Global 5000 Flight Crew Operating Manual (Volume 2)

Pilot’s Windows − COM1 − NAV1 − ATC/TCAS − ADF1 − TCAS DSPY 1 − HF1 Copilot’s Windows − COM2 − NAV2 − ATC/TCAS − ADF2 − TCAS DSPY 2 − HF2 Main Tuning Page Transfer Key Line Select Keys Function Keys RMU 1 (Pilot’s) Tuning Knobs GF1710_003 COM1 NAV1 ATC/TCAS ADF1 TCAS DSPY 1 HF1 NB MEMORY−4 1 ATC ALT ALT: 121.82 118.02 MEMORY−1 117.45 110.00 1200 ADF 1799.5 REL NORMAL 15600 15423 LV NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−3 VHF NAVIGATION RECEIVERS The two VHF Navigation receivers (NAV 1 and NAV 2) provide VHF omnirange (VOR), Localizer (LOC), Glideslope (GS) and Marker Beacon (MB) signals to the navigation systems and flight crew. The navigation receivers operate in the following ranges: System Frequency Range Channel Spacing VOR 108.00 to 117.9 MHz 50 kHz (160 chan) LOC 108.10 to 111.95 MHz 50 kHz (40 chan) GS 329.15 to 335.00 MHz 150 kHz (40 chan) MB 75.00 MHz Preset Frequency selection is through radio tuning units located on the pedestal. COM1 NAV1 ATC/TCAS ADF1 TCAS DSPY 1 HF1 NB MEMORY−4 1 ATC ALT RANGE: 121.82 118.02 MEMORY−1 117.45 110.00 1200 ADF 1799.5 6 NORMAL 15600 15423 LV RMU 1 (Pilot’s) RMU 2 (Copilot’s) GF1710_004 COM2 NAV2 ATC/TCAS ADF2 TCAS DSPY 2 HF2 NB MEMORY−4 1 TA/RA RANGE: 123.45 127.95 MEMORY−2 117.45 110.10 1200 ADF 1799.5 6 NORMAL 15600 11233 LV NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−4 NAV 1 (2) The VHF NAV receiver houses the major navigation functions of the VOR/LOC receiver, glideslope receiver and marker beacon receiver. The NAV line select key is used to select navigation frequencies (VOR, LOC, GS and DME). The cursor will automatically reposition to the NAV receiver active frequency after 17 seconds. Pressing and holding NAV preselect key for more than 3 seconds moves cursor to the top and blanks the preselect window and allows direct tuning of NAV receiver active frequency. COM1 NAV1 ATC/TCAS ADF1 TCAS DSPY 1 HF1 NB MEMORY−4 1 ATC ALT ALT: 121.82 118.02 MEMORY−1 117.45 110.00 1200 ADF 1799.5 REL NORMAL 15600 15423 LV COM1 NAV1 ATC/TCAS ADF1 TCAS DSPY 1 HF1 NB MEMORY−4 1 ATC ALT ALT: 121.82 118.02 117.45 1200 ADF 1799.5 REL NORMAL 15600 15423 LV NOTE Pressing the NAV preselect key highlights the MEMORY window. Rotating the TUNE knob will scroll through the frequencies in MEMORY. GF1710_005 Pressing the transfer key will toggle the Active and Preset frequencies, channeling the NAV receiver to what had been the Preset. GF1710_006 COM1 NAV1 ATC/TCAS ADF1 TCAS DSPY 1 HF1 NB MEMORY−4 1 ATC ALT ALT: 121.82 118.02 MEMORY−1 117.45 110.00 1200 ADF 1799.5 REL NORMAL 15600 15423 LV COM1 NAV1 ATC/TCAS ADF1 TCAS DSPY 1 HF1 NB MEMORY−4 1 ATC ALT ALT: 121.82 118.02 110.00 1200 ADF 1799.5 REL NORMAL 15600 15423 LV 117.45 TEMP − 1 NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−5 NAV 1 (2) (CONT'D) While on the main tuning page, press the PGE button once to bring the NAV memory page into view. DISABLED 110.00 110.30 115.60 116.50 108.70 111.80 RETURN FMS MEMORIES 1 2 3 MORE DELETE INSERT 4 5 6 NAV1 117.45 COM1 NAV1 ATC/TCAS ADF1 TCAS DSPY 1 HF1 NB MEMORY−4 1 ATC ALT ALT: 121.82 118.02 MEMORY−1 117.45 110.00 1200 ADF 1799.5 REL NORMAL 15600 15423 LV GF1710_007 An FMS autotuned VOR or ILS frequency is displayed on the main tuning page. To override an FMS autotuned VOR or ILS frequency, toggle the transfer key, or enter a new active frequency. GF1710_008 ENABLED 1 2 3 4 5 6 RETURN FMS MEMORIES MORE DELETE INSERT 110.00 110.30 115.60 116.50 108.70 111.80 NAV1 117.45 110.25 AUTO 118.02 MEMORY−4 ALT: MEMORY−1 110.00 NB REL NORMAL 1 ATC ALT ADF LV ADF1 ATC/TCAS HF1 TCAS DSPY 1 COM1 NAV1 121.82 1200 1799.5 15423 15600 NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−6 DISTANCE MEASURING EQUIPMENT (DME) The DME simultaneously tracks four selected DME channels for distance, groundspeed and time to station, as well as monitoring two additional channels for ident functions. DME dedicates two of the four channels to the FMS. In normal VOR/ILS/DME operations, one of the six DME channels is paired with the active frequency and another with a preset frequency. Pushing the DME function key will split the NAV window on the main tuning page, allowing the active DME channel to be selected separate from the active VOR/ILS frequency. An H (hold) will be displayed to indicate that the distance display is not paired with the VOR/ILS navigation data. When DME hold is no longer required, cycle the DME function button until the split is removed from the NAV window. H 118.02 MEMORY−4 RANGE: NB NORMAL 1 ATC ALT ADF LV 6 H 118.02 MEMORY−4 RANGE: ADF LV NB 6 NORMAL 1 ATC ALT ADF1 ATC/TCAS HF1 TCAS DSPY 1 COM1 NAV1 121.82 108.30 1200 1799.5 15423 15600 DME IZZ 111.90 ADF1 ATC/TCAS HF1 TCAS DSPY 1 COM1 NAV1 121.82 108.30 1200 1799.5 15423 15600 DME IUL 109.30 GF1710_009 