8.
Minimum enroute temperature............................................... -76. C
9.
Maximum airspeed: Vmo.........................................340 KIAS
Mmo ......................................... mach .84
10.
Max turbulent air speed - Vb............................285 KIAS / mach .79
11.
Design maneuvering speed - Va ........................................ 260 KIAS
12.
The maximum operating limit speed (Vmo/Mmo) may not be deliberately exceeded in any regime of flight (climb, cruise, or descent).
13.
Flight load acceleration limits:
Flaps up .................................................................. +2.5 G to -1.0 G
Flaps down.............................................................. +2.0 G to 0.0 G
14.
Maximum Takeoff/Landing Tailwind Component............... 10 knots
15.
Additional landing crosswind limitations:
Manual rudder .................................................................... 25 knots
Autoland............................................................................. 15 knots
Restricted rudder travel ....................................................... 12 knots
Instrument approach at or below 2400 RVR ........................ 10 knots
(Continued)
16.
Maximum headwind for CAT II approach..........................20 knots
17.
Maximum standing water, slush, or wet snow:
Takeoff .............................................................................. 1/2 inch
Landing ................................................................................ 1 inch
18.
Maximum dry snow (takeoff or landing) ............................ 4 inches
19.
Takeoff with Windshear Warning Alert active is not authorized.
Operating Parameters
1. Maximum Demonstrated Takeoff/Landing Crosswind
Component:
Dry Runway.......................................................................30 knots
Wet Runway.......................................................................20 knots
Icy Runway ........................................................................12 knots
2. Required runway lengths for LAHSO:
Elevation < 2,000 ft.............................................................7100 ft.
Elevation > 2,000 ft.............................................................7700 ft.
GROSS WEIGHT AND C.G. LIMITATIONS
1.
Gross weights:
2.
Maximum takeoff and landing weights may be further restricted by runway selection, weather conditions, abnormal aircraft configurations, minimum equipment list, configuration deviation list, center of gravity limits, and fuel density.
3.
The airplane configuration specified in Section 4 of this manual for various flight profiles is the configuration on which the allowable weights shown in the airport analysis section of the Weight and Balance manual are based. The prescribed configuration must be used to assure the aircraft performance requirements are met.
4.
Compliance with the center of gravity limits is assured by operation under an approved load planning system.
5.
If landing weight exceeds the values prescribed by Quick Turn Around Weight Limits chart, examination of the wheel thermal plugs and a waiting period of 27 minutes is required before a subsequent takeoff unless procedures are followed using the brake temperature monitoring system or the pyrometer measuring system.
802-812 816-843 871 878-879 883-884 892-895 872-875 870 876, 877 885-891 801 813-815 880-882
Maximum Ramp 150,500 150,500 148,000 148,000 148,000 143,000
Maximum Takeoff 149,500 149,500 147,000 147,000 147,000 142,000
Maximum Landing 130,000 130,000 130,000 128,000 128,000 128,000
Maximum Zero Fuel 122,000 118,000 120,000 120,000 118,000 120,000
DC-9-82 Quick Turn Around Weight Limits
LBS X 1,000
Landing Flap 28.
, Slats Extended
AMB TEMP F Pressure Altitude Ft.
0 1000 2000 3000 4000 5000 6000 7000 8000
-10 ML ML ML ML ML ML ML ML ML
0 ML ML ML ML ML ML ML ML 145.8
10 ML ML ML ML ML ML ML ML 144.1
20 ML ML ML ML ML ML ML 145.2 142.5
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