BREAK IN BOX TEST SET

Description:
The scope of the Break in box is to monitor the voltage and current level at all the pins of ADR (Accident Data Recorder) and DAU (Data Acquisition Unit).

End User:
Jaguar Aircraft, Indian Air Force

AC DC TEST SET

Description:
The electrical power generation test set is designed for checking out the “dormant” circuits of the aircraft electrical power generation system and for checking voltage and frequency values at various points within the electrical generation system

End User:
Jaguar Aircraft, Indian Air Force

FUEL DIP TEST SET

Description:
The fuel dip system test box consists of a test panel and cable stowage panel assemblies, contained in a case. The fuel dip test box is used in conjunction with a digital timer to perform a series of static checks on the electrical circuits of the fuel dip systems

End User:
Hawk Aircraft, Indian Air Force

CWS TEST SET

Description:
The centralized warning system (CWS) test set is used on the aircraft to test the aircraft CWS. The test set can be used to test the CWS with or without the CWS related circuits (attention getters and lighting circuits). The test set is also used, off the aircraft, to test the master control unit together with the central warning panel. The warning panel can be tested independently

End User:
Hawk Aircraft, Indian Air Force

LINK TEST SET

Description:
The LTS can perform some of the functions of the ground control station required for checking the operation of the telecommand system of Lakshya in radiate / direct mode.

End User:
Lakshya Pilotless Target Aircraft, Indian Air Force

ANTI-SKID CONTROLLER TEST RIG

Description:
This Test Rig has been designed and manufactured to meet the PIC requirements of Antiskid Controller Pt. No. 228700000 of HJT-36 aircraft.

Test Rig is required for carrying out the following tests such as Insulation test, Input reverse protection test, Skid valve current test, Emergency valve current test, Functional Test.

End User:
HJT-36 Aircraft, Indian Air Force

MICROTURBO STARTER SYSTEM

Description:
This Test set is designed to carry out following functions
a) System monitoring- functional check of the starting system
b) System simulation- check for correct sequencing and the operation of safety circuits in the starting system

End User:
Hawk Aircraft, Indian Air Force

TELELOUD SPEAKING SYSTEM

Description:
The test set is used to carry out comprehensive checks of the aircraft flap and slat system. They provide interconnections, indicator lamps and switches to enable comprehensive checks of the electrical part of the aircraft flap and slat system to be carried out in conjunction with the hydraulic test schedule.

End User:
Jaguar Aircraft, Indian Air force.

SLAT FLAP TEST SET

Description:
The test set is used to carry out comprehensive checks of the aircraft flap and slat system. They provide interconnections, indicator lamps and switches to enable comprehensive checks of the electrical part of the aircraft flap and slat system to be carried out in conjunction with the hydraulic test schedule.

End User:
Jaguar Aircraft, Indian Air force.

FLAP SLATS EOT TEST BOX

Description:
The test set is used for checking the end of travel (EOT) limit adjustment of the aircraft flaps and slats. It provides interconnections, indicator lamps and switches to enable the micro switch settings of the flap and slat limit switches under test to be checked.

End User:
Jaguar Aircraft, Indian Air force.

LASER WINDOW DEMIST SYSTEM

Description:
The test set is used to carry out comprehensive checks of Laser Window Demist System. The toggle switches in the unit are used to carryout electrical checks.

End User:
Jaguar Aircraft, Indian Air force.

LASER WINDOW TEST SET

Description:
The Laser Window Test Set is used to determine the acceptable degree of sand erosion on laser window (in terms of laser ranging/target seeking performance) by measuring light transmission through the window

End User:
Jaguar Aircraft, Indian Air force.

BONDING STRIP

Description:
This spare is used for Static discharge on the Jaguar Aircraft

End User:
Jaguar Aircraft

ERSU TEST RIG TR-27

Description:
Test rig TR 27 is designed for bench testing of the ESRU 72 series. It provides power for the ERSU and tests all microphone, telephone and keying lines, providing modulation loads and monitoring facilities for external test equipment.

End User:
Jaguar Aircraft

JUNCTION BOX (EJB 72 SERIES) TEST RIG TR-41

Description:
Test rig TR 41 is designed for bench testing of the EJB 72 series Junction box. It provides power for the Junction Box amplifier and test receiver, telephone and microphone lines, signal levels and control lines.

End User:
Jaguar Aircraft

GROUND CREW JACK BOX TEST RIG TR-42

Description:
Test rig TR 42 is designed for bench testing CCS ground crew jack boxes. It provides power for the jack box and tests intercom facility, amplifier output and microphone / telephone lines.

End User:
Jaguar Aircraft

ERSU TEST RIG TR-135

Description:
Test rig TR 135 is designed for bench testing of the ERSU 74 series. It provides power for the ERSU amplifiers and tests microphone lines, telephone lines and all switches.

End User:
Jaguar Aircraft

CABLE HARNESS

Harness and cable assemblies starting with functional & interface specifications. Capability to select right components for low loss, high frequency RF cable assemblies Type certification/qualification Testing capability using accredited test laboratories to MIL–STD- & JSS 55555 Harness accessories to meet special requirements such weight, shape, protection etc Harnesses with integrated mechanical parts

ACTUATOR INTERFACE UNIT 1& 2

Description:
The actuator interface box is used during the actuator checks of Lakshya. It provides I/P points and monitor points of signals related to actuation system.
It consists of two boxes. One mates with FCE J1 and J3 connectors of the aircraft loom. The other box consists of a 19-pin fixed connector to which the computer interface cable/actuator test cable is connected.

End User:
Lakshya Pilotless Target Aircraft, Indian Air Force

28V SUPPLY BOX

Description:
This unit consists of a box with cable having a fixed type connector when mated to aircraft loom connector providing the +28V line, which is drawn through two wires to banana sockets mounted on the box.

End User:
Lakshya Pilotless Target Aircraft, Indian Air Force

ACCELEROMETER ELECTRONICS

Description:
The Accelerometer Electronics with linear accelerometer is used for measuring control surface during flight control system check of Lakshya. It is necessary to use this setup to amplify the accelerometer output which is very low.

End User:
Lakshya Pilotless Target Aircraft, Indian Air Force

ENGINE RPM SIMULATOR

Description:
The Engine simulator is designed to simulate signal with frequencies in the operating range of 70% rpm to 100% corresponding to the throttle demand input range of 0 to about 9.44 Volts It also provides audio signal qualitatively corresponding to the simulated rpm.

End User:
Lakshya Pilotless Target Aircraft, Indian Air Force

TOW BODY INDICATOR

Description:
During integration / testing the tow body commands bulbs are connected across the designed pin number to check the availability of particular signal as and when that particular command is initiated

End User:
Lakshya Pilotless Target Aircraft, Indian Air Force

SHORTING CONNECTOR- TOW BODY

Description:
Tow body shorting connector is used for shorting the pyros in tow bodies of Lakshya during integration testing for safety purpose. This connectors are connected to the aircraft loom connector CCP & CCS

End User:
Lakshya Pilotless Target Aircraft, Indian Air Force

PCM BREAK CONNECTOR

Description:
This break connector is used for checking the inputs to PCM encoder.

End User:
Lakshya Pilotless Target Aircraft, Indian Air Force

RATE & POSITION SIMULATOR

Description:
The rate and position simulator is used during the following integration checks
a)Control quantitative checks.
b)Roll rate and pitch rate calibration.
c)Yaw rate and yaw angle checks.

End User:
Lakshya Pilotless Target Aircraft, Indian Air Force