Tender For corrigendum : providing and fixing of digital speed indicator and pressure recorder at main mechanical ventilation fan of gayatri ug mine, rgk sa, bishrampur area.
Tender For supply, installation and commissioing of ferrousdebrismonitor (fdm) for dissolved particle analysis as per detailed specification enclosed in annexure. note: the firm must ensure full compliance with all columns of annexure and upload the completed annexure alongside the bid, else their offer shall be rejected. [ warranty period: 30 months after the date of delivery ]
Tender For corrigendum : procurement of spares for mirage aircraft - power supply, mica data link flts, hbj-twt, hbj-cpu interface board, hbj-lv power supply, tua/vem 130 cable a, mdr - pfc power supply, mdr monitoring board, sidl board, iff701ti test set, supervision pc mainframe, air data test set, pressure indicator manometer, oscilloscope, power supply module, high voltage power supply, cw power sensor, low voltage ps, combiner unit, equipped crt, altitude cell, wiring extn rack i, elv dc power supply module, lv dc power supply, base,voltage regulator, electrical safety tester, circuit card assembly, crash recorder (espar ng)
Tender For corrigendum : procurement of spares for mig-29 upg aircraft - sps assy, copilot seat, communication box (12 us), control flap of cockpit lighting equipment, ahcp panel (fighter), rh outer panel, non-return valve, breathing gas supply sensor, operational onboard recorder, unit, air pressure regulating valve, air pressure reducing valve, bank reducer
Tender For supply, installation, testing & commissioning of ferrousdebrismonitor as per specification no. m/rs/rpm/s/spec/21-22/1. detailed specification as per annexure attached [ warranty period: 30 months after the date of delivery ]
Tender For supply of adopter for grease sample pot (4 ml) of ferrousdebrismonitor for analex fdm plus model of as-k-17143 [ warranty period: 30 months after the date of delivery ]
Tender For procurement of spares for il-78 aircraft - 63 unit control heating, electronic altimeter, arm 62t self contained servo unit rudder installation, relay box 66, relay box 024, left pilot additional speaker, fire extinguisher, kursmp.70 control panel, csd turbine, actuator, fixture, control unit, tape transport mech block, tank unit, pump booster(v), bulb - temperature (v), semi automatic parachute release unit, v trailing edge inner wing (l h), te vane inner wing flap rh sec 2, outer wing flap rh, pipe exhaust, shutter, fuel oil heat exchanger, auto start control, receiverbsi-3k-7, sweep unit, power unit, input information, receiver(av2.026.004.2.03 sp), unit, valve eletro hydraulic, low frequency unit, monitor auto pilot (v), oxygen mask, gear distributive, device(yam2.087.067-01), pannel, switch - power failure, memory block, magnetic recorder, rectifier unit, pcb,y-5, pcb,y-6, differential switch (pressure), sensor