Citation CJ4X User Manual

Audio Control Panel (ACP) ....................................................................................................................................... 30 Electrical Panel............................................................................................................................................................... 30 Primary Flight Display (PFD) .................................................................................................................................... 31 Attitude Indicator .................................................................................................................................................... 32 Flight Guidance System Annunciator .............................................................................................................. 34 Altimeter/Altitude Display ................................................................................................................................... 36 Vertical Speed Display ........................................................................................................................................... 38 Airspeed Display ...................................................................................................................................................... 39 Citation CJ4X User Manual 3 Version 1.0 Build 1709 (September 2017) Angle-of-Attack Indicator (AoA) ....................................................................................................................... 42 Multi-Function Display (MFD) ................................................................................................................................. 43 Engine Indicating System (EIS) ........................................................................................................................... 44 Caution Advisory System (CAS) ......................................................................................................................... 49 Upper Information Panel ...................................................................................................................................... 52 Navigation Display (Apply for both MFD and PFD) ................................................................................... 55 Present Position (PPOS) Map Format .............................................................................................................. 60 Terrain Overlay ......................................................................................................................................................... 61 Plan Map Format ..................................................................................................................................................... 62 TCAS Map Format ................................................................................................................................................... 63 Data Line ..................................................................................................................................................................... 64 PFD Menu ................................................................................................................................................................... 66 Bearing Source Menu (PFD) ................................................................................................................................ 67 Configuration Menu (PFD) ................................................................................................................................... 68 References Menu (PFD) ......................................................................................................................................... 69 MFD Upper Menu.................................................................................................................................................... 70 MFD Lower Menu .................................................................................................................................................... 71 Map Symbology Menu (MFD) ............................................................................................................................ 72 Database Effectivity Page ..................................................................................................................................... 73 Navigation Data Page ............................................................................................................................................ 74 Standby Primary Flight Display (PFD) .................................................................................................................. 75 Airspeed Display ...................................................................................................................................................... 76 Altitude Display ........................................................................................................................................................ 78 Attitude Display........................................................................................................................................................ 79 Display Menu ............................................................................................................................................................ 82 Autopilot Panel (APP) / Flight Guidance Panel (FGP) .................................................................................... 84 Display Control Panel (DCP) .................................................................................................................................... 86 SimIcons Panel .............................................................................................................................................................. 88 Tilt Panel ............................................................................................................................................................................... 89 Cursor Control Panel (CCP) ...................................................................................................................................... 92 Lighting Panel .................................................................................................................................................................... 94 Throttle Quadrant Panel ................................................................................................................................................ 95 Trim Panel ............................................................................................................................................................................ 97 Flight Management System (EasyFMC) ................................................................................................................... 98 Layout ............................................................................................................................................................................... 98 Citation CJ4X User Manual 4 Version 1.0 Build 1709 (September 2017) Pages Components ................................................................................................................................................... 101 Note Regarding Pages Navigation...................................................................................................................... 102 Start ................................................................................................................................................................................. 102 FMC Pages .................................................................................................................................................................... 102 Flight Plan Initialization............................................................................................................................................ 105 Definition of Origin & Destination Airports & Runways........................................................................ 105 Entering Waypoints .............................................................................................................................................. 106 Deleting Waypoints .............................................................................................................................................. 107 Saving The Flight Plan ......................................................................................................................................... 108 Clearing The Flight Plan ...................................................................................................................................... 108 FMC Messages on Scratchpad .............................................................................................................................. 108 Radio Stack ........................................................................................................................................................................ 110 Ramp Manager ................................................................................................................................................................ 113 Virtual Cockpit Tour............................................................................................................................................................ 115 Folder Structure ................................................................................................................................................................... 117 Paint Kit ................................................................................................................................................................................... 119 Fuselage Master.......................................................................................................................................................... 119 Engines Master ............................................................................................................................................................ 120 Left & Right Fuselage Masters .............................................................................................................................. 121 Left & Right Wing Masters ..................................................................................................................................... 122 Installing your new livery ........................................................................................................................................ 122 Product Support .................................................................................................................................................................. 124 Product Changelog ............................................................................................................................................................. 125 Acknowledgements ............................................................................................................................................................ 