Performance_Spec.pdf

Destruction Notice

FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY

ANY METHOD THAT WILL PREVENT DISCLOSURE OF

CONTENTS OR RECONSTRUCTION OF THIS DOCUMENT.

NAWCADLKE MISC 4.8.1.3.00

#0204

1 JUNE 2015

DEPARTMENT OF THE NAVY

PROGRAM EXECUTIVE OFFICE PMA201

NAVAL AIR SYSTEMS COMMAND

PATUXENT RIVER, MARYLAND 20670-1161

A/A42R-1 Air Refueling Store Avionics Upgrade Program

System Specification for the

TTU-571/E Power Interface Test Set

DISTRIBUTION STATEMENT A: APPROVED FOR PUBLIC RELEASE; DISTRIBUTION IS UNLIMITED.

APPROVED: APPROVED:

TITLE: LOGISTICS INTEGRATION MANAGEMENT TITLE: SE AND ALRE SYSTEMS ENGINEERING

(AIR-6.6) (AIR-4.8.1)

APPROVED:

TITLE: PROGRAM MANAGER

(PMA-201AAE/FC APMSE)

NAWCADLKE MISC 4.8.1.3.00

1 June 2015

Revision History

Date Ver. Remarks Authors 21 January 2015 Draft 1st Draft. T. F. Richardson 25 February 2015 Draft 2nd Draft. Added requirements for PITS Jumper

Cable.

T. F. Richardson

21 April 2015 Draft 3rd Draft. T. F. Richardson 1 June 2015 Final (1) Adjudicated comments from SRB.

(2) Added document number.

T. F. Richardson ii

Table of Contents

1.0 SCOPE

2.0 APPLICABLE DOCUMENTS

2.1 GOVERNMENT DOCUMENTS

2.2 NON-GOVERNMENT DOCUMENTS

2.3 DRAWINGS

3.0 REQUIREMENTS

3.1 TEST CAPABILITIES

3.1.1 AIRCRAFT FUEL TO/FROM TEST

3.1.2 LAMP TEST

3.1.3 SELF TEST

3.2 SWITCHES AND CIRCUIT BREAKERS

3.2.1 CIRCUIT BREAKER (CB1)

3.2.2 POWER SWITCH

3.2.3 LAMP TEST SWITCH

3.3 INDICATORS

3.3.1 AIRCRAFT FUEL TO/FROM INDICATORS

3.3.2 115 VAC POWER INDICATOR

3.3.3 28 VDC POWER INDICATOR

3.3.4 15 VDC POWER INDICATOR

3.3.5 DROGUE STOWED INDICATOR

3.3.6 SELF TEST FAULT INDICATOR

3.3.7 HI-LEVEL FLOAT SWITCH INDICATOR

3.4 PORTS

3.4.1 J1 GROUND STUD

3.4.2 J2 POWER PORT

3.4.3 J3 UNIT UNDER TEST (UUT) PORT

3.5 PITS CABLE SET

3.6 JUMPER CABLE ASSEMBLY

3.7 CONNECTIVITY

3.7.1 EXTERNAL CABLES

3.7.2 AIRCRAFT WIRING

3.7.3 ARS

3.7.4 CONTROL PANEL

3.8 INPUT POWER

3.9 OUTPUT POWER

3.10 PHYSICAL CHARACTERISTICS

3.10.1 ELECTRONICS ENCLOSURE (BOTTOM SECTION)

3.10.2 STORAGE LID (TOP SECTION)

3.10.3 DIMENSIONS

3.10.4 WEIGHT

3.10.5 COLOR

3.11 CALIBRATION

3.12 ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (E3)

