Aircraft Records & Condition Survey

Aircraft Records & Condition Survey GIV S/N 1085 N120JE ACTT: 9801.3 ACTL: 4451 ARCS Performed By: Gt ilfst n lams A I • illit.1.401•• n 4 41.140•Aret Disf c Service I :1- --- -------------- 1 While complying with GIV CMP 330007 E-light ops test found aft battery E-light annunciation 'OFF' would remain on when system active. -CND, operating normal at this time- 2 While Complying with GIV cockpit avionics ramp check found cabin and galley 'OFF' lights do not illuminate. 3 TBD, A/C has LED upgrade so may not be bulbs- 3 While Complying with GIV ramp check found copilot's aft ped. Panel lights imp. Est 4 hr parts TBD 4 While Complying with GIV ramp check found pilot's and copilot's side console flood lights inop. Est 3 hr parts $2700 if bulbs 5 While Complying with GIV ramp check found Aircell phone system intercom feature not working. Est 4 hr parts TBD, cabinet handset will not power up and will need to be fixed first. 6 While Complying with avionics ramp check unable to locate security system control unit. 7 While Complying with avionics ramp check found copilots audio control panel back lighting imp. Est 7 hr, $4000 if ACP, would recommend sending customers unit out for repair, it is not standard ACP 8 While Complying with avionics inventory found #4 E-battery overload light flashing. Est 4 hr, parts $4900 if battery 9 While Complying with avionics ramp check found #2 transponder not reporting mode S information. Est 10 hr, parts $12,700 if transponder 10 While Complying with avionics ramp check found both NAV rcvr's self-test inhibited. Est 4 hr, parts TBD 11 While Complying with avionics ramp check found ELT flashed five times after system was deactivated. Est 2 hr, may not have NAV interface unit. 12 While Complying with avionics ramp check could not enter system maintenance test mode. Est 5 hr, parts TBD 13 While complying with GIV CMP 490053 APU Enclosure GTCP 36-150(G) - Inspection noted loose/working rivet on floor on APU enclosure, below exhaust duct, approx 12" aft of fwd wall and 3" inbd of Ext 107-APU-1 panel. Est. 1 hr Report Date: << DRAFT as of xx./xxJxxxx >> Page 1 of x EFTA00802479 Aircraft Records & Condition Survey GIV S/N 1085 N120JE ACTT: 9801.3 ACTL: 4451 ARCS Performed By: ( 111 11 fst n iris •••••InIal .1”i Name.... 4 alA40Afre Disc, /4/prays' Service Discrepancy 14 While complying with GIV CMP 490053 APU Enclosure GTCP 36-150(G) - Inspection noted cracked stringer structure between access panels 106-APU-2 and 106-APU-3. Est. 8 hr, $1200 parts 15 While complying with GIV CMP 490053 APU Enclosure GTCP 36-150(G) - Inspection noted approx gap greater than 1/8" (oil canning) around enclosure Inbd floorboard access panel below APU alternator. Est. lhr 16 While complying with GIV CMP 490053 APU Enclosure GTCP 36-150(G) - Inspection noted missing faying fire retardant sealant on access panels 106-APU-2, -3, and -4. Est. 2hr $150 parts 17 While complying with GIV CMP 490053 APU Enclosure GTCP 36-150(G) - Inspection noted lower plenum drain line chafed. Est. 2 hr 18 While complying with GIV CMP 490053 APU Enclosure GTCP 36-150(G) - Inspection noted missing fire retardant sealant from multiple areas of APU enclosure walls, ceiling panels, stiffeners and brackets. -Info only, no action necessary- 19 While complying with GIV CMP 553005 - Vertical Stabilizer / Rudder (External) - Inspection noted Tail Strobe lens cracked Est 2 hr, $1100 parts 20 While complying with GIV CMP 553005 - Vertical Stabilizer / Rudder (External) - Inspection noted lower aft screw on access panel 109-RH TE-7 making contact with rudder. Est 4 hr 21 While complying with GIV CMP 551019 - Horizontal Stabilizer / Elevator (Exterior) (Left) - Inspection noted horizontal stab rub block clearance beyond limits. Actual .032" Max Allowable .025". Est 8 hr, $50 parts 22 While complying with GIV CMP 553005 Vertical Stabilizer / Rudder (External) - Inspection noted sheared rivet on Right lower side of RAM Air Inlet. Est 2 hr 23 While complying with GIV CMP 553005 Vertical Stabilizer / Rudder (External) - Inspection noted corrosion around drain hole on Left side of Upper Tail Cone. Est 3 hr 24 While complying with GIV CMP 553005 Vertical Stabilizer / Rudder (External) - Inspection noted APU door not fully closing. Est 8 hr 25 While complying with GIV CMP 533005 Exterior Fuselage - Inspection noted Left Pitot to have deformed tip -Info only, deformation within allowable limits- 26 While complying with GIV CMP 533005 Exterior Fuselage - Inspection found Pilot Side Window to have detached Aft Upper Terminal block. Est 6 hrs Report Date: << DRAFT as of xx/xxixxxx >> Page 2 of x EFTA00802480 Aircraft Records & Condition Survey GIV S/N 1085 N120JE ACTT: 9801.3 ACTL: 4451 ARCS Performed By: Gt 11 fst la tits I 4 Iv N ••••• 4 .41.0....