ISO 2685:1998
Current
Current
The latest, up-to-date edition.
Aircraft — Environmental test procedure for airborne equipment — Resistance to fire in designated fire zones
Available format(s)
Hardcopy , PDF , PDF 3 Users , PDF 5 Users , PDF 9 Users
Language(s)
English, French
Published date
17-12-1998
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This International Standard specifies the tests conditions applied to all components, equipments and structures located in zones designated as "fire zones" and built to satisfy the minimum specified level for resistance to fire.
Two grades of resistance to fire are applicable to components, equipments and structures.
Annexes A and B give details of the types of burners providing the standard flame and how they shall be used.
This International Standard does not relate to the resistance to fire outside designated fire zones, nor to flammability requirements, nor to those conditions induced by the flame coming from the combustion chamber.
| DocumentType |
Standard
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| Pages |
29
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| PublisherName |
International Organization for Standardization
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| Status |
Current
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| Supersedes |
| Standards | Relationship |
| BS ISO 2685:1998 | Identical |
| PN ISO 2685 : 2006 | Identical |
| BS G 262:1998 | Aircraft. Declaration of design and performance for aircraft equipment. Standard form |
| 12/30259268 DC : 0 | BS ISO 14186 - AIR CARGO - FIRE CONTAINMENT COVERS - DESIGN, PERFORMANCE AND TESTING REQUIREMENTS |
| BS ISO 23935:2006 | Aircraft. Environmental test procedures for airborne fluid system components. Resistance to fire in designated fire zones |
| 13/30280086 DC : 0 | BS EN 2591-318 - AEROSPACE SERIES - ELEMENTS OF ELECTRICAL AND OPTICAL CONNECTION - TEST METHODS - PART 318: FIRE-RESISTANCE |
| BS EN 3475-417:2009 | Aerospace series. Cables, electrical, aircraft use. Test methods Fire resistance of cables confined inside a harness |
| BS ISO 8913:2006 | Aerospace. Lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 400°F/3000 psi (204°C/20684 kPa) and 204°C/21000 kPa (400°F/3046 psi). Procurement specification |
| 13/30280221 DC : 0 | BS ISO 8278 - AEROSPACE - HYDRAULIC, PRESSURE COMPENSATED, VARIABLE DELIVERY PUMPS - GENERAL REQUIREMENTS |
| 00/715934 DC : DRAFT OCT 2000 | ISO/CD 8913 - AEROSPACE - LIGHTWEIGHT POLYTETRAFLUOROETHYLENE (PTFE) HOSE ASSEMBLIES, CLASSIFICATION 204 DEGREE C/20 684 KPA (400 DEGREE F/ 3000 PSI), 204 DEGREE C/21 000 KPA (400 DEGREE F/ 3046 PSI) - PROCUREMENT SPECIFICATION |
| 04/30115688 DC : DRAFT JUN 2004 | ISO 23935 - AIRCRAFT. ENVIRONMENTAL TEST PROCEDURES FOR AIRBORNE FLUID SYSTEM COMPONENTS - RESISTANCE TO FIRE IN DESIGNATED FIRE ZONES |
| I.S. EN 3475-417:2009 | AEROSPACE SERIES - CABLES, ELECTRICAL, AIRCRAFT USE - TEST METHODS - PART 417: FIRE RESISTANCE OF CABLES CONFINED INSIDE A HARNESS |
| PREN 4560 : 200P2 | AEROSPACE SERIES - PIPE COUPLING, 37 DEGREES, SPHERICAL, UP TO 21000 KPA - INCH SERIES - TECHNICAL SPECIFICATION |
