SPI_System_Specification_150518.pdf

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PMA260C13/4334

3 NOVEMBER 2014

Department of the Navy Program Executive Office PMA260

Naval Air Systems Command Patuxent River, Maryland 20670-1161

System Specification For The

Stationary Penetrant Inspection System

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APPROVED: ___________________________ APPROVED: ____________________________

TITLE: JENNIFER YOUNG, TITLE: MICHAEL O'MEALY,

APEO (E) AIR 1.0 APEO (L) AIR 1.0

APPROVED: ___________________________ APPROVED: ____________________________

TITLE: James R Mathers, TITLE: CAPT Jacobs, PMA260

APEO (T&E) AIR 1.0 PMA260 Program Manager

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SPI Performance Specification i

REVISION HISTORY

Date Version Remarks Author

3 Nov 2014 1.0 Initial Release LSE 18 May 2015 2.0 Clarification to acceleration testing LSE

SRB MEMBERS

Name Title Concurrence (Co-Chair) Robert McCaffery PMA260 ATS/CSE APME 4.1.1.4 (02 Oct 14) (Co-Chair) Eliezer Sanchez PMA260 APMT&E 5.1.1.4 (02 Oct 14) (Co-Chair) Mark Dobson PMA260 Product Support Manager (02 Oct 14)

Patrick Weaver SE T&E Branch Head 4.8.6.11 Email (22 Sep 14) Carolyn Pacella Avionics CSE APML Branch Head 6.6.4.9 (02 Oct 14)

(4.8.1 Delegated to) Janet French Platform SE Projects Branch Head 4.8.1.2 (02 Oct 14) (1.0 Delegated to) Janet DiPasquale PMA-260 Avionics CSE Branch Head (02 Oct 14)

(4.8.6 Delegated to) Gabrielle Korosec Common Avionics SE Branch Head 4.8.6.7 (02 Oct 14) Brian Gilp Reliability & Maintainability AIR 4.1.10.3 Email (08 Sep 14)

David Piatkowski Materials Engineering Supervisor 4.3.4 Email (18 Sep 14) James Gavalchin System Safety 4.1.6.1 Email (16 Sep 14)

Brent Gordon Producibility 4.1.9 Email (19 Sep 14)

IPT MEMBERS

Name Title Concurrence

John Thompson ADPM CNI/EW/SWL/NDI CGSE PMA260C13 Email (18 Sep 14) Marc Donohue NDI IPTL AIR 1.3.1.8.2 Email (09 Sep 14)

Tarun Patel NDI LSE AIR 4.8.1.2 (05 Sep 14) Nick Amabile NDI Principal Engineer 4.8.6.7 Email (09 Sep 14) Roger Ding NDI Principal Engineer 4.8.6.7 Email (09 Sep 14)

Alford Bunting NDI Logistics 6.7.4.4 Email (09 Sep 14) Douglas Waddell Test Technician 4.8.6.11 Email (18 Sep 14) ii

1.0 Scope

1.1 Identification

1.2 System Overview

1.3 Document Overview

2.0 Referenced Documents

3.0 Requirements

3.1 Required States and Modes

3.2 System Capability and Component Requirements

3.2.1 Penetrant Processing Capabilities

3.2.1.1 Penetrant Application

3.2.1.2 Penetrant Drain and Dwell

3.2.1.3 Pre-Rinse

3.2.1.4 Hydrophilic Remover Application

3.2.1.5 Hydrophilic Remover Rinse

3.2.1.6 Drying Oven

3.2.1.7 Developer Application (Form D)

3.2.1.8 Inspection

3.2.2 Black Light Assembly

3.2.3 Handheld Swivel Nozzle

3.2.4 Controls

3.2.5 Baskets

3.2.6 Integrated Timer

3.2.7 Process Control Accessories

3.3 System External Interface Requirements

3.3.1 Interface Identification and Diagrams

3.3.1.1 System Electrical Power Interface Requirements

3.3.1.2 Water Supply Interface Requirements

3.3.1.3 Drainage Interface Requirements

3.4 Safety Requirements

3.4.1 General Safety Requirements

3.4.2 Materials and Processes

3.4.2.1 Materials, Selection of

3.4.2.2 Hazardous Materials

3.4.2.3 Restricted Chemicals

3.4.2.4 Targeted Chemicals

3.4.2.4.1 Metal Alloys

3.4.2.4.2 Lead

3.4.2.5 Hexavalent Chromium

3.4.2.6 Protective Coatings

3.4.2.7 Lithium Batteries

3.5 System Environment Requirements

3.5.1 Air Transportation Acceleration

3.5.2 Vibration

3.6 System Quality Factors

3.6.1 Reliability and Maintainability Program

iii

3.7 Design and Construction Constraints

3.7.1 General Design

3.7.2 Overall System Dimensions

3.7.2.1 Inspection Station Exclusion

3.7.2.2 Tolerances

3.7.3 Weight

3.7.4 Material Construction

3.7.5 Modularity

3.7.6 Workmanship

3.7.7 Mounting

3.8 Personnel Related Requirements

3.8.1 Reach Limitations

3.8.2 Lifting Forward Reach

3.9 Logistics Related Requirements

3.9.1 Maintenance Provisions

3.9.2 Preventive/Scheduled Servicing and Inspections

3.10 Product Marking

3.10.1 Caution and Warning Labels

3.11 Packaging Requirements

3.12 Precedence and Criticality of Requirements

4.0 Verification Requirements

4.1 Performance Test

4.2 Special Tests and Examinations

4.2.1 Demonstration

4.2.2 Inspection

4.2.3 Analysis

4.2.4 Hydrophilic Remover Spray Concentration Test (If applicable)

4.2.5 Drying Oven Temperature Test

4.2.6 Temperature Indicator Test

4.2.7 Thermostat Test

4.2.8 Enclosure Recovery Test

4.2.9 Black Light Test

4.2.10 Excessive White Light Test

4.2.11 System Environment Requirements

4.2.11.1 Low Temperature Storage

4.2.11.2 High Temperature Storage

4.2.11.3 Low Temperature Operation

4.2.11.4 High Temperature Operation

4.2.11.5 Air Transportation Acceleration

4.2.11.6 Vibration

4.2.12 Reliability and Maintainability Program

4.2.13 Leakage Test

4.2.14 Weight Test

Appendix A: Acronyms & Abbreviations

1.0 Scope

1.1 Identification

This System Specification provides the requirements for the Stationary Penetrant Inspection

System, herein referred to as “SPI System”. The SPI System will be utilized at shore based U.S.

