MD-80 MEMORY LIMITATIONS

• Tailwind (AFM) ....................10 kts
• CrossWind (max demo'd)........30 kts

• 275-285 kts
• .75 - .79 mach (whichever is lower)
• 10,000' and below - 250 or min maneuver whichever is greater

MD-82 and MD-83..............130,000 lbs

MD-82 and MD-83......................122,000 lbs

Maximum altitude for unpressurized flight is 14,000 feet.

APU air switch must be off for all in-flight operations

Autothrottle must be disconnected if engine stall (surge) is detected during takeoff.

500 feet AFL

• Automatic landings..................NONE
• ILS coupled approaches (other than Auto Land)
• IFR.......................................70 ft AFL
• VFR......................................50 fl AFL
• Non-Precision appr.................50 ft below MDA

Do not conduct an automatic landing if:

• Align (ALN) mode is not displayed on FMA by 100' radio alt
• Either engine becomes inop at > 50' above rwy
• Automatic ground spoilers are not armed and operational
• Any unusual control position or other abnormal conditions exist in the manual flt cnt sys
• RUDDER CONTROL MANUAL light illuminated
• Landing overweight

• Ground 500^{0 Momentary}
• Flight 625^{0 Momentary}

• Reserve Thrust 625C 5 minutes
• Red Radial (630) 2 minutes

• Max Thrust 590C 5 minutes
• orange radial 2 minutes

Below amber arc (580C) Continuous

540 C Continuous

• Flights scheduled for 4hrs or greater - 12 quarts
• Flight scheduled for < 4 hrs - 4qts + 2 qts/hr

• Do not operate thrust reversers in flight
• Do not exceed 1.3 EPR

• First attempt.....90 sec on, 5 mins off
• (90 seconds or 3 X 30 seconds)

Subsequent attempts....30 secs on, 5 mins off

Do not use flap settings between 13 and 15 degrees

Do not arm spoiler lever prior to gear extension

• Use spd brks only in UP/RET or 0/EXT configuration
• Do not extend or retract gear while speed brakes are deployed
• Moving Spd Brk/Spoiler Lever beyond EXT position in flight is prohibited. Full aft position for ground use only

• Main Wing Tanks........................1500 lbs
• Aux Tanks..................400 lbs

RAT is less than/equal to 6 deg C and visible moisture present, contaminated taxiways, or temp dew point spread is equal to or less than 3 deg C

RAT is less than or equal to 6 deg C and visible moisture is present

For ground, takeoff, and flight operations, engine anti-ice systems must be on when icing conditions exist or are anticipated.

• In Flight- airfoil anti-ice should be used when Icing Conditions exist or are anticipated
• Do not use until reaching 1000' AFL after takeoff
• Minimum duct pressure for airfoil Anti-ice = 20psi
• When in icing conditions maintain sufficient thrust to keep associated ICE PROTECT TEMP LOW light extinguished
• Application of tail De-ice is required:
• - once every 20 minutes
• - One minute prior to extending landing flaps
• - After leaving Icing conditions, prior to turning system off

Do not takeoff if any brake temperature exceeds 205 deg C

The maximum tire speed is 195 knots