Epstein Secrets

light Management System: Long Range Navigation: Weather Radar: Transponder: TCAS II (2) Honeywell Primus 2 - VHF (1) Collins VHF-22B — VHF (2) Collins HF-628 with SELCAL (5) Honeywell Audio Panels (Primus 2) (1) Aircell Iridium— phone + ICS (3 phones) (1) Honeywell AFIS (2) Honeywell Primus2: V

r Cmptrs FZ500 (3) Honeywell IRS Laseref (2) Honeywell GPS (1) Honeywell Laser Trak w/ Display (1) Honeywell Primus P880 (color) (2) Honeywell — Mode S (enhanced) (1) Honeywell w/ change 7 E FTA_R1_00007929 EFTA01733622 Boeing 727 Executive — 20512 Page 6 FLIGHT DECK / AVIONICS Enhanced Groun

ght pulselites, vertical stabilizer AVNCS 13 EFTA_R1_01666752 EFTA02526495 =oneywell SPZ-8500 IFCS / Pro ALTIMTR EFTS RDR ALT =ual Collins F/DIR =oneywell SPZ-8500 IFCS RNAV AP =oneywell SPZ-8500 IFCS LORAN 14 EFTA_R1_01666753 EFTA02526496 RADAR =oneywell Primus 880

DME =ual Collins DME-422 HI FREQ =ual Collins HF-9000 w/SELCAL ADF =ual Collins ADF-462 CVR/FDR =VR/FDR TPDR =ual Collins TDR-94D Mode S w/ TCAS =oneywell TCAS-II w/change 7 16 EFTA_R1_01666755 EFTA02526498 L.R.N =riple Honeywell NZ-2000 w/dual 12-channel GPS, Trip=e Honeywe

AVOliCS Callenlien Center 400 Collins Road NE Mad Station 164100 Cedes Rapids. IA 52498 Tel. 319295.2185 Fax 319 295O337 Rockwell Collins May 14, 2003 W0030737.DOC Flight Options 26180 Curtiss-Wright Parkway Cleveland, 011 44143 Tel: (216) 797-3500 Attention: Subject: Mr. Jody

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

• 1. The following equipment was removed from the aircraft: PART NUMBER QTY MAKEJMODEUDE.SCRIPTION STATION INSTALLATION DATA 622-7203-101 3 Collins VHF-422b Comm 2. The following equipment was Installed In the aircraft. PART NUMBER QTY MAIEJMODEUDESCFtIPTIoN C37c, C38c TSO 450.0 • STATIO

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

B. supplied to the operator. Where the CTL-92E Controller is referenced in the ICA, refer to the existing aircraft maintenance documentation for the Collins RTU-4200 Radio Tuning Unit. • No change to the electrical load for this rotorcraft. • Refer to the updated Aircraft Computed Weight and Balance,

lement describes dual TDR-94D ATC/Mode- S/ADS-B transponder(s) with dual RTU-4200. The RTU-4200 is capable of providing Flight ID information to the Mode S transponder system(s) for ADS-B operations. The Rockwell Collins TDR-94D ATCIMode-S Transponder System with ADS-B Out meets the equipment requireme

ECTION (l)(2) AD Airframe 994015 AD 2014.1801 Rockwell Collins This AD applies to the Mode S Transponders TDR-94/TDR- following Rockwell 94D Collins. Inc. part number (P/N) Mode S transponders: (i) TDR- 94: CPN 622-9352- 008. 622-9352-108. 622.9352-308. 622- 9352.408: and (ii) TDR-94D: CPN 622

3. Revision 1 or JAA.G550.2009.02. Revision 1. as applicable, into the Airplane Flight Manual (AFM). MAN 14 May 2012 I AD EASA AD 2010.0204 Mode S 990204 Airframe Transponder modificationfrei3lacement Mx. Notes: n/a no affected parts installed MAN N/A 1529.8 467 II Oct 2010 C 0.00 A

date work completed.) 1. The following equipment was removed from the aircraft: PART NUMBER QTY MAKE/MODEL/DESCRIPTION STATION 622-7293-101 3 Collins VHF-422b Comm C37c, C38c 450.0 2. The following equipment was installed in the aircraft. • PART NUMBER QTY MAKE/MODEL/DESCRIPTION ISO ,j= S

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