iii

3.12.1 ELECTROMAGNETIC INTERFERENCE (EMI)

3.12.2 ELECTROMAGNETIC COMPATIBILITY (EMC)

3.13 ENVIRONMENTAL REQUIREMENTS

3.13.1 TEMPERATURE

3.13.1.1 OPERATING TEMPERATURE

3.13.1.2 STORAGE TEMPERATURE

3.13.2 RAIN

3.13.3 SALT FOG

3.13.4 DUST

3.13.5 EXPLOSIVE ATMOSPHERE

3.13.6 VIBRATION

3.13.7 MECHANICAL SHOCK

3.13.7.1 TRANSIT DROP

3.13.7.2 BENCH HANDLING

3.14 MATERIALS

3.14.1 HAZARDOUS MATERIALS

3.14.2 RESTRICTED MATERIALS

3.14.3 TARGETED MATERIALS

3.14.4 METAL ALLOYS

3.14.5 LEAD

3.14.6 PROTECTIVE COATINGS

3.14.7 OTHER RESTRICTED MATERIALS AND GASES

3.14.7.1 FLAMMABLE MATERIALS

3.14.7.2 EXPLOSIVE MATERIALS

3.14.8 FUNGUS RESISTANCE

3.15 NAMEPLATES AND PRODUCT MARKING

3.15.1 PLACARDS

3.15.2 ITEM UNIQUE IDENTIFICATION (IUID) MARKING

3.15.3 REFERENCE DESIGNATIONS

3.15.4 WARNING MARKINGS

3.15.5 EQUIPMENT IDENTIFICATION

3.16 WORKMANSHIP

3.16.1 CLEANING

3.16.2 THREADED PARTS OR DEVICES

3.16.3 SOLDERING

3.16.4 CONNECTORS

3.16.5 WIRES AND CABLE ASSEMBLIES

3.16.6 GROUNDING

3.17 SAFETY

3.18 MEAN TIME BETWEEN FAILURE (MTBF)

4.0 VERIFICATION

4.1 VERIFICATION COMPLIANCE

4.2 TEST MODES

4.2.1 OPERATING

4.2.2 STORAGE

4.3 SYSTEM OPERATIONAL TEST

iv

4.4 SPECIAL TESTS AND EXAMINATIONS

4.4.1 SYSTEM INSPECTION

4.4.2 SYSTEM PERFORMANCE TEST

4.4.3 FUNCTIONAL TEST (DEMONSTRATION)

4.4.4 RELIABILITY ANALYSIS

4.4.5 ELECTROMAGNETIC INTERFERENCE (EMI)

4.4.6 ELECTROMAGNETIC COMPATIBILITY (EMC)

4.4.7 HIGH TEMPERATURE

4.3.9 LOW TEMPERATURE

4.3.10 RAIN

4.3.11 SALT FOG

4.3.12 DUST

4.3.13 EXPLOSIVE ATMOSPHERE

4.3.14 VIBRATION

4.3.15 TRANSIT DROP

4.3.16 BENCH HANDLING

4.3.17 SAFETY ASSESSMENT

4.4 REQUIREMENTS CROSS REFERENCE

5.0 PRESERVATION, PACKAGING, AND MARKING

1.0 SCOPE

This document establishes the system requirements for a new Power Interface Test Set (PITS) (P/N 3456AS300-2) and a new Jumper Cable Assembly (P/N 3456AS100-3) to support the new A/A42R-1 Air Refueling Store (ARS) configuration (herein referred to as the "upgraded ARS") that was developed as part of the Avionics Upgrade Program (AUP) for the ARS.

2.0 APPLICABLE DOCUMENTS

This System Specification takes precedence if a conflict exists between this document and any other document specified herein. Nothing in this document, however, supersedes applicable laws and regulations unless the Contractor has obtained a specific exemption. Unless otherwise specified, the latest revision as of the date of the Contract shall be used for each document.

2.1 GOVERNMENT DOCUMENTS

SPECIFICATIONS

Military MIL-DTL-15024F Detail Specification Plates, Tags, and Bands for Identification of Equipment, General Specification for; dated 28 November

MIL-DTL-53022 Detail Specification, Primer, Epoxy Coating, Corrosion Inhibiting Lead and Chromate Free

MIL-PRF-28800 Performance Specification; Test Equipment for use with Electrical and Electronic Equipment, General Specification For

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

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

Other PMA201-08-002 Rev B Performance Specification For The Air Refueling Store

A/A42R-1 Avionics System Upgrade

STANDARDS

Military MIL-STD-130N Department of Defense Standard Practice, Identification

Marking of U.S. Military Property; dated 16 November 2012 MIL-STD-461 Department of Defense Interface Standard, Requirements for the Control of Electromagnetic Interference Characteristics of Subsystems and Equipment

MIL-STD-464 Department of Defense Interface Standard, Electromagnetic Environmental Effects, Requirements for Systems

MIL-STD-704 Department of Defense Interface Standard, Aircraft Electrical Power Characteristics

MIL-STD-810 Department of Defense Test Method Standard, Environmental Engineering Considerations and Laboratory Tests

