Push Spoiler lever down to disarm position. Rotate the autobrake selector to OFF.
[AS REQ] on Missed Approach.
MD-80 Sec. 4 Page 107
Flight Manual Continental Rev. 12/01/00 #29
AFTER TAKEOFF NOTES
Close in Turn After Takeoff
Normally, a turn after takeoff should not be started until reaching 400 feet AGL, even if ATC requests a turn as soon as practical. However, a turn required for obstructions, noise abatement, or adverse conditions may be started before reaching 400 feet AGL but no lower than 50 feet AGL. The maximum bank angle after takeoff will be 15 degrees until reaching V2 +10. At an airspeed of V2 +10 and above, bank angles of 30° are allowable.
Autopilot / FGS / Altitude Alerting Procedures
The minimum altitude for autopilot engagement is 1000 feet AGL. Normally, the autopilot is engaged during the takeoff profile after slats are retracted. The aircraft should be trimmed at the time of engagement. The autopilot is engaged by moving the autopilot switch to ON.
The altitude alerting system shall be used during all phases of flight to assist the flight crew in altitude awareness and to prevent deviation from assigned clearances. During climb and descent, the flight crew shall set and arm the next clearance altitude in the ALT selector window. In those situations where a clearance is received containing multiple crossing restrictions, the ALT selector window will be set and armed for the next altitude restriction and reset and armed for each subsequent restriction.
While the autopilot is ON, the PF will set and arm new clearance altitudes in the ALT selector window. While the autopilot is OFF the PM will set and arm the cleared altitude in the ALT selector window. If the pilot normally expected to set and arm the altitude is distracted by other duties, it is permissible for the other pilot to set and arm the altitude. Both pilots will verbally and visually acknowledge the cleared altitude set and armed in the ALT selector window.
Operation with Autopilot Not Engaged
The PF will verbally command the PM to operate the Flight Guidance System (FGS). Examples: “Heading select 280”, “Set and arm 5,000 feet, vertical speed 1,000 feet down”, “Arm ILS’, “Bank Angle 15°, Set missed approach altitude”, etc. The PM will make the changes to the FGS as called for by the PF. The PM will set and arm the FGS for any ATC directed altitude changes and the PF will visually and verbally confirm the FGS is set and armed for the new altitude. The PM will monitor the FGS and report any discrepancies to the PF.
Example: ATC gives a clearance to climb and maintain 15,000 feet. The PM would read back the climb clearance using proper ATC procedures, set and arm the FGS for 15,000 feet, and confirm the FMA is armed for altitude. The PF will visually confirm the FGS/FMA is armed for 15,000 feet and verbally confirm by response such as:
“ONE-FIVE-THOUSAND, SET AND ARMED”.
Operation with Autopilot Engaged
The PF will operate the FGS system making all FGS inputs including setting and arming altitudes. The PF will vocalize all altitude changes and may vocalize other FGS operations if desired. The PM will monitor the operation of the FGS and report any discrepancies to the PF.
Example: ATC gives a clearance to climb and maintain 15,000 feet. The PM would read back the climb clearance using proper ATC procedures, and visually confirm the FGS/FMA is armed for 15,000 feet. The PF will set and arm the FGS for 15,000 feet and verbally confirm by response such as “ONE-FIVE-THOUSAND, SET AND ARMED”.
PMS Operation
After 3,000 feet AGL, push the PERF button on the flight guidance panel to activate the PMS.
Note: For PMS activation, the following conditions are required:
.
Flaps less than 26°.
.
TRI not in T/O, TO FLEX or GA mode.
.
Flight director on or autopilot engaged.
.
PMS valid and autothrottle on within 5 seconds of PERF selection.
Below 10,000 feet MSL, airspeed will be limited to 250 KIAS and figures will be in brackets. The 250 KIAS restriction can be removed by pushing “Clear” and then pushing line select key “1” two times.
Maximum climbs can be selected by slewing to the “Climb Max” page and pushing line select key “1.” Non-optimum climbs can be selected by editing the speed in either the “Maximum” or “Optimum” pages. Line select key “1” must be pushed again when the light comes on to engage the mode.
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：MD-80 Flight Manual 麥道80飛行手冊 2(4)