Navy and Marine Corps Nondestructive Inspection (NDI) facilities to locate surface defects on aircraft and Support Equipment (SE) parts.

1.2 System Overview

NDI technicians at the Intermediate level (I-level) maintenance shops are required to validate suspect structural parts of Navy or Marine Corps aircraft or SE when required. To accomplish these in-service tasks, NDI methods are employed. Penetrant Testing (PT) is one of five standard NDI disciplines used in this category of maintenance tasks. PT is used to detect surface-breaking discontinuities such as cracks, laps, cold shuts, corrosion, and porosity through capillary action. The trapped penetrant increases the visibility of the discontinuity by providing a visual contrast between the discontinuity and the surrounding surface. The SPI System specified in this document is intended to replace the legacy PT System and provide increased capabilities for NDI I-level technicians.

1.3 Document Overview

This System Specification provides the requirements for the Stationary Penetrant Inspection

System, herein referred to as “SPI System”. The SPI System will be utilized to inspect aircraft and SE parts.

2.0 Referenced Documents

In the event of a conflict between the text of this standard and the references cited herein, the text of this standard shall take precedence. Unless otherwise noted, the most recent revision at the time of contract award shall apply for each document.

MILITARY

A-A-50271 Plate, Identification

DFAR 223 Environment, Energy and Water Efficiency, Renewable Energy

Technologies, Occupational Safety, and Drug-Free Workplace

MIL-S-8512D Support Equipment, Aeronautical, Special General Specification for the Design of

MIL-STD-810G Department of Defense Test Method Standard, Environmental

Engineering Considerations and Laboratory Tests

MIL-STD-1472G DoD Design Criteria Standard, Human Engineering

MIL-STD-1791B Designing for Internal Aerial Delivery in Fixed Wing Aircraft

MIL-PRF-85285E Performance Specification: Coating: Polyurethane, Aircraft and

Support Equipment

NAVAIR 01-1A-16-1 Nondestructive Inspection Methods, Basic Theory

NAVAIR 01-1A-16-2 Nondestructive Inspection General Procedures and Process

Controls

MIL-PRF-20696F Performance Specification, Cloth, Waterproof, Weather Resistant

MIL-DTL-53022E Detail Specification: Primer, Epoxy Coating, Corrosion Inhibiting

Lead, and Chromate Free

PMA260C13/4332 Statement of Work for the SPI System (SOW)

S9310-AQ-SAF-010 Technical Manual for Batteries, Navy Lithium Safety Program

Responsibilities and Procedures

UNITED STATED CODE OF FEDERAL REGULATION

29 CFR Code of Federal Regulations Title 29: Labor

40 CFR Code of Federal Regulations Title 40: Protection of the

Environment

49 CFR Code of Federal Regulations Title 49: Transportation

OTHER PUBLICATIONS

NAS 411, NASC 7013 Hazardous Materials Management Program

SAE AMS2644F Inspection Material, Penetrant

ASTM D3951 Standard Practice for Commercial Packaging

ASTM D7478 Standard Specification for Heavy Duty Sheathed Wood Crates

ASTM E1 Standard Specification for ASTM Liquid-in-Glass Thermometers

ASTM E2297 Standard Guide for Use of UV-A and Visible Light Sources and

Meters used in the Liquid Penetrant and Magnetic Particle

Methods

NFPA 70 National Electrical Code

3.0 Requirements

3.1 Required States and Modes

The only required State and/or Mode is captured in the System Capabilities and Component

Requirements, paragraph 3.2.

3.2 System Capability and Component Requirements

The SPI System is a specialized piece of SE used to perform the Type I, Post-Emulsifiable

Hydrophilic (Method D) Penetrant Processing Operations defined in NAVAIR 01-1A-16-1.

Unless stated otherwise, “SPI System” refers to a complete system. At a minimum, the complete

SPI System shall be a series of modular work stations encompassing the following capabilities and components:

a. Penetrant Application

b. Penetrant Drain and Dwell

c. Pre-Rinse

d. Hydrophilic Remover Application

e. Hydrophilic Remover Rinse

f. Drying Oven

g. Developer Application (Form D)

h. Inspection

i. Black Lights

j. Hose(s) and Handheld Swivel Nozzle(s)

k. Controls

l. Baskets

m. Integral Timer

n. Process Control Accessories

Each capability is not required to have its own unique station. For example, the Pre-Rinse

(paragraph 3.2.1.3), Hydrophilic Remover Application (paragraph 3.2.1.4), and Hydrophilic

Remover Rinse (paragraph 3.2.1.5) can be done in the same station. In that case, all of the requirements of 3.2.1.5 shall be satisfied.

3.2.1 Penetrant Processing Capabilities

The SPI System shall provide the capability to perform Type I, Post-Emulsifiable Hydrophilic

(Method D) Penetrant Processing Operations as defined in NAVAIR 01-1A-16-1.

3.2.1.1 Penetrant Application

The penetrant application capability shall consist of a work station that contains, at a minimum, a frame, tank, and cover with a handle.

a. The tank shall be large enough to completely apply penetrant on parts up to dimensions of 40”L x 20”W x 20”H or greater.

3.2.1.2 Penetrant Drain and Dwell

The penetrant drain and dwell capability shall consist of a work station that allows the part under inspection to drain and dwell after the penetrant has been applied.

a. This work station shall be designed to ensure that the excess penetrant is completely directed back into the penetrant application station tank.

b. The work station surface shall be large enough to allow parts up to dimensions of 40”L x

20”W x 20”H or greater to drain and dwell.

c. The penetrant drain and dwell work station shall have a removable and cleanable 500-600 micron mesh strainer that provides the ability to limit the amount of organic materials, such as paint chips, going back into the penetrant tank.

3.2.1.3 Pre-Rinse

The pre-rinse capability shall consist of a work station that contains, at a minimum, a frame, tank, a splash prevention means, slatted grill, and a flexible hose(s) with handheld swivel nozzle(s).

a. The pre-rinse work station tank shall be large enough to completely rinse parts up to

b. The water pressure exiting the hose nozzle shall not exceed 40 pounds per square inch

(psi).

c. The flexible hose connection(s) shall be made from within the tank.

d. The flexible hose shall be ½ inch (minimum) inner diameter and 48 inches (minimum) in length.

e. The pre-rinse work station shall contain a means for preventing 100% of spray from the rinse station from reaching other stations or the rear of the SPI System.

f. The pre-rinse work station shall have control interfaces and display gauges for water temperature, pressure regulation, and flow regulation.