126 Citation CJ4X User Manual 5 Version 1.0 Build 1709 (September 2017) Introduction Thank you for purchasing Citation CJ4X from NextGen Simulations. From all of us here at NextGen Simulations, we hope you enjoy this product as much as we enjoyed developing and testing it for you. Citation CJ4X consists of a simulated replica of the Citation Model 525C and developed for use with Microsoft® Flight Simulator® X, Microsoft® Flight Simulator® X: Steam Edition, Lockheed Martin® PREPAR3D® v1, v2 and v3 (all of them are 32-bit) and Lockheed Martin® PREPAR3D® v4 (dedicated 64-bit version). This product features a Mid-Level systems programming, featuring also an advanced FMS developed and licensed by Eric Marciano. And it has been simplified as well, to allow you enjoy the simming experience while bringing you a good look-and-feel of this marvelous aircraft. Product Features Summary This package includes:  Two accurate models of the Citation CJ4, differing in its vertical stabilizer shape  Frame-rate friendly models while keeping good look-and-feel  Ground service  12 different liveries  Paint Kit  Different Cameras outside and inside the aircraft  2D Cockpit (Main Panel of Pilot and Copilot, plus 8 subpanels including zoomed displays popups, for a total of 13 subpanels), a Mini Panel and a Semi-functional 3D Virtual Cockpit, with 3D Virtual Cabin  Custom-coded animations, especially for 3D cockpit  Flight Management System developed and licensed by Eric Marciano, using Flight Simulator GPS database  Original replica of Collins ProLine 21 avionics  Easy-to-use Autopilot Citation CJ4X User Manual 6 Version 1.0 Build 1709 (September 2017)  Realistic & Authentic Williams FJ44-4A Engine Soundset, plus cockpit sounds (Environment, CAS Aural Warnings, V-speeds Callouts and GPWS Callouts)  Extensive usage of FSX SDK, and Prepar3D SDKs for better performance  All models are P3Dv4 SDK-compliant Citation CJ4X User Manual 7 Version 1.0 Build 1709 (September 2017) Installation For installation, Setup executable searches automatically your Flight Simulator path, depending on the platform you choose to install at. In case of problems while retrieving directories (e.g.: because it is pointing to a path where there are no FS-related files), it is recommended to repair your Flight Simulator and/or Prepar3D installation. After installing this product on your PC, you will receive these prompts, only if you installed for FSX and/or FSX-SE. Because of the FSX Module Trusting Engine, which is the same one Microsoft developed for software trustiness verification by digital signature, these kind of situations are normal. Just follow these steps and everything will work. Citation CJ4X User Manual 8 Version 1.0 Build 1709 (September 2017) ‘The publisher could not be verified. Are you sure you want to run this software?’ or ‘Do you want to run this software?’ question dialog. Here, you should always answer Run for each of the modules the prompts are requesting permission for loading. Not doing so, will result in the aircraft NOT loading and the sim crashing to desktop when the aircraft is selected and loaded. Also, there is an additional prompt like the one in the figure above this paragraph. In order to prevent prompt nagging with subsequent FS sessions, it is recommended to click Yes on the second prompt for each of the modules, so that the simulator will trust always on them and will never prompt again in the future. If you installed this product under Prepar3D, these prompts never appear, so you will never be disturbed, even on the aircraft’s first load. Citation CJ4X User Manual 9 Version 1.0 Build 1709 (September 2017) Manuals Structure This product includes the following manuals:  Citation CJ4X Main User Manual (You are reading it now!)  Citation CJ4X Tutorial Flight  Citation CJ4X Checklists All together may seem like a lot of information but these manuals were written in order for you to understand clearly how to use this aircraft. The following is a summary about how to get the most out of these manuals: Main User Manual In this document, we have collected into one place as much information about how to use this Citation CJ4X as possible. Here you will find the most important product stuff such as the aircraft features, the explanation of the flight instruments, repaint kit, development changes log, support details, etc. Tutorial Flight In order to help newbies get acclimated to the capabilities of the Citation CJ4X, this tutorial gets you up and running quickly. This tutorial begins first with a Quick-Start Guide that will take you from sim loading to launching off on your first flight, whose purpose is to keep things as simple and straight- forward as possible, in order to give you the opportunity to enjoy what the simulation has to offer without getting you lost! This tutorial will start you in a powered-up and ready-to-go CJ4 from Key West International Airport (KEYW), and you will follow step-by-step everything to eventually arrive at Raleigh-Durham International Airport (KRDU). Checklists For those who are familiar with this aircraft or if you want to follow real procedures like the real pilots, this manual is for you. This section of the general product documentation should be thought as a step-by-step guide to operate the aircraft. No matter if you start your flight in Cold & Dark condition or if you are on the runway and ready for takeoff, this guide gives you a step-by-step process to take you to the next phase of flight. Citation CJ4X User Manual 10 Version 1.0 Build 1709 (September 2017) Quick-Start Guide/Frequently Asked Questions This section is designed to get you flying this aircraft as soon as possible. It is recommended to read it in order to answer most of the questions asked on technical support. Q: Where can I find the airplanes after installing? A: In FSX or FSX-SE, under the Select Aircraft dialog, you can search by manufacturer and by publisher. For this aircraft, Manufacturer is Cessna and Publisher is NextGen Simulations. Just remember to verify if the ‘Show All Variations’ button is checked. If not, please check it and you will get all liveries included in the product. In Prepar3D, under the Select Vehicle dialog, you can search by Manufacturer, Vehicle Type and Publisher, through the vehicles list. For this aircraft, Manufacturer is Cessna, Vehicle Type is Citation CJ4 and Publisher is NextGen Simulations. You can also type ‘nextgen’ on the Search box, and you will get the list of all NextGen’s aircraft and liveries. Citation CJ4X User Manual 11 Version 1.0 Build 1709 (September 2017) Q: How do I perform an Engine Start? A: You can either press Ctrl+E, and the automatic engine start will commence, or follow the procedures for manual engine starting, given in the Tutorial Flight section of the general documentation. Q: How do I access Camera views? A: In FSX, FSX-SE and Prepar3D (up to v2), click on menus Views>View Mode>Cockpit or Views>View Mode>Aircraft. In Prepar3D (since v3), go to Views>Change View>Cockpit or Views>Change View>Aircraft. There you will get all the cameras list for outside and inside the aircraft. Citation CJ4X User Manual 12 Version 1.0 Build 1709 (September 2017) Also, you can access to both cameras lists by right-clicking anywhere in the 3D scene to display the contextual menu (applies on all platforms), then choose your preferred view through the Cockpit menu or the Aircraft menu. Q: How can I update AIRACs or Navdata? A: More details here. Q: Why the FMC in 2D view looks different than the FMC in 3D cockpit? A: More details here. Citation CJ4X User Manual 13 Version 1.0 Build 1709 (September 2017) CJ4 Background The CitationJet (CJ) series (Model 525) are light business jets part of the Citation family. As of June 2017, 2,000 units have been delivered with five million hours flown. The CitationJet is a low-wing cantilever monoplane with retractable trailing-link tricycle landing gear, a pressurized cabin, a T-tail, and is powered by two Williams FJ44 turbofan engines that are pylon- mounted on the rear fuselage. Basically an all new aircraft, the CitationJet used a modified version of the Citation's forward fuselage, but with a new supercritical laminar flow wing, and a new T-tail configured tailplane. It features EFIS avionics and single pilot certification. CitationJet/Model 525 First delivered in 1993, the original CitationJet, or Model 525, was created as a replacement for the Citation I. Compared to the Citation I, the CitationJet has a modified fuselage, a new supercritical laminar flow wing, a new tail, and new avionics. Its cabin also has a lowered aisle for increased cabin height. The CitationJet comes equipped with two Williams FJ44-1A turbofan engines. It has a normal cruise speed of 355 knots, a range of 1,250 nautical miles, a climb rate of 3,311 feet per minute, and requires approximately 3,910 feet of runway for takeoff and 3,309 feet for landing. In 2000, CJ1 was introduced to the market. In 2005, they moved on to the CJ1+. For the CJ1+, the Williams FJ44-1AP FADEC-controlled engines were used, giving the CJ1+ slightly more thrust and increased operating weights. The CJ1+ was also given an interior upgrade, and its ProLine 21 avionics system was equipped with FMS-3000, providing full 3D navigational capabilities. Parallel to the timeline of the CJ1/CJ1+, CJ2 was introduced in 2000 and followed the CJ2+ in 2005. The CJ2 comes equipped with FJ44-2C engines, while the FJ44-3A-24 engines found on the CJ2+ offer better fuel efficiency, an increased range, improved climb rate, better takeoff performance and Citation CJ4X User Manual 14 Version 1.0 Build 1709 (September 2017) increased useful payload, as well as a redesigned cabin for extra noise reduction, making it a significantly more comfortable ride for passengers. FADEC was also added to the CJ2+, making flights more comfortable for the pilot, as well. The CJ3 hit the market in 2004, followed by the CJ3+ in 2014. The biggest changes that took place from the CJ3 to the CJ3+ took place in the cockpit with an upgraded avionics system and complete cockpit redesign, moving from the Rockwell Collins ProLine 21 found on the CJ3 to the Garmin G3000. The change from the ProLine 21 to the G3000 eliminated many of the switches previously found in the cockpit, leading to a complete redesign. FADEC control, air conditioning, pressurization, ignition control, lights and system test, all of which were previously controlled by switches, were integrated into the G3000. Citation CJ4 (Model 525C) Model 525C was first introduced in 2006, with a moderately swept wing similar to those found on the Citation Sovereign. Like its predecessor the Citation CJ3, is a stretch extension of the previous Citation Jet model, its cabin is 21 inches longer than the CJ3, allowing it to seat as many as nine passengers with a single pilot. Like the CJ3, the CJ4 comes equipped with the ProLine 21 avionics system. It first flew on May 5th 2008, from McConnell AFB in Wichita, Kansas and first deliveries started in 2010. It is equipped with two Williams FJ44-4A turbofan engines, and the CJ4 has a normal cruise speed that blows all of the previous Citation Jets out of the water at 443 knots, a range of 2,165 nautical miles, a climb rate of 3,854 feet per minute, and it requires approximately 3,410 feet of runway to takeoff and 2,940 to land. There are 150 Citation CJ4 aircraft in operation with 7 in shared ownership and 143 wholly owned. By continent, North America has the largest percentage at 77%, followed by Europe at 14% for a combined total of 91%. Also, 7% of the 150 Citation CJ4 jets in operation today are in fleet ownership with five different companies each having five aircraft. Additionally, 5% of the Citation CJ4 jets are leased. Citation