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FLIGHT CREW BD-100-1A10 Operating Manual

FLIGHT CREW BD-100-1A10 Manual Online:

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FLIGHT CREW BD-100-1A10 User Manual
FLIGHT CREW BD-100-1A10 User Guide
FLIGHT CREW BD-100-1A10 Online Manual

Text of FLIGHT CREW BD-100-1A10 User Guide:

  • FLIGHT CREW BD-100-1A10, AUTOMATIC FLIGHT CONTROL SYSTEM Volume 2 Flight Crew Operating Manual Sep 14/2005 04-01-26 CSP 100-6 REV 4 PFD MESSAGES (Cont) 16. LNV1 LNV2 LOC1 LOC2 VOR1 VOR2 White Navigation or approach mode — armed (annunciator in the lateral arm field, by identifying nav source) Green Navigation or approach mode — capture/tracking (in the later capture field by identifying the nav source) 17. GS White Glideslope mode — armed (announced in the vertical arm field) Green Glideslope mode — captured (in the vertical capture fiel

  • FLIGHT CREW BD-100-1A10, NAVIGATION Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6 17-01-11 TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) (Cont) TCAS VOICE RELATED AURAL ALERTS VOICE MESSAGE MEANING Climb, Climb Climb at a nominal 1500 fpm Climb, Crossing Climb Same as Climb, Climb, aircraft’s flight path will cross the flight path of the intruder Increase Climb Follows a climb advisory. Climb rate should be increased to the rate on the VSI (nominally 2500 fpm) Adjust Vertical Speed, Adjust Reduce v

  • FLIGHT CREW BD-100-1A10, FLIGHT CONTROLS Volume 2 Flight Crew Operating Manual Sep 14/2005 10-01-02 CSP 100-6 REV 4 PRIMARY FLIGHT CONTROLS COMPONENTS AND OPERATION AILERONS AND MULTIFUNCTION SPOILERS The aileron control cable runs to both control wheels and both ailerons. The roll disconnect mechanism disconnects the pilots control wheel from the aileron circuit. When disconnected, the pilot controls the roll spoilers and the copilot controls both ailerons. Normally the aileron and roll spoilers are interconnected and there is a simultaneous and coordinated move- ment of all lateral control surfaces from either pilot station. Moving the control wheels also generat

  • FLIGHT INSTRUMENTS Volume 2 Flight Crew Operating Manual Dec 05/2006 11-02-18 CSP 100-6 REV 7 GRAPHICAL WEATHER (OPTIONAL) (Cont) WINDS/TEMPS IMAGE The WINDS ALOFT chart depicts forecast wind direction, wind speed and temperature at a specified altitude. Wind speed is indicated with the use of pennants and barbs on an arrow. The pennants represent 50 knots, barbs represent 10 knobs, an

  • FLIGHT CREW BD-100-1A10, NAVIGATION Volume 2 Flight Crew Operating Manual Sep 13/2004 17-01-24 CSP 100-6 REV 1 TERRAIN AWARENESS WARNING SYSTEM (TAWS) (Cont) MODE 6 — Altitude Callouts Mode 6 provides the following advisory alerts: transition through approach minimums, altitude callouts on approach and excessive bank angles. - Transition through the preset approach minimums, (APPROACHING DECISION HEIGHT or APPROACHING MINIMUMS), generates an aural “MINIMUMS, MINIMUMS” warning. The warning function is enabled between 1000 feet and 10 feet radio altitude or DH minimums and when the corrected altitude exceeds the MDA value by 200 fe

  • FLIGHT CREW BD-100-1A10, AIR CONDITIONING/PRESSURIZATION Volume 2 Flight Crew Operating Manual Sep 13/2004 02-04-12 CSP 100-6 REV 1 AIR SOURCE OFF The AIR SOURCE switch is in the OFF position resulting in no conditioned air entering the cabin BLEED OFF The L, R, and APU BLEEDs are OFF DITCHING ON The DITCHING switch/indicator has been selected ON. This closes the flow control valves and commands the outflow valve open for 100 seconds or 10 seconds after cabin differential pressure decreases below 1595 psid. The outflow valve then closes EMER DEPRESS ON Emergency depressuri

