P.I.M Flashcards
What type of engine do we have?
Textron Lycoming normally aspirated, direct drive, air-cooled, horizontal opposed, fuel injected, 4 cylinder engine with 360 cubic inches of displacement.
What type of propeller do we have?
Fixed pitch with 76in in diameter, it is made by McCauley Propeller Systems
What is the Maximum Horse Power and Engine speed?
180 bph at 2700 Rpm
Instruments on Right Wing
Right Fuel Tank
Static Wicks (2)
AOA Vane
Wing Tip Lights
Cabin Vent Inlets
Ailerons
Flaps
Flap Motor
Instruments on Left Wing
Left Fuel Tank
Magnetometer
Static Wicks (2)
Pitot Tube
Cabin Vent Inlets
Fuel Vent
Stall Horn
Wing Tip Lights
Aileron
Flaps
What type of Ailerons Do we have?
Conventional, Differential, and Freeze Type
What Type of Flaps do we have?
Single Slotted with Fowler Type Characteristics
What does the Fuel Vent Do?
Balances the Pressure in the Fuel Tank
What does the Pitot Tube measure?
Airspeed
Instruments on the Fuselage
Oil Quantity
Exhaust
Induction Inlet/ Filter
Alternator
Nose Gear
Static Source Opening
Cabin Air Inlet
Propeller
Power Source
Airframe: the Empennage
Vertical Stabilizer
Rudder
Elevator
Horizontal Stabilizer
Static Wicks (6)
What type of Landing Gear do we have?
Tricycle Fixed Landing Gear with a Tubular Spring Steel Main Landing Gear and the air/oil nose gear shock strut
Fuselage Construction
Conventional formed sheet metal composed of bulkheads, stringers, and skin referred to as semimonocoque.
What kind of Trim do we have?
Electric Trim, Manually Operated elevator trim system, differential trim (functions opposite)
Engine Accessory Package
Major Accessories include a starter and belt driven alternator, dual magnetos, vacuum pump, engine driven fuel pump, and a fuel flow oil filter.
Engine Power is set how?
By Using the Throttle
What Brake System do we have?
The airplane has a single-disc, hydraulically actuated brake pads
What kind of Electrical System do we have?
The airplane is equipped with a 28 volt direct current electrical system consisting of a belt driven 60 ampere alternator and a 24 volt main storage battery
What does the ACU do?
It is the alternator control unit and makes sure the alternator does not overload the system
What controls the main battery and alternator?
The MASTER Switch
Which Brake is the Main Brake?
The left brake is the main brake, it is the only one connected by cylinders, control pressures, and connects them to cables.
What type of current does the Alternator produce?
It generates direct current
What electrical buses do we have?
6
Primary:
Electrical BUS 1
Electrical BUS 2
Avionics BUS 1
Avionics BUS 2
Secondary:
Essential Bus
Crossfeed Bus
Crossfeed
Alternate Master Switch, warnings
Essential Bus
Primary flight display, Air data computer, Attitude Heading reference system, nav 1, comm 1, Standby indicator lights, Standby Battery
PFD, ADC, AHRS, NAV 1, COMM 1, STBY Lights, STDBY Battery
Tell me about the Main Battery
Supplier for all systems (no limit stated) when under 20% the standby switches on (will last maybe 30min)
G1000 Annunciator Panel
Oil Pressure, Low vacuum, Low Fuel (L), Low Fuel (R), Pitch Trim, Low Volts, High Volts, STBY Batt, Co Level High (if applicable)
Electrical Bus 1
Fuel pump, becon light, landing light, flaps, avionics 1, cabin lights/power
Avionics Bus 1
Primary flight display, air data computer, altitude heading reference system, Nav 1
Electrical Bus 2
Pitot Heat, Nav Lights, taxi lights, strobe lights, panel lights, avionics 2
Avionics Bus 2
Multi function display, transponder, nav 2, audio panel, autopilot
G100 Aunnciator Panel
Oil pressure
Low Fuel (R and L)
Low Volts
High Volts
Standby Battery
Low Vacuum
Pitch Trim
Co (lvl) High if applicable
Explain the Electrical System
The airplane is equipped its a 28 volt direct current electrical system consisting of a belt driven 60 amp alternator and a 24 volt main storage battery
