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APPENDIX 1 TO ETSO-C100c - MPS FOR AVIATION CHILD SAFETY DEVICE

Available versions for ERULES-1963177438-9220

ED Decision 2016/013/R found in: CS-ETSO Amdt 17 - European Technical Standard Orders (Oct 2026)

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###### APPENDIX 1 TO ETSO-C100c – MPS FOR AVIATION CHILD SAFETY DEVICE

*ED
Decision
2016/013/R*

The applicable standard is SAE AS5276/1, ‘Child Restraint Systems
in Transport Category Airplanes’, dated November 2000, with the
following modifications:

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AS
				5276/1 section:
</td>
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Action:
</td>
</tr>
</thead>
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Entire
				document:
</td>
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Throughout
				the document, ‘Aviation Child Safety Device (ACSD)’ shall be
				used instead of ‘CRS’.

 


SAE
				AS5276/1 incorporates, as references, the following test
				standards:

 


1.	SAE
				RP J211, Instrumentation for Impact Tests.

2.	SAE
				AS8049A, Performance Standard for Seats in Civil Rotorcraft,
				Transport Aircraft and General Aviation Aircraft.

3.	SAE
				ARP4466, Dimensional Compatibility of Child Restraint System and
				Passenger Seat Systems in Civil Transport Airplanes.

4.	49
				CFR part 572, Anthropomorphic Test Dummies.

5.	CS
				25.853(a) (Appendix F, Part I(a)(iv)).
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Section
				1
</td>
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To
				be disregarded.
</td>
</tr>
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<td bgcolor="#d9d9d9">
Paragraph
				2.1
</td>
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To
				be replaced with:

 


2.1
				Documents:
The
				following publications form part of this AS to the extent
				specified herein. Other publications are provided for reference.
				In the event of conflict between the text of this document and
				the references cited herein, the text of this document takes
				precedence. Nothing in this document, however, supersedes
				applicable laws and regulations unless a specific exemption has
				been obtained.
</td>
</tr>
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Paragraph
				2.1.1
</td>
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To
				be revised:

 


2.1.1
				SAE Publications:

RP
				J211, Instrumentation for Impact Tests

AS8049B,
				Performance Standard for Seats in Civil, Rotorcraft and Transport
				Aircraft and General Aviation Aircraft
ARP4466,
				Dimensional Compatibility of Child Restraint Systems and
				Passenger Seat Systems in Civil Transport Airplanes
</td>
</tr>
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<td bgcolor="#d9d9d9">
Paragraph
				2.1.2
</td>
<td bgcolor="#d9d9d9">
To
				be revised:

 


2.1.2
				Federal Aviation Administration (FAA) Regulations, Advisory
				Circulars, European Technical Standard Orders and Reports:

 


EASA
				Part-21, Certification Procedures for Products and Parts

CS-25,
				Airworthiness Standards: Transport Category Airplanes

 


AC
				91-62A, Use of Child Seats in Aircraft

AC
				120-87B, Use of Child Restraint Systems on Aircraft

ETSO-C22g,
				Safety Belts

ETSO-C39c,
				AIRCRAFT SEATS and BERTHS CERTIFIED BY STATIC TESTING ONLY

ETSO-C127b,
				Rotorcraft, Transport Airplane, and Normal and Utility Airplane
				Seating Systems

DOT/FAA/AAM/-94/19,
				The Performance of Child Restraint Devices in Transportation
				Category Seats, Gowdy and DeWeese, FAA Office of Aviation
				Medicine Report, September 1994
DOT/FAA/AR-00/12,
				Aircraft Materials Fire Test Handbook
</td>
</tr>
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<td bgcolor="#d9d9d9">
Paragraph
				2.1.3
</td>
<td bgcolor="#d9d9d9">
To
				be revised:

 


