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Gradient Correction: Increase by 750 ft for every 1% DOWNHILL
No correction for UPHILL gradient
Wind Correction: Increase by 140 ft for every knot TAILWIND
Decrease by 10 ft for every knot HEADWIND
(refer to PERF–07–3 for wind component
conversions)
LFL = Landing Field Length – Feet – Zero wind
Dry runway = ALD dry / 0.6
Wet runway = 1.15 × ALD dry / 0.6
Shaded area indicates landing data above maximum landing weight
QR1_DXLDG_002
PERF-06-2
REV 76, Jul 17/09
QUICK REFERENCE HANDBOOK
PSP 604-15
APPROACH AND LANDING
DATA
LANDING SPEEDS AND DISTANCES
ALTITUDE – 1,000 FEET
VREF = Speed at 50 ft screen height – KIAS
VAC = Approach climb speed (Flap 20°) – KIAS
VFTO = Final segment speed (Flap 0°) – KIAS
ALD = Actual Landing Distance – Feet – Zero wind and zero runway gradient
Gradient Correction: Increase by 750 ft for every 1% DOWNHILL
No correction for UPHILL gradient
Wind Correction: Increase by 140 ft for every knot TAILWIND
Decrease by 10 ft for every knot HEADWIND
(refer to PERF–07–3 for wind component
conversions)
LFL = Landing Field Length – Feet – Zero wind
Dry runway = ALD dry / 0.6
Wet runway = 1.15 × ALD dry / 0.6
Shaded area indicates landing data above maximum landing weight
QR1_DXLDG_003
PERF-06-3
REV 76, Jul 17/09
QUICK REFERENCE HANDBOOK
PSP 604-15
APPROACH AND LANDING
DATA
LANDING SPEEDS AND DISTANCES
ALTITUDE – 2,000 FEET
VREF = Speed at 50 ft screen height – KIAS
VAC = Approach climb speed (Flap 20°) – KIAS
VFTO = Final segment speed (Flap 0°) – KIAS
ALD = Actual Landing Distance – Feet – Zero wind and zero runway gradient
Gradient Correction: Increase by 750 ft for every 1% DOWNHILL
No correction for UPHILL gradient
Wind Correction: Increase by 140 ft for every knot TAILWIND
Decrease by 10 ft for every knot HEADWIND
(refer to PERF–07–3 for wind component
conversions)
LFL = Landing Field Length – Feet – Zero wind
Dry runway = ALD dry / 0.6
Wet runway = 1.15 × ALD dry / 0.6
Shaded area indicates landing data above maximum landing weight
QR1_DXLDG_004
PERF-06-4
REV 76, Jul 17/09
QUICK REFERENCE HANDBOOK
PSP 604-15
APPROACH AND LANDING
DATA
LANDING SPEEDS AND DISTANCES
ALTITUDE – 4,000 FEET
VREF = Speed at 50 ft screen height – KIAS
VAC = Approach climb speed (Flap 20°) – KIAS
VFTO = Final segment speed (Flap 0°) – KIAS
ALD = Actual Landing Distance – Feet – Zero wind and zero runway gradient
Gradient Correction: Increase by 750 ft for every 1% DOWNHILL
No correction for UPHILL gradient
Wind Correction: Increase by 140 ft for every knot TAILWIND
Decrease by 10 ft for every knot HEADWIND
(refer to PERF–07–3 for wind component
conversions)
LFL = Landing Field Length – Feet – Zero wind
Dry runway = ALD dry / 0.6
Wet runway = 1.15 × ALD dry / 0.6
Shaded area indicates landing data above maximum landing weight
QR1_DXLDG_005
PERF-06-5
REV 76, Jul 17/09
QUICK REFERENCE HANDBOOK
PSP 604-15
APPROACH AND LANDING
DATA
LANDING SPEEDS AND DISTANCES
ALTITUDE – 6,000 FEET
VREF = Speed at 50 ft screen height – KIAS
VAC = Approach climb speed (Flap 20°) – KIAS
VFTO = Final segment speed (Flap 0°) – KIAS
ALD = Actual Landing Distance – Feet – Zero wind and zero runway gradient
Gradient Correction: Increase by 750 ft for every 1% DOWNHILL
No correction for UPHILL gradient
Wind Correction: Increase by 140 ft for every knot TAILWIND
Decrease by 10 ft for every knot HEADWIND
(refer to PERF–07–3 for wind component
conversions)
LFL = Landing Field Length – Feet – Zero wind
Dry runway = ALD dry / 0.6
Wet runway = 1.15 × ALD dry / 0.6
Shaded area indicates landing data above maximum landing weight
QR1_DXLDG_006
PERF-06-6
REV 76, Jul 17/09
QUICK REFERENCE HANDBOOK
PSP 604-15
APPROACH AND LANDING
DATA
LANDING SPEEDS AND DISTANCES
ALTITUDE – 8,000 FEET
VREF = Speed at 50 ft screen height – KIAS
VAC = Approach climb speed (Flap 20°) – KIAS
VFTO = Final segment speed (Flap 0°) – KIAS
ALD = Actual Landing Distance – Feet – Zero wind and zero runway gradient
Gradient Correction: Increase by 750 ft for every 1% DOWNHILL
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庞巴迪挑战者快速检查单Quick Reference Handbook(23)
