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

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

00 w/5 handsets : Dual Collins DME-422 HI FRED : Dual Collins HF-9000 w/SELCAL : Dual Collins ADF-482 CVR/FDR : CVR/FDR : Dual Collins TDR-94D Mode S w/ TCAS : Honeywell TCAS-II w/change 7 EFTA_R1_01510815 EFTA02437876 L.R.N Addl Cockpit Equipment Crew Accessories General CONFIDENTIAL: L

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

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

) Subject: STC ST00881WI-D 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

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

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

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

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

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