Standard Collins Primary Flight Display (pfd) and Multifunction Display (mfd) three display arrangement


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006 Standard Equipment


Avionics

Collins Pro Line 21

Standard Collins Primary Flight Display (PFD) and Multifunction Display (MFD) three display arrangement

Pro Line 21 Flight Display System includes: pilot’s and copilot’s AFD-3010 - primary flight display (PFD) with altitude preselect, minimum decision altitude select, airspeed, vertical speed, radio altitude, attitude, slip/skid, flight guidance mode annunciation, lateral and vertical course deviation, distance, HSI, weather radar, map, bearing, radio frequency display, elapsed time, universal time coordination (UTC) clock, ram air temperature (RAT); - AFD-3010E multifunction flight display (MFD) with engine parameters, map, weather radar, temperature (SAT, ISA), checklists

Integrated flight information system IFIS-5000 which includes a file server unit FSU-5010, cursor control panel CCP-3000, and introduces enhanced MAP function images

DCP-3030 - display control panel with controls for Baro, menu set, range, engine and V speed refs, Nav/BRG source selection, weather radar menu

Copilot’s electronic horizontal situation indicator (EHSI) - Collins SDU-640 monochrome sensor display unit (SDU) that displays HSI, RMI, heading, course, distance, groundspeed, time to station, lateral deviation, and bearing

Automatic Flight Guidance System (FGC-3000 autopilot) includes: dual FGC-3000 flight guidance computers, FGP-3000 flight guidance control panel, SVO-3000 pitch servo, SVO-3000 roll servo, SVO-3000 yaw servo, yaw damper, automatic pitch trim, control wheel manual electric pitch trim, rudder boost, IAPS-3000 integrated avionics processor system

Air data system includes: dual ADC-3000 air data computers, dual Rosemount pitot/static probes

Dual attitude heading reference system (AHRS) includes: dual AHC-3000 attitude heading reference system computers, dual FDU-3000 flux detector units

Flight Management System (single FMS-3000 with data base) includes: dual CDU-3000 control display units (CDU) with alpha & numeric keyboard for FMS and radio tuning (Comm, Nav, ADF, DME and transponder), left side CDU operates FMS and radio tuning, right side CDU only provides radio tuning, single FMC-3000 flight management computer, single GPS-4000A GPS sensor unit with antenna, DBU-4100 data base input unit, RJ-45 jack for access to FMS and file server, battery pack for pilot’s CDU, copilot’s attitude indicator, and Comm 1

Weather radar system includes: WXR-800 radar receiver/transmitter with 12” antenna displayed on PFD/MFD

Radio altitude system includes: ALT-4000 radio altitude receiver/transmitter with dual antennas displayed on PFD

Honeywell Mark V Enhanced Ground Proximity Warning System (EGPWS) provides protection against controlled flight into terrain (CFIT), as well as, providing wind shear warnings. CFIT warnings include excessive rate of descent, terrain closure rate, excessive altitude loss after take-off or missed approach procedure, insufficient terrain clearance, descent below glideslope and excessive bank angle. Aural warnings and evasive commands are provided in the cockpit. Terrain is displayed on the MFD

Artex ELT C406-2 Emergency Locator Transmitter transmits on 121.5, 243.0 and 406.025 MHz frequencies at a power output adequate for reception by satellites.

Dual VHF-4000 digital VHF Comm transceivers with dual antennas that operates in the 118 to 136.975 MHz frequency range with 8.33 KHz spacing increments. Frequency display on PFD and CDU, single CTL-23 standby Comm/Nav tuning panel for ground Comm.

Single Nav-4000 VHF Navigation Receiver with (ADF) automatic direction finder, display on PFD, and MFD - frequency display on PFD and CDU includes: glideslope (GS) and marker beacons, glideslope display on PFD and SDU-640, marker lights display on PFD, includes: Nav, GS, and marker antennas

Single Nav-4500 VHF Navigation Receiver with frequency display on PFD and CDU includes: glideslope (GS) and marker beacons, glideslope display on PFD, marker lights display on PFD, includes: Nav, GS, and marker antennas

Single DME-4000 distance measuring equipment display on PFD and MFD

Dual TDR-94 Mode S transponders

Dual avionics master switches

Static wicks

Engine indicating system includes: dual DCU-3000 data concentrator unit with display on MFD and PFD (in reversionary mode)

Audio system includes: dual db systems DB-700 digital audio amplifiers with crew headset interphone and hot microphone, dual auto Comm switching, dual cockpit speakers, microphone key button on pilot’s and copilot’s control wheels, dual hand held microphones, dual boom microphone headsets with jacks, dual voice and Ident filters, DB-630 aural tone generator, DB-240 paging amplifier with four cabin speakers

Solid state cockpit voice recorder (SSCVR) - L3 Communications FA2100 with remote area microphone (30 minute recording time)

Standby 2” spherical electro-mechanical attitude indicator

Standby 2” pneumatic airspeed indicator - maximum allowable

Standby 2” pneumatic counter-pointer altimeter

MDC-3110 maintenance diagnostic computer

Engines

Two Williams-Rolls FJ44-2A engines (rated 2,300 lb thrust each)

