Price: 1.100.000USD

Contact information

Aviationepica.con for sale 1992 HAWKER 800A ADDITIONAL EQUIPMENT See attached Modification Status Sheet
INSPECTION STATUS CAMP Maintenance Tracking Program Status Report Crew: 2 + jump seat Capacity: 8 / 2,000 lb (907 kg) maximum payload Length: 51 ft 2 in (15.60 m). Located in FLORIDA, active airworthy aircraft, The aircraft has a valid engine program in the United States. Total Time 7,932 Hours Landings 4,664. Cost 1.1 USD
INF. contact@aviationepica.com gerencia@aviationepica.com, info@avaitionepica.com inf. Col. 310-3351797. 318-8223690 USA WhatsApp 1-3057248777

Specifications

Airframe:

Total Time 7,932 Hours
Landings 4,664

Wingspan: 51 ft 4.5 in (15.659 m)
Height: 17 ft 7 in (5.36 m)
Wing area: 374 sq ft (34.7 m2)
Empty weight: 15,600 lb (7,076 kg) basic
Operating weight empty: 16,000 lb (7,257 kg)
Maximum ramp weight: 27,520 lb (12,483 kg)
Maximum zero-fuel weight: 18,000 lb (8,165 kg)

Avionics:

VIONICS
Autopilot: Dual Honeywell DFZ-800
Avionics Package/EFIS: Honeywell EDZ-800 (5-tube)
Communication Radios: Dual Honeywell RCZ-833B
Radios: Dual Honeywell RNZ-850
DME: Dual Honeywell DI-851
FMS: Dual Honeywell FMS NZ-2000 w/GPS
H/F: Collins HF-9010 w/SELCAL (REMOVED)
Radar/RADIO Altimeter: Collins 860F-1
Stormscope: Goodrich WX-1000
TAWS: Sandel TAWS/RMI ST-3400-102
TCAS: ACSS RT-910 TCAS-II w/change 7
Transponder: Dual Garmin GTX-3000 (ADS-B Out)
CVR: L3 HARRIS A100A
Weather Radar: Honeywell Primus 870
GPS DUAL SENSOR HONEYWELL GNSSU
ELT ARTEX C406-1
STBY HORIZON GOODRICH ADI-330E
IRU HONEYWELL LASEREF III
ADC HONEYWELL AZ-810

Engines:

Honeywell TFE731-5R-1H (enrolled on MSP)

LEFT RIGHT
Hours 7,897 7,820
Cycles 4,639 4,602

TBO Interval (overhaul / CZI) 4,200 4,200
Hours Until CZI Due 503 580
APU Sundstrand T-62T-40C9

Hours 4,390
Cycles 10,127

Propellers:

Performance

Maximum speed: 456 kn (525 mph, 845 km/h) max level speed and max cruising speed at 29,000 ft (8,839 m) / M0.87
Cruise speed: 400 kn (460 mph, 740 km/h) economical cruise at 39,000–43,000 ft (11,887–13,106 m)
Stall speed: 92 kn (106 mph, 170 km/h) in landing configuration at typical landing weight
Range: 2,580 nmi (2,970 mi, 4,780 km) with max payload
2,825 nmi (3,251 mi; 5,232 km) with max fuel and NBAA VFR reserves
Service ceiling: 43,000 ft (13,000 m)
Rate of climb: 3,100 ft/min (16 m/s)
Wing loading: 73.26 lb/sq ft (357.7 kg/m2)
Thrust/weight: 0.313
Take-off balanced field length: 5,620 ft (1,713 m) at MTOW
Landing distance from 50 ft (15 m): 4,500 ft (1,372 m) at typical landing weight and 6 pax

Interior:

INTERIOR (Refurbished 2009)
Forward 4-place club, aft 2-place divan opposite single club chair all upholstered in beige leather

Exterior:

EXTERIOR (Repainted 2001)
Overall Matterhorn White with Gold and Red accent striping