oSIST prEN 16602-60-13:2021

Space product assurance - Commercial electrical, electronic and electromechanical (EEE) components

2021-04-21: This EN is based on ECSS-Q-ST-60-13C Rev.1

Raumfahrtproduktsicherung - Anforderungen für die Nutzung von COTS-Komponenten

The purpose of this NWIP is to update EN 16602-60-13(2015), equivalent to ECSS-Q-ST-60-13C “Space product assurance - Commercial electrical, electronic and electromechanical (EEE) components”.
The objectives of this activity are:
1. To disposition all CRs and propose their implementation.
2. Pre-tailoring:
a.   The C version of the ECSS-Q-ST-60-13 standard already provides three classes of EEE COTS components, in line with the ECSS-Q-ST-60C Rev.2,  but the need for modification to the current type of Pre-Tailoring shall be discussed by the WG and the result reported to the TA for instructions.
b   In case the WG believe there will be a need for modification to the current Pre-Tailoring, they will present their request to the TA and specific instructions will be provided.
3. To improve the general usability of the standard by defining requirement rationale where necessary, as specified in Annex B of the present document. The way this information will be published is still to be defined by the TA. The result shall be recorded in a separate document until further instruction by TA.
Justification:
Change Requests have been issued and reviewed by the discipline TAAR. The TA, based on the TAAR assessment, concluded that some of them are important enough and urgent and, as a consequence, required an update of the document.
All CRs recorded on this document shall then be reviewed and implemented by the Policy & Standards Working Group (PSWG) of ESCC that can be supported, if needed, by additional COTS experts that can be properly proposed by the PSWG and approved by the TA and the activities listed in clause 1 shall be carried out.
As identified by the Task Force on New Space Activities, the use of COTS in the current evolving equipment technology is becoming massive and the possibility to use EEE components coming from different business types (Automotive, Aeronautic, Railway, etc.) shall be taken into account .
In addition to the small technical and editorial modifications of Q-ST-60-13C requirements  which have been proposed by the attached CRs, the additional following main technical topics have been identified as needed to be implemented:
-   Enlargement of ECSS-Q-ST-60-13C Rev.1 to passive parts: enlarging the scope of the ECSS-Q-ST-60-13 current issue, by adding requirements about passive parts procurement (the scope of the current issue is limited to active parts).  
-   Automotive standard recognition: This new work item proposal aimed at defining the way to recognize automotive standards (AEC-Q) in EEE parts procurement process.
-   Screening and re-tinning requirements modification: This new work item proposal aimed at reducing screening and re-tinning requirements in certain cases.

Assurance produit des projets spatiaux - Exigences pour l'utilisation de composants commerciaux sur étagère

Zagotavljanje varnih proizvodov v vesoljski tehniki - Zahteve za uporabo COST- komponent

General Information

• Status: Not Published
• Public Enquiry End Date: 30-Nov-2021
• ICS: 49.140 - Space systems and operations
• Technical Committee: I13 - Imaginarni 13
• Current Stage: 4020 - Public enquire (PE) (Adopted Project)
• Start Date: 08-Sep-2021
• Due Date: 26-Jan-2022
• Mandate: M/496 - Mandate addressed to CEN, CENELEC and ETSI to develop standardisation regarding space industry (Phase 3 of the process)
• Ref Project: prEN 16602-60-13 - Space product assurance - Commercial electrical, electronic and electromechanical (EEE) components

RELATIONS

• Replaces: SIST EN 16602-60-13:2015 - Space product assurance - Requirements for the use of COTS components
• Effective Date: 01-Nov-2021

Standards Content (sample)

SLOVENSKI STANDARD
oSIST prEN 16602-60-13:2021
01-november-2021
Nadomešča:
SIST EN 16602-60-13:2015
Zagotavljanje varnih proizvodov v vesoljski tehniki - Zahteve za uporabo COST-
komponent

Space product assurance - Commercial electrical, electronic and electromechanical

(EEE) components
Raumfahrtproduktsicherung - Anforderungen für die Nutzung von COTS-Komponenten

Assurance produit des projets spatiaux - Exigences pour l'utilisation de composants

commerciaux sur étagère
Ta slovenski standard je istoveten z: prEN 16602-60-13
ICS:
49.140 Vesoljski sistemi in operacije Space systems and
operations
oSIST prEN 16602-60-13:2021 en

