# STC SA01436DE

- Type: Supplemental type certificate
- Status: Historical, Reissued
- Holder: Centri-Lube Technologies LLC, United States
- Description: Installation of Firewall Forward Technologies, LLC modified camshaft.
- Applied: July 9, 1998
- Status date: March 16, 2010
- Product: Engine
- Certification basis: Part 21
- Data sheets: [TCDS 1E4](https://openairdocs.org/tcds/1E4), [TCDS E-295](https://openairdocs.org/tcds/E-295), [TCDS E10EA](https://openairdocs.org/tcds/E10EA), [TCDS E14EA](https://openairdocs.org/tcds/E14EA), [TCDS E19EA](https://openairdocs.org/tcds/E19EA)
- Certificate PDF: https://openairdocs.org/files/sha256/89/39/8939c2efc9ec6cabe01634925a1543db3fe4696278c3380ebb06cecb7d8ce936
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2A9AF91686BEBE22862576EF0058A243.0001
- DRS record last changed: July 15, 2010
- Page: https://openairdocs.org/stc/SA01436DE

## ADs that name it (0)

None.

## Approved models (167, first 50)

- Textron Lycoming AVCO Corporation AEIO-540-D4A5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation AEIO-540-D4B5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation AEIO-540-D4C5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation AEIO-540-D4D5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation AEIO-540-L1B5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation AEIO-540-L1B5D ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation AEIO-540-L1D5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-A1A5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-AA1A5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-AA1B5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-AB1A5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-AC1A5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-AE1A5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-B1A5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-B1B5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-B1C5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-C1B5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-C1C5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-C2C ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-C4B5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-C4B5D ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-C4C5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-C4D5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-C4D5D ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-D4A5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-D4B5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-D4C5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-E1A5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-E1B5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-E1C5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-G1A5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-G1B5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-G1C5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-G1D5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-G1E5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-G1F5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-J4A5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-K1A5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-K1A5D ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-K1B5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-K1B5D ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-K1C5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-K1D5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-K1E5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-K1E5D ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-K1F5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-K1F5D ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-K1G5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-K1G5D ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540-K1H5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))

All 167: https://openairdocs.org/stc/SA01436DE/models.md

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA01436DE This certificate issued to: Centri-Lube Technologies, LLC 748 Whalers Way Fort Collins, CO 80525 Part 33* of the Federal Aviation Regulations. *See applicable Type Certificate Data Sheet (T.C.D.S.) for certification basis Original Product Type Certificate Number:

Make: *See attached FAA Approved Model List (AML) for list of approved airplane models and applicable T.C.D.S.

Description of Type Design Change: Installation of Firewall Forward Technologies, LLC modified camshaft in accordance with Master Drawing List FWF-MDL-ST9721LA-E, revision G, dated 2/14/03 or later FAA approved revision. This installation must be done concurrently with STC SA01435LA, which modifies the airplane installation.

Limitations and Conditions: Compatibility of this design change with previously approved modifications must be determined by installer. The installation should not be incorporated in any airplane 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. 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 airplane. 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. See continuation page 3.

Date of Application: July 9, 1998 Date Reissued: 11/10/2009, March 16, 2010 Date of Issuance: February 14, 2003 Date Amended:

FEDERAL AVIATION By Direction of the Administrator elissa Saador Melissa Sandow (Signature) TOMINIST RATION Small Airplane Program Manager Northwest Mountain Region Denver Aircraft Certification Office (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA01436DE Revision Log:

Page No. 1 2 3 Rev. No. - Description of Change - continued:

Certification Basis for this modification: 14 CFR part 33 at Amendment 0 effective February 1, 1965, through amendment 18.

Limitations and Conditions: - continued:

Continued Airworthiness Instructions, document number FFT-CAI-001, is applicable to airplanes modified in accordance with this STC.

This installation must be done concurrently with STC SE01435LA, which modifies the airplanes installation.

-END-

## Every issue (2)

- March 16, 2010: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/89/39/8939c2efc9ec6cabe01634925a1543db3fe4696278c3380ebb06cecb7d8ce936)
- November 10, 2009: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/ad/be/adbe7ead59114e17e004a61dfda8d392fb816f98c834599441415725bb72041a)

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