3.2.1.4 Hydrophilic Remover Application

The hydrophilic remover application capability shall consist of an individual work station consisting of a frame, tank, and cover with a handle or be applied by a spray technique within the rinse tank.

a. If a separate tank is provided, the hydrophilic remover application tank shall be large enough to completely apply hydrophilic remover to parts up to dimensions of 40”L x

20”W x 20”H or greater.

b. If a spray technique is utilized, a device that mixes hydrophilic remover concentrate into a water stream shall be used.

c. If a spray technique is utilized, controls shall be provided for the pressure regulation and concentration of the remover solution being sprayed.

d. If a spray technique is utilized, a separate hydrophilic remover tank is not required as the remover shall be applied within the rinse tank.

e. If a spray technique is utilized within a rinse tank, the concentration control mechanism shall never allow the hydrophilic remover concentration in the water stream to exceed 5%.

3.2.1.5 Hydrophilic Remover Rinse

The hydrophilic remover rinse capability shall consist of a work station that contains, at a minimum, a frame, tank, splash prevention means, slatted grill, black light assembly, and flexible hose(s) with handheld swivel nozzle(s).

a. The hydrophilic remover rinse tank shall be large enough to completely rinse parts up to

b. The water pressure exiting the hose nozzle shall not exceed 40 psi.

c. The flexible hose connection(s) shall be accomplished by the operator from within the tank.

d. The flexible hose shall be ½ inch (minimum) inner diameter and 48 inches (minimum) in length.

e. The hydrophilic remover rinse work station shall have an electrical outlet capable of powering the black light assembly. The electrical outlet shall be Ground Fault Circuit

Interrupter (GFCI) protected.

f. The black light assembly shall be capable of being secured overhead and provide a means for safe handling via a pistol grip, D or flat type handle.

g. The black light assembly shall be supported by adjustable brackets that can be directed towards the part being inspected.

h. The adjustable black light assembly brackets shall allow for dismounting of the black light without removing or loosening of fasteners.

i. The hydrophilic remover rinse work station shall contain a means for preventing 100% of spray from the rinse work station from reaching other stations or the rear portion of the

SPI System.

j. The hydrophilic remover rinse work station shall have control interfaces and display gauges for water temperature, pressure regulation, and flow regulation.

k. If a hydrophilic remover spray technique is used within this rinse tank, the concentration control mechanism shall never allow the hydrophilic remover concentration in the water stream to exceed 5%.

3.2.1.6 Drying Oven

The drying oven capability shall consist of a work station that contains, at a minimum, a frame, front loading drying oven cabinet, forced-air recirculating drying oven, drip pan, and thermostat.

a. The front loading drying oven cabinet shall be large enough to completely fit parts up to

b. The drying oven cabinet’s interior resting area shall be a minimum height of 14 inches from the base footing of the SPI System.

c. The drying oven work station shall be capable of reaching and sustaining a minimum temperature of 160°F within 30 minutes at ambient conditions.

d. The drying oven work station shall contain a removable and cleanable drip pan that collects any fallen residue.

e. The drying oven work station shall provide a thermometer-thermostat scaled, as a minimum, from 0°F to 200°F.

f. The thermostat shall control the drying oven temperature within plus or minus 12°F of the set temperature.

g. The temperature indicator shall display the current drying oven temperature within plus or minus 8°F of the actual temperature.

h. The thermostat shall be protected against inadvertent adjustment.

i. The drying oven work station shall provide a means of enclosing and insulating all four sides, top, and bottom of the oven cabinet.

3.2.1.7 Developer Application (Form D)

The Developer Application capability shall consist of a work station that contains, at a minimum, a frame and surface to support the application of Form D, Non-Aqueous Developer.

a. The developer application work station shall provide the capability of manually applying

Form D, Non-Aqueous Developer, as described in NAVAIR 01-1A-16-1.

b. The developer application work station surface shall be large enough to completely apply

Form D, Non-Aqueous Developer to parts up to dimensions of 40”L x 20”W x 20”H or greater.

c. The developer application work station shall contain a means for preventing developer spray from reaching neighboring stations or work surfaces as well as the rear of the SPI

System.

3.2.1.8 Inspection

The inspection capability shall consist of a work station that contains, at a minimum, a frame, work surface, black light assembly, exhaust fan, and canopy.

a. The inspection work station surface shall be large enough to completely inspect parts up to dimensions of 40”L x 20”W x 20”H or greater.

b. The inspection work station shall have a GFCI protected electrical outlet capable of powering the black light assembly.

c. The black light assembly shall be capable of being secured overhead and provide a means for safe handling via a pistol grip, D or flat type handle.

d. The black light assembly shall be supported by adjustable brackets that can be directed towards the part being inspected.

e. The adjustable black light assembly brackets shall allow for dismounting without removing or loosening of fasteners.

f. The inspection work station shall have a full canopy with side curtains and a front split to allow an entrance and exit to the station.

g. The curtain material shall be weather resistant, waterproof cloth meeting the intent of

MIL-PRF-20696F, Type II, Class 2.

h. The curtain material shall be attached to the canopy with snaps, or hook and pile fasteners for easy removal and replacement.

i. The ambient visible light within the station, when the canopy is closed, shall not exceed 2 foot-candles.

j. When canopy is completely closed the total width of the inspection station, including the area enclosed by the canopy measured from front to rear, shall not exceed 54 inches

k. The inspection work station shall contain a ventilation/exhaust fan capable of exhausting a minimum one (1) cubic foot per minute (cfm) of air per square foot (ft ) of area enclosed by the canopy (1cfm/ft

3.2.2 Black Light Assembly

The SPI System shall provide a minimum of two (2) AC powered ultraviolet black light assemblies as a means to view the fluorescent materials used in the penetrant inspection process.

a. The black light source shall be a Light Emitting Diode (LED).

b. The black light assembly shall emit ultraviolet radiation in the UV-A range with a peak wavelength at 365-370 nanometers (nm) and be properly filtered so that UV-B or visible radiation is not emitted.

c. The black light intensity shall be a minimum of 1,000 microwatts per square centimeter over a 3 inch diameter circle at 15 inches from the source.

d. Each black light assembly shall have a self-contained on/off power switch and be capable of being tied into the System’s master power switch(s).

e. The black light assembly shall have a minimum cord length of 10 feet and meet all applicable safety requirements of this specification.

f. The black light assembly shall be capable of being secured overhead and provide a means for safe handling via a pistol grip, D or flat type handle.

g. The black light assembly shall be supported by adjustable brackets that can be directed towards the part being inspected.

h. The adjustable black light assembly brackets shall allow for dismounting without removing or loosening of fasteners.

i. The black light assembly shall utilize a housing that:

Holds and protects the light source

Holds and supports the filter

Prevents leakage of unwanted visible light

Permits the direction of the beam onto the surface to be inspected

j. The intensity of the black light shall not be affected by variations in the input voltage. A voltage stabilizer or transformer with an efficiency of 97% shall be included.

