AVED 1403 Final Exam Vocabulary
Aircraft Structure & Flight Controls
- Monocoque Airframe: Does not derive its strength and shape from a skeletal frame. Therefore, the answer to question 1 is False.
- Aileron Control: Ailerons control roll about the longitudinal axis.
- Adverse Yaw: The rudder is used to counteract adverse yaw.
Engine (Lycoming IO-360-L2A)
- I: Fuel Injected
- O: Horizontally Opposed
- 360: 360 cubic inch displacement.
- Four Strokes of a Reciprocating Engine
- Intake
- Compression
- Power
- Exhaust
- Magneto Check: Maximum allowable RPM drop during a magneto check for the 172 G-1000 is 175 RPM.
- Magneto Function: A magneto sends a spark to the spark plugs.
- Number of Spark Plugs: There are 8 spark plugs in our engine.
Fuel & Oil
- Fuel with Green Tint: Indicates the presence of AVGAS 100LL, it is generally okay to fly. However, it is important to verify the grade required for operation.
- Rising Oil Temperature & Dropping Oil Pressure: This indicates a serious problem, possibly oil starvation. Immediate action is required, such as reducing power and preparing for a possible emergency landing.
Electrical System (Cessna 172)
- System Voltage: 28 volts
- Battery Voltage: 24 volts
- System Amperage: 60 amps
- Type: DC (Direct Current)
- Standby Battery Power:
- Attitude Indicator
- Airspeed Indicator
- Altimeter
- AHRS
- MFD
Vacuum Pump Failure (Cessna G1000)
- Affected Instruments:
- PFD Attitude Indicator
- Heading Indicator
Alternate Static Source
- Airspeed: Indicates higher than actual.
- Altimeter: Indicates higher than actual.
- VSI: Instantaneous indication then stabilizes.
Medical Factors
- Hypoxia: Abnormally low levels of Oxygen.
- Hyperventilation: Abnormally low levels of Carbon Dioxide.
- Legal Alcohol Limit: The legal limit on alcohol when operating an airplane is 0.04%.
Aircraft Airworthiness
- Required Certificates and Documents: (Not including radio operator certificate)
- Airworthiness Certificate
- Registration Certificate
- Operating Limitations (POH)
- Weight and Balance Information
- Identification Plate
- Required Tests and Inspections:
- Annual Inspection (every 12 calendar months)
- 100-Hour Inspection (if used for hire)
- Transponder (every 24 calendar months)
- ELT (every 12 calendar months, or after 1 hour of cumulative use, or after battery replacement)
- Altimeter and Static System (every 24 calendar months)
- AD's (as required)
- Annual vs. 100-Hour Inspection: An annual inspection can replace a 100-hour inspection.
- Overflying Annual Inspection: Not allowed to overfly for more than 10 hours to reach a maintenance facility.
- Transponder Inspection Due Date: According to the FAA the transponder inspection is due 24 calendar months after the last transponder inspection
- ELT Inspection Due Date: According to the FAA the ELT inspection is due 12 calendar months after the last ELT inspection
- Pilot Performed Maintenance:
- Minimum rating required: Private Pilot License.
- Not allowed: Performing an ELT inspection is typically not allowed as pilot performed maintenance.
Airport Operations
- Red Sign with White Lettering: Mandatory Instruction Sign.
- Holding Short of ILS Critical Area: At a towered airport, you must hold short of an ILS Critical Area when ATC instructs you to.
- Contacting Stillwater FBO: Stillwater UNICOM 122.950.
Airspace
- Airspace Not Controlled by ATC: Class G.
- Floor of Class A Airspace: 18,000’ MSL.
- Two-Way Radio Communications to Enter a Bravo: "OST30 is cleared into the Bravo".
- Class D Airspace Cloud Clearance & Visibility:
- 3 SM visibility
- 1,000’ above
- 500’ below
- 2,000’ horizontal
- Class E Airspace Cloud Clearance & Visibility (above 10,000’ MSL):
- 5 SM visibility
- 1,000’ above
- 1,000’ below
- 1 SM horizontal
- Mode C Transponder in Class Echo: Required above 10,000’ MSL.
- Class G Airspace Cloud Clearance & Visibility (1200’ AGL or less, day): 1 SM, clear of clouds.
Weather
- Unstable Atmosphere Characteristic: Cumuliform clouds.
- METAR "PK WND 13045/1436": At 14:36Z, 130° at 45KTS.
- METAR “T00481027”: 4.8°C Temp, -2.7°C Dewpoint.
- PIREP “/OV DEN245040”: 40 Miles on a 245° bearing away from DEN.
- Aircraft “Stable” Definition: The aircraft can better resist motion.
- CG Loading & Stall Recovery: Forward CG.
- Air Pressure Increase: A decrease in density altitude.
- Humidity Increase: An increase in density altitude.
Navigation
- RAIM: Receiver Autonomous Integrity Monitoring.
- WAAS: Wide Area Augmentation System.
VFR Cruising Altitudes
- VFR Heading of 150°: Acceptable cruise altitude is 5500’ MSL (odd thousands + 500).
- True Heading: True Course corrected for Variation.
- Magnetic Heading: True Heading corrected for Deviation.
- Course Heading: Magnetic Heading corrected for Winds.
- Pilotage: Navigation by visual reference to landmarks.