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PSP 604-15 STEEP APPROACH
STEEP APPROACH (5.5°) LANDING SPEEDS AND DISTANCES
ALTITUDE – 5,000 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 300 ft for every 1% DOWNHILL
No correction for UPHILL gradient
Wind Correction: No TAILWIND allowed
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 for steep
approach operations
QR1_DX_006
SUPP-02-6
REV 76, Jul 17/09
QUICK REFERENCE HANDBOOK
PSP 604-15 STEEP APPROACH
CONTAMINATED RUNWAY CORRECTIONS
TAKE-OFF CORRECTIONS – WET RUNWAY
V1 DRY 110 115 120 125 130 135 140 145 150 155 160
V1 WET 113 113 113 117 122 127 133 138 146 152 158
Distance 1.22 1.22 1.07 1.07 1.07 1.07 1.07 1.07 1.07 1.07 1.07
DISPATCH WITH ONE THRUST REVERSER INOPERATIVE
FOR V1 < 115 KIAS, ΔDistance = 660 ft and ΔV1 = 0 KIAS
FOR V1 ≥ 115 KIAS, ΔDistance = 660 ft and ΔV1 = –2.0 KIAS
TAKE-OFF CORRECTIONS – 0.125 IN. WATER OR EQUIVALENT
V1 DRY 110 115 120 125 130 135 140 145 150 155 160
V1 0.125IN 113 113 113 114 119 124 130 136 142 148 155
Distance 1.58 1.58 1.58 1.38 1.38 1.38 1.38 1.38 1.38 1.38 1.38
EQUIVALENT: 0.125 IN SLUSH, 0.25 IN WET SNOW, 0.60 IN DRY SNOW
DISPATCH WITH ONE THRUST REVERSER INOPERATIVE
FOR V1 < 117 KIAS, ΔDistance = 2300 ft and ΔV1 = 0 KIAS
FOR V1 ≥ 117 KIAS, ΔDistance = 1970 ft and ΔV1 = –6.0 KIAS
TAKE-OFF CORRECTIONS – 0.25 IN. WATER OR EQUIVALENT
V1 DRY 110 115 120 125 130 135 140 145 150 155 160
V1 0.25IN 110 114 118 122 127 132 136 141 146 151 156
Distance 1.56 1.56 1.56 1.56 1.56 1.56 1.56 1.56 1.56 1.52 1.48
EQUIVALENT: 0.25 IN SLUSH, 0.50 IN WET SNOW, 1.20 IN DRY SNOW
DISPATCH WITH ONE THRUST REVERSER INOPERATIVE
FOR V1 < 115 KIAS, ΔDistance = 1640 ft and ΔV1 = 0 KIAS
FOR V1 ≥ 115 KIAS, ΔDistance = 1970 ft and ΔV1 = –3.0 KIAS
TAKE-OFF CORRECTIONS – RUNWAY COVERED WITH ICE
V1 DRY 110 115 120 125 130 135 140 145 150 155 160
V1 ICE 113 113 111 111 111 111 111 119 129 140 151
Distance 2.05 2.05 1.92 1.78 1.64 1.50 1.50 1.50 1.50 1.50 1.50
DO NOT DISPATCH WITH ONE THRUST REVERSER INOPERATIVE
SUPP-03-1
REV 69, Jun 04/07
QUICK REFERENCE HANDBOOK
PSP 604-15 CONTAMINATED RUNWAY
CONTAMINATED RUNWAY CORRECTIONS
TAKE-OFF CORRECTIONS – RUNWAY COVERED BY
COMPACTED SNOW
V1 DRY 110 115 120 125 130 135 140 145 150 155 160
V1 WET 113 113 110 114 119 125 130 136 143 150 157
Distance 1.32 1.32 1.12 1.12 1.12 1.12 1.12 1.12 1.12 1.12 1.12
DISPATCH WITH ONE THRUST REVERSER INOPERATIVE
FOR V1 < 116 KIAS, ΔDistance = 980 ft and ΔV1 = 0 KIAS
FOR V1 ≥ 116 KIAS, ΔDistance = 980 ft and ΔV1 = –4.0 KIAS
LANDING CORRECTIONS
CONTAMINANT
TWO THRUST
REVERSERS
ONE THRUST
REVERSER
ICE 2.30 2.90
COMPACTED SNOW 1.54 1.64
LOOSE SNOW 1.82 2.06
SLUSH
STANDING WATER
1.92 2.24
SUPP-03-2
REV 69, Jun 04/07
QUICK REFERENCE HANDBOOK
PSP 604-15 CONTAMINATED RUNWAY
GO / NO GO GUIDE
This Go / No Go Guide contains data for quick reference.
This guide in no way supersedes data outlined in the MMEL.
In case of conflict, the MMEL takes precedence.
AFTER PERFORMING THE APPLICABLE QRH PROCEDURE
and the message persists, check dispatchability as follows:
WARNING MESSAGES (RED)
EICAS MESSAGE DISPATCH AND / OR MEL REF
AFCS MSGS FAIL 22–10–1
ANTI-ICE DUCT NO GO
APU FIRE NO GO
APU OVERSPEED 49–00–2
APU OVERTEMP 49–00–2
CABIN ALT NO GO
CONFIG (AP, FLAPS,
SPOILERS, STAB). NO GO
DIFF PRESS NO GO
EMER PWR ONLY NO GO
ENG OIL PRESS L (R) NO GO
ENGINE NO GO
ENGINE FIRE L (R) NO GO
ENGINE START SOV L (R) NO GO
GEAR DISAGREE NO GO
JETPIPE OVHT L (R) NO GO
MLG BAY OVHT NO GO
NOSE DOOR OPEN NO GO
PARKING BRAKE NO GO
PASSENGER DOOR NO GO
WING OVHT NO GO
10TH (14TH) DUCT L (R) NO GO
GO / NO GO-1
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15 GO / NO GO GUIDE
GO / NO GO GUIDE (CONT'D)
　
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