3.2.3 Handheld Swivel Nozzle

The SPI System shall contain handheld nozzle(s) attached to the end of the hose(s) at the Pre-

Rinse and Hydrophilic Remover Rinse Station.

a. The nozzle(s) shall have a spring-operated, lever-type hand swivel valve.

b. The nozzle(s) shall deliver plain water and/or hydrophilic remover through a fan-shaped coarse spray.

c. The pressure of the plain water and/or hydrophilic remover flowing from the nozzles shall not exceed 40 psi.

d. Nozzles capable of producing spray patterns such as solid streams, a fine mist, or any adjustable spray patterns shall not be provided.

3.2.4 Controls

The SPI System and the inspection booth shall contain a master power switch and indicator light.

a. The master power switch shall be easily accessible while the SPI System is being operated.

b. The master power switch shall be protected from inadvertent activation and be identified with a label with character size no less than 0.31 inches in height.

c. The SPI System shall also have individual component power controls and indicator lights as required.

d. All power controls shall be fitted with safety devices or covers to eliminate safety hazards.

3.2.5 Baskets

Three (3) wire baskets shall be provided with the SPI System.

a. The baskets shall be made of corrosion resistant steel and contain hooks on one side in order to suspend the basket from the inside of the tanks.

b. The baskets shall have minimum dimensions of 12 inches in diameter and a maximum mesh opening of ½ inch square.

3.2.6 Integrated Timer

The SPI System shall contain an integrated digital timer.

a. The timer shall be capable of performing count-down timing for durations of no fewer than 59 minutes and 59 seconds.

b. The timer shall provide an audible alarm of no less than 80 dBA to signify when the preset time has expired.

c. The timer shall be Ingress Protection IP65 rated for moisture and water resistance.

3.2.7 Process Control Accessories

The SPI System shall contain the following accessories to be used for process control checks in accordance with NAVAIR 01-1A-16-2, WP 102 00. All accessories listed below will be packaged and delivered in a protective transit case. The permissible case construction materials are aluminum, plastic (including fiber reinforced plastic (FRP) or rotomolded plastic) or a combination of above materials. Noncorrosive hinges, handle, and locking devices are mandatory. Reinforced corners are desirable but are not mandatory, if case construction is ruggedized.

a. Nickel Chromium (NiCr) Panel Set with crack depths of 10 microns to test performance of “in-use” penetrant (Magnaflux P/N 506251 or equivalent). Hexavalent chromium and hexavalent chromium compounds shall not be used in the manufacture of the test panel.

b. Nickel Chromium (NiCr) Panel Set with crack depths of 20 microns to test performance of “in-use” penetrant (Magnaflux P/N 506252 or equivalent). Hexavalent chromium and hexavalent chromium compounds shall not be used in the manufacture of the test panel.

c. A pair of identical known defect standard (KDS) panels with matching cracks patterns

(Sherwin Twin KDS Panels or equivalent).

d. Hydrometer to measure specific gravity of water (Magnaflux P/N 5857 or equivalent).

e. Refractometer to measure hydrophilic remover concentration (Magnaflux P/N 513829 or equivalent).

f. Each accessory shall have its own foam cut-out housing within the case.

g. Foam material shall be cross-linked polyethylene that is resistant to jet fuel and hydraulic fluid.

3.3 System External Interface Requirements

3.3.1 Interface Identification and Diagrams

The SPI System shall interface with the following external services provided by the facility in which it is installed:

Electrical Power

Water Supply

Waste Water Drainage

3.3.1.1 System Electrical Power Interface Requirements

All wiring, insulation, and electrical components of the SPI System shall be in compliance with the National Electrical Code, NFPA 70.

a. The system shall contain a junction box in order to make the connection to the facility electrical power source.

b. The drying oven heater element shall be capable of operating from input voltages of 115, 230, or 440 VAC (4400 Watt Max) (+/- 10%), single phase, 60 Hz.

c. The heater element shall be the only component of the SPI System to operate directly from line voltage above 115 VAC.

d. The rest of the components shall operate from 115 VAC (+/-10%), (20 Amp Max), single phase, 60 Hz.

3.3.1.2 Water Supply Interface Requirements

The SPI System shall not require a water supply greater than 15 Gallons Per Minute (GPM) at 40

PSI and be capable of mating with ¾ inch standard pipe connections.

3.3.1.3 Drainage Interface Requirements

Gravity drainage shall be all that is required for the complete draining of all tanks contained within the SPI System.

a. Drainage connections and variable cut-off valves to control the drainage flow shall be provided at the bottom of all tanks using standard 1-1/4 inch National Pipe Thread (NPT) pipe connections.

Stationary Penetrant

Inspection (SPI) System

Electrical Power

Water Supply

Waste Water Drainage

3.4 Safety Requirements

3.4.1 General Safety Requirements

The following General Safety Requirement shall be incorporated into the design of the SPI

System.

a. The danger to personnel from fire and explosions shall be avoided by use of appropriate fire prevention measures.

b. Design shall locate items so that access during operations, maintenance, repair, or adjustment minimizes personnel exposure to hazards.

c. Design shall minimize human error in the operation and support of the unit.

d. All parts that present safety hazards shall be fitted with safety devices or covers that do not impair operating procedures.

e. Design shall minimize the severity of personnel injury or damage to equipment in the event of a mishap.

3.4.2 Materials and Processes

3.4.2.1 Materials, Selection of

a. Materials and parts which are not specified or which are not covered by documents listed herein shall be of the best commercial quality, entirely suitable, and readily commercially available, where applicable.

b. Materials resistant to deterioration, especially corrosion, shall be selected as the primary choice when feasible.

c. The materials shall be of uniform quality and condition, free from any defects that may adversely affect appearance, strength, endurance, wear resistance, and/or serviceability.

d. All selected materials shall perform satisfactorily during the service life of the unit, at the environmental extremes stated herein.

3.4.2.2 Hazardous Materials

Hazardous materials shall be avoided at all times in the design, manufacture, testing, operation, maintenance, and disposal of the SPI System. A hazardous material is any material that due to its chemical, physical, or biological nature causes safety, public health, or environmental concerns.