• Dist a Service DM • 27 While Compl • k D 0 9 ' A li Inspection foun w up o e mu ip i that will require further evaluation. Est 8 hr . • 28 While Complying with CMP 534018 Main Landing Gear Wheel Well Compartment - Inspection found L/H MLG Strut placard to be worn. Est 1 hr, $75 parts 29 While Complying with CMP 534018 Main Landing Gear Wheel Well Compartment - Inspection found L/H MLG wheel well A/C ducting to have signs of surface corrosion near the gama coupling attach clamps. Est 4 hr 30 While Complying with CMP 534018 Main Landing Gear Wheel Well Compartment - Inspection found L/H MLG follow up door, main door and landings to have minor chaffing. Est 4 hr 31 While Complying with CMP 534018 Main Landing Gear Wheel Well Compartment - Inspection found both L/H MLG and R/H MLG wheel wells to be dirty. -Info only, 8 hrs to clean if desired- 32 While Complying with CMP 534018 Main Landing Gear Wheel Well Compartment - Inspection found R/H MLG follow up door, main door and landings to have minor chaffing. Est 4 hr 33 While Complying with CMP 534018 Main Landing Gear Wheel Well Compartment - Inspection found R/H MLG wheel well aft inboard flange corroded with evidence of blue water staining. Est 40 hr, parts tbd 34 While Complying with CMP 534018 Main Landing Gear Wheel Well Compartment - Inspection found R/H MLG Door aft upper corner to be corroded with evidence of blue water staining. Est 40 hr, parts tbd 35 While Complying with CMP 534018 Main Landing Gear Wheel Well Compartment - Inspection found R/H MLG wheel well aft wall where the composite structure meets an aluminum stiffener to be corroded. Est 10 hr 36 While Complying with CMP 534018 Main Landing Gear Wheel Well Compartment - Inspection R/H MLG wheel well A/C ducting to have signs of surface corrosion near the gama coupling attach clamps. Est 6 hr 37 While Complying with CMP 534020 Nose Wheel Well and Gear - Inspection found NLG Trunnion L/H mount pin to be incorrectly installed. (Per GIV MM 32-24-01 the lubrication fitting should be below center line) Est 4 hrs Report Date: << DRAFT as of xx./xx/xxxx >> Page 3 of x EFTA00802481 Aircraft Records & Condition Survey GIV SIN 1085 N120JE ACTT: 9801.3 ACTL: 4451 ARCS Performed By: Gulfstreard it•assnat 'arra...rat all•••••• Id V Report Date: « DRAFT as of xxhochootx » Page 4 of x EFTA00802482 Aircraft Records & Condition Survey GIV S/N 1085 N120JE ACTT: 9801.3 ACTL: 4451 ARCS Performed By: Gill fist n itt& •••••1••••••I NA EWA,. 4.4.1a40AMV 38 While Complying with CMP 534020 Nose Wheel Well and Gear - Inspection found NLG Wheel well hydraulic phenolic block to be missing a fastener. Est 2 hrs 39 While Complying with CMP 534020 Nose Wheel Well and Gear - Inspection found NLG Wheel well on the R/H side to have Hydraulic line that shows signs of leaking. Est 2 hrs 40 While Complying with CMP 534020 Nose Wheel Well and Gear - Inspection found NLG Wheel well Accumulator Plexiglas protective cover to be cracked. Est 1 hr, parts $250 41 The following CMP codes are due before the proposed aircraft release date: 237004, 240262, 320004, 320005, 320006, and 322042 42 While complying with CMP 534020 Nose Wheel Well and Gear — Inspection found NLG RH door to have small area of corrosion. Est 2 hr 43 While Complying with CMP 534018 Main Landing Gear Wheel Well Compartment - Inspection found R/H MLG Shock strut placard to be worn. Est 1 hr, parts $75 44 While Complying with CMP 534018 Main Landing Gear Wheel Well Compartment - Inspection found MLG Torque Box Shelf to have multiple hydraulic feed through at aluminum brackets to show signs of surface corrosion. Est 4 hr, parts TBD 45 While Complying with CMP 534018 Main Landing Gear Wheel Well Compartment - Inspection found R/H MLG Follow up door to have multiple spots of surface corrosion that will require further evaluation. Est 10 hrs 46 While Complying with CMP 534020 Nose Wheel Well and Gear - Inspection found NLG follow up door link rods to have excessive play. Est 2 hrs, parts $200 47 While Complying with CMP 534020 Nose Wheel Well and Gear - Inspection found NLG follow up door to have excessive play at fuselage hinge. Est 14 hrs, parts $200 48 While complying with GIV CMP 532067 - Tail Compartment Above Floor - Inspection, found elevator trim cable turnbuckle safety clips are not locked. 