Engines And General Knowledge Flashcards
What kind of engines power the CRJ-700?
2 General Electric CF34-8C5B1 High Bypass Turbofans.
What is the range of the CRJ-700?
Standard 1685 nm.
Extended 1985 nm.
What are the dimensions of the CRJ-700?
Height 24’10”.
Length 106’8”.
Span 76’3”.
What are the intake and exhaust danger areas?
Idle - Intake 13 ft exhaust 100 ft.
Maximum - Intake 26 ft exhaust 300 ft.
What can be controlled from the flight attendant’s control panel?
Cabin lighting.
Emergency lighting.
Main passenger door.
Interphone system.
What is the maximum speed and altitude of the CRJ550?
0.85 Mach.
41,000 ft.
What is the minimum pavement width required for a 180 degree turn?
75 ft.
What is the size of the APU exhaust danger area?
15 ft.
What emergency equipment is located behind the Captain’s and First Officer’s seats.
CA - Flashlight and PBE.
FO - Flashlight, crash axe and fire extinguiser.
How much thrust is developed by each engine?
12,670 lb at take-off.
13,790 at APR.
13,280 at MCT.
Decribe the major sections of the N1 and N2 spools.
N1 - Outer section including 1 large turbine and a 4 stage low pressure turbine.
N2 - Inner section including a 10 stage axial compressor and a 2 stage high pressure turbine.
What components are located on the accesory gearbox?
Oil pump. Fuel pump. Hydraulic pump. FADEC alternator. Integrated Drive Generator (IDG). Fuel metering unit. Air Turbine Starter.
What is the purpose of the N2 variable geometry?
To prevent compressor stall and surges.
It also improves overall efficiency.
How the is the N2 variable geometry operated?
Controlled by FADEC.
Fuel is used to actuate the vanes.
Where is the N2 varibale gemoetry located?
On the first 4 stages of the N2 compressor.
What does the FADEC control?
Fuel control system.
Engine start and ignition system.
Compressor airflow.
How many chanels does each FADEC have and when do they operate?
Two, an A and B channel.
One channel is ‘in control’ the other is in standby.
Both channels simultaneously operate and share data but only the ‘in control’ channel provides actual engine commands.
When does the FADEC’s standby channel provide commands to the engine?
In an engine overspeed condition. The result is an engine flame out then an auto relight once the N2 spools below a set threshold.
How is the FADEC powered?
Below 50% N2 RPM by the aircraft’s electrical system.
Above 50% N2 RPM by it’s own alternator driven by it’s onside engine.