PERFORMANCE - ISA CONDITIONS

MAXIMUM SPEED				335 kts. (385 mph)
CRUISING SPEED (TAS)
Average Cruise Weight			12,500 lbs.

MAXIMUM CRUISE POWER - 1600 RPM
At 22,000 ft				335 kts. (385 mph)
At 31,000 ft				327 kts. (376 mph)
At 35,000 ft				318 kts. (366 mph)
At 37,000 ft				308 kts. (355 mph)

RECOMMENDED CRUISE POWER - 1600	RPM
At 25,000 ft				324 kts. (373 mph)
At 31,000 ft				317 kts. (365 mph)
At 35,000 ft				307 kts. (353 mph)
At 37,000 ft				295 kts. (340 mph)

MAXIMUM RANGE POWER - 1600 RPM
At 25,000 ft				254 kts. (292 mph)
At 31,000 ft				259 kts. (298 mph)
At 35,000 ft				272 kts. (313 mph)
At 37,000 ft				279 kts. (321 mph)

CRUISE RANGE FOR 564 GAL. (3752 LBS.)
USABLE FUEL
Range Allows For Start, Taxi, And Runup; Includes Cruise Climb and
Descent; And Allows For 45 Minutes Reserve	Fuel At Maximum Range
Power, Zero Wind, 14,900 Lbs Takeoff Weight.

MAXIMUM CRUISE POWER
At 25,000 ft				1,128 nm (1,298 sm)
At 31,000 ft				1,342 nm (1,543 sm)
At 35,000 ft				1,494 nm (1,720 sm)

RECOMMENDED CRUISE POWER
At 25,000 ft				1,148 nm (1,321 sm)
At 31,000 ft				1,372 nm (1,578 sm)
At 35,000 ft				1,514 nm (1,743 sm)

MAXIMUM RANGE POWER
At 25,000 ft				1,350 nm (1,554 sm)
At 31,000 ft				1,513 nm (1,740 sm)
At 35,000 ft				1,576 nm (1,814 sm)

RATE OF CLIMB AT SEA LEVEL

TWO ENGINES
At 14,900 lbs 				2,748 ft./min.

ONE ENGINE
At 14,900 lbs 				670 ft./min.

SERVICE CEILING

TWO ENGINES (100 ftjmin.)
At 14,900 lbs				35,800 ft.

ONE ENGINE (50 ftjmin.)
At 14,900 lbs				18,000 ft.

MAXIMUM CERTIFIED ALT			41,000 ft.

TAKE-OFF DISTANCE - FLAPS EXTENDED
Take-off Field Length @ 14,900 lbs   	3854 ft.
Take-off Field Length @ 13,000 lbs   	3112 ft.

LANDING DISTANCE - FLAPS EXTENDED
Landing Distance @ 13,680 lbs   	2390 ft.
Ground Roll       			1,264 ft.

SPECIFICATIONS

WEIGHTS
Maximum Ramp Weight			15,010 lbs.
Maximum Take-Off Weight			14,900 lbs.
Maximum Landing Weight			13,680 lbs.
Maximum Zero Fuel Weight		12,600 lbs.
Basic Empty Weight (With Unusable Fuel,
	Oil and Standard Equipment)	10,120 lbs.
Useful Load (Standard Airplane)		4,890 lbs.
Maximum Usable Fuel (@ 6.7 lbs./gal.)	565 gal./3785 lbs.

WING AREA AND LOADINGS
Wing Area				280.88 sq. ft.
Wing Loading				53.0 lbs./sq. ft.
Power Loading (PT6A-67A: 1200 SHP)	6.21 lbs./shp.

DIMENSIONS
Aft Wing Span				54 ft. 4.7 in.
Forward Wing Span
	Cruise				21 ft. 11.5 in.
	Landing				25 ft. 8 in.
Length					46 ft. 1 in.
Height to Top of Vertical Stabilizer	12 ft. 1 1  in.
Cockpit Height				58.2 in.
Cockpit Width				67 in.
Cockpit Door Width			18.5 in.
Cabin Length (includes Aft Baggage)	253.5 in.
	(Excludes Pilot's Compartment)
Cabin Width				66 in.
Cabin Height				63.5 in.
Entrance Door				28 x 50.4 in.
Forward Baggage Compartment		160 lbs., 19.5 cu ft.
Aft Baggage Compartment			525 lbs., 35 cu. ft.
Total Baggage Capacity			685 lbs., 54.5 cu. ft.

