Aircraft Performance Calculations and Charts Guide
"Explore selected performance examples including V1 and VR calculations, corrections, climb and cruise EPR, ground distance covered, and stall speed reference for aircraft operating conditions. Get insights into aircraft performance with detailed charts and calculations."
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SELECTED PERFORMANCE EXAMPLES
QNH 1020 => CORRECTION -200FT PA = 4,200 200 = 4,000 FT
V1 corrections: Temp & PA: +2 Slope: 0 HW (15 kts): +0.45 Ice: +0.80 V1 = 136.75kts VR corrections: Temp & PA: +2 Slope: 0 HW (15 kts): 0 Ice: +0.80 VR = 141.80kts REVISED V1 AND VR: 136.75 & 141.8
(REFER TO FIGURES 59 AND 60.) WHAT IS THE MAX CLIMB EPR FOR OPERATING CONDITIONS T-1?
(REFER TO FIGURES 59 AND 60.) WHAT IS THE MAX CRUISE EPR FOR OPERATING CONDITIONS T-3?
(REFER TO FIGURES 48, 49, AND 50.) WHAT IS THE GROUND DISTANCE COVERED DURING EN ROUTE CLIMB FOR OPERATING CONDITIONS W-5?
No wind data: Distance: 73.9NM / Time: 11.3 min = 6.54NM/min No wind GS = 6.54NM/min x 60 min = 392.4 knots Adjusting for headwind: 392.4 knots 40 knots (HW) = 352.4 knots 352.4knots x 11.3 min = 66.4NM traveled SOLUTION: 66.4NM
(REFER TO FIGURE 465.) AT A WEIGHT OF 60,000 POUNDS WITH 35 FLAPS, THE REFERENCE STALL SPEED IS 96 KNOTS