| PREN 3576 : 200P2 | AEROSPACE SERIES - PTFE FLEXIBLE HOSE ASSEMBLY OF A NOMINAL PRESSURE EQUAL TO 10500 KPA WITH 8 DEGREE 30 MINUTES FITTING IN TITANIUM - PRODUCT STANDARD |
| SAE ARP4925B | Aerospace Design and Installation of Commercial Transport Helicopter Hydraulic Systems |
| PREN 4832 : DRAFT 2017 | AEROSPACE SERIES - ADAPTOR, PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) RING-LOCKED FITTING AND RING-LOCKED FITTING-REDUCER - INCH SERIES - TECHNICAL SPECIFICATION |
| ISO 12333:2000 | Aerospace Constant displacement hydraulic motors General specifications for 35 000 kPa systems |
| PREN 3588 : 200P2 | AEROSPACE SERIES - LIGHTWEIGHT PTFE FLEXIBLE HOSE ASSEMBLY OF A NOMINAL PRESSURE EQUAL TO 28000 KPA WITH 8 DEGREE 30 MINUTES FITTING IN TITANIUM - PRODUCT STANDARD |
| PREN 3580 : 200P1 | AEROSPACE SERIES - STANDARD WEIGHT PTFE FLEXIBLE HOSE ASSEMBLY OF A NOMINAL PRESSURE EQUAL TO 21000 KPA WITH 8 DEGREE 30 MINUTES FITTING IN TITANIUM - PRODUCT STANDARD |
| I.S. EN 3275:2002 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30 MINUTES UP TO 28 000 KPA - DYNAMIC BEAM SEAL - METRIC SERIES - TECHNICAL SPECIFICATION |
| ISO 9528:1994 | Aerospace Standard-weight polytetrafluoroethylene (PTFE) hose assemblies, classification 204 degrees C/21 000 kPa Procurement specification |
| ISO 8913:2006 | Aerospace Lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 400 degrees F/3 000 psi (204 degrees C/20 684 kPa) and 204 degrees C/21 000 kPa (400 degrees F/3 046 psi) Procurement specification |
| 15/30292344 DC : 0 | BS ISO 19281 - AIR CARGO - FIRE RESISTANT CONTAINERS - DESIGN, PERFORMANCE AND TESTING REQUIREMENTS |
| BS EN 3475-408:2005 | Aerospace series. Cables, electrical, aircraft use. Test methods Fire resistance |
| BS EN 4560:2015 | Aerospace series. Pipe coupling 37°, spherical up to 21 000 kPa. Inch series. Technical specification |
| 04/30115718 DC : DRAFT JUL 2004 | ISO 8829-2 - AEROSPACE - TEST METHODS FOR POLYTETRAFLUOROETHYLENE (PTFE) INNERTUBE HOSE ASSEMBLIES - PART 2: NON-METALLIC BRAID |
| 12/30237808 DC : DRAFT JUNE 2012 | BS ISO 19631 - AEROSPACE - TUBE FITTINGS FOR FLUID SYSTEMS, 5000 PSI (35000 KPA) - QUALIFICATION SPECIFICATION |
| BS EN 3197:2010 | Aerospace series. Design and installation of aircraft electrical and optical interconnection systems |
| BS EN 4814:2017 | Aerospace series. Flange couplings up to 21 000 kPa. Technical specification. Inch series |
| BS ISO 19631:2015 | Aerospace series. Tube fittings for fluid systems, 5 080 psi (35 000 kPa). Qualification specification |
| 13/30294318 DC : 0 | BS EN 2591-326 - AEROSPACE SERIES - ELEMENTS OF ELECTRICAL AND OPTICAL CONNECTION - TEST METHODS - PART 326: FUEL FIRE IMMERSION AND CONTAINMENT |
| SAE ARP5757A | Guidelines for Engine Component Tests |
| BS ISO 8278:2016 | Aerospace series. Hydraulic, pressure compensated, variable delivery pumps. General requirements |
| BS ISO 23933:2006 | Aerospace series. Aramid reinforced lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 135°C/20 684 kPa (275°F/3 000 psi) and 135°C/21 000 kPa (275°F/3 046 psi). Procurement specification |
| BS 2G 229:1987 | Schedule for environmental conditions and test procedures for airborne equipment |
