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97 Cards in this Set
- Front
- Back
A complete description of system operations is available in which aircraft manual
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Pilot's Operating Manual (POM)
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What manuals should be in the aircraft during flight?
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AFM, POM, OH
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Supplemental equipment operations can be found in?
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AFM (Supplements in back of AFM)
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Taxi Radius is?
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40 Feet
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Wing span dimensions are?
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43 Feet 6 Inches
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Height of tail?
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13 Feet 11 Inches
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Each generator is capable of producing how many amps?
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400 amps
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Generator power is distributed through?
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Two main buses
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The DC electrical power distribution system is divided into four subsystems:
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Power source distribution
Primary power distribution Secondary power (load) distribution Emergency power distribution |
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If the EMER BUS FDR FAIL annunciator comes on, the emergency relay opens and the emergency bus receives power from the?
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LH load bus
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The nonessential buses are protected by?
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Toggle-switch type circuit breaker on main circuit breaker panel
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To disconnect the LH Main bus from the battery charge bus, pull the:
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LH BUS TIE RCCB
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Which position of the battery switch isolates the battery from the start bus?
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EMER or OFF
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During normal operation of the AC electrical system, the number 1 inverter powers:
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Primary 115 VAC & Primary 26 VAC buses
The 115 VAC shed bus The 26 VAC shed bus |
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If the number 1 inverter fails, the number 2 inverter:
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Transfers power to the primary buses leaving the secondary buses powerless
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Maximum generator load with BOTH Gens operating up to 41,000 feet?
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280 amps
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The No. 1 inverter is powered from the:
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LH Load bus
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Yellow arc of the ITT gauge indicates temperatures between:
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680 to 700 degrees C
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How many stages of compression does the low compressor section of the JT15D engine have?
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Two
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The high compressor section consists of:
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One single-stage centrifugal compressor
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Section controls mixing of fuel and air and contains igniters?
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Combustion section
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Description of the turbine section of the JT15D engine:
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A single-stage high-pressure turbine and a two-stage low-pressure turbine.
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The high-pressure turbine drives:
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The high-pressure compressor and the accessory section.
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Thrust from the engine is delivered by the exhaust section which:
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Combines bypass air with expanding gases of combustion to provide thrust.
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What is is driven by the accessory section?
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Starter-Generator
Oil Pump N2 Tach Fuel Pump Fuel control unit (HMU) Hydraulic pump |
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Engine oil is cooled by means of:
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A fuel/oil heat exchanger.
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Fuel flow to the engine of the Beechjet is controlled by:
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An electronic control (EFC) working in conjunction with a hydromechanical unit (HMU).
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The ignition switches are:
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Three position ON-OFF-STBY switches.
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The engine thrust levers have four marked positions:
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OFF, IDLE, NORM T.O. and T. O.
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The Beechjet utilizes what make and model number engine
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Pratt & Whitney JT15D-5
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What are the maximum sea level static thrust and maximum continuous thrust ratings:
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2,965 LBS and 2,900 LBS
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Maximum permissible engine operating speeds are:
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104% N1
96 % N2 |
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The maximum permissible ITT during an engine start is:
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550 C to 600 C = 4 seconds
600 C to 700 C = 2 seconds |
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What is the primary instrument for determining takeoff thrust settings?
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N1
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Maximum time for continuous reverse thrust above reverse idle is:
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30 seconds
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The maximum stow cycle time after actuation of the reverser lever is:
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5 seconds
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The emergency thrust reverser restow flight envelope is (altitude/airspeed):
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30 Feet or Below 135 KIAS or Below
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During a generator-assisted start (ground-start), ensure the operating engine is between:
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52 to 54 % N2
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A GPU start is recommended at ambient temperature below approximately:
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Minus 15 degrees C.
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The engine fire detection system operates based on:
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A closed loop, semiconductor coaxial cable around the engine
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The fire detect circuits are powered by their respective
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Load buses
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The engine fire bell is powered by the
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Emergency bus
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Pushing the LH ENG FIRE PUSH switch light:
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Closes the left engine fuel valve
Hydraulic shutoff valves Trips the left generator field Arms the fire extinguisher bottles |
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Pushing the BOT 1 ARMED PUSH switch light:
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Discharges the # 1 bottle to the engine corresponding to the last ENGINE FIRE PUSH button pressed
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The location of engine fire bottles are as follows:
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Both bottles are located above the rear baggage compartment
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How many portable fire extinguishers are located on the aircraft?
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2
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The fire warning bell will silence after:
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When the silence button is depressed
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If the red discharge disk is missing during preflight, the following has occurred?
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Overheating of the extinguisher bottles causing the bottle fuse to rupture
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The fuel storage system consists of two independent wing tanks:
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two forward fuselage tanks, two mid fuselage tanks, and aft fuselage tank and a fuselage fill tank
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Which tank feeds the left engine during normal operation?