CJ4X User Manual 15 Version 1.0 Build 1709 (September 2017) Product Package Overview Exterior Models Two different models are included here, they differ in their vertical stabilizer shape. All models are optimized for better performance while keeping good look and feel. On Prepar3D (since v3), they count with Dynamic Reflection and Dynamic Lighting capabilities (since v4) for greater experience. Citation CJ4 using traditional CJ V-Stab since 525C-0001 Citation CJ4 using new and improved V-Stab since 2014 production units Liveries Choose from 12 high-quality liveries included in this product. List of available repaints out-of-box Citation CJ4X User Manual 16 Version 1.0 Build 1709 (September 2017) Paintkit This product features also a detailed paint kit for those who would like to paint their own liveries. Offered in Photoshop format and GIMP format, no matter which of them you use, your imagination is the limit. Flight Deck Both 2D and 3D versions of the CJ4’s flightdeck are provided. Option for different screen ratios is available as well, and 16:9 widescreen is default. Ratios available are: 16:9 and 4:3. Citation CJ4X User Manual 17 Version 1.0 Build 1709 (September 2017) 16:9-widescreen 2D panel counts with 4 main panel alternatives: Pilot IFR view, Pilot VFR view, Copilot IFR view and Copilot VFR view. 4:3-squarescreen 2D panel counts with only 2 main panel alternatives: Pilot view and Copilot View (both IFR view-mode). The 2D flightdeck also counts with the following subpanels:  Tilt Panel (Left)  Tilt Panel (Right)  Lighting Panel  Throttle Quadrant Panel/Control Stand  Trim Panel  FMC  Radio Stack All 2D panel functionality is available on the 3D Virtual Cockpit. Flight Management System NextGen Simulations is proud to feature EasyFMC, developed and licensed for use with this product by FS developer Eric Marciano. This EasyFMC is intended for using ONLY with this aircraft. It CANNOT and is STRICTLY PROHIBITED its installation or use with any other NextGen aircraft or third-party aircraft. For more information about EasyFMC, check here: http://emarciano.free.fr/En/EasyFMC.htm The FMS interacts with the autopilot to provide route lateral navigation (LNAV). The NAV mode of the autopilot, when switched to FMS navigation source, directs the Autopilot to fly the flight plan route automatically. Users can use the FMS to manually create flight plans without using the FSX/P3D default flight planner. About navigation database, this FMC utilizes Flight Simulator GPS database to maintain consistency with the world you are flying on, so this product does not count with support for third-party databases such as Navigraph FMS Data or Aerosoft NavDataPro, however this feature is being reviewed for future development. For more information about how to update the default GPS database, please visit this website: https://www.aero.sors.fr/navaids3.html Systems Programming The real-life CJ4 is a complex aircraft in terms of systems, especially autopilot and engine control (FADEC). There is a high level of automation on this aircraft, but here the Citation CJ4X has been simplified for you, so that you enjoy a greater flight-simming experience without being overwhelmed by a full-level simulation. Most of the essential systems (Hydraulics, Electrical and Fuel Systems especially) have been simulated for normal conditions ONLY, so abnormal conditions such as engine fires or in-flight emergencies are not simulated here. This aircraft also counts with a basic GPWS rendition as well, with Altitude & Decision Height Callouts and Sinkrate & Excessive Bank Angle Awareness Callouts. Sounds This product counts with the most realistic sound rendition of the Williams FJ44-4A turbofan engines, ever available for Flight Simulator. In addition to the engines, a mix of cockpit sounds has been included in the Citation CJ4X, to provide a more comfortable feeling of being in the real-life aircraft. Citation CJ4X User Manual 18 Version 1.0 Build 1709 (September 2017) Listen to the sound of the aural warnings, guard clicks, button clicks, and a virtual copilot guiding you with v-speeds at takeoff, plus all the GPWS callouts each time you are approaching and preparing for landing. Every essential sound is covered here. Flight Dynamics Invisible to the eye, but you can feel it when using your joystick or yoke. Based on real-life specifications, the Flight Dynamics will always bring you a really great flight experience. Citation CJ4X User Manual 19 Version 1.0 Build 1709 (September 2017) Airplane Flight Manual General The purpose of this manual is to bring you (the end-user) a document which serves as an aid to become familiar with this product. This section of the User Manual provide general information about the aircraft and the flight deck components to allow you interact with the aircraft and its systems. Each relevant panel is described in detail and a general description of the systems is also provided. Areas to Cover: Aircraft  Operating Limitations & Specifications  Dimensions  Flight Controls  Doors  Exterior Lights  Ground Service Main Instrument Panel  Audio Panel  Electrical Panel  Primary Flight Display (PFD)  Multi-Function Display (MFD)  Standby Primary Flight Display  Landing Gear Lever  Autopilot Panel (APP) / Flight Guidance Panel (FGP)  Display Control Panel (DCP) Tilt Panel  Cursor Control Panel (CCP) Lighting Panel Throttle Quadrant Panel Trim Panel Flight Management System (EasyFMC) Radio Stack Ramp Manager Citation CJ4X User Manual 20 Version 1.0 Build 1709 (September 2017) Aircraft Operating Limitations & Specifications Design Weights & Capacities Maximum Ramp Weight (MRW) 17,230 lb. (7,815 kg) Maximum Takeoff Weight (MTOW) 17,110 lb. (7,761 kg) Maximum Landing Weight (MLW) 15,660 lb. (7,103 kg) Maximum Zero Fuel Weight (MZFW) 12,500 lb. (5,670 kg) Standard Empty Weight (including unusable fuel, full oil, standard interior and standard avionics) 9,920 lb. (4,500 kg) Full Fuel Payload 1,000 lb. (454 kg) Maximum Payload 2,180 lb. (989 kg) Usable Fuel Capacity Jet A1 @ 6.70 lb. /gal. 5,828 lb. (2,644 kg) Max Baggage Weight @ Nose Compartment 400 lb. (182 kg) Max Baggage Weight @ Tailcone Compartment 600 lb. (272 kg) Max Baggage Load Distribution (Nose) 35 lb. /ft2 (171 kg/m2) Max Baggage Load Distribution (Tailcone) 150 lb. /ft2 (733 kg/m2) Performance Takeoff Field Length MTOW, Sea Level, ISA +0°C and Flaps 15° 3,190 ft. (972 m) Climb Performance @ MTOW 30 min from SL to 45,000 ft. (13,716 m) Climb Rate: 1,500 ft. /min (457 m/min) Maximum Altitude (Service Ceiling) 45,000 ft. (13,716 m) Maximum Cruise Speed Gross Weight 14,000 lb. and 31,000 ft. (9,449 m) 451 KTAS (836 km/hr. or 519 mph) Range MTOW, 100NM fuel reserves 1,920 NM (3,556 km or 2,209 mi) Landing Distance MLW, Sea Level, ISA +0°C, No Wind, Flaps 30° 2,740 ft. (835 m) Speeds VMO from 8,000 ft. (2,438 m) to 27,900 ft. (8,504 m) 305 KIAS (565 km/hr. or 351 mph) MMO @ 27,900 ft. (8,504 m) and above Mach 0.77 (Indicated) Flap Extension Speeds VFE at Flaps 0° to 15° Extension 200 KIAS (370 km/hr. or 230 mph) VFE at Flaps 15° to 35° Extension 160 KIAS (296 km/hr. or 184 mph) Landing Gear Operating & Extended Speeds VLO (extending) 200 KIAS (463 km/hr. or 288 mph) VLO (retracting) 200 KIAS (463 km/hr. or 288 mph) VLE 200 KIAS (463 km/hr. or 288 mph) Citation CJ4X User Manual 21 Version 1.0 Build 1709 (September 2017) Engine Specifications (Williams International FJ44-4A) Overall Length 68.6 in. (1.74 m) Overall Height 32.3 in. (0.82 m) Fan Diameter 25.3 in. (0.64 m) Inlet Area 502.7 in2 (0.32 m2) Overall Engine Weight (dry) 670 lb. (304 kg) Maximum Thrust @ SL 3,621 lbf. (16,107 N) Thrust Specific Fuel Consumption (TSFC) 0.460 lb. / (hr. lbf.) Bypass Ratio 4.1 Dimensions Overall Height 15 ft. 5 in. (4.69 m) Overall Length 53 ft. 4 in. (16.26 m) Overall Width 50 ft. 10 in. (15.49 m) Wing Wingtip (not including tip lights) 50 ft. 5 in. (15.37 m) Wing Area 330.0 ft2 (30.66 m2) Wing sweepback @ 25% chord 12.5 deg. Horizontal Stabilizer Overall H-Tail Span 22 ft. 1 in. (6.73 m) H-Tail Area 79.6 ft2 (7.40 m2) H-Tail Sweepback @ 25% chord 20 deg. Vertical Stabilizer V-Stab Height 7 ft. 5 in. (2.26 m) V-Stab Area 59.3 ft2 (5.51 m2) V-Stab Sweepback @ 25% chord 49 deg. Cabin Interior Height (maximum over aisle) 57 in. (1.45 m) Width (trim to trim) 58 in. (1.47 m) Length (from FWD Pressure Bulkhead to AFT Pressure Bulkhead) 22 ft. 4 in. (6.81 m) Landing Gear Landing Gear Tread (main to main) 12 ft. 4 in. (3.76 m) Landing Gear Wheelbase (nose to main) 21 ft. 2 in. (6.45 m) Citation CJ4X User Manual 22 Version 1.0 Build 1709 (September 2017) CJ4 - Top View Citation CJ4X User Manual 23 Version 1.0 Build 1709 (September 2017) CJ4 – Front View CJ4 – Side View Citation CJ4X User Manual 24 Version 1.0 Build 1709 (September 2017) Flight Controls CJ4 – Flight Control Surfaces (1) Elevators (red) Elevators control the aircraft’s pitch along its lateral axis. Pitch is the Nose-Up and Nose- Down movement of the aircraft, also known as Attitude. The greater fins move for short-term attitude changes, while long-term pitch changes are controlled by the trim tabs. There is one elevator with trim fin on each horizontal stabilizer. The elevators move UP and DOWN in order to make the aircraft climb or descend. For instance, when you push the control column forward, the elevators move down making the aircraft’s nose pitch downward. Instead, if you pull the control column backward, the elevators will move up, thus making the nose pitch upward. Elevators are controlled either manually by the pilot or automatically by the Autopilot and they are cable-operated. Pitch can be monitored through the Attitude Indicator. (2) Ailerons (green) Ailerons control the aircraft’s roll along its longitudinal axis. There is one aileron with trim tab on each wing. Ailerons move on opposite directions to each other in order to make the aircraft turn. Citation CJ4X User Manual 25 Version 1.0 Build 1709 (September 2017) For instance, when you turn the control wheel to the left, the left aileron raises to ‘dip’ the left wing, while the right aileron ‘raises’ the right wing. Elevators are controlled either manually by the pilot or automatically by the Autopilot and they are cable-operated. Roll can be monitored through the Attitude Indicator. (3) Rudder (blue) A single cable-operated rudder controls the aircraft yaw along its directional/vertical axis. Yaw is the side-to-side movement of the aircraft. The rudder is located at the vertical stabilizer. It counts with a trim tab, and is controlled via the pedals. For instance, when you push the left pedal forward, the rudder moves to the left, causing the aircraft nose turn to the left. Be aware that rudder movements may induce rolls, so if the rudder is fully deployed to the left, the aircraft will turn to the left in the same way as described in the previous example. This is because the right wing speeds up a bit, so that increases lift on that wing. Rudder is controlled either manually by the pilot or automatically by the Autopilot and Yaw Damper. (4) Trailing-Edge Flaps / Wing Flaps (purple) Flaps modify the aerodynamic configuration of the airplane, in order to improve performance during specific flight conditions. With them, takeoff and landing characteristics are improved and greater maneuverability is provided to meet climb and descent requirements. The flap system consists of a flap control surface mounted on each wing that extend from the trailing edge of the latter. Both Trailing-Edge flaps are hydraulically actuated by the main hydraulic system and