| 16/30345017 DC : 0 | BS EN 3475-408 - AEROSPACE SERIES - CABLES ELECTRICAL AIRCRAFT USE - TEST METHODS - PART 408: FIRE RESISTANCE |
| I.S. EN 2591-318:1999 | AEROSPACE SERIES - ELEMENTS OF ELECTRICAL AND OPTICAL CONNECTION - TEST METHODS - PART 318: FIRE-RESISTANCE |
| BS 2M 60:1993 | Specification for separable tube fittings, 24° cone, for aerospace fluid systems |
| SAE AIR 2000 : 2000 | AEROSPACE FLUID SYSTEM STANDARDS, METRIC, NATIONAL AND INTERNATIONAL |
| SAE ARP4752B | Aerospace - Design and Installation of Commercial Transport Aircraft Hydraulic Systems |
| PREN 2591-326 : DRAFT 2017 | AEROSPACE SERIES - ELEMENTS OF ELECTRICAL AND OPTICAL CONNECTION - TEST METHODS - PART 326: FIRE IMMERSION TEST |
| ISO 23933:2006 | Aerospace Aramid reinforced lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 135 degrees C/20 684 kPa (275 degrees F /3 000 psi) and 135 degrees C/21 000 kPa (275 degrees F/3 046 psi) Procurement specification |
| PREN 2255 : DRAFT 96 CORR 2 98 | AEROSPACE SERIES - FLEXIBLE HOSE ASSEMBLIES IN POLYTETRAFLUOROETHYLENE (PTFE) - TYPE 3 - TECHNICAL SPECIFICATION |
| PREN 3275 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREES 30 MINUTES UP TO 28000 KPA DYNAMIC BEAM SEAL - METRIC SERIES - TECHNICAL SPECIFICATION |
| BS EN 3275:2002 | Aerospace series. Pipe coupling 8°30\' up to 28000 kPa. Dynamic beam seal. Metric series. Technical specification |
| I.S. EN 4560:2015 | AEROSPACE SERIES - PIPE COUPLING 37 DEGREES, SPHERICAL, UP TO 21000 KPA - INCH SERIES - TECHNICAL SPECIFICATION |
| BS EN 6049-009:2016 | Aerospace series. Electrical cables, installation. Protection sleeve in meta-aramid fibres Self-wrapping fire protection sleeve, flexible, post installation, operating temperature from -55 °C to 260 °C. Product standard |
| ISO 8278:2016 | Aerospace series Hydraulic, pressure compensated, variable delivery pumps General requirements |
| 05/30128217 DC : DRAFT JAN 2005 | ISO/DIS 23933 - AEROSPACE - ARAMID REINFORCED LIGHTWEIGHT POLYTETRAFLUOROETHYLENE (PTFE) HOSE ASSEMBLIES, CLASSIFICATION 135 DEGREE C/20 684 KPA (275 DEGREE F/3 000 PSI) AND 135 DEGREE C/21 000 KPA (275 DEGREE F/3 046 PSI) - PROCUREMENT SPECIFICATION |
| 17/30358538 DC : 0 | BS EN 3275 - AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30 MINUTES UP TO 28000 KPA - DYNAMIC BEAM SEAL - METRIC SERIES - TECHNICAL SPECIFICATION |
| NF EN 3475-417 : 2009 | AEROSPACE SERIES - CABLES, ELECTRICAL, AIRCRAFT USE - TEST METHODS - PART 417: FIRE RESISTANCE OF CABLES CONFINED INSIDE A HARNESS |
| DIN EN 2591-318:1998-08 | AEROSPACE SERIES - ELEMENTS OF ELECTRICAL AND OPTICAL CONNECTION, TEST METHODS - PART 318: FIRE-RESISTANCE |
| 15/30328108 DC : DRAFT JULY 2015 | BS EN 6059-309 - AEROSPACE SERIES ELECTRICAL CABLES, INSTALLATION - PROTECTION SLEEVES - TEST METHODS - PART 309: FIRE RESISTANCE WHEN FITTED ON A CABLE BUNDLE |
| BS ISO 12334:2000 | Aerospace. Hydraulic, pressure-compensated, variable delivery pumps. General requirements for 35000 kPa systems |
| 06/30160259 DC : 0 | BS ISO 8829-1 - TEST METHODS (PTFE) INNERTUBE HOSE ASSYS - PART 1: STAINLESS STBRAID |
