Download or read book BS ISO 9528 Aerospace Standard weight Polytetrafluoroethylene PTFE Hose Assemblies Classification 204 C 21 000 KPa Procurement Specification written by British Standards Institution and published by . This book was released on 2020 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aerospace Standard weight Polytetrafluoroethylene PTFE Hose Assemblies Classification 204 C 21 000 KPa Procurement Specification written by British Standards Institution and published by . This book was released on 2022 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book BS ISO 9938 Aerospace Polytetrafluoroethylene PTFE Hose Assemblies Classification 204 C 28 000 KPa Procurement Specification written by British Standards Institution and published by . This book was released on 2020 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Lightweight Polytetrafluoroethylene PTFE Hose Assemblies Classification 400 0DF 3000 Psi 204 0DC 20684 KPa and 204 0DC 21000 KPa 400 0DF 3046 Psi Procurement Specification written by British Standards Institute Staff and published by . This book was released on 2007-01-31 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aircraft components, Hydraulic equipment, Pneumatic equipment, Flexible pipes, Polytetrafluoroethylene, Thermoplastic polymers, Classification systems, Temperature, Pressure, Quality assurance, Delivery, Purchasing

Download or read book Aerospace Series Aramid Reinforced Lightweight Polytetrafluoroethylene Ptfe Hose Assemblies Classification 135 0dc20 684 Kpa 275 0df 3 000 Psi and 135 0dc 21 000 Kpa 275 0df 3 046 Psi Procurement Specification written by British Standards Institute Staff and published by . This book was released on 2006-03-16 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: Flexible pipes, Fluids, Air transport engineering, Aircraft components, Vehicle components, Vehicle fuel tanks, Fuel oil, Fuels, Hydraulic control equipment, Reinforced materials, Aramide fibres, Polytetrafluoroethylene

Download or read book Hose Assembly Polytetrafluoroethylene PTFE Up to 232 C and 10 500 KPa Procurement Specification Metric ISO DIS 10502 written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2015 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This Metric Aerospace Standard (MA) covers the requirements for polytetrafluoroethylene (PTFE) hose assemblies for use in aerospace hydraulic, fuel, and lubricating oil systems at temperatures between -55°C and 232°C for Class I assemblies, -55°C and 135°C for Class II assemblies, and at nominal pressures up to 10 500 kPa (105 bar). The hose assemblies are also suitable for use within the same temperature and pressure limitations in aerospace pneumatic systems where some gaseous diffusion through the wall of the PTFE liner can be tolerated.The use of these hose assemblies in pneumatic storage systems is not recommended. In addition, installations in which the limits specified herein are exceeded, or in which the application is not covered specifically by this standard, for example oxygen, shall be subject to the approval of the purchaser. MA2126B has been reaffirmed to comply with the SAE five-year review policy.This standard is word-for-word equivalent to ISO/DIS 10502 except that U.S. backup specifications are used and updated.

Download or read book Hose Assembly Polytetrafluoroethylene PTFE Up to 232 C and 10 500 KPa Procurement Specification Metric ISO DIS 10502 written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2004 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This Metric Aerospace Standard (MA) covers the requirements for polytetrafluoroethylene (PTFE) hose assemblies for use in aerospace hydraulic, fuel, and lubricating oil systems at temperatures between -55°C and 232°C for Class I assemblies, -55°C and 135°C for Class II assemblies, and at nominal pressures up to 10 500 kPa (105 bar). The hose assemblies are also suitable for use within the same temperature and pressure limitations in aerospace pneumatic systems where some gaseous diffusion through the wall of the PTFE liner can be tolerated.The use of these hose assemblies in pneumatic storage systems is not recommended. In addition, installations in which the limits specified herein are exceeded, or in which the application is not covered specifically by this standard, for example oxygen, shall be subject to the approval of the purchaser.

Download or read book HOSE ASSEMBLY POLYTETRAFLUOROETHYLENE PTFE UP TO 450 F 232 C AND 1500 Psi 10 500 KPa PROCUREMENT SPECIFICATION written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 1994 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This Aerospace Standard (AS) covers the requirements for polytetrafluoroethylene (PTFE) hose assemblies for use in aerospace hydraulic, fuel, and lubricating oil systems at temperatures between -67°F and 450°F for Class I assemblies, -67°F and 275°F for Class II assemblies, and at nominal pressures up to 1500 psi. The hose assemblies are also suitable for use within the same temperature and pressure limitations in aerospace pneumatic systems where some gaseous diffusion through the wall of the PTFE liner can be tolerated.The use of these hose assemblies in pneumatic storage systems is not recommended. In addition, installations in which the limits specified herein are exceeded, or in which the application is not covered specifically by this standard, for example oxygen, shall be subject to the approval of the purchaser.

Download or read book Hose Assembly PTFE Heavy Duty 65 To 400 F 55 To 204 C 8000 Psi 56 000 KPa Hydraulic and Pneumatic written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2013 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This Aerospace Standard (AS) defines the requirements for polytetrafluoroethylene (PTFE) heavy duty hose assemblies suitable for use in aircraft and missile hydraulic fluid systems service to 8000 psi and -65 to 400 °F. Gaseous service shall be limited to 150 °F. AS4388 has been reaffirmed to comply with the SAE five-year review policy.

