Gulfstream GIV N167AA S/N 1096 Specifications and Summary
Transcript of Gulfstream GIV N167AA S/N 1096 Specifications and Summary
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Gulfstream GIV
N167AA S/N 1096
Specifications and Summary
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1989 Gulfstream G-IV N167AA S/N 1096
OFFERED AT: $3,295,000
AIRCRAFT HIGHLIGHTS: GoGo Biz High Speed WiFi Internet FANS1/A & ADS-B Out (Version 2)
Engines on Roll Royce Corporate Care APU on MSP Gold Avionics on HAPP
Avtech LED Cabin Lighting
STATUS: As of August 7th, 2018
TOTAL TIME: 10,210 LANDINGS: 4,326 ENGINES: Rolls Royce TAY 611-8 (GIV) LEFT RIGHT TOTAL TIME SINCE NEW: 9,876.7 9,849.3 CYCLES SINCE NEW: 4,191 4,188 TIME @ LAST MIDLIFE: 9,825.1 / Aug 2017 9,797.7 / Aug 2017 TIME @ LAST OVERHAUL: 7,527.3 / Jun 2007 7,499.9 / Jun 2007 MID LIFE NEXT DUE: 13,825.1 / Aug 2027 13,797.7 / Aug 2027 OVERHAUL NEXT DUE: 15,527.3 or Jun 2027 15,499.9 or Jun 2027 SERIAL NUMBER: 16195 16196 Engines enrolled on Corporate Care APU: Honeywell GTCP-36-100 (GIV) Serial Number: P478 TSN: 5,962 APU enrolled on MSP Gold
WEIGHT: MAX RAMP WEIGHT: 73,600 Lbs. MAX TAKE-OFF WEIGHT: 73,200 Lbs. MAX LANDING WEIGHT: 58,500 Lbs. BOW (2 Crew): 43,569 Lbs. EMPTY WEIGHT: 42,436 Lbs. MAX ZERO FUEL WEIGHT: 46,500 Lbs.
CAPABILITIES: RNP-10 (-4 Capability) BRNAV FANS 1/A RVSM LNAV / VNAV ADS-B Out (Version 2) Auto Throttles EGPWS (TDB 604) MNPS TCAS 7.1
102A Broad Street • Guilford • Connecticut • 06437 • 203-453-0800 • www.guardianjet.com 3
AVIONICS
AVIONICS: Honeywell SPZ-8000 Six Tube EFIS
AIR DATA COMPUTER: Dual Honeywell AZ 810 DADC AUTO PILOT: Honeywell SPZ-8000 AUTOMATIC DIRECTION FINDER: Dual Rockwell Collins ADF-462 AUTOTHROTTLES: Dual Honeywell Auto Throttle Computers COCKPIT VOICE RECORDER: Fairchild A100 CVR COMMUNICATIONS: Dual Rockwell Collins VHF-422D VHF Transceivers with 8.33 Spacing CONTROL DISPLAY UNITS: Dual Honeywell CDUs with Universal UNS-1LW (For Datalink) DATA LOADER: Honeywell DL-950 Data Loader DISTANCE MEASURING EQUIPMENT: Dual Rockwell Collins DME-442 EMERGENCY LOCATOR TRANSMITTER: Artex C406-N ELT FLIGHT DATA RECORDER: L3 Communications F1000 FDR FLIGHT GUIDANCE COMPUTER: Dual Honeywell FGCs FLIGHT MANAGEMENT SYSTEM: Dual Honeywell FMS NZ-2000, version 5.2 GLOBAL POSITIONING SYSTEM: Dual Honeywell GNSSU GPS Receivers HIGH FREQUENCY: Dual HF-190 Transceivers LONG RANGE NAVIGATION: Triple Honeywell Laseref Inertial Reference Units NAVIGATION: Dual Rockwell Collins VIR-432 Nav Receivers with FM Immunity RADIO ALTIMETER: Dual Rockwell Collins ALT-55B Radio Altimeters SELCAL: SELCAL Decoder TERRAIN AWARENESS and WARNING SYSTEM: Honeywell Mark V EGPWS (TDB 604) TRAFFIC ALERT & COLLISION AVOIDANCE SYSTEM: TCAS 2000 with Change 7.1 TRANSPONDER: Dual Rockwell Collins TDR-94D Transponders with Mode S Enhanced Surveillance, and ADS-B Out (Ver. 2) Transponder WEATHER RADAR: Honeywell Primus 870 Weather Radar
102A Broad Street • Guilford • Connecticut • 06437 • 203-453-0800 • www.guardianjet.com 4
CABIN ENTERTAINMENT & COMMUNICATIONS
ENTERTAINMENT