NOTE Cycling the DME function button will display the following in sequence: VOR/ILS − VOR/ILS and DME − VOR/ILS and TACAN − VOR/ILS. DME Hold ILS/VOR DME Ident NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−7 AIR TRAFFIC CONTROL (ATC) TRANSPONDER ATC Transponder operations are controlled by the adjacent line select keys and the tuning knobs. Both RMUs will display the same transponder information. If a code or mode is changed on one RMU, the other RMU will track it. GF1710_010 118.02 MEMORY−4 RANGE: NB NORMAL 1 ATC ALT ADF LV 6 ADF1 ATC/TCAS HF1 TCAS DSPY 1 COM1 NAV1 121.82 108.30 1200 1799.5 15423 15600 DME IZZ 111.90 The transponder will go into ident mode for approximately 18 seconds when the ID function key is pushed and an ID annunciator will appear. A reply annunciator (rectangular box), located in the upper right corner of the ATC window, will turn yellow, whenever the transponder is replying to an interrogation from a ground station or TCAS. When ID button is pressed, the reply annunciator will come on steady for approximately 20 seconds. 118.02 MEMORY−4 ATC ID RANGE: NB NORMAL 1 ATC ALT ADF LV 6 ADF1 HF1 TCAS DSPY 1 COM1 NAV1 121.82 108.30 1200 1799.5 15423 15600 DME IUL 109.30 GF1710_011 Reply Annunciator Ident Annunciator NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−8 TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) The TCAS is an airborne system that interrogates ATC transponders in nearby airplanes to identify and display potential and predicted collision threats, within 700 feet of closest point of approach. TCAS monitors a radius of up to 40 nautical miles about the airplane, computes range, bearing and closure rate of up to 12 other transponder equipped airplanes relative to the “own” airplane. TCAS and ATC transponder modes are set on the RMUs. Active (interrogated) range is possible up to 70 to 100 NM depending on atmospheric conditions. Passive range to a distance of 120 NM is possible if intruder aircraft has a TCAS change 7 and a GPS installed. The system provides appropriate aural and visual cues to the flight crew when TCAS computer analysis of an airplane signal predicts a penetration of TCAS protected airspace. Target/Threat Advisories The system provides four types of advisories: • Traffic Advisory − Traffic advisories (TA) symbols appear on the MFD, when target(s) is projected to converge with the TCAS equipped airplane in less than 45 seconds, with the closest point of approach being inside a minimum vertical separation envelope. Traffic advisories are generated for aircraft with operative mode S, mode C, or mode A transponders. The relative bearing and range of the intruder are displayed. • Resolution Advisory − Resolution advisories (RA) intruder symbols appear on the MFD, when target (s) is predicted to penetrate the protected vertical envelope in less than 30 seconds. A green fly-to Pitch Target Zone rectangle is also displayed on the PFD ADI which indicates the rate that must be achieved to maintain safe separation. Similarly, red Pitch Avoidance Zones appear which indicate pitch rates that should be avoided. RA display can only be issued if intruder airplane is equipped with mode S transponder. • Proximity Traffic − Proximity Traffic (PT) symbols appear on the MFD when non-threat airplane(s), which have a flight path that approaches the collision area. The PT symbol is displayed if the target does not qualify for a TA but is currently within 6.5 NM and 1200 feet of the TCAS airplane. • Other Traffic − Other Traffic (OT) symbols appear on the MFD to indicate targets outside of the 1200 foot relative altitude region of PT, up to the TCAS range set by the pilot and at a relative altitude difference of 2700 feet. The TCAS system provides no indication of traffic conflicts if the intruder airplane is without an operative transponder. NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−9 TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) (CONT'D) TCAS Symbology THREAT LEVEL CAUSE SYMBOL Resolution Advisory (RA) Traffic Advisory (TA) Proximate Traffic (PT) Other Traffic (OT) Intruding aircraft is 100 feet above and descending at least 500 feet per minute. Traffic is 1,200 feet below and climbing at least 500 feet per minute. Intruding aircraft level with and not climbing or descending. Traffic is 2,700 feet above and descending at least 500 feet per minute. +01 −12 +27 Up Arrow Indicates climbing traffic. Down Arrow Indicates descending traffic. Plus Sign (+) Relative altitude threat, airplane is above own airplane. Minus Sign (−) Relative altitude threat, airplane is below own airplane. DEFINITION DATA TAGS GF1710_016 TCAS Modes The following TCAS modes are selectable on the RMU: • TA/RA Mode − Normal operation mode providing full TCAS coverage. TCAS tracks up to 12 airplanes in the