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SITION AND OTHER NAVIGATION INFORMATION FROM THE NO. 1 UNS- ID FMS THROUGH AN EVENTIDE AVIONICS ARINC 419/429 ADAPTER UNIT AND THE AIRCRAFT'S NO. 3 HONEYWELL "LASERREF" INERTIAL REFERENCE SENSOR (IRS) DIRECTIONAL HEADING SYSTEM WHICH, PROVIDES MAP GRAPHICS AND BEARING ORIENTATION. THE FOLLOWING SWITCHES

NUED AIRWORTHINESS DUE TO THIS MODIFICATION. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES DUE TO THIS MODIFICATION. END K Additional Sheets Are Attached * V.S. G.P.O 1990-781.753 I SDNY_Gtol_02759780 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246702 EFTA01331165 a D

& RECEIVER / TRANSMITTER UNIT P/N 7012640-902 AND INSTALLED NEW WU- 880 ANTENNA & RECEIVER / TRANSMITTER UNIT P/N 7021450-801 (TSO C63c). INSTALLED A HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM CONSISTING OF AN LP-860 PROCESSOR P/N 7011822-904 (TSO C110) AND AN AT-855 ANTENNA PIN 7014062-901 (TSO C110). THE

6/11/01 BY STRUCTURES DER NO. DERT-510394-CE. THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES DUE TO THIS MODIFICATION. END K Additional Sheets Are Attached * U.S. G. P.O 1990-761-753 EFTA00277691 ••• yr 44t.c.c000v..)4 0 AgiA U ri't S • to 002 U.S. DEPARTMENT OF TRANSPORTATION PEDERAL AVIATION

ER AIRCRAFT EQUIPMENT. NO WIRING OR STRUCTURAL ALTERATIONS WERE ACCOMPLISHED. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER HONEYWELL MST67A MODE S TRANSPONDER SYSTEM MANUAL 006-00681-0006 WITH NO DISCREPANCIES. AN EMI TEST, REPORT NO.: G2B-20895-080 WAS CONDUCTED AND THE INSTALLE

above mentioned approved data and continues to meet the airworthiness criteria under which it was originally certificated. 18) No further entries. K Additional Sheets Are Attached EFTA00278136 U.S. DEPARTMENT OF TRANSPORTATION . . . FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULAT