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时间:2011-04-23 09:57来源:蓝天飞行翻译 作者:航空
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Magnetic heading indi-cations  Gyro Mag-netic Com-pass AN/ASN-43  Navigational Aid.  Lower console 
Identi.cation friend or foe  Transpon-der Set AN/ APX-100(V)  Transmits a specially coded reply to a ground-based IFF radar Inter-rogator system.  *Line sight  of  Lower console 
Absolute altimeter  Radar Altimeter AN/APN-209  Measures absolute altitude.  0 to feet  1500  Instrument panel 
NOTE 
*Range of transmission or reception depends upon many variables including weather conditions, time of day, operating frequency, power of transmitter and altitude of the helicopter. 

3.4 AVIONICS MANAGEMENT SYSTEM.
a. The avionics management system provides the pilot with a means of controlling the avionics communications and navigation systems, and displays information on the Multi Function Displays (MFD), the Horizontal Situation Indicators (HSI), and Night vision goggle heads up display (NVG HUD). The CDU is the primary controller for com-munication and navigation radios and sensors, and displays mission and system data as well as permitting operator entry and modi.cation of mission data. The CDU front panel provides a data display, a keyboard composed of al-phanumeric keys, two rocker keys, software-programmed keys (soft keys) whose functions depend on the adjacent display, and annunciators that indicate failures, status changes, or message alerts. The CDU keyboard is used to access top level menus or screens of the system functional areas and to enter or edit displayed data. Power for the AMS is provided from the dc essential bus, through circuit breakers marked CPLT CDU and PLT CDU, and from the battery utility bus through a circuit breaker marked CDU BKUP. The dc power from the battery utility bus acts only as a backup power source, maintaining power on AMS to for up to 10 seconds in the event of a dc essential bus power interruption.
3.4.1 CDU Controls and Functions. Controls for the AMS are on the front panel (Figure 3-2), and on the col-
lective stick (Figure 2-11). The function of each control is as follows:
CONTROL  FUNCTION
Fixed Function
buttons:

CAU/ADV button  Toggles between caution advisory and normal screen of CDU.
CLR  Clears all data present in the scratch pad, and ends the edit.
COM  Access main communication screen.
NAV  Access main navigation screen, to select modes of navigation and tune radio navaids.
FPN  Access .ight planning screen.
FIX  Access screen to update position, and create waypoints.

VHF.FM NO. 1 / VHF.AM

RADAR WARNING ANTENNA
RADAR ALTIMETER ANTENNA
GLIDE SLOPE ANTENNA VOR / LOC ANTENNA (SAME BOTH SIDES)
VHF.FM NO. 2 
ANTENNA 
TRANSPONDER (IFF) 
ANTENNA (TOP) 
GPS ANTENNA 
INFRARED 
COUNTERMEASURE 
TRANSMITTER 

HF ANTENNA

VHF.FM HOMING ANTENNA (SAME BOTH SIDES)
UPPER TACAN ANTENNA

DOPPLER ANTENNA  PLS ANTENNA  VHF / AM.FM ANTENNA  LD / ADF ANTENNA  RADAR WARNING ANTENNA 
TRANSPONDER (IFF) 
ANTENNA (BOTTOM) 

UHF
LOWER

COMM
TACAN

ANTENNA
MARKER ANTENNA
PLS RADAR STORMSCOPE

BEACON RADARANTENNA WARNING ANTENNAANTENNA WARNINGANTENNA
ANTENNA AB0333
SA

Figure 3-1. Antenna Arrangement
FIXED
FUNCTION
BUTTON

SOFT KEY
SOFT KEY


KEYBOARD ANNUNCIATOR
KEYBOARD ANNUNCIATOR
ROCKER KEY FIXED FUNCTION BUTTONS
AB0326
SA

Figure 3-2. AMS Control Display Unit
CONTROL DAT INI PPS
CLC
STS
SNS
IFF

TST
LTR

LNK
ZRO

ENT
Keyboard annunciators
ADV
STS
MSG
CDU
 
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