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HAWKER700

Background/History

The Hawker 700 has its origins in the de Havilland DH.125 medium-sized corporate jet which first flew in August 1962. A total of 77 units were built by de Havilland before the company was absorbed by Hawker Siddeley.

Following the merger, the design was refined to produce the -400 series and then the -600 series, whose stretched fuselage increased main cabin seating capacity from six passengers to eight, or as many as fourteen in a high-density arrangement. A new model, the HS.125-700, made its first flight in June 1976.

Powered by Garrett TFE731-3R-1H engines, the -700 offered substantial improvements in cruise speed and range along with reduced fuel consumption. The -700 received US and UK certification in mid-1977, with initial deliveries that same year. A total of 243 units were produced before the -700 was replaced by the HS.125-800 in 1984.http://jetav.com/hawker-beechcraft-125-700-performance-specs/

Power

The Hawker 700 is powered by two Honeywell TFE731-3R-1H engines rated at 3,700 lbs. thrust each. Engine inspection interval is 4,200 hours.

Avionics

The Hawker 700 was originally equipped with the comm/nav/ident radios typical for the period, along with analog electromechanical instrument displays. The panels of many of these aircraft have been updated with a variety of modern instruments and equipment.http://jetav.com/hawker-beechcraft-125-700-performance-specs/

Design Features

The Hawker 700 is a medium range, twin turbofan-powered business aircraft configured as a cantilever low swept-wing monoplane with a swept cruciform tail and retractable tricycle landing gear. The two engines are mounted on the rear fuselage, and most have been fitted with thrust reversers, although reversers were not standard equipment on the -700.

Accomodations

The Hawker 700 is normally configured to accommodate eight passengers in a standard double-club arrangement. With a cabin height of 5.8 ft., width of 5.9 ft., and internal length of 21.3 ft., the 700s cabin is somewhat roomier than the cabins of many aircraft in its class.http://jetav.com/hawker-beechcraft-125-700-performance-specs/

Pesos (libras)Hawker 125-700Max Rampa25000Max Despegue24800Landing Max22000Cero Combustible16050 cBOW14100Max Payload1950Carga til10900Payload Ejecutivo1600Max Fuel9450Max Fuel9450Payload Disponibilidad Max Fuel1450Payload Disponibilidad Fuel Max8950Disponibilidad de combustible Exec Payload9300LmitesHawker 125-700MMO0.800Transicin Altitud FL / VMON / ACabin presurizacin (PSI)8.6AIRCRAFTPERFORMANCEAeropuerto PerformanceHawker 125-700A (el nivel del mar, ISA Temp)5800A (5000 ', @ 25 C)6950Hot / Alto WAT21000NBAA IFR RangosV2 @ SL ISA, MTOW1350131VREF108Distancia de aterrizaje con 4 Pasajeros2019AscensoHawker 125-700Tiempo para subir / AltN / ACambio de motor Out pies por minuto1350FAR 25 Motor de salida Grad (ft / nm)330AIRCRAFTPERFORMANCETechos (ft)Hawker 125-700Titulado41000Todo Eng Srv41000Eng Servicio Out21600Nivel del Mar Cabaa21500Crucero de Largo AlcanceHawker 125-700KTAS390Flujo de combustible1275AltitudFL 390Rango Especfico0.306Crucero de alta velocidadHawker 125-700KTAS425Flujo de combustible1600AltitudFL 350Rango Especfico0.266AIRCRAFTPERFORMANCE

The present index makes representation of part of the equipment manual, to publicize the use of information search, since there is much personal aircraft that don't know the suitable use of information search mechanism.

Pag. 62 del manualExample.

When a revision is the inserted, the revision number, the date the revision is inserted into the manual, and the of initials the person(s) inserting the revision should be recorded on this page.

DIMENSIONS AND AREAS

LIFTING AND SHORINGPLACARDS AND MARJINGS

11ENVIRONMENTAL/AIR CONDITIONING

21

AUTO FLIGHT 1351

22COMUNICATIONS 1351

23ELECTRICAL POWER

24EQUIPMENT / FURNISHINGS

25

FIRE PROTECTIN

26FLIGHT CONTROL

27FLIGHT CONTROL

27FUEL28

HYDRAULIC PORWER29

ICE AND RAINPROTECTION

30ICE AND RAINPROTECTION

FINREFERENCIAS.Aircraft Maintenance ManualVol.1 Introduction thru Chapter 27

Aircraft Maintenance ManualVol.2 Chapter 28 thre chapter 57 (&91)

Published By RAYTHEON AIRCRAFT COMPANYP.O. Box 85 Wichita, Kansas 67201 U.S.A.

Aircraft Technical Publishers101 South Hill DriveBrisbane, CA 94005ATP

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SectionTopicGeneral InformationManufactureS IntrodutionService BulletinNumerical Index.Aircraft GeneralPlacards and MarkingsList of Effective PAGESGENRALEXTERIOR PLACARDS AND MARKINGS

AirframeEnviromental / Air ConditioningList of Effective PagesCompressionDistributionPressurization ControlTemperature ControlAutoFlightList of EffectiveSpeed Attitude CorrectionSystem MonitorComunicationsGeneralElectrical PowerGeneralAC GenerationDC Generator..