Engines are twin spool, turbofan, jet propulsion engines with a full length annular bypass duct

Electronic and hydro-mechanical fuel controls

Engine fire detection system

Engine fire extinguishing system

Engine fan synchronizer

Flight Control System

Mechanical primary flight controls

Electric roll trim

Electric pitch trim - normal and standby

Electric rudder trim

Electric flaps with asymmetric protection

Hydraulic roll control (augments aileron control)/speedbrakes/lift dump spoilers

Dual stall warning system/angle of attack system

Takeoff configuration warning system

Rudder boost

Yaw damper

Hydraulic

Two engine driven pumps (3,000 PSI)

1.7 gallon pressurized system with low level annunciator

Ground service connections

Landing Gear And Brakes

Hydraulic extension and retraction system

Single nose gear wheel and tire (18 x 4.4, 10 ply rating)

Single main gear wheels and tires (H22 x 8.25-10, 10 ply rating)

Emergency gear extension system (free-fall)

Mechanical nose wheel steering

Nose wheel pivots 360° with steering pin removed

Independent main wheel disc brakes

Power brakes with anti-skid system

Parking brake

Hydraulic emergency brake system

Electrical

Two starter/generators, 325 Ampere, 28 Volt D.C.

Left and right generator busses, essential bus

Standby bus

24 Volt, 42 Ampere-hour sealed lead acid battery

External power receptacle (28V-1,500 Ampere limit)

Over-voltage protection

Reverse current protection

Feeder fault protection generator

Internal Lights

Internally lighted instruments

Electroluminescent switch panels and control placards

Standby instrument lights

Two overhead map lights with rheostats

Two sidewall map lights with rheostats

Cabin ceiling lights

Entry lights

Cabinetry lights

Overhead reading lights

Table lights

External Lights

Entry lighting

Taxi/landing lights

Wing tip and tail navigation lights

Wing tip and tail strobe lights

Wing inspection ice lights (left side)

Ground awareness beacon

Recognition lights - wingtip

Nose baggage light

Tail cone light

Fuel Systems

548 gallons total usable fuel

Capacitance fuel quantity indicating system

Low fuel quantity warning system

Fuel temperature indicator

Cross transfer fuel pump

Two ejector jet fuel pumps

Two fuel boost pumps (electrical)

Two shut-off valves

Two transfer ejector jet pumps

Six manual defuel drain valves

Lightning protection (flame arrestors)

Fuel vent system

Environmental

Air conditioning (32,000 BTU) and heating system (67,000 BTU)

Dual bleed air pressurization system (8.4 PSI)

Two pressure regulated shut-off valves

Cabin and cockpit ventilation blower

Automatic/manual mode selector

Dual zone, cabin and cockpit temperature system with independent control and cabin control transfer switch

Aft baggage heat provides heat through a convection system in the aft baggage compartment.

Pressurization

Automatic pressurization controller

Low cabin pressurization annunciator

Two outflow valves includes: dump solenoid, maximum differential pressure (DP) limiters and negative DP limiters

Cabin altitude limiters

Oxygen

40 cu. ft. oxygen system

Two diluter demand regulated crew masks with microphones (quick donning)

Seven constant flow passenger oxygen masks

Anti-ice And Rain

Engine inlet anti-ice (bleed air)

Wing leading edge anti-ice (bleed air)

Windshield anti-ice (electrical heat)

Pilot and copilot side window anti fog (electrical heat)

Horizontal stabilizer de-ice (electrical heat/ electrical mechanical)

Pitot-static system anti-ice (electrical heat)

Angle of attack (AOA) transmitter anti-ice (electrical heat)

Windshield defog (heated air)

Dual ice detectors (electrical heat)

Controls And Instrumentation:
Pilot’s/Copilot’s Panel


Primary flight display presentation in normal operation:

Altitude (MDA, preselect altitude)

Distance measuring equipment (DME) readout

Airspeed indicator (with V1, V2, VR, speed references)

Altimeter/vertical speed indicator combined

Radio altitude display/decision height

Attitude indicator (pitch and roll)

Flight guidance annunciation

Lateral deviation - flight management system (FMS), LOC, VOR

Vertical deviation - FMS, glideslope

Radar symbology

Radio frequency - Comm 1 and 2, ATC 1 or 2, Nav 1 and 2, ADF

Ram air temperature (RAT)

Map display

UTC clock/timer

Engine parameters (in reversionary mode only)

Multi-function display presentation in normal operations:

N1: digital display and analog scale with N1 reference markers

ITT: digital and analog display

N2: digital display

Fuel flow: digital display

Fuel temperature: digital display

Oil pressure and temperature: digital display

UTC clock

Checklist/maintenance diagnostics

Radar symbology

Moving map presentation

Audio panel

Display control panel

Master warning and master caution lights

Controls And Instrumentation:
Center Panel/Sub Panel/Pedestal


Center panel:

Flight guidance panel

Annunciator panel

CTL-23 tuning unit

Pressurization controls

Engine firewall controls

Engine fire extinguisher controls

Sub panel:

