2g a1
2g a1, Total:86 items.
The international standard classification for "2g a1" includes: .
The Chinese standard classification for "2g a1" includes: .
British Standards Institution (BSI)
- BS 2G 180:1974 Specification for permanent splicing of aircraft electrical cables
- BS 2G 143:1965 Specification for a.c. and d.c. rotary and linear actuators for aircraft
- BS 2G 210:1991 Specification for PTFE insulated equipment wires and cables, single and multi-core, with silver plated copper conductors (190°C) or nickel plated copper conductors (260°C)
- BS 2G 221:1980 Specification for Minyvin type electric cables (metric units)
- BS 2G 182:1975 Specification for pressure-driven machmeters for aircraft
- BS 2G 146:1966 Specification for d.c. motors for aircraft
- BS 2G 199:1984 Schedule for tables relating to altitudes, airspeed and Mach numbers for use in aeronautical instrument design and calibration
- BS 2G 135:1967 Specification for electrically-heated pitot and pitotstatic pressure heads
- BS 2G 202:1988 Specification for design and performance requirements for airframe-fit electrical connectors for d.c. and low frequency a.c. applications
- BS 2G 114:1953 Specification for direct current ratiometer indicators for aircraft
- BS 2G 191:1988 Specification for lighting for aircraft indicators using integral filament lamps
- BS 2G 181:1968 Specification for aircraft filament lamps
- BS 2G 147-1:1966 Specification for a.c. motors for aircraft - Three-phase constant frequency squirrel-cage induction motors
- BS 2G 198-1:1982 Sleeves for aircraft electric cables and equipment wires-Specification for elastomeric sleeves for binding and identification
- BS 2G 112:1956 Specification for air-driven directional gyroscopes for aircraft
- BS 2G 127:1967 Specification for power and current transformers for use in aircraft electrical power supply systems
- BS 2G 132:1981 Specification for general requirements for electromagnetically operated contactors for aircraft
- BS 2G 213:1974 Specification for mechanically operated switches
- BS 2G 215-1:1985 Nickel-chromium and nickel-aluminium thermocouple extension cables for aircraft. Specification for conductors
- BS 2G 223:1989 Specification for screen terminating devices for aircraft electric cables
- BS 2G 115:1956 Specification for sensitive altimeters for aircraft
- BS 2G 231:1990 Specification for conductors for general-purpose aircraft electrical cables and aerospace applications
- 2G 117-1975 Specification for pressure-driven airspeed indicators
- 2G 196-1971 Specification for static invertors
- BS 2G 238:1996 Specification for electric cables for general airframe or equipment interconnect use (260 °C), nickel plated copper and copper alloy conductors, with wrapped insulation
- BS 2G 113:1956 Specification for manifold pressure gauges for aircraft
- BS 2G 134:1970 Specification for d.c. generators
- BS 2G 232:1987 Specification for electric cables for general airframe or equipment interconnect use (135 °C), wrapped insulation
- BS 2G 229:1987 Schedule for environmental conditions and test procedures for airborne equipment
- BS 2G 219:1983 Specification for general requirements for ground support electrical supplies for aircraft
- 2G 191-1988 Specification for lighting for aircraft indicators using integral filament lamps
- 2G 113-1956 Specification for manifold pressure gauges for aircraft
- BS 2G 124-1:1966 Specification for a.c. generators for aircraft - Constant frequency
- 2G 215 Pt.1-1985 Nickel-chromium and nickel-aluminium thermocouple extension cables for aircraft. Specification for conductors
- 2G 231-1990 Specification for conductors for general-purpose aircraft electrical cables and aerospace applications
- 2G 114-1953 Specification for direct current ratiometer indicators for aircraft
- BS 2G 148:1963 General purpose platinum wire thermometer bulbs and connectors for aircraft
- BS 2G 230:1991 Specification for general requirements for aircraft electrical cables (second series)
- BS 2G 233:1987 Specification for electric cables for general airframe or equipment interconnect use (135°C), extruded insulation
- BS 2G 201:1996 Specification for counter and pointer pressure altimeters
- BS 2G 111:1955 Specification for rate of climb indicators for aircraft
- BS 2G 201:1996(1999) Specification for Counter and pointer pressure altimeters
- BS 2G 180:1974(1999) Specification for crimp connectors for permanently connecting aircraft electrical cables
- BS 2G 100-1:1961 Specification for general requirements for electrical equipment and indi cating instruments for aircraft. Environmental and operating conditions-Identification, declarations and construction
- BS 2G 196:1971 Specification for static invertors
- BS 2G 117:1975 Specification for pressure-driven airspeed indicators
- BS 2G 239:1992 Specification for primary active lithium batteries for use in aircraft
