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91.205 VFR Day
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Stipulations
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Altimeter
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-
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Tachometer
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for each engine
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Oil Pressure
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for each engine
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Manifold Pressure
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for each altitude engine
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Airspeed
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-
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Temperature Gauge
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for each liquid cooled engine
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Oil Temperature Gauge
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for each air cooled engine
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Fuel Gauges
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for each tank
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Landing Gear Position Indicator
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if retractable
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Anti Collision Lights
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after 1996
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Magnetic Direction
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-
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ELT
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-
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Seatbelts
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for each occupant 2 years and older
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VFR Night
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91.205
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Fuses
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1 set or 3 of each kind
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Landing Light
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aircraft operated for hire
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Anti Collision Lights
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after 1971
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Position Lights
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-
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Source of Power
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-
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Required Documents in Plane
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91.203
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Airworthiness
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must be visible
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Registration
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valid for 7 years
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Radio Station License
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international flights
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Operating Limitations
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aircraft specific
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Weight and Balance Data
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aircraft specific
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Supplemental
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-
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Maintenance Requirements
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91.409 91.171 91.411 91.413 91.207
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Airworthiness Directives
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once, recurring, or emergency
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Annual
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every 12 cm
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VOR
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every 30 days (for IFR)
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100 hour
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for hire
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Altimeter
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every 24 cm (for IFR)
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Transponder
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every 24 cm
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ELT
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every 12 cm (battery replaced after 1 hour or 50%)
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Hypoxia
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Hypoxic
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Hypemic
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Histotoxic
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Stagnant
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Go Around
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Cram
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Climb
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Clean
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Cool
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Call
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91.103 Preflight Actions
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NOTAMs
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Weather
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Known ATC Delays
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Runway Lengths
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Alternatives
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Fuel Requirements
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Takeoff and Landing Distances
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Engine Specs
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Lycomming
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4 stroke
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4 cylinder
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Horizontally Opposed
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Air Cooled
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Naturally Aspirated
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Direct Drive
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15nm / Inbound
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Weather
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Instruments
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Radios
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Environment
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Downwind / IAF
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Boost Pump on
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Gas fullest tank
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Undercarriage fixed
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Mixture rich
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Power set
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Seatbelts secured
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FAF
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Time
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Gear
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Power
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Tower
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Lights
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Lights
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Flaps
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Spin Recovery
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Rudder opposite
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full forward
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ailerons neutral
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throttle idle
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rudder neutral
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smooth back pressure
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Engine fire on startup
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start switch continue cranking
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mixture idle
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throttle full
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fuel pump off
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fuel selector off
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evacuate
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extinguish
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Engine Failure on Takeoff
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Sufficient Runway:
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safe airspeed
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land straight ahead
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brakes as needed
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Insufficient Runway:
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safe airspeed
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flaps as needed
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shallow turns
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Sufficient Altitude
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airspeed 76
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fuel selector switch tanks
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fuel pump on
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mixture rich
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alt air open
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land power off
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mayday
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secure
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Engine Fire during Flight
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fuel selector off
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throttle idle
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mixture idle
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fuel pump off
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heat defrost off
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emergency descent
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Electrical Fire
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E battery arm
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battery off
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alternator off
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vents open
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heat defrost off
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extinguish
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emergency descent
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Emergency Descent
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throttle idle
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flaps as needed
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no flaps 125
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flaps 102
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bank 45
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Engine Failure in Flight
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airspeed 76
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locate landing area
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fuel selector switch tanks
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fuel pump on
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mixture rich
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alt air open
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left mag off then on