are electrically controlled. Normal flap travel is from 0 to 35 degrees, with an intermediate detent at 15 degrees, installed for take-off and approach configurations. (5) Speed Brakes (orange) The speed brakes are installed on the upper and lower surfaces of each wing for rapid rates of descent, rapid deceleration, and to spoil lift during landing roll, together with the ground spoilers. They are electrically controlled and hydraulically actuated. (6) Ground Spoilers (yellow) The ground spoilers are installed on the upper surface of each wing and used in conjunction with the speed brakes for lift dumping after landing, they cannot be used while the aircraft is airborne, even if the speed brake lever is at full deployment position. They are hydraulically actuated and electrically controlled. Citation CJ4X User Manual 26 Version 1.0 Build 1709 (September 2017) Doors Doors can be controlled via Standard FS Key Combinations or via the Ramp Manager. This aircraft counts with a main entry door on the left side and an emergency exit on the right side (not simulated here), plus two baggage compartments (one in the nose of the aircraft, and the other one in the tailcone). Both nose baggage doors open simultaneously when called from the simulator. CJ4 - Doors (1) Main Exit SHIFT + E (2) Rear (Tailcone) Baggage SHIFT + E + 2 (3) Nose Baggage SHIFT + E + 3 Citation CJ4X User Manual 27 Version 1.0 Build 1709 (September 2017) Exterior Lights This aircraft counts with the following external lights emulated: CJ4 – Exterior Lights Location Taxi & Landing Lights Two brighter lights located in the belly, near the leading edge of both wings. They serve as lights for taxiing and runway approaching. Navigation Lights Two lights (one on each wing). Standard red light on the left wingtip and green light on the right wingtip. Strobe Lights Two anti-collision and white flashing lights (one on each wing). Wing Inspection Light A white light located in the fuselage, illuminating the leading edge of the left wing. Logo Lights Two lights (one on each horizontal stabilizer) to illuminate the logo in the vertical stabilizer surface. Beacon Light A flashing red light located on the vertical stabilizer tip. Cockpit Lighting Cockpit lighting is provided as well to illuminate both flight deck and cabin. Citation CJ4X User Manual 28 Version 1.0 Build 1709 (September 2017) Ground Service Citation CJ4X counts with the following ground service elements simulated. They can be controlled via Ramp Manager. CJ4 – Ground Service (1) Pitot Covers These covers are emulated to prevent the pitot tubes from dust or any other foreign object. They have a distinctive REMOVE BEFORE FLIGHT red ribbon. When they are set, airspeed indicators and altimeters will not work unless removed. (2) Engine Cowling Used to cover the engines inlet and nozzle, and protect them from foreign objects. Remove them before starting a flight. (3) Wheel Chocks & Traffic Cones When parked on ground, use the chocks to ensure the aircraft is completely in rest and not moving. Also, traffic cones are set for warning around the aircraft. (4) Ground Power Unit Use the GPU to provide auxiliary electrical supply and charge battery, while the aircraft is in ground and you require a long waiting time before you start your flight plan. Citation CJ4X User Manual 29 Version 1.0 Build 1709 (September 2017) Main Instrument Panel Main Instrument Panel – 16:9 Widescreen Configuration (1) Audio Control Panel (ACP) (2) Electrical Panel (3) Pilot Primary Flight Display (PFD) (4) Pilot Multi-Function Display (MFD) (5) Standby PFD (6) Landing Gear Lever (self-explanatory) (7) Autopilot Panel (APP) / Flight Guidance Panel (FGP) (8) Pilot Display Control Panel (DCP) (9) Master Warning & Master Caution Lights (10) Operating Limitations Placard (11) Tail Registration Placard (12) Elevator Trim No Takeoff & Fuel Low Lights (13) Copilot Multi-Function Display (MFD) (14) Left Engine Fire Light (15) Fire Bottle Armed Light Citation CJ4X User Manual 30 Version 1.0 Build 1709 (September 2017) Audio Control Panel (ACP) The Audio Control Panel (ACP) installed at the pilot and copilot position provides control of the microphone selection and audio volume (radio, interphone, speaker, and headphone). Separate volume knobs/switches allow the pilot to select which radios to listen to. There are 7 available audio selector/volume controls: COM1, COM2, DME1, ADF1, MKR, NAV1, and NAV2. The controls are push-lock switches. In the out position, the selected source is output to the headphones and speaker. In the in position, the audio is off for the selected source. Electrical Panel This panel controls everything related with aircraft’s electrical supply sources. (1) Left Generator Switch. Only two positions (ON and OFF). By default ON. Controls whether the left engine generator is working or not. (2) Battery Switch. Only two positions (ON and OFF). This switch controls the main battery supply. When there is no GPU working, all panel circuit turns off. Otherwise, the panel circuit (instruments) remains on regardless of the battery off. (3) Right Generator Switch. Only two positions (ON and OFF). By default ON. Controls whether the right engine generator is working or not. To change position for this switch and the previous ones, use single click only. (4) Emergency Lights Switch. Three positions (ARMED, OFF and ON). Used for emergencies and/or abnormal situations. When they are not armed, a message appears in the CAS. More information about the CAS here. (5) Standby Flight Display Switch. Three positions (ON, OFF and TEST). Place the switch to ON so the standby/backup PFD remains on. When placing it to OFF position, the unit’s display is blank. When TEST position is used, the unit’s display shows zebra-kind strips, in order to verify if the unit works as expected. (6) Avionics Switch. Three positions (ON, OFF and DISPATCH). When ON, all avionics and flight instruments are online and ready for flight. When OFF, all displays except Standby PFD (when switch is in either ON or TEST position) and Pilot MFD remain on. On DISPATCH mode, only Standby PFD and MFD remain on, but avionics online. More information about the MFD display here. For this switch and the two previous switches, left-click to move them down and right-click to move them up. Apply for both 2D and 3D views. Citation CJ4X User Manual 31 Version 1.0 Build 1709 (September 2017) Primary Flight Display (PFD) Primary Flight Display Parts Citation CJ4X User Manual 32 Version 1.0 Build 1709 (September 2017) Attitude Indicator Attitude Indicator Parts Name Description Attitude Ball The attitude ball is the traditional blue sky & brown earth depiction separated by a white horizon line. A V-shaped single cue aircraft symbol is in the center of the attitude ball. Roll Scale The roll scale at the top of the attitude ball indicates the current roll attitude. A fixed triangle at the top of the scale indicates 0° of roll. The white tick marks indicate 10°, 20°, and 30° of roll. The small triangles indicate 45° of roll. The white tick marks outside of the triangles indicate 60° of roll. The roll pointer moves left or right as appropriate to indicate roll. Pitch Tape The white pitch tape is centered on the attitude ball. The white horizon line indicates 0° of pitch, and pivots in roll around the aircraft symbol. Pitch marks are in increments of 2.5° up to ±30° of pitch. When the aircraft exceeds ±30° of pitch, the scale expands to ±90° of pitch. Slip/Skid Indicator A white rectangle at the base of the roll pointer indicates slip/skid attitude. The slip/skid indicator moves with the roll pointer in turns. The slip/skid indicator moves sideways to show lateral acceleration. One-rectangle displacement equals a one-ball displacement of a traditional inclinometer (turn coordinator). Unusual Attitude Indication When pitch angle is greater than 30° nose up or 20° nose down, or roll angle exceeds 65°, red warning chevrons show on the pitch tape. Citation CJ4X User Manual 33 Version 1.0 Build 1709 (September 2017) Flight Director Command Bars The FD command bars show on the attitude ball as a magenta inverted V- shaped indicator. The command bars present pitch and roll guidance information from the FGS / Autopilot when the FD is active. The command bars are normally centered on the aircraft symbol (zero input). The command bars move up and down to command a climb or descent, and rotate right and left to command a right or left bank. Marker Beacon Annunciation The marker beacon annunciation shows on the left side of the attitude ball. • The outer marker annunciation is a cyan, boxed “OM” that appears when the aircraft is passing over an outer marker beacon. • The middle marker annunciation is a yellow, boxed “MM” that appears when the aircraft is passing over a middle marker beacon. • The inner marker annunciation is a white, boxed “IM” that appears when the aircraft is passing over an inner marker beacon. ILS Vertical Deviation Display The ILS vertical deviation display consists of a scale and pointer that shows between the attitude ball and the altitude display as a “cutout” section. The ILS vertical deviation display shows when LOC is the active course to indicate deviation from the glideslope (G/S). • The deviation scale consists of two gray dots above and below a center tick mark. • The deviation scale shows when LOC is the active NAV source. • The scale goes out of view when B/C localizer logic is active. • The deviation pointer is a diamond shape and is the same color as the LOC source. • Each of the inner dots represents approximately a ¼-degree displacement. The outer dots represent approximately a ½-degree displacement. • The pointer indicates the position of the glideslope relative to the aircraft. The glideslope is below the aircraft when the pointer is above the center mark, and above the aircraft when the pointer is below the center mark. Citation CJ4X User Manual 34 Version 1.0 Build 1709 (September 2017) Flight Guidance System Annunciator FGS Annunciator Parts Name Description Lateral Mode Field (Left) The lateral mode field is split into the active mode field and the armed mode field. The active mode is the upper field and the armed mode is the lower field. • The lateral mode field shows the mode currently selected for the FGS. • Once the lateral mode is captured, the navigation sensor (LNV, VOR or LOC) shows in green in the active mode field, and the ROLL or HDG annunciation is removed. The FGS lateral mode annunciations and the function are as follows: ROLL Heading Hold/Roll Hold HDG Heading Select LNV1 FMS Navigation Arm/Capture/Track VOR1 VOR Navigation Arm/Capture/Track LOC1 LOC Navigation Arm/Capture/Track APPR ILS Approach Arm APPR LNV1 FMS Approach Arm/Capture/Track APPR VOR1 VOR Approach Arm/Capture/Track APPR LOC1 LOC Approach Arm/Capture/Track APPR B/C Back-course Approach Arm/Capture/Track GA Go Around, Heading Hold TO Takeoff/Go Around (TOGA), Heading Hold Citation CJ4X User Manual 35 Version 1.0 Build 1709 (September 2017) AP/YD Field (Middle) The autopilot/yaw damper field is split into the AP/YD engaged window and the AP transfer window. The AP/YD engaged window is the upper window, and the AP transfer window is the lower window. • AP shows in green in the AP/YD engaged window when the autopilot is engaged. If the autopilot is disconnected either by the pilot or automatically, AP is removed. • YD shows in green in the AP/YD engaged window when only the yaw damper is engaged. If the yaw damper is disconnected, YD is removed. The yaw damper may be