For the purpose of this contract, this includes but is not limited to the following materials:

a. Materials regulated as a hazardous material 49 CFR 173.2, or

b. Materials requiring a Material Safety Data Sheet (MSDS) per 29 CFR 1910.1200, or

c. Materials that during end use, treatment, handling, packaging, storage, transportation, or disposal meet or has the potential to meet the definition of a Hazardous Waste as defined by 40 CFR 261 Subparts A, B, C, or D, or

d. Materials regulated as an Ozone Depleting Substances (ODS) per 40 CFR 82 Subpart A, Appendices A and B, or

e. Materials identified in the Clean Air Act as a Hazardous Air Pollutant per 40 CFR Part 63, or

f. Materials regulated as an Extremely Hazardous Substance per 40 CFR 355, Appendices

A and B, or

g. Materials regulated as a toxic chemical or as a Persistent, Bio accumulative, Toxic (PBT) chemical under Section 313 of the Emergency Planning and Community Right-to-Know

Act (EPCRA) per 40 CFR Part 372, or

h. Materials referred to in section 101(14) or Section 102 of the Comprehensive

Environmental Response, Compensation, and Liability Act (CERCLA) per 40 CFR 302.4, or

i. Materials identified as a Volatile Organic Chemical (VOC) per 40 CFR Part 51.100(s), or

j. Materials regulated as a toxic or flammable substances under section 112(r) of the Clean

Air Act per 40 CFR Part 68.

3.4.2.3 Restricted Chemicals

a. The following hazardous materials shall be prohibited from use during the SPI System lifecycle: Asbestos, Class I ODS, Class II ODS, Hexavalent Chromium and

Polychlorinated Biphenyls (PCBs).

b. No exemptions shall be given for restricted chemicals with the exception of Hexavalent

Chromium per paragraph 3.4.2.5.

3.4.2.4 Targeted Chemicals

The following hazardous materials shall require NAVAIR approval for use during the SPI life cycle: Arsenic & Arsenic Compounds, Benzene, Beryllium & Beryllium Compounds, Cadmium

& Cadmium Compounds, Chloroform, Chromium & Non-Hexavalent Chromium Compounds, Cyclotrimethylenetrinitramine (RDX), Cyanide Compounds, Ethylene Glycol, Formaldehyde, Glycol Ethers, Hydrazine, Hydrofluoric Acid, Isocyanates, Lead & Lead Compounds, Mercury

& Mercury Compounds, Methyl Ethyl Ketone (MEK), Methyl Isobutyl Ketone (MIBK), Methylene Chloride, Methylene Dianiline (MDA), Naphthalene, Nickel & Nickel Compounds, Perchlorates, Perchloroethylene, Perfluorooctanoic Acid (PFOA), Phenol, Polybrominated

Diphenyl Ethers (PBDEs), Radioactive Materials, Toluene, Trichloroethylene (TCE), and

Xylene & Xylene Isomers. Approval will not be given unless it can be documented that there is no viable technically feasible alternative.

3.4.2.4.1 Metal Alloys

Chromium and nickel as a constituent of metal alloys are exempt.

3.4.2.4.2 Lead

Lead as a constituent of lead solder is exempt.

3.4.2.5 Hexavalent Chromium

Hexavalent Chromium exceeding 0.1 percent by weight in any homogeneous material is banned in the delivered system per DFAR 223-7008 except as provided in 223.7304 and 223.7305. Use of hexavalent chromium where an exception from 223.7304 does not apply requires Program

Executive Office (PEO) and Corrosion Control and Prevention Executive (CCPE) approval per

DON Hexavalent Chromium Authorization Process, 22 November 2011. If exemptions provided in DFAR 223.7304 and 223.7305 apply, approval by NAVAIR is required.

Any use of hexavalent chromium not cited by DFAR 223-7008 shall also require NAVAIR approval.

Approval will not be given for any use of hexavalent Chromium unless it can be documented that there is no viable technically feasible alternative.

3.4.2.6 Protective Coatings

a. Coatings shall contain no pigments in concentrations that will render the coating residues toxic during application or removal. The use of powder coatings is preferred.

b. On components where powder coating is not employed, the unit shall be finished and coated using an epoxy primer and a polyurethane topcoat. The primer will have a maximum Volatile Organic Compound (VOC) content of 420 grams/liter (3.5 pounds/gallon).

c. The topcoat shall have a maximum VOC content of 340 grams/liter (2.8 pounds/gallon).

Note: The following information is provided for guidance only. Triglycidyl Isocyanurate

(TGIC) polyester powder coating has been found to meet Navy requirements. Primer in accordance with MIL-DTL-53022E Type II and topcoat in accordance with MIL-PRF-

85285E Type II or Type III has been found to meet the Navy primer and topcoat requirements.

3.4.2.7 Lithium Batteries

All lithium batteries proposed for use in the SPI System shall be in accordance with NAVSEA

TM S9310-AQ-SAF-010 Revision 2. Detailed instructions for the approval process including testing requirements are contained in the technical manual. In some cases, the testing requirements can be waived if particular conditions are met, per TM S9310-AQ-SAF-010

Revision 2.

3.5 System Environment Requirements

The SPI System shall be capable of operation in all types of environments as defined herein.

Table 1 Environment Operating Conditions

Environmental Condition Requirement Low Temperature Storage -40 F

Low Temperature Operation +50 F

High Temperature Storage +160 F

High Temperature Operation +104 F

3.5.1 Air Transportation Acceleration

The SPI System, in its assembled configuration, shall withstand the following acceleration forces without damage: 3.0 G and 10ft/sec forward, 1.5 G and 5ft/sec aft, 1.5 G and 5ft/sec lateral, 2.0 G and 10ft/sec up, and 4.5 G and 11.5ft/sec down.

3.5.2 Vibration

The SPI System, in its assembled configuration, shall withstand the effects of random vibration levels experienced while transported as Jet Aircraft cargo as defined by MIL-STD-810G.

3.6 System Quality Factors

3.6.1 Reliability and Maintainability Program

The reliability shall be at 90% to ensure successful mission completion and the inherent availability level goal of 99.9%.

a. The predicted Mean-Time-Between-Failure (MTBF) value shall not be lower than 2,500 hours.

b. The predicted Mean-Time-To-Repair (MTTR) value shall not be higher than 2.50 hours.

The repair time shall be defined as the time required to fault isolate, remove and replace, repair, adjust and verify.