surrounding airspace and generates TAs and RAs as required. • TA ONLY Mode − TCAS tracks all PT airplanes and generates TAs, no RAs. Automatically selected when airplane is flying lower than 1100 feet AGL (while climbing) or 900 feet AGL (while descending). • TEST Mode − Pressing the TST button on the RMU, will start a self-test program that will verify proper operation of the TA and RA displays and of the aural advisories. The TEST mode does not affect normal TCAS operation. Should an actual TA or RA occur during TEST sequence, the test is automatically terminated and the advisory is announced and displayed. NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−10 TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) (CONT'D) ATC/TCAS Mode Select ATC/TCAS operations are controlled by the adjacent line select keys and the tuning knobs. The modes are: • ATC ON − Replies on Modes S and A, no altitude reporting. • ATC ALT − Replies on Modes A, C and S, with altitude reporting. • STANDBY − Transponder in standby mode. • TA ONLY − TCAS traffic advisory mode selected. • TA/RA − TCAS traffic advisory/resolution advisory mode selected. 1000 0 1 2 3 1 2 3 DME RANGE: 118.02 MEMORY−4 TA ONLY NB NORMAL ADF LV 6 ADF1 ATC/TCAS HF1 TCAS DSPY 1 COM1 NAV1 121.82 108.30 1200 1799.5 15423 15600 IZZ 111.90 TA ONLY NOTE Pressing adjacent line key will annunciate STBY or displayed mode. NOTE Rotating the tuning knob will select ATC ON, ATC ALT, TA ONLY or TA/RA. GF1710_017 The PGE function key provides access to a menu page. The menu allows access to the TCAS operational selections. ATC/TCAS CONTROL PAGE INTRUDER ALTITUDE: REL TA DISPLAY ; AUTO ATC ALT : 1 2500 RETURN TO RADIOS INTRUDER ALTITUDE REL Targets altitude displayed relative to one’s own airplane. − FL Targets altitude displayed as a flight level, for 20 seconds, then returns to REL. TA DISPLAY AUTO Traffic targets displayed only when a TA or RA target condition exists. MANUAL All traffic targets displayed within the viewing airspace. RETURN TO RADIOS Returns to main tuning page. ATC ALT 1, (2) Indicates that the transponder selected on the main tuning page is communicating at a displayed pressure altitude. This is not a control feature, only a cross check. GF1710_018 NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−11 TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) (CONT'D) TCAS DSPY 1 (2) Select The primary TCAS selection is selected via the adjacent line select keys. The TCAS selections are as follows: • Range − Selectable at 6, 12, 20, 40, 80, and 120 NM. • Altitude Band Select − NORMAL: With TA display set to AUTO, ± 1200 feet TCAS display altitude. With TA display set to MANUAL, ± 2700 feet TCAS display altitude. ABOVE: +7000 feet, −2700 feet TCAS display altitude. BELOW: −7000 feet, +2700 feet TCAS display altitude. RANGE: 118.02 MEMORY−4 NB 6 NORMAL 1 ATC ALT ADF LV ADF1 ATC/TCAS HF1 TCAS DSPY 1 COM1 NAV1 121.82 108.30 1200 1799.5 15423 15600 DME IZZ 111.90 NOTE GF1710_019 Rotate the tuning knob to change the range when adjacent line select key is selected. Rotate the tuning knob to change the altitude band select when adjacent line select key is selected. TCAS Mode Select Annunciation The indications for intruder alert and altitude band selections are as follows: GF1710_020 REL 4000 KDVT 1+36 12.5 KDVT ABOVE ETE NM KPHX TOC KSRP 4000 FL180 ABOVE 6 +10 REL TCAS Zoom Window MFD (MAP format) NAVIGATION Rev 3, Apr 25, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−12 TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) (CONT'D) TCAS Mode Select Annunciation (Cont’d) The indications for TCAS TEST are as follows: −04 +12 +10 360 −11 −03 +20 +03 TCAS TEST 6 12.5 NM TCAS TEST N 20 20 30 6 33 3 GF1710_021 TCAS TEST (when test initiated), then TCAS TEST PASS or TCAS TEST FAIL TCAS Status Messages TCAS status messages are annunciated as follows: TCAS Status Message Area GF1710_022a −Indicates resolution advisory failure. −Indicates that TCAS has been selected to −Indicates a functional test is in progress. −Indicates TCAS failure. −Indicates TCAS is selected and transponder is in STBY. traffic advisories only TCAS STBY TCAS TEST TCAS FAIL TA ONLY RA FAIL 1000 0 1 2 3 1 2 3 TCAS FAIL Digitized Voice TCAS will provide voice warnings. The voice warnings cannot be cancelled or reduced in volume. TA voice warning is “TRAFFIC, TRAFFIC“ RA voice warnings are: • ADJUST VERTICAL SPEED, ADJUST. • CLEAR OF CONFLICT • CLIMB, CLIMB NOW! − CLIMB, CLIMB NOW! • CLIMB, CROSSING CLIMB − CLIMB, CROSSING CLIMB. • CLIMB − CLIMB. • DESCEND, CROSSING DESCEND − DESCEND, CROSSING DESCEND. • DESCEND, DESCEND NOW! − DESCEND, DESCEND NOW! • DESCEND − DESCEND. • INCREASE CLIMB − INCREASE CLIMB. • INCREASE DESCENT − INCREASE DESCENT. • MAINTAIN VERTICAL SPEED, CROSSING MAINTAIN. • MAINTAIN VERTICAL