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TERRAIN AWARENESS WARNING SYSTEM (TAWS) (Cont)

MFD CONTROL PANEL (MCP)

Illustration of the MFD is shown with the optional 3D Map Display switches (refer to Chapter 11-1-24 for
further description).

DISPLAY CONTROL PANEL (DCP)

TAWS WARN PANEL

CAS

CKLST

SKIP

FRMT

TFC

ENTER

TR/WX

SUMRY

A/ICE

ECS

ELEC

FLT

FUEL

HYD

L

R

C

F

O1

101002_00

9

AUTO

PLAN

SHLDR

SIDE

CF

O

170

1002_005

OFF

OFF

OFF

TAWS WARN

GS

FLAPS

TERRAIN

1/2

DME/H

NAVSRC

RADIO

BRGSRC

FRMT

TFC

TR/WX

REFS

RADAR

TUNE

MENU

DATA

TILT

RANGE

CF

O

1101002_007

S

U

P

H

AUTO

T

L

I

T

S

U

P

H

T

C

E

L

E

S

Challenger Global 300 - Navigation

Page 14

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Summary of Contents for Challenger Global 300

Page 1: ...on of any of the system components will not adversely affect or will not be adversely affected by the simultaneous operation of any other radio or electronic unit or system The Challenger 300 is equip...

Page 2: ...o and visual marker information for cockpit indi cations The ADF receiver operates in the frequency range of 190 to 1799 kHz and the maritime distress bands of 2088 2094 kHz and 2179 2185 kHz It can o...

Page 3: ...the selection box on the CONTROL menu Turn the DATA knob to change the mode or select an option or push the PUSH SELECT button to step through available options Push the PUSH SELECT button to step thr...

Page 4: ...Turn the MENU knob to move the selection box to the Flight ID control Turn the TUNE knobs to set the desired Flight ID characters Select the ATC TCAS TEST mode Turn the MENU knob to move the selectio...

Page 5: ...control of both the on side and cross side radios Data entry to the CDU is made through the scratchpad and the line select keys Information is entered on the scratchpad then transferred to the approp...

Page 6: ...the paired tuning between DME and VHF navigation systems to enable independent opera tion The DME hold function holds the DME transceiver to the current VHF navigation frequency and permits the VHF n...

Page 7: ...power up on the ground the system powers up in standby mode TA RA is the normal TCAS mode When TA RA mode is set the TCAS computer generates intruder traffic symbology and resolution advisory vertica...

Page 8: ...mid air collisions The TCAS II system provides no indication of traffic conflicts with the other aircraft without operative transponders COMPONENTS AND OPERATION The TCAS II system provides the follo...

Page 9: ...tive tuning control operation and any code may be entered between 0000 and 7777 The IDENT switch is located on both control wheels and stays active for approximately 18 seconds when pushed The TRANSPO...

Page 10: ...alify for a TA but is currently within 6 nm and 1200 feet of the TCAS airplane Other Traffic open cyan color diamond The other traffic OT is in the surveillance area but is not a collision threat When...

Page 11: ...escend Crossing Descend Same as Descend Descend aircraft s flight path will cross the flight path of the intruder Increase Descent Follows a descent advisory Descent rate should be increased to the ra...

Page 12: ...OFF appears when the system is off The failure messages appear on the VSI and MFD They are TCAS RA FAIL TCAS FAIL TCAS RESOLUTION ADVISORIES RA INHIBITS TCAS Resolution Advisories RA and some aural a...

Page 13: ...automatically displayed on the MFD when a terrain hazard is encountered Each time the TAWS computer commands a terrain popup the MFD automatically commands terrain over lay to be added to the current...

Page 14: ...n DISPLAY CONTROL PANEL DCP TAWS WARN PANEL CAS CKLST SKIP FRMT TFC ENTER TR WX SUMRY A ICE ECS ELEC FLT FUEL HYD L R CFO1101002_009 AUTO PLAN SHLDR SIDE CFO1701002_005 OFF OFF OFF TAWS WARN GS FLAPS...

Page 15: ...NT RATE SINKRATE PULL UPI MODE 1 SINK AFTER TAKEOFF DON T SINKI MODE 3 EXCESSIVE DEVIATION BELOW GLIDESLOPE GLIDESLOPE MODE 5 EXCESSIVE BANK ANGLE BANK ANGLEI MODE 6 FIVE HUNDRED ALTITUDE CALL OUTS WI...

Page 16: ...aural SINKRATE SINKRATE The aural alert will be annunciated once and will be repeated only if condition degrades by more than 20 based on computed time to impact The visual alert will remain until th...

