BOMBARDIER GLOBAL 5000 Flight Crew Operating Manual Download | Manualshive

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TOWING

A fitting for towing or pushing the airplane is located on the nose landing gear.

During towing, nose wheel swivel through the range of ±75° each side of center is possible, without
disconnecting the nose wheel steering torque links. The Aircraft Maintenance Manual (Chapter 09)
has a detailed description of towing operations.

NOTE

Disconnecting the nose wheel steering torque links is recommended for
all towing operations.

TOW BAR ATTACHMENT SCHEMATIC

TOW BAR ASSEMBLY

GF0110_013

AIRPLANE GENERAL

Rev 3, Apr 25, 2005

Flight Crew Operating Manual

CSP 700−5000−6

Volume 2

01−10−28

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Summary of Contents for GLOBAL 5000

Page 1: ...es For Ground Operation 01 10 20 Steering Radii 01 10 21 Steering Radii Schematic 01 10 21 Turning Radii 01 10 22 Turning Radii Schematic 01 10 22 Jet Exhaust Single Engine Ground Idle Thrust 01 10 23...

Page 2: ...els 01 10 40 Overhead Panel 01 10 41 Glareshield 01 10 42 Centre Pedestal 01 10 43 Copilot s Instrument Panel 01 10 44 Copilot s Side Panel 01 10 45 Copilot s Side Console 01 10 46 Airplane Doors 01 1...

Page 3: ...ion 01 10 58 Baggage Door Indication 01 10 58 Door Indication and Control 01 10 59 STAT Page 01 10 59 Passenger Door 01 10 59 Emergency Exit 01 10 59 Baggage Door 01 10 60 Large Maintenance Doors 01 1...

Page 4: ...AIRPLANE GENERAL TABLE OF CONTENTS Rev 2A Apr 11 2005 Flight Crew Operating Manual CSP 700 5000 6 Volume 2 01 00 4 THIS PAGE INTENTIONALLY LEFT BLANK...

Page 5: ...titude Director Indicator ADS Air Data System AFCS Automatic Flight Control System AFT Aftward AGL Above Ground Level AHC Attitude Heading Computer AIL Aileron ALIGN Aligning alignment ALPHA alpha ALT...

Page 6: ...ed Air Speed CAS Crew Alerting System CAT Category CAT II Category II CB C B Circuit Breaker CBP Circuit Breaker Panel CCBP Cockpit Circuit Breaker Panel CCW Counter Clockwise CDL Configuration Deviat...

Page 7: ...r DEV Deviation DFDAU Digital Flight Data Acquisition Unit DFDR Digital Flight Data Recorder DG Directional Gyro DH Decision Height DIFF Differential DIM Dimming DIR Direct DIS Distance to way point D...

Page 8: ...Engine Vibration Monitor Unit EVMS Engine Vibration Monitor System F F CTL Flight Controls FAA Federal Aviation Administration USA FADEC Full Authority Digital Electronic Control FAIL Failure FCC Fli...

Page 9: ...Mercury HI High HLDR Holder HOR HORIZ Horizontal HOT Hot Oil Temperature HP High Pressure HPSOV High Pressure Shut off Valve HPA Hecto Pascals HSI Horizontal Situation Indicator HSTA Horizontal Stabi...

Page 10: ...Processor J JAA Joint Airworthiness Authority K K KT KTS Knots kg s Kilogram s kHz KiloHertz KIAS Knots Indicated Airspeed kW s KiloWatt s L L Left Landing L T Landing Taxi LAV Lavatory LB s Pound s L...

Page 11: ...MEL Minimum Equipment List MFD Multi function Display MGP MLS Glideslope MHz MegaHertz MI Miles MIC Microphone MID AFT Middle Aftward MID FWD Middle Forward MILS 001 of an inch MIN Minimum MISC Misce...

