IS 5416 Part 11988AI Search Enabled✦ AI Generated

Adjustable metal chairs for the use of typists and operators in telephone exchanges-Specification

IS 5416 Part 1 (1988) specifies the methods of testing strength and stability for adjustable metal chairs used by typists and telephone exchange operators. It defines detailed procedures for static load, fatigue, impact, and wear tests to ensure these chairs meet safety, durability, and functional performance requirements. This standard is essential for manufacturers, quality controllers, and engineers involved in designing or evaluating office seating for telecommunication environments.

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What This Standard Covers

IS 5416 Part 1 (1988) specifies the methods of testing strength and stability for adjustable metal chairs used by typists and telephone exchange operators. It defines detailed procedures for static load, fatigue, impact, and wear tests to ensure these chairs meet safety, durability, and functional performance requirements. This standard is essential for manufacturers, quality controllers, and engineers involved in designing or evaluating office seating for telecommunication environments.

Who Uses This Standard

  • Furniture Manufacturers
  • Quality Assurance Engineers
  • Product Designers
  • Office Facility Managers
  • Telecommunication Equipment Suppliers
  • Safety Inspectors
  • Ergonomics Specialists

Key Topics Covered

Static load testing for seat, back, arms, and legs
Fatigue testing for seat and back durability
Impact tests on seat, back, arms, and wings
Wear testing for swiveling mechanisms and seat height adjustments
Diagonal base stability tests
Test load levels and force application methods
Loading pad specifications and positioning
Inspection procedures before and after testing
Defect criteria affecting strength and function
Test sequencing and sampling plans
Environmental conditioning for testing
Test reporting requirements

Table of Contents

1Scope

IS 5416 Part 1 - Scope & Key Specifications Summary

Scope:

  • Applies to strength testing of chairs and stools.
  • Includes timber products moisture content control:
    • Moisture content must be 12-15% (checked by electric moisture meter).
    • If higher, dry in warm ventilated room until within limits.
  • Conditioning/testing atmosphere:
    • Temperature: 27 ± 3°C
    • Relative Humidity: 50 ± 5%

Sampling & Permissible Defects (Clause 4.3 - Table 4)

Lot Size (No. of Samples)Sample SizePermissible Defective Chairs/Stools
Up to 5030
51 to 15050
151 to 30080
301 to 500130
501 to 1,000201
1,001 to 3,000322
Above 3,000503

Test Types & Purposes (Clause 3.2 - Table 1)

Test No.Test TitlePrimary PurposeSecondary Purpose
1a, 1bSeat & Back Static Load TestBasic StrengthDamage Initiation
2Arm & Wing Sideways Static Load--
3Arm Downwards Static Load--
4a, 4bSeat & Back Fatigue TestService DurabilityDamage Propagation
5a, 5bLeg Forwards/Sideways & Static LoadHandling StrengthResidual Strength
6Seat Impact TestImpact Strength-
7a, 7bBack & Arm Impact Test--
8Drop Test--
2Definitions

IS 5416 Part 1 - Definitions & Key Specifications Summary

1. Definitions

  • Refer to IS 4415-1967 for all definitions related to furniture testing (Clause 2.1).

2. Test Purposes (Clause 3.2, Table 1)

  • Tests include static load, fatigue, impact, wear, and drop tests.
  • Primary purposes: strength, durability, impact resistance, handling strength, service wear.
  • Secondary purposes: damage initiation, propagation, residual strength, acceptable misuse.

3. Test Loads & Levels (Clause 3.2, Table 2)

  • Test levels 1 to 5 indicate increasing severity.
  • Example loads at Level 3:
    • Seat static load: 1600 N
    • Back static load: 760 N per pad
    • Arm sideways load: 600 N
    • Seat fatigue cycles: 50,000
    • Seat impact drop height: 240 mm
  • Drop test heights vary by chair type and leg length (75-900 mm).