engaged independently of the autopilot. If the autopilot is subsequently engaged, the yaw damper remains engaged, and the AP annunciation replaces the YD annunciation. • The transfer arrow shows in the AP transfer window to indicate which FGC is driving the control servos when the autopilot is engaged (or would be driving the servos upon autopilot engagement). • A closed arrowhead points to the side that is providing navigation inputs to the FGS. • The arrow is green when the autopilot is engaged and white when the autopilot is not engaged but the FD is active. Vertical Mode Field (Right) The vertical mode field is split into two fields, an upper active mode field and a lower armed mode field. Armed modes show in white on the lower field, and active modes show in green on the upper mode field. The FGS vertical mode annunciations and the associated function are as follows: PTCH Pitch Hold ALT CAP Altitude Hold Acquisition ALT Altitude Hold Track ALTS Pre-Selected Altitude Hold Arm VS NNNN↑ Selected VS acquisition/track. NNNN in the VS mode annunciation indicates the selected VS value, and the arrow indicates whether the nose pitches upward or downwards. GS Vertical approach capture GA Pitch Attitude Hold to 7 degrees TO Pitch Attitude Hold to 10 degrees Citation CJ4X User Manual 36 Version 1.0 Build 1709 (September 2017) Altimeter/Altitude Display The altitude display consists of a moving altitude tape with a fixed position pointer on the PFD. The equivalent metric value of Barometric Altitude can show in addition to the display in feet. Metric Preselect Altitude is also available for display. Barometric Pressure Setting and RA/BARO MIN Readout also show on the PFD. Altitude Display Parts Name Description Barometric Pressure Setting Barometric (BARO) pressure setting shows under the altitude display on the PFD. The BARO knob on the DCP controls the setting. The units of measurement can be set in inches of mercury (INHG) or HectoPascals (hPa) via the CONFIG menu. The PUSH STD knob on the DCP sets the standard BARO setting to 29.92. More information about Display Control Panel here. More information about CONFIG menu here. Radio Altitude Display The radio altitude display consists of an analog scale and a digital readout. The digital readout shows when the aircraft is within 2500 feet of the ground, and shows on the lower part of the attitude ball. The readout is normally green. • The analog scale is brown and replaces a portion of the dark blue background of the altitude scale. The scale comes into view when radio altitude is approximately 225 feet. • The analog scale moves up as the aircraft approaches ground level. It meets the 0 FT mark when the radio altitude is 0 feet AGL. Citation CJ4X User Manual 37 Version 1.0 Build 1709 (September 2017) Pre-Select Altitude Display The Pre-Select Altitude (PSA) display consists of a digital readout above the altitude tape and a reference bug on the tape. The ALT knob sets the Pre-Select Altitude. • The normal increments for PSA are 100 feet. • If BARO MIN bug is enabled, PSA can be set to the same value as the BARO MIN altitude. • The range for PSA is 0 to 55,000 feet, or 0 to 16,765 meters. • The PSA readout is normally cyan. • The PSA bug shows on the altitude tape as a sideways cyan “M” centered at the PSA altitude. • At system power up, the PSA readout is off. Cyan dashes shows in the PSA field and the reference bug does not show on the altitude tape. The first turn of the ALT knob brings the PSA readout into view. Slip/Skid Indicator A white rectangle at the base of the roll pointer indicates slip/skid attitude. The slip/skid indicator moves with the roll pointer in turns. The slip/skid indicator moves sideways to show lateral acceleration. One-rectangle displacement equals a one-ball displacement of a traditional inclinometer (turn coordinator). Citation CJ4X User Manual 38 Version 1.0 Build 1709 (September 2017) Vertical Speed Display Vertical Speed Display Parts Name Description Vertical Speed (VS) Display The vertical speed (VS) display consists of a vertical analog scale and pointer with a green “drag line.” The pointer moves up and down on the scale to indicate current vertical speed. As the pointer moves, the drag line appears to emphasize the vertical speed. • Range of the scale is ±4000 feet per minute (fpm). • Range of the VS pointer is ±4300 fpm. Vertical Speed Readout A digital readout of the current VS appears at the top or bottom of the VS scale. The VS readout is always rounded to the nearest 100 feet. • The readout shows at the top of the scale when the climb rate is greater than or equal to 300 fpm. • The readout shows at the bottom of the scale when the descent rate is greater than or equal to 300 fpm. • Range of the digital VS readout is 0 to ±15,000 fpm. Selected VS Display The selected VS display shows on the VS scale as a reference bug and as a digital display on the FGS field above the attitude display. • The selected VS bug and display only show when the autopilot VS or ALT mode is active. • The Pitch wheel on the APP sets the selected VS. • The reference bug shows as a cyan arrow. • Clearing the autopilot VS or ALT mode or selecting another vertical mode removes the reference bug and readout from display. Citation CJ4X User Manual 39 Version 1.0 Build 1709 (September 2017) Airspeed Display Airspeed Display Parts Name Description Airspeed Display The airspeed display consists of a vertical airspeed tape, fixed position pointer, and the current airspeed readout inside the pointer. • An analog moving scale is centered on the airspeed tape with 80 knots of the scale in view at all times. Short tick marks show at intervals of 5 knots, and longer tick marks show every 10 knots. Numbers show every 20 knots. • Range for the airspeed scale is 40 to 400 knots. • The current airspeed shows in a digital readout inside the fixed pointer. • Range for the airspeed readout is 40 to 999 knots. Airspeeds below 40 knots show as two green dashes. Airspeed Trend Vector The airspeed trend vector is a vertical, variable-length magenta line that shows to the right of the airspeed scale. The airspeed trend vector approximates what the airspeed will be in 10 seconds at the present rate of acceleration or deceleration. • The airspeed trend vector originates from a gray tick mark directly opposite the airspeed pointer. • The end of the airspeed trend vector is a horizontal line that points at the airspeed scale. • The length of the airspeed trend vector is limited to the span of 40 knots on the airspeed scale. • The airspeed trend vector extends up for acceleration, and down for deceleration. • The airspeed trend vector shows when the aircraft is airborne. Citation CJ4X User Manual 40 Version 1.0 Build 1709 (September 2017) • The airspeed trend vector does not show on the ground, and is removed if any of the data inputs to calculate the airspeed trend are missing. Impending Stall Speed Cue The impending stall speed (ISS) cue shows at the bottom right of the airspeed tape to warn the pilot when the aircraft approaches to stall. • The stall speed cue is a thick red vertical line that extends from the design stall speed (VS0 and VS1, depending on aircraft configuration) to the bottom of the airspeed tape. • ISS is variable and is equal to 1.1VS. • The ISS cue does not show on the ground. The ISS cue is removed if the IAS failure flag shows. More information about display flags here. Overspeed Cue The overspeed cue shows to warn the pilot that the airspeed is approaching or exceeding the airspeed limit for the airframe. • The overspeed cue is a thick red vertical line that shows at the top right of the airspeed tape. • The bottom of the overspeed cue is positioned at VMO speed, until MMO speed becomes more restrictive. The bottom of the overspeed cue then shifts to MMO speed (shown in knots). V-Speed Reference Bugs V-speed reference bugs show on the airspeed tape as a visual cue of the takeoff and approach speeds. V-speeds are set through the REFS menu. Each V-speed must be selected (turned on) for the reference bug to show on the airspeed tape. Each reference bug shows as a cyan horizontal line with a cyan label on the airspeed tape at the appropriate speed. Labels for the bugs are as follows: - 1 V1 – Takeoff decision speed - R VR – Rotation speed - 2 V2 – Takeoff safety speed - RF VREF – Reference Airspeed at 50 ft. runway threshold - AP VAPP – Approach climb speed (1.3VS1) with 15° flaps and gear up - T VT – General-purpose target speed • V1, VR, and V2 speed references are automatically removed from the airspeed tape when the aircraft is airborne and the airspeed reaches 200 knots. • VREF and VAPP are automatically removed from the airspeed tape any time the IAS is less than 50 knots. Selected Speed Bug The selected speed bug shows on the airspeed tape, and as an icon and digital readout above the airspeed tape. The bug, icon, and readout are all cyan. Citation CJ4X User Manual 41 Version 1.0 Build 1709 (September 2017) • The selected speed bug and icon only show when the autopilot FLC mode is active. • The speed bug initially shows at the current airspeed or Mach. The setting may be changed by moving the APP speed knob. • The selected speed bug setting may be referenced to IAS or Mach. When the speed bug is first in view IAS or Mach is the reference. Selecting FLC button on the APP toggles the reference from IAS to Mach or Mach to IAS. • The PFD automatically changes the speed reference from IAS to Mach when the aircraft is climbing through 31,000 feet or above, and changes from Mach to IAS when the aircraft is descending through 31,000 feet or below. • The selected speed bug and digital readout are removed from the display if selected speed data is missing. Speed Reference Table The speed reference table on the bottom half of the airspeed tape shows the digital readouts of the selected V-speed references. • The speed reference table overwrites the airspeed scale when the aircraft is on the ground and the airspeed is less than 40 knots. The speed reference table rolls out of view as the airspeed increases above 40 knots. • V-speed values show in magenta on the speed reference table. Mach Display The Mach display is a green digital readout preceded by a decimal point and a gray “M” that shows below the airspeed tape. • Range of the Mach display is .400 to .998. • The Mach display comes on when Mach is ≥.400. The Mach display does not show when Mach is less than .400. • When Mach data is missing or invalid, the decimal point turns red and the readout is replaced by three red dashes. Citation CJ4X User Manual 42 Version 1.0 Build 1709 (September 2017) Angle-of-Attack Indicator (AoA) The angle-of-attack indicator offers a visual indication of the amount of lift the wing is generating at a given airspeed or angle of bank. The AOA delivers critical information visually to indicate the actual safety margin above an aerodynamic stall. It is accompanied by an indexer that functions only when the landing gear is down and the aircraft is airborne. More information about the indexer here. Angle-of-Attack Indicator Parts Name Description AoA Display The angle-of-attack indicator consists of vertical tape with a moving pointer and a digital readout preceded by a decimal point. • Range of the AoA scale is 0.2 to 1.0. • Range for the AoA readout is .00 to 1.00 (absolute). • When AoA data is invalid or missing, the vertical tape, pointer and readout are replaced by an AOA flag. Citation CJ4X User Manual 43 Version 1.0 Build 1709 (September 2017) Multi-Function Display (MFD) Multi-Function Display Parts Citation CJ4X User Manual 44 Version 1.0 Build 1709 (September 2017) Engine Indicating System (EIS) Engine Panel – Normal View Engine Panel – Compressed View Citation CJ4X User Manual 45 Version 1.0 Build 1709 (September 2017) EIS Parts Name Description N1 % N1 Display The N1 display shows the turbine engine fan RPM (expressed as a percentage). The display consists of a vertical analog scale, moving pointer, and digital readout for each engine. • Range for the N1 analog scale and pointer is 20 to 110%. Range for the digital readout is 0 to 120% • The redline marker shows on the N1 scale at the redline limit. • The N1 pointer moves up and down the side of the N1 scale to indicate the N1 percentage. The pointer is white when N1 is in the normal range. • The N1 digital readout shows below the N1 scale and pointer. The N1 readout is green when N1 is in the normal range. • The pointer and readout turn yellow when N1 enters the transient limit region. • The pointer and readout turn red when N1 enters the redline limit region. • Four yellow dashes replace the N1 readout, and the pointer is removed when N1 data from all sources is missing or invalid. ITT ITT Display (Engine Running) The ITT (interstage turbine temperature) display consists of a vertical analog scale and moving pointer for each engine. • Range for the ITT analog scale is 100 to 1050 °C. • The yellow caution band shows on the ITT scale at the transient limit range. • The redline marker shows on the ITT scale at the redline limit. • The ITT pointer moves up and down the side of the ITT scale to indicate the ITT. The pointer is white when ITT is in the normal range. • The pointer turns yellow when ITT enters the transient limit region. • The pointer turns red when ITT enters the redline limit region. • The ITT pointer is removed when ITT data from all sources is missing or invalid. Also, a FAIL flag is accompanied. ITT ITT Display (Engine Start) During engine start, the ITT display shows a start limit mark on the ITT scale. The start limit mark is a red triangle. ITT normal and transient limits do not apply while the ITT start limit mark is in view. IGN Ignition Annunciation The vertical green IGN legend appears on the left or right side of the ITT scale to indicate the left or right engine ignition switch is in the ON position. N2 % N2 Display The N2 display is a digital readout of the engine turbine RPM measured against a fixed 100% value. • Range for the N2 readout is 0 to 120%. • The N2 readout is green when N2 is within the normal limit. • The N2 readout is yellow when N2 is within the caution limit. • The N2 readout is red when N2 reaches the redline limit. Citation CJ4X User Manual 46 Version 1.0 Build 1709 (September 2017) • Four yellow dashes replace the N2 readout when N2 data from all sources is missing or invalid. OIL PSI Oil Pressure Display (Normal View) The oil pressure display consists of an analog scale and moving pointer, and a digital readout of the oil pressure for each engine. The analog scale shows only when the EIS panel is in normal view. • The oil pressure scale is a wide line with linear scaling from 0 to 125 PSI. The line is divided into color sections to indicate the normal, transient (caution), and redline ranges. • The pointer is a solid triangle that moves up and down the scale to indicate the oil pressure range. Each engine has its own pointer, and the two pointers move independently. The pointer color indicates the oil pressure is within the normal, caution, or redline range. • The pointer turns yellow when oil pressure enters the caution limit. • The color of the digital readout and the pointer are the same. • Range of the digital readout is 0 to 150 PSI. • The oil pressure pointer is removed and four yellow dashes replace the readout when oil pressure data is missing or invalid. OIL °C Oil Temperature Display (Normal View) The oil temperature display consists of an analog scale and moving pointer, and a digital readout of the oil temperature for each engine. The analog scale shows only in the normal EIS format. • The oil temperature scale is a wide line with linear scaling from 0 to 160 °C. The line is divided into color sections to indicate the normal, transient (caution), and redline ranges. • The pointer is a solid triangle that moves up and down the scale to indicate the oil temperature range. Each engine has its own pointer, and the two pointers move independently. The pointer is green when oil temperature is within the normal range. • The pointer turns yellow when oil temperature enters the transient limit region. • The pointer turns red when oil temperature enters the redline limit region. • The color of the digital readout and the pointer are the same. A minus sign (-) shows for any negative values. • Range of the digital readout is -50 to 140 °C. • The oil temperature pointer is removed and four yellow dashes replace the readout when oil temperature data is missing or invalid. FUEL PPH Fuel Flow Display The fuel flow display consists of a green digital readout of the fuel flow for each engine. • Fuel flow is measured in pounds per hour (PPH). • Range of the readout is 0 to 2000 PPH. • Four yellow dashes replace the readout when fuel flow data is missing or invalid. Citation CJ4X User Manual 47 Version 1.0 Build 1709 (September 2017) FUEL °C Fuel Temperature Display The fuel temperature display consists of a digital readout of the temperature of the fuel in each wing tank. Each wing tank has its own readout. • Range of the readout is -64 to 64 °C. A minus sign (-) shows for negative values. • The readout is green when fuel temperature is within normal limits. If the temperature goes outside the normal limits, the readout turns yellow. • Two yellow dashes replace the readout when fuel temperature data is missing or invalid. FUEL LBS Fuel Quantity Display The fuel quantity display shows the amount of fuel in each wing tank. The display consists of a digital readout for each tank. • Fuel quantity is measured in pounds (LBS). • Range for the fuel quantity readout is 0 to 2600 lbs. • The fuel quantity digital readout shows in green when fuel quantity is greater than or equal to 250 lbs. • The fuel quantity digital readout turns yellow when fuel quantity is greater than zero and less than 250 lbs. • The fuel quantity digital readout turns red when fuel quantity is zero. • Four yellow dashes replace the fuel quantity readout when fuel quantity data is missing or invalid. TRIM AIL/RUD Aileron Trim & Rudder Trim Display The aileron & rudder trim display shows the percentage of trim tab deflection for both aileron and rudder. The display consists of an analog scale and moving pointer. • The trim scale is a wide line with linear scaling from -100% to 100% of deflection. For aileron, -100% represents 19 degrees down to the left and 100% represents 19 degrees down to the right. For rudder, -100% represents 20 degrees fully to the left and 100% represents 20 degrees fully to the right. • The pointer is a solid triangle that moves left and right the scale to indicate the trim tab deflection. The pointers move independently. The aileron trim is the upper pointer, and the rudder trim is the lower pointer. • The pointers are white when both trim tabs are within the normal limits. • Range of normal limits is -30% to 30%. For aileron, ±5.7 degrees. For rudder, ±6 degrees. • The pointers turn yellow when either of them go outside the normal limits. TRIM ELEV Elevator Trim Display The elevator trim display shows the percentage of trim tab deflection for elevator. The display consists of an analog scale and moving pointer. • The trim scale is a wide line with scaling from -100% to 100% of deflection. For elevator, -100% represents 14 degrees nose down and 100% represents 14 degrees nose up. • The pointer is a solid triangle that moves left and right the scale to indicate the trim tab deflection. • The pointer is white when trim tab is within the normal limit. • Range of normal limit is 0° to 5°. Citation CJ4X User Manual 48 Version 1.0 Build 1709 (September 2017) • The pointer turns yellow when trim tab goes outside the normal limits. FLAPS Wing Flaps Display The wing flaps display shows the angle of flap deflection for elevator. The display consists of an analog scale and moving pointer. • The scale is split in three for the detents 0°, 15° and 30°. • The pointer is a solid airfoil that moves clockwise and counterclockwise to indicate the current flaps detent. Citation CJ4X User Manual 49 Version 1.0 Build 1709 (September 2017) Caution Advisory System (CAS) CAS Annunciations Message In Display Description Warning Messages ENG FIRE L ENG FIRE R ENG FIRE L-R Either the left or right engine is in fire. Discharge the fire bottle(s) of the affected engine(s). CABIN ALTITUDE The aircraft exceeded 14,000 ft. of cabin altitude or 9.0 psi of differential pressure. Descend as soon as possible in order to depressurize the airplane and extinguish the annunciation. Caution Messages CABIN DOOR The main exit is open or its lock is on open position. Close the door to extinguish this message. AFT BAGGAGE DOOR The tailcone baggage door is open or its lock is on open position. Close the door to extinguish this message. NOSE DOOR L-R The nose baggage door is open or its lock is on open position. Close the door to extinguish this message. FUEL LEVEL LOW L FUEL LEVEL LOW R FUEL LEVEL LOW L-R Either the left or right fuel tank has less than 250 lbs. of usable fuel. On ground, refuel the aircraft before the next flight. While airborne, be sure you have enough fuel for safe arrival to destination, otherwise, descent and land as soon as possible. FUEL IMBALANCE This message appears if the difference of each fuel tank quantity (i.e., left fuel tank quantity minus right tank quantity) is greater than Citation CJ4X User Manual 50 Version 1.0 Build 1709 (September 2017) or equal to 200 lbs. In order to extinguish it, use the FUEL XFER knob to transfer fuel from one tank to another. More information here. ANTISKID FAIL If landing gear anti-skid has any malfunction, this message will appear. BRAKE PRESSURE LOW This message appears when the brake pressure is lower than 28.8 kpsf. (Kilo-pounds per square feet). When engines are running, this message will extinguish as gear braking system is hydraulically- actuated. L GEN FAIL R GEN FAIL L-R GEN FAIL When either of the engine generators are off, this message will appear. Unless a failure is induced in-sim, turn the affected generator(s) on and the message will extinguish. EMER LIGHTS NOT ARMED Emergency lights are not in ARMED position. Move the EMER LIGHTS switch to ARMED position in order to extinguish this message. ICE DETECTED When the aircraft detects ice in the airframe (wings, engine or tail), it is required to use the Anti-Ice System. More information here. Informative Messages PITOT STATIC COLD L-R- STBY Appears when pitot heat is off. Turn it on, so the pitot tubes remain working during the entire flight. NO TAKEOFF This message appears when any of the following conditions are met: • Aileron and/or Rudder Trim tabs are not within their normal limit. • Elevator Trim tab is not properly set to the green normal limit. • Flaps asymmetry is detected. • When flaps are not set at 15° (normal take-off detent). • When speed brakes and/or ground spoilers are deployed. Verify all the conditions above and fix them before starting takeoff roll. GROUND SPOILERS EXTENDED Ground spoilers are deployed. To extinguish this message, stow them. GROUND SPOILERS ARMED Ground