STC SA7232SW-D

^/I&zt6/<i& States of America Bepartmcnt of transportation—federal atriation Administration mpplemental 'Cgpe Certificate SA7232SW-D Dassault Falcon Jet P.O. Box 967 Little Rock, Arkansas 72203 .M&^^de^ 25 Federal Aviation A46EU Dassault Aviation Mystere - Falcon 900 Battery Installation (36 or 40 hour) in accordance with Drawing List Report No. F90-01053, Revision G, dated 10-18-01, or later FAA approved revision.

See Page 2.

See Page 2.

tw^ £$ctmvn*& May3, 1988 May 24, 1988 9-27-93, 10-9-01, 11-3-01 Rev. 3 (Signature ) Andrew A. Boersma DAS8SW COORDINATOR (Title)

FAAFotM 8110-2(10-68)

Btpartmcnt of Transportation-ftdcral gtiatfon administration Supplemental t:gpe Certificate(Continuation gheet) SA7232SW-D Revision 3 Description of Type Design Change (Continued):

1) When the -501 installation is utilized:

FAA Approved Airplane Flight Manual Supplement, Report No. 36071-1, dated 5-24-88, or later FAA approved revision is required.

2) When the -503 installation is utilized:

a) FAA Approved Airplane Flight Manual Supplement, Report No. 36071-2, dated 9-27-93, or later FAA approved revision is required.

b) Airplane Maintenance Manual Supplement Report No. 36333, dated 8-26-93, or later FAA approved revision is required.

3) When the -505 installation is utilized:

a) FAA Approved Airplane Flight Manual Supplement, Report No. 36071-3, dated 10-9-01, or later FAA approved revision is required.

b) Airplane Maintenance Manual Supplement Report No. 36333, dated 8-26-93, or later FAA approved revision is required.

4) When the -507 installation is utilized:

c) FAA Approved Airplane Flight Manual Supplement, Report No. 36071-4, dated 11-3-01, or later FAA approved revision is required.

d) Airplane Maintenance Manual Supplement Report No. 36943, dated S-25-01, or later FAA approved revision is required.

Limitation and Conditions:

1) The F90-01053-501 Installation is valid only in the Mystere Falcon 900 Model Aircraft.

2) The F90-01053-503 Installation is valid only in the Mystere Falcon 900 Model Aircraft.

3) The F90-01053-505 Installation is valid only in the Falcon 900C Definition Aircraft.

4) The F90-01053-507 Installation is valid only in the Falcon 900C Definition Aircraft.

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

FAA FORM «t 10-2-1 (IO-«») This ctrlifitatt may be traniftrrtd in accordant with FAR 21.17.

PAGE 2 OF 2 CAGES C FAA AC 82 03578

lit. Slate, and ^IT code I Extent of Authority (if licensing agreement):

Signature of grantor (In ink): __