STC SA01078SE

Supplemental type certificate · Aero Air, LLC

Holder
Aero Air, LLC · United States
Status
Current · Issued
Status date
April 17, 2002
Applied
September 9, 1999
Product
Aircraft · Small Multi-Engine
Certification basis
Part 21, Part 23
Data sheet
TCDS2A4

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of externally mounted fuel pump manufactured in accordance with Master Drawing List AEA105-90, Revision A, dated April 5, 2002, or later FAA approved revision, and installed in accordance with Installation Instructions VT-AEA105-12, Revision IR, dated April 5, 2002, or later FAA approved revision. Maintain in accordance with Instructions for Continued Airworthiness AEA-105-13, Revision IR, dated April 5, 2002, or later FAA approved revision.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate Number SA01078SE

This certificate, issued to Aero Air, LLC 2050 NE 25th Ave.

Hillsboro, OR 97124 Part 23 of the Federal Aviation Regulations.

Original Product  Type Certificate Number: 2A4 Make: Twin Commander Model: 690, 690A, 690B

Description of the Type Design Change: Installation of externally mounted fuel pump manufactured in accordance with Master Drawing List AEA105-90, Revision A, dated April 5, 2002, or later FAA approved revision, and installed in accordance with Installation Instructions VT-AEA105-12, Revision IR, dated April 5, 2002, or later FAA approved revision. Maintain in accordance with Instructions for Continued Airworthiness AEA-105-13, Revision IR, dated April 5, 2002, or later FAA approved revision.

Limitations and Conditions: This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the relationship between this change and other previously approved modification will introduce no adverse effect upon the airworthiness of the aircraft. A copy of this Certificate must be maintained as part of the permanent records for 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.

Date of application: September 9, 1999 Date reissued:

Date of issuance: April 17, 2002 Date amended:

Any alteration of this certificat e is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both.

_ (Signature) Acting Manager, Seattle Aircraft Certification Office

(Title)

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 3

MakeModelData sheet
Twin Commander Aircraft Corporation6902A4
Twin Commander Aircraft Corporation690A2A4
Twin Commander Aircraft Corporation690B2A4