Criteria

Text:
Content:
Topic:
Display:

Results

Viewing 1 to 30 of 2111
HISTORICAL
1974-12-01
Standard
AMS3380B
This specification covers polytetrafluoroethylene resin in the form of extruded and sintered flexible hose reinforced with wire braid.
HISTORICAL
1983-07-01
Standard
AMS3380C
This specification covers polytetrafluoroethylene resin in the form of extruded and sintered flexible hose reinforced with wire braid.
CURRENT
1991-04-01
Standard
AMS3380D
This specification covers a polytetrafluoroethylene resin in the form of extruded and sintered flexible tube reinforced with wire braid.
HISTORICAL
1960-01-01
Standard
AMS3380
This specification covers polytetrafluoroethylene resin in the form of extruded and sintered flexible tube reinforced with wire braid. Primarily for fluid lines operating in service up to 230 degrees C (446 degrees F) and under pressures up to 1500 psi (10,342 kPa).
HISTORICAL
1965-09-01
Standard
AMS3380A
This specification covers polytetrafluoroethylene resin in the form of extruded and sintered flexible tube reinforced with wire braid. Primarily for fluid lines operating in service up to 230 degrees C (446 degrees F) and under pressures up to 1500 psi (10,342 kPa).
CURRENT
1993-10-01
Standard
AMS3389D
This specification covers a synthetic rubber in the form of a nonrigid, smooth bore, noncollapsing-type hose.
HISTORICAL
1991-10-01
Standard
AMS3388C
This specification covers a synthetic rubber in the form of a non-rigid, smooth bore, noncollapsing-type hose.
HISTORICAL
1961-07-01
Standard
AMS3389A
This specification covers a synthetic rubber in the form of a nonrigid, smooth bore, noncollapsing-type hose. This hose has been used typically for fueling aircraft, but usage is not limited to such applications. This hose is not intended for flexible connection between tractor and trailer, to be collapsed for drainage, or for operating pressures higher than 250 psi (1724 kPa).
HISTORICAL
1961-07-01
Standard
AMS3388A
This specification covers a synthetic rubber in the form of a non-rigid, smooth bore, noncollapsing-type hose. This hose has been used typically for fueling aircraft, but usage is not limited to such applications. This hose is not intended for flexible connection between tractor and trailer, to be collapsed for drainage, or for operating pressures higher than 185 psi (1276 kPa).
HISTORICAL
1991-10-01
Standard
AMS3389C
This specification covers a synthetic rubber in the form of a non-rigid, smooth bore, noncollapsing-type hose.
HISTORICAL
1958-08-01
Standard
AMS3389
This specification covers a synthetic rubber in the form of a nonrigid, smooth bore, noncollapsing-type hose. This hose has been used typically for fueling aircraft, but usage is not limited to such applications. This hose is not intended for flexible connection between tractor and trailer, to be collapsed for drainage, or for operating pressures higher than 250 psi (1724 kPa).
CURRENT
1993-10-01
Standard
AMS3388D
This specification covers a synthetic rubber in the form of a non-rigid, smooth bore, noncollapsing-type hose.
CURRENT
1993-10-01
Standard
AMS3387E
This specification covers a synthetic rubber in the form of a non-rigid, smooth bore, noncollapsing hose with textile reinforcement.
HISTORICAL
1958-08-01
Standard
AMS3388
This specification covers a synthetic rubber in the form of a non-rigid, smooth bore, noncollapsing-type hose. This hose has been used typically for fueling aircraft, but usage is not limited to such applications. This hose is not intended for flexible connection between tractor and trailer, to be collapsed for drainage, or for operating pressures higher than 185 psi (1276 kPa).
HISTORICAL
1991-10-01
Standard
AMS3386C
This specification covers a synthetic rubber in the form of a soft wall, smooth bore, collapsing type hose.
CURRENT
1993-10-01
Standard
AMS3386D
This specification covers a synthetic rubber in the form of a soft wall, smooth bore, collapsing-type hose.
HISTORICAL
1961-07-01
Standard
AMS3386A
This specification covers a synthetic rubber in the form of soft wall, smooth bore, collapsing-type hose. This hose has been used typically for fueling aircraft from tank trucks or pits where the hose will be rolled flat for stowage on a reel, but usage is not limited to such applications. Not recommended for operating pressures higher than 125 psi (862 kPa).
CURRENT
2015-08-06
Standard
AMS2755G
This specification covers the engineering requirements for producing a thin carbide-bearing nitride case on parts by means of a low-temperature, aerated, molten salt bath process, and the properties of the case.
CURRENT
1994-08-01
Standard
AIR4918
