Rugged, field-deployable diagnostic, calibration, charging, and flight-line verification instruments
The Pitot-Static Test Set is used during aircraft instrument maintenance to check that pitot-static line connections are sealed properly and free of leaks. A technician connects it to the aircraft's pitot-static system, applies pressure or vacuum through the unit, and watches the readings to confirm the lines are holding steady. This helps catch faults early, keeps flight instruments accurate, and reduces the chance of unexpected readings. Portable and user-friendly for field and hangar use.
The Pneumatic Control Panel is a test equipment used to charge aircraft pneumatic systems with controlled pressure and to check those systems for leaks. It is used during maintenance and testing to verify that pneumatic lines, seals and fittings are holding pressure correctly, helping confirm the system is airtight and fit for use before the aircraft returns to service.
Used to charge aircraft systems with pressurised nitrogen and to verify that those systems are correctly pressurised and free of leaks. It is used to charge landing gear struts and other pneumatic systems to their required operating pressure, and to fill or top up onboard nitrogen supply during servicing. As a testing tool, it also allows the operator to check the charged system for leaks before the aircraft is released for use. Trolley-mounted for easy flight line mobility.
Used to test and verify thermocouple junctions, particularly in Su-30 engine exhaust systems. It delivers hot air, up to 200°C, through a precisely designed pointed probe to accurately test the thermocouple's response. The device has a digital meter that gives direct readings of thermocouple output, making the testing process simple and quick. Its compact, sturdy build makes it easy to carry and use in demanding field conditions.
Used for testing and calibration of fuel transmitters used in aircraft fuel systems. The equipment enables calibration and functional testing of fuel transmitters using Aviation Turbine Fuel (“ATF”), tanks, valves, connectors and pipes, designed to be compatible with ATF to facilitate safe and reliable testing and calibration.
| S. No. | Test Equipment | Indicative Image | Key Specifications | Application / Use |
|---|---|---|---|---|
| 1 | Pitot-Static Test Set | |
• Size: 420 X 260 X 305 mm • Temperature Range: -20°C to +55°C • Operating power supply: 27 VDC ± 10% • Indicated air speed range: 0–1,499 km/hr • Indicated altitude range: 0–16,000 m • Weight: 18 kg |
The Pitot-Static Test Set is used during aircraft instrument maintenance to check that pitot-static line connections are sealed properly and free of leaks. A technician connects it to the aircraft's pitot-static system, applies pressure or vacuum through the unit, and watches the readings to confirm the lines are holding steady. Portable and user-friendly for field and hangar use. |
| 2 | Pneumatic Control Panel | |
• Working fluid: Gases (Nitrogen) • Pressure range Line 1: 5 to 200 kg/cm² (max.) • Pressure range Line 2: Up to 8 kg/cm² (max.) • Pressure leak check line: Up to 1.6 kg/cm² (max.) • Overall dimensions (L×W×H): 640 × 475 × 250 mm |
The Pneumatic Control Panel is a test equipment used to charge aircraft pneumatic systems with controlled pressure and to check those systems for leaks. It is used during maintenance and testing to verify that pneumatic lines, seals and fittings are holding pressure correctly, helping confirm the system is airtight. |
| 3 | Charging Trolley Equipment | |
• Working fluid: Nitrogen (N₂) • Charging/outlet pressure: Up to 2.5 kg/cm² • Boosted supply pressure: Up to 400 kg/cm² • Cylinder working pressure: Up to 150 kg/cm² • Mobility: Trolley-mounted, portable |
Used to charge aircraft systems with pressurised nitrogen and to verify that those systems are correctly pressurised and free of leaks. Used to charge landing gear struts and other pneumatic systems to their required operating pressure, and to top up onboard nitrogen supply during servicing. |
| 4 | Electrical Test Equipment | |
• Working Media: Air • Input: 28 VDC, 25A • Output Air Range: 25–200°C • Probe Length: 1680 mm • Indicator Size: 120 x 120 mm • Thermocouple Gun Weight: 1.5 kg • Indicator Panel Weight: 2.1 kg |
Used to test and verify thermocouple junctions, particularly in Su-30 engine exhaust systems. Delivers hot air up to 200°C through a pointed probe to accurately test thermocouple response with direct digital readout. |
| 5 | Fuel Transmitter Calibration Test Equipment | |
• Connector: Part No. 95102E-14-19S50 or equivalent • Connectors: P1 to P6 • Banana terminals: 5 A, Ø4 mm, red and black (B1 to B50) • High and Low terminals with (+) and (-) • Input current / Output current calibration |
Used for testing and calibration of fuel transmitters used in aircraft fuel systems. The equipment enables calibration and functional testing of fuel transmitters using Aviation Turbine Fuel (“ATF”), tanks, valves, connectors and pipes designed for safe testing. |