| 14/30310862 DC : 0 | BS EN 4832 - AEROSPACE SERIES - ADAPTOR, PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) RING-LOCKED FITTING AND RING-LOCKED FITTING-REDUCER - INCH SERIES - TECHNICAL SPECIFICATION |
| PREN 2347 : 200P1 | AEROSPACE SERIES - FLEXIBLE HOSE ASSEMBLIES IN POLYTETRAFLUOROETHYLENE (PTFE) - TYPE 4 - TECHNICAL SPECIFICATION |
| PREN 4814 : DRAFT 2015 | AEROSPACE SERIES - FLANGE COUPLINGS UP TO 21000 KPA - TECHNICAL SPECIFICATION - INCH SERIES |
| PREN 3475-408 : 200P1 | AEROSPACE SERIES - CABLES, ELECTRICAL, AIRCRAFT USE - TEST METHODS - PART 408: FIRE RESISTANCE |
| PREN 3572 : 200P1 | AEROSPACE SERIES - PTFE FLEXIBLE HOSE ASSEMBLY WITH CONVOLUTED INNER TUBE OF A NOMINAL PRESSURE UP TO 6800 KPA AND 8 DEGREE 30 MINUTES FITTING IN TITANIUM - PRODUCT STANDARD |
| ISO 10502:2012 | Aerospace — Hose assemblies in polytetrafluoroethylene (PTFE) for use up to 232 °C and 10 500 kPa — Technical specifications and requirements |
| ISO 9938:1994 | Aerospace Polytetrafluoroethylene (PTFE) hose assemblies, classification 204 degrees C/28 000 kPa Procurement specification |
| ISO 19281:2016 | Air cargo Fire resistant containers Design, performance and testing requirements |
| I.S. EN 6049-009:2016 | AEROSPACE SERIES - ELECTRICAL CABLES, INSTALLATION - PROTECTION SLEEVE IN META-ARAMID FIBRES - PART 009: SELF-WRAPPING FIRE PROTECTION SLEEVE, FLEXIBLE, POST INSTALLATION, OPERATING TEMPERATURE FROM -55 DEGREES C TO 260 DEGREES C - PRODUCT STANDARD |
| EN 2591-318:1998 | Aerospace series - Elements of electrical and optical connection - Test methods - Part 318: Fire-resistance |
| ISO 9206:2016 | Aerospace series Constant displacement hydraulic motors General specifications |
| BS EN 2591-318:1998 | Elements of electrical and optical connection. Test methods Fire-resistance |
| UNI EN 3197 : 2012 | AEROSPACE SERIES - DESIGN AND INSTALLATION OF AIRCRAFT ELECTRICAL AND OPTICAL INTERCONNECTION SYSTEMS |
| BS ISO 8829-2:2006 | Aerospace. Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies Non-metallic braid |
| NF EN 3275 : 2002 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREES 30 MINUTES UP TO 28 000 KPA - DYNAMIC BEAM SEAL - METRIC SERIES - TECHNICAL SPECIFICATION |
| BS ISO 9206:2016 | Aerospace series. Constant displacement hydraulic motors. General specifications |
| 13/30280018 DC : 0 | BS EN 2997-001 - AEROSPACE SERIES - CONNECTORS, ELECTRICAL, CIRCULAR, COUPLED BY THREADED RING, FIRE-RESISTANT OR NON FIRE-RESISTANT, OPERATING TEMPERATURES -65 DEGREES C TO 175 DEGREES C CONTINUOUS, 200 DEGREES C CONTINUOUS, 260 DEGREES C PEAK - PART 001: TECHNICAL SPECIFICATION |
| 09/30208359 DC : 0 | BS EN 4814 - AEROSPACE SERIES - FLANGE COUPLINGS - UP TO 21000 KPA - TECHNICAL SPECIFICATION, INCH SERIES |
| BS ISO 10502:2012 | Aerospace. Hose assemblies in polytetrafluoroethylene (PTFE) for use up to 232 °C and 10 500 kPa. Technical specifications and requirements |
| XP PREN 2591-318 : 1992 XP | AEROSPACE SERIES - ELEMENTS OF ELECTRICAL AND OPTICAL CONNECTION - TEST METHODS - PART 318: FIRE-RESISTANCE |
| PREN 2591-318 : DRAFT 2017 | AEROSPACE SERIES - ELEMENTS OF ELECTRICAL AND OPTICAL CONNECTION - TEST METHODS - PART 318: FIRE-RESISTANCE |
