munirabbasi

Hello Avionic expertise Frequency sensitive relays of C-130 are supplied by AC generator Phase C on "AC" point its TB . The Query is raised in my mind that why phase "B" or A is not supply from the generator for frequency monitorin g of the system. Best Regards Munir Abbasi Home Hercules Pakistan

Excellent Best Regards Munir Abbasi

Oh! Yes I have Training manual (EM) of L-100 and C-130 B/E and H series in hard copy. Best regards Munir Abbasi Home of Hercules Pakistan

Dear reason of high scale of indicator is short circuiting either tank unit or compensater unit due seal damage Amity the AUX fuel tank trouble shoot as per TO Best Regards Munir Abbasi

Drain AUX fuel tank from draining point to eliminate water contamination. Use tester (MD2) for proper operation of tank units and compensator unit. Best Regards Munir Abbasi

As You know at high altitude of aircraft less pressure is require to move rudder ( reduce pressure 1275 to 1300 psi both system) Pilot must be monitored the both pressure through booster rudder and UTY indicators. for this purpose HYD rudder booster and Utility diverter panels are installed at above aft cargo door. System can be overridden (3000 Psi) by push button SW is mounted at same place and toggle guarded SW is mounted at flight pedestal at any time. Best Regards Munir Abbasi Home of Hercules Pakistan

DCU are installed by Rockwell Collin As integrated avionics upgraded system program modification in Engine instrument Display system. Munir Abbasi

Dear brother Gary Tinyclark I mean to say, How DCU works "I" level Maintenance Munir Abbasi

Hello Avionics Expertise How Data Concentration Unit Works? Munir Abbasi Home of Hercules Pakistan

Formation Light.docx

Kindling Attached file Best regards Munir Abbasi Formation Light.docx

Oh Thanks Tiny clark Best regards Munir abbasi Home of Hercules Pakistan

AT What pressure Dumping manifold relief valve open? Munir Abbasi Home of Hercules Pakistan

Replace the FCU Munir Abbasi

Please see T56A-15 and C-130A-3 publications and contact to AFZAL LAB for NDI Munir Abbasi home of Hercules Pakistan

Thanks Munir Abbasi

Adjust START POT of TD control with TD tester Check NULL TIT Munir Abbasi

Thanks Munir Abbasi

NATOPS1 Anti-skid Control Box PCB A2 was burnt out what is reason behind it? Do not test ant-skid during while aircraft is taxing (IC-130B-1 caution) if the testing is carried out during aircraft taxing what happen with the system. Munir Abbasi Home of Hercules

What is selection of TD SWs. Null or AUTO Munir Abbasi

If you see optimum blade angle relationships phase angle measure opposite with No #1 blade to No #3 for example 20 degree angle lagging or leading to No#3 to No#1 blade Munir Abbasi

Hello propeller expertise Optimum angular relationship shown in diagram master of No #2 or No#3 with respect other slave with NO # 3 blade AT 12 O clock why the phase angle relation of No#3 Blade only with master. Any dynamic reason opposite blade of No.#1 to No #3 Munir Abbasi

Thanks Munir Abbasi

Hello Hydraulic Expertise At Pressure relief valve of Anti skid control release the pressure Munir Abbasi

Thanks ,Defect was rectified with sufficient hydraulic bleeding. Munir Abbasi