Super 80 Professional – AOM
PERFORMANCE
Section 23 Page 17
Super 80 Professional – Aircraft Operating Manual
Coolsky, 2018
MACH .80 CRUISE
PRESS
ALT
1000FT
STD
TAS
KTS
IAS
KTS
STD
RAT
°C
GROSS WEIGHT – 1000 POUNDS
146 142 138 134 130 126 122 118 114 110 106 102 98
94
90
37
459
260
-31
1)
2)
2.04
66.6
2.02
68.7
1.99
71.0
1.96
73.7
1.93
73.7
1.89
79.3
1.87
81.5
1.84
83.9
1.82
85.9
35
461
272
-28
2.04
60.5
2.02
62.3
1.99
64.3
1.97
66.4
1.94
68.7
1.91
71.1
1.88
73.2
1.86
74.9
1.84
76.8
1.82
78.6
1.79
80.3
1.78
82.0
33
465
285
-23
2.02
56.6
2.02
57.0
1.99
58.6
1.96
60.4
1.94
62.3
1.92
64.3
1.89
66.1
1.87
67.6
1.84
69.2
1.83
70.6
1.81
72.1
1.79
73.5
1.77
74.9
1.76
76.1
1.74
77.3
31
469
297
-19
1.98
53.9
1.96
55.4
1.94
57.0
1.92
58.6
1.89
60.2
1.87
61.4
1.85
62.8
1.83
64.0
1.82
65.2
1.80
66.4
1.78
67.6
1.77
68.6
1.76
69.7
1.74
70.7
1.73
71.7
1.72
72.6
29
474
311
-16
1.91
53.9
1.89
55.1
1.87
56.1
1.85
57.3
1.84
58.3
1.82
59.3
1.81
60.3
1.79
61.3
1.78
62.2
1.76
63.1
1.75
64.0
1.74
64.8
1.73
65.6
1.72
66.4
1.71
67.2
1.70
67.9
1)
EPR required
2)
Specific Range (NM/1000 LBS)
TO OBTAIN TOTAL FUEL FLOW:
Total Fuel Flow = TAS / Specific Range x 1000 (LBS/HR)
Correct STD TAS for deviation from standard temperature before computing total fuel flow.
Add 1 KTS for every 1°C above standard temperature, or subtract 1 KTS for every 1°C below
standard temperature.
ENGINE ALTITUDE CAPABILITY:
PRESS
ALT
1000 FT
TEMP DEV FROM STD - °C
-15 -10
-5
0
+5 +10 +15 +20
GROSS WEIGHT - 1000 POUNDS
37
130 124 124 122 116 114 110 102
35
142 142 142 132 128 128 124 110
33
149 148 144 142 134 128 124 116
31
149 149 149 149 136 130 122
29
142 134 146
27
142 140 126
25
140 124 120
NOTE:
The weights in this table are the maximum gross weights at which Mach .80 can be
achieved without exceeding maximum cruise