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HIGH INTENSITY RADIATED FIELD (FIRF) Discuss the methods of protection against HIRF and the checks/ inspections which would be carried out after a fault was entered in the technical log. INTRODUCTION High Intensity Radiated Field (HIRF) is produced by high energy systems located on the ground ground and occurs occurs at all frequ frequenc encies ies.. It affects affects any electr electroni onic c and digita digitall systems on the aircraft, causing affected systems to operate erratically. PROTECTION Aircraft and systems can be protected against HIRF by proper shielding of cables, EMI filters filters,, good good bondin bonding, g, electr electro o static static discha discharge rger. r. Prope Properr termin terminatio ation n of airc aircra raft ft syst system em conn connec ecto tors rs and and seal sealin ing g of LRUs LRUs cond conduc uctin ting g surf surfac ace e on windows, screening of cables. CHECKS / INSPECTIONS If a fault had been entered in the technical log as HIRF I would make the aircraft safe in accordance with the Aircraft Maintenance Manual (AMM) and raise any other paper paper work required required.. I would would attempt attempt to isolate isolate the fault, fault, debrie debrieff the air crew, crew, if necessary and confirm it is HIRF and and not just a fault with with the systems involved. involved. The technical technical log could be consulted consulted to establish establish if there is a pattern of previous previous similar faults. faults. If HIRF appeared appeared to be the the cause I would would check the the serviceability of EMI filters, continuity check of shielding and bonding and carry out BITE (Built In Test Equipment) tests where where possible to rectify rectify the defect. And also check for the following: Detailed bonding resistance Usin Using g loop loop resi resist stan ance ce test tester er to meas measur ure e the the loop loop resi resist stan ance ce// impe impeda danc nce e measurement. Disassemble the connector to detect corrosion. Arrang Arrange e to reconf reconfirm irm loop loop positio position n within within the limit. limit. Carry Carry out relate related d system system functional test. CERTIFICATION Any work carried carried out would be recorded recorded and signed as the job progresse progressed. d. If any item items s were were repl replac aced ed cros crossc sche heck ck the the EASA EASA Form Form 1 or FAA FAA 8130 8130-3 -3 for for items items airworthiness conformity and would be attached to paper work, part numbers GRN’s, seri serial al numb number ers s on and and off off woul would d be recor recorde ded. d. CRS CRS woul would d be issue issued d by a appropriately authorized engineer and a statement would be made in the technical log to monitor the systems affected on the next flights. REPORTING As any occurrence of HIRF is an incident this must be reported to the CAA through the Mandato Mandatory ry Occurren Occurrence ce Report Report (MOR) scheme. scheme. I would would also report report it to the organisation HIRF programme.