# STC SA3753NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Griggs Aircraft Refinishing LLC, United States
- Description: Installation of stiffening ribs in the aileron and rudder surfaces and redistribution of the mass balance in the aileron, rudder and elevator surfaces.
- Applied: December 17, 1986
- Status date: January 13, 2017
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A21](https://openairdocs.org/tcds/3A21)
- Certificate PDF: https://openairdocs.org/files/sha256/0d/0d/0d0d2e7d07cbdc825f26cda8f69c29a5312689ec13c732c80922d28227dcc45b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FA364B513822A8E4862580B4006D5C01.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA3753NM

## ADs that name it (0)

None.

## Approved models (9)

- Cessna Aircraft Company 210K ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210L ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210M ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210N ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company P210N ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210K ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210L ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210M ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210N ([TCDS 3A21](https://openairdocs.org/tcds/3A21))

## 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 SA3753NM Griggs Aircraft Refinishing, LLC.

172 Runway Road Tunkhannock, PA 18657 Federal Aviation Regulations.

1. Installation of stiffening ribs in the aileron and rudder surfaces and redistribution of the mass balance in the aileron, rudder, and elevator surfaces, in accordance with FAA sealed O&N Aircraft Modifications, Incorporated, Master Drawing List No.

ON-10000, Revision B, dated October 7, 1987, or later FAA Approved sealed revision.

1. The installer must determine whether this design change is compatible with previously approved modifications

2. The limitations and conditions of data sheet 3A21 apply to aircraft modified by these control surface(s) installations and redistributions.

3. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

Gaetano Sciortino Manager New York Aircraft Certification Office Cessna Aircraft Company P210N, 210K, 210L, 210M, 210N, T210K, T210L, T210M, & T210N June 8, 2015, October 15, 2015, June 22, 2016, January 13, 2017 December 17, 1986 December 9, 1987 3A21 2

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

To (Name and address of transferee)

From (Name and address of grantor)

2 SA3753NM

## Every issue (4)

- January 13, 2017: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/0d/0d/0d0d2e7d07cbdc825f26cda8f69c29a5312689ec13c732c80922d28227dcc45b)
- June 22, 2016: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/a4/42/a4427d2ca60c0fe49a222574d9e71334f1ccf784aaf901c607b4ee838086660e)
- October 15, 2015: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/55/b4/55b460050df377b950638cbd6c15294e817de328705516bb8b29236e440acb99)
- June 8, 2015: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/64/77/647728c1c8656ec9556f46dc89a95a617bf64bf493902b5f0d49e929eca4582d)

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