Page 12: ...oad OVSP Overspeed OVSPD Overspeed OVTEMP Over Temperature OXY O2 Oxygen P P 6 Panel 6 P S Pitot Static PA Passenger Address PASS Passenger PBE Portable Breathing Equipment Smoke Hood PCU Power Contro...

Page 13: ...ation RPM Revolutions Per Minute RSB Radio System Bus RT R T Receiver Transmitter RTE Route RTE DATA Route Data RTO Rejected Take off RTU Radio Tuning Unit RUD Rudder RVR Runway Visual Range RVSR Reve...

Page 14: ...TRU Transformer Rectifier Unit TST Test TTC TRU Transfer Contactor U UNSCHD Unscheduled USB Upper Side Band USG United States Gallons UTIL Utility V V Volt VA Design Maneuvering Speed VB Design Speed...

Page 15: ...Visual Meteorological Conditions VNAV Vertical Navigation VOL Volume VOLT Voltage VOR VHF Omnidirectional Range Station VORTAC VOR and TACAN Co located V L VOR Localizer VSI Vertical Speed Indicator W...

Page 16: ...ABBREVIATIONS CONT D Y YD Y D Yaw Damper Z ZFW Zero Fuel Weight AIRPLANE GENERAL Rev 2A Apr 11 2005 Flight Crew Operating Manual CSP 700 5000 6 Volume 2 01 10 12...

Page 17: ...m Kilograms 2 205 lb Kilometers 0 6214 0 54 miles nautical miles Km hr 0 54 0 6214 knots mph Knots 1 151 1 852 mph km hr kPa 0 145 psi Liters 0 2642 0 22 USG Imperial gal Meters 3 281 ft Meters 10 76...

Page 18: ...8 0 249 8 251 6 253 4 255 2 76 1 77 2 77 8 78 3 78 9 170 171 172 173 174 338 0 339 8 341 6 343 4 345 2 59 4 58 9 58 3 57 8 57 2 75 74 73 72 71 103 0 101 2 99 4 97 6 95 8 31 7 31 1 30 6 30 0 29 4 25 24...

Page 19: ...attention is given to surface finishes protection against corrosion and to external surface smoothness throughout the airplane Sealing requirements include environmental sealing protection of faying s...

Page 20: ...02 3 07 m 94 ft 0 in 28 65 m 13 ft 4 in 4 06 m 8 ft 10 in 2 70 m 42 ft 7 in 12 98 m 25 ft 6 in 7 77 m 96 ft 9 in 29 49 m 83 ft 9 in 25 53 m AIRPLANE GENERAL Rev 2A Apr 11 2005 Flight Crew Operating Ma...

Page 21: ...ane 2 5 Spar locations Front 14 0 Rear 67 0 Flaps 3 per side Single Slotted Fowler Flaps Slats 4 L E segments per side Ground spoilers 2 per side Multi function spoilers 4 per side Horizontal tail sur...

Page 22: ...e fuselage 1022 sq ft 94 95 sq m Horizontal tail area Gross 245 sq ft 22 76 sq m Vertical tail area Gross 186 sq ft 17 28 sq m Doors Passenger door LH fwd Height to sill one step below the floor line...

Page 23: ...f installed FGF0110_003 VHF COMM 3 SATCOM WARNING Personnel should not stand nearby and in front of the radar antenna when it is transmitting When the antenna is not scanning the danger increases GLID...

Page 24: ...VISUAL EYE REFERENCES FOR GROUND OPERATION FGF0110_004 AIRPLANE GENERAL Rev 3 Apr 25 2005 Flight Crew Operating Manual CSP 700 5000 6 Volume 2 01 10 20...

Page 25: ...ng angle 3 slip Dry runway Slow continuous turn Max A C weight AFT CG 40 ft 4 in 12 30 m 56 ft 6 in 17 24 m 128 ft 2 in 39 07 m 14 ft 0 in 4 26 m 65 ft 4 in 19 92 m 52 ft 5 in 15 97 m 44 ft 9 in 13 64...

