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ur Window) 23 20 Jun 2013 17 Mar 2014 292502 Power Transfer Unit Manifold Differential G550 AMM 50
Projected Through • 5966.5 Hours 77 2203 Landings 19 Jan 2020 Date 4544.5 APU Hours 30 APU Cycles COMPONENT TIMES G-CGUL Current TT 3466.5 Current Lndgs 953 Current Hr Mtr 3423.6 Position Logbook Description Serial Number Total Time Total Cycles TSO CSO 1 Engine Rolls Royce 8R700.71004.11
14 31 Jul 2016 5 Mos 240122 Emergency Battery Power System (Right) 6550 AMM 2320.2 * Airframe MA
rough: 3590 Hours TT 1956 Landings Cycles 900 Cycles 2 10 Feb 2019 Date 2834.5 APU Hours 1356 APU Cycles COMPONENT TIMES Current TT 2590.0 Current Lndgs 1056 Current Hr Mtr 2571.0 Position Logbook Description Serial Number Total Time Total Cycles TSO CSO 1 Engine Rolls Royce BR700.110C411
14 31 Jul 2016 5 Mos 240122 Emergency Battery Power System (Right) 6550 AMM 2320.2 * Airframe MA
rough: 3590 Hours TT 1956 Landings Cycles 900 Cycles 2 10 Feb 2019 Date 2834.5 APU Hours 1356 APU Cycles COMPONENT TIMES Current TT 2590.0 Current Lndgs 1056 Current Hr Mtr 2571.0 Position Logbook Description Serial Number Total Time Total Cycles TSO CSO 1 Engine Rolls Royce BR700.110C411
13 Airframe 23.15.01 for O310229 232103 High Power Amplifier Removal / Installation 0.0 2354.6 Hrs
ook Position CURRENT STATUS LOG DATE -- 08 Nov 2014 Analyst: Gary Leever Phone: +44 790.312.5319 COMPONENT TIMES G-CGUL Current TT 3466.5 Current Lndgs 953 Current Hr Mtr 3423.6 Position Logbook Description Serial Number Total Time Total Cycles TSO CSO 1 Engine Rolls Royce BR700-710C4-11
9 Apr 2008 C 0.00 887186 SB BR700-71.101206 • Power Plant Engine 1 External Drain Tubes And Fitting
ELI-EASA Technical Bulletins G-CGUL Report Filters: Log Date - 08 Nov 2014 TYPE: ALL Current TT 3466.5 Analyst: Gar Leaver CW Status: ALL Current Lndgs 953 FA)4 Phone: Current Hr Mtr 3423.6 COMPONENT TIMES Position Logbook Description Serial Number Total Time Total Cycles TSO CSO 1 Engi
Entities connected to both Samantha Power and Current Lndgs

Honeywell
ORGANIZATIONVALVE
ORGANIZATIONGeneral Dynamics Company
ORGANIZATIONWing Rear Beam
ORGANIZATIONFirst Aid Kit
ORGANIZATIONCowl Doors
ORGANIZATIONAileron Control
ORGANIZATIONTrim Cables
ORGANIZATIONRudder Control
ORGANIZATIONAir Turbine Starter Oil - Change
ORGANIZATIONService Life
ORGANIZATIONMain Fuel Boost Pump
ORGANIZATIONFuel Shut
PERSONEmpennage FS
ORGANIZATIONPower Transfer Unit
ORGANIZATIONMain Landing Gear Corrosion
ORGANIZATIONTrash Receptacle Enclosure
ORGANIZATIONAir Data Module
ORGANIZATIONUpper Surface of Center Wing
ORGANIZATIONWing Rear Beam (Left
ORGANIZATION