# STC SA02511CH

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Saf-Air Products Inc., United States
- Description: Installation of Saf-Air Products fuel quick drain backing plate C187 and fuel drain valve B187
- Applied: June 22, 2007
- Status date: January 7, 2008
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13), [TCDS 3A21](https://openairdocs.org/tcds/3A21), [TCDS 3A24](https://openairdocs.org/tcds/3A24), [TCDS 5A6](https://openairdocs.org/tcds/5A6), [TCDS A16CE](https://openairdocs.org/tcds/A16CE), [TCDS A4CE](https://openairdocs.org/tcds/A4CE), [TCDS A9CE](https://openairdocs.org/tcds/A9CE)
- Certificate PDF: https://openairdocs.org/files/sha256/a2/da/a2da689e16166e20410b5f5c385f00f4a6e8334945a79a3d2860e3f9c6ea9512
- Approved model list and other attachments: [SA02511.AML.pdf](https://openairdocs.org/files/sha256/95/9b/959bb8cdc14ff58af79d64f630c03e19097a24376e5c1c8c7b314168222131b8)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C520352E562F6E9A862574BA00662C2F.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02511CH

## ADs that name it (0)

None.

## Approved models (83, first 50)

- Cessna Aircraft Company 180 ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180A ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180B ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180C ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180D ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180E ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180F ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180G ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180H ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180J ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180K ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182A ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182B ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182C ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182D ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182E ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182F ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182G ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182H ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182J ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182K ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182L ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182M ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182N ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182P ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182Q ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 185 ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185A ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185B ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185C ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185D ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185E ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 188 ([TCDS A9CE](https://openairdocs.org/tcds/A9CE))
- Cessna Aircraft Company 188A ([TCDS A9CE](https://openairdocs.org/tcds/A9CE))
- Cessna Aircraft Company 188B ([TCDS A9CE](https://openairdocs.org/tcds/A9CE))
- Cessna Aircraft Company 206 ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company 207 ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company 207A ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company 210 ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210-5 (205) ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210-5A (205A) ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210A ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210B ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210C ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210D ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210E ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210F ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company A185E ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company A185F ([TCDS 3A24](https://openairdocs.org/tcds/3A24))

All 83: https://openairdocs.org/stc/SA02511CH/models.md

## 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.

Part * of the * Regulations.

Original Product--Type Certificate Number: *See attached FAA Approved Model List (AML) Make: *No. SA02511CH for list of a pproved airplane models and Model: *applicable airworthiness regulations Description of Type Design Change:

Installation of Saf-Air Products fuel quick drain backing plate C187 and fuel drain valve B187 in accordance with the Saf-Air Products Installation Instructions, SA-C187, rev. none, dated August 27, 2007 or later FAA approved revision.

1. The following approved Alternative Method of Compliances (AMOC’s) can be granted based on the specific sections of Airworthiness Directive (AD)84-10-01R1 and requirements identified below:

a. Paragraph (a); specifically, the B187 drain valve is an AMOC to the AD required “quick drains” drain valve requirements, when installed with the C187 backing plate in the wing tank, bladder sump area.

b. Paragraph (c)(2); specifically, the C187 backing plate and B187 drain valve are an AMOC to the Cessna drain kit parts described in Cessna service Letter SE 84-9, and required by this AD.

c. The above AMOC’s are only applicable to airpla nes with fuel bladders that are manufactured in January of 1984 or after. The above AMOC’s do not relinquish the airplane owner from any of the other requirements of AD84-10-01R1.

2. Compatibility of this design change with previous modifications must be determined by the installer.

3. A copy of this certificate must be maintained as part of the permanent records for the modified aircraft.

4. 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.

Saf-Air Products, Inc.

32839 Manor Park Drive Garden City, MI 48135 Date reissued :

( Signature) Thaddeus D. Krolicki Jr.