PRESSURIZATION
(8.4 Differential)			Cabin Altitude
Actual Aircraft Altitude - 21,400 ft	Sea Level
Actual Aircraft Altitude - 25,000 ft	1,560 ft.
Actual Aircraft Altitude - 30,000 ft	3,860 ft.
Actual Aircraft Altitude - 35,000 ft	5,940 ft.
Actual Aircraft Altitude - 41,000 ft	8,060 ft.

STANDARD EQUIPMENT

AVIONICS

STANDARD COLLINS PRO LINE 4 WITH DUAL DIGITAL EFIS (H.I.R.F. CERTIFIED) SYSTEM
COMMs (VHF) - Dual Collins VHF-422A's with Dual Antennas VOR/ILS/NAV (VHF)
Dual Collins VIR-432 with ND-870 Indicator and Single NAV Antenna
ADF - Collins ADF-462 with Display in SDU-640B and Antenna

MARKER BEACONS - Dual in VIR-432's with Display in PFD-870
Indicators, and Antenna

GLIDESLOPES - Dual in VIR-432's with Display in ND-870 Indicators, and Antenna

DME's - Dual Collins DME-442's with Display in ND-870 Indicators, and Dual Antennas

TRANSPONDERS - Dual Collins TDR-94's with Dual Antennas, and Pilot and Copilot Control Wheel ATC Ident Buttons 

RADAR - Collins TWR-850 4-Color 2 Channel Doppler/Turbulence Detection Radar with 14' Phased Array Antenna/RT Unit and Display in MFD-870 Multi-Function Display (MFD) 

CONTROLS - Dual Collins CDU-850A Primary ControVDisplays for COMM, NAV, ND, ADF, DME, Transponder, Radar Dual RTU-870A Secondary Controls

AUDIO - Dual DB Systems Model 418 Audio Systems with Dual
Auto COMM and Audio Switches, Crew Interphone, Ground

COMM Power Switch for COMM 1, Dual Cockpit Speakers,
Mic Key Button on Pilot and Copilot Control Wheels,
Dual Hand Held Microphones, Dual Boom Mic Headsets,
Voice and ldent Filters, and Ramp Paging

SENSOR DISPLAY UNITS (RMI's) - Dual Collins SDU-640B Indicators with Bearing from VOR/ADF/FMS and Data from DME/VOR/ILS/FMS

COMPASS SYSTEMS - Dual Collins AHC-85D Attitude Heading Reference System (AHS)

FLIGHT MANAGEMENT - Collins Computers with CMA-764

VLF/Omega Long Range NAV System (FMS) Receiver, DBU-850
Data Base Input Unit, and "E' Field Antenna

FLIGHT DIRECTORS - Dual Collins FCC-850's with Pilot and
Copilot PFD-870 and ND-870 Indicators, Dual MSP-850A Mode
Selectors, CHP-850 Course/Heading Panel, and Dual
Reversionary Controls

AUTOPILOT - Collins APS-850 with APP-85D Control, Electric
Trim (3-Axes) and Pilot or Copilot Flight Director Coupling Selector

AIR DATA SYSTEMS - Dual ADC-850 Air Data Computers with
Dual ASI-850A Indicators for TAS, IAS, OAT, IOAT, and ISA,

AAP-850 Altitude Awareness Controls, and Rosemount Probe

ALTIMETERS/ALTITUDE ALERTER/PRESELECTOR/VERTICAL

SPEED INDICATORS - Dual Collins ALI-850A Indicators

RADIO ALTIMETER - Collins ALT-55B with readout in PFD-870
Indicators, and Dual Antennas

PILOT'S HORIZON INDICATOR - Collins PFD-870 Electronic Primary Flight Display

COPILOT'S HORIZON INDICATOR - Collins PFD-870 Electronic Primary Flight Display

PILOT'S COURSE INDICATOR - Collins ND-870 Electronic Navigation Display

COPILOT'S COURSE INDICATOR - Collins ND-870 Electronic
Navigation Display

STANDBY INSTRUMENTS - 2-inch Altimeter, 2-Inch Airspeed Indicator, 2-inch J.E.T. Al-804 Gyro Horizon with Battery Pack 

