STC SA7041SW-D

<Hmtrd£tataofamtrica Bcpartment of transportation— iefltral 3toiation administration Supplemental "Cgpe Certificate SA7041SW-D Dassault Falcon Jet P.O. Box 967 Little Rock, Arkansas 72203 ^/^.^i^z^^

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A46EU Dassault Aviation Mystere - Falcon 50 Installation of the Collins Dual ADS-80/82 Air Data System in accordance with Drawing List Report No.

F50-01076, Revision Y, dated 4-7-97, or later FAA approved revision.

See Page 2.

See Page 2.

£Xcfo March 17, 1986 September12, 1986 9-15-86, 10-10-86, 10-25-87, See Page 2. Rev. 10 v £j(dmvntAJra£>r' (Signature) Andrew A. Boersma DAS8SW COORDINATOR (Title)

47.

fHtttt ff flJBfTlfB Btpartmtnt of 'Transportation- Jpctoa! action administration Supplemental t:gpe Certificate(Continuation &hCtt) SATCMISW-D Revision 10 Date Amended: 9-11-90, 5-30-91, 10-30-91, 1-7-92, 10-5-95, 4-5-97, 4-10-97.

1) Configuration 1: F50-01 076-507 Installation (ADS-82, no cross switching): FAA Approved Airplane Flight Manual Supplement, Report No. 35313-2, Rev. D dated 12-19-91, or later FAA approved revision is required.

2) Configuration 2: F50-01 076-509 Installation (ADS-82, with cross switching): FAA Approved Airplane Flight Manual Supplement, Report No. 35313-5 dated 12-19-91, or later FAA approved revision is required.

3) Configuration 3: F50-01 076-511 Installation (ADS-80, RVSM): FAA Approved Airplane Flight Manual Supplement, Report No. 35313-6 dated 4-5-97, or later FAA approved revision is required.

4) Configuration 4: F50-01 076-51 3 Installation (ADS-82, RVSM, no cross switching) FAA Approved Airplane Flight Manual Supplement, Report No. 35313-2 Rev. D dated 12-19-91, or later FAA approved revision is required.

5) Configuration 5: F50-01 076-51 5 Installation (ADS-82, RVSM, with cross switching) FAA Approved Airplane Flight Manual Supplement, Report No. 35313-5 dated 12-19-91, or later FAA approved revision is required.

6) Optional TAI-80A Installation : FAA Approved Airplane Flight Manual Supplement, Report No. 3531 3-4 dated 9-1 1-90, or later FAA approved revision is required.

1 ) Compatibility of this modification with other previously approved modifications must be determined by the installer.

2) This STC utilizes STC SA4764SW, issued September 7, 1982, as a certification basis of compliance.

FAA FOMM •lio-2-l (lo-W) This ttrtificatt may It tronsfentJ in accordant! with FAR 21.47.

PAGE OF PAGES 22 C FAAAC820357B

INSTRUCTIONS : The transfer endorsement below may be used to notify the appropriate FAA Regional Office of the transfer of this Supplemental Type Certificate.

The FAA will reissue the certificate in the name of the transferre and forward it to him.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (9{ame of transferee) (Address of transferee) _ (y^anier and street) (City, State, andZlT code.)

from (9{ame of grantor) (Trint or type) ___^ __ _ (Address of grantor) (9{um6er and street) (City, State, amCZlf code) Exent of Authority (if licensing agreement) :

Signature of grantor (In Page 2 of 2