Download or read book HOSE ASSEMBLY POLYTETRAFLUOROETHYLENE PTFE WIRE REINFORCED 204 C 28 000 KPa HYDRAULIC METRIC written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 1994 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Standard establishes the requirements for polytetrafluoroethylene (PTFE) hose assemblies for use in aerospace hydraulic systems at temperatures between -55 °C and 204 °C and at a nominal pressure up to 28 000 kPa (280 bar). The hose assemblies are also suitable for use within the same temperature and pressure limitations in aerospace pneumatic systems where some gaseous diffusion through the wall of the PTFE liner can be tolerated.The use of these hose assemblies in high pressure pneumatic storage systems is not recommended. In addition, installations in which the limits specified herein are exceeded, or in which the application is not covered specifically by this document, for example, oxygen, shall be subject to the approval of the purchaser.

Download or read book Hose Assembly Polytetrafluoroethylene Metallic Reinforced 21 000 KPa 204 C Lightweight Hydraulic and Pneumatic Metric written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2015 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This Aerospace Standard (AS) defines the requirements for a lightweight polytetrafluoroethylene (PTFE) lined, metallic reinforced, hose assembly suitable for use in high temperature, 204 °C, high pressure, 21,000 kPa (210 bar), aircraft hydraulic systems, also for use in pneumatic systems which allow some gaseous diffusion through the PTFE wall. MA1339 has been reaffirmed to comply with the SAE five-year review policy.

Download or read book HOSE ASSEMBLY POLYTETRAFLUOROETHYLENE PTFE CRES REINFORCED 204 C 21 000 KPA LIGHTWEIGHT BEAM SEAL STRAIGHT TO STRAIGHT METRIC written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2015 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: MA2170 HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY. Length "L" is a four digit number of which the first three digits describe the hose assembly length in whole centimeters (cm), and the fourth digit, the fraction of a cm in millimeters (mm). Length "L" is measured from "face of seat" to "face of seat". For length increments and tolerances see Table 3. A true circular cross section is not required through the fitting I.D. However, the applicable ball diameter listed in Table 1 shall pass through the end fitting after it is attached to the hose assembly. Distance across corners of the coupling nut may exceed this dimension. Standard coupling nuts shall be in accordance with MA2275 or MA2276 and mate with MA2273 fitting ends. Nonstandard coupling nuts may be used provided they are dimensionally and functionally equivalent and provided they cannot be removed from the fitting. Nonstandard nuts shall meet torque test requirements per MA2007. Diameters are listed for clamp selection. Tubular sleeves may not be a perfect round and shall be measured with a diameter tape rule (often referred to as a pi-tape). Tubular abrasion (TFE) sleeves shall have an I.D. no greater than hose O.D. + 1.27 mm. Axial movement of the sleeve installed on the hose shall not exceed 1.27 mm. Ends of the tubular sleeve shall be terminated with a length of MIL-I-23053/11 (FEP) class 1 or 2, color clear, per Table 5 and Figure 2. Coil abrasion sleeves, when assembled on a straight hose, shall have an average gap between coils not exceeding 1.27 mm. Displacement of the coils of the sleeve, causing a greater gap, shall not be cause for rejection if the coils can be repositioned to meet the gap requirements. Ends of the coil sleeve shall be terminated with a length of heat shrinkable sleeving in accordance with Table 5 and Figure 2. Code "B" (nylon coil) abrasion sleeves shall be terminated with MIL-I-23053/5 class 1 or 3, color black. Code "L" (coil abrasion) sleeves shall be terminated with MIL-I-23053/12A, class 1, color transparent, PTFE. (Optional MIL-I-23053/11 (FEP) class 1 or 2, color clear.) The Table 2 sleeve diameters for AS1072 sleeves apply when the sleeve is compressed, or clamped, to contact the hose. In this case, a wrinkle may occur over approximately 10% of the sleeve circumference. The cut ends of the firesleeve shall be coated with RTV silicone rubber, prior to installation, to prevent wicking of the fluids. The firesleeve ends shall be secured to the hose assembly end fittings with corrosion resistant steel bands. After installation, cracks or voids in the firesleeve that expose the fiberglass shall be coated with RTV silicone rubber. Integral abrasion sleeve shall form an integral, permanent part of the hose and shall terminate a maximum of 3.0 mm from the end of the collars. FEP and polyolefin shrink abrasion sleeves shall be shrunk to a snug fit over the hose and end fitting collars. HOSE SIZELENGTH (mm) DN 0650.0 ± 6 DN 10 DN 1263.5 ± 6 DN 16 DN 2076.0 ± 6 DN 25TABLE 5 FIGURE 2 Add "AS1055 type IIb class B-S/P" to identification marking to show level of confidence, "fire proof" (15 min), with AS1055. The ends of the integral firesleeve shall be covered with a length of silicone sleeve extending over the end fitting socket.

