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G450 Condensed Notes G U L F S T R E A M G 4 5 0 Condensed Notes Revision 4.0 T A B L E O F C O N T E N T S For corrections, suggestions, or to be added to the revision distribution list please email: [email protected] Thank you, G U L F S T R E A M G 4 5 0 Condensed Notes TABLE OF CONTENTS T A B L E O F C O N T E N T S A C R O N Y M N S ....................................................................... 3 S Y S T E M PAGE G E N E R A L ................................................................................... 4 D O O R S ........................................................................................ 4 L I G H T I N G .................................................................................. 4 F I R E P R O T E C T I O N .............................................................. 4 C O M M U N I C A T I O N S ............................................................ 5 E L E C T R I C A L ............................................................................. 5 A P U ............................................................................................... 6 P O W E R P L A N T ......................................................................... 7 F U E L ............................................................................................. 8 H Y D R A U L I C .............................................................................. 8 L A N D I N G G E A R ..................................................................... 9 F L I G H T C O N T R O L S ............................................................. 9 P N E U M A T I C S ........................................................................ 10 A I R C O N D I T I O N I N G ......................................................... 10 P R E S S U R I Z A T I O N .............................................................. 11 I C E A N D R A I N ...................................................................... 11 O X Y G E N .................................................................................... 12 F L O W S ...................................................................................... 12 P L A N E V I E W A V I O N I C S ................................................... 13 S O P ............................................................................................. 