CRK 7

The rotary FORMAT knob can be used to select one of the following navigation formats. MFD format selection. Navaid sector map. Navigation source selection. Cross-side navigation data and course display.

FMS Vertical Navigation. In advisory VNAV, the FMS provides steering commands on the Primary Flight Display (PFD) of the vertical deviation. With NAV selected on the FCP , FMS altitude constraint readout is presented as a white digital readout above the altitude tape. The FMS has two available modes of vertical navigation (VNAV) − advisory and coupled. When the airplane over ies the TOD point, the snow ake tracks upward on the scale.

CRK - AIR CONDITIONING - Single pack operation with the APU... Is recomended. Is prohibited except for takeoff, approach, go-around and landing phases of Flight. Is prohibited except for cruise. Is mandatory.

CRK - AIR CONDITIONING - The maximum altitude for dual pack operation with the APU as the bleed source is. 13.000 feet. 25.000 feet. 15.000 feet. 31.000 feet.

CRK - AIR CONDITIONING - CABIN AL T WARN HI... Is an Advisory Msg to indicate a landing hight altitude (above 8.000'). Is an Status Msg to indicate a landing hight altitude (above 8.000'). Is an Caution Msg to indicate a landing hight altitude (above 8.000'). Is an Warning Msg to indicate a landing hight altitude (above 8.000').

CRK - AIR CONDITIONING - Failure of the ground valve in open position in flight will be indicated by an: OVBD COOL (RED). OVBD COOL (AMBER). GND VALVE (STATUS). GND VALVE (AMBER).

CRK - COMMUNICATIONS - Which of the following communication system is no longer present in the CRK?. HF System. PA System. Cockpit Voice Recorder. Back Up Radio Tuning Unit.

CRK - COMMUNICATIONS - How many pages has the CRK´s RTU?. 2; Top Level and Main. 2; Main and Secondary. 3; Top Level, Main Page, Preset page. 3; Main Level, Secondary; Misc page.

CRK - COMMUNICATIONS - How is the FMS tune inhibit function selected on the CRK?. Pressing control+alt+sup. By a pushbutton on the tunning select panel. By a rotary selector. This function does not exist in the CRK.

CRK - COMMUNICATIONS - Where is the BTU in the CRJ 1000?. There is not any BTU. On the 3rd page of RTU1. On the 2nd page of RTU2. A new tuning panel replaces backup tuning unit and panel.

CRK - COMMUNICATIONS - Ground Crew Interphone. There are three external interphone stations that enable the users to communicate on the service interphone system. There is one interphone station positioned in the refuel/defuel panel. All the positions are disabled in ight. There are ve external interphone stations that enable the users to communicate on the service interphone system.

CRK - COMMUNICATIONS - Audio Control Panels. Selecting VOICE on the VOICE/BOTH switch enables the station Morse code identi er from VOR, ILS and ADF received signals. The MASK/BOOM switch gives the ight crew a choice between headset with boom mike, or the oxygen mask microphone. When the pilot’s EMER/NORM switch is set to EMER, the pilot’s headset is connected directly to NAV 2 navigation radio and VHF 2 communication radio. Two audio control panels, located in the centre pedestal, provide the ight crew access to the audio system.

CRK - CRK ICE & RAIN - Air Data Sensor (ADS) anti-ice system. On ground the controllers automatically supply full power to all the air data probes and sensors. The ground mode has three operational heating modes, automatic, half and full. In the ight mode, the automatic control function is completely independent from the control switches. On ground automatic mode is not functional when the airplane is being powered by the APU generator or external power.

CRK - CRK ICE & RAIN - Windshield wiper system. is designed to remove rain and/or snow from the pilot and co-pilot windshields at airplane speeds up to 220 kts. both wipers will operate in the same mode when selected from either panel. If each selector is set to a different mode, the fastest selection overrides the slowest selection. If one wiper system fails, the remaining system will stop for balance reasons.

CRK - CRK ICE & RAIN - A WING OVHT warning (red). Indicates failure of both channels of left or right outboard wing temperature sensors with wing anti−ice selected on. Indicates that respective wing anti−ice valve has failed closed or a low temperature has been detected. Indicates that the wing cross−bleed valve has failed closed. Indicates that an overheat condition has been detected by at least one of the inboard wing skin temperature sensors.

CRK - CRK ICE & RAIN - The L or R COWL A/I DUCT warning (red). Indicates that respective cowl anti−ice valve failed to close when selected off. Indicates that a bleed leak is detected by the leak pressure transducer in the cowl anti−ice duct. Indicates that the respective cowl anti−ice valve failed to open when selected on. Indicates that the respective T2 heater has failed.