SPEED, MAINTAIN. • MONITOR VERTICAL SPEED, MONITOR VERTICAL SPEED. NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−13 TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) (CONT'D) Resolution Advisories TCAS resolution advisories and status messages are displayed on the PFDs. The vertical maneuver is also accompanied by TCAS voice warnings. Resolution Advisory Indication CORRECTIVE ACTION CLEAR OF CONFLICT INDICATION CLIMB CLIMB DESCEND DESCEND FGF1710_001 Green rectangle advises pilot of fly-to-zone. Red avoidance zone advises pilot to fly out of, or do not enter indicated area. avoidance zone advises pilot to fly out of, 20 20 10 10 20 20 10 10 NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−14 TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) (CONT'D) TCAS Zoom Window TCAS zoom window is displayed on either or both MFDs and is selected on the MFD control panel, located on the pedestal. Ranges of 6, 12, 20, 40 and 120 NM can be selected by using the up or down buttons on the MFD control panel or on the RMU. 2 Mile Range Ring. Only shown when range is < 20 NM. When range is >20 NM, a half arc will appear. +12 −02 315 KLAX −04 +10 TERR OFF 1+36 345 12.5 KDVT KDVT WX T5 . 0 LX LUF 360 234 −40 −56 +12 −02 WX T5 . 0 LX LUF +10 KLAX −04 TERR OFF 345 234 −40 −56 1+36 12.5 KDVT KDVT FMS1 TRU N 50 50 KPHX TOC KSRP KLAX ETE NM 6 HDG ETE NM FMS1 N 50 50 KPHX TOC KSRP 6 Range Arc TCAS Zoom GSPD TAT TAS SAT GSPD TAT TAS SAT 30 6 33 3 GF1710_024a UP Button DOWN Button NOTE The TCAS zoom window shall be restored after menu usage, if the TCAS zoom window was previously in use. Plan Format Map Format NAVIGATION Rev 3, Apr 25, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−15 TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) (CONT'D) TCAS Traffic Display (MAP Format) The TCAS overlay is the default condition on the MFD during power-up. TCAS display can also be enabled on MAP format and is selected through the TCAS button on the MFD control panel. TCAS cannot be displayed on PLAN format. 315 TERR OFF −40 LX 360 LUF WX 234 −56 1+36 12.5 KDVT KDVT KDVT 4000 345 FMS1 The button sequence is as follows: not shown − TCAS zoom window − TCAS overlay − TCAS zoom window − not shown HDG ETE NM N 20 20 KPHX KPHX TOC TOC KSRP 4000 FL180 KSRP GSPD TAT TAS SAT 30 6 33 3 −04 +12 315 LX 360 LUF WX 1+36 12.5 KDVT KDVT KDVT 4000 GSPD TAT TAS −40 234 345 −56 SAT TERR IOFF FMS1 HDG ETE NM N 20 20 KPHX KPHX TOC TOC KSRP 4000 FL180 KSRP +10 30 6 33 3 GF1710_025a NOTE TCAS STBY, TA ONLY, TCAS, TCAS FAIL (amber), TCAS TEST (red) are available annunciations. TCAS not shown TCAS overlay NOTE TCAS STBY msg displayed on MFD and PFD when TCAS is selected with transponder in STBY. NAVIGATION Rev 3, Apr 25, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−16 TCAS SCHEMATIC FLIGHT DATA RECORDER ADVISORY DISCRETES ATC TRANSPONDER 1, 2 RADIO ALTIMETER SYSTEM OMNI−DIRECTIONAL ANTENNA AUDIO INTEGRATING SYSTEM IAC 1, 2, 3 DIRECTIONAL ANTENNA TCAS RECEIVER/TRANSMITTER WOW SYNTHESIZED VOICE TA/RA DISPLAY DATA 1 TA/RA DISPLAY DATA 2 DAU 4 EICAS ADC 1, 2, 3 AIR DATA COMPUTER SYSTEM ALT>15000FT VHF COM SYSTEM GF1710_026 NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−17 AUTOMATIC DIRECTION FINDER (ADF) The two ADF receivers (ADF1 and ADF2) provide relative bearing between the airplane and a selected ground station for display on the PFDs. ADF operations are controlled by the adjacent line select keys and the tuning knobs. For more information, see Chapter 6 COMMUNICATIONS. NB 6 NORMAL 1 ATC ALT ADF LV 118.02 RANGE: ADF1 ATC/TCAS HF1 TCAS DSPY 1 COM1 NAV1 121.82 108.30 1200 1799.5 15423 15600 DME IZZ 111.90 GF1710_027 The receivers operate in the following modes and are controlled by the adjacent line select keys or the tuning knobs. 118.02 RANGE: NB 6 NORMAL 1 ATC ALT LV ADF ADF1 ATC/TCAS HF1 TCAS DSPY 1 COM1 NAV1 121.82 108.30 1200 1799.5 15423 15600 DME IZZ 111.90 GF1710_028 VOICE Maximum audio clarity and fidelity, no bearing. BFO ADF adds a beat frequency oscillator (BFO) for detection of ADF Bearing determination. Some loss of received audio range and sensitivity. ANT Maximum sensitivity and range. Aural beacon ident and voice only, no bearing. cw signals. NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−18 BEARING (BRG) SOURCE Bearing information, VOR1, ADF1 or FMS1 and bearing information VOR2, ADF2 or FMS2, is selected on either the pilot’s and/or the copilot’s PFD control panel, located on the glareshield. VOR1 ADF 1 FMS 1 VOR2 ADF 2 FMS 2 NOTE Pushing BRG button (s) will toggle the following in sequence: − VOR − ADF − FMS − Blank GF1710_029 PFD Control Panel HDG 030 VOR1 CRS 360 VOR 2 3 N 6 33 E W 24 21 s 15 30 12 12 HDG 030 VOR1 3 N 6 33 E W 24 21 s 15 30 RAD BARO MINIMUMS NAV SCR BARO SET PUSH STD HPa IN RAD BARO MINIMUMS NAV SCR BARO SET PUSH STD HPa IN NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−19 VOR/LOC NAV SOURCE NAV source, VOR/LOC, is selectable on the pilot’s and/or the copilot’s PFD control panel. PILOT’S PFD NOTE Pushing V/L button will toggle the NAV source in the following sequence: on-side VOR/LOC − X-side VOR/LOC − on-side VOR/LOC On-side PILOT’S PFD COPILOT’S PFD NOTE If FMS is the primary NAV source, the first push of the V/L button will set preview NAV source. The second push of V/L button will cancel FMS as primary NAV source and set VOR/LOC as primary NAV source. PREVIEW NAV SOURCE PREVIEW COURSE POINTER X-side COPILOT’S PFD GF1710_030 HDG 030 VOR1 VOR1 CRS 360 3 N 6 33 E W 24 21 s 15 30 12 HDG 030 VOR2 CRS 360 VOR 2 3 N 6 33 E W 24 21 s 15 30 12 HDG 030 VOR2 CRS 360 VOR 2 3 N 6 33 E W 24 21 s 15 30 12 HDG 030 VOR2 CRS 360 VOR 2 3 N 6 33 E W 24 21 s 15 30 12 LOC1 FMS1 DTK 360 3 N 6 33 E W 24 21 s 15 30 12 HDG 330 NAV SCR NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−20 FMS NAV SOURCE FMS source, FMS1, FMS2, FMS3 (if installed) or Navigation Display Unit (NDU), also referred to as Lasertrack (LTRK) (if installed) is selectable on the pilot’s and/or the copilot’s PFD control panel. NOTE Pushing FMS button will toggle the NAV source in the following sequence: on-side FMS − X-side FMS − LTRK (if installed) − on-side FMS or, on-side FMS − FMS3 (if installed) − X-side FMS − on-side FMS. NOTE If V/L is the primary NAV source, pushing the FMS button will cancel V/L as primary NAV source and will set on-side FMS as primary NAV source. Pushing FMS button while V/L preview NAV source is displayed, will cancel preview NAV source. On-side X-side GF1710_031 PILOT’S PFD COPILOT’S PFD PILOT’S PFD COPILOT’S PFD HDG 360 FMS1 DTK 030 3 N 6 33 E W 24 21 s 15 30 12 HDG 360 FMS2 DTK 060 3 N 6 33 E W 24 21 s 15 30 12 HDG 360 FMS1 DTK 030 3 N 6 33 E W 24 21 s 15 30 12 HDG 360 FMS1 DTK 030 3 N 6 33 E W 24 21 s 15 30 12 NAV SCR NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−21 WEATHER RADAR (WX) The weather radar control panel, located on the pedestal, controls GAIN, RADAR modes, TILT and Lightning Sensor System (LSS) (if installed). It also enables turbulence (TRB) mode, antenna stabilization (STAB), target alert (TGT) and sector scan (SECT). TRB Button Used to determine if turbulence is present in WX mode at 50 NM or less. STAB ON/OFF Button Used to enable or disable antenna stabilization. TGT Button Used to detect weather conditions beyond selected range. SECT Button Used to select either the normal scan (120°) or alternate scan (60°). GAIN Knob Used to control receiver gain. RADAR Rotary Knob Used to select the following functions: OFF − Turns the radar system off. SBY − Selects standby mode, stops antenna scan and transmitter. WX − Selects weather radar mode. RCT − Selects rain echo attenuation compensation technique. GMAP − Selects ground mapping mode. FP − Selects flight plan mode. TST − Selects the radar test mode. Lightning Sensor System (LSS) (if installed) Used to select the following LSS operating modes: OFF − Turns the LSS off. SBY − Selects standby mode. LX − Displays LSS data on MFD. CLR/TST − Selects test mode. TILT Knob Used to select tilt angle. Clockwise rotation tilts beam upward to +15°, counterclockwise tilts the beam downward to −15°. SLV Annunciator Comes on to indicate which radar is slaved to the primary. The primary is the first WX turned on. GF1710_032 SLV NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−22 WEATHER RADAR (WX) (CONT'D) The weather radar system provides a display of X−band radar detectable areas of precipitation along and within 60° on either side of the airplane’s flight path. Weather radar returns, turbulence and lightning (if LSS installed) are displayed on the MFDs (MAP mode only). A range of up to 300 NM from the airplane is selectable using the up or down buttons on the MFD control panel. MAP MODE WX MODE AND STATUS ANNUNCIATION LIGHTNING ANNUNCIATION WX Radar Range 10 NM 25 NM 50 NM 100 NM 200 NM 300 NM NOTE GF1710_033 TOC KSRP HDG 315 ETE1+36 12.5 KDVT NM FMS1 360 N 50 50 KPHX LUF KDVT KPHX TOC KSRP KDVT 4000 4000 FL180 WX T5.0 G85% LX SAT GSPD −56 TAT TAS −40 234 345 30 6 33 3 WX RADAR will synchronize to whatever range is displayed on MFD (on power up). RADAR ANTENNA The antenna sweep is selectable for either 120° (60° each side of the airplane) or 60° (30° each side). The antenna tilt is adjustable between −15° (down) and +15° (up). The antenna maintains its stabilization with respect to the horizon regardless of the airplane attitude (within −15° to +15°). GF1710_034 ANTENNA NAVIGATION Rev 3, Apr 25, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−23 MODE SELECTION The weather radar operating modes, gain and antenna tilt functions are all controlled by the two radar control panels. Both the pilot and copilot