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28/EXT  80 120 160  6.8 6.8 6.8  58.2 66.6 72.7  115 141 162  0 0 0  16.8 17.7 18.6 
-217 & -217A FINAL APPROACH BASED ON 3° GLIDESLOPE. ADJUST POWER TO MAINTAIN PITCH ATTITUDE. FLY GLIDE SLOPE OR IF NOT AVAILABLE, FLY TO RATE OF DESCENT 
40/EXT  80 120 160  2.2 2.2 2.2  51.9 61.1 67.1  111 136 157  600 735 849  16.7 17.5 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 (%)  -2.2  -1.2  0  +1.0  +2.2 
D DESCENT (FPM)  -25  -20  0  +20  +25 

MD-80 Sec. 3 Page 109
Flight Manual Continental Rev. 05/15/95  #23

-217 GO-AROUND SPEED V2 + 20 FLAPS / SLATS 15 / EXT 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  23.8 18.7 14.8  91.9 92.0 92.2  148 157 179  5727 3255 2333  17.9 18.2 19.2
 5,000  80 120 160  22.0 16.6 12.3  94.2 94.4 94.6  140 157 179  4590 2882 1996  8.1 8.9 10.0 
10,000  80 120 160  19.6 14.1 11.4  92.9 93.0 93.1  132 157 179  3645 2271 1447  -1.7 -0.4 0.9 
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. 5,000 10,000  -3.2 -1.2 -0.2  -2.0 -1.2 -0.2  0 0 0  +1.2 +1.5 +1.5  +3.0 +0.5 +0.6 
D PITCH (DEG)  S.L. 5,000 10,000  +0.5 +0.5 +0.5  +0.3 +0.3 +0.3  +0.0 +0.0 +0.0  -0.2 -0.2 -0.2  -0.6 -0.6 -0.2 
D CLIMB (FPM)  S.L. 5,000 10,000  -110 +40 +100  -60 -20 +80  0 0 0  +60 +60 +20  -80 -80 +60 

Sec. 3 Page 110 MD-80
Rev. 05/15/95 #23 Continental Flight Manual

-217A GO-AROUND SPEED V2 + 20 FLAPS / SLATS 15 / EXT 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  24.1 18.6 14.8  92.0 92.1 92.3  146 157 179  5240 3268 2340  17.8 18.3 19.2
 5,000  80 120 160  22.6 16.9 13.5  95.8 96.0 96.2  139 157 179  4713 2989 2082  8.1 8.9 10.0 
10,000  80 120 160  19.9 14.2 11.5  93.9 94.3 94.5  132 157 179  3709 2345 1516  -1.7 -0.4 0.9 
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. 5,000 10,000  -3.2 -3.4 -3.8  -1.6 -1.7 -1.8  0 0 0  +1.6 +1.4 +1.6  +0.6 +0.2 +3.4 
D PITCH (DEG)  S.L. 5,000 10,000  0 0 0  0 0 0  0 0 0  0 0 0  -0.6 -0.6 0 
D CLIMB (FPM)  S.L. 5,000 10,000  -120 -120 -80  -60 -60 -60  0 0 0  +60 +60 +60  -80 -120 +80 

MD-80 Sec. 3 Page 111
Flight Manual Continental Rev. 05/15/95  #23

CADC FAILURE

Note:  After failure of one or both CADCs, AHRS 1 and 2 will revert to basic mode. It may require up to 5 minutes for system to revert.
Failure of the No. 1 CADC will be indicated by the following flags in the Captain’s instruments:
.
Mach Off Flag

.
A/S Flag

.
Altimeter Off Flag

.
Vertical Speed Off Flag

.
GPWS Light On

.
Auto Slat Fail Light On

Failure of the No. 2 CADC will be indicated by the following flags in the First Officer’s instruments:

.
Mach Off Flag

.
A/S Flag

.
Altimeter Off Flag

.
Vertical Speed Off Flag

.
Auto Slat Fail Light On

CADC Selector............................................BOTH ON 1 OR BOTH ON 2

Select unaffected system.
Transponder.................................................SELECT OPERABLE CADC

* * * *
Sec. 3 Page 112 MD-80
Rev. 08/01/98 #27 Continental Flight Manual

DIGITAL LIGHTS BLANKOUT / FAILURE
　
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