To present a summary of the guidelines and practices presently being used by the aerospace industry for the selection of coiled tubes, flexible hoses, swivel fittings, and extension fittings in aircraft fluid systems.
CURRENT
2005-01-05
Standard
AIR4985
The purpose of this SAE Aerospace Information Report (AIR) is to present a quantitative approach for evaluating the performance and capabilities of an Engine Monitoring System (EMS). The value of such a methodology is in providing a systematic means to accomplish the following: Determine the impact of an EMS on key engine supportability indices such as Fault Detection Rate, Fault Isolation Rate, Mean Time to Diagnose, In-flight Shutdowns (IFSD), Mission Aborts, and Unscheduled Engine Removals (UERs). Facilitate trade studies during the design process in order to compare performance versus cost for various EMS design strategies, and Define a “common language” for specifying EMS requirements and the design features of an EMS in order to reduce ambiguity and, therefore, enhance consistency between specification and implementation.
HISTORICAL
2006-11-15
Standard
AIR5120
For Engine Monitoring Systems to meet their potential for improved safety and reduced operation and support costs, significant attention must be focused on their reliability and validity throughout the life cycle. This AIR will provide program managers, designers, developers and customers a concise reference of the activities, approaches and considerations for the development and verification of a highly reliable engine monitoring system. When applying the guidelines of this AIR it should be noted that engine monitoring systems physically or functionally integrated with the engine control system and/or performing functions that affect engine safety or are used to effect continued operation or return to service decisions shall be subject to the Type Investigation of the product in which they'll be incorporated and have to show compliance with the applicable airworthiness requirements as defined by the responsible Aviation Authority.
HISTORICAL
1999-03-01
Standard
AIR4986
Turbine engine malfunctions account for a substantial portion of the maintenance actions required to keep both fixed and rotary wing aircraft operational. Undetected incipient component failures can result in secondary engine damage and expensive unscheduled maintenance actions. Recent developments of electrostatic methods now provide the potential for the detection of foreign object ingestion and early detection of distress in gas path components. This SAE Aerospace Information Report (AIR) seeks to outline the history of the electrostatic technique and provides examples of state-of-the-art systems for both inlet and exhaust gas debris monitoring systems along with examples of most recent testing.
CURRENT
2009-10-28
Standard
AIR4986A
Turbine engine malfunctions account for a substantial portion of the maintenance actions required to keep both fixed and rotary wing aircraft operational. Undetected incipient component failures can result in secondary engine damage and expensive unscheduled maintenance actions. Recent developments of electrostatic methods now provide the potential for the detection of foreign object ingestion and early detection of distress in gas path components. This SAE Aerospace Information Report (AIR) seeks to outline the history of the electrostatic technique and provides examples of state-of-the-art systems for both inlet and exhaust gas debris monitoring systems along with examples of most recent testing.
HISTORICAL
1978-04-01
Standard
AIR1377
This Aerospace Information Report (AIR) describes equivalent types of equipment that can perform fire tests in accordance with requirements of AS 1055.
CURRENT
1975-09-01
Standard
AIR1378B
This Aerospace Information Report (AIR) is written as a guide for the wording recommended for use, when applicable, in design and procurement specifications for tube fittings and tube assemblies, both for general aerospace fluid power applications and for specific applications.
CURRENT
1980-01-01
Standard
AIR1377A
This Aerospace Information Report (AIR) describes equivalent types of equipment that can perform fire tests in accordance with requirements of AS 1055.
CURRENT
1996-08-01
Standard
AIR1418A
This SAE Aerospace Information Report (AIR) presents flexure fatigue strength of tube fitting joints in the form of graphs showing applied deflection D and total calculated axial stress S versus number of cycles to failure N. The graphs have been prepared from data obtained by actual testing conducted in accordance with ARP1185.
Viewing 1 to 30 of 2111

Filter

  • Standard
    2111
  • Range:
    to:
  • Year: