# STC SA00356DE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Fly In Vacations, United States
- Description: Installation of modified Textron Lycoming engine equipped with turbo normalizing system.
- Applied: October 22, 1996
- Status date: April 12, 2012
- Product: Aircraft, Single-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A12SO](https://openairdocs.org/tcds/A12SO)
- Certificate PDF: https://openairdocs.org/files/sha256/69/da/69da4a741f90c9159d0c96abe05b2db3438cd1e86939003170b98da437d3803f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/18A213B273A67C8A862579E9005B7C25.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00356DE

## ADs that name it (1)

- [AD 2002-19-03](https://openairdocs.org/ad/2002-19-03): Crankshaft · Lycoming Engines IO-540-A1A5, IO-540-AA1A5, IO-540-AA1B5 and 81 more. Effective Sep 20, 2002. Named in the applicability

## Approved models (2)

- Commander Aircraft Company 114 ([TCDS A12SO](https://openairdocs.org/tcds/A12SO))
- Commander Aircraft Company 114A ([TCDS A12SO](https://openairdocs.org/tcds/A12SO))

## 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.

This Certificate issued to Fly In Vacations 6395 Parkhill Road Santa Margarita, California 93453 Part 23* of the Federal Aviation Regulations *Certification basis is set forth in Type Certificate Data Sheet (TCDS) Original Product Type Certificate Number :

A12SO

Commander Aircraft Company

114, 114A Description of Type Design Change: Installation of a modified Textr on Lycoming engine equipped with a Turbonormalizing system in accordance with FAA Appr oved Camarillo Aircraft Service Master Drawing List (MDL) CA540, Revision N/C, dated June 24, 1999, or later FAA approved revisions. Camarillo Aircraft Service FAA Approved Pilot’s Operating Handbook and/or Airplane Flight Manual Supplement AFMS-114-CAS dated March 14, 2000, or later FAA approved revisions, is required with this installation.

See NOTE 4 for additional FAA approvals for this installation.

Limitations and Conditions: The installation should not be incor porated 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. This 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. See Page 3 for continuation.

Date of application : October 22, 1996

Date of issuance : October 14, 1998

Date reissued : December 28, 1998, February 28, 2012, April 12, 2012

Date amended : March 14, 2000

( Signature) Thomas A. Enyart Manager, Propulsion Branch Los Angeles Aircraft Certification Office ( Title)

NOTE:

**DO NOT DELETE THIS PAGE.**

**DO NOT ADD ANY DATA TO THIS PAGE.**

**THIS PAGE IS FOR PAGE NUMBERING PURPOSES, PLEASE DISCARD PRINTED COPY.**

Number SA00356DE

NOTE 1: Installation of STC SE00357DE is required with this modification.

NOTE 2: The following cockpit instrument must be marked accordingly:

Manifold pressure gage: 28.5 In Hg. (red line)

NOTE 3: Refer to Camarillo Aircraft Service FAA Approved Pilot’s Operating Handbook and/or Airplane Flight Manual Supplement AFMS-114-CAS, dated March 14, 2000, or later FAA approved revisions, for required placards.

NOTE 4: Turbo-Flite 540 (Turbo 2000 Corp.) Master Drawing List No. TF540, Revision A, dated June 24, 1998, or later FAA approved revision; FAA Approved Airplane Flight Manual Supplement AFMS-114, Revision IR, dated October 14, 1998, or later FAA approved revisions; and Instruction for Continued Airworthiness, Turbo-Flite Operations and Maintenance Manual Report 135-10, Revision none, dated March 12, 1998, or later FAA approved revisions; are also approved for this installation.

-END-

## Every issue (2)

- April 12, 2012: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/69/da/69da4a741f90c9159d0c96abe05b2db3438cd1e86939003170b98da437d3803f)
- February 28, 2012: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/f3/90/f390114b8774c3c95dc483b6bc90cb4195cbc057d0fcce871a9f7bf772aa39d9)

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