4. Application of Test Levels (Clause 3.2, Table 3)

  • Domestic chairs typically tested at Levels 1-3.
  • Institutional and hospital furniture require Levels 4-5.
  • Folding garden/camping chairs at Levels 2-3.

Example: Seat Static Load Test Levels (N)

Level12345
Load1100130016002000

flowchart TD
    A[Definitions] --> B[IS 4415-1967]
    B --> C[Test Purposes]
    C --> D[Static Load]
    C --> E[Fatigue]
    C --> F[Impact]
    C --> G[Wear]
    C --> H[Drop Test]
    D --> I[Test Loads & Levels]
    I --> J[Level 1 to 5]
    J --> K[Application by Furniture Type]

For detailed load values and test cycles, refer to IS 5416 Part 1 Table 2 & Appendix A.

3Principle and Purpose of Tests

IS 5416 Part 1: Principle and Purpose of Tests

Key Points from Clause 3.2 & 3.2.1, 3.2.3

  • Purpose: Evaluate static strength, fatigue durability, impact resistance, and residual strength under occasional high loads.
  • Test Types:
    • Static Tests: Assess strength under high, slow-applied loads (Clause 3.2.1).
    • Fatigue Tests: Evaluate durability under repeated loading.
    • Impact Tests: Assess strength under rapid, sudden loads (Clause 3.2.3).

Table 1: Test Sequence & Purpose (Summary)

SeqTest TitlePrimary PurposeSecondary PurposeType
1Seat & Back Static LoadBasic strengthDamage initiationFunctional
4Seat & Back Fatigue TestService durabilityDamage propagation
5Leg Forwards & SidewaysHandling strengthResidual strengthAcceptable misuse
6Seat Impact TestImpact strength
9Chair Swivelling Wear TestService wearNoneFunctional

Severity Grading (Table 3 Reference)

  • Load magnitude and number of load cycles are varied to grade test severity.

Summary Formula (Static Load Test Concept)

[ \sigma = \frac{P}{A} ]

Where:

  • (\sigma) = Stress in the component
  • (P) = Applied static load (from test specification)
  • (A) = Cross-sectional area resisting load

flowchart LR
    A[Static Tests] --> B[Basic Strength & Damage Initiation]
    A --> C[Fatigue Tests]
    C --> D[Service Durability & Damage Propagation]
    A --> E[Impact Tests]
    E --> F[Impact Strength]
    A --> G[Handling & Residual Strength Tests]

Use Table 2 (IS 5416 Part 1) for exact test loads and Table 3 for load application cycles.

4General Requirements for Testing

IS 5416 Part 1: General Requirements for Testing

Sampling & Inspection (Clause 4.3)

Lot Size (No. of Samples)Sample SizePermissible Defectives
Up to 5030
51 – 15050
151 – 30080
301 – 500130
501 – 1000201
1001 – 3000322
3001 and above503
  • Samples must be randomly drawn from the lot.
  • Timber parts: moisture content 12–15% checked via electric moisture meter.
  • Conditioning atmosphere: 27 ± 3°C, 50 ± 5% RH.

Test Sequences & Purposes (Clause 3.2, Table 1)

Seq.Test NamePrimary PurposeSecondary PurposeType
1a,1bSeat & Back Static Load TestBasic strengthDamage initiationFunctional
2Arm & Wing Sideways Static Load
3Arm Downwards Static Load
4a,4bSeat & Back Fatigue TestService durabilityDamage propagation
5a,5bLeg Forwards/Sideways & StaticHandling strengthResidual strengthMisuse
6Seat Impact TestImpact strength
7a,7bBack & Arm Impact Test
8Drop Test
9Chair Swiveling Wear TestService wearNoneFunctional
10Seat Height Adjustment Wear Test

