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 through HAL-Aircraft Div
AC DC TEST SET
Description:
Function-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 through HAL –Overhaul&Aircraft Div
FUEL DIP TEST SET
Description:
The fuel dip system test box consists of test panel and cable stowage panel assembly, 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 to the fuel dip systems.
End User:
Jaguar Aircraft, Indian Air Force through HAL –Aircraft Div
CWS TEST SET
Description:
The Centralised 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 lightening circuits).
End User:
Hawk Aircraft, Indian Air Force through HAL –Aircraft & Overhaul Div
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 through HAL –Aircraft Div
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:
This test 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 through HAL –Aircraft Div
FLAP SLATS EOT TEST BOX
Description:
This test is used for checking the end of travel 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
End User:
Jaguar Aircraft, Indian Air Force through HAL-Aircraft
LASER WINDOW DEMIST SYSTEM
Description:
This test is used to carry out comprehensive checks of Laser Window Demist System. The toggle switches in the unit are used to carry out electrical checks
End User:
Jaguar Aircraft, Indian Air Force through HAL –Aircraft Div
LASER WINDOW TEST SET
Description:
This test set is used to determine the acceptable degree of sand erosion on the laser window (in terms of laser ranging / target seeking performance) by measuring the light transmission through the window. A transmission level between 45% and 55% is considered as acceptable limit.
End User:
Jaguar Aircraft, Indian Air Force through HAL –Aircraft & Overhaul Div
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 ERSU 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, Indian Air Force through HAL-Aircraft Div
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:
Function-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, Indian Air Force through HAL-Aircraft Div
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 facilities.
End User:
Jaguar Aircraft, Indian Air Force through HAL-Aircraft Div
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
AUXILIARY CARD TEST JIG
AC Module test jig has provision to set certain signals in the UUT and to monitor all pins on the AC Module edge connector. The Fixture interfaces the cards to the appropriate power supplies, signal sources and monitoring devices like CRO, DMM and logic analyzer. Further provision is available to monitor activities on the various important pins. The power supplies are interfaced to UUT via wires.
End User:
BEL-LCA
DIGITAL MODULE TEST JIG
The Manual Test Jig has provisions to set certain signals in the UUT and to monitor all pins on the Digital Module edge connector. The fixture interfaces the cards to the appropriate power supplies, signal sources and monitoring devices like CRO, DMM and logic analyzer. Further provision is available to monitor activities on the various important pins. The power supplies are interfaced to UUT via wires
End User:
BEL-LCA
EJB 72 Series Test Rig TR-41
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, Indian Air Force through HAL-Aircraft Div
Engine Electronics Unit
Engine Electronics Unit (EEU) is an electronics interface to receive signals and commands, to suitably condition, modify them and produce electrical outputs to kill the engine. It also monitors the engine.
End User:
ADE
ACCELERATION SENSOR ASSEMBLY (ASA) TEST JIG
ASA test jig and ASA sensor test jig. Acceleration sensor assembly (ASA) 3-Axis Test Jig (STTE) for measuring longitudinal, lateral, normal axis acceleration using ASA unit.
End User:
BEL-LCA
AC MK2 SCM & SDIM SEMI ATE
Servo Control Module (SCM) Test Jig is used for tes
ng the Servo Control Module at SRU level with the help of PCB Interface Module which contains 196 Pin Airborne Connector for interacting between SCM Module and Test Jig. Test Jig Consist of test fixture test and monitoring point at the front panel and interface connector, for interface UUT (servo control module) with it. It also consists of workstation with DIO module and Respective driver software, used for simulation Digital module of AC Mk2
Servo Discrete interface Module (SDIM) test Jig is used for testing the Servo Discrete Interface Module at SRU level with the help of PCB Interface Module which contains 196 Pin Airborne Connector for interacting between SDIM Module and Test Jig. This Test Jig will have 6.5 digit Digital
Multimeter, Fixed dc voltages +/-5v, +/- 15v supply and programmable 28VDC power supply for Servo Discrete interface Module (SDIM). Test JIG also consists of TTL Logic conversion board which converts 5V TTL, The logic conversion board will have +/- 10V Reference voltage generation circuit with 10mA current.
End User – BEL / LCA
End User:
BEL-LCA
Power Supply Module (PSM) Test Jig
The Power Supply Module (PSM) Test Jig consists of test panel assemblies. The Test Jig is used in conjunction with Power Supply Module (PSM) and interfacing through interconnecting loom. This Test Jig unit consists of Resistive and Capacitive loads to test the 3 types of Power Supply Module, CH–1 (5 VDC) 6A, CH–2 (28 VDC) 6.25A and CH–3 (115 VAC) 0-390mA with 400Hz.
End User:
LUH-CIVIL through HAL Accessories Division, Lucknow
Go No Go Tester Hardware Mms
The Go/ No Go Tester is used to test the hardware interfaces of Airborne LRUs such as Interface Computer, Display Computer, and Display test results to enable the user to declare serviceability.
End User:
Dornier DO-228 through HAL MCSRDC Division, Bengaluru.
Load Bank
The load bank is designed to carry out grounding checks of the Helicopter. Periodically tested ground support devices with 28VDC load bank ensure critical power and detect potential failures.
End User:
LCH, ALH and other Helicopters through HAL Helicopter Division, Bengaluru
Test Box
The test bench for control units is special purpose test that is designed to test the control unit of automatic control box. Control unit consists of a Relay PCB which is assembled inside AC master box. The test bench enables quick functional check of the control box at the laboratory.
End User:
Artouste III B Engine through HAL Engine Division, Bengaluru
Decade Resistance Box
This device offers 6 decades of resistance ranges from 0.1Ω to over 111.1KΩ. Rotary switches allow easy addition and subtraction of resistance values. Binding posts offer simple and secure connections.
End User:
HAL Avionics Division, Hyderabad.
WIRE HARNESS P/N:8819796000
End User:
Shakti Engine , HAL Engine Division, Bengaluru.
Wire Harness P/N: TM1625G001
End User:
Shakti Engine , HAL Helicopter Division, Bengaluru.
Wire Harness P/N: TM2925G002
End User:
Shakti Engine , HAL Helicopter Division, Bengaluru.
Wire Harness P/N: TM4227G001
End User:
Shakti Engine , HAL Helicopter Division, Bengaluru.
Wire Harness P/N: TM4229G001
End User:
Shakti Engine , HAL Helicopter Division, Bengaluru.
Wire Harness P/N: TM4898G002
End User:
Shakti Engine , HAL Helicopter Division, Bengaluru.