  • FLIGHT CREW BD-100-1A10, FLIGHT CONTROLS Volume 2 Flight Crew Operating Manual May 06/2005 10-02-14 CSP 100-6 REV 2 STALL PROTECTION SYSTEM (Cont) The ADCs supply primary Mach data to the SPS computer for Mach compensation of the aircraft’s stall margin. The SPS uses the above inputs to calculate the angle-of-attack trip points. The stick shaker activation and ignition activation are simultaneous. In the event of an AOA increase rate greater than 1 degree per second, the stall protection computer lowers the activation trip point. This prevents the aircraft’s pitching momentum from carrying i

  • FLIGHT CREW BD-100-1A10, FLIGHT CONTROLS Volume 2 Flight Crew Operating Manual Sep 13/2004 10-02-16 CSP 100-6 REV 1 CONTROLS AND INDICATIONS FLAP CONTROL LEVER EICAS TRIM STATUS DISPLAY CFO1005002_007 FLAPS VFE 210 VFE 210 VFE 175 10 20 30 0 CFO1001002_010 TRIM STAB AIL LWD RWD RUD L R NU ND 6.6

  • FLIGHT CREW BD-100-1A10, FLIGHT CONTROLS Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6 10-02-03 SECONDARY FLIGHT CONTROLS (Cont) HORIZONTAL STABILIZER TRIM The stabilizer trim can be moved manually by control wheel trim switches or automatically via computer-controlled inputs from the autopilot, spoilers, or flaps. Manual trim rates differ, depending on which channel is engaged. When the primary channel is engaged, the trim rate is a function of airspeed (mach). When the pitch trim secondary channel is engaged, the trim rate is a constant 0.2 d

  • FLIGHT CREW BD-100-1A10, LANDING GEAR Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6 15-01-17 LANDING GEAR INDICATIONS The EICAS landing gear indications provide the pilots increased situational awareness regarding the position and condition of the landing gear. LANDING GEAR DOWNLOCKED “SAFE”: ONE OF THE TWO REDUNDANT DOWNLOCK SENSORS DETECTS THAT THE GEAR IS DOWN AND LOCKED LANDING GEAR UP: UPLOCK SENSOR DETECTS GEAR UP AND BOTH DOWNLOCK SENSORS DETECT GEAR NOT DOWNLOCKED GEAR UP AND NO GEAR WARNING AND EITHER NO GEAR DISAGREE OR GEAR DISAGREE WITH HANDLE UP G

  • AIRPLANE GENERAL Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6 01-05-01 PASSENGER DOOR DESCRIPTION The passenger door is located on the left side of the aircraft in the forward section of the fuselage and is the primary entry and exit for the aircraft. The passenger door is attached to the fuselage by a goose-neck hinge at the centerline of the door. The door

  • FLIGHT CREW BD-100-1A10, AIR CONDITIONING/PRESSURIZATION Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6 02-04-07 CONTROLS AND INDICATIONS (Cont) TAKEOFF FROM AIRFIELD ABOVE 7850 FT AND LANDING FIELD ELEVATION ABOVE 7850 FT TAKEOFF FROM AIRFIELD LESS THAN 7850 FT AND LANDING FIELD ELEVATION ABOVE 7850 FT CFO0204002_007 ALTITUDE THROTTLES ADVANCED TAKEOFF ELEVATION 10 000 ft DESCENT RATE 300 fpm 7850 ft CABIN ASCENT RATE 300 fpm LANDING ELEVATION 9000 ft TIME A I R C R A F T C L I M B AIRCRAFT ALTITUDE MAX 45 000 ft > - DESCENT ft/MIN FOR > 10