Summary

  • Follow Table 4 for sampling size & acceptance.
5Requirements for Tests

IS 5416 Part 1: Requirements for Tests

1. Test Sequence & Purpose (Table 1)

SequenceTest NumberTitlePrimary PurposeSecondary PurposeType
11a, 1bSeat & Back static load testBasic strengthDamage initiationFunctional
22Arm & wing sideways static load
33Arm downwards static load
44a, 4bSeat & Back fatigue testService durabilityDamage propagation
55a, 5b, 50Leg tests & diagonal base testHandling strengthResidual strengthAcceptable misuse
66Seat impact testImpact strength
77a, 7bBack & Arm impact test
88Drop test
99Chair swivelling wear testService wearNoneFunctional
1010Seat height adjustment wear test

2. Sampling & Acceptance Criteria (Table 4)

Lot Size (No. of samples)Sample SizePermissible Defectives
Up to 5030
51 - 15050
151 - 30080
301 - 500130
501 - 1000201
1001 - 3000322
Above 3000503

3. Conditioning & Moisture Content

  • Moisture content for timber parts: 12% to
6Inspection and Conditioning of Articles

IS 5416 Part 1: Inspection and Conditioning of Articles

Key Specifications & Formulas:

  • Conditioning Time (Clause 5.2):

    • Articles (e.g., glued joints in timber/plastics) must be aged ≥ 4 weeks under normal conditions before testing to ensure full strength.
  • Moisture Content for Timber Parts:

    • Use an electric moisture meter.
    • Moisture content must be 12% to 15%.
    • If above 15%, dry in a warm, ventilated room until within range.
  • Standard Conditioning Atmosphere:

    • Temperature: 27 ± 3°C
    • Relative Humidity: 50 ± 5%
  • Sampling & Permissible Defectives (Clause 4.3, Table 4):

Lot Size (No. of Samples)Sample SizePermissible Defective Articles
Up to 5030
51 to 15050
151 to 30080
301 to 500130
501 to 1,000201
1,001 to 3,000322
Above 3,000503
  • Post-Test Inspection (Clause 6.2):
    • Thoroughly inspect articles.
    • Note any defects or changes since initial inspection.
    • Record flexibility quotient and any non-functional damage.

flowchart TD
    A[Manufacture] --> B[Conditioning ≥ 4 weeks]
    B --> C[Moisture Check (12-15%)]
    C --> D{Moisture OK?}
    D -- Yes --> E[Standard Atmosphere Conditioning]
    D -- No --> F[Dry in Warm Ventilated Room]
    F --> C
    E --> G[Testing]
    G --> H[Post-Test Inspection]
    H --> I[Record Defects & Changes]

This ensures reliable, repeatable test results per IS 5416 Part 1.

7Test Apparatus and Loading Pads

IS 5416 Part 1 (1988) — Test Apparatus & Loading Pads

Key Specifications:

  • Back Loading Pad (Clause 7.8)

    • Rigid rectangular block
    • Dimensions: 200 mm height × 250 mm width
    • Face: Convex cylindrical curvature radius 450 mm
    • Front edges: Rounded with 12 mm radius
  • Local Loading Pad (Clause 7.10)

    • Rigid cylindrical object
    • Diameter: 100 mm
    • Flat face with 12 mm radius on front edge
  • Seat Loading Pad (Clause 7.6)

    • Naturalistically shaped rigid indentor (complex shape)
    • Defined by existing moulds, not by drawing

Loading Details (Clause 9.1.1):

  • Seat Static Load Test:
    • Mount seat loading pad on seat plane at:
      • Seat loading point (Clause 8)
      • 100 mm back from front edge
    • Apply downward force ( V_s ) (from Table 2) 10 times

Summary Table (Dimensions):

Pad TypeShapeDimensions (mm)Edge Radius (mm)Notes
Back Loading PadRectangular200 (H) × 250 (W)12Convex cylindrical face, radius 450 mm
Local Loading PadCylindrical100 diameter12Flat face
Seat Loading PadComplex shape--Defined by moulds

flowchart LR
    A[Test Apparatus] --> B[Back Loading Pad]
    B -->|Dimensions| B1[200mm x 250mm]
    B -->|Curvature| B2[450mm radius convex]
    B -->|Edges| B3[12mm radius]