MIL-STD-882 Military Standard, System Safety Requirements MIL-STD-1399 Military Standard, Interface Standard for Shipboard Systems

STANDARDS

Military MIL-STD-1399-300 Military Standard, Interface Standard for Shipboard Systems, Section 300, Electric Power, Alternating Current MIL-STD-1472 Department of Defense Design Criteria Standard, Human

Engineering MIL-STD-2073-1 Department of Defense, Standard Practice for Military

Packaging

STANDARDS

Other Government Agency 29 CFR 1910.1200 Hazard Communication 40 CFR Part 51.100 Definitions 40 CFR Part 63 National emission standards for Hazardous Air Pollutants for

Source Categories (a.k.a. Maximum Achievable Control Technology (MACT))

40 CFR 82 Protection of stratospheric ozone 40 CFR 261 Identification and listing of hazardous waste 40 CFR 302.4 Release Notification Hazardous Substances 40 CFR 355 Emergency planning and notification 40 CFR 372 Toxic chemical release reporting 49 CFR 173.2 Hazardous materials, classes and index to hazard class definitions CFR Title 29: Par 1910 Occupational Safety and Health Standards - Hazard

Communication FED-STD-595 Colors Used in Government Procurement

HANDBOOKS

Military MIL-HDBK-217 Military Handbook, Reliability Prediction of Electronic

Equipment MIL-HDBK-454 Department of Defense Handbook, General Guidelines for

Electronic Equipment MIL-HDBK-2084 Department of Defense Handbook for Maintainability of

Avionic and Electronic Systems and Equipment

MANUALS

Military AT-823T0-MIB-000 Power Interface Test Set TTU-571/E Technical Manual

INSTRUCTIONS

Military NAVSEAINST 8020.6E Department of the Navy Weapon Systems Explosives Safety

Review Board

2.2 NON-GOVERNMENT DOCUMENTS

STANDARDS

ANSI/J-STD-001A Requirements for Soldered Electrical and Electronic Assemblies ASTM F1166 Marine Systems, Equipment and Facilities, Human Engineering

Design for IEEE-STD-200 Reference Designations for Electrical and Electronics Parts and

Equipments IEEE-STD-315 Graphic Symbols for Electrical and Electronics Diagrams

2.3 DRAWINGS

NAVAIR

3456AS100 Jumper Cable Assembly 3456AS300 Power Interface Test Set, TTU-571/E

3.0 REQUIREMENTS

The operation and performance of the new PITS and new Jumper Cable Assembly shall be in accordance with this document and NAVAIR AT-823TO-MIB-000. If a conflict exists between this document and NAVAIR AT-823TO-MIB-000, then this document takes precedence.

3.1 TEST CAPABILITIES

The test capabilities of the legacy PITS (as listed in this section) shall be retained by the new PITS. The new PITS shall simulate the aircraft functions required to operate and test the upgraded ARS on-aircraft and off-aircraft at the Organizational, Intermediate, and Depot maintenance levels.

3.1.1 AIRCRAFT FUEL TO/FROM TEST

The new PITS shall verify proper operation of the fuel transfer circuits in the upgraded ARS without transferring any fuel.

(a) The OFF indicator on the new PITS shall illuminate when the STORE switch on the new

ARS Control Panel is set to the OFF or TO position.

(b) The TO indicator on the new PITS shall illuminate when the STORE switch on the new

ARS Control Panel is set to the TO position.

(c) The OFF and TO indicators on the new PITS shall not illuminate when the STORE switch on the new ARS Control Panel is set to the FROM position.

3.1.2 LAMP TEST

The new PITS shall verify proper operation of all indicators on the front panel. The Lamp Test shall be initiated when the LAMP TEST switch is moved to the ON position. The Lamp Test shall function with and without a new Control Panel installed in the front panel.

3.1.3 SELF TEST

The new PITS shall verify proper operation of all electronics inside the PITS Electronics Enclosure. The Self Test shall be initiated when the LAMP TEST switch is moved to the ON position. The Self Test shall function with and without a new Control Panel installed in the front panel.

3.2 SWITCHES AND CIRCUIT BREAKERS

The switches and circuit breakers below shall be mounted on the front panel assembly of the new

PITS.

3.2.1 CIRCUIT BREAKER (CB1)

The new PITS shall include a circuit breaker labeled "CB1" that disconnects the new PITS from the AC input power when the current through the J2 port exceeds 15 Amperes AC.

