What are the entry requirements, Basic VFR weather minimums, cloud clearance requirements, and speed limits in the Class A airspace?
Class A:
Name the two types of drag AND what causes them AND the relationship to airspeed.
Induced drag is a byproduct of lift.
- Half airspeed = four times induced drag
- Low airspeed, high angles of attack = more induced drag
-Greatest when aircraft is heavy slow and clean
- Caused by the spanwise airflow around the wing.
Parasite drag includes all the drag not related to the production of lift.
- Double Airspeed = four times parasite drag
- Form drag – turbulent wake caused by airflow around a structure
- Interference – interaction of varied currents that flow over an airplane and mix together
- Skin friction drag – roughness of airplane surfaces
Explain the Pitot-Static System
A combined pitot-static probe below the left wing. Pitot port in front, static port in back, drain port in bottom.
Airspeed: uses the pitot port and the static port. Uses the difference between ram air pressure and static air pressure to indicate the airspeed
Altimeter: uses the static air pressure to indicate the altitude MSL
VSI: uses the rate of change of static pressure to indicate the direction and rate of altitude change
Blind altitude encoder: does not have an adjustment for weather induced changes. Located on the aft side of the firewall on the left and sends static pressure to the transport for mode c operation and the GPS system for altitude input.
Define the ISA
International Standard Atmosphere
Sea Level Barometric pressure: 29.92 in Hg
Sea Level Temperature: 15 degrees C
Relative humidity: 0%
Brief Diversion
What are the entry requirements, map depiction, cloud clearance requirements, and speed limits in the Class D airspace?
What are the 4 turning tendencies
Torque- from rotation of propeller - left turning
Gyroscopic - force applied to rim of propeller - right yaw
P-factor - asymmetrical thrust - left yaw
Spiraling Slip Stream - wraps the fuselage and hits rudder - left yaw
How much flight time does a full tank of fuel provide?
4 hours of flight time
6 gallons per hour
every 1/8th of a tank is 30 minutes of flight (3 gallons)
What is a windshear and the 4 things associated with it?
Wind Shear is a sudden, drastic change in wind speed and/or direction over a small area
1. Passing Frontal Systems
2. Thunderstorms
3. Temperature Inversions
4. Surface Obstructions
What are the entry requirements, map depiction, cloud clearance requirements, and speed limits in the Class G airspace?
What are the entry requirements, map depiction, cloud clearance requirements, and speed limits in the Class E airspace?
Class E:
Indications, Actions, and Considerations of Stall Recovery
Indications
Spin: Stall + Yaw
Actions
Throttle - Idle
Rudder - Full Opposite Spin Direction
Control Stick - Ease Foward
Rudder - Neutral When Rotation Stops
Flaps - Cruise
Control Stick - Pull Cautiously
Considerations
CAUTION: Recover to level flight cautiously to avoid inducing a secondary stall, but do not allow the airspeed to exceed 164 KIAS.
The stall pattern on the DA20-C1 wing progresses from the wing root toward the wingtip. This design helps prevent undesirable rolling moments at high lift coefficients, contributes to early stall warning, and preserves aileron effectiveness at high angles of attack.
“Stall and yaw” are required to enter a spin.
Proper stall recovery technique (i.e., maintaining coordinated flight throughout the setup and recovery) will prevent inadvertent spins.
Do not confuse a spin with a spiral dive. A spin involves flight at high angles of attack and low airspeed, but a spiral dive involves spiral motion at a relatively low angle of attack and high airspeed.
Use the miniature airplane on the turn coordinator to verify spin direction. Do not use the ball in the inclinometer to determine spin direction because its indications are not always reliable.
Perform a CONTROLLABILITY CHECK if you suspect structural damage following an over-G during spin recovery.
Fuel Planning
- How much fuel do you need to carry for each type of sortie?
- 1.4, 1.5, 1.8, 1.9, 2.0, Area, X/C?
- how long for reserve?
Fuel Planning
what are the stages of a thunderstorm?
Cumulus Stage: height 3-5 mi, updrafts begin, needs moisture and instability
Mature: height 5-10mi, most violent, when precipitation begins to fall, violent turbulance
Dissipating: 5-7 mi, updrafts dissipate, downdrafts begin spreading out
Describe the Clock-Map-Ground Method
What are the entry requirements, map depiction, cloud clearance requirements, and speed limits in the Class C airspace?
Class C:
Magnetic Variation vs Magnetic Deviation
Magnetic Variation: Angle between Mag. North and True North
Magnetic Deviation: Deviation from magnetic compass and actual magnetic heading due to interference from aircraft
What is the Oil System Pathway
Read this:
KCOS 162354Z 31009KT 10SM FEW090 07/M06 A2978 RMK AO2 WSHFT 2322 SLP070 T00721061 10139 20072 53024
KCOS 162321Z 1700/1724 04012KT P6SM FEW100
TEMPO 1700/1701 04012G22KT
FM170100 33010KT P6SM
you probbly did it good
Decode Trinidad Airport Information Block
Magenta Color: Un towered
Perry Stokes (RAD): airport name and code
ASOS frequency: 119.025
Elevation: 5762 ft
*L: lighting limitations exist
Longest runway available: 55 ft
UNICOM: 122.8
RP 21: Right hand pattern for runway 21
Solid C: indicates CTAF
What are the entry requirements, map depiction, cloud clearance requirements, and speed limits in the Class B airspace?
Class B:
What is the fuel system pathway
System Pathway: Fuel Tank; Gascolator; Duke’s Fuel Pump or Bypass; Fuel Shutoff Valve; Engine Driven Pump (and swirl chamber); Fuel Control Unit; Fuel Distribution Manifold; Fuel Injector Nozzles; Engine Cylinders
What are the Weather Minimums for Nav Routes
1) Minimum flight visibility is 3 sm with an IP on board, and 5 sm for student solos.
(2) 500 feet below clouds.
(3) 1000 feet above clouds with an IP on board. Student solos shall not fly in conditions without visual reference to the surface.
(4) 2000 feet horizontal from clouds
Brief from memory:
ENGINE MALFUNCTION—INSUFFICIENT ENGINE POWER AFTER TAKEOFF
Indications, Actions, Considerations.
INDICATIONS
Inability to maintain positive rate of climb after takeoff due to partial loss of engine power.
ACTIONS
1. AIRSPEED…60 KIAS.
2. THROTTLE…FULL.
3. MIXTURE…FULL RICH.
4. FUEL SHUTOFF VALVE…ON.
5. IGNITION SWITCH…BOTH..
6. FUEL PUMP…ON.
7. ALTERNATE AIR…ON.
8. FORCED LANDING IF SUFFICIENT PWR IS NOT RESTORED
9. PRECAUTIONARY EMERGENCY LDG IF PWR RESTORED
CONSIDERATIONS
WARNING: Do not attempt to turn back to the departure runway without sufficient altitude. The safest option for a forced landing shortly after takeoff is generally to land straight ahead, or small turns as required to avoid obstacles and hazards