Epstein Secrets

79-035 Exclusive Broker -Jet Advisors, LLC 9769 W. 119th Drive, Suite 33 Broomfield, CO 80021-2711

Honeywell MCS-3000; TAWS: Honeywell Mark V EGPWS w/RAAS & windshear detection; TCAS: Honeywell TCAS-II: Transponder Dual Collins TDR-94D w/enhanced Mode S; Weather Radar: Honeywell Primus 880: GULFSTREAM G-IVSP SN # IV-1305 Aircraft Information (Page • 1. .1. — • .„4: P•31 flat I, EFTA_R1_000122

tions, please call me at (319) 295-0618. Douglas W. Jessen Collins Avionics Certification Center Ma

ns on-site) STC ST00881WI-0 Modification of Collins TCAS II System Installation with Collins TTR-920 Change 6.04a Receiver Transmitter and TPR-900 Mode S to a Collins TCAS II System Installation with Collins TTR-920, Collins TTR-921 or Collins TTR-4000 Change 7.0 TCAS II Receiver Transmitter and opti

28, 1997, 8110-3 approved by D.E.R. SW-880, John W. Goswick July 28, 1997. END SDNYGlvl_02759883

units accommodate Mode C • altitude input o( 1OO-foot increments and that the system will be tracked and coordinated by Intruding aircraft when the Mode S transponder CA field Is act at CA•7. • (bl-WPrtor to Anther' flight 'after accompUshin,i the requinneents- otperageapir (eat this?. -.W.—nrylle di

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mately 1090 MHz • Transponder test set tail number matches aircraft • Transponder test set — Mode S UFO Test, RI =I I • Transponder test set — Mode S UF5 Test, FS =0 10. Reset the LDG GR CTL circuit breaker. (On Ground) I I. On transponder test set, initiate the Auto Test Sequence by pressing the

TION(S) SW - 880 Systems & Equipment // John W. Goswick V orm - EFTA00277818 a • . ••

e units accommodate Mode C altitude input of 100-foot Increments and that the system will be tracked and coordinated by Intruding aircraft when the Mode S transponder CA field Ls set at CA.7. • • (b) WPrior. to further -after accomplishing the requirements- of paragrapir (al- of tidal? AD.—revise t