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时间:2011-04-23 10:12来源:蓝天飞行翻译 作者:航空
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X-PT* procedure cannot be used before last planned TOC on PMS profile has been reached. If X-PT* data is entered prior to last planned TOC, PMS will display X-PT BEFORE TOC in scratchpad.
If X-PT BEFORE TOC is displayed, pushing CLEAR key will remove message from scratchpad.
If a X-PT* is desired:
WAYPOINTS Page:
Note:  If a X-PT* is created on a WPTS page, PMS will automatically place X-PT* in proper sequence according to its altitude.
Altitude / Distance....................................ENTER INTO SCRATCHPAD

Enter altitude, / and distance into scratchpad using data entry keys.
Line Select Key .................................................................................PUSH

Push any Line Select key and observe X-PT* and its corresponding altitude / distance and time have been placed in their proper sequence and are now displayed on Data Line 2.
CRZ or DES Page:
Altitude / Distance....................................ENTER INTO SCRATCHPAD

Enter altitude, / and distance into scratchpad using data entry keys.
Line Select Key 3 ..............................................................................PUSH

Push Line Select key 3 and observe PMS automatically transitions to
basic waypoints page with X-PT* event displayed on Data Line 2.
Note:  After a X-PT* has been created, altitude and/or distance may be edited (one at a time) on WPTS page.
(Continued)
If an altitude or distance edit is desired:
Altitude or / Distance.............................ENTER INTO SCRATCHPAD

Enter altitude or / distance into scratchpad using data entry keys.
Note: If a distance edit is to be made, it must be preceded by a  /.

Line Select Key .................................................................................PUSH

Push appropriate Line Select key and observe altitude or / distance now displays edited value.
If further definition of a X-PT* is desired:
Note:  A X-PT* definition can be expanded further to include lateral position and a speed restriction.
To expand X-PT* definition, PMS must display WPT X-PT* page. WPT X-PT* page may be displayed by one of the following methods:
.  
From a CRZ or DES page, push VERT WPTS key and slew until X-PT* event is displayed, then push Line Select key adjacent to X-PT*.

.  
From a VERT WPTS page, slew until X-PT* event is displayed, then push Line Select key adjacent to X-PT*.

.  
From expanded PPOS page, slew up until WPT-X-PT* page is displayed.

.  
From expanded BOD page, slew down until WPT X-PT* page is displayed.


Note:  Data Line 1 defines lateral position of X-PT*. It can be loaded as a frequency, frequency / radial / distance or, if an ILS frequency is used, as a frequency  /  /  distance.
Lateral Position Data...............................ENTER INTO SCRATCHPAD

Enter lateral position data into scratchpad using data entry keys.
Line Select Key 1 ..............................................................................PUSH

Push Line Select key 1 and observe lateral position data is displayed in Data Line 1.
Desired Speed...........................................ENTER INTO SCRATCHPAD

Enter desired speed (at X-PT*) into scratchpad using the data entry keys.
(Continued)
Continental
Rev. 12/01/00 #29 Flight Manual
Line Select Key 2 ..............................................................................PUSH

Push Line Select key 2 and observe desired speed is displayed in Data
Line 2. 
Note:  If no speed is entered, PMS will automatically display a X-PT* speed after X-PT* has been completely defined on Data Line 3. This speed will be an optimum POA speed, non-optimum default descent speed or 250 KTS if X-PT* is at or below 10,000 feet and speed restriction is in effect. 

Altitude / Distance....................................ENTER INTO SCRATCHPAD

Enter altitude / distance into scratchpad using data entry keys.
Line Select Key 3 ..............................................................................PUSH

Push Line Select key 3 and observe altitude and distance are displayed in Data Line 3.
Note: Distance will now decrease until X-PT* is reached.
PMS SINGLE ENGINE OPERATION

Note:  Engine failure is detected based on either a loss of an EPR sensor or excessive difference between EPR readings (indicating loss of power on one engine).
At engine failure, PMS will annunciate SELECT MCT thrust mode unless mode was previously engaged.
Note:  If engine failure indication is in error, pushing CLEAR key will remove SELECT MCT message from scratchpad.
MCT Button......................................................................................PUSH
 
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本文链接地址:MD-80 Flight Manual 麦道80飞行手册 2(158)