2.1.3
				National Highway Traffic Safety Administration (NHTSA)
				Regulations and Documents:

49
				CFR 571.213, Federal Motor Vehicle Safety Standard No. 213 Child
				Restraint Systems

49
				CFR 571.225, Federal Motor Vehicle Safety Standard No. 225 Child
				Restraint Anchorage Systems

49
				CFR 572, Anthropomorphic Test Dummies
NHTSA
				Drawing Package SAS-100-1000, dated June 1, 1993
</td>
</tr>
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Paragraph
				2.1.4
</td>
<td bgcolor="#d9d9d9">
To
				be revised:

 


2.1.4
				ANSI Publications:
ANSI
				Z535.4 -1998 Product Safety Signs and Labels
</td>
</tr>
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<td bgcolor="#d9d9d9">
Paragraph
				2.3
</td>
<td bgcolor="#d9d9d9">
To
				be revised:

 


2.3
				Classification of Children: The physical characteristics of small
				children govern the proper ACSD for use. Mass, standing height,
				and developmental maturity (i.e. age) are important for proper
				ACSD configuration and orientation. As children develop at
				different rates, combined application of these characteristics in
				selecting an ACSD may be difficult. To assist in this process,
				Table 1 defines three stages of child development each
				with a single dominant characteristic underlined. Where an
				occupant falls between categories, the dominant characteristic is
				used to determine the proper ACSD configuration and orientation.

 


Table
				1 — Definitions of Child Categories
<table bgcolor="#d9d9d9" cellpadding="7" cellspacing="0">
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Child
							category
</td>
<td bgcolor="#d9d9d9">
Mass,
							kg (lb)
</td>
<td bgcolor="#d9d9d9">
Height,
							cm (in.)
</td>
<td bgcolor="#d9d9d9">
Age,
							month
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Newborn
</td>
<td bgcolor="#d9d9d9">
Birth
							to 5 (11)
</td>
<td bgcolor="#d9d9d9">
Birth
							to 65 (26)
</td>
<td bgcolor="#d9d9d9">
N/A
</td>
</tr>
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<td bgcolor="#d9d9d9">
Infant
							

</td>
<td bgcolor="#d9d9d9">
5-10
							(11-22)
</td>
<td bgcolor="#d9d9d9">
65-85
							(26-34)
</td>
<td bgcolor="#d9d9d9">
under
							12
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Toddler
							

</td>
<td bgcolor="#d9d9d9">
10-18
							(22-40)
</td>
<td bgcolor="#d9d9d9">
85-110
							(34-44)
</td>
<td bgcolor="#d9d9d9">
over
							12
</td>
</tr>
</table>

 

</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				2.5d
</td>
<td bgcolor="#d9d9d9">
To
				be revised: 


 


d.
				Any child that has attained his or her first birthday, with a
				mass greater than 10 kg (22 lb) and having a standing stature of
				less than 110 cm (44 in.) in height is considered a ‘toddler’
				and should be seated in a forward-facing ACSD with both upper and
				lower torso restraint (Type III).
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				2.6
</td>
<td bgcolor="#d9d9d9">
New
				paragraph to be added:

 


2.6
				Definitions: Refer to 49 CFR 571.213 S4. for aircraft child
				safety device definitions.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				3.2
</td>
<td bgcolor="#d9d9d9">
To
				be revised:

 


3.2
				ACSD Design/Functional Performance:
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				3.2.5
</td>
<td bgcolor="#d9d9d9">
To
				be revised:

 


3.2.5
				If an ACSD is equipped with a means of attaching to a rigid bar
				anchorage system, as prescribed by 49 CFR 571.225 S9, then the
				provided attachment hardware must comply with the requirements of
				49 CFR 571.213 S5.9(a). If rigid prongs are provided for that
				attachment, they shall be retractable to the extent necessary to
				ensure proper positioning of the ACSD in an airplane passenger
				seat not equipped with rigid bar lower anchorages to avoid damage
				to the airplane seat or injury to nearby seat occupants.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				3.2.6
</td>
<td bgcolor="#d9d9d9">
New
				paragraph 3.2.6 to be added:

