| Term 
 
        | What engine is installed on the LJ35 and what is the rated thrust? |  | Definition 
 
        | - TFE731-2-2B OR 2C - 3,500lbs of thrust at sea level up to 72 degrees F
 |  | 
        |  | 
        
        | Term 
 
        | Concerning the -2C DEEC fuel computers, what are the buffer (memory) limits? |  | Definition 
 
        | - 40 cycles and the fuel computer light flashes at slow interval. - 50 cycles and the buffer overwrites the oldest cycles.
 |  | 
        |  | 
        
        | Term 
 
        | What are the engine starter limits? |  | Definition 
 
        | 1 minute 1 minute
 15 minutes
 1 minute
 1 minute
 60 minutes
 |  | 
        |  | 
        
        | Term 
 
        | What activates the igniters during a normal engine ground start? |  | Definition 
 
        | Moving the thrust levers from cutoff to idle. |  | 
        |  | 
        
        | Term 
 
        | What is the purpose of the soft start protection and explain its operation? |  | Definition 
 
        | To prevent shearing the tower shaft. DC voltage is reduced to 12VDC for 1.5 seconds when the start sequence is initiated. |  | 
        |  | 
        
        | Term 
 
        | When may engine sync not be used? |  | Definition 
 
        | - Takeoff - Landing
 - Single engine operation
 |  | 
        |  | 
        
        | Term 
 
        | What is the maximum continuous cruise ITT? |  | Definition 
 
        | -2B: 795 degrees C recommended, 832 degrees C for 30 minutes recommended, 832 degrees C Do not exceed maximum N1 
 -2C: 827 degrees C recommended, 865 degrees C for 30 minutes recommended, 865 degrees C Do not exceed maximum N1
 |  | 
        |  | 
        
        | Term 
 
        | What does a slow flashing fuel computer light represent on the -2C DEEC fuel computers? |  | Definition 
 
        | The fuel computer buffer (memory) is full and needs to be downloaded. |  | 
        |  | 
        
        | Term 
 
        | what is the power source for the oil pressure gauge? |  | Definition 
 | 
        |  | 
        
        | Term 
 
        | What type of engine oil is utilized in the TFE731? |  | Definition 
 | 
        |  | 
        
        | Term 
 
        | What is the normal oil temperature range? |  | Definition 
 
        | (30-127)degrees C 
 Note: (127-139)degrees C is yellow caution range and 140 degrees C is redline.
 |  | 
        |  | 
        
        | Term 
 
        | When should the oil level be checked? |  | Definition 
 
        | Within one hour after shutdown, preferably 15 minutes up to one hour after shutdown. |  | 
        |  | 
        
        | Term 
 
        | If the fuel computer fails, what protection do you loose? |  | Definition 
 
        | - Ultimate overspeed protection (109% N1 or 110% N2) is lost 
 _ You will still have the mechanical overspeed governor protection (105% N2)
 |  | 
        |  | 
        
        | Term 
 
        | What engine systems are affected when a Fuel computer fails? |  | Definition 
 
        | - Ultimate overspeed protection is lost - Over temperature protection is disabled
 - Engine response is slower
 - Single engine takeoff, climb and landing performance are degraded
 - Fuel consumption is affected
 - Surge bleed valve fails to 1/3 open
 - SPR is disabled
 - Engine sync
 |  | 
        |  | 
        
        | Term 
 
        | What are five major components of the TFE731-2 engine and how many bearings do they rest on? |  | Definition 
 
        | - Spinner and Fan (11,502 RPM) - Low pressure spool (N1)(20,688 RPM)
 - High pressure spool (N2)-2B(29,692 RPM) -2C(30,100 RPM)
 - Annular combustion Chamber
 - Transfer gearbox and Accessory gearbox
 - 6 bearings
 |  | 
        |  | 
        
        | Term 
 
        | How many duplex fuel atomizers supply fuel for the combustion chamber? |  | Definition 
 | 
        |  | 
        
        | Term 
 
        | How many thermocouples, which are located between the high pressure turbine(N2) and the low pressure turbine(N1), measure ITT? |  | Definition 
 | 
        |  | 
        
        | Term 
 
        | What are the approximate thrust percentages between the core and the fan? |  | Definition 
 
        | - At Sea Level: Fan=60%  Core=40% - At FL 400:    Fan=40%  Core=60%
 |  | 
        |  | 
        
        | Term 
 
        | Why is the engine core rotation clockwise and the fan rotation counterclockwise(as viewed from aft)? |  | Definition 
 
        | Smaller engine mounts are utilized because of the counteracted torque.  If part of the engine seizes, the torque is counteracted and will not shear the engine from its mounts. |  | 
        |  | 
        
        | Term 
 
        | A solid-state, high energy ignition system consists of a dual ignition exciter(induction vibrator) mounted on the engine and two igniter plugs in the combustion chamber. What are the locations of the ignitors on the engine as viewed from aft? |  | Definition 
 | 
        |  | 
        
        | Term 
 
        | What is the apporximate voltage output of the induction vibrator? |  | Definition 
 
        | - Input= 28VDC - Output= (18,000 to 24,000) VDC
 |  | 
        |  | 
        
        | Term 
 
        | The oil reservoir and oil system quantities are what? |  | Definition 
 
        | - Reservoir= 1.5 gallons or 6 quarts - System= 3.0 gallons or 12 quarts
 |  | 
        |  | 
        
        | Term 
 
        | If outside temp is less than -25 C, how long must engine warm up? |  | Definition 
 | 
        |  | 
        
        | Term 
 | Definition 
 
        | "OFF"- for T/O, Landing and single engine operations |  | 
        |  | 
        
        | Term 
 | Definition 
 
        | - .05 Gal/Hr 
 - .1875 QTS/Hr over 15 hour period
 |  | 
        |  | 
        
        | Term 
 
        | Max Continuous Temp(ITT)? |  | Definition 
 
        | 832 C (795 C Recommended) |  | 
        |  | 
        
        | Term 
 | Definition 
 
        | 860 C (870 C for 10 seconds) |  | 
        |  |