  • FIRE PROTECTION Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6 09-01-03 FIRE PROTECTION SYSTEM OVERVIEW SCHEMATIC CFO0901002_002 ENGINE L ENG FIRE FIRE 2 ARMED 1 ARMED APU ON ON FIRE EXT IGNITIO N MACH HOLD AUTO SYN C N1 N2OFF EVENT OFF AUTO APR OFF R STARTER CRANK START OFF CRANK STA RT L STARTER R ENG FIRE FIRE 600 600 93.0 61.0 NI MACH H

  • AURAL/VISUAL ALERTS Volume 2 Flight Crew Operating Manual Sep 13/2004 03-03-06 CSP 100-6 REV 1 MESSAGES (Cont) MESSAGE MESSAGE SOUND AFT EQPT BAY DOOR TONE ALTITUDE ALERT TONE “APU FIRE” VOICE MESSAGE APU FIRE DET FAIL TONE APU FUEL SOV FAIL TONE APU GEN FAIL TONE APU GEN OVERLOAD TONE AUTOPILOT DISCONNECT TONE AUX HYD TEMP HIGH TONE LEFT (R) BATT FAIL TONE BATTERY BAY DOOR TONE LEFT

  • FLIGHT CREW BD-100-1A10, ICE AND RAIN PROTECTION Volume 2 Flight Crew Operating Manual May 06/2005 14-01-10 CSP 100-6 REV 2 CONTROLS AND INDICATIONS (Cont) ANTI-ICE SYNOPTIC PAGE The ANTI-ICE synoptic page is used to monitor the pneumatically operated anti-icing and ice detection systems. CFO0305002_009 CAS CKLST SKIP FRMT TFC ENTER ELEC FLT HYD L R ECS FUEL TR/WX SUMRY COM1 NAV1 ATC1/TCAS ADF1 HF1 COM3 COM2 118.000 108.00 7777 1799.5 118.000 118.000 118.000 118.0002.0000 190.0108.00118.000 STBY ABV TX 2.0000 AM DN UP CAB ALT CAB RATE APU RPM APU EGT FUEL QTY LBS TOTAL N2 OIL PRESS OIL TEMP FF PPH I T T N1 NU ND STAB AIL TRIM LWD RWD RUD GEAR FLAPS SPOILERS 7300 1000 0

  • FLIGHT CREW BD-100-1A10, AUTOMATIC FLIGHT CONTROL SYSTEM Volume 2 Flight Crew Operating Manual May 06/2005 04-01-14 CSP 100-6 REV 2 FLIGHT DIRECTOR VERTICAL MODES (Cont) PITCH MODE When pitch mode is selected, the flight director generates commands to hold the current pitch attitude. Selection of the Pitch Mode is automatic in the following cases: - Any other vertical mode has been deselected, either manually or automatically - Autopilot is engaged with the FD off - Flight Director is ON with no other vertical mode(s) selected - The SYNC button is pressed in go-around

  • AUTOMATIC FLIGHT CONTROL SYSTEM Volume 2 Flight Crew Operating Manual May 06/2005 04-01-22 CSP 100-6 REV 2 AUTOPILOT (Cont) 2 0 DUAL RVDT (A) (B) DUAL RVDT (A) (B) DUAL RVDT (A) (B) SINGLE RVDT SINGLE RVDT LVDT (ANALOG) LVDT (ANALOG) LVDT (ANALOG) LVDT (ANALOG) RDC CH A CH B FCU-2 FLAPS OVERRIDE (FROM FCU) 28VDC TRIM SELECT SWITCH RELAY PILOT MANUAL TRIM SWITCH COPILOT MANUAL TRIM SW

  • FLIGHT CREW BD-100-1A10, ICE AND RAIN PROTECTION Volume 2 Flight Crew Operating Manual May 06/2005 14-01-06 CSP 100-6 REV 2 ENGINE ANTI-ICE DESCRIPTION Each of the engine nacelle inlets are anti-iced with engine bleed-air. The left and right engine anti-icing systems are con- trolled by L (R) ENG switches on the ANTI-ICE control panel located on the center pedestal. COMPONENTS AND OPERATION NACELLE ANTI-ICING VALVES Nacelle anti-icing valves are located on top of each engine downstream of the high pressure duct. The valves are electrically operated and pneumatically controlled and incorporates a fail safe open feature. ENGINE NACELL

