STC SA00832SE

FAA DRS lists SA00832SE as Current · Issued, held by Micro AeroDynamics Inc, for Cessna Aircraft 170B and Cessna Aircraft 170A. Recorded change: Installation of vortex generators on wings and tail surfaces. Snapshot dated June 30, 2026.

FAA-listed holder

Micro AeroDynamics Inc

Aircraft configurations

FAA revision date

August 4, 2000

FAA status

Current · Issued

Recorded modification

What the FAA record covers

SA00832SE identifies the approval, recorded holder, named aircraft, and modification scope. It does not confirm kit availability, serial-number effectivity, data rights, price, or installation authority.

Applicability

Aircraft named in FAA DRS

Named aircraft: Cessna Aircraft 170B and Cessna Aircraft 170A. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Cessna Aircraft 170BA-799 Cessna Aircraft 170AA-799

SA01293WIOther aircraft modificationsRevised Nov 22, 2004

Operation of airplane on unleaded automotive gasoline, 87 minimum antiknock index and leaded automotive gasoline, 88 minimum antiknock index (RON+MON)/ 2 per ASTM Specification D-439. Intermixing with aviation gasoline also approved. Data required: 1. Petersen Drawing No. 1521A dated November 15, 1989, or later FAA Approved revision. 2. Airplane Flight Manual Supplement dated November 22, 2004 or later FAA Approved revision.

FAA holder: Petersen Aviation Inc

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ST01475SEOther aircraft modificationsRevised Nov 22, 2004

Descriptive data pertaining to this design change are considered inadequate for duplication on other products. This approval is limited to the McDonnell Douglas Model DC-9-15 Serial Number 45797 only.

FAA holder: AeroMech Incorporated

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ST02027NYOther aircraft modificationsRevised Nov 22, 2004

Limited to installation on serial number 1017 ONLY.

FAA holder: Innotech Aviation Ltd

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ST10354SCOther aircraft modificationsRevised Nov 19, 2004

Installation of a dual TAWS system in accordance with Pyka MDL 1B07-DL-001-501 Rev. D dated October 29, 2004, or later FAA approved revision. Airplane Flight Manual Supplement 1B07-FM-001 Rev. IR dated November 05, 2004, or later FAA approved revision, is required.

FAA holder: Pyka Aerospace Corp

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FAA record reference

STC number: SA00832SE
Product: Aircraft · Single-Engine
Country: United States
Application date: May 31, 2000
Revision date: August 4, 2000
CFR references: Part 3, Part 21

What the FAA record covers

Aircraft named in FAA DRS

Related other aircraft modifications STCs

Descriptive data pertaining to this design change are considered inadequate for duplication on other products. This approval is limited to the McDonnell Douglas Model DC-9-15 Serial Number 45797 only.

Limited to installation on serial number 1017 ONLY.

Installation of a dual TAWS system in accordance with Pyka MDL 1B07-DL-001-501 Rev. D dated October 29, 2004, or later FAA approved revision. Airplane Flight Manual Supplement 1B07-FM-001 Rev. IR dated November 05, 2004, or later FAA approved revision, is required.

FAA record reference