3.7 Design and Construction Constraints

3.7.1 General Design

a. The SPI System shall be constructed to hold aircraft parts and support equipment assemblies weighing up to 90 pounds without deformation of the parts or causing any damage to the SPI System.

b. The SPI System shall be designed and manufactured so that during operations there is no leakage of penetrant, remover, developer, and/or water within the area bounded by the outside dimensions of the SPI System.

c. Access to all components requiring calibration shall be provided from the front of the system. It is preferred that any component in the design of the SPI system used to identify a quantitative measurement already exist in the METCAL system to avoid the requirement to develop calibration procedures or standards. Refer to the Statement of

Work (SOW) PMA260C13/4332 concerning calibration requirements.

3.7.2 Overall System Dimensions

The SPI System shall conform to the following overall system dimensional requirements:

Length: No more than 132 inches

Width: No more than 36 inches

Work Area Surface Height: 36 inches ± 0.5 inches

Overall Height: No higher than 80 inches

The overall system dimensional requirements pertain to the following capabilities: Penetrant

Application, Penetrant Drain and Dwell, Pre-Rinse, Hydrophilic Remover Application, Hydrophilic Remover Rinse, Drying oven, Developer Application (Form D).

Note: The length dimension is measured left to right; the width dimension is measured front to rear.

3.7.2.1 Inspection Station Exclusion

The Inspection Booth may be excluded from the overall dimensions.

The Inspection booth dimensions shall not exceed:

Length: No longer than 36 inches

Width: No longer than 36 inches

Total Width (with canopy closed): No longer than 54 inches

Work Area Surface Height: 36 inches ± 0.5 inches

Overall Height: No higher than 80 inches

Note: The length dimension is measured left to right; while the width dimension is measured front to rear.

3.7.2.2 Tolerances

All tolerances for dimensional requirements listed in this performance specification are ± 0.5 inches unless otherwise noted.

3.7.3 Weight

In its operational configuration with tanks filled, the SPI System shall not exceed a maximum uniform floor contact loading of 157 lbs/ft

3.7.4 Material Construction

The SPI System shall be constructed of corrosion resistant steel unless otherwise noted.

3.7.5 Modularity

Each unique station used to perform the required penetrant operations shall be of a modular design in order to enable customization of installation.

a. All stations shall be capable of being separated, moved, and recombined only requiring the use of common hand tools.

b. When assembled, all modular components shall be secured and connected together through the use of mechanical fasteners.

c. SPI System modular components shall be sized to fit through doorways which are 48” x

76” and be capable of being properly assembled within the constraints of an area with dimensions 176.5”L x 70”W x 82”H.

d. The inspection station shall be constructed of two pieces and be able to be assembled within the floor to ceiling height of 82”.

3.7.6 Workmanship

The unit shall be completed using best commercial workmanship practice with emphasis on the following items:

a. Parts and assembled equipment shall be cleaned, after fabrication, of loose, spattered, or excess solder; weld metal; metal chips, cutting fluids, and mold release agents; or any other foreign material that might detract from the intended operation, function or appearance of the equipment.

b. Screws, nuts and bolts shall show no evidence of corrosion, cross threading, mutilation, or detrimental or hazardous burrs, and be firmly secured.

c. Any screw or bolt secured with a nut shall have at least two threads protruding through the nut.

d. Contacting surfaces shall be void of surface defects such as tool marks, gouge marks and nicks.

e. All parts shall be free from defects such as: seams, laps, laminations, cracks, casting fins

(at mold parting lines), extraneous material, visible steps or irregularities, sharp edges, nicks, scratches, burrs, tool scores and gouges.

f. Wires and cables shall be positioned or protected to avoid contact with rough or irregular surfaces, rotating components and sharp edges to avoid damage such as cuts, abrasions, and chaffing, to conductors or adjacent parts.

3.7.7 Mounting

The SPI System shall contain footing pads with a minimum thickness of 0.250 +0.030/-0.000 inches at the bottom of each standing leg. Each footing pad shall contain a mounting hole with a diameter of 0.397 +0.000/-0.007 inches.

3.8 Personnel Related Requirements

The SPI System design shall conform to the following human interface requirements as defined in MIL-STD-1472G.

3.8.1 Reach Limitations

The maximum effective forward reach (i.e., able to grasp and turn/push/pull) shall be 24 inches from the front of the user’s body.

3.8.2 Lifting Forward Reach

The lifting and placing of the part under inspection within each station shall be kept within 12 inches of the front of the user’s body. If a hazard (e.g., hot surface, electrical contact) exists within these reach envelopes, it must be guarded, removed, or moved beyond the maximum reach of the user.

3.9 Logistics Related Requirements

3.9.1 Maintenance Provisions

Maintenance Provisions shall be in accordance with MIL-S-8512D Paragraphs 3.3.7 - 3.3.7.4.

a. The SPI System shall be designed such that any maintenance inspections and tasks that are required to determine physical wear, condition, suitability for use, and fluid and lubrication level and condition, be within the capability of Naval maintenance personnel utilizing common/standard tools and maintenance equipment.

b. The SPI System design, packaging, and architecture shall facilitate rapid visual and/or measurement determination of all external physically wearing components, consumable fluids, and consumable parts/materials.

c. The SPI System shall be designed to allow the changing of fluids and other materials from the front side of the system.

3.9.2 Preventive/Scheduled Servicing and Inspections

Servicing, maintenance, and inspection tasks that are identified with a daily frequency will be accomplished by, and shall be within the capabilities of, the equipment operators.

a. Daily inspection and servicing tasks shall include, but are not limited to, the following:

inspection for leaks, checking fluid levels, checking for corrosion, damage, and security of components.

b. Tools shall not be required to perform any routine daily task.

3.10 Product Marking

3.10.1 Caution and Warning Labels

Caution and warning labels indicating the location, nature, and extent of a hazard shall be provided on the SPI System.

a. The labels shall be located as close as possible to the point of danger.

b. Letters of the labels shall be no less than 0.31 inches in height.

c. Warning or caution markings shall have a high contrast between the letters and background colors.

3.11 Packaging Requirements

The SPI System shipping container and packaging shall be designed to withstand the rough handling of logistic operations such as overseas shipment, stacking, and outside storage for up to one year.

a. ASTM D7478 shall be used in the design of a Type I, Class II, Style A shipping containers.

b. The packaging shall be weather resistant and designed for export shipments in accordance with ASTM D3951.

c. The packaged SPI System shall provide forklift provisions to allow for the movement of the packaged SPI System without causing any physical damage to the packaging or packaged SPI System.

3.12 Precedence and Criticality of Requirements

All requirements contain within this System Specification possess equal precedence and criticality.

4.0 Verification Requirements

The inspections and tests depicted in Table 2 and sections 4.1 and 4.2 are the minimums necessary to determine conformance to the requirements in Section 3 of this specification.

Table 2 Requirements and Verification Cross Reference

D = Demonstration – An actual operation of an item to provide evidence that the required functions were accomplished under specific scenarios.

I = Inspection – Examination of items to determine whether they conform to the specified requirements.

T = Testing – Perform a test as defined in Section 3 and Section 4.

A = Analysis – Using established technical or mathematical models, simulations, and procedures to provide evidence that the stated requirements were met.

N/A = Not Applicable

Table 2 Requirements and Verification Cross Reference

Requirements

Description

Pilot

Production

Testing

Production

Acceptance

Testing

Method

Paragraph

3.0 Requirements N/A N/A

3.1 Required States and Modes N/A N/A

3.2 System Capability and Component

Requirements

X D 4.2.1

3.2.1 Penetrant Processing Capabilities X D 4.2.1

3.2.1.1 Penetrant Application Station X D 4.2.1

3.2.1.1.a Penetrant Application Station X I 4.2.2

3.2.1.2 Penetrant Drain and Dwell Station X D 4.2.1

3.2.1.2.a Penetrant Drain and Dwell Station X D 4.2.1

3.2.1.2.b Penetrant Drain and Dwell Station X I 4.2.2

3.2.1.2.c Penetrant Drain and Dwell Station X D 4.2.1

3.2.1.3 Pre-Rinse Station X D 4.2.1

3.2.1.3.a Pre-Rinse Station X I 4.2.2

3.2.1.3.b Pre-Rinse Station X I 4.2.2

3.2.1.3.c Pre-Rinse Station X I 4.2.2

3.2.1.3.d Pre-Rinse Station X I 4.2.2

3.2.1.3.e Pre-Rinse Station X I 4.2.2

3.2.1.3.f Pre-Rinse Station X I 4.2.2

3.2.1.4 Hydrophilic Remover Application Station X D 4.2.1

3.2.1.4.a Hydrophilic Remover Application Station X I 4.2.2

3.2.1.4.b Hydrophilic Remover Application Station X D 4.2.1

3.2.1.4.c Hydrophilic Remover Application Station X I 4.2.2

3.2.1.4.d Hydrophilic Remover Application Station X D 4.2.1

3.2.1.4.e Hydrophilic Remover Application Station X T 4.2.4

3.2.1.5 Hydrophilic Remover Rinse Station X D 4.2.1

3.2.1.5.a Hydrophilic Remover Rinse Station X I 4.2.2

3.2.1.5.b Hydrophilic Remover Rinse Station X I 4.2.2

3.2.1.5.c Hydrophilic Remover Rinse Station X I 4.2.2

3.2.1.5.d Hydrophilic Remover Rinse Station X I 4.2.2

3.2.1.5.e Hydrophilic Remover Rinse Station X I 4.2.2

3.2.1.5.f Hydrophilic Remover Rinse Station X I 4.2.2

3.2.1.5.g Hydrophilic Remover Rinse Station X I 4.2.2

3.2.1.5.h Hydrophilic Remover Rinse Station X I 4.2.2

3.2.1.5.i Hydrophilic Remover Rinse Station X I 4.2.2

3.2.1.5.j Hydrophilic Remover Rinse Station X I 4.2.2

3.2.1.5.k Hydrophilic Remover Rinse Station X X T 4.2.4

3.2.1.6 Drying Oven Station X D 4.2.1

3.2.1.6.a Drying Oven Station X I 4.2.2

3.2.1.6.b Drying Oven Station X I 4.2.2

3.2.1.6.c Drying Oven Station X X T 4.2.5

3.2.1.6.d Drying Oven Station X I 4.2.2

3.2.1.6.e Drying Oven Station X I 4.2.2

3.2.1.6.f Drying Oven Station X X T 4.2.7, 4.2.8

3.2.1.6.g Drying Oven Station X X T 4.2.6

3.2.1.6.h Drying Oven Station X I 4.2.2

3.2.1.6.i Drying Oven Station X I 4.2.2

3.2.1.7 Developer Application Station (Form D) X D 4.2.1

3.2.1.7.a Developer Application Station (Form D) X D 4.2.1

3.2.1.7.b Developer Application Station (Form D) X I 4.2.2

Production

Testing

Production

3.2.1.7.c Developer Application Station (Form D) X I 4.2.2

3.2.1.8 Inspection Station X D 4.2.1

3.2.1.8.a Inspection Station X I 4.2.2

3.2.1.8.b Inspection Station X I 4.2.2

3.2.1.8.c Inspection Station X I 4.2.2

3.2.1.8.d Inspection Station X I 4.2.2

3.2.1.8.e Inspection Station X I 4.2.2

3.2.1.8.f Inspection Station X I 4.2.2

3.2.1.8.g Inspection Station X I 4.2.2

3.2.1.8.h Inspection Station X I 4.2.2

3.2.1.8.i Inspection Station X T 4.2.10

3.2.1.8.j Inspection Station X I 4.2.2

3.2.1.8.k Inspection Station X I 4.2.2

3.2.2 Black Light Assembly X D 4.2.1

3.2.2.a Black Light Assembly X D 4.2.1

3.2.2.b Black Light Assembly X X T 4.2.9

3.2.2.c Black Light Assembly X X T 4.2.9

3.2.2.d Black Light Assembly X D 4.2.1

3.2.2.e Black Light Assembly X I 4.2.2

3.2.2.f Black Light Assembly X I 4.2.2

3.2.2.g Black Light Assembly X I 4.2.2

3.2.2.h Black Light Assembly X I 4.2.2

3.2.2.i Black Light Assembly X I 4.2.2

3.2.2.j Black Light Assembly X I 4.2.2

3.2.3 Handheld Swivel Nozzle X I 4.2.2

3.2.3.a Handheld Swivel Nozzle X I 4.2.2

3.2.3.b Handheld Swivel Nozzle X I 4.2.2

3.2.3.c Handheld Swivel Nozzle X I 4.2.2

3.2.3.d Handheld Swivel Nozzle X I 4.2.2

3.2.4 Controls X D 4.2.1

3.2.4.a Controls X I 4.2.2

3.2.4.b Controls X I 4.2.2

3.2.4.c Controls X I 4.2.2

3.2.4.d Controls X I 4.2.2

3.2.5 Baskets X I 4.2.2

3.2.5.a Baskets X I 4.2.2