CRK - CRK ICE & RAIN - T2 Sensor Probe. is mounted on the engine fan. A test of the T2 heater function is automatically performed by the FADEC after engine start on ground. is used to provide engine air inlet temperature data to the FADEC. Power to the probe heating element is controlled by the EICAS.

CRK - CRK ICE & RAIN - A test of the T2 heater function is automatically performed by the FADEC after engine shutdown on the ground. Following left engine shutdown, electrical power must be maintained on the airplane for at least one minute. If the T2 heater test fails on one channel, the respective L ENG TAT HEAT or R ENG TAT HEAT caution message will be displayed on the EICAS. Following a successful test the FADEC will not attempt to energize the T2 heater. The FADEC will verify that the T2 heater is functional by energizing the heater and looking for an appropriate temperature rise during a 30 second period.

CRK - INDICATING / RECORDING SYSTEMS - What indication appears if we advance thrust levers to MAX POWER during take off on the CRK (Optional)?. MAX appears inside N1 arch. APR appears inside N2 arch. MAX Power advisory message appears on EICAS. N1 exceedance on EICAS#1.

CRK - INDICATING / RECORDING SYSTEMS - What is the message that replaced No starter Cutout message on the CRK?. L/R Starter ON. L/R Starter No cut out. L or R Strt Vlv Open. No Cut Out.

CRK - INDICATING / RECORDING SYSTEMS - When will you hear the "Too low gear" aural warning?. If any landing gear is not down and locked and with radio altitude less than 500 ft AGL. Whit the radio altitude less than 500 ft AGL and the indicated airspeed at less than 190 knots. If any landing gear is not down and locked and the indicated airspeed less than 190 knots. If any landing gear is not down and locked with radio altitude less than 500 ft AGL and the indicated airspeed at less than 190 knot.

CRK - INDICATING / RECORDING SYSTEMS - During what phases of distracting warning or caution menssages?. During the initial take-off, nal take-off and landing phases. During the cruise phase and initial descend phase. During take-off phase and cruise phase. During landing roll phase only.

CRK - INDICATING / RECORDING SYSTEMS - The DCUs provide logic determination for?. EICAS messages and FMS autotune. EICAS messages,Master Warning/Caution lights and the DCU aural alert functions. Master Warning/Caution lights and the DCU aural alert functions. Master Warning/Caution lights and FMS autotune.

CRK - INDICATING / RECORDING SYSTEMS - Can the pilot mark an event in the FDR?. YES,by the FDR EVENT page of the FMS. YES,by FDR EVENT page of the EICAS. YES,Pressing and holding the FDR Event Button for two seconds. We don´t have FDR installed in the CRJ.

An invalid V speed or ap setting will result in?. A FD failed indication displayed on the PFD. An IRS failed indication displayed on the PFD. A MAG failed indication displayed on the PFD. A msg of failed indication displayed on the FMS.

What will the FCC do if you select a V2 lower than VR for take off?. This setting is considered INVALID by the FCC and a IRS (boxed ag) will be displayed in the PFD. This setting is considered INVALID by the FCC and a FD (boxed ag) will be displayed in the PFD. This setting is considered INVALID by the FCC and a MAG (boxed ag) will be displayed in the PFD. This setting is considered INVALID by the FCC and a SPEED REVERTED (boxed ag) will be displayed in the FMS.

Which comparison is performend continuosly by the PFD´s?. Comparison of roll,pitch,heading,altitude and airspeed information is performed continuosly. Only Comparison of altitude and airspeed information is performed continuosly. Comparison of radio altitude, ight director pitch,ILS localizer and ILS glide slop information is performed continuosly. Comparison for FMS database information is performed continuosly.

The EFIS COMP Mon plus The AL T indicator will display when?. When both altitud sources are valid. When the cross-side data is valid. When the AL T difference of > 60 feet + (AL T 1 +AL T2) /460. All the cristerias above shall be meet to show the indication.

CRK - MOB - Single engine taxi must be accomplished... with APU running and both PACKS operating, unless MEL dispatched. with APU running and one PACK operating, unless MEL dispatched. with APU running and both PACKS operating, even if MEL dispatched. with APU or one engine running and both PACKS operating.

CRK - MOB - Excessive rotation rates of more than 5 degrees per second ... may lead to the airplane overshooting the target pitch attitude and potentially risk of stall. may lead to the airplane overshooting the target pitch attitude and potentially risk of a tail strike. may be enough for rotation. is not enouch for overshooting the target pitch attitude and potentially risk of a tail strike.