Epstein Secrets

nics: Collins Proline 3-Tube EFIS Dual Collins FMS-5000's w/ GPS 4000 Collins APS-4000 Autopilot Collins VHF-422C Comm Dual Collins VIR-432 Nays Collins ADF-462 ADF Dual Collins DME-422 DME Dual Collins TDR-94D's Mode "S" Transponders Collins ALT-55B Radar Altimeter Collins SDU-640A RMI Dual Coll

and 17 EFTA_00242393 EFTA01327509 SDNY_GM_02755472 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_00242394 EFTA01327510 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION CROSS-REFERENCE-RECORDATION ECORDED CONVEYANCE FILED IN: NNUM: 493LX SERIAL NUM: RK-244 MFR: RAYTHEDN AIRCRAFT

ished Of more space Is required attach additional sheets. Identify with aircraft nationality and registration mark and date work completed) Removed Collins Part Number 822.9210-008 TDR-94D Mode S Diversity Transponders Serial Numbers 2221 and 3672 and Installed factory modified per Service Bulletin 504

and 17 EFTA_00240740 EFTA01326333 SDNY_GM_02753819 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00240741 EFTA01326334 U.S. DEPARTMENT OF TRANSPORTATION. FEDERAL AVIATOR ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE April 4, 2007 AIRCRAFT OR AIRCRAFT COMPONENT

k and date work completed.) Modified the existing Third Comm & Nat Systems by removing the Gables G6860-09 Conun/Nav Control Head, and installing a Collins CTL-23 Digital Control Head, P/N 622-9851-001. The third Comm / NAV system's interface was retained as previously installed with the exception of th

PRINTING OFFICE: 1,12-755-017/60I57 SONY GM 02754077 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_002 40999 EFTA01326592 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATION DATE February 9.1996 AIRCRAFT OR AIRCRAFT COMPONENT

ing Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (IRS), dual internal GPS sensors, and VORIDME from the Collins No. 1 and No. 2 VORIDME systems in accordance with manufacture's InstalatIon and Checkout Manual No. 34-60-09, Rev. 2, dated August 15, 1997 or lat

nly." Additional Shies are Attached SDNY_GM_02759688 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246610 EFTA01331073 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE October 07,2006 AIRCRAFT OR AIRCRAFT COMPONENT

ing Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (IRS), dual internal GPS sensors, and VOR/DME from the Collins No. 1 and No. 2 VORJDME systems in accordance with manufacture's Installation and Checkout Manual No. ?4-60-09, Rev. 2. dated August 15, 1997 or la

.are. 14,-.1.-- DERT-810028-NE Structural FAA FOITTI 8110-3 (11-70) SUPERSEDES PREVIOUS EDITION ER01202.cloc EFTA00277686 a i EFTA00277687 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE June 18, 2001 AIRCRAFT OR AIRCRAFT COMPONENT I

te tapes. All channels'operated.normal. The tapes are on file at this facility. The operator was supplied with "Pilots Operation Instructions" for Collins AVR-101 Cockpit Voice Recorder", report no. A8910001. This report must be aboard.the aircraft during all flight operations. The above mentioned ins

to the cabin or cockpit -in accordance with FAR 45.23. 6 - 4.5? -8P9 Date of Issue Representative Designation/Office No. EFTA00278308 FAA_ U.S. DEPARTMENT OF TRANSPORTATION Form Antlered . . • FEDERAL AVIATION ADMINISTRATION Baer Bonn No. 04-R060.I FOR FAA L'SE ONLY ". MAJOR REPAIR AND ALTERATION oFFINOSoatfola111