3.2.5.b Baskets X I 4.2.2

3.2.6 Integrated Timer X D 4.2.1

3.2.6.a Integrated Timer X D 4.2.1

3.2.6.b Integrated Timer X D/A 4.2.1/4.2.3

3.2.6.c Integrated Timer X A 4.2.3

3.2.7 Process Control Accessories X D 4.2.1

3.2.7.a Process Control Accessories X I 4.2.2

3.2.7.b Process Control Accessories X I 4.2.2

3.2.7.c Process Control Accessories X I 4.2.2

3.2.7.d Process Control Accessories X I 4.2.2

3.2.7.e Process Control Accessories X I 4.2.2

3.2.7.f Process Control Accessories X I 4.2.2

3.2.7.g Process Control Accessories X I 4.2.2

3.3 System External Interface Requirements X D 4.2.1

3.3.1 Interface Identification and Diagrams X N/A

Production

Testing

Production

3.3.1.1 System Electrical Power Interface

Requirements

X I 4.2.2

3.3.1.1.a System Electrical Power Interface

Requirements

X I 4.2.2

3.3.1.1.b System Electrical Power Interface

Requirements

X I 4.2.2

3.3.1.1.c System Electrical Power Interface

Requirements

X I 4.2.2

3.3.1.1.d System Electrical Power Interface

Requirements

X I 4.2.2

3.3.1.2 Water Supply Interface Requirements X I 4.2.1

3.3.1.3 Drainage Interface Requirements X D 4.2.1

3.3.1.3.a Drainage Interface Requirements X I 4.2.2

3.4 Safety Requirements X N/A

3.4.1.a General Safety Requirements X I 4.2.2

3.4.1.b General Safety Requirements X I 4.2.2

3.4.1.c General Safety Requirements X I 4.2.2

3.4.1.d General Safety Requirements X I 4.2.2

3.4.1.e General Safety Requirements X I 4.2.2

3.4.2 Materials and Processes X N/A

3.4.2.1 Materials, Selection of X N/A

3.4.2.1.a Materials, Selection of X I 4.2.2

3.4.2.1.b Materials, Selection of X I 4.2.2

3.4.2.1.c Materials, Selection of X I 4.2.2

3.4.2.1.d Materials, Selection of X I 4.2.2

3.4.2.2 Hazardous Materials X I 4.2.2

3.4.2.2.a Hazardous Materials X I 4.2.2

3.4.2.2.b Hazardous Materials X I 4.2.2

3.4.2.2.c Hazardous Materials X I 4.2.2

3.4.2.2.d Hazardous Materials X I 4.2.2

3.4.2.2.e Hazardous Materials X I 4.2.2

3.4.2.2.f Hazardous Materials X I 4.2.2

3.4.2.2.g Hazardous Materials X I 4.2.2

3.4.2.2.h Hazardous Materials X I 4.2.2

3.4.2.2.i Hazardous Materials X I 4.2.2

3.4.2.2.j Hazardous Materials X I 4.2.2

3.4.2.3 Restricted Materials X N/A

3.4.2.3.a Restricted Materials X I 4.2.2

3.4.2.3.b Restricted Materials X I 4.2.2

3.4.2.4 Targeted Materials X I 4.2.2

3.4.2.4.1 Metal Alloys X I 4.2.2

3.4.2.4.2 Lead X I 4.2.2

3.4.2.5 Hexavalent Chromium X I 4.2.2

3.4.2.6 Protective Coatings X N/A

3.4.2.6.a Protective Coatings X I 4.2.2

3.4.2.6.b Protective Coatings X I 4.2.2

3.4.2.6.c Protective Coatings X I 4.2.2

3.4.2.7 Lithium Batteries X I 4.2.2

3.5 System Environmental Requirements X T,I 4.2.11

3.5.1 Air Transportation Acceleration X T 4.2.11.5

3.5.2 Vibration X T 4.2.11.6

Production

Testing

Production

3.6 System Quality Factors X N/A

3.6.1 Reliability and Maintainability Program X A 4.2.3,4.2.12

3.6.1.a Reliability and Maintainability Program X A 4.2.3,4.2.12

3.6.1.b Reliability and Maintainability Program X A 4.2.3,4.2.12

3.7 Design and Construction Constraints X N/A

3.7.1 General Design X X N/A

3.7.1.a General Design X X I/T 4.2.2,4.2.14

3.7.1.b General Design X X T 4.2.13

3.7.1.c General Design X X I 4.2.2

3.7.2 Overall System Dimensions X I 4.2.2

3.7.2.1 Inspection Station Exclusion X I 4.2.2

3.7.2.2 Tolerances X I 4.2.2

3.7.3 Weight X I 4.2.2

3.7.4 Material Construction X I 4.2.2

3.7.5 Modularity X I 4.2.2

3.7.5.a Modularity X D 4.2.1

3.7.5.b Modularity X I 4.2.2

3.7.5.c Modularity X I 4.2.2

3.7.5.d Modularity X I 4.2.2

3.7.6 Workmanship X X I 4.2.2

3.7.6.a Workmanship X X I 4.2.2

3.7.6.b Workmanship X X I 4.2.2

3.7.6.c Workmanship X X I 4.2.2

3.7.6.d Workmanship X X I 4.2.2

3.7.6.e Workmanship X X I 4.2.2

3.7.6.f Workmanship X X I 4.2.2

3.7.7 Mounting X X I 4.2.2

3.8 Personnel Related Requirements X N/A

3.8.1 Reach Limitations X I 4.2.2

3.8.2 Lifting Forward Reach X I 4.2.2

3.9 Logistics Related Requirements X N/A

3.9.1 Maintenance Provisions X I 4.2.2

3.9.1.a Maintenance Provisions X I 4.2.2

3.9.1.b Maintenance Provisions X I 4.2.2

3.9.1.c Maintenance Provisions X I 4.2.2

3.9.2 Preventative/Scheduled Servicing and

Inspections

X I 4.2.2

3.9.2.a Preventative/Scheduled Servicing and

Inspections

X I 4.2.2

3.9.2.b Preventative/Scheduled Servicing and

Inspections

X I 4.2.2

3.10 Product Marking X X N/A

3.10.1 Caution and Warning Labels X X I 4.2.2

3.10.1.a Caution and Warning Labels X X I 4.2.2

3.10.1.b Caution and Warning Labels X X I 4.2.2

3.10.1.c Caution and Warning Labels X X I 4.2.2

3.11 Packaging Requirements X X I 4.2.2

3.11.a Packaging Requirements X X I 4.2.2

3.11.b Packaging Requirements X X I 4.2.2

3.11.c Packaging…