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RAYTHEON BAe-125-700/800

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H25B
Aircraft
Name BAe-125-700/800
Manufacturer RAYTHEON
Body Narrow
Wing Fixed Wing
Position Low wing
Tail Cruciform tail
WTC Medium
APC C
Type code L2J
Engine Jet
Engine count Multi
Position Both sides of rear fuselage
Landing gear Tricycle retractable
Mass group 3


Manufacturered as:

BRITISH AEROSPACE U-125
BRITISH AEROSPACE BAe-125-700
BRITISH AEROSPACE BAe-125-800
BRITISH AEROSPACE C-29
HAWKER BEECHCRAFT Hawker 850
HAWKER BEECHCRAFT Hawker 900
HAWKER BEECHCRAFT Hawker 750
HAWKER SIDDELEY HS-125-700
RAYTHEON Hawker 800
RAYTHEON Hawker 850
RAYTHEON U-125


RAYTHEON BAe-125-700/800

RAYTHEON BAe-125-700/800 RAYTHEON BAe-125-700/800 3D

Description

Twin turbofan executive jet. In service since 1977 (800 since 1984). Recent version of the worlds longest running corporate-jet program (DH-125, HS-125, BAe-125-700, BAe-125-800). US-Mil. type: C-29. The original Bae 125-800 type has been improved and sold to RAYTHEON, USA, now designated Hawker 800 (new developments: Hawker 850SP, 850XP). Over 1000 aircraft were built in all versions.

Technical Data

Wing span 15.7 m51.509 ft
Length 15.6 m51.181 ft
Height 5.4 m17.717 ft
Powerplant 700: 2 x 16.6kN Garrett TFE 731-3-RH turbofans.

800: 2 x 20.7kN Garrett TFE 731-5BR-1H turbofans.

Engine model Garrett TFE731

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
Descent
(to FL100)
Descent (FL100
& below)
Approach
V2 (IAS) kts IAS kts IAS kts IAS kts MACH TAS 463 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance 1645 m ROC 3100 ft/min ROC ft/min ROC ft/min ROC ft/min MACH 0.86 ROD ft/min ROD ft/min MCS kts Distance 1250 m
MTOW 1243012,430 kg
12.43 tonnes
kg
Ceiling FL430 ROD ft/min APC C
WTC M Range 30003,000 nm
5,556,000 m
5,556 km
18,228,346.47 ft
NM

Accidents & Serious Incidents involving H25B

  • H25B, vicinity Owatonna MN USA, 2008 (RE LOC HF) (On 31 July 2008, the crew of an HS125-800 attempted to reject a landing at Owatonna MN after a prior deployment of the lift dumping system but their aircraft overran the runway then briefly became airborne before crashing. The aircraft was destroyed and all 8 occupants were killed. The Investigation attributed the accident to poor crew judgement and general cockpit indiscipline in the presence of some fatigue and also considered that it was partly consequent upon the absence of any regulatory requirement for either pilot CRM training or operator SOP specification for the type of small aircraft operation being undertaken.)