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right mag off then on
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mayday
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secure
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Categories of Aircraft (in respect to Airmen)
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Airplane
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Rotorcraft
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Glider
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Lighter Than Air
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Class of Aircraft (in respect to Airmen)
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Single Engine Land
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Multi Engine Land
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Single Engine Sea
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Multi Engine Sea
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Categories of Aircraft (with respect to certification of aircraft)
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Transport
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Normal
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Utility
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Acrobatic
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Limited
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Restricted
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Provisional
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Classes of Aircraft (with respect to certification of aircraft)
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Airplane
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Rotorcraft
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Glider
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Balloon
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ATC Light Gun Signals
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Ground
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Steady Green
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Cleared for Takeoff
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Flashing Green
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Cleared for Taxi
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Steady Red
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STOP
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Flashing Red
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Taxi clear of runway in use
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Flashing White
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Return to starting point on airport
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Alternating Red and Green
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Exercise Extreme Caution
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ATC Light Gun Signals
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Air
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Steady Green
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Cleared to Land
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Flashing Green
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Return for landing
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Steady Red
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Give way to other aircraft and continue circling
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Flashing Red
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Airport unsafe, do not land
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Flashing White
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Not Applicable
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Alternating Red and Green
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Exercise extreme caution
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AIRSPACE
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Class A
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Visibility
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Not Applicable
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Cloud Clearance
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Not Applicable
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Class B
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Visibility
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3 sm
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Cloud Clearance
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clear of clouds
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Class C
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Visibility
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3 sm
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Cloud Clearance
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1000 above 500 below 2000 horizontal
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Class D
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Visibility
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3 sm
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Cloud Clearance
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1000 above 500 below 2000 horizontal
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Class E
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<10,000 MSL
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Visibility
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3 sm
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Cloud Clearance
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1000 above 500 below 2000 horizontal
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Class E
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>=10,000
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Visibility
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5 sm
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Cloud Clearance
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1000 above 1000 below 1 sm horizontal
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Class G (DAY)
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<=1200 AGL
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Visibility
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1 sm
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Cloud Clearance
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clear of clouds
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Glass G (NIGHT)
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<=1200
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Visibility
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3 sm
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Cloud Clearance
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1000 above 500 below 2000 horizontal
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Class G (DAY)
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>1200 AGL, <10,000 MSL
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Visibility
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1 sm
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Cloud Clearance
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1000 above 500 below 2000 horizontal
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Class G (NIGHT)
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>1200, <10,000
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Visibility
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3 sm
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Cloud Clearance
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1000 above 500 below 2000 horizontal
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Class G (D/N)
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>1200 AGL and 10,000 MSL
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Visibility
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5 sm
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Cloud Clearance
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1000 above 1000 below 1 sm horizontal
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Special Use Airspace
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Other Airspace
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warning area
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Military Training Route
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controlled firing area
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Parachute jump
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restricted area
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Special Flight Rules Area
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alert area
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Temporary Flight Restriction
|
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military operations area
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Terminal Radar Service Area
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prohibited area
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VFR Route
|
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national security area
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Weather Reconnaissance Area
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Piper Archer Specs
|
Answer
|
|
takeoff power (bhp)
|
180
|
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takeoff power engine speed (rpm)
|
2700
|
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fuel capacity (gal)
|
50
|
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usable fuel (gal)
|
48
|
|
fuel (minimum octane)
|
100 Green
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OR
|
100LL Blue
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oil capacity (qt)
|
8
|
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maximum ramp weight (normal) (lbs)
|
2558
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maximum takeoff weight (normal) (lbs)
|
2550
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maximum landing weight (normal) (lbs)
|
2550
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maximum weight in baggage compartment (normal) (lbs)
|
200
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Maximum Demonstrated Crosswind Velocity (kts)
|
17
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Max Oil Temperature (F)
|
245
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Min Oil Pressure (PSI)
|
25
|
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Max Oil Pressure (PSI)
|
115
|
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Alternator Minimum (A)
|
70
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Emergency Battery Minimum (V)
|
23.3
|
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Positive Load Factor Maximum (normal) (G)
|
3.8
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Negative Load Factor Maximum (normal)(G)
|
-1.5
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maximum ramp weight (utility) (lbs)
|
2138
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maximum takeoff weight (utility) (lbs)
|
2130
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maximum weight in baggage compartment (utility) (lbs)
|
0
|
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Positive Load Factor Maximum (utility) (G)
|
4.4
|
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Negative Load Factor Maximum (utility) (G)
|
-1.7
|
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V Speeds
|
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Vs0
|
45
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Vs1
|
50
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Vr (2)
|
55, 60
|
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Vx
|
64
|
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Vy
|
76
|
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Vg
|
76
|
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Va
|
98-113
|
|
Vfe
|
102
|
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Vno
|
125
|
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Vne
|
154
|
|