2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

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oSIST prEN 16602-60-13:2021
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oSIST prEN 16602-60-13:2021
EUROPEAN STANDARD
DRAFT
prEN 16602-60-13
NORME EUROPÉENNE
EUROPÄISCHE NORM
October 2021
ICS 49.140
Will supersede EN 16602-60-13:2015
English version
Space product assurance - Commercial electrical,
electronic and electromechanical (EEE) components

Assurance produit des projets spatiaux - Exigences Raumfahrtproduktsicherung - Anforderungen für die

pour l'utilisation de composants commerciaux sur Nutzung von COTS-Komponenten
étagère

This draft European Standard is submitted to CEN members for enquiry. It has been drawn up by the Technical Committee

CEN/CLC/JTC 5.

If this draft becomes a European Standard, CEN and CENELEC members are bound to comply with the CEN/CENELEC Internal

Regulations which stipulate the conditions for giving this European Standard the status of a national standard without any

alteration.

This draft European Standard was established by CEN and CENELEC in three official versions (English, French, German). A

version in any other language made by translation under the responsibility of a CEN and CENELEC member into its own

language and notified to the CEN-CENELEC Management Centre has the same status as the official versions.

CEN and CENELEC members are the national standards bodies and national electrotechnical committees of Austria, Belgium,

Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy,

Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Republic of North Macedonia, Romania, Serbia,

Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom.

Recipients of this draft are invited to submit, with their comments, notification of any relevant patent rights of which they are

aware and to provide supporting documentation.Recipients of this draft are invited to submit, with their comments, notification

of any relevant patent rights of which they are aware and to provide supporting documentation.

Warning : This document is not a European Standard. It is distributed for review and comments. It is subject to change without

notice and shall not be referred to as a European Standard.
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oSIST prEN 16602-60-13:2021
prEN 16602-60-13:2021 (E)
Table of contents

European Foreword .......................................................................................... 5

Introduction ....................................................................................................... 6

1 Scope .............................................................................................................. 8

2 Normative references .................................................................................... 9

3 Terms, definitions and abbreviated terms ................................................. 11

3.1 Terms from other standards ........................................................................... 11

3.2 Terms specific to the present standard .......................................................... 11

3.3 Abbreviated terms.......................................................................................... 11

3.4 Conventions................................................................................................... 13

3.5 Nomenclature ................................................................................................ 14

4 Requirements for class 1 components ...................................................... 15

5 Requirements for class 2 components ...................................................... 35

6 Requirements for class 3 components ...................................................... 53

7 Quality levels ............................................................................................... 70

8 Procurement test table ................................................................................ 71

9 Pure tin lead finish – risk analysis ........................................................... 109

Annex A (normative) Component control plan (CCP) - DRD .................... 110
Annex B (normative) Declared components list (DCL) - DRD .................. 111

Annex C (normative) Internal Supplier’s specification - DRD ................... 112

Annex D (normative) Parts approval document - DRD .............................. 113

Annex E (informative) EEE documents delivery per review ..................... 114

Annex F (normative) Justification document - DRD .................................. 115

Annex G <> ................................................................................... 118

Annex H (informative) Flow chart for construction analysis and

destructive physical analysis .................................................................. 119

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Bibliography .................................................................................................. 123

Figures

Figure 4-1: <> .............................................................................................. 23

Figure 4-2: <> .............................................................................................. 28

Figure 5-1: <> .............................................................................................. 42

Figure 5-2: <> .............................................................................................. 47

Figure 6-1: <>Lot acceptance test flow chart for Class 3 components ......... 64

Figure 8-1: <> .............................................................................................. 71

Figure 8-2: <> .............................................................................................. 71

Figure 8-3: <> .............................................................................................. 71

Figure 8-4: <> .............................................................................................. 71

Figure 8-5: <> .............................................................................................. 71

Figure 8-6: <> .............................................................................................. 72

Tables

Table 4–1: <> ......................... 24

Table 4–2: <> ....................... 27

Table 4–3: <> ....................... 28

Table 4-4: Documentation for Class 1 components ..................................................... 34

Table 5–1: <> ...................... 42

Table 5–2: <> ...................... 46

Table 5–3: <> ...................... 47

Table 5–4: Documentation for Class 2 components .................................................... 52

Table 6–1: <> .............................................................................................. 60

Table 6–2: <> .............................................................................................. 63

Table 6–3: <> .......................... 64

Table 6–4: Documentation for Class 3 components .................................................... 69

Table 8–1: Procurement test table for ceramic capacitors chips .................................. 74

Table 8–2: Procurement test table for solid electrolyte tantalum capacitors chips ........ 75

Table 8–3: Procurement test table for discrete parts (diodes, transistors,

optocouplers) ............................................................................................ 78

Table 8–4: Procurement test table for fuses ................................................................ 80

Table 8–5: Procurement test table for magnetics......................................................... 81

Table 8–6: Procurement test table for microcircuits ..................................................... 84

Table 8–7: Procurement test table for resistors ........................................................... 85

Table 8–8: Procurement test table for Thermistors ...................................................... 88

Table 8–9: Legacy test files - Evaluation tests for Class 1 components ....................... 90

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Table 8–10: Legacy test files - Screening tests for Class 1 components ..................... 93

Table 8–11: Legacy test files - Lot acceptance tests for Class 1 components ............. 95

Table 8–12: Legacy test files - Evaluation tests - Class 2 components ........................ 98

Table 8–13: Legacy test files - Screening tests - Class 2 components ...................... 101

Table 8–14: Legacy test files - Lot acceptance tests - Class 2 components .............. 103

Table 8–15: Legacy test files - LAT tests - Class 3 components ................................ 106

Table H-1 : Construction analysis sequence .............................................................. 120

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oSIST prEN 16602-60-13:2021
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European Foreword
This document (prEN 16602-60-13:2021) has been prepared by Technical
Committee CEN/CLC/TC 5 “Space”, the secretariat of which is held by DIN
(Germany).
This document (prEN 16602-60-13:2021) originates from ECSS-Q-ST-60-13C
Rev.1 DIR1.
This document is currently submitted to the ENQUIRY.
This document will supersede EN 16602-60-13:2015.
The main changes with respect to EN 16602-60-13:2015 are listed below:
 to be completed (currently the changes are identified with revision
tracking).
This document has been developed to cover specifically space systems and will
therefore have precedence over any EN covering the same scope but with a wider
do-main of applicability (e.g. : aerospace).
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oSIST prEN 16602-60-13:2021
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Introduction
This standard is based on and complementary to ECSS-Q-ST-60C (with upward
revisions). This standard can only be used in conjunction with ECSS-Q-ST-60C in
its current revision. This standard applies only to commercial components - as
defined in its scope - which meet defined technical parameters that are on the
system application level demonstrated to be unachievable with existing space
components or only achievable with qualitative and quantitative penalties. The
standard requires that qualitative and quantitative penalties are specified, as
applicable, as a minimum in terms of quantifiable parameters such as: functional
capability, parts count, power dissipation, frequency of operation, data/signal
processing efficiency, interconnect complexity, mass, volume, …
For traceability to ECSS-Q-ST-60, the modifications or additions are marked in
blue. Text in black colour is unmodified text.
The objective of the EEE component selection, control, procurement and use
requirements is to ensure that EEE components used in a space project enables
the project to meet its mission requirements.
Important elements of EEE component requirements include:
a. component programme management,
b. component selection, evaluation and approval,
c. procurement,
d. handling and storage,
e. component quality assurance,
f. specific components, and
g. documentation.
The main tools which can be used to reach the objective are:
a. concurrent engineering,
b. standardization of component types,
c. characterization of components,
d. assessment of component manufacturers including declared competencies
and processes,
e. testing, screening, lot acceptance and periodic testing,
f. procurement specifications,
g. control and inspection,
h. control of nonconforming materials,
i. assessment and use of existing component data,
j. application of specific control to mitigate risk for components with limited
data or confidence, and
k. information management.
The basic approach is as follows:
 The customer of a given space project defines the EEE component
requirements within the boundaries of this standard. They appear in the
appropriate clauses of the project requirements as defined in ECSS-M-ST-10.
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 The supplier defines a component control plan to implement those
requirements into a system which enables, for instance, to control the
selection, approval, procurement, handling in a schedule compatible with his
requirements, and in a cost-efficient way.
 The supplier ensures that the applicable parts requirements are passed down
to lower level suppliers and ensure that they are compliant to these parts
requirements.
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oSIST prEN 16602-60-13:2021
prEN 16602-60-13:2021 (E)
Scope
This standard defines the requirements for selection, control, procurement and
usage of EEE commercial components for space projects.
This standard is applicable to commercial parts from the following families:
 Ceramic capacitors chips
 Solid electrolyte tantalum capacitors chips
 Discretes parts (transistors, diodes, optocouplers)
 Fuses
 Magnetic parts
 Microcircuits
 Resistors
 Thermistors
Other families of EEE components are not addressed by the present ECSS
standard doesn’t mean that they are forbidden in commercial grade.
In line with ECSS-Q-ST-60, this standard differentiates between three classes of
components through three different sets of standardization requirements
(clauses) to be met.

The three classes provide for three levels of trade-off between assurance and risk.

The highest assurance and lowest risk is provided by class 1 and the lowest

assurance and highest risk by class 3. Procurement costs are typically highest for

class 1 and lowest for class 3. Mitigation and other engineering measures can
decrease the total cost of ownership differences between the three classes. The

project objectives, definition and constraints determine which class or classes of

components are appropriate to be utilised within the system and subsystems.
a. Class 1 components are described in Clause 4
b. Class 2 components are described in Clause 5
c. Class 3 components are described in Clause 6
The requirements of this document are applicable to all parties involved at all
levels in the integration of EEE commercial components into space segment
hardware and launchers.
For easy tailoring and implementation of the requirements into a Requirement
Management Tool, and for direct traceability to ECSS-Q-ST-60, requirements in
this standards have been written in the way of a ECSS Applicability Requirement
Matrix (EARM), as defined in Annex A of ECSS-S-ST-00 “ECSS system –
Description, implementation and general requirements”.

This standard may be tailored for the specific characteristics and constrains of a

space project in conformance with ECSS-S-ST-00.
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oSIST prEN 16602-60-13:2021
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Normative references
The following normative documents contain provisions which, through
reference in this text, constitute provisions of this ECSS standard. For dated
references, subsequent amendments to, or revision of any of these publications
do not apply. However, parties to agreements based on this ECSS Standard are

encouraged to investigate the possibility of applying the more recent editions of

the normative documents indicated below. For undated references, the latest
edition of the publication referred to applies.
EN reference Reference in text Title
EN 16601-00-01 ECSS-S-ST-00-01
ECSS system - Glossary of terms
EN 16602-60 ECSS-Q-ST-60 Space product assurance - Electrical, electronic and
electromechanical (EEE) components

EN 16602-60-14 ECSS-Q-ST-60-14 Space product assurance - Relifing procedure - EEE

components
EN 16602-60-15 ECSS-Q-ST-60-15 Space product assurance – Radiation hardness
assurance – EEE components
ESCC 21300 Terms, definitions, abbreviations, symbols and units
ESCC 24900 Minimum requirements for controlling
environmental contamination of components
ESCC 25500 Methodology for the detection of pure tin in the
external surface finish of case and leads of EEE
components
MIL-STD-750 Test methods for semiconductor devices
MIL-STD-883 Test method standard microcircuits
JESD22-A101 Steady state temperature humidity bias life test
JESD22-A110 Highly accelerated temperature and humidity stress
test
JESD22-A113 Preconditioning of plastic surface mount devices prior
to reliability testing
JESD22-A121 Test Method for Measuring Whisker Growth on Tin
and Tin Alloy Surface Finishes
JESD22-B106 Resistance to soldering temperature for through hole
mounted devices
JESD-201 Environmental Acceptance Requirements for Tin
Whisker Susceptibility of Tin and Tin Alloy Surface
Finishes
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J-STD-020 Moisture/Reflow sensitivity classification for
nonhermetic solid state surface mount devices
J-STD-033 Handling, packing, shipping and use of moisture/
reflow sensitive surface mount devices
GEIA-STD-005-2 Standard for Mitigating the Effects of Tin Whiskers in
Aerospace and High Performance Electronic Systems.
ESCC 21004 GUIDELINES FOR INCOMING INSPECTION OF
EEE COMPONENTS (ESCC Basic Specification No.
21004)
ESCC25100 Single Event Effects Test Method and Guidelines
ESCC22500 GUIDELINES FOR DISPLACEMENT DAMAGE
IRRADIATION TESTING
ESCC20600 Preservation Packaging and Despatch of SCC
Components
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Terms, definitions and abbreviated terms
3.1 Terms from other standards
For the purpose of this standard, the terms and definitions from ECSS-S-ST-00-01
apply.
For the purpose of this standard, the following terms and definitions from ECSS-
Q-ST-60 apply:
agent
characterization
commercial component
concurrent engineering
franchised distributor
parts engineer
parts procurer
qualified parts
screening
space qualified parts
3.2 Terms specific to the present standard
3.2.1 traceability information (trace code)
unique identifier used by manufacturers to label and trace a quantity of
components with a common manufacturing history and thereby common
characteristics.
NOTE 1 The notion of "lot of EEE parts" used for the radiation and
lot acceptance tests is defined by the trace code.
NOTE 2 Several trace codes can be part of a same delivery from the
manufacturer or the distributor.
NOTE 3 It is possible to have several diffusion lots and wafer fabs
(as per ESCC 21300) in the same trace code.
3.3 Abbreviated terms
For the purpose of this Standard, the abbreviated terms from ECSS-S-ST-00-01
and the following apply:
Abbreviation Meaning
AOQ average outgoing quality
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Abbreviation Meaning
ASIC application specific integrated circuit
BGA ball grid array
CA construction analysis
CCD charge coupled device
CCP component control plan
CN change notice
CoC certificate of conformance
CDR critical design review
CR change request
DCL declared components list
DPA destructive physical analysis
DRD document requirement definition
DSM deep Sub-Micron
Ea activation energy
ECSS European Coordination for Space
Standardization
EEE electrical, electronic, electromechanical
EFR early failure rate
ESCC European space components coordination
GSE ground support equipment
HAST highly accelerated stress test
HTRB high temperature reverse bias
JD justification document
LAT lot acceptance test
LED light emitting diode
LVT lot validation testing
MMIC microwave monolithic integrated circuit
PAD parts approval document
PCB parts control board
PCN process change notice
PDA percent defective allowable
PED plastic encapsulated device
PIND particle impact noise detection
QBSD full quadrant back scatter electron detector
QCI
quality conformance inspection
RFD request for deviation
RH relative humidity
RoHs restriction of the use of certain hazardous
substances
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Abbreviation Meaning
RVT radiation verification testing
SCSB Space Components Steering Board
SAM scanning accoustic microscopy
SEM scanning electron microscope
SMD surface mount device
TCI technology conformance inspection
Tg glassivation temperature
THB temperature humidity bias
Tj junction temperature
T/C thermal cycling
3.4 Conventions
a. The term “EEE component“ is synonymous with the terms "EEE Part",
"Component" or just "Part".
b. The term “for approval” means that a decision of the approval authority is
necessary for continuing the process.
c. The term “for review” means that raised reviewers comments are
considered and dispositioned.
d. The term “for information” means that no comments are expected about
the delivered item.
e. For the purpose of clear understanding of this document, hereunder is a
listing of component categories which are covered by the term EEE
component, encapsulated or non-encapsulated, irrespective of the quality
level:
1. Capacitors
2. Connectors
3. Crystals
4. Discrete semiconductors (including diodes, transistors)
5. Filters
6. Fuses
7. Magnetic components (e.g. inductors, transformers, including in-
house products)
8. Monolithic Microcircuits (including MMICs)
9. Hybrid circuits
10. Relays
11. Resistors, heaters
12. Surface acoustic wave devices
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13. Switches (including mechanical, thermal)
14. Thermistors
15. Wires and Cables
16. Optoelectronic Devices (including opto-couplers, LED, CCDs,
displays, sensors)
17. Passive Microwave Devices (including, for instance, mixers,
couplers, isolators and switches)
NOTE Microwave switches consisting of multiple EEE components are
considered as equipment. The requirements of this standard are
applicable to the EEE parts they incorporate and to microwave
switches having a simple design (single EEE part).
3.5 Nomenclature
The following nomenclature applies throughout this document:
a. The word “shall” is used in this Standard to express requirements. All the
requirements are expressed with the word “shall”.
b. The word “should” is used in this Standard to express recommendations.
All the recommendations are expressed with the word “should”.
NOTE It is expected that, during tailoring, recommendations in this
document are either converted into requirements or tailored out.
c. The words “may” and “need not” are used in this Standard to express
positive and negative permissions, respectively. All the positive
permissions are expressed with the word “may”. All the negative
permissions are expressed with the words “need not”.
d. The word “can” is used in this Standard to express capabilities or
possibilities, and therefore, if not accompanied by one of the previous
words, it implies descriptive text.
NOTE In ECSS “may” and “can” have completely different meanings:
“may” is normative (permission), and “can” is descriptive.
e. The present and past tenses are used in this Standard to express statements
of fact, and therefore they imply descriptive text.
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Requirements for class 1 components
Identifier Requirement Applicability
4.1 Component programme management
4.1.1 General
4.1.1a The supplier shall establish and implement throughout the duration N/A
of the business agreement a component programme which ensures
that the requirements of the project as defined by the customer and
the supplier in the related business agreement are in compliance with
this standard.
4.1.2 Components control programme
4.1.2.1 Organization
4.1.2.1a Applicable
4.1.2.1b The supplier’s organization shall comply with all the requirements N/A
of ECSS-M-ST-10.
4.1.2.2 Component control plan
4.1.2.2a Applicable
4.1.2.2b Applicable
4.1.2.2c Applicable
4.1.3 Parts control board
4.1.3a Applicable
4.1.3b Applicable
4.1.3c Applicable
4.1.3d Applicable
4.1.4 Declared component list

4.1.4a For each equipment, its supplier shall issue a DCL in an editable and Applicable

sortable electronic format such as .xls or .xlsx or .csv., as a minimum
compatible with CSV, identifying all component types needed.
NOTE CSV is a common file format that can be used to transfer data
between database or spreadsheet tables (a spreadsheet program is
for example Excel®)
4.1.4b Applicable
4.1.4c Applicable

4.1.4d After equipment CDR, all modifications affecting the PAD and JD Applicable

information shall be implemented, in the "as design" DCL, through
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the CN / CR process and submitted to the customer for approval,
before mounting.
NOTE For JD generation, see 4.2.4.d.
4.1.4e Applicable
4.1.4f Applicable
4.1.4g Applicable
4.1.4h Applicable

4.1.4i The supplier shall establish and update a consolidated “as design" Applicable

DCL at its level and deliver it to the customer
4.1.5 Electrical and mechanical GSE
4.1.5a Applicable
4.1.5b Applicable
4.1.6 EQM components
4.1.6a EEE components used in Engineering Qualification Model (EQM) Applicable
shall be fit, form and function representative of the flight
components and from the same manufacturers.

4.1.6b If thermal vacuum tests are performed on the EQM, the EEE parts Applicable

shall be material representative of the FM parts.
4.2 Component selection, evaluation and approval
4.2.1 General
4.2.1a Applicable
4.2.1b Applicable
4.2.2 Manufacturer and component selection
4.2.2.1 General rules
4.2.2.1a Applicable
4.2.2.1b Applicable
4.2.2.1c <>Preference shall be given to N/A
components which necessitate the least evaluation or qualification
effort.
4.2.2.1d <>Starting with the design phase of N/A
the project the supplier shall ensure maximum use of preferred (see
4.2.2.3) and qualified components to achieve an effective component
reduction and standardization.

4.2.2.1e <>When selecting items, the supplier N/A

shall check the current data, applicability of the basis of qualification,
problem notifications and alerts, and adequacy of specifications.
4.2.2.1f <>The supplier shall implement a N/A
type reduction activity.
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4.2.2.1g For the assessment of commercial components, the supplier shall New
collect the available data on the manufacturer and the component in
the JD specified in the requirement 4.2.4d.
NOTE It is important to check the exhaustiveness
of the manufacturer documentation & data
sheet with respect to e.g. the following
items:
 component marking,
 mechanical description,
 electrical and thermal description.
4.2.2.1h <>For Deep Sub-Micron Technologies (<90nm), the Deleted
detailed test definition shall identify the technology through the
construction analysis and the application.
NOTE 1 It is important to ensure that the test
conditions remain as close as possible to
application.
NOTE 2 This requirement is important due to the
specificities of Deep Sub-Micron
Technologies (<90nm).
4.2.2.2 Parts and material restriction
4.2.2.2a Applicable
4.2.2.2b Applicable

4.2.2.2c With respect to health and safety, beryllium oxide, lithium (except if Applicable

identified in the procurement specification), cadmium, lithium,
magnesium, mercury, zinc, radioactive material and all material
which can cause safety hazard shall not be used.

4.2.2.2d For limited life duration, known instability, safety hazards or Applicable

reliability risk reasons, EEE components listed below shall not be
used:
1. <>EEE components with pure tin (le
...