    A --> C[Local Loading Pad]
    C -->|Diameter| C1[100mm]
    C -->|Edge Radius| C2[12mm]

    A --> D[Seat Loading Pad]
    D -->|Shape| D1[Complex moulded shape]

This setup ensures standardized load application for furniture strength testing per IS 5416

8Determination of Seat and Back Loading Points

IS 5416 Part 1 (1988) – Determination of Seat and Back Loading Points

Key Specifications & Setup:

  • Back Loading Pad (Clause 7.8):

    • Rigid rectangular pad
    • Height = 200 mm, Width = 250 mm
    • Convex cylindrical curvature radius = 450 mm (across width)
    • Front edges rounded with radius = 12 mm
  • Loading Point Template (Clause 7.3):

    • Two shaped members joined by a pivot
    • Positioned at 90° angle (see Fig. 1)
    • Seat loading arm mass = 20 kg applied at seat loading point
    • Template contours designed to sink into upholstery for realistic load distribution

Procedure (Clause 8.1):

  • Place template on chair with load at seat loading point on chair centerline, as far rearward as possible.
  • Push back loading portion into chair back to lever seat portion forward.
  • Adjust until template shape matches chair contours.
  • Mark seat and back loading points from template.

Load Application:

  • Seat load (A) and back load (B) applied at marked points.
  • For stools, seat load (C) applied similarly.

Summary Table of Dimensions:

ParameterDimension (mm)
Back loading pad height200
Back loading pad width250
Curvature radius450
Edge radius12
Seat loading arm mass20 kg
Template angle90°

flowchart LR
  A[Place template on chair seat] --> B[Apply 20 kg load at seat loading point]
  B --> C[Push back loading pad into chair back]
  C --> D[Adjust until template fits chair contours]
  D --> E[Mark seat and back loading points]
  E --> F[Apply static load tests as per Clause 9.1]

This method ensures accurate positioning of load points for static load testing of chairs and stools per IS 5416 Part 1.

9Test Methods

IS 5416 Part 1: Key Test Methods & Specifications

1. Test Types & Purposes (Clause 3.2, Table 1)

Test No.TitlePrimary PurposeSecondary PurposeType
1a,1bSeat & Back Static Load TestBasic strengthDamage initiationFunctional
2Arm & Wing Sideways StaticStrength assessment--
3Arm Downwards StaticStrength assessment--
4a,4bSeat & Back Fatigue TestService durabilityDamage propagation-
5a,5b,50Leg Forward/Sideways & Diagonal BaseHandling strengthResidual strengthAcceptable misuse
6Seat Impact TestImpact strength--
7a,7bBack & Arm Impact Test---
8Drop Test---
9Chair Swivelling Wear TestService wearNoneFunctional
10Seat Height Adjustment Wear Test---

2. Sampling & Acceptance Criteria (Clause 4.3, Table 4)

Lot Size (No. of Samples)Sample SizePermissible Defectives
Up to 5030
51 to 15050
151 to 30080
301 to 500130
501 to 1000201
1001 to 3000322
Above 3000503

3. Conditioning Requirements

  • Moisture content for timber parts: 12–15% (checked with electric moisture meter)
  • Standard atmosphere for testing:
10Test Levels and Load Specifications

IS 5416 Part 1: Test Levels & Load Specifications Summary

1. Test Purpose & Sequence (Table 1)

SeqTestPrimary PurposeSecondary PurposeType
1a,1bSeat & Back Static LoadBasic strengthDamage initiationFunctional
2,3Arm/Wing Sideways & Arm Downwards Static LoadStrength--
4a,4bSeat & Back Fatigue TestService durabilityDamage propagation-
5a,5b,50Leg Forward/Sideways & Diagonal Base TestHandling strengthResidual strengthAcceptable misuse
6,7a,7bSeat, Back & Arm Impact TestImpact strength--
8Drop Test---
9,10Swivelling & Height Adjustment WearService wear-Functional

2. Test Loads (Table 2)

Test NoDescriptionTest Level 1 (Min)Level 5 (Max)Unit
1aSeat static load11002000N
1bBack static load410 (pad)760 (pad)N
2Arm sideways load300900N
3Arm downwards load7001000N
4aSeat fatigue cycles12,500200,000cycles
4bBack fatigue cycles12,500200,000cycles
5aLeg forward force300760N
5bLeg sideways force250760N
6Seat impact drop height140300mm
7aBack impact drop height120620mm
8Drop test height (stacking chairs)150900mm

Note: Some tests not applicable at all levels.


