AP.IV.E.S1
SkillClear the area and select an entry altitude that allows the recovery to be completed no lower than 3,000 feet above ground level (AGL).
From the FAA library
- Chapter 8: Flight Instruments › Altimeter Operation
altimeter indicates an altitude above the actual field elevation. If the barometric pressure setting is reset to the current altimeter setting of 29.68 "Hg, then the field elevation is again indicated on the altimeter. This pressure change ... easily noticed in flight since aircraft fly at specific altitudes. The aircraft steadily decreases true altitude while the altimeter is held constant through pilot action as discussed in the previous section. Knowing the aircraft’s altitude is vitally important…
- Chapter 11: Aircraft Performance › Performance › Rate of Climb (ROC)
Rate of Climb (ROC) ROC is a comparison of altitude gained relative to the time needed to reach that altitude. ROC is simply the vertical component of the aircraft’s flight path velocity vector. For maximum ROC performance, a pilot ... flies the aircraft at VY so as to achieve a maximum gain in altitude over a given period of time. Maximum ROC expedites a climb to an assigned altitude. This gains the greatest vertical distance over a period of time…
- Chapter 2: Personal Minimums › Personal Minimums › Step 2—Assess Experience and Comfort Level
Figure 2-3, Figure 2-4, and Figure 2-5 layout a sample assessment. Figure 2-3 shows how entries might look in the Experience & Comfort Level Assessment VFR & MVFR table. Suppose a pilot’s flying takes place ... part of the country where clear skies and visibilities of 30 miles or more are normal. The entry might specify the lowest VFR ceiling as 7,000 feet, and the lowest visibility as 15 miles. A pilot may never experience…
- Chapter 11: Aircraft Performance › Climb Performance Factors › Range Performance
NOTE: The straight line that is tangent to the sea level power curve is also tangent to the altitude power curve. The effect of altitude on specific range can also be appreciated from the previous relationships. If a change ... altitude causes identical changes in speed and power required, the proportion of speed to power required would be unchanged. The fact implies that the specific range of a propeller-driven aircraft would be unaffected by altitude. Actually, this is true…
- Chapter 8: Flight Instruments › Types of Altitude
Indicated altitude—read directly from the altimeter (uncorrected) when it is set to the current altimeter setting. 2. True altitude—the vertical distance of the aircraft above sea level—the actual altitude. It is often expressed as feet above mean ... level (MSL). Airport, terrain, and obstacle elevations on aeronautical charts are true altitudes. 3. Absolute altitude—the vertical distance of an aircraft above the terrain, or above ground level (AGL). 4. Pressure altitude—the altitude indicated when the altimeter setting…
- Chapter 11: Aircraft Performance › Performance Charts › Sample Problem 7
Sample Problem 6 Fuel Carrying Capacity..................38 gallons, no reserve Find 5,000 feet pressure altitude in the first column on the left side of the table. Next, find the correct rpm of 2,400 in the second column. Follow ... table gives the correct cruise power settings, as well as the fuel flow and airspeed performance numbers at that altitude and airspeed. Sample Problem 7 Pressure Altitude at Cruise................................6,000 feet Refer to Figure 11-28 for this sample…