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T-45C TS INav 03; ADV INav-01
Use and Operation of TACAN, VOR, VOR/DME
(1) TACAN pointer hunts or rotates
(2) Courseline removed from display
b. DME and identifier signal not affected
2. 40o off bearing TACAN pointer lock-on error: locking on to multiples
of 40o from the desired radial due to inherent operating functions of
the older crystal controlled receivers. Solid state electronics in the
T-45C should preclude this problem from occurring. 2.7.4.2.1
NOTE: Rechanneling the receiver and tuning back to the original
station may remedy the error.
3. Failure to lock on
a. Misalignment of equipment
b. Worn aircraft control box
NOTE: Rechanneling the receiver and tuning from the opposite
direction back to the original station may remedy the error.
4. Co-channel interference: receiving signals (DME, azimuth,
identifier) from more than one TACAN station due to the
relationship between aircraft’s high altitude and station locations
III. VOR
A. Location and use of VOR equipment controls and indicators for tuning/
identifying 2.7.5.1.1.1
1. FWD/AFT option on HSI display selects and identifies which cockpit
Fig 5: HSI Display
controls the HSI display format, and VOR/ILS and TACAN selection
2. Communication control panel: VOR toggle switch provides routing
Fig 6: Communication
of Morse code and possible recorded information through inter-
Control Panel (See page 12)
communication system (ICS) to pilot’s headset
3. VOR/ILS Control Panel
Fig 9: VOR/ILS
Control Panel
a. Power selector controls power to system and initiates system
BIT when in TEST position
(1) Select VOR steering on HSI display
(2) Set course (CRS) to 000 on HSI display
(3) Set and hold the power/frequency knob in the TEST
position on the VOR/ILS control panel
(4) If the VOR is receiving a valid VOR signal a good BIT
check results in the following HSI indications
Page 3-17
Original (2-02)


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