Page 26: ...TURNING RADII Minimum paving width for 180 turn 65 ft 19 92 m TURNING RADII SCHEMATIC AIRPLANE GENERAL Rev 3 Apr 25 2005 Flight Crew Operating Manual CSP 700 5000 6 Volume 2 01 10 22...

Page 27: ...JET EXHAUST SINGLE ENGINE GROUND IDLE THRUST GF0110_008 AIRPLANE GENERAL Rev 3 Apr 25 2005 Flight Crew Operating Manual CSP 700 5000 6 Volume 2 01 10 23...

Page 28: ...JET EXHAUST SINGLE ENGINE TAKE OFF THRUST GF0110_009 AIRPLANE GENERAL Rev 3 Apr 25 2005 Flight Crew Operating Manual CSP 700 5000 6 Volume 2 01 10 24...

Page 29: ...JET EXHAUST TWO ENGINE GROUND IDLE THRUST GF0110_010 AIRPLANE GENERAL Rev 3 Apr 25 2005 Flight Crew Operating Manual CSP 700 5000 6 Volume 2 01 10 25...

Page 30: ...JET EXHAUST TWO ENGINE TAKE OFF THRUST GF0110_011 AIRPLANE GENERAL Rev 3 Apr 25 2005 Flight Crew Operating Manual CSP 700 5000 6 Volume 2 01 10 26...

Page 31: ...E SUPPORT NYLON PLUG JACK PAD JACKING POINT SUPPORT BEAM REAR FUSELAGE SUPPORT LEGEND GF0110_012 The nose jacking point is located on the fuselage centerline Gear jacking points are also provided for...

Page 32: ...onnecting the nose wheel steering torque links The Aircraft Maintenance Manual Chapter 09 has a detailed description of towing operations NOTE Disconnecting the nose wheel steering torque links is rec...

Page 33: ...RLESS REAR GATE CRADLE Ground Locking Safety Pins Ground safety locks are provided for the nose and each main gear gear doors and for the Ram Air Turbine RAT Refer to the applicable chapter for the sa...

Page 34: ...ing procedures are located in the Aircraft Maintenance Manual Chapter 10 MOORING ATTACHMENT POINTS SCHEMATIC MAIN AND NOSE AREAS TAIL AREA MOORING ADAPTER PLATE JACKING PAD TIE DOWN RING GF0110_014 30...

Page 35: ...seats provide adjustments fore and aft inboard outboard lateral adjustment J track height and armrest position GF0110_015a AIRPLANE GENERAL Rev 12 Aug 14 2006 Flight Crew Operating Manual CSP 700 500...

Page 36: ...e seat laterally to its fully inboard position NOTE There is no mechanical lock to keep the seat in its position until you move it forward Keeping the seat in its fully inboard position raise the fore...

Page 37: ...d post to enable seat adjustment for correct eye to wheel height FRONT VIEW TOP VIEW The support bracket is not shown GF0110_016 PILO T S SIG HT LINE CO PILO T S SIG HT LINE NOTE AIRPLANE GENERAL Rev...

Page 38: ...t to control the trim from each control wheel Autopilot Flight Director Touch Control The Touch Control Switch TCS is located on the control wheel It enables the pilot to maneuver the airplane without...

Page 39: ...L 1 2 ELT FOR AVIATION EMER USE ONLY UNAUTHORIZED OPERATION PROHIBITED ON ARM RESET L HYD SOV HYDRAULIC CLOSED L HYD SOV CLOSED HYDRAULIC ELECTRICAL ON OFF AUTO ON OFF ON OFF AUTO ON OFF AUTO 1B 3A 3B...

Page 40: ...HMENT POWER RESERVOIR LH ENG APU RH ENG SYSTEM ON TANK LO PUMP ON LO OIL VLV OPEN LO OIL VLV OPEN LO OIL VLV OPEN PRINT MAINT REPORT DATA UPLOAD DOWNLOAD DAU 1A DAU 1B DAU 2A DAU 2B DAU 3A DAU 3B DAU...

