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Abnormal
Flaps UP
Altitude F39°
Shake
F39°
Push VAPP VREF VAPP VREF VAPP VREF VAPP VREF
0 129 121 167 157 171 161 178 168 188 178
2000 129 121 167 157 171 161 178 168 188 178
4000 129 121 167 157 172 162 179 169 190 180
6000 130 121 168 158 174 164 181 171 192 182
8000 131 123 169 159 175 165 183 173 194 184
10000 132 124 171 161 177 167 185 175 197 187
12000 134 125 173 163 179 169 187 177 199 189
14000 135 126 174 164 180 170 190 180 202 192
15000 136 127 175 165 181 171 191 181 203 193
CAUTION: Fuseplug Release Possible
With Max. Braking
CAUTION: Tire Speed Limit
Quick Reference Handbook
NON-SP GIV PERFORMANCE REVISION 7
Page PC - 6 (NON-SP GIV AIRPLANES ONLY) May 30/02
Non-SP GIV Landing Distance Using Twin-Engine
Reverse Thrust Only (No Braking) OM 07-01-80
The table on the following page shows landing distances when using
reverse thrust only to bring the aircraft to a stop. The distances shown
below assume reverse thrust is used to 20 knots with stowage by 10
knots.
Conditions:
• Two Engine Reverse Thrust Only
• No Slope
• No Wind
• Standard Day Temperature
• AUTO Ground Spoilers
• No Runway Surface Contamination Accumulation
• Full Reverse Thrust To 20 Knots
• Stowage By 10 Knots
• Minimal Braking Below 10 Knots
• Flaps 39°
NOTE: Flight Manual procedures recommend that cancellation of thrust
reversers be initiated by 70 knots so as to be completely cancelled by the
time normal taxi speed is achieved. If landing runway conditions will result in
compromised braking performance, this table may be used to provide
additional information for pilot judgement.
Quick Reference Handbook
REVISION 7 NON-SP GIV PERFORMANCE
May 30/02 (NON-SP GIV AIRPLANES ONLY) Page PC - 7
Non-SP GIV Landing Distance Using Twin-Engine Reverse Thrust
Only (No Braking), ctd… OM 07-01-90
Landing Distance (Feet)
ALT Gross Weight (lb)
(Ft) 74,600 73,200 70,000 66,000 65,000 60,000
15,000 15,166 14,850 14,122 13,209 12,985 11,890
14,000 14,346 14,045 13,359 12,501 12,287 11,264
12,000 12,837 12,569 11,960 11,204 11,019 10,112
10,000 11,495 11,255 10,719 10,052 9,886 9,082
8,000 10,524 10,309 9,823 9,215 9,068 8,342
6,000 9,847 9,649 9,199 8,639 8,500 7,831
4,000 9,265 9,081 8,665 8,144 8,015 7,395
2,000 8,771 8,601 8,213 7,727 7,608 7,028
0 8,320 8,161 7,795 7,343 7,230 6,692
Landing Distance (Feet)
ALT Gross Weight (lb)
(Ft) 58,500 55,000 50,000 45,000 40,000
15,000 11,564 10,813 9,787 8,776 7,827
14,000 10,952 10,250 9,282 8,330 7,440
12,000 9,837 9,212 8,359 7,516 6,732
10,000 8,841 8,289 7,532 6,788 6,093
8,000 8,122 7,623 6,940 6,270 5,648
6,000 7,630 7,169 6,541 5,925 5,358
4,000 7,207 6,784 6,204 5,638 5,116
2,000 6,855 6,458 5,920 5,398 4,921
0 6,530 6,160 5,657 5,178 4,744
Quick Reference Handbook
NON-SP GIV PERFORMANCE REVISION 7
Page PC - 8 (NON-SP GIV AIRPLANES ONLY) May 30/02
Non-SP GIV Aircraft Classification Number (ACN)
GIV-GER-481
Aircraft Classification Number (ACN) is a number expressing the
relative effect of an aircraft on a pavement for a specified subgrade
category. ACN values are calculated for both flexible and rigid
pavement. If the aircraft gross weight and runway subgrade strength
are known, the ACN value can be determined from the charts on the
following pages.
Pavement Classification Number (PCN) is a number expressing the
bearing strength of a pavement for unrestricted operations. It is
reported in the Jeppesen charts in a format such as 24/F/C/Y/T,
where:
24 is the PCN
F is the type of pavement, where:
R = Rigid
F = Flexible
C is the subgrade strength, where:
D = Ultra Low
C = Low
B = Medium
A = High
Y is the tire pressure, where:
W = High, no pressure limit
X = Medium, limited to 217 psi
Y = Low, limited to 145 psi
Z = Very Low, limited to 73 psi
T is the PCN classification, where:
T = Technical Evaluation
U = Aircraft Experience
Non-SP GIV ACN values are:
Flexible Pavement Rigid Pavement
Subgrade D 21 23
Subgrade C 22 24
Subgrade B 23 25
Subgrade A 24 26
(Based on 73,600 lb gross weight and 175 psi tire pressure.)
ACN values must be less than or equal to the airport PCN for
unrestricted use. ACN input variables are gross weight, percent load
on main wheels, wheel spacing and maximum tire pressure.
Quick Reference Handbook
REVISION 8 NON-SP GIV PERFORMANCE
Oct 11/02 (NON-SP GIV AIRPLANES ONLY) Page PC - 9
　
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