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|  MIL-D-23222A(AS)
TABLE OF CONTENTS (Cont)
Paragraph
Avionics Demonstration Tests
3.14
Performance
3.14.1
3.14.1.1
Interference
Intercommunication System
3.14.2.2
3.14.1.3
Temperature and Vibration
Condensation
3.14.1.3.1
Antennas
3.14.1.4
Navigation Equipment
3.14.1.6
Identification Equipment
Communications Equipment
3.14.1.7
3.14.1.8
Radar and Infrared Equipments
Countermeasures
3.14.1.9
ASW Equipment
3.14.1.10
Radio Relay Equipment
3.14.1.11
Indicating Equipment
3.14.12
Instruments
3.14.2
Pitot and Pitot static Systems (Altimeter and
3.14.2.1
Airspeed Indicator)
3.14.2.2
Automatic Pilot
3.14.2.3
Fuel Quantity Gage Systems
3.14.2.4
Compass Systems
3.14.2.5
Attitude Indicating Systems (Remote)
3.14.2.6
Engine Power Parameter Systems
3.14.2.7
Performance
Engine and Flight Instrument Transmitter Mountings,
3.14.2.8
Temperature and Vibration Limit Tests
3.15
Shipboard Suitability Demonstration Tests
General
3.15.1
3.16
Photographic Demonstration
3.16.1
General
3.16.2
Ground Check
3.16.3
Flight Check
Reliability and Maintainability Demonstration
3.17
Requirements
3.17.1
General
3.17.1.1
Test Plan
3.17.1.2
Aircraft Changes
3.17.1.3
Test Flights
3.17.1.4
Maintenance
3.17.1.5
Acceptance Criteria
vii
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