3.2.2 POWER SWITCH

The new PITS shall include a toggle switch labeled "POWER". When the POWER switch is moved to the ON position, the new PITS shall be powered by the AC input power present at the J2 port.

3.2.3 LAMP TEST SWITCH

The new PITS shall include a momentary toggle switch labeled "LAMP TEST". When the LAMP TEST switch is held in the ON position, all indicators on the front panel shall illuminate.

3.3 INDICATORS

The indicators below shall be mounted on the front panel assembly of the new PITS.

3.3.1 AIRCRAFT FUEL TO/FROM INDICATORS

The new PITS shall include two indicators labeled "OFF" and "TO" that show the state of the fuel transfer circuits.

3.3.2 115 VAC POWER INDICATOR

The new PITS shall include an indicator labeled "115 VAC". The indicator shall illuminate when the POWER switch is moved to the ON position and MIL-STD-704 compliant 115 Volts AC, 400 Hertz single-phase power is present at the J2 port.

3.3.3 28 VDC POWER INDICATOR

The new PITS shall include an indicator labeled "28 VDC". The indicator shall illuminate when the POWER switch is moved to the ON position and MIL-STD-704 compliant 28 Volts DC power is present at the J3 port.

3.3.4 15 VDC POWER INDICATOR

The new PITS shall include an indicator labeled "15 VDC". The indicator shall illuminate when the POWER switch is moved to the ON position and MIL-STD-704 compliant 15 Volts DC power is present at the J3 port from the new ARS Controller.

3.3.5 DROGUE STOWED INDICATOR

The new PITS shall include an indicator labeled "DROGUE STOWED" that illuminates when a STOWED signal is transmitted from the Drogue Stowage Sensor in the upgraded ARS.

3.3.6 SELF TEST FAULT INDICATOR

The new PITS shall include an indicator labeled "SELF TEST FAULT" that shows whether a fault was detected during Self Test.

3.3.7 HI-LEVEL FLOAT SWITCH INDICATOR

The new PITS shall include an indicator labeled "HI-LEVEL SHUTOFF" that shows the state of the Hi-Level Float Switch in the upgraded ARS. This indicator will be illuminated when there is continuity through the ARS high level float switch. It will extinguish when the switch contacts open.

3.4 PORTS

The ports below shall be mounted on the front panel assembly of the new PITS. Each port shall include the same signals as the corresponding port in the legacy PITS.

3.4.1 J1 GROUND STUD

The J1 Ground Stud shall mate with the terminal lug (P/N PN10-8F-L) on the PITS Grounding Cable Assembly (P/N 3456AS303-1).

3.4.2 J2 POWER PORT

The J2 Power Port shall mate with the PITS Power Cable Assembly (P/N 3456AS306-1). The J2 port shall include all power and return lines required to supply the new PITS and upgraded ARS with 115 Volts AC, 400 Hertz single-phase input power. The contacts in the J2 port shall be rated for a continuous current draw of 15 Amps or greater.

3.4.3 J3 UNIT UNDER TEST (UUT) PORT

The J3 UUT Port shall mate with the new Jumper Cable Assembly (P/N 3456AS100-3). The J3 port shall include all power, return, and signal lines required for the new PITS to power, operate, and test the upgraded ARS. The power and return contacts in the J3 port shall be rated for a continuous current draw of 15 Amps or greater

3.5 PITS CABLE SET

The new PITS shall include a set of the following legacy cable assemblies as part of its configuration:

(a) Power Adapter Assembly, P/N 3456AS302-1

(b) Power Cable Assembly, P/N 3456AS306-1

(c) Grounding Cable Assembly, P/N 3456AS303-1

3.6 JUMPER CABLE ASSEMBLY

(a) The new Jumper Cable Assembly (P/N 3456AS100-3) shall not be part of the PITS Cable Set.

(b) One connector shall be labeled P1 and the other P2.

(c) Part number D38999/26ZD19PN (or equivalent) shall be used for the P1 connector.

(d) Part number D38999/26ZD19SN (or equivalent) shall be used for the P2 connector.

(e) The P1 connector shall mate with the J3 port on the new PITS.

(f) The P2 connector shall mate with the J210 port on the upgraded ARS.

(g) Part number M85049/38S15N shall be used as the backshell for each connector.

