SAE AS25427
Current
The latest, up-to-date edition.
Coupling Assembly, Hydraulic, Self-Sealing, Quick Disconnect
Hardcopy , PDF
English
27-07-2015
1 SCOPE
2 APPLICABLE DOCUMENTS
3 REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY
6 NOTES
This specification covers the detail requirements for aircraft hydraulic self-sealing quick disconnect couplings, for use in types I and II hydraulic systems (-65°F to +275°F temperature range) as defined by Specification MIL-H-5440.
| DevelopmentNote |
Supersedes MIL C 25427 (A). (06/2005)
|
| DocumentType |
Standard
|
| Pages |
17
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
This specification covers the detail requirements for aircraft hydraulic self-sealing quick disconnect couplings, for use in types I and II hydraulic systems (-65°F to +275°F temperature range) as defined by Specification MIL-H-5440.
| SAE ARP994B | Design of Tubing Installations for Aerospace Hydraulic Systems |
| SAE ARP994C | Design of Tubing Installations for Aerospace Hydraulic Systems |
| MIL-STD-130 Revision N:2007 | Identification Marking of U.S. Military Property |
| MIL-F-18280 Revision F:1995 | Fittings, Flareless Tube, Fluid Connection (S/S by SAE-AS18280) |
| MS24335 Revision C:1994 | Flange, Bulkhead Mounting, Hydraulic, Self-Sealing Coupling |
| MS24334 Revision E:1992 | Coupling Assembly, Hydraulic, Self-Sealing, Flareless Fitting to Internal Thread Boss |
| MS28774 Revision M:2009 | Retainer, Packing Backup, Single Turn, Polytetraflouroethylene |
| MS28775 Revision E:1984 | PACKING, PREFORMED, HYDRAULIC, +275 DEG. F (\"O\" RING) (S/S BY SAE-AS28775) |
| MS28782 Revision E:2006 | Retainer, Packing, Back-up, Teflon |
| MIL-H-8775 Revision D:1976 | Hydraulic System Components, Aircraft and Missiles General Specification for (S/S by SAE-AS8775) |
| MIL-F-5509 Revision D:1978 | Fitting, Flared Tube, Fluid Connection (see Notice 2 for Additional Superseding Information) |
| MS28783 Revision F:2006 | Ring, Gasket, Back-up, PTFE |
| MIL-H-5440 Revision H:1993 | Hydraulic Systems, Aircraft, Design and Installation Requirements for (S/S by SAE-AS5440) |
| MIL H 5606 : G | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE |
| AND10064 : LATEST | FITTINGS - INSTALLATION OF FLARED TUBE, STRAIGHT THREADED CONNECTORS |
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