spoilers are armed and ready to deploy once the aircraft touches down. This message appears when the speed brakes are armed on approach. SPEED BRAKES EXTENDED Speed brakes are extended. To extinguish this message, retract them. Citation CJ4X User Manual 51 Version 1.0 Build 1709 (September 2017) SPEED BRAKES ARMED Speed brakes are armed and ready to deploy after the aircraft touches down. When pressed the spoiler arm command on FS, this message appears. FUEL BOOST ON L FUEL BOOST ON R FUEL BOOST ON L-R Fuel pumps of either left or right engine are on. Turn them off to extinguish this message. More information here. PARKING BRAKE Parking brake is set. Citation CJ4X User Manual 52 Version 1.0 Build 1709 (September 2017) Upper Information Panel Upper Information Panel – Systems View Upper Information Panel – FMS Text View Citation CJ4X User Manual 53 Version 1.0 Build 1709 (September 2017) Upper Information Panel Parts Name Description FMS Text View FMS TEXT INCOMPATIBLE Annunciation This annunciation shows when there is no flight plan open either by the FMC or the FS flight planner. FMS Flight Plan Display The FMS flight plan display shows when there is an active flight plan. The display consists of a table of four rows and five columns. • The rows display information about the flight plan waypoints. The first row show information for the previous waypoint, the second row is for the current waypoint enroute, the third row is the next waypoint and the last row brings information about flight plan destination. • The colums are (from left to right): Waypoint ident, distance to waypoint (for destination, this column shows the total trip distance), estimated time enroute (ETE), estimated time of arrival (ETA) and gross weight and remaining fuel estimations. The latter is not simulated yet due to bugs with FS GPS module, it will be revised in a future update. • The color of previous waypoint information is cyan. The color for current enroute waypoint is magenta. The last two rows of waypoint information are white. • The ETE and ETA displays format is two digits, a colon, followed by two digits. Both values are measured to the nearest minute. • Range for distance is 0 to 4,096 nautical miles (NM). When distance is less than 100 nautical miles, the distance is shown in decimal format, in range of 0.0 to 99.9 NM. • Five dashes replace the ident column when any of the data for the respective row is missing or invalid. • Four dashes replace the distance column when any of the data for the respective row is missing or invalid. • Four dashes replace the ETE and ETA columns when any of the data for the respective row is missing or invalid. • Three dashes and zero pound indication replace the fuel and GW estimations column when any of the data for calculation is missing or invalid. Systems View DC ELEC DC Generator Display The DC generator display consists of two digital readouts for each engine generator. One readout (upper) is for current (measured in amperes) and the other (lower) is for voltage. BATT Battery Display The battery display consists of three digital readouts for battery parameters. The readouts are for the following parameters (going up to down): current, voltage and temperature. OXY PSI The oxygen supply display consists of an analog scale and moving pointer of the oxygen supply pressure. Citation CJ4X User Manual 54 Version 1.0 Build 1709 (September 2017) Oxygen Supply Display • The oxygen pressure scale is a wide line with linear scaling from 0 to 2400 PSI. The line is divided into color sections to indicate the normal and caution ranges. • The pointer is a solid triangle that moves up and down the scale to indicate the pressure range. The pointer color indicates the oxygen pressure is within the normal or caution range. • The pointer turns yellow when oxygen pressure enters the caution limit. HYD Hydraulics Display The hydraulics display is a digital readout of the engine hydraulic system pressure. • The HYD PSI readout is green when engine hydraulic pressure is within the normal limits (greater than 2,200 PSI and less than 3,400 PSI). • The HYD PSI readout is yellow when engine hydraulic pressure is outside the normal limit. FUEL PPH Fuel Flow Display The fuel flow display consists of a green digital readout of the fuel flow for each engine. • Fuel flow is measured in pounds per hour (PPH). • Range of the readout is 0 to 2000 PPH. • Four yellow dashes replace the readout when fuel flow data is missing or invalid. FUEL °C Fuel Temperature Display The fuel temperature display consists of a digital readout of the temperature of the fuel in each wing tank. Each wing tank has its own readout. • Range of the readout is -64 to 64 °C. A minus sign (-) shows for negative values. • The readout is green when fuel temperature is within normal limits. If the temperature goes outside the normal limits, the readout turns yellow. • Two yellow dashes replace the readout when fuel temperature data is missing or invalid. Citation CJ4X User Manual 55 Version 1.0 Build 1709 (September 2017) Navigation Display (Apply for both MFD and PFD) Partial Arc Formats Full Compass Rose Format Citation CJ4X User Manual 56 Version 1.0 Build 1709 (September 2017) The navigation displays on the PFD and the MFD are identical with a few exceptions that are noted in the individual display descriptions that follow. Control for the displays is through the DCP for PFD and CCP for MFD. Common display formats, such as the compass rose and the partial compass arc, as well as display overlays compatible with the selected display format, operate in the same manner for both the PFD and MFD. Navigation Display Parts Name Description Compass Rose/Arc The display shows a full compass rose or compass arc for the heading display. • The compass rose is a full 360° compass card. The card rotates around the center aircraft symbol, and current heading shows under the lubber line index. White open triangles mark 45 degree increments. The white triangles do not rotate with the compass card. • The compass arc shows 125°, with the current heading showing under the lubber line index. The arc also shows when FMS map mode is selected. • Tick marks show every 5° and heading numbers show every 30°. Letters replace the numbers at the 0°, 90°, 180°, and 360° heading marks to indicate the cardinal directions (N, E, S and W). Heading Readout A green three digit readout of the current heading shows in the lubber line index. If the heading data is missing or invalid, the compass rose or arc rotates to north-up, the lubber line index and digital heading readouts are removed, and the red HDG flag shows. Selected Heading Bug The heading bug is a cyan rectangular bug that shows on the compass rose or partial arc. The HDG knob on the APP sets the heading bug. A dashed cyan heading vector shows full time when the heading bug is out of view (in the partial arc or map mode). The dashed heading vector originates from the center aircraft symbol, and extends toward the selected heading. The heading vector rotates around the heading display in the same manner as the heading bug. Selected Heading Readout A three-digit readout of the selected heading shows below the attitude display on the PFD and below the EIS & Upper Information Panels on the MFD. The selected heading readout is a full-time display. The selected heading readout is removed if the heading data is missing or invalid. FMS Track/Drift Pointer The FMS drift pointer is positioned on the compass rose or partial arc at the current ground track. The drift angle is the difference between the drift pointer and the current heading. The drift pointer is a small magenta open circle. Citation CJ4X User Manual 57 Version 1.0 Build 1709 (September 2017) Range Display The selected display range shows when the partial arc or map mode is active. In the full compass rose format, it is displayed when TCAS overlay is active. The RANGE knob on the DCP controls the display range. • The partial compass arc serves as the range arc at the selected range. A digital readout of the selected range shows at the left end of the arc. • A full circle with the aircraft symbol at the center shows at half of the selected range, along with a digital readout of the half range. • The half range ring does not show when map mode is selected. • Display ranges available are: 5, 10, 25, 50, 100, 200, 300, and 600 NM. TCAS Range A 3 NM range ring is displayed only when TCAS overlay is active either in the PFD or MFD. The 3 NM range ring is formed by grey tick marks at the 12 cardinal clock positions. A circle (not shown) bisecting each line is the 3 NM range ring. The 3 NM range ring shows when the full range is 5, 10, or 25 NM. Course Pointer The course pointer is a single arrow that points to the selected course. The CRS left knob on the Autopilot Panel (APP) sets the pilot’s side VOR/LOC course pointer. The CRS right knob on the APP sets the copilot’s side VOR/LOC course pointer. • The CRS knob is not active when FMS is the active navigation source. • The course pointer does not show when the PPOS Map format is selected. • The tail of the course pointer is set to the inbound course of a B/C approach. • The course pointer is color-coded to indicate the active navigation source. Green indicates an onside source. Yellow indicates a cross-side source. Magenta indicates an onside FMS source. TO/FROM Indicator Pointer This indicator is a wide triangle that rotates with the course pointer. The point of the triangle indicates the aircraft is heading toward or away from the navigation source (VOR or FMS). The arrow is the same color as the course pointer. Lateral Deviation Pointer The lateral deviation bar is the same width and color as the course pointer. The bar moves left and right of the aircraft symbol to indicate the relative lateral deviation from the selected course. The lateral deviation freezes on zero position if lateral deviation data is missing or invalid. Lateral Deviation Scale The lateral deviation scale in the center of the display indicates the relative course displacement. The scale rotates around the aircraft symbol with the compass rose or partial arc. • The scale consists of two open white dots equally spaced on either side of the aircraft symbol. The scale is removed when the map mode is active or the lateral deviation bar freezes at zero position because of invalid data. • Lateral deviation scaling is as shown below: • VOR/LOC — One dot = 5° deviation • FMS — One dot = 5NM deviation. Citation CJ4X User Manual 58 Version 1.0 Build 1709 (September 2017) Wind Arrow The wind arrow indicates the direction of the wind relative to the heading of the aircraft. The velocity shows in a digital readout just above the wind arrow. • Wind Magnitude and Direction are sourced from the onside FMS. As there is only one FMS installed, it provides wind information to both displays. • Range for wind velocity readout is 0 to 255 knots. Active Navigation Source Display The active navigation source display consists of the navigation source annunciation, course or desired track readout, FMS waypoint identification, time to go (MFD only) and distance. • An identifying label precedes the course/desired track readout. Label nomenclature indicates whether the readout is a course or a track, as shown below. • CRS — VOR or LOC • DTK — FMS Desired Track • The FMS waypoint identifier shows up to seven characters for the waypoint name. • MFD Only: The time to go (TTG) readout source is the same as the distance source. Display format is two digits, a colon, followed