- BS 2G 101:1975 Specification for general requirements for aircraft indicators
- BS 2G 223:1989(1999) Specification for Screen terminating devices for aircraft electric cables
- BS 2G 196:1971(1999) Specification for Static invertors
- BS 2G 124-1:1966(2009) Specification for A.C. generators for aircraft — Part 1 : Constant frequency
- BS 2G 143:1965(2009) Specification for A.C. andD.C. rotaryand linear actuators for aircraft
- BS 2G 114:1953(1999) Specification for Direct current ratiometer indicators for aircraft
- BS 2G 117:1975(2009) Specification for Pressure - driven airspeed indicators
- BS 2G 238:1996(1999) Specification for Electric cables for general airframe or equipment interconnect use (260 °C), nickel plated copper and copper alloy conductors, with wrapped insulation
- BS 2G 146:1966(2009) Specification for D.C. Motors for aircraft
- 2G 215 Pt.2-1989 Nickel-chromium and nickel-aluminium thermocouple extension cables for aircraft. Specification for terminations
- BS 2G 147-1:1966(2009) Specification for A.C. motors for aircraft — Part 1 : Three - phase constant frequency squirrel - cage induction motors
- BS 2G 115:1956(2000) Specification for Sensitive altimeters for aircraft
- BS 2G 112:1956(1999) Specification for Air - driven directional gyroscopes for aircraft
- BS 2G 215-2:1989 Nickel-chromium and nickel-aluminium thermocouple extension cables for aircraft - Specification for terminations
- BS 2G 132:1981(1999) Specification for General requirements for electromagnetically operated contactors for aircraft
- BS 2G 134:1970(1999) Specif ication f or D.C. generators
- BS 2G 182:1975(2009) Specification for Pressure - driven machmeters for aircraft
- BS 2G 113:1956(2000) Specification for Manifold pressure gauges for aircraft
- BS 2G 232:1987(1999) Specification for Electric cables for general airframe or equipment interconnect use (135 °C), wrapped insulation
- BS 2G 135:1967(2009) Specification for Electrically - heated pitot and pitotstatic pressure heads
- BS 2G 147-2:1966 Specification for a.c. motors for aircraft - Three-phase variable frequency squirrel-cage induction motors
- BS 2G 191:1988(2000) Specification for Lighting for aircraft indicators using integral filament lamps
- BS 2G 100-2:1962 Specification for general requirements for electrical equipment and indicating instruments for aircraft. Environmental and operating conditions
- BS 2G 215-2:1989+A1:2016 Aircraft. Nickel-chromium and nickel-aluminium thermocouple extension cables. Terminations. General requirements and tests
- BS 2G 124-2:1966 Specification for a.c. generators for aircraft - Variable frequency
- BS 2G 198-2:1982 Sleeves for aircraft electric cables and equipment wires-Specification for slip-on sleeves for identification purposes
- BS 2G 111:1955(1999) Specification for Rate ofclimb indicators for aircraft
- BS 2G 202:1988(1999) Specification for Design and performance requirements for airframe - fit electrical connectors for D.C. and low frequency A.C. applications
- BS 2G 221:1980(1999) Specification for Minyvin type electric cables (metric units)
- BS 2G 198-3:1985 Sleeves for aircraft electric cables and equipment wires-Specification for heat-shrinkable sleeving for binding and insulation
- BS 2G 147-2:1966(2009) Specification for A.C. motors for aircraft — Part 2 : Three - phase variable frequency squirrel - cage induction motors
- BS 2G 100-2:1962(2000) Specification for General requirements for electrical equipment and indicating instruments for aircraft — Part 2 : Environmental and Operating Conditions
- BS 2G 198-4:1990 Sleeves for aircraft electric cables and equipment wires-Specification for semi-rigid high performance heat shrinkable sleeving for binding and insulation
- BS 2G 100-3:1968 General requirements for aircraft electrical equipment and indicating in struments-Characteristics of aircraft electrical systems
Society of Automotive Engineers (SAE)
- SAE AMS2759/2G Heat Treatment of Low-Alloy Steel Parts, Minimum Tensile Strength 220 ksi (1517 MPa) and Higher
- SAE AMS2431/2G Peening Media (ASH), Cast Steel Shot, High Hardness (55 to 62 HRC)
Association for Electrical, Electronic & Information Technologies (VDE)
- VDE 0631-2-5 A1 Berichtigung 1-1998*DIN EN 60730-2-5 A1 Berichtigung 1:1998 IEC 60730-2-5:1995/A1:1996 Amendment to DIN EN 60730-2-5/A1
- VDE 0616-2 A1 E*DIN EN 61184 A1:2021-04 IEC 61184:2017/A1
German Institute for Standardization
- DIN EN 50123-2/A1 Berichtigung 1:1997 Corrigenda to DIN EN 50123-1/A1 (VDE 0115 Part 300-2/A1):1997-01: Railway applications - Fixed installations; D.C. switchgear - Part 2: D.C. circuit breakers; Amendment A1; German version EN 50123-2:1995/A1:1996
din a1,a1 instrument,cispr a1,2g,a1,a1 iram,a1 flame retardant,Flame retardant a1,a1 polarized light,Flame retardant a1,a1 flame retardant,EU 2g,a1 material,fluorescent a1,astm a1,laser a1,rice a1,Worm a1,2g a1