 


Except
				for components designed to attach to a child restraint anchorage
				system, an ACSD must not have any means designed for attaching
				the system to an aircraft seat cushion or aircraft seat back and
				any component (except belts) that is designed to be inserted
				between the aircraft seat cushion and the aircraft seat back. An
				ACSD shall be capable of meeting the requirements of this
				standard when installed solely by the passenger seat lap belt
				(pelvic portion of the restraint). If the ACSD is equipped with a
				child restraint anchorage system, then it shall also be capable
				of meeting the requirements of this standard when installed
				solely by attachment to rigid bar lower anchorages as prescribed
				by 49 CFR 571.225 S9. No passenger seat belt may contact the
				child-occupant of the ACSD. Each belt that is part of an ACSD and
				that is designed to restrain the child using the system, shall,
				when tested in accordance with Section 4 of this standard, impose
				no loads on the child as a result from the mass of the system or
				from the mass of the standard seat assembly specified therein.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				3.2.7
</td>
<td bgcolor="#d9d9d9">
New
				paragraph 3.2.7 to be added:

 


3.2.7
				An ACSD shall comply with the force distribution requirements of 


49
				CFR 571.213 S5.2.1.1, S5.2.1.2, S5.2.2.1 (a), (b) and (c),
				S5.2.2.2, and S5.2.4.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				3.2.8
</td>
<td bgcolor="#d9d9d9">
New
				paragraph 3.2.8 to be added:

 


3.2.8
				ACSD belt systems shall comply with the requirements of 


49
				CFR 571.213 S5.4.1.2, S5.4.1.3, S5.4.2, S5.4.3.1, S5.4.3.3,
				S5.4.3.5.

References
				to paragraph S6.1 therein shall be considered to refer to Section
				4 of this standard.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				3.3
</td>
<td bgcolor="#d9d9d9">
To
				be revised:

 


3.3
				Fire Protection: Cushions, upholstery, and all other exposed
				materials used in the ACSD except small parts (knobs, triggers,
				fasteners, seals and electrical parts) that would not contribute
				significantly to the propagation of a fire shall meet the fire
				protection provisions of CS 25.853(a) (Appendix F, Part I
				(a)(1)(ii)). Seat belts and shoulder harnesses shall meet the
				provisions of CS 25 (Appendix F, Part I (a)(iv)).
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				4
</td>
<td bgcolor="#d9d9d9">
To
				be revised:

 


4.
				PERFORMANCE TEST SPECIFICATIONS: The dynamic test described in
				this section is used to evaluate the performance of the ACSD in a
				horizontal impact where the force is applied against the
				longitudinal axis of a forward-facing airplane passenger seat
				that holds the ACSD. The structural adequacy of the ACSD, the
				effectiveness of the ACSD attachments, and the adequacy of
				restraint of the child occupant, as prescribed in paragraph 4.1
				of this AS, are the issues evaluated. One dynamic impact test
				shall be performed, with the ACSD secured using the passenger
				seat lap belt, for each category of child-occupant, as defined in
				paragraph 2.3 of this AS, for which the ACSD is intended for use.
				ACSD equipped with lower anchorage attachment hardware per 49 CFR
				571.213 S5.9(a) must be tested with each category of child
				occupant when secured using the rigid bar lower anchorages,
				except when the ACSD is in full compliance with 49 CFR 571.213.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				4.1
</td>
<td bgcolor="#d9d9d9">
To
				be revised:

 


4.1
				Child-Occupant Simulation: One or more ATD representing the child
				categories for which the ACSD is intended for use shall be used
				to simulate a child-occupant in the dynamic test. Selection of
				the ATD shall be based on compliance with the following
				requirements:

 


a.
				A newborn infant ATD, per 49 CFR part 572, Subpart K, shall be
				used to test a Type I ACSD.