15 PLEASE EMAIL CORRECTIONS TO: [email protected] REV 4.0, 201909 P A G E 2 G U L F S T R E A M G 4 5 0 Condensed Notes TABLE OF CONTENTS S O U R C E S GSCP GROUND SERVICE CONTROL PANEL HOPS HARDOVER PROTECTION SYSTEM GULFSTREAM HMG HYDRAULIC MOTOR GENERATOR FLIGHT SAFETY INTERNATIONAL HUD HEAD UP SYSTEM www.CODE7700.com IDG INTEGRATED DRIVE GENERATOR IVAN LUCIANI I-NAV INTEGRATED NAVIGATION IRU INERTIAL REFERENCE UNIT LAN LOCAL AREA NETWORK A C R O N Y M S LEER LEFT ELECTRONIC EQUIPMENT RACK LPV LOCALIZER PERFORMANCE WITH VERTICAL GUIDANCE LRU LINE REPLACEABLE UNIT ACC AIR CONDITIONING CONTROLLER MAU MODULAR AVIONICS UNIT ACM AIR CYCLE MACHINE MCDU MULTIFUNCTION CONTROL DISPLAY UNIT ACP AUDIO CONTROL PANEL MWS MONITOR AND WARNING SYSTEM ACS AIR CONDITIONING SYSTEM NBPT NO BREAK POWER TRANSFER ADC AIR DATA COMPUTER ND NAVIGATION DISPLAY ADM AIR DATA MODULE NIC NETWORK INTERFACE CARD ADS AIR DATA SYSTEM PDP POWER DISTRIBUTION PANEL AUTOMATIC DEPENDENT SURVEILLANCE POP PILOT OVERHEAD PANEL AEER AUX ELECTRONIC EQUIPMENT RACK PTU POWER TRANSFER UNIT AFCS AUTOMATIC FLIGHT CONTROL SYSTEM REER RIGHT ELECTRONIC EQUIPMENT RACK AGM ADVANCED GRAPHICS MODULE RVDT ROTARY VARIABLE DIFFERENTIAL TRANSDUCER ASC AIRCRAFT SERVICE CHANGE SAV STARTER AIR VALVE ASCB AVIATION STANDARD COMMUNICATIONS BUS SEP STANDBY ELECTRICAL POWER ATN AERONAUTICAL TELECOMMUNICATIONS NETWORK SFD STANDBY FLIGHT DISPLAY BAC BLEED AIR CONTROLLER SVO START VALVE OPEN BAS BLEED AIR SYSTEM SVS SYNTHETIC VISION SYSTEM BIT BUILT-IN TEST SV-PFD SYNTHETIC VISION PRIMARY FLIGHT DISPLAY BITE BUILT-IN TEST EQUIPMENT TCS TOUCH CONTROL STEERING BPCU BUS POWER CONTROL UNIT TLA THRUST LEVER ANGLE BTMS BRAKE TEMP MONITORING SYSTEM TROV THRUST RECOVERY OUTFLOW VALVE CAS CREW ALERT SYSTEM VGP VNAV GLIDE PATH CCD CURSER CONTROL DEVICE VSD VERTICAL SITUATION DISPLAY CDU CONTROL DISPLAY UNIT CMC CENTRAL MAINTENANCE COMPUTER CMF COMMUNICATIONS MANAGEMENT FUNCTION CPC CABIN PRESSURE CONTROLLER CPCP CABIN PRESSURE CONTROL PANEL CPOP CO-PILOT OVERHEAD PANEL CPSP CABIN PRESSURE SELECTOR PANEL NOTES CPIP CABIN PRESSURE INDICATOR PANEL CSD CONSTANT SPEED DRIVE DAU DATA ACQUISITION UNIT DC DISPLAY CONTROLLER DMU DATA MANAGEMENT UNIT DU DISPLAY UNIT EBDI ELECTRONIC BEARING AND DISTANCE INDICATOR ECS ENVIRONMENTAL CONTROL SYSTEM ECU ELECTRONIC CONTROL UNIT EDS ELECTRONIC DISPLAY SYSTEM EDM EMERGENCY DESCENT MODE EEC ELECTRONIC ENGINE CONTROL EVM ENGINE VIBRATION MONITOR EVS ENHANCED VISION SYSTEM FGCP FLIGHT GUIDANCE CONTROL PANEL FGC FLIGHT GUIDANCE COMPUTER FCOC FUEL COOLED OIL COOLER FPV FLIGHT PATH VECTOR FMU FUEL METERING UNIT FSECU FLAP/STAB ELECTRONIC CONTROL UNIT FQSC FUEL QUANTITY SIGNAL CONDITIONER FWC FAULT WARNING COMPUTER GCU GENERATOR CONTROL UNIT