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.

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

/13/2013 IJIGN1005D Rev (IR) 06/11/2013 Report: IJIGIV1065DSA Rev (IR) 013/22/2013 Structures Note: Interior !me sht 1 - 4 LH Aft Closet Mod Instl slit 1 - 5 Structural Analysis LH Aft Closet Mod Intl Gulfstream G-IV Aircraft 1) The structural aspects only of the above listed data are approve

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

, 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

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

Time' action to ensure incorporation of ASC 059. To be accomplished with in the next 24 months. Ref ASC 059. CB CB 46 No. 2 ADF Antenna Lead Instl This is a One Time 980460 46 MAN NIA 14 May 2007 I Airframe At F.S. 288 Action to inspect the No.2 ADF antenna lead. Elf: is for 5003 thr