 


b.
				A newborn infant ATD and a 12-month-old child ATD, per 49 CFR
				part 572, Subpart R, shall be used to test a Type II ACSD.

 


c.
				A 12-month-old child ATD and a 3-year-old child ATD, per 49 CFR
				part 572, Subpart P, shall be used to test a Type III ACSD.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				4.1.2
</td>
<td bgcolor="#d9d9d9">
To
				be revised:

 


4.1.2
				ATD Preparation and Clothing: All three types of ATDs used shall
				have a target point marker on each side of the head that is
				located on the transverse axis passing through the centre of mass
				of the ATD’s head and perpendicular to the head’s midsgittal
				plane. The 12-month-old and 3-year-old ATD’s must also have
				target points located on each knee pivot axis. ATDs must be
				clothed and prepared for use, as prescribed in 49 CFR 571.213 S9.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				4.2
</td>
<td bgcolor="#d9d9d9">
To
				be revised:

 


4.2
				Test Fixtures: The fixture on which the ACSD is installed for the
				dynamic test is based on the FMVSS-213 standard seat assembly
				test fixture defined in 49 CFR 571.213 S6.1.1(a)(1)(i). For the
				test specified by this AS, the back cushion, seat cushion, lap
				belts, and belt anchor points are different from the FMVSS-213
				standard seat test fixture configuration. Appendix A to this AS
				presents the locations, dimensions, and materials used to
				reconfigure the FMVSS-213 standard seat assembly test fixture for
				the test specified by this AS.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				4.2.1
</td>
<td bgcolor="#d9d9d9">
To
				be revised:

 


4.2.1
				Passenger Seat Restraints: Airplane passenger seat lap belts
				shall be installed on the seat test fixture as the primary means
				of attaching the ACSD to the seat test fixture depicted in
				Appendix A to this AS. The buckle shall be a lift latch type
				release mechanism. The belts shall meet the requirements of
				ETSO-C22g and conform to the length dimensions shown in Appendix
				A, Figure A5, to this AS. The webbing shall be made of nylon.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				4.2.2
</td>
<td bgcolor="#d9d9d9">
New
				paragraph 4.2.2 to be added:

 


4.2.2
				Rigid Bar Lower Anchorages: If testing ACSD equipped with lower
				anchorage attachment hardware, the aforementioned modified seat
				test fixture must have rigid bar lower anchorages installed per
				Figures 1A and 1B of 49 CFR 571.213.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				4.5
</td>
<td bgcolor="#d9d9d9">
The
				last sentence of paragraph 4.5 Photometric Instrumentation shall
				be revised:

 


The
				resolution of the images shall be sufficient to enable accurate
				measurements of the maximum excursion of the head and knee of the
				ATD in Type III ACSD tests, or the maximum rotation of the ACSD
				in aft-facing Type I and Type II ACSD tests.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				4.6
</td>
<td bgcolor="#d9d9d9">
To
				be revised:

 


4.6
				Test Severity: The dynamic impact pulse shall meet the
				requirements specified for Type A seats in AS8049B, i.e. the 16
				g, 13.4 m/s (44 ft/s) horizontal test condition for transport
				category airplane seats. The pulse described in Figure 2A of 49
				CFR 571.213 is acceptable to show compliance with this
				requirement. The yaw and floor deformation specified in AS8049B
				are not required.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				4.7
</td>
<td bgcolor="#d9d9d9">
New
				paragraph 4.7 to be added:

 


4.7
				Test Conditions: During the test, maintain the environmental
				conditions specified in 49 CFR 571.213 S6.1.1(d).
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				5.1
</td>
<td bgcolor="#d9d9d9">
To
				be revised:

 


