Systems Flashcards
General
Make: Piper
Model: PA-28-181
Identifier: P28A
Max Gross: 2550
Primary Flight Controls
- Differential Ailerons
- Elevator
- Rudder
Secondary Flight Controls
- Single Slot Wing Type Flaps (Manually Actuated) at 0, 10, 25, 40
Trim
- Elevator: Manually and Electronically Actuated
- Rudder: Located by copilot left leg
Propeller
- Manufacturer: Sensenich
- Type: Fixed Pitch
- Diameter: 76in
- No of Blades: 2
- Material: Metal
Powerplant
Manufacturer: Lycoming
Model No.: IO-360-B4A
Fuel Metering System: Injected
No. Of Cylinder: 4
Cylinder Config: Horizontally Opposed
Propeller Drive: Direct
Cooling: Air
Aspiration: Naturally Aspirated
Horsepower: 180@2700rpm
Ignition: Dual Magnetos
Fuel/Air Control: Mixture
Oil System
Sump Type: Wet
Capacity: 5-8 quarts
School Policy: 6 quarts
Oil Type: Philips X/C 20W-50
Fuel Systems
Fuel Pumps: As needed per POH, Mechanical, Engine Driven
Capacity:50, 48 Usable
Hydraulic System
- Fluid Type: MIL 5606H
- External Reservoir on Firewall
- Actuates Caliper Disk Brakes on Main Wheels
Landing Gear
Configuration: Fixed Tricycle
Brakes: Differential Toe Brakes
Nose gear: Steerable, Air/Oil Shock Strut(OLEO)
Main Gear: Air/Oil Shock Strut(OLEO)
Electrical System
System Voltage: 28
Power Generation: 70Amp Alternator
Main Battery Voltage: 24
Additional Battery: 1 Emergency Battery, (24 Volts Approx 30 Minutes Power to Emergency Bus)
Avionics
Transponder: Mode S with A, C and S Functions
Displays: G1000 PFD & MFD
Flight Instruments: ADAHRS
Standby Instrument: Garmin G5
Autopilot: Garmin GFC-700 2-axis integrated with auto pitch trim
IFR Navigator: 2x Garmin GPS
Deicing and Anti-Ice
- Pitot Heat
- Windscreen Defroster
- Heated Static Port on Pitot Mast
- Alternate Static Source
- Alternate Air