Environmental controls

Oxygen pressure gauge

Hydraulic pressure gauge

Load meters

Volt meter

Fuel quantity indicators

Cabin altitude/pressure indicator

Pedestal:

Engine controls

Dual control display units (CDU’s) (pilot’s CDU provides radio tuning and FMS control, copilot’s CDU provides radio tuning only)

Flap position indicator

Cursor control panel

Flap control

Pitch trim indicator

Rudder trim indicator

Roll trim indicator

Rudder boost

Yaw damper

Speed brake

Parking brake/emergency brake

Lift dump control

Cabin

Six passenger chairs in cabin - four arranged in forward club configuration and two forward facing aft seats. All chairs feature retractable adjustable headrest, retractable inboard armrest, three-point restraint system, life vest storage, and seat back storage pocket. The four chairs in the club configuration also feature lateral and fore-aft tracking, 180° swivel and full berthing recline (this recline is limited by the door and cabinet)

New seat base contour to give more foot room for the 5th and 6th seat.

Aft cabin, non-belted, flushing toilet with toilet paper dispenser

Aft cabin partitions with sliding privacy doors

Forward right hand refreshment/baggage cabinet features a cabin light switch, hot water switch, lighting over the service area, hot water tank, cup dispenser, condiment bin, drip pan with sponge, front fold down work surface, pull out bin for mini liquor bottle and general storage, JEPP book storage (2 books), stainless steel trash container, ice chest, general storage provisions, fold out coat rod, and baggage tie down provisions

Cabin temperature and lighting control panel

Two executive tables

3 personal computer power outlets (110 VAC) provides outlets in each table console and a 3rd outlet in cockpit right side circuit breaker panel for use with a laptop personal computer.

Cabin fire extinguisher* (Halon)

*Warning - contains Halon substance which harms public health and environment by destroying ozone in the upper atmosphere

Fasten seat belt/no smoking signs

Emergency exit signs

Cabin coat rod in cabinet

Overhead panels containing an oxygen mask, air vent and reading light for each passenger

2 cupholders for each passenger

Pleated window shades

Relief tube in the lavatory

Cockpit

Two complete crew stations with dual controls includes: control wheels, adjustable pedals and brakes

Removable lighted control wheel approach chart holders

Crew seats are adjustable and include four-point restraint harnesses

Emergency oxygen system provides two diluter demand masks for the crew members

Pilot and copilot Nav chart storage cases

Crew station cupholders

Crew station assist handle

Cockpit/cabin partition with curtain

Cold/fresh air outlets

115V Outlet (right side circuit breaker panel)

Cockpit hand fire extinguisher* (Halon)

*Warning - contains Halon substance which harms public health and environment by destroying ozone in the upper atmosphere

Additional Features

Remote low engine oil sensor system provides the operator of the aircraft the ability to check the oil system without a stool or ladder. The remote oil test switch/indicator is located on a maintenance panel in the aircraft right side maintenance bay.

Publications*

*Note: additional publications not specified here may also be supplied

Directory - Raytheon Aircraft Service Centers

Certificate of aircraft registration

Certificate of airworthiness

Aircraft component Serial No. Inventory

Aircraft log book

Engine log books

CD-ROM aircraft maintenance manual

Engine maintenance manual (Williams-Rolls)

Avionics systems manual (Rockwell Collins)

Avionics systems pilots guide (Rockwell Collins)

CD-ROM illustrated parts catalog

CD-ROM wiring diagram manual

Main battery log

FAA approved Airplane Flight Manual

Pilot’s operating manual

Pilot’s checklist

CD-ROM structural repair manual

CD-ROM component maintenance manual

Passenger briefing card

Ground personnel emergency briefing card

Loose Equipment

2 Bose aviation AHX 32-01 headsets

Aircraft model

Aircraft keys

Jack pads (2) and nose jack adapter

Pitot, AOA, ice detector covers

Gust lock assembly

Emergency exit locking pin assembly

Tow bar (portable)

CPAS-3000 Collins portable access software

Fuel sample unit

Rigging pin set

Engine intake covers (2)

Smoke goggles (2)

Individual flotation devices

Flashlight (2 D-cell)

Nose landing gear adjustment tool

Touch up paint kit

2nd center aisle carpet

Training Entitlements*

*Note: training entitlements expire one year after retail delivery

Flight training - training to type rating for two pilots

Pilot’s minimum prerequisites - private or commercial license; multi-engine rating, instrument rating, and a minimum of 1,000 hours total flight time

Maintenance training - standard maintenance training for two maintenance personnel, course not to exceed ten training days

General Standard Warranty*

*Standard warranty coverage is for “normal” use only. Not for fractional aircraft or high utilization operators

Raytheon Aircraft Company manufactured parts and Supplier systems and components - five years (no hours limit)

Exterior paint and interior finish items - two years (no hours limit)

Collins avionics - five years (no hours limit)

Williams-Rolls engines - three years or 1,500 hours, from first use (whichever occurs first: balance prorated on a straight line basis to 1,750 hours)


12/21/05 Aircraft Offered Subject To Prior Sale: Standard Equipment And Price Subject To Change Without Notice

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