Rosen Moving Map Forward Cabin 20” Bulkhead Monitor 20” Credenza Monitor (4) 7” Plug-In Rosen Monitors Dual DVD Player XM Radio
COMMUNICATIONS
GoGo Biz WiFi High Speed Data / Aircell ATG 5000 Iridium Phone System
(1) Cockpit Handset (2) Cabin Handsets
MAINTENANCE PROGRAMS & INSPECTIONS STATUS
MAINTENANCE & INSPECTIONS
Engines on Rolls Royce Corporate Care APU on MSP Gold Avionics on Honeywell HAPP Aircraft maintenance tracked per CMP
INSPECTION NEXT DUE 24 Month May 2020 48 Month May 2022 72 Month May 2024
102A Broad Street • Guilford • Connecticut • 06437 • 203-453-0800 • www.guardianjet.com 5
GULFSTREAM G-IV TECHNICAL DATA
Cabin Height – 6.1 feet Cabin Width: Max / at Floor Level – 7.3 feet / 5.5 feet
Take Off Distance at Sea Level – 5,280 feet Take Off Distance at 5,000 feet elevation – 7,300 feet
Landing Distance – 3,361 feet Maximum Altitude – 45,000 feet Range with 4 Pax – 4,212 NM
600 NM Flight Time – 1h25 1,000 NM Flight Time – 2h17
Long Range Cruise Speed – 459 knots High Speed Cruise Speed – 480 knots
Fuel Consumption – 479.07 Gallons/Hour Total Variable Costs per hour – $ 3,713.05
Performance Information from ARGUS International, Inc. Information presented is model based and not necessarily specific to serial number 1096
102A Broad Street • Guilford • Connecticut • 06437 • 203-453-0800 • www.guardianjet.com 6
INTERIOR Forward Cabin
INTERIOR DESCRIPTION
This unique interior comfortably seats up to 13 passengers. The forward cabin features three-person divan opposite a two-club seat arrangement. The aft cabin features two aft-facing club seats, a four-person conference table area with adjacent credenza, and two forward-facing club seats. A well-equipped aft galley and spacious aft lavatory completes the interior.
Additional Features
AvTech LED Lighting
Cockpit Jumpseat (Certified for takeoff)
Forward Cabin Looking Aft
102A Broad Street • Guilford • Connecticut • 06437 • 203-453-0800 • www.guardianjet.com 7
INTERIOR Forward Cabin
Forward Cabin looking Forward
Left Hand Seat facing Forward
102A Broad Street • Guilford • Connecticut • 06437 • 203-453-0800 • www.guardianjet.com 8
INTERIOR Mid Cabin
Mid Cabin looking Aft
Mid Cabin looking Forward
102A Broad Street • Guilford • Connecticut • 06437 • 203-453-0800 • www.guardianjet.com 9
INTERIOR Aft Cabin
Aft Cabin looking Forward
INTERIOR Floor Plan
102A Broad Street • Guilford • Connecticut • 06437 • 203-453-0800 • www.guardianjet.com 10
GALLEY & LAVATORY
AFT GALLEY DESCRIPTION
Coffee Maker Ice Drawers (2)
Dual Temperature Oven Microwave
Gasper-Cooled Compartment
102A Broad Street • Guilford • Connecticut • 06437 • 203-453-0800 • www.guardianjet.com 11
EXTERIOR
EXTERIOR DESCRIPTION
(New Paint in 2006 by Capital Aviation Inc., Bethany, OK)
Matterhorn White with Fighter Blue, Titanium and Nordic Gray Striping
This aircraft is being brokered by Guardian Jet, LLC. Prospective purchasers are encouraged to conduct their own independent pre-purchase inspection as Guardian Jet, LLC makes no representations as to the airworthiness of the aircraft or the accuracy of the above information. Specifications subject to verification
upon inspection. Aircraft subject to prior sale. 2018 08 30 / MB