Figure 35: Normal Landing Chart

2,800 2,400 2,000 1,600 1,200 800 400 0 0 20 40 60 80 100 24 26 28 30 32 34 0 10 20 30 OAT − °F HEADWIND − KTS WEIGHT X 100 LB TOTAL LANDING DISTANCE OVER A 50 FT OBSTACLE − FEET REFERENCE LINE REFERENCE LINE PRESSURE ALTITUDE − FT 8,000 6,000 4,000 2,000 S.L. IAS APPROACH SPEED (ASSUMES ZERO INSTR ERROR) WEIGHT (LB) KNOTS MPH 3,400 3,200 3,000 2,800 2,600 2,400 90 87 84 81 78 75 78 76 73 70 68 65 ASSOCIATED CONDITIONS: POWER AS REQUIRED TO MAINTAIN 800 FT/MIN DESCENT ON APPROACH FLAPS DOWN RUNWAY PAVED, LEVEL, DRY SURFACE APPROACH SPEED IAS AS TABULATED NOTE: GROUND ROLL IS APPROX 53% OF TOTAL LANDING DISTANCE OVER A 50 FT OBSTACLE. EXAMPLE: OAT 75 °F PRESSURE ALTITUDE 4,000 FT LANDING WEIGHT 3,200 LB HEADWIND 10 KNOTS TOTAL LANDING DISTANCE OVER A 50 FT OBSTACLE 1,475 FT GROUND ROLL (53% OF 1,475) 782 FT IAS TAKEOFF SPEED 87 MPH IAS