can look at different ranges and tilt settings at the same time on their respective MFDs. The weather radar modes and features are as follows: TRB − Momentarily pressing the TRB button enables the turbulence mode. When this mode is selected, the radar determines if turbulence is present. TRB can only be engaged in the WX mode and in selected ranges of 50 NM or less. The weather/turbulence WX/T mode is annunciated in the status display. Areas of at least moderate turbulence are shown in white. ANNUNCIATION N 20 20 KPHX TOC KSRP KDVT 4000 4000 FL180 WX G85% LX SAT GSPD −56 TAT TAS −40 234 345 30 6 33 3 GF1710_035 T5.0 STAB − Momentarily pressing the STAB button, holds the elevation of the antenna beam constant at all azimuths, regardless of airplane bank or pitch maneuvers and relative to the earth’s surface. The stabilization system uses IRS as a reference. Momentarily pressing the STAB button disables antenna stabilization and STAB is annunciated in the status display. KPHX TOC KSRP KDVT 4000 4000 FL180 WX G85% STAB SAT GSPD −56 TAT TAS −40 234 345 GF1710_036 ANNUNCIATION T5.0 NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−24 MODE SELECTION (CONT'D) TGT − Target alert monitors for red or magenta weather conditions (rainfall rate) beyond the selected range and 7.5° on each side of the airplane heading and is selectable in all but the 300 NM range. If such weather is detected, outside the selected range the TGT alert annunciation changes from green armed to an amber alert condition on the MFD WX Status display. When this warning is received, the pilot should select longer ranges to view target alert. When TGT button is selected, TGT annunciation will replace the GAIN annunciation in the status display. TGT will be displayed as TGT (flashing), if red or magenta is detected outside selected range. Rainfall Rate RAINFALL COLOUR CODING in/hr mm/hr Colour .04 to .16 1 to 4 .16 to .47 4 to 12 .47 to 2.0 12 to 50 >2 >50 KPHX TOC KSRP KDVT 4000 4000 FL180 WX TGT SAT GSPD −56 TAT TAS −40 234 345 GF1710_037 T5.0 SECT − The normal radar sweep is ± 60° from the airplane nose at a rate of 14 sweeps/min. Pressing SECT button reduces the angle of sweep to ± 30° at a rate of 28 sweeps/min. Pressing the SECT button again, returns to normal sweep. Both the pilot’s and copilot’s displays will show the same sweep angle. N 50 50 N 50 50 30 6 33 3 30 6 33 3 GF1710_038 120° arc 60° arc GAIN − The GAIN knob is a rotary control and push/pull switch that is used to control the receiver gain. Push on the GAIN switch to enable the preset calibrated gain mode. Calibrated gain is the normal mode and is used for weather avoidance. Pull out on the GAIN switch to enable the variable gain mode. Variable gain is used to provide additional weather analysis and for ground mapping. In WX mode, variable gain receiver sensitivity can be increased to show weak targets or can be reduced to eliminate weak returns. ANNUNCIATION KPHX TOC KSRP KDVT 4000 4000 FL180 WX G85% SAT GSPD −56 TAT TAS −40 234 345 GF1710_039 T5.0 NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−25 WX SYSTEM OPERATION The RADAR rotary knob is used to select the following functions: OFF − Turns the radar off. The system is no longer radiating and the antenna is stowed. KPHX TOC KSRP KDVT 4000 4000 FL180 SAT GSPD −56 TAT TAS −40 234 345 WX/OFF TGT GF1710_040 ANNUNCIATION T5.0 SBY − Selects the WX system in standby mode. It takes approximately 45 seconds for the system to warm up after being switched out of OFF. There is also a hidden mode, Forced Standby (FSBY). This mode is enabled automatically on the ground, if the airplane is powered up, with the radar powered. To exit FSBY, push STAB button 4 times within 3 seconds. This mode prevents the radar from radiating, thereby protecting the ground personnel from radiation exposure. STBY TGT FSBY KPHX TOC KSRP KDVT 4000 4000 FL180 SAT GSPD −56 TAT TAS −40 234 345 GF1710_041 ANNUNCIATION T5.0 WX − Selects the WX mode of operation. When WX is selected, airplane inflight, the system is fully operational and all parameters are set for enroute weather detection. If the rotary knob is moved directly from OFF to WX, the system will first go into SBY for approximately 45 seconds, then become active. KPHX TOC KSRP KDVT 4000 4000 FL180 WX T5.0 TGT SAT GSPD −56 TAT TAS −40 234 345 GF1710_042 ANNUNCIATION NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−26 WX SYSTEM OPERATION (CONT'D) RCT − Enables the Rain Attenuation Compensation Technique (REACT). The REACT compensates for attenuation of the radar signal as it passes through rainfall. Strong targets (high attenuation levels) cause the receiver to reach its maximum gain value in a short time/short range. Weak targets (low attenuation levels) cause the receiver to reach its maximum gain in a longer time/longer range. When this maximum gain value is reached, a cyan background field will appear. Any target inside of the cyan area will appear in magenta colour, indicating maximum severity. 