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Eclipse 500 User Manual

Eclipse 500
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Table of Contents Eclipse 5OO Systems Manual
Copyright © — Eclipse Aviation Corporation
viii Version 2.0 April 2007
13.3.1 Attitude and Heading Reference System (AHRS) ...............................................278
13.3.2 Air Data Computer 3 (ADC 3)..............................................................................278
13.4 SYSTEM DESCRIPTION ..............................................................................................280
13.4.1 Pitot/ AOA............................................................................................................280
13.4.2 Static Ports ..........................................................................................................281
13.4.3 Pitot / Static .........................................................................................................281
13.4.4 Probe and Port Heat............................................................................................282
13.4.5 Outside Air Temperature (OAT)...........................................................................282
13.4.6 Air Data Computers (ADC) ..................................................................................283
13.4.7 Integrated Sensor Suite (ISS)..............................................................................283
13.5 CONTROLS AND INDICATORS ...................................................................................284
13.5.1 Sensor Selection .................................................................................................284
13.6 NORMAL OPERATIONS...............................................................................................285
13.7 ABNORMAL PROCEDURES .........................................................................................286
13.7.1 Air Data Disagreement ........................................................................................286
13.7.2 Sensor Failure .....................................................................................................286
13.8 CREW ALERTING SYSTEM MESSAGES ....................................................................287
13.9 AIR DATA REVIEW QUESTIONS.................................................................................288
14. Primary Flight Display (PFD)..............................................................................................290
14.1 GENERAL .....................................................................................................................290
14.2 LIMITATIONS AND SPECIFICATIONS.........................................................................291
14.3 SYSTEM DESCRIPTION ..............................................................................................292
14.3.1 Initialization..........................................................................................................292
14.3.2 Normal Mode.......................................................................................................293
14.3.3 Tile 1 – Flight Mode Annunciation (FMA) ............................................................294
14.3.4 Tile 2 – Attitude Direction Indicator & Primary Flight Information ........................295
14.3.5 Tile 3 – Primary, Secondary NAV Source Selection, Data block and
Left Line Select Keys...........................................................................................313
14.3.6 Tile 4 – Horizontal Situation Indicator (HSI) and Overlays...................................316
14.3.7 Tile 5 –Communication, Navigation, Surveillance Display, Data Block and Right
Line Select Keys..................................................................................................323
14.4 NORMAL OPERATIONS...............................................................................................327
14.4.1 Communication, Navigation and Surveillance (CNS) ..........................................327
14.5 ABNORMAL PROCEDURES ........................................................................................336
14.5.1 PFD Failure .........................................................................................................336
14.5.2 PFD Composite Mode .........................................................................................336
14.6 CREW ALERTING SYSTEM MESSAGES ...................................................................344
14.7 PFD REVIEW QUESTIONS .........................................................................................345
15. Multi Function Display (MFD).............................................................................................348
15.1 GENERAL .....................................................................................................................348
15.2 LIMITATIONS AND SPECIFICATIONS.........................................................................349
15.3 SYSTEM DESCRIPTION ..............................................................................................350
15.3.1 Initialization..........................................................................................................350
15.3.2 Multi Function Display (MFD) Layout...................................................................351
15.4 TILE 1 – MFD ATTITUDE DIRECTION INDICATOR (ADI) ...........................................352
15.4.1 Air Data Source Selection (ADC & AHRS) ..........................................................353
15.4.2 Attitude Heading Reference System (AHRS) Sources ........................................353
15.4.3 Air Data Computer Sources.................................................................................353
15.5 TILE 2 – ENGINE INSTRUMENTS ...............................................................................354

Table of Contents

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Eclipse 500 Specifications

General IconGeneral
ManufacturerEclipse Aerospace
ModelEclipse 500
TypeVery Light Jet
Engines2 × Pratt & Whitney Canada PW610F turbofans
Thrust per engine900 lbf (4.0 kN)
Wingspan37.9 ft (11.6 m)
Height11.0 ft (3.4 m)
AvionicsAvio NG
First FlightAugust 26, 2002
Maximum Speed430 mph
Range1, 125 nautical miles
Service Ceiling41, 000 ft (12, 500 m)
Crew1 or 2
Max Takeoff Weight6, 000 pounds
Seating Capacity4-6
Length33 feet 6 inches
Empty Weight3, 550 pounds
PayloadVaries with configuration and fuel load

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