Aerospace - Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies - Part 1: Metallic (stainless steel) braid

ISO 8829-1:2009 specifies test methods for flexible polytetrafluoroethylene (PTFE) inner tubes with metallic (stainless steel) braided hose and hose assemblies used in aircraft fluid systems, in the pressure and temperature ranges covered by pressure classes and temperature types, as specified in ISO 6771. If performance requirements are not defined in ISO 8829-1:2009, they are defined in the performance specification. ISO 8829-1:2009 is applicable when reference is made to it in a procurement specification or other definition document.

Aéronautique et espace — Méthodes d'essai des tuyauteries flexibles à tube intérieur en polytétrafluoroéthylène (PTFE) — Partie 1: Tresses métalliques (en acier inoxydable)

General Information

Status
Published
Publication Date
22-Mar-2009
Current Stage
9020 - International Standard under periodical review
Start Date
15-Oct-2025
Completion Date
15-Oct-2025

Overview

ISO 8829-1:2009 - Aerospace - Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies - Part 1: Metallic (stainless steel) braid specifies standardized test methods for flexible PTFE inner tubes used with stainless-steel braided hoses and hose assemblies in aircraft fluid systems. The standard applies within the pressure and temperature ranges defined by pressure classes and temperature types in ISO 6771. ISO 8829-1:2009 is referenced when required by procurement or performance specifications and defines how to verify material and assembly performance where tests are not otherwise specified.

Key topics and requirements

ISO 8829-1:2009 focuses on test methods rather than prescriptive performance limits (performance requirements are provided in procurement or performance specifications). Major technical topics include:

  • Inner-tube material tests

    • Density and relative density measurements (to control PTFE crystallinity) following ISO 7258 methods.
    • Tensile testing procedures (specimen preparation, test speeds, machine calibration, measurement of tensile strength and elongation).
    • Rolling (diametral flexing) to detect manufacturing flaws and subsequent proof pressure testing.
  • Electrical properties

    • Electrical conductivity/resistivity test setup and procedure for inner tubes (preconditioning, salt-water electrode method).
  • Hose and hose-assembly tests

    • Stress degradation, pneumatic effusion, volumetric expansion, leakage and proof-pressure tests.
    • Burst pressure, impulse (dynamic) testing, flexure, fuel resistance, low-temperature flexure, pneumatic surge, vacuum and thermal shock tests.
    • Fire resistance testing in accordance with ISO 2685 zones where applicable.
  • Test media and preparation

    • Test fluids listed in Annex A are referenced for specific tests.
    • Conditioning, cleaning, and humidity control procedures for reproducible results.

Practical applications and users

ISO 8829-1:2009 is used to ensure safety, reliability, and traceability of PTFE-lined stainless-steel braided hoses in aerospace fluid systems. Typical users include:

  • Aerospace component manufacturers and hose assemblers validating product conformance
  • Test laboratories performing acceptance, qualification, or failure analysis
  • Procurement and quality engineers writing specifications and acceptance criteria
  • Design and certification teams verifying hydraulic, fuel, pneumatic, or fluid-transfer systems
  • MRO (maintenance, repair and overhaul) organizations assessing in-service hose integrity

Applying ISO 8829-1 helps reduce variability in test methods, supports supplier acceptance, and assists compliance with aircraft system safety and reliability requirements.

Related standards

  • ISO 6771 - Pressure classes and temperature types for aerospace hoses
  • ISO 8829-2 - PTFE inner-tube hose assemblies - Non‑metallic braid
  • ISO 7258 - PTFE tubing density and relative density methods
  • ISO 6772, ISO 6773 - Impulse and thermal shock test methods for aerospace fluid systems
  • ISO 2685 - Fire resistance procedures for airborne equipment

Keywords: ISO 8829-1:2009, PTFE inner-tube hose assemblies, stainless steel braid, aerospace test methods, hose testing, fluid systems, pressure classes, tensile test, proof pressure, electrical conductivity.

Standard

ISO 8829-1:2009 - Aerospace -- Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies

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Frequently Asked Questions

ISO 8829-1:2009 is a standard published by the International Organization for Standardization (ISO). Its full title is "Aerospace - Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies - Part 1: Metallic (stainless steel) braid". This standard covers: ISO 8829-1:2009 specifies test methods for flexible polytetrafluoroethylene (PTFE) inner tubes with metallic (stainless steel) braided hose and hose assemblies used in aircraft fluid systems, in the pressure and temperature ranges covered by pressure classes and temperature types, as specified in ISO 6771. If performance requirements are not defined in ISO 8829-1:2009, they are defined in the performance specification. ISO 8829-1:2009 is applicable when reference is made to it in a procurement specification or other definition document.

ISO 8829-1:2009 specifies test methods for flexible polytetrafluoroethylene (PTFE) inner tubes with metallic (stainless steel) braided hose and hose assemblies used in aircraft fluid systems, in the pressure and temperature ranges covered by pressure classes and temperature types, as specified in ISO 6771. If performance requirements are not defined in ISO 8829-1:2009, they are defined in the performance specification. ISO 8829-1:2009 is applicable when reference is made to it in a procurement specification or other definition document.

ISO 8829-1:2009 is classified under the following ICS (International Classification for Standards) categories: 49.080 - Aerospace fluid systems and components; 83.140.40 - Hoses. The ICS classification helps identify the subject area and facilitates finding related standards.

You can purchase ISO 8829-1:2009 directly from iTeh Standards. The document is available in PDF format and is delivered instantly after payment. Add the standard to your cart and complete the secure checkout process. iTeh Standards is an authorized distributor of ISO standards.

Standards Content (Sample)


INTERNATIONAL ISO
STANDARD 8829-1
First edition
2009-04-01
Aerospace — Test methods for
polytetrafluoroethylene (PTFE) inner-tube
hose assemblies —
Part 1:
Metallic (stainless steel) braid
Aéronautique et espace — Méthodes d'essai des tuyauteries flexibles à
tube intérieur en polytétrafluoroéthylène (PTFE) —
Partie 1: Tresses métalliques (en acier inoxydable)

Reference number
©
ISO 2009
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©  ISO 2009
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ii © ISO 2009 – All rights reserved

Contents Page
Foreword. iv
1 Scope .1
2 Normative references .1
3 Terms and definitions .1
4 Tests of PTFE inner tubes .2
4.1 Density and relative density .2
4.2 Tensile tests .2
4.3 Rolling and proof pressure tests .4
4.4 Electrical conductivity test .6
5 Tests on hoses and hose assemblies .7
5.1 Stress degradation test.7
5.2 Pneumatic effusion test .7
5.3 Electrical conductivity test .8
5.4 Visual and dimensional inspection.10
5.5 Determination of elongation or contraction.10
5.6 Volumetric expansion test.11
5.7 Leakage test .12
5.8 Proof pressure test.12
5.9 Burst pressure tests.13
5.10 Impulse test.13
5.11 Flexure test.14
5.12 Fuel resistance test .14
5.13 Low temperature flexure testing .15
5.14 Pneumatic leakage test .15
5.15 Vacuum test.16
5.16 Pneumatic surge test .16
5.17 Thermal shock test .17
5.18 Fire test .17
Annex A (informative) Test fluids .18
Bibliography .19

Foreword
ISO (the International Organization for Standardization) is a worldwide federation of national standards bodies
(ISO member bodies). The work of preparing International Standards is normally carried out through ISO
technical committees. Each member body interested in a subject for which a technical committee has been
established has the right to be represented on that committee. International organizations, governmental and
non-governmental, in liaison with ISO, also take part in the work. ISO collaborates closely with the
International Electrotechnical Commission (IEC) on all matters of electrotechnical standardization.
International Standards are drafted in accordance with the rules given in the ISO/IEC Directives, Part 2.
The main task of technical committees is to prepare International Standards. Draft International Standards
adopted by the technical committees are circulated to the member bodies for voting. Publication as an
International Standard requires approval by at least 75 % of the member bodies casting a vote.
ISO 8829-1 was prepared by Technical Committee ISO/TC 20, Aircraft and space vehicles, Subcommittee
SC 10, Aerospace fluid systems and components.
ISO 8829 consists of the following parts, under the general title Aerospace — Test methods for
polytetrafluoroethylene (PTFE) inner-tube hose assemblies:
⎯ Part 1: Metallic (stainless steel) braid
⎯ Part 2: Non-metallic braid
iv © ISO 2009 – All rights reserved

INTERNATIONAL STANDARD ISO 8829-1:2009(E)

Aerospace — Test methods for polytetrafluoroethylene (PTFE)
inner-tube hose assemblies —
Part 1:
Metallic (stainless steel) braid
1 Scope
This part of ISO 8829 specifies test methods for flexible polytetrafluoroethylene (PTFE) inner tubes with
metallic (stainless steel) braided hose and hose assemblies used in aircraft fluid systems, in the pressure and
temperature ranges covered by pressure classes and temperature types, as specified in ISO 6771.
If performance requirements are not defined in this part of ISO 8829, they are defined in the performance
specification.
This part of ISO 8829 is applicable when reference is made to it in a procurement specification or other
definition document.
NOTE Fluids used for the tests are listed in Annex A. The requirements for non-metallic braid hose assemblies are
given in ISO 8829-2.
2 Normative references
The following referenced documents are indispensable for the application of this document. For dated
references, only the edition cited applies. For undated references, the latest edition of the referenced
document (including any amendments) applies.
ISO 2685, Aircraft — Environmental test procedure for airborne equipment — Resistance to fire in designated
fire zones
ISO 6772, Aerospace — Fluid systems — Impulse testing of hydraulic hose, tubing and fitting assemblies
ISO 6773, Aerospace — Fluid systems — Thermal shock testing of piping and fittings
ISO 7258, Polytetrafluoroethylene (PTFE) tubing for aerospace applications — Methods for the determination
of the density and relative density
3 Terms and definitions
For the purposes of this document, the following terms and definitions apply.
3.1
room temperature
temperature in the test laboratory between 15 °C (59 °F) and 32 °C (90 °F)
3.2
fire protection
flame- and heat-retardant element over the hose assembly
4 Tests of PTFE inner tubes
4.1 Density and relative density
4.1.1 Principle
This test is intended to control the crystallinity of PTFE inner tubes.
4.1.2 Test methods
The relative density of the PTFE tubing shall be measured in accordance with ISO 7258, method A or
method B. The density of the PTFE tubing shall be measured in accordance with ISO 7258, method C.
4.2 Tensile tests
4.2.1 Principle
This test is intended to determine the mechanical properties of the PTFE tubing.
4.2.2 Test conditions
Test specimens shall be conditioned for at least 2 h at room temperature prior to testing.
4.2.3 Apparatus
4.2.3.1 Testing machine
The test shall be carried out using a power-driven machine which is capable of maintaining a uniform rate of
jaw separation at 50 mm/min (2 in/min) and which has a suitable dynamometer and a device for measuring
the force applied within ± 2 %. If the capacity range cannot be changed during a test, as in the case of
pendulum dynamometers, the force applied at breaking point shall be measured within ± 2 %, and the
smallest tensile force measured shall be accurate to within ± 10 %.
If the dynamometer is of the compensating type for measuring tensile stress directly, means shall be provided
to make adjustments for the cross-sectional area of the test specimen. The response of the recorder shall be
sufficiently rapid that the force applied is measured accurately during the elongation of the test specimen to
breaking point. If the test machine is not equipped with a recorder, a device shall be provided that indicates,
after fracture, the maximum force applied during elongation. Testing machines shall be capable of measuring
elongation in increments of 10 %.
4.2.3.2 Micrometer
The micrometer used for measuring flat test specimen thickness shall be capable of exerting a pressure of
(25 ± 5) kPa [(3,63 ± 0,7) psi] on the test specimens and of measuring the thickness to within ± 0,025 mm
(0,001 in).
NOTE Dial micrometers exerting either a force of (0,8 ± 0,15) N [(0,18 ± 0,034) lbf] on a circular foot 6,35 mm
(0,25 in) in diameter, or a force of (0,2 ± 0,04) N [(0,045 ± 0,009) lbf] on a circular foot 3,2 mm (0,125 in) in diameter,
conform to the pressure requirement specified above. It is not advisable to use a micrometer to measure the thickness of
test specimens narrower in width than the diameter of the foot unless the contact pressure is properly adjusted.
4.2.4 Calibration of testing machine
The testing machine shall be calibrated.
2 © ISO 2009 – All rights reserved

