Standard
STEEL, NITRIDING .65 Ni 1 Cr 1 Mo
1946-04-01
HISTORICAL
AMS6480
Search Results
Standard
STEEL TUBING (WELDED) Chromium Molybdenum (.27 - .33 Carbon) (Normalized)
1942-06-01
HISTORICAL
AMS6510
Standard
STEEL COTTER PINS, GALVANIZED Low Carbon
1942-12-01
CURRENT
AMS7212
Standard
NUTS, SELF-LOCKING, STEEL High Strength, Prevailing-Torque, All Metal 450 F (232 C) Use, Unified "J" (MIL-S-8879) Thread Form
1969-11-01
HISTORICAL
AMS7252
Standard
NUTS, SELF-LOCKING, STEEL High Strength, All Metal 450° F (230° C) Use, Unified "J" (MIL-S-8879) Thread Form
1980-01-15
HISTORICAL
AMS7252B
This specification covers all-metal, self-locking nuts, plate nuts, and gang channel nuts made of a carbon or low-alloy steel.
Standard
NUTS, SELF-LOCKING, STEEL High Strength, Prevailing Torque, All Metal 450° F (232° C) Use, Unified "J" (MIL-S-8879) Thread Form
1973-05-15
HISTORICAL
AMS7252A
This specification covers all-metal, self-locking, prevailing-torque nuts, plate nuts, and gang channel nuts made of a carbon or low-alloy steel.
Standard
Combination Tail and Floodlamp for Industrial Equipment
2003-05-15
CURRENT
J94_200305
This SAE Standard provides performance and general design requirements and related test procedures for a combination tail and floodlamp for use on industrial wheeled equipment that may be operated on public roads.
Standard
Procedure for the Continuous Sampling and Measurement of Non-Volatile Particle Emissions from Aircraft Turbine Engines
2013-11-18
HISTORICAL
AIR6241
This SAE Aerospace Information Report (AIR) describes procedures, required continuous sampling conditions, and instrumentation for the measurement of non-volatile particle number and mass concentrations from the exhaust of aircraft gas turbine engines. Procedures are included to calculate sampling loss performance. This AIR is not intended for in-flight testing, nor does it apply to engine operating in the afterburning mode.
Standard
Procedure for the Continuous Sampling and Measurement of Non-Volatile Particle Emissions from Aircraft Turbine Engines
2020-07-28
CURRENT
AIR6241A
This Aerospace Information Report (AIR) is a historical technical record describing procedures, required continuous sampling conditions, and instrumentation for the measurement of non-volatile particle number and mass concentrations from the exhaust of aircraft gas turbine engines. Procedures are included to calculate sampling loss performance. This AIR is not intended for in-flight testing, nor does it apply to engine operating in the afterburning mode. This Aerospace Information Report is a historical technical record of the initial document detailing the measurement of non-volatile particle emissions at the exit plane of aircraft gas turbine engines. This methodology was adopted by ICAO into Annex 16 Vol II and updated into Aerospace Recommended Practice ARP6320. Future updates of this document may include explanations of the reasoning and assumptions used to develop this measurement methodology.
Standard
AS6070-6117 Chain (1/2" Pitch) and Fittings Assembly Code Non-Reversible Control
1951-06-11
CURRENT
AS6070-3
No scope available.
Standard
Validation Methods For MIL-STD-1760D Mission Stores
2014-09-29
CURRENT
AS42701
This document establishes techniques for validating that a mission store complies with the interface requirements contained in MIL-STD-1760 Revision D.
Standard
Electronic Design Interchange Format Version 200
2016-05-31
CURRENT
EIA548
Standard
Procedure for the Continuous Sampling and Measurement of Non-Volatile Particle Emissions from Aircraft Turbine Engines
2020-07-28
WIP
AIR6241B
This Aerospace Information Report (AIR) is a historical technical record describing procedures, required continuous sampling conditions, and instrumentation for the measurement of non-volatile particle number and mass concentrations from the exhaust of aircraft gas turbine engines. Procedures are included to calculate sampling loss performance. This AIR is not intended for in-flight testing, nor does it apply to engine operating in the afterburning mode.
This Aerospace Information Report is a historical technical record of the initial document detailing the measurement of non-volatile particle emissions at the exit plane of aircraft gas turbine engines. This methodology was adopted by ICAO into Annex 16 Vol II and updated into Aerospace Recommended Practice ARP6320.
Future updates of this document may include explanations of the reasoning and assumptions used to develop this measurement methodology.
Standard
CIRCUIT BREAKER - AIRCRAFT, TRIP-FREE, PUSH-PULL, SOCKET TERMINAL, 1 THROUGH 25 AMPS, TYPE I -55 THROUGH +121 °C
2018-09-18
WIP
AS33203
SCOPE IS NOT AVAILABLE
Standard
Circuit Breaker - Aircraft, Trip-Free, Blade Terminal, 3 Phase, 1 Thru 25 Amp, Type I -55°C Thru +71°C
2017-09-25
WIP
AS14155
This detail specification defines the dimensional and performance requirements for a three phase aircraft circuit breaker with flat blat style terminals.
Standard
CIRCUIT BREAKER - AIRCRAFT, TRIP-FREE, SOCKET TERMINAL, 3 PHASE, 1 THRU 25 AMP, TYPE I -55°C THRU +71°C
2018-09-18
WIP
AS14156
SCOPE IS NOT AVAILABLE
Standard
WIRE, ELECTRICAL, FLUOROPOLYMER-INSULATED, CROSSLINKED MODIFIED ETFE, FLUORIDE CONTROLLED, MEDIUM WEIGHT, SILVER-COATED COPPER, 200 °C, 600 VOLT, ROHS
2022-06-20
CURRENT
AS22759/59
Standard
WIRE, ELECTRICAL, FLUOROPOLYMER-INSULATED CROSSLINEKD MODIFIED ETFE, FLUORIDE CONTROLLED, MEDIUM WEIGHT, SILVER-COATED HIGH STRENGTH COPPER ALLOY, 200 °C, 600 VOLT, ROHS
2022-06-13
CURRENT
AS22759/60
Standard
SILICONE RESIN, ELASTOMERIC, TRANSPARENT ROOM TEMPERATURE CURE
1968-11-01
HISTORICAL
AMS3370
Standard
Insulation, Sound and Thermal Resin-Bonded Glass Fiber, Medium Filament
2015-05-13
CURRENT
AMS3676D
This specification covers resin-bonded glass fibers in the form of felted pads, flat or in rolls.