5.1
				ACSD Installation: Install the ACSD at the centre of the seating
				position of the modified FMVSS-213 standard seat assembly test
				fixture in accordance with the manufacturers instructions
				provided with the system except that no tether strap shall be
				used. For the belted test condition, use only the aircraft lap
				belt. For tests with a child restraint anchor system, use only
				the lower anchorages of the child restraint anchor system.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				5.2
</td>
<td bgcolor="#d9d9d9">
New
				paragraph 5.2 to be added:

 


5.2
				ATD Installation: The ATD shall be placed in the ACSD. Position
				it, and attach the child restraint belts, if appropriate, per 49
				CFR 571.213 S10.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				5.3
</td>
<td bgcolor="#d9d9d9">
To
				be revised:

 


5.3
				ACSD Integral Restraint Adjustment: The ACSD integral restraint
				system shall be routed through the ACSD and fastened over the ATD
				as called for by the manufacturer’s instructions and per 49 CFR
				571.213 S6.1.2(d)(1)(i).
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				5.4
</td>
<td bgcolor="#d9d9d9">
To
				be revised:

 


5.4
				ACSD Attachment Adjustment: The aircraft lap belt or child
				restraint anchor system straps attaching the ACSD to the standard
				seat assembly test fixture shall be adjusted per 49 CFR 571.213
				S6.1.2(d)(1)(ii) or (iii) as appropriate.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				6.1
</td>
<td bgcolor="#d9d9d9">
To
				be revised:

 


6.1
				Excursion Limits: The ATD and ACSD excursions and initial
				positions described below shall be obtained by measuring the
				high-speed film or video images recorded during the test, or in
				the case of initial position, measured directly prior to the
				test.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				6.1.1
</td>
<td bgcolor="#d9d9d9">
To
				be revised:

 


6.1.1
				Test of Forward-Facing ACSD: The ACSD shall retain the ATD’s
				torso within the system. No portion of the ATD head shall pass
				through a vertical transverse plane passing through a point 813
				mm (32 in.) forward of the seat back pivot axis on the standard
				seat assembly test fixture shown in Appendix A, Figure A2. This
				limit is referred to as the head excursion limit.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				6.1.2
</td>
<td bgcolor="#d9d9d9">
The
				second paragraph shall be revised:

 


6.1.2
				Test of Aft-Facing ACSD: The angle between the ACSD back child
				support surface and the vertical transverse plane shall not
				exceed 70 degrees at any time during the test. The initial
				(pre-test) angle between the ACSD back child support surface and
				the vertical transverse plane shall not be less than 45 degrees.

 


All
				portions of the ATD torso shall be retained within the ACSD. The
				centre of the target points on either side of the ATD head shall
				not pass through the transverse orthogonal planes whose
				intersection contains the forward-most and top-most points on the
				ACSD surfaces.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				6.2
</td>
<td bgcolor="#d9d9d9">
To
				be revised:

 


The
				Head Injury Criterion (HIC36) is calculated according to the
				following equation:

<img align="absmiddle" name="Object6" src="image028.png"/>


Where:

t1,
				t2 = Any two points in time during the head impact which are not
				separated by more than a 36 millisecond time interval

a(t)
				= The resultant head acceleration at the centre of gravity of the
				ATD head expressed as a multiple of g (the acceleration of
				gravity).

 


The
				maximum value of the HIC36 computation from data acquired during
				the impact test, including rebound motion of the ATD and ACSD,
				shall not exceed a value of 1 000.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				6.4
</td>
<td bgcolor="#d9d9d9">
A
				new second paragraph shall be added:

 


The
				ACSD shall also meet the requirements of 49 CFR 571.213 S5.1.1.
				References to paragraph S6.1 therein shall be considered to refer
				to Section 4 of this standard.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraphs
				7.1a

through
				7.1e
</td>
<td bgcolor="#d9d9d9">
Paragraphs
				7.1a. through e. shall be disregarded.