| SAE AS595D | Aerospace – Civil Type Variable Delivery, Pressure Compensated, Hydraulic Pump |
| TR 2675 : 1 | AEROSPACE SERIES - DESIGN AND CONSTRUCTION OF FLEXIBLE HOSES AND HOSE ASSEMBLIES FOR FLUIDS IN LIQUID AND GASEOUS CONDITION, INSTALLATION |
| PREN 3584 : 200P2 | AEROSPACE SERIES - LIGHTWEIGHT PTFE FLEXIBLE HOSE ASSEMBLY OF A NOMINAL PRESSURE EQUAL TO 21000 KPA WITH 8 DEGREE 30 MINUTES FITTING IN TITANIUM - PRODUCT STANDARD |
| SAE ARP 986 : 2015 | GUIDE FOR QUALIFICATION TESTING OF AIRCRAFT AIR VALVES |
| SAE MA2005B | Tube Fittings, Aerospace Fluid Systems, Separable, For 24° Cone, General Specification, Metric (ISO 7169) |
| ISO 8829-2:2006 | Aerospace Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies Part 2: Non-metallic braid |
| NF EN 2591-318 : 1998 | AEROSPACE SERIES - ELEMENTS OF ELECTRICAL AND OPTICAL CONNECTION - TEST METHODS - FIRE-RESISTANCE |
| EN 3275:2002 | Aerospace series - Pipe coupling 8°30' up to 28 000 kPa - Dynamic beam seal - Metric series - Technical specification |
| ISO/TR 224:1998 | Aircraft Declaration of design and performance for aircraft equipment Standard form |
| EN 3197:2010 | Aerospace series - Design and installation of aircraft electrical and optical interconnection systems |
| EN 6049-009:2016 | Aerospace series - Electrical cables, installation - Protection sleeve in meta-aramid fibres - Part 009: Self-wrapping fire protection sleeve, flexible, post installation, operating temperature from -55 °C to 260 °C - Product standard |
| EN 3475-417:2009 | Aerospace series - Cables, electrical, aircraft use - Test methods - Part 417: Fire resistance of cables confined inside a harness |
| EN 4814:2017 | Aerospace series - Flange couplings up to 21 000 kPa - Technical specification - Inch series |
| EN 4560:2015 | Aerospace series - Pipe coupling 37°, spherical up to 21 000 kPa - Inch series - Technical specification |
| EN 3475-408:2005 | Aerospace series - Cables, electrical, aircraft use - Test methods - Part 408: Fire resistance |
| EN 3079:2006 | Aerospace series - Pipe coupling 8°30' up to 28 000 kPa - Adaptors - Metric series - Technical specification |
| 11/30254515 DC : 0 | BS EN 4560 - AEROSPACE SERIES - PIPE COUPLING 37 DEGREES, SPHERICAL, UP TO 21000 KPA - INCH SERIES - TECHNICAL SPECIFICATION |
| I.S. EN 3197:2010 | AEROSPACE SERIES - DESIGN AND INSTALLATION OF AIRCRAFT ELECTRICAL AND OPTICAL INTERCONNECTION SYSTEMS |
| BS ISO 8829-1:2009 | Aerospace. Test methods for polytetraflouroethylene (PTFE) inner-tube hose assemblies Metallic (stainless steel) braid |
| PREN 6049-009 : 200P3 | AEROSPACE SERIES - ELECTRICAL CABLES, INSTALLATION - PROTECTION SLEEVE IN META-ARAMID FIBRES - PART 009: SELF-WRAPPING FIRE PROTECTION SLEEVE, FLEXIBLE POST INSTALLATION OPERATING TEMPERATURE FROM -55 DEGREES C TO 260 DEGREES C - PRODUCT STANDARD |
| ISO 8829-1:2009 | Aerospace Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies Part 1: Metallic (stainless steel) braid |
| 13/30279576 DC : 0 | BS ISO 9206 - AEROSPACE - CONSTANT DISPLACEMENT HYDRAULIC MOTORS - GENERAL SPECIFICATIONS |
| ISO 12334:2000 | Aerospace Hydraulic, pressure-compensated, variable delivery pumps General requirement for 35 000 kPa systems |