Page 41: ...ing Handwheel 4 3 1 2 HEADSET PANEL FLASHLIGHT FLASHLIGHT Indicates Chapter in which information on item may be found 8 6 17 15 STS GS TK SYSTEM SELECT FROM TO WPT ON OXYGEN MASK RESET TEST N PUSH 100...

Page 42: ...r Switch 3 Clock 4 Air Conditioning Gasper 7 10 2 11 1 2 3 4 CIRCUIT BREAKER SYSTEM 1 2 AFCS AIR COND PRESS APU BLEED CAIMS COMM DOORS ELEC ENGINE FIRE FLT CONTROLS FUEL BRT STALL PUSHER ON OFF SEL DT...

Page 43: ...ERING AT SEA LEVEL AT 87 700 LB 240 AT 20 000 FT AT 78 600 LB 250 VMO BELOW 8 000 FT 300 VMO 8 000 TO 30 267 FT 340 MMO 30 267 FT TO 35 000 FT 0 89 MMO AT 47 000 FT 0 858 MMO AT 51 000 FT 0 842 VLO EX...

Page 44: ...tem Anti Ice System Electrical System AC and DC Fuel System Flight Controls Hydraulics Airplane Status Information and the following synoptic pages 11 11 18 3 12 10 15 10 2 2 7 12 10 13 OIL QTY QTS EN...

Page 45: ...CRANK AUTO ENG START AUTO WING XFER OFF AUTO AFT XFER OFF ON WING FEED INHIBIT AUX PUMP OFF PRI PUMP OFF L RECIRC OFF L WING FEED INHIBIT AUX PUMP OFF PRI PUMP OFF R RECIRC OFF R XFEED SOV FAIL OPEN...

Page 46: ...1 4 3 MASTER WARNING CAUTION WARNING CAUTION ROLL SPLRS CPLT CONT ROLL SEL CPLT ROLL RAD BARO MINIMUMS NAV SCR BARO SET PUSH STD HPa IN RAD BARO MINIMUMS NAV SCR BARO SET PUSH STD HPa IN SPD PUSH CHG...

Page 47: ...ALT 118 00 131 27 TEMP 1 131 10 112 00 1605 ANT 620 0 REL NORMAL 2000 15423 LV COM1 NAV1 ATC TCAS ADF1 TCAS DSPY 1 HF1 NB MEMORY 1 STANDBY ALT 118 00 131 27 TEMP 1 131 10 112 00 1605 ANT 620 0 REL NOR...

Page 48: ...VERING AT SEA LEVEL AT 87 700 LB 240 AT 20 000 FT AT 78 600 LB 250 VMO BELOW 8 000 FT 300 VMO 8 000 TO 30 267 FT 340 MMO 30 267 FT TO 35 000 FT 0 89 MMO AT 47 000 FT 0 858 MMO AT 51 000 FT 0 842 VLO E...

Page 49: ...sher Switch 3 Clock 4 Air Conditioning Gasper 7 10 2 11 1 2 3 4 CIRCUIT BREAKER SYSTEM 1 2 AFCS AIR COND PRESS APU BLEED CAIMS COMM DOORS ELEC ENGINE FIRE FLT CONTROLS FUEL STALL PUSHER ON OFF SEL DT...

Page 50: ...oice Recorder 6 Cockpit Printer If installed 6 6 3 COCKPIT VOICE RECORDER MICROPHONE MONITOR TEST ERASE STATUS HEADPHONE PASSENGER OXYGEN CLOSED OVERRIDE NORMAL FIRST AID TEST PORT PASS ON OFF FAULT L...

Page 51: ...y which opens outwards and downwards turns on two brackets attached to each side of the airstairs and hinge points in the fuselage Handrails are attached to each side of the airstairs and the fuselage...

