1993 Hawker 1000A
Description
The Hawker 1000A is a super-midsize business jet produced by Hawker Beechcraft Corporation. It was first introduced in 1993 and is an upgrade of the earlier Hawker 800 model. It features an increased MTOW, a longer cabin, and improved performance. The Hawker 1000A is powered by two Garrett TFE731-5BR-1H turbofan engines and is capable of a maximum cruising speed of 517 knots. It has a range of 2,890 nautical miles and a service ceiling of 41,000 feet. The aircraft can accommodate up to nine passengers in a spacious cabin and is typically configured with a full galley and lavatory.
Features
- Engine(s)
- Pratt & Whitney PW305B
- Total Time: (1) 8,229 h/ (2) 5,817 h
- Cycles: (1) 5,097/ (2) 4,016
- Enrolled on ESP Gold
- APU Details
- Sundstrand T-62T-40C8D1
- Total Time: 3,622
- Cycles: 6,203
- Avionics
- 4 Electronic Display – Honeywell ED 800
- 1 TCAS 2000 II – Honeywell RT-951
- 3 Audio Selector Panel – Honeywell AV 850A
- 2 FMS/GPS- Honeywell FMZ 2000
- 2 Symbol Generator-Honeywell SG 818
- 2 Transponder – Honeywell RCZ 833E
- 2 Int Nav Unit – Honeywell RNZ 850
- 1 DME Indicator – Honeywell DI 851
- 2 Flight Guidance Comp – Honeywell FZ 800
- 2 Altimeter – Honeywell BA141
- 1 CVR- Fairchild A100A
- 1 HF COMM – King KTR 953
- 1 EGPWS – Allied Signal MKV
- 2 IRU – Honeywell HG 2001 AB02
- 1 ELT – Kannad 406 AF
- FDR
- ADSB
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