EFTA00802479.pdf

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