Manager, Propulsion Branch Chicago Aircraft Certification Office

(Ti l )

Date of application : June 22, 2007

Date of issuance : January 7, 2008

FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES

Number

### SA02511.AML.pdf

**FAA APPROVED MODEL LIST (AML) NO. SA02511CH SAF-AIR PRODUCTS, INC.**

**INSTALLATION OF C187 BACKING PLATE AND B187 FUEL DRAIN VALVE**

Date of Issuance: January 7, 2008

1 of 2

**ORIGINAL TYPE**

**CERTIFICATION**

**INSTALLATION**

**INSTRUCTIONS**

AFM

AML

**ITEM**

**AIRCRAFT MAKE**

**AIRCRAFT MODEL**

**CERTIFICATE NUMBER**

**BASIS FOR**

**ALTERATION**

**NUMBER**

**REVISION NO. / DATE**

**SUPPLEMENT NO. / DATE**

AMENDMENT DATE 1 Cessna

180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 180K

**5A6 CAR 3 SA-C187**

Rev. None, Dated 8/27/07 or later FAA approved revision.

N/A Original 1/16/2008 2 Cessna 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, R182

**3A13 CAR 3, FAR 23 SA-C187**

Rev. None, Dated 8/27/07 or later FAA approved revision.

N/A Original 1/16/2008 3 Cessna 185, 185A, 185B, 185C, 185D, 185E, A185E, A185F

**3A24 CAR 3 SA-C187**

Rev. None, Dated 8/27/07 or later FAA approved revision.

N/A Original 1/16/2008 4 Cessna 188, 188A, 188B, A188, A188A, T188C, A188B

**A9CE FAR 23 SA-C187**

Rev. None, Dated 8/27/07 or later FAA approved revision.

N/A Original 1/16/2008

**FAA APPROVED MODEL LIST (AML) NO. SA02511CH SAF-AIR PRODUCTS, INC.**

**INSTALLATION OF C187 BACKING PLATE AND B187 FUEL DRAIN VALVE**

Date of Issuance: January 7, 2008

2 of 2

**ORIGINAL TYPE**

**CERTIFICATION**

**INSTALLATION**

**INSTRUCTIONS**

AFM

AML

**ITEM**

**AIRCRAFT MAKE**

**AIRCRAFT MODEL**

**CERTIFICATE NUMBER**

**BASIS FOR**

**ALTERATION**

**NUMBER**

**REVISION NO. / DATE**

**SUPPLEMENT NO. / DATE**

AMENDMENT DATE 5 Cessna 206, U206, U206A, TU206A, U206B, TU206B, U206C, TU206C, U206D, TU206D, U206E, TU206E, U206F, TU206F, U206G, TU206G P206, P206A, TP206A, P206B, TP206B, P206C, TP206C, P206D, TP206D, P206E, TP206E,

**A4CE CAR 3 SA-C187**

Rev. None, Dated 8/27/07 or later FAA approved revision.

N/A Original 1/16/2008 6 Cessna 207, T207, 207A, T207A 210, 210A, 210B, 210C, A16CE FAR 23 SA-C187

Rev. None, Dated 8/27/07 or later FAA approved revision.

N/A Original 1/16/2008 7 Cessna 210D, 210E, 210F, T210F, 210-5 (205), 210-5A (205A)

**3A21 CAR 3 SA-C187**

Rev. None, Dated 8/27/07 or later FAA approved revision.

N/A Original 1/16/2008

FAA Approved:_________________________________________ Thaddeus D. Krolicki, Jr.

Manager, Propulsion Branch Chicago Aircraft Certification Office

## Every issue (1)

- January 7, 2008: Issued, Current. [certificate](https://openairdocs.org/files/sha256/a2/da/a2da689e16166e20410b5f5c385f00f4a6e8334945a79a3d2860e3f9c6ea9512), [SA02511.AML.pdf](https://openairdocs.org/files/sha256/95/9b/959bb8cdc14ff58af79d64f630c03e19097a24376e5c1c8c7b314168222131b8)

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