* * * *
IF Panel Does Not Retract: Continue at .
(Continued)
MD-80 Sec. 3 Page 51
Flight Manual Continental Rev. 05/15/95 #23
.
IF Time Does Not Permit and/or Panel Remains Extended: Hydraulic Pumps...........................................ON, HI, HI, ON Aileron / Rudder Trim .................................. AS REQUIRED Trim aircraft using aileron trim and control wheel displacement. Approximately 100 degrees of control wheel angle is available. Expect to use full aileron trim and up to 70 degrees of control wheel angle at approach speed. Some rudder trim may be required to counteract spoiler drag and aileron trim.
Landing Flaps, Speed ...................................28.,
28 REF + 10
Note: Spoilers may be armed for landing.
* * * *
Sec. 3 Page 52 MD-80
Rev. 05/15/95 #23 Continental Flight Manual
SPOILER / SPEED BRAKE LEVER NOT FULLY DISARMED
Note: This could be caused by failure of ground spoiler actuator to retract. Red arming placard is partially exposed until ground spoiler actuator is retracted.
IF Autobrakes Installed:
Spoiler / Speed Brake Lever .................... SQUEEZE, OBSERVE
Squeeze lever to retract ground spoiler actuator. Observe position of lever. Lever Fully Disarmed: Continue normal operation.
* * * *
IF Lever Not Fully Disarmed (All Airplanes):
Caution: If speedbrake lever is not fully down, the speedbrake aft stop and intermediate notches will not be engaged. Caution should be exercised to ensure lever is not inadvertently moved to full aft position as this would permit speedbrakes to extend to full, 60 degree position.
When speedbrakes are required, pull lever UP and AFT to approximate speedbrake stop position. Lever must be held in this position as long as speedbrakes are required.
* * * *
MD-80 Sec. 3 Page 53
Flight Manual Continental Rev. 08/01/98 #27
STABILIZER INOPERATIVE
Primary Trim is Normal:
Continue normal operation.
* * * *
Alternate Trim is Normal:
Allow for slower trim rate. Autopilot may be used, as desired.
* * * *
Neither Trim System Operates:
Consider stabilizer jammed.
IF Flaps are At 28. or 40. and the Aircraft Is On Speed and Trimmed:
Land with selected flaps.
OR
* * * *
IF Flaps are At Any Other Setting Or the Aircraft is Not Trimmed:
Land with flaps 15°. Vref is 15°/T.O. maneuver speed increased by
increment from the following table.
(Continued)
STABILIZER TRIM (Red Guarded) Switch..........................NORM Primary Longitudinal Trim / Autopilot & Alternate Longitudinal Trim Circuit Breakers......................................RESET IF TRIPPED
EPC D-9,10,11 G-22,23 / L GEN BUS Row 4
Autopilot....................................................................................... OFF
Sec. 3 Page 54 MD-80
Rev. 08/01/98 #27 Continental Flight Manual
Note: Use takeoff C.G. if landing C.G. is unknown:
STABILIZER ANGLE IN DEGREES
AND ANU
2 1 0 1 2 3 4 5 6 7 8
C G % M A C -.8 40 35 30 25 21 17 14 10 7 4 2
0 40 34 29 24 20 16 13 9 6 3 0
5 32 27 22 18 14 10 7 4 1 0 0
10 24 19 15 11 7 4 1 0 0 0 0
15 17 12 8 4 1 0 0 0 0 0 0
20 8 4 0 0 0 0 0 0 0 0 0
SPEED INCREMENT IN KNOTS
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