25 25 N KPHX TOC KSRP KDVT 4000 4000 FL180 WX/R/T TGT SAT GSPD −56 TAT TAS −40 234 345 30 6 33 3 GF1710_043 ANNUNCIATION T5.0 GMAP − Selects the ground mapping mode. The auto TILT control is turned down until the desired amount of terrain is displayed. The colour scheme is changed to cyan (least reflective return), yellow (moderate return) and magenta (strong return). 100 100 N KPHX TOC KSRP KDVT 4000 4000 FL180 GMAP TGT SAT GSPD −56 TAT TAS −40 234 345 30 6 3 GF1710_044 ANNUNCIATION 33 T5.0 FP − Selects the flight plan mode. This clears the screen of radar data so ancillary data can be displayed, such as navigation displays and lightning data. In the FP mode the radar RTA is put to standby and the FPLN legend is displayed in the mode field. KPHX TOC KSRP KDVT 4000 4000 FL180 FPLN SAT GSPD −56 TAT TAS −40 234 345 GF1710_045 ANNUNCIATION NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−27 WX SYSTEM OPERATION (CONT'D) TST − Selects the test mode. The test position selects a special test pattern, to verify system operation. When the TEST is complete, the radar enters the FSBY mode. TEST KPHX TOC KSRP KDVT 4000 4000 FL180 SAT GSPD −56 TAT TAS −40 234 345 GF1710_046 ANNUNCIATION NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−28 WX SYSTEM OPERATION (CONT'D) TILT The TILT rotary knob is used to manually select the tilt angle of the antenna. Clockwise rotation of the knob tilts the antenna upward to +15° and counter-clockwise rotation of knob tilts antenna downward to −15°. When the TILT knob is pulled out (auto-tilt), the antenna tilt is automatically adjusted with regard to selected range and barometric altitude. The tilt control can fine tune the tilt setting by ± 2°. When in auto-tilt, an A symbol will appear following the digital tilt readout. AUTO-TILT GF1710_048a 4000 KDVT 234 −56 −40 345 KPHX TOC KSRP 4000 FL180 GMAP G85% SAT GSPD TAT TAS ANNUNCIATION T5.0 A T5.0 80,000 70,000 60,000 50,000 30,000 20,000 10,000 0 0 100 50 25 CENTER OF RADAR BEAM ZERO TILT 7,400 ft 5.6° 14,800 ft 29,000 ft RANGE NAUTICAL MILES ELEVATION IN FEET 40,000 30,000 20,000 10,000 5,000 0 0 10 CENTER OF RADAR BEAM ANTENNA ADJUSTED 7,400 ft 5.6° 14,800 ft RANGE NAUTICAL MILES ELEVATION IN FEET 20 30 40 50 60 70 80 FOR 2.8° UPTILT 3,000 ft NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−29 WX SYSTEM OPERATION (CONT'D) TILT MANAGEMENT The pilot can use tilt management techniques to minimize ground clutter when viewing weather targets. Assume the aircraft is flying over relatively smooth terrain that is equivalent to sea level in altitude. The pilot must make adjustments for the effects of mountainous terrain. The following figure helps to visualize the relationship between tilt angle, flight altitude, and selected range. It shows: • Distance above and below aircraft altitude that is illuminated by the flat-plate radiator during level flight with 0° tilt. • Respective low altitude situation, with the antenna adjusted for 2.8° up-tilt. AUTO-TILT GF1710_048a 4000 KDVT 234 −56 −40 345 KPHX TOC KSRP 4000 FL180 GMAP G85% SAT GSPD TAT TAS ANNUNCIATION T5.0 A T5.0 80,000 70,000 60,000 50,000 30,000 20,000 10,000 0 0 100 50 25 CENTER OF RADAR BEAM ZERO TILT 7,400 ft 5.6° 14,800 ft 29,000 ft RANGE NAUTICAL MILES ELEVATION IN FEET 40,000 30,000 20,000 10,000 5,000 0 0 10 CENTER OF RADAR BEAM ANTENNA ADJUSTED 7,400 ft 5.6° 14,800 ft RANGE NAUTICAL MILES ELEVATION IN FEET 20 30 40 50 60 70 80 FOR 2.8° UPTILT 3,000 ft NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−30 WX SYSTEM OPERATION (CONT'D) TILT MANAGEMENT (Cont’d) The following figure gives the approximate tilt settings at which ground targets begin to be displayed on the image periphery for an 18-inch radiator. The range at which ground targets can be oberved is affected by the curvature of the earth, the distance from the aircraft to the horizon, and altitude above the ground. As the tilt control is rotated downward, ground targets first appear on the display at less than maximun range. To find the ideal tilt angle after the aircraft is airborne, adjust the TILT control so that ground clutter does not interfere with viewing of weater targets. Usually, this can be done by tilting the antenna downward in 1° increments until ground targets begin to appear at the display periphery. Ground returns can be distinguished from strong storm cells by watching for closer ground tragets that are displayed. When ground targets are displayed, move the tilt angle upward in 1° increments until the ground targets begin to disappear. Proper tilt adjustment is a pilot judgment, but typically the best tilt angle lies where ground targets are barely visible