STC SR00853DE

Supplemental type certificate · Upper Limit Aviation

Holder
Upper Limit Aviation · United States
Status
Current · Amended
Status date
June 27, 2024
Applied
September 9, 2013
Product
Aircraft · Rotorcraft
Certification basis
Part 27
Data sheets
TCDSH2SWTCDSH9EU

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

What it approves

Installation of Fibrotek survey stinger

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 AviationAdministration Supplemental Type Certificate Number: SR00853DE

This certificate issued to: Upper Limit Aviation 619 North 2360 West Salt Lake City, Utah 84116 27 of Title 14 CFR .

Original Product see Rotorcraft Model List Make: see Rotorcraft Model List SR00853DE Type Certificate Number:

Model: see Rotorcraft Model List SR00853DE Description of Type Design Change:

Installation of Fibrotek Survey Stinger on various rotorcraft models listed in Aircraft Model List SR00853DE.

Date of Application:9/9/13 Date Reissued:

3/23/17

Date Amended: 6/27/2024

Title: for Manager, West Certification Branch

United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate Number: SR00853DE

Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SR0853DE

United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate

(Continuation Sheet) Number: SR00853DE Limitations and Conditions (continued from Page 1):

1. This approval does not include installation of equipment inside the Fibrotek survey stinger. This approval only certifies the installation of a hollow Fibrotek Survey Stinger (FST). Installation of equipment inside the FST would require a separate FAA approval for each specific installation, which would include effects on; a) electrical loads, b) electromagnetic interference (EMI) and c) electromagnetic compatibility (EMC).

2. The installation should not be incorporated on any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration of the aircraft will not introduce any adverse effect the airworthiness of the aircraft.

3. Must manufactured in accordance with Master Drawing List for that aircraft on the Aircraft Model List.

4. Installations of this STC must be operated in accordance the Flight Manuals listed for that aircraft on the Aircraft Model List.

5. Installations of this STC must be maintained in accordance with the Instructions for Continued Airworthiness listed for that aircraft on the Aircraft Model List.

6. If the holder permits another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

End

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 · 12

MakeModelData sheet
Airbus HelicoptersAS350BH9EU
Airbus HelicoptersAS350B1H9EU
Airbus HelicoptersAS350B2H9EU
Airbus HelicoptersAS350B3H9EU
Airbus HelicoptersAS350BAH9EU
Airbus HelicoptersAS350DH9EU
Airbus HelicoptersAS350D1H9EU
Bell Helicopter Textron Canada Limited206BH2SW
Bell Helicopter Textron Canada Limited206LH2SW
Bell Helicopter Textron Canada Limited206L-1H2SW
Bell Helicopter Textron Canada Limited206L-3H2SW
Bell Helicopter Textron Canada Limited206L-4H2SW

Every issue · 2

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
June 27, 2024Amended, currentCertificateApproved model list
March 23, 2017Issued, earlier issueCertificate