曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

Longitude
CV Speed
CV Heading
HUD Display Roll (Symbols)
Pitch (Symbols)
Magnetic Heading (Symbol)
Flight Path Marker (Symbol)
Potential Flight Path Marker (Symbol)
System Altitude
Radar Altitude
Vertical Velocity
Calibrated Airspeed
Barometric Setting
ORIGINAL 20-18
Figure 20-10. Navigation Data Display Summaq (Sheet 1 of 2)
NAVAIR Ol-F14AAD-1
DISPLAY I NAVIGATION DATA DISPLAYED
MFD VDI Format
MFD HSD Format
Flight Director Position and Rotation
Angle-of-Attack
Mach Number
Normal Acceleration (g)
ACL Lateral &Vertical Errors (Symbol)
ILS Azimuth & Elevation Deviation (Symbols)
Command Heading (Symbol)
Roll (Symbols)
Pitch (Symbols)
Magnetic Heading (Symbol)
Flight Path Marker (Symbol)
System Altitude
Radar Altitude
Vertical Velocity
Calibrated Airspeed
Barometric Setting
Mach Number
ACL Lateral 8. Vertical Errors (Symbol)
ILS Azimuth &Elevation Deviation (Symbols)
Command Heading (Symbol)
Range to Tacan/Destination
D/L Command Alt/Mach No
D/L Command Heading (Symbol)
Magnetic Heading (Symbol)
Magnetic Course (Symbol)
Wind Direction/Speed
True Airspeed
Groundspeed
Way Point No/Brg/RangeiTfG
Tacan Sta NoIBrglRangeilTG
Tacan Brg/Deviation (Symbols)
Tacan Command Course (Symbol)
Destination No
Destination Brg/Cmd Course (Symbols)
ADF Bearing (Symbol)
Command Heading
Course Select
Heading Select
Figure 20-10. Navigation Data Display Summary (Sheet 2 of 2)
20-19 ORIGINAL
NAVAIR Ol-F14AAD-1
ORIGINAL
Figure 20-I 1. MFD MENU1 and MENU2 Displays
20-20
NAVAIR Ol-Fl4AAD1
*ONLY THE RESPECTIVE CHARACTER
LEGENDS (S, -, W. N. +, E, OR BLANK)
APPLICABLE TO THE PARAMETER
SELECTED WILL APPEAR ON THE
OPTION DISPLAY LEGEND
TYPICAL DATA ENTRY DISPLAYS
OWN AIC PARAMETER
SELECTED/DATA KEYED IN.
OWNAC-ALT - OWN Ax:. ALT
1050
OWN AC. THDG
210
_ OWN NC WSPO - OWN AIC~ WSPD
35
_ OWN A/c. WDlR OWN NC. WOIR
--- 030
_ OWN AC - MVAR OWN A/o. MVAR
17.5E
OWN AIO~ BAR0
29.92
Figure 20-12. DEU Own-Aircraft Data Enhy (Typical)
20-21 ORIGINAL
NAVAIR Ol-F14AAD-1
Figure 20-13. DD/TID Own-Aircrafi Data Entry
ORIGINAL
NAVAIR 01.F14AAD-1
GROUND ALIGNMENT
STORED HEADING GROUND ALIGNMENT
OWN A/C
SHOG RND BUN0 000000
INSISWRS
PUAL- 6.59
TIME- , .31
Figure 20-14. MFD Ground Alignment Fomats
20-23 ORIGINAL
NAVAIR Ol-F14AAD-1
5. Verify that SHDG is not boxed. If it is, press the
SHDG pushbutton to unbox SHDG.
Note
Unboxing of SHDG must be performed
within 17 seconds of selecting GND ALIGN
on the NAV MODE switch or the boxed
SHDG will be selected and unboxed by the
system and deselection will not be available.
Verify latitude and longitude and enter correct values
if necessaryI.f new entries arer equired at this
time, the alignment time may be extended, depending
on the differences between the newly entered
values and those displayed when alignment
was initiated.
Alignment progressc an be monitoredb y observing
the QUAL and TIME acronyms and the alignment
scale on the MFD OWN A/C format. The indicator
on the alignmentp rogresss calec hangesR ooma “V”
to a diamond symbol at the fmt tic mark. This representsa
n 8 nm per hour estimatedn avigationq uality.
The secondt ic mark representsa n estimated2
nm per hour quality and the third an estimated 0.8
nm perh our quality.A t this point a dot appearsin the
diamond. An INS ALIGN COMPLETE message
normally appearsa t the top of the MFD display in 4
minutes. At this time the QUAL acronym is near or
slightly below 1 nm per hour and the pointer on the
align scale should be near the last tic mark.
During concurrent alignment, it is advisable to
monitor the SAHRS alignment progress by pressing
the SAHR pushbutton on the MFD. The OWN
A/C MFD format will show SAHR boxed; and the
QUAL and TIME acronyms and the align scale
now refer to the SAHR. A SAHRS ALIGN COMPLETE
message normally appears in approximately
2.5 to 3 minutes from the time when the
parking brake was set. The QUAL will be approximately
10 (nm per hour) at this time.
9. Alignment may bec ontinueda ftert he appearancoef
the INS ALIGN COMPLETE messageif time permits.
This will provide only slight improvement in
alignment quality but will provide some gyro biasing
and eliminate unnecessaryd rift in the INS mode, If
　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：F-14D 飛行手冊 Flight Manual 3(20)