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2014 08 Jun 2015 119 Days Air Turbine Starter Oil Change 500 Hrs 6910.1 7418.6 Hrs' 166.0 Hrs 121400 1719 3.0 Engine 1 15 Jul 2014 GVAMM Lubrication/Servicing (L) 121400 Air Turbine Starter Oil Change 500 Hrs 6945.2 7453.7 Hrs' 166.0 Hrs (121401) 1789 3.0 Engine 2 15 Jul2014 GVAMM Lubrication/Serv
Gear Bungee (Right) - Lubrication 7109.1 323038 1755 3.0 Airframe 24 MOS 25 Nov 2014 31 Oct 2016' 20 Mos GV AMM Lubrication/Servicing (L) Landing Gear Emergency Extension Nitrogen Blow-Down Bottle (Right) - Discard 3473.5 323909 1159H50091-21 7339 0.0 0 90 919 $5.593.00 Airframe No 180 MOS 10 Oct
4 Airframe os Operation 4 MOS 1040.0 334 03 Jun 2016 30 Sep 2016' 71 Days 321005 Airframe Main Landing Gear (Leh) • Lubrication G550 AMM Lubrication/Servicing (L) 4 MOS 1040.0 334 03 Jun 2016 30 Sep 2016' 71 Days 94 2.0 321006 Airframe Main Landing Gear (Right) - Lubrication 0550 AMM Lubrication/Se
uisher (Aft Lavatory) • Weight Check 1040.0 C354TS 334 12 MOS 01 Jun 2016 31 May 2017 10 Mos G550 AMM LubricatioNServicing (Z) Weight Check Landing Gear Emergency Extension Nitrogen Blow-down Bottle (Left) - (Hydrostatic) Functional Test 01 1.0 262612 Airframe 01 1.0 262632 Airframe 01 1.0 323002 A
able Stator Vane Mechanism - Lubrication 1000 Hrs 1974.4 2974.4Hrs 2974.4 127.8 Hrs 753025 946 16.0 30 Mar Engine 1 2011 RR 8R710-C4 EMM Lubrication/Servicing (L) 753025 Variable Stator Vane Mechanism - Lubrication 1000 Hrs 1974.4 2974.4Hrs 2974.4 127.8 Hrs (753026) 946 16.0 30 Mar Engine 2 2011
rrosion Inhibiting Compound Reapplication 2689.1 1320 18.0 24 MOS 26 Jul 2014 31 Jul 5 Mos Airframe 20W G550 AMM Lubrication/Servicing (S) Landing Gear Emergency Extension Nitrogen Blow-down Bottle (Left) • (Hydrostatic) Functional 2525.3 323002 Test 3.0 1159SCH233.5 29118C1 1234 Airframe 36 MOS 15 M
Entities connected to both Lubrication/Servicing (L and Landing Gear Emergency

Samantha Power
PERSONGeneral Dynamics Company
ORGANIZATIONMain Landing Gear Corrosion
ORGANIZATIONFunctional/Ops Test
ORGANIZATIONFirst Aid Kit
ORGANIZATIONWing Rear Beam
ORGANIZATIONPower Transfer Unit
ORGANIZATIONFuel Shut
PERSONForward Cabin
PERSONMain Fuel Boost Pump
ORGANIZATIONEmpennage FS
ORGANIZATIONTSOHR
ORGANIZATIONTrim Cables
ORGANIZATIONAir Data System No.
ORGANIZATIONValve (Left) Operational
ORGANIZATIONInlet Areas
LOCATIONCowl Doors
ORGANIZATIONRudder Control
ORGANIZATIONTSNMO
ORGANIZATIONElevator Control
ORGANIZATION