3. Application of Test Levels (Table 3)

| Furniture Use | Test Level Recommended

11Test Report

IS 5416 Part 1 - Test Report: Key Specifications & Tables


1. Test Report Must Include (Clause 11.1):

  • Article details tested
  • Test level applied
  • Defects before and after testing
  • Additional requirements (Clause 9.1.2):
    • Flexibility quotient ≤ 0.0008 × Hg (Hg = seat height)
    • Back deflection ≤ 100 mm (for all-foam chairs)
    • Back force ≥ 410 N applied
    • Compliance with product specs

2. Purpose & Sequence of Tests (Clause 3.2, Table 1):

SeqTest No.TitlePrimary PurposeSecondary Purpose
11a, 1bSeat & Back Static Load TestBasic StrengthDamage Initiation
22Arm & Wing Sideways Load
33Arm Downwards Static Load
44a, 4bSeat & Back Fatigue TestService DurabilityDamage Propagation
55a, 5b, 50Leg & Diagonal Base TestsHandling StrengthResidual Strength
66Seat Impact TestImpact Strength
77a, 7bBack & Arm Impact Tests
88Drop Test
99Chair Swiveling Wear TestService WearNone
1010Seat Height Adjustment Wear

3. Loading Severity (Clause 3.2):

  • Load magnitude and number of cycles vary to grade severity.
  • Tests assess:
    • Static strength & initial damage
    • Fatigue strength & damage propagation
    • Residual strength after misuse

4. Flexibility Quotient Formula (Clause 9.1.2):

[ \text{Flexibility Quot

Popular Questions About IS 5416 Part 1

?What types of static load tests are specified for adjustable metal chairs?

According to IS 5416 Part 1 (1988), the specified static load tests for adjustable metal chairs include:

Key Static Load Tests:

  • Back Static Load Test (Fig. 10): Apply a vertical force to the backrest with flexibility assessment. Use a balancing load if the chair tends to overturn.
  • Arm Downwards Static Load Test (Clause 9.3, Fig. 12): Apply a vertical force (Va) at the arm location most likely to fail, repeated 10 times.
  • Arm and Wing Sideways Static Load Test (Fig. 11): Apply lateral force to arms/wing parts.
  • Seat Fatigue Test (Fig. 13): Repeated force of 950 N applied to the seat.
  • Leg Tests (Clause 9.5.1): For chairs/stools with legs or pedestals, excluding swivel chairs. No rearward leg loading test required.

Force Magnitudes:

  • Typical forces: 330 N for castors, 950 N repeated seat load.
  • Balancing force applied to prevent overturning as needed.

These tests ensure strength, stability, and durability under expected static loads.

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?How does the standard define fatigue testing for seat and back components?

IS 5416 Part 1 — Fatigue Testing of Seat and Back Components

The standard defines fatigue testing as follows:

  • Combined Test: Seat and back fatigue tests (Clauses 9.4.1 & 9.4.2) are usually performed together due to common load and cycle requirements.

  • Load Application:

    • Apply a force of 950 N on the seat using a seat loading pad (Clause 7.6).
    • Apply a force of 330 N on the back using a back loading pad, or lesser if needed to prevent overturning (Clause 7.8).
  • Cycle Count: Number of cycles is specified in Table 2 (not shown here).

  • Load Position:

    • Seat load applied at the seat loading point (Clause 8, Fig. 13).
    • Back load applied at a distance 'A' as per Clause 8 (Fig. 14).
  • Special Cases: For stools or chairs with asymmetrical seats, forces are applied in multiple directions as per the standard.


