Sec. 3 Page 106 MD-80
Rev. 05/15/95 #23 Continental Flight Manual
-217A MAX CLIMB SPEED 1.5 VS + 10 FLAPS / SLATS 0 / RET FLY TO PITCH ATTITUDE
ALTITUDE (FT) WEIGHT (1000 LB.) TARGET PITCH ATTITUDE (DEG) APPROX N1 RPM REQUIRED (%) APPROX AIRSPEED (KIAS) APPROX RATE OF CLIMB (FPM) STD TAT (°C)
0 80 120 160 20.1 12.7 9.3 85.7 85.5 85.5 194 235 270 5660 3798 2684 19.9 22.2 24.5
5,000 80 120 160 17.7 11.3 8.4 86.3 86.4 86.4 194 235 270 5223 3470 2419 10.8 13.5 16.2
10,000 80 120 160 15.2 9.8 7.3 87.2 87.3 87.3 194 235 270 4676 3018 2030 1.8 5.0 8.1
15,000 80 120 160 12.9 8.4 8.3 88.4 88.2 88.1 195 237 273 4076 2528 1605 -6.9 -3.3 0.4
CHANGE TO N1 RPM, PITCH ATTITUDE, AND RATE OF CLIMB DUE TO DIFFERENCE BETWEEN INDICATED TAT AND STD TAT
Subtract the STD TAT presented above from the indicated TAT to calculate DTAT
ALTITUDE (FT) DTAT IN .C
-20 -10 0 +10 +20
DN1 (%) S.L. 15,000 +1.8 +2.2 +1.4 +0.6 0 0 -0.2 -2.6 +1.2 +1.2
DPITCH (DEG) S.L. 15,000 +2.1 +1.0 +1.5 +0.5 0 0 -1.0 -0.6 -1.0 -0.4
DCLIMB (FPM) S.L. 15,000 +740 +300 +500 +250 0 0 -240 -230 -260 -220
MD-80 Sec. 3 Page 107
Flight Manual Continental Rev. 05/15/95 #23
-217 & -217A CRUISE ADJUST POWER TO MAINTAIN FLAPS / SLATS 0 / RET PITCH ATTITUDE, LEVEL FLIGHT
ALTITUDE (FT) WEIGHT (1000 LB.) TARGET PITCH ATTITUDE (DEG) APPROX N1 RPM REQUIRED (%) APPROX AIRSPEED (KIAS) APPROX RATE OF DESCENT (FPM) STD TAT (°C)
20,000 80 120 160 0.6 1.9 3.3 71.8 73.8 77.5 285 0 -5.5
25,000 80 120 160 0.6 2.0 3.4 74.4 77.0 80.5 285 0 -12.3
30,000 80 120 160 0.7 2.1 3.6 77.1 79.9 84.6 285 0 -18.5
35,000 80 120 1.2 2.8 78.2 84.5 268 .79M 0 -27.5
-217 &-217A DESCENT FLY TO PITCH ATTITUDE FLAPS / SLATS 0 / RET
10,000 80 120 160 -4.8 -2.2 -0.3 IDLE THRUST 285 3031 2283 1974 9.4
20,000 80 120 160 -4.2 -1.7 0.1 IDLE THRUST 285 3200 2426 2144 -5.5
30,000 80 120 160 -3.5 -1.1 0.7 IDLE THRUST 285 3273 2509 2239 -18.4
CHANGE TO N1 RPM AND RATE OF DESCENT DUE TO DIFFERENCE BETWEEN INDICATED TAT AND STD TAT
Subtract the STD TAT presented above from the indicated TAT to calculate DTAT
DTAT IN °C
-20 -10 0 +10 +20
DN1 RPM (%) -3.2 -1.8 0 +1.8 +3.2
D DESCENT (FPM) -100 -50 0 +50 +100
Sec. 3 Page 108 MD-80
Rev. 05/15/95 #23 Continental Flight Manual
217 & -217A HOLDING FLAPS / SLATS 0 / RET ADJUST POWER TO MAINTAIN PITCH ATTITUDE, LEVEL FLIGHT
ALTITUDE (FT) WEIGHT (1000 LB.) TARGET PITCH ATTITUDE (DEG) APPROX N1 RPM REQUIRED (%) APPROX AIRSPEED (KIAS) APPROX RATE OF DESCENT (FPM) STD TAT (°C)
10,000 80 120 160 4.1 4.1 4.1 56.4 64.5 70.3 184 225 260 0 0 0 1.2 4.2 7.2
-217 &-217A TERMINAL AREA FLIGHT PATTERN ALTITUDE ADJUST POWER TO MAINTAIN PITCH ATTITUDE, LEVEL FLIGHT
0/RET 80 120 160 4.1 4.1 4.1 50.3 59.0 65.1 184 225 260 0 0 0 19.4 21.6 23.8
15/EXT 80 120 160 8.3 8.3 8.3 53.4 62.4 68.6 123 151 174 0 0 0 17.0 18.0 19.0
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