Other rate-of-climb charts use density altitude as a starting point. [Figure 8-6] While it cleans up the chart somewhat, you must first determine density altitude. Notice also that this chart requires a change in the indi- cated airspeed with a change in altitude. affected by atmospheric wind is the angle of climb and not the rate of climb. Determine the best rate of climb using figure 8-5. Use the following conditions: With this chart, first locate the temperature of +10°C (point A). Then proceed up the chart to the 12,000-foot pressure altitude line (point B). From there, move hori- zontally to the right until you intersect the 3,000-foot line (point C). With this performance chart, you must now determine the rate of climb with anti-ice off and then subtract the rate of climb change with it on. From point C, go to the bottom of the chart and find that the maximum rate of climb with anti-ice off is approxi- mately 890 feet per minute. Then, go back to point C and up to the anti-ice-on line (point D). Proceed hori- zontally to the right and read approximately 240 feet per minute change (point E). Now subtract 240 from 890 to get a maximum rate of climb, with anti-ice on, of 650 feet per minute. 8-6 Figure 8-5. Maximum Rate-of-Climb Chart. Figure 8-6. This chart uses density altitude in determining maximum rate of climb. RATE OF CLIMB — MAXIMUMGLYPH<.notdef> TAKEOFF POWER  –40 –20 0 20 40 0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 OAT —  C ANTI-ICE OFF RATE OF CLIMB — FT./MIN. (X 100) 0 100 200 300 400 500 R/Correction — FT./MIN. This Chart is Based on:GLYPH<.notdef>  Indicated Airspeed 60 MPH 52 KNOTSGLYPH<.notdef> N2 ENGINE RPM 100% P R E S U R E A L T $_{I}$T U D $_{E}$— F T . 2 0 $_{,}$0 0 1 8 $_{,}$0 0 1 6 $_{,}$0 0 1 4 , 0 0 1 2 , 0 0 1 0 , 0 6 , 0 0 4,000 2,000 S.L. G R O S S W E I G H T P O U N D S 2 , 0 0 0 2 , 2 0 0 2 , 4 0 0 2 , 6 0 0 2 , 8 0 0 3 , 0 0 0 3 , 2 0 0 8 , 0 0 (P oint A) (P oint B) (P oint C) (P oint D) (P oint E) 890 ft/min.GLYPH<.notdef> – 240 ft/min.GLYPH<.notdef> 650 ft/min. HO TGLYPH<.notdef> DA Y ANTI-ICE ON 400 600 800 1,000 1,200 1,400 12,000GLYPH<.notdef> GLYPH<.notdef> 10,000GLYPH<.notdef> GLYPH<.notdef> 8,000GLYPH<.notdef> GLYPH<.notdef> 6,000GLYPH<.notdef> GLYPH<.notdef> 4,000GLYPH<.notdef> GLYPH<.notdef> 2,000GLYPH<.notdef> GLYPH<.notdef> 0 Rate of Climb, Feet Per Minute Density Altitude — Feet RATE OF CLIMB/DENSITY ALTITUDEGLYPH<.notdef> 2,350 LBS. GROSS WEIGHTGLYPH<.notdef> BEST RATE OF CLIMB SPEED VARIES WITHGLYPH<.notdef> ALTITUDE; 57 MPH AT S.L. DECREASING TO 49GLYPH<.notdef> MPH, IAS AT 12,000 FT. Pressure Altitude................................12,000 feet Outside Air Temperature ...........................+10°C Gross Weight..................................3,000 pounds Power ...........................................Takeoff Power Anti-ice ..........................................................ON Indicated Airspeed .................................52 knots SAMPLE PROBLEM 4