GP GUIDANCE PANEL PLEASE EMAIL CORRECTIONS TO: [email protected] REV 4.0, 201909 P A G E 3 G U L F S T R E A M G 4 5 0 Condensed Notes TABLE OF CONTENTS ▪ STROBE ▪ THE SYSTEM DEFAULTS TO THE TOP STROBE LIGHT 1 G E N E R A L LIGHT ▪ IT ONLY GOES TO THE BOTTOM STROBE IF THERE IS DIMENSIONS: FAULTS A PROBLEM WITH THE TOP STROBE ▪ LENGTH 89’ 3” ▪ A TRIPPED FAULT INDICATOR COULD BE A BAD TOP ▪ WINGSPAN 77’ 4” BULB, A MOMENTARY ELEC SPIKE, OR A HARD ▪ TAIL HEIGHT 25’ 2” LANDING ▪ WHEELBASE 39’ 1” X 13’ 8” ▪ ANN LIGHT ▪ TESTS ALL BULBS EXCEPT 5: TEST - FIRE HANDLES (2) ▪ MIN TAXI STRIP FOR 1800 TURN 55’ 3” - FUEL CONTROL SWITCHES (2) WEIGHTS: - PAX OXYGEN ▪ MAX RAMP 75,000 LBS (ASC 016) ▪ CABIN RATE OF CHANGE – FULL DESCENT ▪ MAX TAKEOFF 74,600 LBS (ASC 016) ▪ MAX LDG 66,000 LBS / 58,500 LBS (ASC 007C) 4 F I R E P R O T E C T I O N ▪ MAX ZERO FUEL 49,000 LBS / 48,000 LBS (ASC 008) ▪ COMPONENTS ▪ SMOKE DETECTION ▪ BAG COMP SPEEDS: ▪ VMO / MMO 340 KTS / M.88 MT ▪ SMOKE EVAC HANDLE ▪ DEFLATES BAG DOOR SEAL ▪ VTURB >10,000 FT 270 KTS / 0.75 MT ▪ VTURB <10,000 FT 240 KTS ▪ ENG FIRE DETECTION ▪ TWO FIRE LOOPS ▪ FLAPS 100/200/390 250 / 220 / 180 KTS (0.60 MT) ▪ FIRE DETECTOR CONTROL UNIT ▪ MINIMUM MANEUVERING SPEEDS FLAPS 00/100/200/390 200 / 180 / 160/ VREF +5 KTS ▪ PYLON OVERHEAT ▪ 2500F ▪ VLE / VLO / EMERG 250 / 225 / 175 KTS (0.70 MT) ▪ APU FIRE DETECTION ▪ SINGLE LOOP ▪ VA 206 KTS ▪ SENSES FIRES AND ▪ TIRE LIMIT 195 KTS FAULTS ▪ VMCG / VMCA / VMCL 109 / 106 / 99 KTS ▪ PAX COMP AND TAIL ▪ THERMAL SWITCHES ▪ INOP TRIM (MACH/ELEC) 0.75 MT COMP O’HEAT ▪ 1500F ▪ INOP STAB / JAMMED ELEV 270 KTS / 0.75 MT ▪ PAX COMP ▪ LEER, REER, AEER ▪ INOP YD ABOVE 20,000 FT 210 KTS MINIMUM AND TAIL ▪ FWD, L AFT, CENTER AFT, R AFT FLOOR ▪ MAX DEMONSTRATED X-WIND 24 KTS COMP O’HEAT ▪ AFT EQUIPMENT ALTITUDES: DETECTION APU: ▪ MAX OPERATING: 45,000 FT ▪ FIRE ▪ SEALED TUBE ▪ HELIUM GAS ▪ INOP YD AND MACH TRIM 41,000 FT DETECTION 0 0 ▪ FLAPS 10 / 20 25,000 FT 0 ▪ HIGH GAS ▪ LDG GEAR / FLAPS 39 20,000 FT PRESSURE ▪ MAX FIELD ELEV 14,500 FT / 15,000 FT (ASC 068) ▪ HEAT PRODUCES HIGH ▪ SENSOR AUTO-SHUTDOWN PRESSURE ▪ LOW GAS 2 D O O R S PRESSURE ▪ LOOKS FOR RUPTURED ▪ EMERGENCY EXITS ▪ PRIMARY ▪ MAIN ENTRANCE DOOR SENSOR ▪ TUBE NO AUTO-SHUTDOWN (LAND EVAC) ▪ CABIN WINDOWS (4) ▪ FIRE BELL ▪ SECONDARY ▪ BAGGAGE DOOR (GND) ▪ APU FIRE TEST ▪ 6 LIGHTS, 2 CAS MSGs 3 L I G H T I N G APU FIRE ▪ SUBSYSTEMS ▪ FLIGHT DECK LIGHTING APU FIRE DETECTOR FAIL ▪ CABIN LIGHTING ▪ A TEST WILL NOT SHUTDOWN THE APU ▪ SERVICE COMPARTMENT LIGHTING ▪ FIRE BELL WILL ONLY SOUND ON THE GND ▪ EXTERIOR