Term
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Definition
pg. 10-8: Air Data Reference Panel
Provides selectable information on the PFD.
Reference Speeds, MDA reference altitude, decision height, and the barometric altitude setting |
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Definition
pg. 10-9: Display Control Panel
Provides control for the MFD format, NAV source selection, bearing pointer selection, cross-side NAV data and course display, Weather radar or EGPWS presentation, TCAS presentation |
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Definition
pg. 2-7: Flight Control Panel
Mode selection panel that selects and controls the FD and auto pilot functions. Located on the Glairshield and is accessible to both pilots.
Divided into 4 sections: FD/ COURSE SELECTOR, AUTOPILOT, VERTICAL MODES, LATERAL MODES. |
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Definition
pg 2-6: Flight Mode Annunciator
Vertical and lateral FD modes are presented in the FMA displayed on each PFD.
FMA is divided into 2 fields and separated by a vertical cyan line. the left side is the active/captured. The right side is the armed field. Each field presents lateral and vertical mode indications. |
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Term
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Definition
pg. 17-7: Radio Tuning Units
Used to tune Comm, NAV, ADF and Transponder |
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Definition
pg. 17-42: Traffic Collision Avoidance System: Resolution Advisory
25-second surveillance area and is considered a threat.
Preventive RA= avoid a conflict now by maintaining current flight track
Corrective RA= Advises to alter current flight path in the vertical plane. avoid a conflict now by following the command climb or descent. |
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Term
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Definition
pg. 17-60: Required Navigation Performance
Statement of the navigation performance accuracy necessary for operation within a defined airspace. located on 2nd page of progress screen. |
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Term
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Definition
pg. 10-4: Primary Flight Display
Located on the main panel. 2 screens, 1 for CA other for FO.
Displays airspeed/mach, vertical speed, altitude, attitude, heading, FD command bars, Nav info, flight mode annuciation (FMA) and autopilot info |
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Term
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Definition
pg. 10-6: Multifunction Display
Displays that combine HSI and map display data on selectable navigation formats. can also become reversionary display if PFD or EICAS fails.
Displays HSI, NAV SECTOR, FMS MAP, TCAS, FMS PLAN MAP, RADAR |
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Term
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Definition
pg. 14-3: engine Indicating Crew Alerting System
Displays the engine instruments, visual and aural crew alert messages and real-time interpretation of aircraft system operation. |
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Definition
pg 4-36: Flight Data Recorder
CL-65 has a Solid State Flight Data Recorder located in the tail section of the aircraft.
Records the last 25 hours of critical aircraft and flight parameter data.
FDR starts when: Beacon turned on, Strobes turned on, Weight of Wheels. |
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Term
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Definition
Total Air Temperature
TAT is what is measured by the aircraft sensor. When air hits a temperature sensor it effectively stops and the kinetic energy in the air is turned into heat therefore at rest TAT and SAT are the same but at speed TAT is always greater than SAT. |
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Definition
Static Air Temperature
The true temperature of the air around an aircraft. |
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Term
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Definition
pg 13-12: Air Data Sensor Heater Controllers
Anti-ice control logic guarantees that the probes and sensors are heated prior to takeoff regardless of the PROBE switch position. |
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Term
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Definition
Shut Off Valves
Used to stop the flow of Hydraulic Fluid in a given position. |
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Definition
Shut Off Valves
Used to stop the flow of fuel in a given position. |
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Definition
pg. 9-21: Spoiler Electronic Control Unit
Controls the extension/retraction of the spoilerons, flight spoilers and ground lift dumping system. |
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Definition
pg. 7-4: Pneumatic Air Conditioning Kit
2 Pneumatic Air Conditioning Kits that can heat or cool the cabin (R pack) or Flight Deck (L pack) if one is lost it provides a 70/30% split to provide opposite side enough air to help ease the pain inside the WiSCOD. |
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Term
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Definition
pg. 7-14: Cabin Pressure Controller
2 CPCs control all phases of pressurization in the auto mode. Only 1 is activated at any given time. the backup is on standby ready to take control if the other is lost.
There are 8 modes: Ground, Prepressurization, takeoff Abort, Flight Abort, Climb, Cruise, Descent and Landing modes.
Im to Lazy to describe each one so look at pg 7-14 - 7-16. |
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Term
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Definition
pg. 6-16: Air-Driven Generator
ADG provides "last hope" power. 115Vac, 400Hz and 15kVA to power the essential buses in-flight when all other generators are inoperative.
exaggerates and gives credit ti the CL-65's nick name--- WiSCOD!! |
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Term
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Definition
pg. 6-4: Integrated Drive Generators
2 Engine driven IDGs that supply 115Vac, 400Hz, three-phase electrical power to 6 AC buses.
composed of 2 sub-components: Constant Speed Drive and an Electrical Generator.
IDGs rate 30kVA from 0-35,000 & 25kVA above |
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Term
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Definition
pg. 6-4: Constant Speed Drive
Turn a constant rpm to produce the steady 400Hz needed.
Cooled by a air/oil heat exchanger. |
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Term
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Definition
pg. 6-21: Transformer Rectifier Units
The normal source of 28Vdc for the DC system.
5 total TRUs located in nose section of the Air Craft |
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Term
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Definition
pg. 3-7: Exhaust Gas Temperature
DO NOT START APU above 974*c
APU EGT Limt= RED>743....Amber 713 to 742...Green<712 (Pg. 18 FCM LIM) |
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Term
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Definition
pg. 2-10: Flight Director Synchronization Switch.
Switch that synchronizes the FD's command bars to vertical and lateral aircraft values present at the time of selection.
Has no effect when autopilot is engaged. |
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Term
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Definition
Proximity Sensing Electronic Unit
Used in critical areas like the landing gear. Magnets that determine range from one-another allowing the computer to sense if the object is closed/latched/locked or not. |
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Term
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Definition
| pg. 4-47: Cockpit Voice Recorder |
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Term
| Define the R/T-I/C switch on the control yoke |
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Definition
pg 4-8: Radio transmit/Intercom switch
Hold Up is Radio transmit. Activates the boom or mask microphone to allow VHF communication.
Hold Down for Intercom. Provides a hot mike to talk over the intercom.
It should return to center when let go... be careful for a "stuck-mike" if it dose not return. |
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Term
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Definition
pg. 9-27: Stall Protection System
Provides flight crew with aural, visual and tactile (stick shaker) indications of an impending stall |
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Term
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Definition
pg. 10-2: Electronic Flight Instrument System
4 cathode ray tubed electronic flight displays |
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Term
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Definition
pg. 15-24: Brake temperature Monitoring System
BTMS continuously monitors the temp of each break by means of a thermocouple.
displayed as in a range from 00-20 units. each unit is 35*c (Hot as shit)
Green: 00 to 05
White: 06 to 12
Red: 13 to 20
a red number that is in the green means that it once was red and needs to be inspected because you probably warped the brakes with that landing you just accomplished. Good job... |
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Term
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Definition
Horizontal Stabilizer Trim Control Unit
controls Horizontal stabilizer angle of incidence
+2° (Leading edge up) to –13°(Leading edge down)
Two motors
Equipped with a brake to prevent runaway
Two channels - CH1 & CH2
Receives inputs from:
Control wheel trim switches
Autopilot
MACH trim system |
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