by two digits. Time to go is measured to the nearest minute. • The distance readout is the distance to the active navigation source. • Distance is to the VOR/DME (or VORTAC) station when VOR is the active source. • Distance is to the runway when LOC is the active source. • Distance is to the FMS waypoint when FMS is the active source. • Range for the distance readout is 0 to 512 NM for DME, and 0 to 4,096 NM for FMS. • The navigation source display is color-coded to indicate the active navigation source. Green indicates an onside source. Magenta indicates an onside FMS source. • Blank line replace the identification readout when the VOR, Localizer or FMS waypoint identification data is missing or invalid. • Four dashes replace the time-to-go readout when ETE data (either from the FMS or DME) is missing or invalid. • Four dashes replace the distance readout when distance data is missing or invalid. TCAS Status/Mode Message The TCAS status or mode shows below the TFC legend in the TCAS data field on the right side of the MFD. Only one TCAS status or mode can show at a time. The priority order is: TCAS OFF and TA ONLY. • The message TCAS OFF shows in cyan on the PFD and MFD when the TCAS system is in standby mode and the TCAS traffic display (overlay) is selected. • The message TA ONLY shows in white on the PFD and MFD when TA ONLY mode is selected. Citation CJ4X User Manual 59 Version 1.0 Build 1709 (September 2017) ABOVE/BELOW The message ABOVE or BELOW shows in white when TCAS is in standby mode and in cyan when TCAS is on. Here, by default, all flying vehicles are displayed ether above or below the aircraft, as long as they are airborne. Elapsed Time (PFD Only) The elapsed time readout display consists of a white ET label, followed by two digits, a colon and two digits. It shows only when the pilot presses the ET button on the DCP. • If elapsed time is less than an hour, the elapsed time is measured to the nearest second. If greater than an hour, the elapsed time is measured to the nearest minute. LOC Lateral Deviation Display (PFD Only) The LOC lateral deviation display consists of a scale and pointer that shows at the bottom of the attitude display as a “cutout” section. The LOC lateral deviation display shows when LOC is the active NAV source or FMS is the active NAV source. • The deviation scale consists of two gray dots on either side of a center tick mark. • The deviation pointer is the same color as the active NAV source. The pointer is a waypoint (four-point star) shape when FMS is the NAV source, and a diamond shape when LOC is the NAV source. • Pointer movement is automatically reversed when B/C localizer logic is active. • LOC lateral deviation scaling is as shown below: • LOC — One dot ≈ 3° deviation • FMS — One dot = 5NM deviation. Bearing Pointers Two bearing pointers can show on the compass rose or partial arc format. One bearing pointer receives data from onside bearing sources, the other pointer receives data from the cross-side bearing sources. The bearing source is selected from the BRG SOURCE menu. More information here. • The sensor 1 (VOR1, FMS1, ADF1) bearing pointer is a cyan single-bar arrow. • The sensor 2 (VOR2, ADF2) bearing pointer is a white double-bar arrow. • Bearing pointer icons show as miniature representations of the bearing pointers. Icons are the same color as the bearing pointers. The bearing source icon does not show if the BRG source selection is OFF. • The bearing source annunciation (VOR, FMS, LOC) and the sensor side (1 or 2) shows with each icon. • The bearing icons show on the lower left side of the PFD and MFD. • If BRG1 is selected to FMS1 and the active NAV source is changed to FMS1, the BRG1 pointer reverts to VOR1 and vice versa. Citation CJ4X User Manual 60 Version 1.0 Build 1709 (September 2017) Present Position (PPOS) Map Format The FMS Present Position Map (PPOS Map) is a heading-up, present position moving map that graphically depicts the active FMS flight plan. When there is a flight plan in the FMS, the map format shows the legs of the flight plan as solid lines that connect the waypoints. FS-GPS-supplied background symbology including navaids, intersections, and airports is available for display on the PPOS Map. Geo-political boundaries, airspaces and airways are also available for display on the PPOS Map. A menu available on the MFD allows selection of the map symbology, showing the same symbols in both the PFD and MFD. The radius of the map is set with RANGE knob on the DCP. A NO FLIGHT PLAN message appears only when no route is open either via FMC (described here) or via FS Flight Planner. NOTE: Be careful with the map symbology because of performance. The more the symbology is displayed and the grater the map radius, the greater the performance impact (low frames). Citation CJ4X User Manual 61 Version 1.0 Build 1709 (September 2017) Terrain Overlay The Terrain overlay is an enhancement to the map. It contains a worldwide terrain elevation database. Graphical terrain elevation data is available for display on the PFD and MFD Arc and PPOS Map formats. When TERR is inactive, only water is displayed while ground is displayed in black. The graphical terrain data shows in a ± 90° arc in front of the aircraft. System messages and warnings value also show on the flight displays. Terrain Awareness Warning System (TAWS) is not emulated here. NOTE: Together with the map symbology, it is recommended to be careful with the terrain overlay because of performance. The grater the map radius, the greater the performance impact (low frames). Citation CJ4X User Manual 62 Version 1.0 Build 1709 (September 2017) Plan Map Format The FMS plan map format is a fixed, true north-up stationary map that depicts the active FMS flight plan. When a flight plan is in the FMS, the map format shows the legs of the flight plan as solid lines that connect the waypoints. An airplane symbol shows centered on the map and is oriented to the aircraft heading and the position is updated as the flight progresses. FS-GPS-supplied background symbology is available for display, including navaids, intersections, and airports. Geo-political boundaries, airspaces and airways are also available to display in this map format. The FMS plan map shows a single full circle as the range ring. The digital readout of the range shows in a cutout of the circle, and the circle is centered on the aircraft present position. Display ranges available for the FMS plan map are: 5, 10, 25, 50, 100, 200, 300, and 600 NM. NOTE: As before, it is recommended to be careful with the map symbology because of performance. The more the symbology is displayed and the grater the map radius, the greater the performance impact (low frames) and/or delay in map updating. Citation CJ4X User Manual 63 Version 1.0 Build 1709 (September 2017) TCAS Map Format The Traffic Alert and Collision Avoidance System (TCAS) traffic symbology is available for display on the MFD. A TCAS Only format is available, along with a TCAS overlay, on the PPOS Map, the full compass rose, the partial arc and the PLAN map formats. The map radius is selected with the RANGE knob on the DCP. When the TCAS Only option is available, the CCP is used to select the TCAS Only format. The TCAS-Only Map is a heading-up 360° moving map that graphically depicts the relative bearing, range, altitude, and vertical direction of nearby transponder-equipped aircraft that reply to TCAS interrogations. When the TCAS-Only format is in view, a full-range ring and a half-range ring show. A 3 NM range ring is also in view at the shorter ranges. Heading is read at the top of the full-range ring. Azimuth marks are provided every 30° around the full-range ring. An aircraft symbol shows in the center of the map. When TCAS-Only is active, GPS or optional Terrain information, if previously in view, are removed from display. NOTE: TCAS II is not emulated here, but a basic TCAS I without Traffic Advisory (TA) callouts is brought here, using the standard Flight Simulator TrafficInfo module and GPS module. TCAS II support is under revision for future updates. Citation CJ4X User Manual 64 Version 1.0 Build 1709 (September 2017) Data Line Data Line Callouts Name Description Cabin Pressurization Display (Pilot MFD) The cabin pressurization readouts show only on the pilot MFD. The readouts consist of cabin altitude reading, cabin rate reading and pressure differential reading. • Range of the digital cabin altitude readout is 0 to +15,000 feet. • Range of the digital cabin rate readout is 0 to ±15,000 fpm. • Range of the digital pressure differential readout is -1.0 to +10.0 PSI. • The CAB ALT, RATE, DIFF, DEST ELV labels and unit labels are always white. • The cabin altitude readout is green within normal limits (0 to 14,000 ft.). • The cabin altitude readout turns red outside the normal limits. • The pressure differential readout is green within normal limits (-0.5 to +9.1 PSI). • The pressure differential readout turns red outside the normal limits. Destination Elevation Readout (Pilot MFD) A digital destination elevation readout appears at the bottom right side of the pilot MFD. • The readout is always magenta and displays the elevation of the destination field airport in the flight plan. Usually part of the pressurization system calculations. • Four yellow dashes replace the readout when no flight plan is loaded either via FMC (described here) or via FS Flight Planner. Citation CJ4X User Manual 65 Version 1.0 Build 1709 (September 2017) Groundspeed Display (Copilot MFD) The groundspeed readout shows at the bottom of the MFD. Range for the groundspeed readout is 0 to 999 knots. The GS label is always white and the actual groundspeed readout is always magenta. True Airspeed Readout (Copilot MFD) The true airspeed readout shows at the bottom of the MFD, next to the groundspeed readout. • Range for the TAS readout is 0 to 999 knots. • The TAS label is always white and the TAS readout is always green. Ram Air Temperature Readout (Both PFDs and Copilot MFD) The RAT readout shows at the bottom of the PFD and MFD. • Range for the readout is -99 to +99 °C. • A minus sign precedes a negative RAT value. • The RAT label is always white and the RAT readout is always green. Static Air Temperature Readout (Copilot MFD) The SAT readout shows at the bottom of the MFD, next to the RAT readout. • The SAT label is always white and the SAT readout is always green. Range for the readout is -99 to +99 °C. • A minus sign precedes a negative SAT value. International Standard Atmosphere Differential Readout (Copilot MFD) The ISA readout shows at the bottom right side of the MFD and indicates the temperature deviation from the standard atmosphere temperature based upon standard lapse rates. • The ISA label is always white and the ISA readout is always green. Range for the readout is -99 to +99 °C. • A minus sign precedes a negative ISA value, and a plus sign precedes a positive ISA value. No plus or minus sign shows when ISA is 0°. COM Active Frequencies & Transponder Readout (PFD) This readout shows at the bottom of the PFD and indicates the active COMM1 frequency, COMM2 frequency and transponder code (Squawk). • The COM1 label is always white and the COM1 frequency readout is always green. • The COM2 label is always white and the COM1 frequency readout is always green. • The ATC1 label is always white and the transponder code readout is always green. UTC Readout (PFD) The UTC readout shows at the bottom right side of the PFD and indicates the current Zulu time or GMT time. • The UTC label is al