| 17/30356394 DC : 0 | BS ISO 9206 ED 3 - AEROSPACE - FIXED DISPLACEMENT HYDRAULIC MOTORS - GENERAL SPECIFICATIONS |
| 96/702228 DC : 0 | PREN 4231 - AEROSPACE SERIES - PIPE COUPLINGS 60 DEGREES UP TO 1000 KPA; METRIC SERIES - TECHNICAL SPECIFICATION |
| 12/30275061 DC : 0 | BS EN 6049-009 - AEROSPACE SERIES - ELECTRICAL CABLES, INSTALLATION - PROTECTIVE SLEEVE IN ARAMID FIBRES - PART 009: SELF WRAPPING FIRE PROTECTION SLEEVE, FLEXIBLE POST INSTALLATION OPERATING TEMPERATURE FROM -55 DEGREES C TO 260 DEGREES C - PRODUCT STANDARD |
| BS M 60:1986 | Specification for separable tube fittings for fluid systems |
| ISO 19631:2015 | Aerospace series Tube fittings for fluid systems, 5 080 psi (35 000 kPa) Qualification specification |
| 10/30212765 DC : 0 | BS ISO 10502 - AEROSPACE - HOSE ASSEMBLIES IN POLYTETRAFLUOROETHYLENE (PTFE) FOR USE UP TO 232 DEGREES C AND 10500 KPA - TECHNICAL SPECIFICATION |
| BS ISO 14186:2013 | Air cargo. Fire containment covers. Design, performance and testing requirements |
| BS ISO 12333:2000 | Aerospace. Constant displacement hydraulic motors. General specifications for 35000 kPa systems |
| SAE AS6453 | Fire Containment Cover - Design, Performance, and Testing Requirements |
| PREN 3197 : 200P2 | AEROSPACE SERIES - DESIGN AND INSTALLATION OF AIRCRAFT ELECTRICAL AND OPTICAL INTERCONNECTION SYSTEMS |
| PREN 3079 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30 MINUTES UP TO 28000 KPA - ADAPTORS - METRIC SERIES - TECHNICAL SPECIFICATION |
| PREN 6059-309 : DRAFT 2016 | AEROSPACE SERIES - ELECTRICAL CABLES, INSTALLATION - PROTECTION SLEEVES - TEST METHODS - PART 309: FIRE RESISTANCE WHEN FITTED ON A CABLE BUNDLE |
| PREN 3475-417 : 200P1 | AEROSPACE SERIES - CABLES, ELECTRICAL, AIRCRAFT USE - TEST METHODS - PART 417: FIRE RESISTANCE OF CABLES CONFINED INSIDE A HARNESS |
| I.S. EN 4814:2017 | AEROSPACE SERIES - FLANGE COUPLINGS UP TO 21000 KPA - TECHNICAL SPECIFICATION - INCH SERIES |
| ISO 8829:1990 | Aerospace Polytetrafluoroethylene (PTFE) hose assemblies Test methods |
| ISO 23935:2006 | Aircraft Environmental test procedures for airborne fluid system components Resistance to fire in designated fire zones |
| ISO 14186:2013 | Air cargo — Fire containment covers — Design, performance and testing requirements |
| BS EN 3079:2006 | Pipe coupling 8°30\' up to 28000 kPa. Adaptors. Metric series. Technical specification |
| BS ISO 19281:2016 | Air cargo. Fire resistant containers. Design, performance and testing requirements |
| SAE AS1055D | Fire Testing of Flexible Hose, Tube Assemblies, Coils, Fittings, and Similar System Components |
| BS 3G 100-2.3.13:1973 | Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Resistance to fire in designated fire zones |
| FAA AC 20-104 : 1978 | REVISED POWER PLANT ENGINEERING REPORT NO. 3A, STANDARD FIRE TEST APPARATUS AND PROCEDURE (FOR FLEXIBLE HOSE ASSEMBLIES) |
| ISO 228-1:2000 | Pipe threads where pressure-tight joints are not made on the threads Part 1: Dimensions, tolerances and designation |
| FAA AC 20-135 : 0 | POWERPLANT INSTALLATION AND PROPULSION SYSTEM COMPONENT FIRE PROTECTION TEST METHODS, STANDARDS AND CRITERIA |
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