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2.6 Post Installation Tests
To certify the installation, FAA Form 337 must be completed. In addition,
weight and balance or any operating limitations must be entered into the
aircraft logbook. Refer to the current Federal Aviation Regulations for any
additional requirements.
Weight |
2.3 lbs (I. 04 kg) |
Power Requirements |
1. 0 Amperes, Receive |
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1.6 Amperes, Transmit |
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0.26 Amperes, Pilot Lamps |
2.6.1 Preflight Tests
A preflight test should be performed using an ATC-600A Transponder and DME
test set or equivalent. The test set should be set-up as described in the
ATC-600A Operators Manual and following tests should be conducted:
- Pilot Code
- Peak Transmitter power
- Transmitter Frequency
- SLS Operation
- IDENT
- Percent Reply
In the event that an altitude digitizer has been installed, the altitude
digitizer manual should be consulted for proper procedures and the following
tests should be conducted:
- Altitude Code
- Invalid Altitude Code Output
2.6.2 Flight Test
After installation, a flight test should be performed to check overall
operation and system compatibility.
- Range Test
The AT 150 should furnish a strong and stable return signal to an
interrogating radar facility that is 50 NM away when the aircraft is flying
at 6000 feet. At this altitude and distance, fly a flat circle while having
an FAA station monitor the transponder return signal. There should be no
more than two sweeps of the interrogating radar without a return response.
- Surveillance Approach
Perform an approach to a runway of an airport starting at least 10 NM from
the airport served by Airport Surveillance Radar (ASR) having an Air Traffic
Control Radar Beacon System (ATCRBS) facility. Alternately, a simulated
approach and letdown may be made along a path parallel to, but separated,
three to four miles from a vertical plane through the location of the ASR
facility. The approach should be made at the normal rate of descent and
normal approach and landing configuration for the aircraft and should
continue down to an altitude of 200 feet. Not more than one "drop
out" should occur for any 10 radar sweeps during final approach.
- Electromagnetic Compatibility
The transponder should <unintelligible> other systems aboard the
aircraft to be degraded below their normal capability and transponder
operation should not be adversely affected by other equipment.
2.7 Aircraft License Requirements
The AT 150 TSO, as installed in the aircraft, requires an Aircraft Radio
Station License. This license may be obtained by filing FCC Form 404. The unit
may be operated for up to 30 days after filing the FCC Form 404 providing a copy
of the FCC Form 404 is kept in the aircraft.
This equipment has been type accepted by the FCC and entered in their list of
type accepted equipments as "NARCO AT 150 TSO".
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