If the dynamometer is of the strain-gauge type, the test machine shall be calibrated at one or more forces at
regular intervals.
4.2.5 Test specimens
The specimens shall be in accordance with Figure 1.
NOTE Careful maintenance of the cutting edges of the die is extremely important and can be achieved by light daily
honing and touching up of the cutting edges with jeweller’s hard honing stones. The condition of the die can be assessed
by determining the breaking point on any series of broken test specimens. When broken test specimens are removed from
the jaws of the test machine, it is advantageous to pile these test specimens and note if there is any tendency to break at
or near the same portion of each test specimen. Breaking points consistently occurring at the same place can be an
indication that the die is dull, nicked or bent at that particular position.
Dimensions in millimetres
Figure 1 — Test specimen for tensile test
4.2.6 Determination of tensile strength and elongation
4.2.6.1 Procedure
Place the test specimens (see 4.2.5) in the jaws of the testing machine (see 4.2.3.1), taking care to adjust the
specimen symmetrically so that the tension will be distributed uniformly over the cross-section. Start the
machine and note continuously the distance between the jaws, taking care to avoid parallax. At fracture,
measure and record the elongation to the nearest 10 % on the scale.
4.2.6.2 Expression of results
1)
Calculate the tensile strength, R , expressed in newtons per square millimetre , using Equation (1):
m
F
R = (1)
m
S
where
F is the measured force, in newtons, required to fracture the test specimens;
S is the cross-sectional area, in square millimetres, of the test specimen before application of force.

1) 1 N/mm = 1 MPa.
Calculate the percentage total elongation at fracture, A , using Equation (2):
t

⎛LL−
uo
A=×100 (2)


t

L
⎝ o

where
L is the length measured between the jaws at fracture of the test specimen;

u
L is the original length measured between the jaws before application of force.

o
4.3 Rolling and proof pressure tests
4.3.1 Principle
This test is intended to check that there are no flaws in the sintered tube.
4.3.2 Rolling test — Procedure
Pass each tube, in a single pass, through six sets of metal rollers, so that it is subjected to the sequence of
diametral flexings specified in Table 1. Rollers shall be arranged to prevent inadvertent rotation in the tube. It
is assumed that the tube is in a horizontal position and that pressure of the first set of rollers is exerted
vertically. Angles given for the final three sets of rollers may be taken as either clockwise or counter clockwise
from the vertical diameter of the tube. Roller angles shall be as specified in Table 1. A tolerance of ± 2° is
allowed on each roller angle.
Table 1 — Roller functions and angles
Set of metal rollers Type of action Roller angle
1 Flattening 0°
2 Flattening 90°
3 Rounding 0°
4 Flattening 45°
5 Flattening 135°
6 Rounding 45°
4 © ISO 2009 – All rights reserved

