Jason J. Brys Acting Manager Military Certification Branch 3

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ST00065MC Limitations and Conditions (continued):

The approval of this modification applies to the above noted airplane model series only.

A copy of this STC must be included in the permanent records of the modified aircraft.

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.

**END 3 3**

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## Every issue (2)

- April 3, 2024: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/fc/62/fc62f3843ea55540eb930298a7ebb6389ae6e50c91ef538acede65271c3d5584)
- July 27, 2011: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/20/8d/208db65678494965a7703b7f5a7fbd5b2be224057abfd591013799f4c07033ce)

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