Download or read book HOSE ASSEMBLY TETRAFLUOROETHYLENE LIGHTWEIGHT 204 C 21 000 KPa HYDRAULIC METRIC written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 1983 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification covers lightweight hose assemblies intended for use in high-temperature, 204°C, high-pressure, 21 000 kPa (210 bar) aircraft hydraulic systems, also for use in pneumatic systems which allow some gaseous diffusion through the PTFE wall.

Download or read book HOSE ASSEMBLY POLYTETRAFLUOROETHYLENE PTFE CRES REINFORCED 204 C 21 000 KPA LIGHTWEIGHT BEAM SEAL STRAIGHT TO 45 METRIC written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2015 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: MA2171 HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY. Length "L" is a four digit number of which the first three digits describe the hose assembly length in whole centimeters (cm), and the fourth digit, the fraction of a cm in millimeters (mm). Length "L" is measured from "face of seat" to "face of seat". For length increments and tolerances see Table 3. A true circular cross section is not required through the fitting I.D. However, the applicable ball diameter listed in Table 1 shall pass through the end fitting after it is attached to the hose assembly. Distance across corners of the coupling nut may exceed this dimension. Standard coupling nuts shall be in accordance with MA2275 or MA2276 and mate with MA2273 fitting ends. Nonstandard coupling nuts may be used provided they are dimensionally and functionally equivalent and provided they cannot be removed from the fitting. Nonstandard nuts shall meet torque test requirements per MA2007. Diameters are listed for clamp selection. Tubular sleeves may not be a perfect round and shall be measured with a diameter tape rule (often referred to as a pi-tape). Tubular abrasion (TFE) sleeves shall have an I.D. no greater than hose O.D. + 1.27 mm. Axial movement of the sleeve installed on the hose shall not exceed 1.27 mm. Ends of the tubular sleeve shall be terminated with a length of MIL-I-23053/11 (FEP) class 1 or 2, color clear, per Table 5 and Figure 2. Coil abrasion sleeves, when assembled on a straight hose, shall have an average gap between coils not exceeding 1.27 mm. Displacement of the coils of the sleeve, causing a greater gap, shall not be cause for rejection if the coils can be repositioned to meet the gap requirements. Ends of the coil sleeve shall be terminated with a length of heat shrinkable sleeving in accordance with Table 5 and Figure 2. Code "B" (nylon coil) abrasion sleeves shall be terminated with MIL-I-23053/5 class 1 or 3, color black. Code "L" (coil abrasion) sleeves shall be terminated with MIL-I-23053/12A, class 1, color transparent, PTFE. (Optional MIL-I-23053/11 (FEP) class 1 or 2, color clear.) The Table 2 sleeve diameters for AS1072 sleeves apply when the sleeve is compressed, or clamped, to contact the hose. In this case, a wrinkle may occur over approximately 10% of the sleeve circumference. The cut ends of the firesleeve shall be coated with RTV silicone rubber, prior to installation, to prevent wicking of the fluids. The firesleeve ends shall be secured to the hose assembly end fittings with corrosion resistant steel bands. After installation, cracks or voids in the firesleeve that expose the fiberglass shall be coated with RTV silicone rubber. Integral abrasion sleeve shall form an integral, permanent part of the hose and shall terminate a maximum of 3.0 mm from the end of the collars. FEP and polyolefin shrink abrasion sleeves shall be shrunk to a snug fit over the hose and end fitting collars. HOSESIZELENGTH (mm) DN0650.0 ± 6 DN10 DN1263.5 ± 6 DN16 DN2076.0 ± 6 DN25TABLE 5 FIGURE 2 Add "AS1055 type IIb class B-S/P" to identification marking to show level of confidence, "fire proof" (15 min), with AS1055. The ends of the integral firesleeve shall be covered with a length of silicone sleeve extending over the end fitting socket.

Download or read book Hose Assembly Tetrafluoroethylene Lightweight 204 C 21 000 KPa Hydraulic Metric written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2015 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification covers lightweight hose assemblies intended for use in high-temperature, 204 °C, high-pressure, 21 000 kPa (210 bar) aircraft hydraulic systems, also for use in pneumatic systems which allow some gaseous diffusion through the PTFE wall. This document has been reaffirmed to comply with the SAE 5-Year Review policy.

Download or read book Hose Assembly Polytetrafluoroethylene Heavy Duty Metallic Reinforced 204 C 35 000 KPa Hydraulic and Pneumatic Metric written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2015 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This Aerospace Standard (MA) defines the requirements for a heavy duty polytetrafluoroethylene (PTFE) lined, metallic reinforced, hose assembly suitable for use in 204 °C, 35 000 kPa, aircraft and missile hydraulic fluid systems. MA4098 has been reaffirmed to comply with the SAE five-year review policy.

Download or read book Hose Assemblies Polytetrafluoroethylene Aramid Reinforced 135 C Standard Duty 28 000 21 000 KPa Hydraulic Aircraft Systems written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2015 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This document defines the requirements for a PTFE lined, aramid reinforced assembly suitable for use up to 135 °C and up to 28 000 kPa aircraft and missile hydraulic and pneumatic systems. MA1975 has been reaffirmed to comply with the SAE five-year review policy.