P.a.A.
The Hawker 800 will carry eight passengers in excess of 2000 nautical miles,in luxury and style
1993 Hawker 800 in London, United Kingdom
Details
- Jahr 1993
- Geschwindigkeit 1565 kph
- Maximum 2800 mi
- Max. Abhebegewicht 27400 lbs
- Flughöhe 43000 ft
- Kabinenlänge 21.03 m
- Kabinenhöhe 5,67 ft
- Kabinenbreite 5,75 ft
- Außenhöhe 17,42 ft
- Außenlänge 15.6 m
- Kapazität 8
- Flugzeugtyp Light Jet
- Spannweite 15.66 m
- Referenznummer J006
Beschreibung
Luxuriously appointed with a spacious stand-up cabin, the aircraft offers an enviable combination of quality, performance and safety with sophisticated instrumentation and navigation equipment.
To the rear of the passenger cabin is a stylish, fitted washroom and to the front, a self contained galley. Enhanced in-flight facilities include DVD player, Airshow and the provision for hot food to be served. The Hawker meets the demands for longer range trips to destinations such as Eastern Europe, Russia and the Middle East
General Information
Date of Manufacture: 1993
Assigned Engines Type and Model: TFE731-5R-1H
Country of Registration: Great Britain
Current Location: Chester ,UK
Airworthiness Authority Approval: United Kingdom Civil Aviation Authority
Aircraft on Cam p: Yes
EU Ops Com pliance: Yes
Operating Limitations
Maximum Taxi Weight (MTW): 27,520 Ib
Maximum Take off Weight (MTOW): 27, 400 12 Ib
Maximum Landing Weight (MLW): 23,350 Ib
Maximum Zero Fuel Weight (MZFW): 1 8,000 Ib
Operating Empty Weight: 15, 451 Ib
Last Weighing: 12th January 2007
Engine Thrust: 4,750
Total Time Since New: 5,758 Hours
Total Cycles Since New: 5,068 Cycles
Maintenance Status
‘B’ Check Due: 6,075 hours
‘C’ Check Due: 6,308 hours
‘D’ Check Due: 7,908 hours
‘E’ Check Due: Date: 19th May 2009
‘F’ Check (24 month inspection) Due: Date: 19th May 2010
‘G’ Check (48 month inspedtion) Due: Date: 5th May 2010
Auxiliary Power Unit
Manufacturer: Sundstrand
Type: T62-40C8D1
Time Since New: 3,435 Hours 6,714 Cycles
First Life Limiter: Turbine Rotor 14,886 Cycles
Avionics
HAWKER1000 Flightdeck
FCS: Dual Honeywell DFZ800
FMS: Dual Honeywell FMZ900 + colour CDUs
EFIS: Dual Honeywell EDZ818
Coms: Dual Honeywell RCZ833
Navs: Dual Honeywell RNZ850 (FM Immunity)
GPS: Honeywell DG1086
Laseref: Dual Honeywell IRS.3
Air Data: Dual Honeywell ADZ810
Radar: Honeywell P870
Rad Alt: Honeywell AA300
EGPWS: Honeywell Mark V111
TCAS: Honeywell TCAS II
RVSM: Yes
ELT: Kannad 406 Mk 2
FDR: Plessey PV1584N
HF: Dual King KHF-950
CVR: Fairchild A-1001
Other Notable Modifications
TCAS II
Dual FMS
Transponder ELS Only
Third Battery Installed
EGPWS
Long Range Oxygen System
Steep Approach Capability
Aircraft
Interior Colours & Furnishings
New 2006 Interior
8 passenger seats including VIP chairs in beige leather with Airshow in-flight entertainment system
Forward and rear interior cargo holds
Forward galley and oven
Exterior
Exterior
New paint in 2006 in Matterhorn white with black and blue cheetlines
To the rear of the passenger cabin is a stylish, fitted washroom and to the front, a self contained galley. Enhanced in-flight facilities include DVD player, Airshow and the provision for hot food to be served. The Hawker meets the demands for longer range trips to destinations such as Eastern Europe, Russia and the Middle East
General Information
Date of Manufacture: 1993
Assigned Engines Type and Model: TFE731-5R-1H
Country of Registration: Great Britain
Current Location: Chester ,UK
Airworthiness Authority Approval: United Kingdom Civil Aviation Authority
Aircraft on Cam p: Yes
EU Ops Com pliance: Yes
Operating Limitations
Maximum Taxi Weight (MTW): 27,520 Ib
Maximum Take off Weight (MTOW): 27, 400 12 Ib
Maximum Landing Weight (MLW): 23,350 Ib
Maximum Zero Fuel Weight (MZFW): 1 8,000 Ib
Operating Empty Weight: 15, 451 Ib
Last Weighing: 12th January 2007
Engine Thrust: 4,750
Total Time Since New: 5,758 Hours
Total Cycles Since New: 5,068 Cycles
Maintenance Status
‘B’ Check Due: 6,075 hours
‘C’ Check Due: 6,308 hours
‘D’ Check Due: 7,908 hours
‘E’ Check Due: Date: 19th May 2009
‘F’ Check (24 month inspection) Due: Date: 19th May 2010
‘G’ Check (48 month inspedtion) Due: Date: 5th May 2010
Auxiliary Power Unit
Manufacturer: Sundstrand
Type: T62-40C8D1
Time Since New: 3,435 Hours 6,714 Cycles
First Life Limiter: Turbine Rotor 14,886 Cycles
Avionics
HAWKER1000 Flightdeck
FCS: Dual Honeywell DFZ800
FMS: Dual Honeywell FMZ900 + colour CDUs
EFIS: Dual Honeywell EDZ818
Coms: Dual Honeywell RCZ833
Navs: Dual Honeywell RNZ850 (FM Immunity)
GPS: Honeywell DG1086
Laseref: Dual Honeywell IRS.3
Air Data: Dual Honeywell ADZ810
Radar: Honeywell P870
Rad Alt: Honeywell AA300
EGPWS: Honeywell Mark V111
TCAS: Honeywell TCAS II
RVSM: Yes
ELT: Kannad 406 Mk 2
FDR: Plessey PV1584N
HF: Dual King KHF-950
CVR: Fairchild A-1001
Other Notable Modifications
TCAS II
Dual FMS
Transponder ELS Only
Third Battery Installed
EGPWS
Long Range Oxygen System
Steep Approach Capability
Aircraft
Interior Colours & Furnishings
New 2006 Interior
8 passenger seats including VIP chairs in beige leather with Airshow in-flight entertainment system
Forward and rear interior cargo holds
Forward galley and oven
Exterior
Exterior
New paint in 2006 in Matterhorn white with black and blue cheetlines