DIGITAL CLOCKS - Dual with 24-Hour Time, GMT, Count Up/Down Timers, Trip Timer, and Date (Date for FMS, not displayed on clock)

PAGING - Two Speakers for Cabin Paging

BEECH RADIO ACCESSORIES

WHITE LIGHTING

DUAL AVIONICS MASTER SWITCHES

EMERGENCY LOCATOR TRANSMITTER

ENGINES
Two Pratt & Whitney PT6A-67A Free Turbine Engines flat rated at 1200 Shaft Horsepower each
Propellers - 104" Diameter, Five Blade Metal, Full
Feathering, Reversible, Hydraulically Controlled Constant
Speed, Dynamically Balanced
Fuel Cross Transfer System
Submerged Electric Standby Fuel Boost Pumps
Jet Type Fuel Transfer Pumps
Low Fuel Quantity Warning System
Engine Driven Fuel Boost Pumps
Primary Propeller Governors
Overspeed Propeller Governors
Fuel Topping Governors
Heated Fuel Tank Vents
Complete Engine Anti-icing System with Bleed Air
Heated Engine Inlet
Magnetic Chip Detector
Auto Ignition System
EPA Fuel Purge System
Propeller Synchrophaser
Engine Fire Detection System
Engine Fire Extinguishers *
Propeller Autofeather System

LANDING GEAR AND BRAKES
Tricycle Type Steerable Nose Wheel equipped with shimmy damper,
Beech oil-air struts designed for smooth taxiing
Dual Main Wheel Tires (each side)
Main Wheels and Tires - H19.5 x 6.75 - 10, 8 ply rated
Nose Wheel Tire - 19.5 x 6.75 - 8, 10 ply rated
Two Carbon Disc Brakes on Each Main Gear (Power,
Anti-Skid Brakes)
Landing Gear Position Lights, Down and Locked
Landing Gear Warning Horn and In-Transit Light

CONTROLS
Dual Conventional 3-Axis Control System
Dual Adjustable Rudder Pedals and Toe-Operated Brakes Parking Brake with Hand Control
Two Power Levers, two Propeller rpm Selectors and two Fuel Cut-Off and Condition Levers
Hydraulic Landing Gear with Mechanical Uplock
Hand-Pump Type Auxiliary Landing Gear Extension Control Electric Elevon Trim Tabs (Roll)
Electric Rudder Trim Tabs (Yaw)
Electric Elevator Trim Tabs (Pitch)
Yaw Damper System (Part of Autopilot) Electric Flap/Forward Wing Control
Stall Warning System with Shaker/Pusher Logic

ELECTRICAL
Starter/Generator (Two 300 amp - 28 volt)
Solid State Generator Control Panel - Two One Electric Motor for Operating Flaps One Electric Motor for Operating Forward Wing Landing Gear Warning System with Manual Over-Ride and Automatic Reset
Heated Stall Warning System with Preflight Self Test System
Dual Heated Pilot & Static Heads - Nose Mounted
External Power Receptacle with Annunciation and
Overvoltage Protection
Master Warning and Annunciators, with Push to Test Heated Fuel Vents
Static Wicks
Air Cooled NiCad Battery - 34 AH
Triple Bus System with Auto Load Shedding
Nose Gear Mic and Phone Jack (part of Avionics)
Two Loadmeters (with Left Capable of Battery Ammeter)
One Voltmeter

LIGHTS
Wing Ice Lights
Three Landing Lights (One Nose, Two Wing)
Nose Gear Taxi Light
Position Lights
Dual Map Lights
Adjustable Reading Light for each Cabin Chair and
Toilet Compartment
Indirect Cabin Lighting
One Cockpit Overhead Reading Light
Aisle Courtesy Lights
Entrance Door Light
Aft Compartment Lights
Primary and Secondary Instrument Lighting Systems
Lighting Controlled from Overhead Panel
EL Indirect Cockpit Lighting
Anti-Collision Strobe System (High and Low
Intensity Selectable)