LIGHTING ▪ BEFORE STARTING THE APU CONFIRM ▪ EMERGENCY LIGHTING FIRE BOTTLE DISCHARGE, L-R NOT DISPLAYED ▪ EXTERIOR ▪ BEACON, STROBE, NAV, ICE INSP, LOGO, RAMP, ESSENTIAL AC-BUS FAIL LIGHTING LANDING, PULSE, TAXI, WING TIP TAXI, AND WHEEL ENG: WELL LIGHTS ▪ SENSORS ▪ AT THE 7TH AND 12TH STAGES ▪ STROBE LIGHT – 2 IN EACH LOCATION MOUNTED ON RAILS ▪ AT THE IDG ▪ STROBE LIGHT FAULT INDICATOR ▪ AT THE BLEED AIR DUCT ▪ SHEATHS OF STAINLESS NAV LIGHTS - 2 IN EACH LOCATION ▪ FRONT ENG MOUNT ▪ TAXI LIGHTS (3) – AUTO OFF ON GEAR RETRACTION STEEL SURROUNDED BY GLASS OXIDE MATERIAL. ▪ ENG ANTI-ICE DUCT (L ENG) ▪ LANDING LIGHTS – AUTO OFF AT 18000’ HEAT AFFECTS CURRENT ▪ L ENG LOOP A, R ENG LOOP B – L ESS DC ▪ LANDING LIGHT OPERATION LIMITED TO 5 ▪ L ENG LOOP B, R ENG LOOP A – R ESS DC MINUTES WHEN ON THE GND ▪ EMERGENCY ▪ OVERWING EGRESS, UNDERWING EGRESS, EMERG ▪ FIRE HANDLE ▪ FUEL – AT THE TANK, FUEL SHUTOFF VALVE LIGHTING LIGHT BATTERIES, EMERG CONTROL SWITCHES, SHUTS OFF: ▪ HYD – HYD SHUTOFF VALVE BETWEEN THE HYD AND MAIN ENTRANCE DOOR EMERG LIGHTS RESERVOIR AND THE HYD PUMP ▪ WHEN ON E-BATTS ONLY THE MASTER LIGHTING ▪ ELEC – AT THE IDG CONTROL KNOB FUNCTIONS PLEASE EMAIL CORRECTIONS TO: [email protected] REV 4.0, 201909 P A G E 4 G U L F S T R E A M G 4 5 0 Condensed Notes TABLE OF CONTENTS ▪ 2 FIRE BOTTLES ▪ HALON 1301 (CF3Br) ▪ CVR ▪ 120 MIN (L AND R) ▪ 600 PSI AT 700F ▪ COCKPIT VOICE RECORDER UNIT – TAIL COMP – SOLID ▪ “BOTTLE DISCHARGE” CAS WHEN AT 200 PSI STATE DIGITAL MEMORY, WATER ACTIVATED BEACON – ▪ RIGHT BOTTLE IS #1 SHOT INTERNAL BATTERY ▪ LEFT BOTTLE IS #2 SHOT ▪ 2.5 G IMPACT SWITCH ▪ INTENTIONAL DISCHARGE: INTO THE ENG ▪ DFDR ▪ 25 HRS OF DATA – TAIL COMP NACELLE ▪ DFR/CMC EVENT SWITCH ON OVERHEAD ▪ THERMAL DISCHARGE: INTO THE TAIL (RECORDS -30 SEC + 1 MIN) COMPARTMENT ▪ ELT ▪ AEER ▪ L/R ENGINE ▪ 121.5 MHz, 243.0 MHz, and SAT FREQ 406.025 MHz FIRE TEST ▪ 72 HR TRANSMIT TIME ▪ LAT LONG INTERFACE FROM IRS “EIGHT LIGHTS” 6 E L E C T R I C A L 6 LIGHTS, 2 CAS MSGs: ▪ LOOP A LIGHTS (2) LOOP B ▪ MASTER WARN LIGHTS (2) ▪ FIRE HANDLE LIGHTS (1) ▪ L/R FUEL CONTROL SWITCH LIGHTS (1) ▪ THREE-CHIME AURAL WARNING TONE ▪ ENGINE FIRE CAS MESSAGE (1) ▪ ▪ ENGINE FIRE LOOP ALERT CAS MESSAGE (1) ▪ ENGINE FIRE DETECTION FAULT TEST “EIGHT LIGHTS” NOTE: CHECKS THE FAULT DETECTION EIGHT (8) AMBER LIGHTS: CIRCUIT OF THE FIRE ▪ TEST LEGEND IN THE FAULT TEST SWITCH ▪ 1 HMG (SEP) ▪ G450, 5 Kva, 115 V, 400 HZ, 3 PHASE DETECTION CONTROL ▪ FAULT LEGENDS IN THE LEFT/RIGHT LOOP A/B AC UNIT, NOT THE LOOPS.
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