Page 17: ...n flaps are not in the landing position Penetration of the alert area will annunciate a GND PROX amber CAS on the PFD and generate an aural TERRAIN TERRAIN The aural is annunciated once and the visual...

Page 18: ...TERRAIN TERRAIN The aural and the visual alerts are annunciated continuously and will remain until the condition is rectified Penetration of the warning area will annunciate a red PULL UP on the atti...

Page 19: ...ent began and compares successive altitude data to the stored value Activation of the warning is induced when the minimum terrain clear ance as a function of altitude lost is exceeded Penetration of t...

Page 20: ...tude of 500 feet AGL During penetration of the alert area above 190 knots the upper boundary increases with airspeed to a maximum of 1000 feet radio altitude at 250 knots or more This annunciates an a...

Page 21: ...lane exits the envelope Penetration of the alert area below 159 knots annunciates an amber GND PROX display on the PFD and generates an aural TOO LOW FLAPS warning NOTE Aural TOO LOW FLAPS warning can...

Page 22: ...OX display on the PFD and generate an aural TOO LOW TERRAIN warning CFO1701002_018 200 0 400 600 800 1000 1200 1400 1600 1800 2000 2200 2400 2600 2800 3000 100 800 2800 0 MIN TERRAIN CLEARANCE FEET RA...

Page 23: ...glideslope an aural GLIDESLOPE warning is generated at the same volume level as all other warnings An amber GND PROX is dis played on the PFD The aural and visual alerts and warnings are continuously...

Page 24: ...d altitudes The aural ONE HUNDRED FIFTY and THIRTY indicates the transition through 100 50 and 30 feet AGL The last annun ciated or transition altitude is memorized This will prevent the repeat annunc...

Page 25: ...50 feet AGL This will generate an aural BANK ANGLE BANK ANGLE The alert is annunciated once and will repeat if the bank angle increases by 20 The alert will be annunciated continuously if the bank ang...

Page 26: ...ormance shear WINDSHEAR W flashes for 5 seconds then remains steady An aural tone WINDSHEAR WINDSHEAR warning is activated For a decreasing performance shear downdraft tailwind the flight director dis...

Page 27: ...lert criteria 2 SOLID AMBER Areas of terrain that satisfy the terrain caution alert criteria 3 GREEN AMBER RED DOT PATTERN Areas of terrain that are significantly close to the aircraft but do not sati...

Page 28: ...ated areas which meet the terrain collision alert criteria are depicted red Terrain automatically comes up in MAP mode on MFD at a 10 nm range if there is a terrain warning at 30 seconds from impact N...

Page 29: ...st runway center point position and radio altitude along with an internal database that includes all worldwide hard surfaced runways greater than 3500 feet in length Penetration of the alert envelope...

Page 30: ...2 SAT 15 5 C ISA TAS GS 250 254 30 MFD CONTROL TR WX LX 24 W 30 33 N 3 6 DBQ ALO TNU NEBOR CID IOW IA 200 KCID 100 270 150 FUEL SUMRY TR WX 1 3 2 FMS1 DTK 350 KCID TTG 15 01 95 0 NM HDG 340 STAB NU ND...

Page 31: ...sing the RADAR button on the display control panel Selection of the radar display is accomplished by pressing the TR WX button on the display control panel Range and tilt are controlled by the respect...

Page 32: ...cted those radar returns that appear as ground clutter are suppressed This feature eases the interpretation of rainfall when viewed from higher altitudes by eliminating much of the display caused by g...

Page 33: ...talled on the right side of the center pedestal When two FMS systems are installed each CDU controls its on side FMS The FMS can be initialized waypoints and destination selected by a variety of means...

Page 34: ...e PFD the aircrew should verify that the inputs that were entered into the FMS for computation of takeoff or approach performance reflect the actual or intended takeoff or approach conditions A summar...

Page 35: ...tion solution shows on the MFD LRN STATUS page RAIM is used to assure that the GPS solution meets the required accuracy criteria that follow 4 nm for oceanic remote 2 nm for enroute 1 nm for terminal...

Page 36: ...TUN CLR DEL BRT DIM A B C D E F G H I J K L M N O P Q R S T U V W X Y Z SP 1 2 3 4 5 6 7 8 9 0 COM1 COM2 COM3 HF1 HF2 CAB PA HDPH SPKR INPH MKR 2 ADF 1 2 1 DME 2 1 NAV VOICE EMER 02 MASK BOTH NORM NO...

Page 37: ...in function of the terrain awareness system has failed TAWS TERR NOT AVAIL TO LAND The TAWS terrain data base has no data for the current location TAWS WINDSHEAR FAIL TO LAND The windshear function of...

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