Page 52: ...or the door structure which hangs below the airstairs when open The airstairs are hinged to the airplane via two hinges and two pins The handrails are attached to the fuselage and the airstairs They s...

Page 53: ...il the G locks engage Once the locks are in and the flap is shut the pressure holds the flap firmly shut The vent flap is opened by the lockshaft mechanism as the G locks are disengaged to release any...

Page 54: ...tion the handles are held in position with spring tension When the handles are moved out of the locked position the spring assists in lifting the door and reduces the load on the handles The internal...

Page 55: ...off by the DOOR switch installed next to the main passenger door EXTERNAL DOOR SWITCH ACCESS PANEL DOOR OPERATING SWITCH DOOR OPERATION PUSH IN FLAP TO GRASP HANDLE LIFT HANDLE FULL UP PULL DOOR OUT...

Page 56: ...DLE DOWNWARDS TO STOW Internal Door Operation To open the passenger door internally OPERATE DOOR HANDLE FROM THE LOCKED POSITION DOOR MOVES INWARD AND UPWARD PUSH DOOR OUT TO OPEN To close the passeng...

Page 57: ...Y EXIT DOOR GF0110_036 Two lower hook fittings and two upper latch fittings position the door in the door opening Three stop fittings on each side of the door and surround structure react to the press...

Page 58: ...r is lifted inwards away from the door opening QUICK RELEASE LATCH MECHANISM HAND GRIP GF0110_038 To unlatch the emergency exit door from the exterior the upper push plate vent flap is depressed to di...

Page 59: ...om over travel and striking the belly fairing using two door to fairing mounted lanyards The door locking mechanism is capable of operation only from outside of the airplane AFT EQUIPMENT BAY DOOR SCH...

Page 60: ...ch handle is flush fitting and is secured by an integral push trigger which when depressed releases the handle to the free open position The door is secured by returning the handle flush with the door...

Page 61: ...an emergency exit The door moves inward and upward to a stowed position above and clear of the door aperture DOOR HANDLE RECESS PUSH TRIGGER OUTER HANDLE CARGO DOOR OPEN STOWED POSITION GF0110_043 The...

Page 62: ...l the handle until the outer handle trigger latches into the trigger mechanism and the handle is stowed into the recessed housing OPENING THE BAGGAGE DOOR EXTERNALLY Press the trigger button to releas...

Page 63: ..._045 SERVICE DOORS Passenger Door The passenger door is monitored by three proximity sensors to determine the locked and handle stowed position Proximity sensors one at each location are located on th...

Page 64: ...indication The LGECU combines the status of the aft equipment bay door with the status of the maintenance hatches to produce a single EICAS indication The maintenance hatches that are monitored are R...

Page 65: ...to indicate that the applicable emergency exit door is not in position SMALL SERV DOORS Comes on to indicate that any one or more of the small service doors are not closed LARGE SERV DOORS Comes on t...

Page 66: ...AIRPLANE GENERAL Rev 12 Aug 14 2006 Flight Crew Operating Manual CSP 700 5000 6 Volume 2 01 10 62 THIS PAGE INTENTIONALLY LEFT BLANK...

Page 67: ...AKER SYSTEM 1 2 SYSTEM CIRCUIT BREAKER AFCS AIR COND PRESS APU BLEED CAIMS COMM DOORS ELEC ENGINE FIRE FLT CONTROLS FUEL PAX DOOR MOTOR 1 1 CB DOORS SYSTEMS AV BATT DCPC IN BRT AIRPLANE GENERAL EMS CI...

Page 68: ...AIRPLANE GENERAL EMS CIRCUIT PROTECTION Rev 2A Apr 11 2005 Flight Crew Operating Manual CSP 700 5000 6 Volume 2 01 20 2 THIS PAGE INTENTIONALLY LEFT BLANK...

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