49 While complying with GIV CMP 532067 - Tail Compartment Above Floor - Inspection, found bent landing on left and right side of tail compartment door cutout. Est 2 hrs 50 While complying with GIV CMP 532067 - Tail Compartment Above Floor - Inspection, found floorboard (FLR-64) is bowed in throughout most of the surface and core is crushed. Est 10 hrs, parts $1000 51 While complying with GIV CMP 532067 - Tail Compartment Above Floor - Inspection, found flight hydraulic filter manifold is wet with Skydrol at upper cap. Est 2 hrs Report Date: << DRAFT as of xx./xxJxxxx >> Page 5 of x EFTA00802483 Aircraft Records & Condition Survey GIV S/N 1085 N120JE ACTT: 9801.3 ACTL: 4451 ARCS Performed By: Gt 11 fist Hearn' I 1...i.aftant4 n 4.M...ft...I 52 While complying with GIV CMP 532067 - Tail Compartment Above Floor - Inspection, found hydraulic fluid spillage and bubbled paint on structure below utility pump. Est 2 hrs 53 While complying with GIV CMP 532067 - Tail Compartment Above Floor - Inspection, found APU bleed air duct fire seal clamp is missing. Est 1 hr, parts $15 54 While complying with GIV CMP 532067 - Tail Compartment Above Floor - Inspection, found wire harness tie-down is disbonded from the pressure bulkhead beam lightning hole. Est 1 hr 55 While complying with GIV CMP 532067 - Tail Compartment Above Floor - Inspection, found rudder actuator is wet with hydraulic fluid. Est 2 hr 56 While performing ARCS hot cockpit / cabin inspection noted source switching on cabin VIP Switch Panel will cycle thru DVD 1 and 2 but does not display video to the monitor. DVD will play, as we were able to get sound playing thru the sound system for the DVD Est TBD S7 While performing ARCS hot cockpit / cabin inspection noted Custom Bose surround sound system will not play aft cabin audio when attempting to play DVD audio. System will play correctly with iPod selected Est TBD 58 While performing ARCS hot cockpit / cabin inspection noted All the headphone switch panels do not work. When plugged in and turning the volume to max, you can hear the cycling of audio sources but none of the iPod/DVD audio came thru Est TBD 59 While performing ARCS hot cockpit / cabin inspection noted RH Window No. 5 and LH Window No. 1 upwash lights are inop Est 3 hrs, parts $320 60 While performing ARCS hot cockpit / cabin inspection noted Left Seat No. 1 has a switch that says seat window shade, upon activating said switch it controls all the shades. Est TBD 61 While performing ARCS hot cockpit / cabin inspection noted RH Seat No. 2 VIP switch panel will consistently override whatever action you are trying to make to show cabin temp. For example, when trying to cycle thru Video sources after every selection the cabin temp would display Est TBD 62 While performing ARCS hot cockpit / cabin inspection noted All the 60Hz outlets had polarity reversed but seem to function as advertised Est TBD 63 While performing ARCS hot cockpit / cabin inspection noted The cabin remote that is docked at the VIP seat would only control certain functions. For example, it would eject the DVD from the player, but when attempting to select the FWD Monitor source, nothing would happen Est TBD 64 While complying with CMP 534018 Main landing gear wheel well compartment inspection found MLG torque box surface to show signs of corrosion that will require further evaluation. Est 10 hrs Report Date: << DRAFT as of xxixrJxxxx >> Page 6 of x EFTA00802484 Aircraft Records & Condition Survey GIV S/N 1085 N120JE ACTT: 9801.3 ACTL: 4451 ARCS Performed By: ( it ilfst mutt& ••••••1.4.4.