Summary Table of Loads

ComponentLoad (N)Load Application PointNotes
Seat950Seat loading pointUse seat loading pad
Back330Distance 'A'Use back loading pad, adjust if overturn risk

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This ensures durability under repeated loading simulating real use.

?What are the impact test procedures for chair arms and backrests?

Impact Test Procedures for Chair Arms and Backrests (IS 5416 Part 1)

  • Back Impact Test (Clause 9.7.1):

    • Place chair with front feet blocked to prevent forward movement.
    • Strike the center of the top outside of the backrest horizontally with an impact hammer (see Fig. 18).
    • Drop hammer from height/angle per Table 2.
    • Repeat 10 times.
    • For stools without backs, impact the front seat edge or direction likely to cause overturn.
    • For swivel bases, impact direction must pass through swivel vertical axis.
    • For chairs with wings, repeat impact on wing top outside at right angles.
  • Arm Impact Test (Clause 9.7.2):

    • Similar to back impact test but impact is applied inward on the outside face of one arm.
    • Place stops against feet opposite to the arm tested (see Fig. 19).
    • For swivel bases, impact direction passes through swivel vertical axis.

Summary:

  • Impact hammer used horizontally.
  • 10 repetitions per test.
  • Positioning and direction critical to simulate realistic failure modes.
  • Swivel chairs require impact through swivel axis.
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This ensures durability against realistic forces on arms and backrests.

?How is the seat height adjustment mechanism tested for wear?

IS 5416 Part 1 - Seat Height Adjustment Wear Test (Clause 9.10)

The seat height adjustment mechanism is tested as follows:

  • Set seat at maximum height.
  • Apply a vertical downward force of 950 N at the seat loading point using the seat loading pad.
  • Maintain force for at least 3 seconds.
  • Lower seat just above its lowest height.
  • Reapply the 950 N force for 3 seconds, then remove.
  • Return seat to maximum height.
  • Repeat this loading cycle for the number of cycles specified in Table 2.
  • After cycles, maintain the 950 N force for 1 hour at maximum height.

Purpose:
This test simulates the wear on semi-automatic seat height mechanisms under repeated loading/unloading, ensuring durability under user weight.


Summary Table (from IS 5416 Table 2 excerpt)

Test TypeForce (N)Duration per CycleNumber of Cycles
Seat Height Adjustment Wear9503 s per loadAs per Table 2
Final Load Holding9501 hour1

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This ensures the seat height mechanism can withstand repeated use without excessive wear or failure.

?What criteria determine if a chair passes or fails the strength and stability tests?

IS 5416 Part 1: Criteria for Chair Strength & Stability Tests

The chair passes or fails based on its ability to withstand specified static and fatigue loads without failure or excessive deformation.

Key Test Criteria:

  • Back Static Load Test (Clause 9.5.1 & Fig. 10):
    Apply a vertical load at the backrest; chair must not overturn or fail. If overturning tendency exists, apply a balancing load on the opposite side.

  • Arm Downwards Static Load Test (Clause 9.3 & Fig. 12):
    Apply vertical force (Va) at arm's critical point 10 times. Chair must resist without damage.

  • Leg Tests (Clause 9.5.1):
    Applicable only to chairs with legs/pedestals (excluding swivel chairs). No rearward leg load test needed if back static test is passed.

  • Castor Test (Clause 7.8):
    Repeated force of 330 N or lesser to prevent overturning, plus 950 N seat load cycles. No failure or instability allowed.

  • Seat Fatigue Test (Fig. 13):
    Horizontal backward force applied cyclically on seat edges; chair must maintain integrity.

Pass/Fail Summary:

  • No structural failure (cracks, breaks).
  • No permanent deformation beyond limits.
  • No overturning under balancing loads.
  • Stability maintained throughout cyclic loading.
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This ensures chairs meet minimum safety and durability per IS 5416 Part 1.

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