# STC SA4404NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Falcon Jet Corporation, United States
- Description: Installation of Sperry AD-650A ADI and RD-650A HSI flight instruments.
- Applied: January 19, 1982
- Status date: April 18, 1984
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A7EU](https://openairdocs.org/tcds/A7EU)
- Certificate PDF: https://openairdocs.org/files/sha256/8c/c3/8cc3118355fd57152731fb785e514d7092bf0de4071c5df5413b6d733cf9a5b0
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5B1F971795B7D69E85256CC2000E3C45.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA4404NM

## ADs that name it (0)

None.

## Approved models (1)

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

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

niced States of Slarico Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA4404NM This certificate issued to: Falcon Jet Corporation Pard 4bt y the CiVil Air Requlalions. (*See T.C. Data Sheet ATEU, Rev. 9, for certification basis) Original Product Type Pertificate, Nurter AZEU

• Make Avions Marcel Dassault (A.M.D.)

Merted Fan Jet Falcon Series F Description of Type Design Change: Installation of Sperry AD-650A ADI and RD-650A ISI flight instruments in accordance with FAA sealed AiResearch Data Index Lisi No. IL 1101919 "B" Revision, dated February 1, 1982, or later FAA sealed revision. AiResearch Airplane Flight Manual Supplement, Document No. C-4071, FAA approved on March 12, 1982, or later FAA approved revision is required as part of this modification.

Limitations and Conditions: The approval of this change in type design applies to A.M.D. Model Fan Jet Falcon Series F airplanes only. 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 interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft.

This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight of the fuselage.

Blomer Manager, western Aircraft Certification Office (Title) 47 TAA FORM 8110-2 (10-60)

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) - (Number and street) (City, State, and ZIP code ) from (Name of grantor) (Print or type) - (Address of grantor) (Number and street) (City, State, and ZIP code ) Extent of Authority (if licensing agreement):

Signature of grantor (In ink): _

## Every issue (1)

- April 18, 1984: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/8c/c3/8cc3118355fd57152731fb785e514d7092bf0de4071c5df5413b6d733cf9a5b0)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.