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FAA - AD 91-06-20 - ELECTRICAL EQUIPMENT\BRITISH AEROSPC (ENGLAND)\ATP Organization: FAA
FAA - AD 95-02-09 - ELECTRICAL POWER\BRITISH AEROSPC (ENGLAND)\ATP Organization: FAA
FAA - AD 89-15-09 - ELECTRICAL SYSTEM\BRITISH AEROSPC (SCOTLAND)\JETSTREAM SERIES 3101 Organization: FAA
FAA - AD 95-11-17 - ELECTRICAL SYSTEM\BRITISH AEROSPC (SCOTLAND)\JETSTREAM 3201\JETSTREAM SERIES 3101 Organization: FAA
FAA - AD 86-24-08 - ELECTRICAL SUPPLY SOURCE MOD.\BRITISH AEROSPC (SCOTLAND)\JETSTREAM SERIES 3101 Organization: FAA
FAA - AD 95-NM-251 - EMERGENCY ELECTRICAL SYSTEM\BRITISH AEROSPACE\BAE-146-100A\BAE-146-200A\BAE-146-300A Organization: FAA
FAA - AD 78-05-09 - FUEL BOOST PUMP ELECTRICAL CONNECTORS\BRITISH AEROSPC AIRBUS LTD\BAC 1-11 200 SERIES\BAC 1-11 400 SERIES Organization: FAA
FAA - AD 98-NM-43 - FAILURE OF THE ELECTRICAL CIRCUIT TERMINAL LUGS\BRITISH AEROSPC\AVRO 146-RJ85A\AVRO 146-RJ100A Organization: FAA
FAA - AD 96-22-05 - LOSS OF THE EMERGENCY ELECTRICAL SYSTEM\BRITISH AEROSPC (ENGLAND)\AVRO 146-RJ100A\AVRO 146-RJ70A\AVRO 146-RJ85A\BAE 146-100A\BAE 146-200A\BAE 146-300A Organization: FAA
FAA - AD 97-NM-217 - ACCUMULATION OF MOISTURE INSIDE THE ELECTRICAL CONNECTORS\JETSTREAM AIRCRFT LTD (FORMERLY BRITISH AEROSPC )\JETSTREAM MODEL 4101 Organization: FAA
FAA - AD 96-NM-97 - OVERHEATING OF THE ELECTRICAL GROUND POSTS\JETSTREAM AIRCRAFT LTD (FORMERLY BRITISH AEROSPACE)\JETSTREAM MODEL 4101 Organization: FAA
FAA - AD 98-11-28 - FAILURE OF THE ELECTRICAL CIRCUIT TERMINAL LUGS, WHICH COULD RESULT IN ELECTRICAL SYSTEM FAILURE\BRITISH AEROSPC (ENGLAND)\AVRO 146-RJ100A\AVRO 146-RJ85A Organization: FAA
FAA - AD 97-21-15 - PREVENT POSSIBLE OVERHEATING OF THE ELECTRICAL GENERATOR FEEDER CABLES AND CONSEQUENT DAMAGE, WHICH COULD LEAD TO POSSIBLE FIRE OR LOSS OF ESSENTIAL ELECTRICAL SYSTEMS\BRITISH AEROSPC (ENGLAND)\AVRO 146-RJ100A\AVRO 146-RJ70A\AVRO 146-RJ85A Organization: FAA
BSI - BS 6709 - SPECIFICATION FOR INTERCONNECTION OF ELECTRICAL APPARATUS, CONSTRUCTED TO TWO OR MORE BRITISH STANDARDS, FOR USE IN MINES SUSCEPTIBLE TO FIREDAMP Organization: BSI
Date: 1986-07-31
Description: Requirements for the construction, including marking, and testing of interconnected electrical apparatus, including systems and components.
FAA - AD 99-26-17 - PREVENT CHAFING AND SUBSEQUENT DAMAGE TO THE ENGINE INTAKE DE-ICING SYSTEM WIRING, AND CONTAMINATION OF ELECTRICAL CONNECTORS AND PLUGS\BRITISH AEROSPC (ENGLAND)\ATP Organization: FAA
FAA - AD 99-NM-201 - PREVENT CHAFING AND SUBSEQUENT DAMAGE TO THE ENGINE INTAKE DE-ICING SYSTEM WIRING, AND CONTAMINATION OF ELECTRICAL CONNECTORS AND PLUGS\BRITISH AEROSPC\ATP SERIES Organization: FAA
FAA - AD 99-NM-115 - PREVENT ELECTRICAL ARCING DUE TO DAMAGED FUEL STANDBY PUMP CABLE ASSEMBLIES AND CONDUIT PIPES\BRITISH AEROSPC\JETSTREAM MODEL 4101 Organization: FAA
CENELEC - EN 50341-2-9 - OVERHEAD ELECTRICAL LINES EXCEEDING AC 1 KV - PART 2-9: NATIONAL NORMATIVE ASPECTS (NNA) FOR GREAT BRITAIN AND NORTHERN IRELAND Organization: CENELEC
Date: 2015-06-01
Description: General (ncpt) GB.1 General T...
DS/EN 50341-2-9 - OVERHEAD ELECTRICAL LINES EXCEEDING AC 1 KV - PART 2-9: NATIONAL NORMATIVE ASPECTS (NNA) FOR GREAT BRITAIN AND NORTHERN IRELAND (BASED ON EN 50341-1:2012) Organization: DS
BSI - BS EN 50341-2-9 - OVERHEAD ELECTRICAL LINES EXCEEDING AC 1 KV PART 2-9: NATIONAL NORMATIVE ASPECTS (NNA) FOR GREAT BRITAIN AND NORTHERN IRELAND (BASED ON EN 50341-1:2012) Organization: BSI
Date: 2015-07-31

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