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The left wing collector tank
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Refueling of the Beechjet 400A is accomplished through:
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Three filler ports, one on each wing and one on aft right fuselage.
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Usable fuel capacity of the Beechjet 400A is:
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733 gallons
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During cruise flight, electrical boost pump switches should be selected:
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AUTO
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With the electric boost pumps in AUTO, the crew can expect the respective pump to operate:
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If fuel feed line pressure drops - 5psi
engine start when collector tank level drops - 11.5 g |
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When an electric boost pump is operating, the crew is informed by means of:
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A white light above the boost pump switch
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The jet pump switches are:
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Two-position switches, labeled NORM and OFF
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The fuel transfer switches are three position switches labeled:
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ON, AUTO and RESET
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The ON position of the fuel transfer pump switch is used:
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On the ground or as a back up if the automatic system fails.
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Selecting the FUEL XFEED switch to the L TANK position allows fuel from the left tank to supply:
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Both engines
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The fuselage fuel in the Diamond 1/1A should be transferred:
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in level cruising flight
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Motive flow for the primary jet pump is supplied by the
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Engine driven fuel pump
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Which tanks are foam filled
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Aft fuselage tank and Aft fuselage fill tank
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Fuel from the aft filler and aft fuselage tank flows to the mid fuselage tanks by
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Gravity
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The purpose of sniffle valves located in the outbaord and middle wing bays and at the gravity refueling port is
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To provide pressure and vacuum relief
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How is fuel transferred from the fuselage tanks to the wing tanks
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Electric fuel transfer pumps located in the mid fuselage tanks
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How can the fuel shutoff valves be closed
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Pressing the LH or RH ENG FIRE PUSH switchlight or the R HYD/FUEL VALVE switchlight
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Illumination okf the L or R WG TK OV PRESS annunciator indicates pressure in the wing tank in excess of 3.5 psid and also causes
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Respective transfer pump to shut down if selected to ON or AUTO
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When the trim interrupt switch is engaged
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The autopilot and yaw damper are disengaged and all trim systems except the emergency pitch trim system are interrupted
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Control column shaking and angle of attack display on the cockpit indicators warn of
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Impending stalls
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As the spoilers on one wing extend, the spoilers on the other wing
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Move below the upper surface of that wing
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What are the seletable flap positions
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Zero, 10, 20, 30
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Rudder boost must be operable and
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armed for all operations
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The hydraulically actuated flight controls consist of
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Speed brakes, flaps
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Flap asymmetry protection
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Stops flap movement if an asymmetric condition of the main flaps is detected
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The speed brakes will automatically retract when
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The throttles are advanced approaching takeoff power and the flaps are exteded beyond 10 degrees
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The auto pilot controls pitch via the
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Emergency pitch trim motor
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On takeoff, the pitch trim warning horn sounds. This means
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The pitch trim is not in the T.O. green band
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The rudder boost system activates the rudder servo to deflectthe rudder and counteract yaw from asymmetric engine thrust by
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Comparing engine bleed air pressure
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Which are considered the primary flight controls
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Elevators, rudder spoilers
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Which flight controls are operated via cables
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Rudder and spolier
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A hydraulic pressure reading of 1850 PSI would be indicated on the hydraulic pressure gauge at the
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Red Line
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The hydraulic reservoir is pressurized with 15psi engine bleed air in order to
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Prevent foaming of the hydraulic fluid in the reservoir and provide head pressure to pumps
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The engine driven hydraulic pumps are
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Variable displacement, rotary plunger type pumps
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Hydraulic reservoir capacity is
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1.1 US Gallons
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Positioning the HYD PRESS switch from NORM to REL
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Opens the hydraulic bypass valve, directing the fluid back to the reservoir
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Normal hydraulic system pressure is
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1350-1550 psi (green arc)
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Which component does not require hydraulic pressure to operate
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Nose wheel steering
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Which is true regarding nosewheel steering
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Nosewheel steering is disengaged when the gear is retracted.
Rudder pedal deflection allows the nose wheel to travel 25 degrees in each direction. Assymetric brake application and thrust can result in 45 degrees of nosewhee travel in each direction |
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A rotating-disc-type assembly in each main gear assembly provides
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Braking force
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During the n ormal gear retraction cycle, what happens first after raising the gear handle
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The grar doors open
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With gear in the UP position, gear and gear doors are held up by
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Mechanical uplocks
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The nose wheel steering system is
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Mechanically actuated
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In the event both pilots are pressing the toe brakes
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The pilot who presses harder controls the brakes
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the parking brake should be
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Set only from the pilot's side
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When using the nitrogen system fro braking
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Anti-skid is unavailable and should make a steady, smooth application of the brakes
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When the anti-skid activates, which brake does it release
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both brakes
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Pressure above_____PSIG or temperature above ______F will close both pressure-regulator and shutoff valves, and ope the emegency pressuraization valve
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53 psig........400F
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