# STC SA2243NM

- Type: Supplemental type certificate
- Status: Historical, Surrendered
- Holder: Hollingsead International Inc., United States
- Description: Installation of dual Tracor Model 7800 VLF/Omega Naviation System.
- Applied: May 23, 1983
- Status date: March 19, 2009
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 25
- Data sheets: [TCDS A7EU](https://openairdocs.org/tcds/A7EU)
- Certificate PDF: https://openairdocs.org/files/sha256/97/fc/97fcefe7f378a8a7421bb3d53ecde21bcc44a6189c84c94735f0763c8dca9f4b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3312A0B225DB1208862570D10068F6F7.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA2243NM

## ADs that name it (0)

None.

## Approved models (4)

- Dassault-Aviation Fan Jet Falcon Series C ([TCDS A7EU](https://openairdocs.org/tcds/A7EU))
- Dassault-Aviation Fan Jet Falcon Series D ([TCDS A7EU](https://openairdocs.org/tcds/A7EU))
- Dassault-Aviation Fan Jet Falcon Series E ([TCDS A7EU](https://openairdocs.org/tcds/A7EU))
- Dassault-Aviation Fan Jet Falcon Series F ([TCDS A7EU](https://openairdocs.org/tcds/A7EU))

## 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 Hollingsead International 7416 Hollister Avenue Goleta, CA 93117 Part 4b of t he Civil Air Regulations. *See T.C. Data Sheet A7EU Original Product Type Certificate Number A7EU Make : Avions Marcel Dassault Model : Fan Jet Falcon Series C, D, E and F Description of Type Design Change: Installation of dual Tracor Model 7800 VLF/Omega navigation system in accordance with FAA sealed Tracor Aviation Drawing List DL-329-001, Revision A, dated December 15, 1983; or later FAA sealed revision. FAA approved Tracor Aviation Airplane Flight Manual Supplement dated December 30, 1983 or later FAA approved revision is required as part of this installation.

Limitations and Conditions: The 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 interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of the aircraft. This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight of the fuselage. 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.

This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of application: May 23, 1983

Date of issuance : December 30, 1983

Date reissued: August 12, 1991; July 11, 1995;

March 15, 1996; April 1, 1998; August 1, 2005

( Signature)

Manager, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office (Title)

## Every issue (1)

- March 19, 2009: Surrendered, Historical. [certificate](https://openairdocs.org/files/sha256/97/fc/97fcefe7f378a8a7421bb3d53ecde21bcc44a6189c84c94735f0763c8dca9f4b)

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