 


Marking
				of the article shall be in accordance with paragraphs 7.1f.
				through 7.1h., and paragraph 4 of this ETSO.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				7.1g
</td>
<td bgcolor="#d9d9d9">
The
				second paragraph shall be revised:

 


				‘Place
				this Type I, II and III child restraint in a rear-facing position
				when using it with an infant weighing less than ____ pounds
				(______Kg).’
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraphs
				7.1h

through
				7.1m
</td>
<td bgcolor="#d9d9d9">
To
				be disregarded.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				7.1h
</td>
<td bgcolor="#d9d9d9">
New
				paragraph 7.1h to be added:

 


7.1h
				The following statement on yellow background with black text,
				regarding the installation and use of ACSD:

 


				‘WARNING!
				DEATH OR SERIOUS INJURY CAN OCCUR. Follow all instructions on
				this aviation child restraint and in the manufacturer’s written
				instructions located [insert location].

 


				—Do
				not place this device behind any wall or seat back in an airplane
				that has an airbag.

				—Do
				not use in any passenger seat that has an inflatable seat belt.

				—Use
				only in a forward-facing seat. Do not use in a rear-facing seat
				or a side-facing seat.

				—Attach
				this aviation child restraint with the airplane passenger seat
				lap belt or rigid bar anchorage system if so equipped.

				—This
				aviation child restraint is not designed to be used with a
				shoulder strap or any other tether strap to the seat or airplane.

				—Snugly
				adjust the belts provided with this aviation child restraint
				around your child.’
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Paragraph
				7.1i
</td>
<td bgcolor="#d9d9d9">
New
				paragraph 7.1i to be added:

 


7.1i
				Additional label for ACSD that do not meet FMVSS-213. Any ACSD
				that meets the MPS of this TSO, but does not met the requirements
				of FMVSS-213, the label in new Figure A6 must be permanently
				affixed to the webbing of the ACSD so that it is clearly visible
				when the ACSD is installed.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Figure
				A1
</td>
<td bgcolor="#d9d9d9">
Figure
				A1 shall be revised as follows:

 


The
				horizontal distance between the seat back pivot axis to the lap
				belt anchor axis shall be changed from 269 (10.6) to 246 (9.7).
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Figure
				A2
</td>
<td bgcolor="#d9d9d9">
Figure
				A2 shall be revised as follows:

 


The
				horizontal distance between the seat back pivot axis to the lap
				belt anchor axis shall be changed from 269 (10.6) to 246 (9.7).

 


A
				new item 9 shall be added: 


Aluminium
				rod: 25.4 (1.0) Dia. welded to the front edge of item 1 such that
				the rod surface is tangent to the plane of the bottom of the
				aluminium plate.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Figure
				A3
</td>
<td bgcolor="#d9d9d9">
Figure
				A3 shall be revised as follows:

 


The
				vertical dimension of the anchor pivot shall be changed from 47.8
				(1.88) to 50.8 (2.0), and the vertical dimension of the anchor
				height from 60.5 (2.38) to 63.5 (2.5).
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Figure
				A4
</td>
<td bgcolor="#d9d9d9">
Figure
				A4 shall be revised as follows:

 


A
				depiction of the 25.4 (1.0) Dia. rod defined in Figure A2 shall
				be added.
</td>
</tr>
<tr valign="top">
<td bgcolor="#d9d9d9">
Figure
				A6
</td>
<td bgcolor="#d9d9d9">
Figure
				A6 shall be replaced as follows:

 


FIGURE
				A6 — Label for ACSD Not Meeting FMVSS-213

 


<img align="bottom" border="0" name="etso-11image4.emf" src="image029.png"/>


 


				— Box
				outline of label is red, 6-point line width.

				— Box
				is 4.75 inches long by 1.25 inches high.

				— Interior
				of box is yellow background.

				— Text
				is Arial bold black letters.

				— Large
				text is 18 point.

				— Smaller
				text is 16 point.
</td>
</tr>
</tbody>
</table>

[Amdt ETSO/11]