• ••••• 4 4•••••••••,/ 65 While C/W CMP 571005 Wing Exterior (Left) Inspection found sealant missing on leading edge gap bands. Est 1 hr 66 While C/W CMP 571005 Wing Exterior (Left) Inspection found all flap tracks to have rust/corrosion where rollers contact the track. Est 40 hrs, parts TBD 67 While C/W CMP 571005 Wing Exterior (Left) Inspection found wing to flap seal between inboard and second flap track on wing trailing edge to be torn. Est 1 hr 68 While C/W CMP 571006 Wing Exterior (Right) Inspection found wing to flap seal between second and third flap track on wing trailing edge to be torn. Est 1 hr 69 While C/W CMP 571006 Wing Exterior (Right) Inspection found all flap tracks to have rust/corrosion where rollers contact the track. Est 40 hrs, parts TBD 70 While C/W CMP 571006 Wing Exterior (Right) Inspection found right wing navigation light lens to have major crazing/cracking. Est 6 hrs, parts $1200 71 While C/W CMP 532005 Cabin Compartment Above Floor Inspection found cabin upwash light over right fwd emergency exit to be out. -NA DUPLICATE- 72 While C/W CMP 532005 Cabin Compartment Above Floor Inspection found cabin downwash light between right emergency exits and last right cabin downwash light to be out. 73 While C/W CMP 532027 Entrance Compartment Behind Panel Inspection, found engine synchronizer amplifier/control box to be missing one of four screws securing it to the cabinet. Est 1 hr 74 While C/W CMP 533005 Exterior Fuselage Inspection, noted skeg paint is worn down to bare metal around fwd drain hole. Est 1 hr 75 While complying with CMP 571006 Wing Exterior (Right) - Inspection found R/H A track flap trough to show signs of surface corrosion that will require further evaluation. Est 3 hrs 76 While complying with CMP 571006 Wing Exterior (Right) - Inspection found R/H A track flap trough roller to be corroded. Est 3 hrs, parts $150 77 While complying with CMP 571006 Wing Exterior (Right) - Inspection found R/H B track flap trough roller to be seized. Est 3 hrs, parts $150 78 While complying with CMP 571006 Wing Exterior (Right) - Inspection found R/H B track Aft outboard small roller to be worn. Est 1 hrs, parts $50 79 While complying with CMP 571006 Wing Exterior (Right) - Inspection found R/H C track flap trough roller to be corroded. Est 3 hrs, parts $150 Report Date: << DRAFT as of xx/xxfxxxx >> Page 7 of x EFTA00802485 Aircraft Records & Condition Survey GIV S/N 1085 N120JE ACTT: 9801.3 ACTL: 4451 ARCS Performed By: Git first ira.rns • I I IniNa••••• 4 41.0.....afre 80 While complying with CMP 571006 Wing Exterior (Right) - Inspection found R/H D track Roller rub strips to be worn beyond limits. Est 1 hr, parts $50 81 While complying with CMP 571005 Wing Exterior (Left) - Inspection found L/H A track flap trough roller to be corroded. Est 3 hrs, parts $150 82 While complying with CMP 571005 Wing Exterior (Left) - Inspection found L/H B track aft inboard small roller worn. Est 1 hrs, parts $50 83 While complying with CMP 571005 Wing Exterior (left) - Inspection found L/H C track aft outboard small roller worn. Est 1 hrs, parts $50 84 While complying with CMP 571005 Wing Exterior (left) - Inspection found L/H C track flap trough roller to be corroded. Est 3 hrs, parts $150 85 While complying with CMP 571005 Wing Exterior (Left) - Inspection found L/H D track Roller rub strips to be worn beyond limits. Est 1 hrs, parts $50 86 While complying with CMP 533005 - Exterior Fuselage - Inspection found Co-pilot windshield to have inter-pane cracking at bus bar. Est 12 hr, parts $53,150 87 While complying with CMP 533005 - Exterior Fuselage - Inspection found Co-pilot side window to have inter-pane cracking at bus bar. Est 12 hr, parts $12,000 88 While complying with GIV CMP 532067 Tail compartment above floor — inspection noted light coating con of fluid and small misc debris on and within tail compartment FS 596 Junction box. Est 2 hrs 89 While complying with GIV CMP 532067 tail compartment above floor — inspection noted failed fastener on tail compartment FS 596 junction box cover. Est 1 hr 90 During APU operational test noted overspeed test did not test. Est 4 hrs, parts TBD 91 While complying with CMP 532017 Cockpit compartment above floor inspection, found pilot side window has long scratches and waviness as well as outer seal deterioration that will required further investigation. Est 4 hrs 92 While complying with CMP 532041 baggage compartment inspection found baggage door to have cracks in the fwd and aft lower radius and fwd upper radius that will require further evaluation. Est 30 hrs, parts TBD Report Date: << DRAFT as of xx./xxJxxxx >> Page 8 of x EFTA00802486