  • FLIGHT CREW BD-100-1A10, FLIGHT CONTROLS Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6 10-02-07 SECONDARY FLIGHT CONTROLS (Cont) FLAP CONTROL LEVER The FLAP control lever operates in one of four positions, (0, 10, 20, and 30) with detents at the 10 and 20 positions.To prevent inadvertent retraction of flaps from 30 to 0 in one motion during a go-around maneuver, a gate is located at the 10 position and must be pulled up slightly when retracting the flaps to 0. The lever is attached to dual RVDTs co-located with a flap lever dete

  • FLIGHT CREW BD-100-1A10, FLIGHT INSTRUMENTS Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6 11-01-11 AIR DATA SYSTEM DESCRIPTION Air data information is sensed by the pitot static system and total air temperature (TAT) probe. This data is processed by the air data computers (ADCs) and sent to the flight displays, IAPS, and several aircraft systems. Cockpit controls include the BARO SET knob, ADC REVERSION switch, several flight guidance panel (FGP) controls, and the reference speeds (REFS) menu settings. COMPONENTS AND OPERATION Airspeed information displayed on the PFD include: - Airspeed display - Reference speeds - Low/high

  • FLIGHT CREW BD-100-1A10, AIR CONDITIONING/PRESSURIZATION Volume 2 Flight Crew Operating Manual Sep 13/2004 02-04-02 CSP 100-6 REV 1 PRESSURIZATION (Cont) AUTOMATIC PRESSURIZATION MODES The following automatic pressurization modes are a function of the active IASC: - Pre-pressurization mode - Takeoff and return to base sequence - Climb mode -Cruise mode - Descent mode - Depressurization sequence on ground PRE-PRESSURIZATION MODE The pre-pressurization mode is activated on the ground when the thrust levers are advanced for takeoff. Pre-pressurizing the aircraft will allow the outflow valve to achieve a controlling position prior to takeoff to eliminate any noticeable pres- sure changes at take

  • FLIGHT CREW BD-100-1A10, FLIGHT INSTRUMENTS Dec 05/2006 Flight Crew Operating Manual Volume 2 REV 7 CSP 100-6 11-01-37 CONTROLS AND INDICATIONS (Cont) MULTIFUNCTION DISPLAYS (MFD) COM1 NAV1 ATC1/TCAS ADF1 HF1 COM3 COM2 118.000 108.00 1200 1799.5 118.000 118.000 118.000 118.000 2.0000 190.0108.00118.000 STBY ABV TX 2.0000 AM 25 25 CID DIRECT 3.0° 10000A 0 : 20 / 18325 12000B 95NM CID 95 NM 77 NM 0 : 20 IRK OSH 215 NM 0 : 59 KORD 339 NM 1 : 20 HDG 340 FMS2 340 UTC ° C 11 : 42 SAT -15 -5 ° C ISA TAS GS 250 254 30 FMS2 180NM FIX MFD CONTROL TR / WX / LX WX T-1.5A 2 4 W 3 0 33 N 3 6 DBQ ALO TNU NEBOR ANOSA CID IOW IA MXO 200 KCID 100 270 / 150 CFO1101002_005 FIRE 600 600 93

  • ELECTRICAL May 06/2005 Flight Crew Operating Manual Volume 2 REV 2 CSP 100-6 07-01-11 ELECTRICAL SYSTEM (Cont) CB5 LEFT DC POWER CENTER CIRCUIT BREAKER PANEL (TYPICAL) CB6 RIGHT DC-POWER CENTER CIRCUIT BREAKER PANEL (TYPICAL) 2345678 A C B 12 HF 1 PWR L ATS/ HYD SOLA PRI STAB MOTORL LDG L DCPC ESS BUS L SPC BAT BUS R DCPC ESS BUS AVNX ENGINE FIREX FCTL LIGHTS ELECTRICAL EXT BAG/ AFT B

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