What it approves
Installation of Collins FIS-85 flight instrument system and optional installation of Intercontinental Dynamics Corp. (IDC) servoed altimeter, mach/ airspeed indicators and barometric altimeter.
What the certificate saysOCR
This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA1213EA This certificate issued to: Falcon Jet Corporation P.O. Box 967 - Adams Field Little Rock, Arkansas 72203 Certifies that the change in the type design for the fellowing product with the limitations and conditions therefor as specified hereon meets the airerthiness requirement's of Part 25 of the Federal Aviation Regulations Original Product - Type berlificate Number: ASSEU Make: Avions Marcel Dassault-Breguet Aviation (AMD/BA) Model: Falcon 10 Description of Type Design Change:
Installation of Collins FIS-85 Flight Instrument System and optional installation of Intercontinental Dynamics Corporation's (IDC) Servoed Altimeter, Mach/Airspeed Indicators and Barometric Altimeter in accordance with Atlantic Aviation Corporation's (AAC) Drawing List No. AAC 80-16, Revision No. 4, dated November 3, 1980.
1. When pilot's and copilot's altimeters are servoed altimeters (requiring electrical power), the standby barometric altimeter must be installed.
2. When the Collins FIS-85 Flight Instrument System is installed, the FAA approved AAC Airplane Flight Manual Supplement No. 2, dated December 4, 1980, is required.
(See STC Continuation Sheet, Page 2)
Date of Application: August 25, 1980 Date Reissued: April 14, 1982 Date of Issuance: . December 4, 1980 Date Amended:
FEDERAL AVIATION By Direction of the Administrator Raymonal I. Borowski (Signature.)
TOMNIS RAISE RAYMOND J. BOROWSKI Chief, N.Y. Aircraft Certification Office (Title)
47.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SAI213EA Date Reissued: April 14, 1982 Limitations and Conditions: (Continued):
3. When the optional IDC instruments are installed, the FAA approved AAC Airplane Flight Manual Supplement No. 3, dated December 4, 1980, is required.
This approval should not be incorporated in any aircraft of this specific model on which other approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those previously incorporated approved modifications will not introduce any adverse effect upon the airworthiness of the aircraft.
....END....
FAA FORM 8110-2-1 (10-69) PAGE 2 OF 2 PAGES FAA AC 73-2651
INSTRUCTIONS. The transfer endorsement below may be used to notify the appropriate FAA F'egional Office of the transfer of this Supplemental Type Certificate.
The FAA will reissue the certificate in the name of the transferee and forward it to him.
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, Stale, and RIP code) Extent of Authority (if licensing agreement):.
Signature of grantor (In ink):
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Dassault Aviation | Falcon 10 | A33EU |