or just off the radar image. NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−31 WX SYSTEM OPERATION (CONT'D) TILT MANAGEMENT (Cont’d) The figure gives the approximate tilt settings required for different altitudes and ranges. If the altitude changes or a different range is selected, adjust the tilt control as required to minimize ground returns. GF1710_182 LINE OF SIGHT (NM) RANGE SCALE (NM) ALTITUDE (FEET) 10 25 50 100 200 40,000 35,000 30,000 25,000 20,000 15,000 10,000 5,000 4,000 3,000 2,000 1,000 39 55 67 78 87 123 151 174 195 213 230 246 −5 −9 −7 −8 −9 −13 −13 (LINE OF SIGHT LIMITED REGION) (TILT LIMITED REGION) −11 −10 −5 −5 −6 −6 −8 −4 −12 −11 −10 −5 −6 −7 −8 −9 −5 −5 −4 −6 −7 −7 −8 −8 −6 −5 ALTITUDE TILT RANGE Tilt angles shown are approximate. Where the tilt angle is not listed, the operator must exercise good judgment. NOTE The line of sight distance is nominal. Atmospheric conditions and terrain affect this value. NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−32 WX SYSTEM OPERATION (CONT'D) TILT MANAGEMENT (Cont’d) For more information on WX Radar, see manufacturer’s Manual A28−146−102−00. NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−33 LIGHTNING SENSOR SYSTEM (LSS) (IF INSTALLED) The lightning sensor system is used to detect lightning. The LSS rotary knob is used to select the following functions: OFF − Turns off the LSS. KDVT 4000 345 234 −56 −40 GMAP TGT LX OFF (If installed) KPHX TOC KSRP 4000 FL180 SAT GSPD TAT TAS GF1710_049 ANNUNCIATION T5.0 SBY − Selects the LSS in standby mode. The data is inhibited, but LSS accumulates data. KDVT 4000 345 −56 −40 234 GMAP TGT STBY KPHX TOC KSRP 4000 FL180 SAT GSPD TAT TAS GF1710_050 ANNUNCIATION T5.0 LX − LSS is fully operational and displays data on the MFD. KDVT 4000 234 −56 −40 345 GMAP TGT LX N 50 50 Rate 1: Lightning rate of 2−15 strokes in the last 2 minutes. Rate 2: Lightning rate of 16−31 strokes in the last 2 minutes. Rate 3: Lightning rate of >32 strokes in the last 2 minutes. ALERT: Range is indeterminate but bearing accurately determined. Azimuth should be closely monitored. KPHX TOC KSRP 4000 FL180 SAT GSPD TAT TAS 30 6 33 3 GF1710_051 ANNUNCIATION T5.0 CLR/TST − LSS accumulated data is cleared from memory. After 3 seconds the test mode is initiated. 345 KDVT 4000 −40 −56 234 GMAP TGT LX/T KPHX TOC KSRP 4000 FL180 SAT GSPD TAT TAS GF1710_052 ANNUNCIATION T5.0 For more information on Lightning Sensor System, see manufacturer’s manual. NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−34 WEATHER RADAR SCHEMATIC MFD CONTROLLER 2 IAC 1 IAC 1 IAC 2 IAC 2 IAC 3 IAC 3 PILOT’S WX CONTROLLER COPILOT’S WX CONTROLLER WOW WX RECEIVER/ TRANSMITTER/ ANTENNA DU 5 DU 2 IRU 2 WOW WOW CAIMS MFD CONTROLLER 1 GF1710_053 SLV SLV IRU 1 TOC 1+36 KDVT 4000 KDVT 360 −40 −56 234 LX 345 0.05 WX 00:10 315 ET GSPD TAT TAS L HDG ETE NM KPHX KSRP 4000 FL180 SAT TOC FMS1 N 5 5 KPHX KSRP 30 33 3 6 TOC 1+36 KDVT 4000 KDVT 360 −40 −56 234 LX 345 0.05 WX 00:10 315 ET GSPD TAT TAS L HDG ETE NM KPHX KSRP 4000 FL180 SAT TOC FMS1 N 5 5 KPHX KSRP 30 33 3 6 NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−35 ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) The primary purpose of the EGPWS is to provide alerts and warnings to avoid controlled flight into terrain and to provide detected windshear warning. The EGPWS is categorized into 7 modes. The basic GPWS function is comprised of modes 1 through 6. The windshear function and the enhanced feature, terrain awareness alerting and display function, are mode 7. The Enhanced Ground Proximity Warning Computer (EGPWC) processes all inputs and provides all aural and visual alerts and warnings. The following priority, from highest to lowest, is used to determine which annunciation is displayed if more than one is active : • WIND SHEAR • PULL UP • GND PROX • WIND SHEAR An alert annunciation indicates potential for impact with terrain. A warning annunciation indicates a prediction for impact with terrain. All annunciations are displayed on pilot’s and copilot’s PFDs. The MFD control panel provides for the selection of the Terrain display on the respective MFD. For more information on the MFD Control Panel, see Chapters 3 and 11. TERR BUTTON Used to enable terrain display. GF1710_058 The EGPWS control panel, located on the pedestal, provides for the selection of GS WARN (MUTED), FLAP OVRD (OVRD) and TERRAIN (MUTED). FLAP OVRD Switch Used to mute flap aural warning when flaps are not properly configured for landing. GS WARN Switch Used to mute glideslope warning. TERRAIN Switch Used to inhibit terrain clearance floor, terrain awareness alerting and display functions (in a case where landing at an airport, that is not in the database). GF1710_059 EGPWS OFF OVRD MUTED NAVIGATION Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 17−10−36