Epstein Secrets

r-system..J.1.i. Dual Collins DME-40 DFIE system', _..* Dual Collins TDR-90 transponder system':.'_. Dual Collins DF-206 AOF system_. .. . • . . Collins FPC-75 groUnd proximity warning systaa vo Collins 54141C comparator warning. system _ Collins 51Z-4 marker beacon system ., RCA Primus-400,14XD c

proach Idles-E.O.: 103 VA732315 NC Relay-Inttlf Pilots Overhead Panel E.O.: 002; 101, Chapter 76 ENGINEIOTROl. ' • A760000 A .Eng)ne COntrols,Instl. - Strut-E.O.: 002A VA760014 A . Drum Instl. Eng. Controls E.O.:- 100, 101 VA760015 A . Bradkit Assy.:.- Pulley ESTA 100 E.O.: 105 EFTA00277916

in addition to the above document: - • NOTE: - °VA" denotes Valsan Deaiting. a: `'Chapter 24 ELECTRICAL POWER • A240000 A Electrical .System Instl. - Strut E.O.: 003A,'101 VA240007 E -, Panel-Load Control Center Modification. E.O.: 003A, 004, 005, 006 b.. Chaster 28 FUEL SYSTEM INSTALLATION.

• 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

hapter 73 ENGINE FUEL AND CONTROL VAJ32301 K Approach Idle Solenoid Wiring Diagram E.0: 002(Rev L), 002 (Rev. MI, 003(Rev. M) VA732303 0 Relay Instl. - Approach Idle Solendid E.O.: 103, 003, 1008 VA732304 0 Switch/IND Light Instl - Approach Idle E.O.: 002, VA732310 A Switch Instl. - Nose Gea

ransponder system . . • ' l i, c Dual Collins DF-206 kW system Collins FPC -75 ground proximity warning Systel‘we -.. . ... ...-...„„, ..- . Collins 54W1C comparator warning system . . . • Collins 512-4 marker beacon system RCA Primus-400 HKO coloradar system Wulfsberg fligbtfone III air to

, 111, 0064 Cha ter 73 ENGINE FUEL AND CONTROL 301 K Approach Idle Solenoid Wiring Diagram E.0: 002(Rev 002 (Rev. M), 003(Rev. M) 303 D Relay Instl. — Approach Idle Solenoid E.O.: 103, 003, 100B 304 D Switch/IND Light Instl - Approach rdle E.O.: 002, 310 A Switch Instl. - Nose Gear Position

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

3 ENGINE g. FUEL AND CONTROL VA732301 .K Approach Idle Solenoid Wiring Diagram E.O: 002(Rev L), . 002 (Rev. M), 003(Rev. M) VA732303 0 Relay Instl. - Approach Idle Solenoid E:0.:. 103, 003, 100B VA732304 0 Switch/IND Light Instl - Approach Idle E.O.: 002, VA732310 A Switch Instl. - Nose Ge