COCKPIT
Dual Electrically Heated, Glass Windshields with Redundant Pilot Windshield Element & Control
Hot Air Windshield Defroster, Main Windshields
Electrically Heated, Cockpit Side Windows
Dual Adjustable Sun Visors
Cigarette Lighter, Two Ash Trays
Fresh Air Outlets
Oxygen Outlets and Console Stored Crew Pressure/Diluter Demand Oxygen Masks with Mic
Sub Panel Mounted Oxygen Controls
Coffee Cup Holders
Dual Cockpit Speakers
Pilot and Copilot Four-Way Adjustable Seats with Shoulder Harness Restraint System and Reclining Feature
Pilot and Copilot Chart Storage Cases and Flight Manual Storage Compartment (Seven Compartments)
Lighted Control Wheel Approach Plate Holders
Two Electronic/Digital Fuel Quantity Indicators
Electronic, Analog Pitch Trim Indicator
Electronic, Analog Roll Trim Indicator
Electronic, Analog Rudder Trim Indicator
Digital Fuel Temperature Indicator
Digital Cabin Temperature Indicator
Dual Digital Deice Pressure Indicator
Digital Oxygen Pressure Indicator
Pneumatic Analog Cabin Altitude and Differential Pressure Indicator
Pneumatic Analog Cabin Climb Indicator
Fire Extinguisher * (Halon) - Hand Held

CABIN
Forward Club Arrangement with Six Lateral Tracking Chairs All are Fully Adjustable with Shoulder Harnesses, Lap Belts and Rectractable Inboard Armrests
Ash Trays for All Occupants
Cupholder for each Cabin Chair
Individual Reading Lights and Fresh Air Outlets
Two Folding Tables
Upright Refreshment Cabinet, Forward Left Side with Water Tank, One Gallon Heated Liquid Container, Two Cup Dispensers; Overboard Drain; Ice Chest, Four Decanters and Waste Container
Oxygen, 77 cu. ft. - One Mask per Passenger including Toilet Compartment (Automatic Deployment)
"No Smoking - Fasten Seat Belt" Signs with Audible Chime
Forward Right Side Baggage Cabinet/Coat Closet
Forward Cabin Closure Door
Aft Cabin Privacy Partition with Sliding Doors and Aisle
Facing Flushing Toilet with Relief Tube
Aft Baggage Compartment with Doors and Baggage Webbing
Cabin Carpet Protector - Vinyl
Air Conditioning * (Freon)
Automatic Bleed Air Type Heating
Fail-Safe (Dual-Pane) Cabin Windows with Manual Dimming (Polarized)
Carpet - Wool Plush - Low Nap
Pressurization - 8.4 Differential
Airstair Door with Hydraulic Snubber, Airstair Door
Courtesy Light
Fire Extinguisher * (Halon) - Hand Held

PUBLICATIONS
Service Information Kit
Airplane Log Book
Two Engine Log Books
Two Propeller Log Books
Pilot's Check List
Beechcraft Warranty ID Card
Eight Passenger Briefing Cards

SERVICE
Two Cabin Door Lock Keys
Tow Bar
Two Pitot Tube Covers
Two Prop Slings
Two Inlet Covers
Inlet Cover Installation/Removal Too]
Two Pair Exhaust Covers
Two AOA Probe Covers
Three Ice Detector Covers
Three Tiedown Rings
Paint Kit
Flight Bag
Control Lock
Three Landing Gear Lock Pins
Nose Landing Gear Door Pin
Six Coat Hangers
Two Boom Mic Pilot's Headsets

ADDITIONAL FEATURES

EICAS (Engine Indicating Crew Advisory System)
All Engine Data (Analog and Digital):
ITT, Torque, Prop RPM, N,, Fuel Flow, Oil Temperature,
Oil Pressure
All Master Caution (Yellow), Status (White)
And Advisory (Green) Messages.  Master
Caution Message With Flasher System
Propeller Syncrophaser Display And
Autofeather Arm Display
Digital Capacitance Type High Accuracy Temperature
Compensating Fuel Gauging System
Inertial Separator Engine Anti-icing System, with Dual
Electric Ice Vane Actuators
Automatic, Lightweight, Low Profile Pneumatic Deicing System
Complete Exterior Urethane Paint
Dual Bleed Air Heating and Pressurization
Electroluminescent Lighted Control Panels
Battery Charging Current Sensor (Safety Sentinel)
External Oxygen Filler Port and Pressure Gauge


All performance specifications and standard equipment subject to change without notice at the option of RAYTHEON AIRCRAFT COMPANY.

Beech airplanes are manufactured by Raytheon Aircraft Company
Wichita, Kansas 67201, U.S.A.