The roller gap dimensions shall not be greater than those specified in Table 2 for each size.
Table 2 — Roller gap dimensions
Hose size Maximum flattening gap Maximum rounding gap
Class B Class D Class B Class D
Inch part
Metric 10 500 kPa 21 000 kPa 10 500 kPa 21 000 kPa
Equivalent outside
part (1 523 psi) (3 046 psi) (1 523 psi) (3 046 psi)
diameter of tube
hose and higher hose hose and higher hose
Size Size mm (in) mm (in) mm (in) mm (in) mm (in)
DN05 4,762 (0,187) 5,2 (0,205) 5,2 (0,205) 5,5 (0,216) 6,4 (0,252)
−3
DN06 −4 6,350 (0,250) 5,5 (0,216) 7,1 (0,279) 5,5 (0,216) 6,4 (0,252)
DN08 −5 7,937 (0,312) 5,5 (0,216) — — 6,4 (0,252) — —
DN10 −6 9,525 (0,375) 5,5 (0,216) 7,1 (0,279) 7,9 (0,311) 8,3 (0,327)
DN12 −8 12,700 (0,500) 5,9 (0,232) 8,3 (0,327) 9,5 (0,374) 11,9 (0,468)
DN16 15,875 (0,625) 6,4 (0,252) 8,3 (0,327) 12,7 (0,500) 14,7 (0,578)
−10
DN20 −12 19,050 (0,750) 6,4 (0,252) 8,3 (0,327) 12,7 (0,500) 17,5 (0,689)
DN25 −16 25,400 (1,000) 6,4 (0,252) 8,3 (0,327) 19,1 (0,752) 21 (0,827)
DN32 −20 31,750 (1,250) 7,9 (0,311) 11,1 (0,437) 22,2 (0,874) 25,4 (1,000)
DN40 38,100 (1,500) 9,5 (0,374) — — 31,8 — — —
−24
NOTE Special size high pressure hose assembly callout utilizes the lower hose size value noted.

4.3.3 Proof pressure test — Procedure
After the roll test, hold the tube for not less than 2 min at proof pressures as shown in Table 3, using water or
air as the test medium.
Table 3 — Proof pressures
Hose size Proof pressures
Class B Class D
Inch part
Metric part
10 500 kPa (1 523 psi) 21 000 kPa (3 046 psi)
Equivalent outside diameter of tube
hose and higher hose
Size Size mm (in) kPa (psi) kPa (psi)
DN05 −3 4,762 (0,187) 2690 (390) 2690 (390)
DN06 −4 6,350 (0,250) 2480 (360) 2620 (380)
DN08 7,937 (0,312) 2000 (290) — —
−5
DN10 −6 9,525 (0,375) 1590 (230) 1930 (280)
DN12 −8 12,700 (0,500) 1240 (180) 1520 (220)
DN16 −10 15,875 (0,625) 1170 (170) 1170 (170)
DN20 19,050 (0,750) 965 (140) 890 (130)
−12
DN25 −16 25,400 (1,000) 621 (90) 660 (95)
DN32 −20 31,750 (1,250) 448 (65) 660 (95)
DN40 −24 38,100 (1,500) 310 (45) — —
NOTE Special size high pressure hose assembly callout utilizes the lower hose size value noted.
4.4 Electrical conductivity test
4.4.1 Preconditioning
The test specimen shall be a 350 mm (13,78 in) length of PTFE hose tube, with braid removed. The inner
surface of the tube shall be washed first with solvent (test fluid No.1; see Annex A) and then with isopropyl
alcohol (test fluid No.2; see Annex A) to remove surface contamination. The inside of the tube shall then be
thoroughly dried at room temperature.
4.4.2 Procedure
Arrange the test specimen vertically as shown in Figure 2. The relative humidity shall be kept below 70 %.
Apply (1 000 ± 10) V d.c. between the upper and lower electrodes (salt water solution). The salt water solution
shall be a solution of sodium chloride in chemically pure water [ρ (NaCl) = 450 g/l].
2)
Measure the current with an instrument having a sensitivity of at least 1 µA .
Dimensions in millimetres
Key
1 probe 6 O-ring
2 conductor tube 7 vent (if any)
3 vent 8 polytetrafluoroethylene (PTFE) (tube hose inner liner)
4 upper electrode (mercury or salt water solution) 9 non-metallic container
5 non-metallic plug 10 lower electrode (mercury or salt water solution)
Figure 2 — Test set-up for electrical conductivity test on inner tubes

−6
2) 1 µA = 1 × 10 A.
6 © ISO 2009 – All rights reserved

5 Tests on hoses and hose assemblies
5.1 Stress degradation test
5.1.1 Principle
This test is intended to verify that the hose inner tube has been sintered and quenched to the proper
crystallinity to eliminate stress cracking or creep with subsequent leakage.
5.1.2 Class D 21 000 kPa (3 046 psi) and higher hose — Procedure
5.1.2.1 Fill the hose assemblies with a high-temperature test fluid (test fluid No.3; see Annex A) and
place in an oven maintained at (204 ± 5) °C [(400 ± 9) °F]. Apply to the hose assemblies the nominal working
pressure specified in the procurement specification.
Precautions shall be taken to ensure that the hose assemblies do not come into contact with parts of the oven
that are at a higher temperature.
5.1.2.2 After at least 20 h at 204 °C (400 °F), gradually release the pressure, remove the assemblies
from the oven, drain and cool to room temperature. Then flush the assemblies with a quantity of fresh high-
temperature test fluid (test fluid No.3; see Annex A), equivalent in volume to at least twice the volume of the
test specimen volume, and drain.
5.1.2.3 Fill the hose assemblies with hydraulic test fluid (test fluid No.4; see Annex A). Apply to the hose
assemblies the nominal working pressure specified in the procurement specification and hold that pressure for
at least 2 h at room temperature.
5.1.2.4 Repeat the procedure specified in 5.1.2.1 to 5.1.2.3 a total of three times.
5.1.2.5 Within 4 h after the final pressurization period of 2 h, drain the hose assemblies, flush with
trichlorotrifluoroethane (test fluid No.5; see Annex A) and place in an oven for at least 1 h at a temperature of
(70 ± 5) °C [(158°± 9) °F].
5.1.2.6 Within 8 h after the drying process has been completed, remove the hose assemblies from the
oven, cool to room temperature, and then subject to a pneumatic effusion (air under water) test. For this test,
install the hose assemblies in a test set-up constructed similarly to that shown in Figure 3.
5.1.2.7 Immerse the test set-up with the hose assemblies installed in water. Apply nominal pressure for at
least 15 min to allow any entrapped air in the hose to escape.
5.1.2.8 Hold the pressure for a further period of 5 min, during which time collect the gas escaping from
the test specimen, including the juncture of the hose and the fitting, but not including the fitting nut. After the
pressurization period of 5 min, calculate the average rate of effusion through the hose and two fittings
expressed as millilitres per minute per metre of the hose length.
5.1.3 Class B 10 500 kPa (1 523 psi) hose – Procedure
The hose assemblies shall be tested in the same manner as specif
...

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제목: ISO 8829-1:2009 - 항공우주 - 폴리테트라플루오로에틸렌 (PTFE) 내부 튜브 호스 어셈블리를 위한 시험 방법 - 제1부: 금속 (스테인레스 스틸) 브레이드 내용: ISO 8829-1:2009는 항공기 유체 시스템에서 사용되는 스테인레스 스틸로 이루어진 메탈 브레이드 호스 어셈블리와 유연한 폴리테트라플루오로에틸렌 (PTFE) 내부 튜브에 대한 시험 방법을 규정한다. 이 표준은 ISO 6771에서 정의된 압력 및 온도 범위에 해당한다. 만약 ISO 8829-1:2009에서 성능 요구 사항이 정의되지 않은 경우, 이는 성능 사양에서 정의된다. 이 표준은 구매 명세 또는 다른 정의 문서에서 참조되는 경우에 적용된다.

ISO 8829-1:2009 is a standard that specifies test methods for polytetrafluoroethylene (PTFE) inner tubes with metallic braided hose assemblies used in aircraft fluid systems. The standard covers the pressure and temperature ranges defined in ISO 6771. If there are no performance requirements defined in ISO 8829-1:2009, they will be defined in the performance specification. The standard is applicable when referenced in a procurement specification or other definition document.

記事のタイトル:ISO 8829-1:2009 - 航空宇宙 - ポリテトラフルオロエチレン(PTFE)内部チューブホースアセンブリのテスト方法 - パート1:金属(ステンレス鋼)ブレード 記事の内容:ISO 8829-1:2009は、航空機の流体システムで使用される金属(ステンレス鋼)ブレードホースアセンブリとフレキシブルなポリテトラフルオロエチレン(PTFE)内部チューブに対するテスト方法を定めています。この規格は、ISO 6771で定義された圧力および温度範囲に適用されます。ISO 8829-1:2009で性能要件が定義されていない場合は、性能仕様書で定義されます。この規格は、調達仕様書または他の定義文書で参照される場合に適用されます。