(h) The pin-to-pin connections in the new Jumper Cable Assembly shall be the same as the legacy Jumper Cable Assembly (P/N 3456AS100-2).

(i) A continuous EMI shield shall be applied over the entire wire assembly in the new

Jumper Cable Assembly. This EMI shield shall be electrically bonded to the backshell of each connector in the cable assembly. Neither the outer EMI shield nor the connector assembly shall be used as a signal ground path in the cable assembly.

(j) The new Jumper Cable Assembly shall provide all power and signal lines required for the new PITS to power, operate, and test the upgraded ARS.

(k) The pin outs and signal names for the new Jumper Cable Assembly shall be in accordance with the table below:

PITS SIDE STORE SIDE SIGNAL NAME

CONN. PIN CONN. PIN

P1 H P2 H 15 VDC REG

P1 L P2 L 15 VDC REG RTN

P1 D P2 D Data 1 P1 E P2 E Data 2

P1 F P2 F DUMP STATUS (NOT USED)

P1 R P2 R JETTISON SIGNAL

P1 M P2 M 28 VDC SWITCHED

P1 K P2 K STORE SWITCH 28 VDC

P1 B P2 B 115 VAC Hi

P1 A P2 A STRUCTURE GROUND

P1 P P2 P STRUCTURE GROUND

P1 G P2 G DROGUE STOWAGE STATUS

P1 J P2 J 28 VDC

P1 T P2 T HI LEVEL FLOAT OUTPUT Hi

P1 N P2 N SPARE

P1 S P2 S HI LEVEL FLOAT OUTPUT Lo

P1 C P2 C DUMP RETURN (NOT USED)

3.7 CONNECTIVITY

3.7.1 EXTERNAL CABLES

With the exception of the Jumper Cable Assemblies P/N 3456AS100-1 and P/N 3456AS100-2, the new PITS shall interface with the same external cable assemblies as the legacy PITS.

3.7.2 AIRCRAFT WIRING

The new PITS shall not use aircraft wiring to operate and test the upgraded ARS.

3.7.3 ARS

When attached to the J3 port on the new PITS and the J210 port on the upgraded ARS, the new Jumper Cable Assembly shall provide the electrical connections that enable the new PITS to power, operate, and test the upgraded ARS.

Figure 1 - Upgraded ARS O-Level Test Setup

3.7.4 CONTROL PANEL

The new Control Panel has dimensions 5.750" W x 3.750" H x 6.000" D. The front panel of the new PITS shall include a sealed cavity large enough to accommodate the new Control Panel.

(a) When seated inside the cavity, the retaining screws on the new Control Panel shall be used to hold it securely in place.

(b) The cavity shall prevent water intrusion inside the PITS.

(c) The cavity shall mitigate electromagnetic interference (EMI) issues with the PITS.

(d) The cavity shall provide the electrical connections required to power and operate the new

Control Panel.

(e) When a new Control Panel is seated inside the cavity, and a new Jumper Cable Assembly is attached to the J3 port on the new PITS and the J210 port on the upgraded ARS, the cavity shall provide the electrical connections required for the new Control Panel to operate and control the upgraded ARS on-aircraft and off-aircraft.

3.8 INPUT POWER

The new PITS shall operate using MIL-STD-704 compliant 115 Volts AC, 400 Hertz single-phase input power with a continuous current draw of 15 Amps or less supplied through the J2 port.

3.9 OUTPUT POWER

The new PITS shall concurrently supply MIL-STD-704 compliant AC and DC power to the upgraded ARS through the J3 port:

(a) 115 Volts AC, 400 Hertz single-phase pass-thru power with a continuous current draw of up to 15 Amps.

(b) 28 Volts DC power with a continuous current draw of 3.6 Amps or greater.

3.10 PHYSICAL CHARACTERISTICS

The enclosure for the new PITS shall have a top section and a bottom section. The top section shall be attachable and detachable to the bottom section.

3.10.1 ELECTRONICS ENCLOSURE (BOTTOM SECTION)

The bottom section of the enclosure for the new PITS shall house the front panel assembly and all internal electronics, and provide a cavity to accommodate the new Control Panel.

3.10.2 STORAGE LID (TOP SECTION)

The top section of the enclosure for the new PITS shall include a compartment to store the PITS Cable Set.

3.10.3 DIMENSIONS

(a) The new PITS shall be 18 inches +/- 1 inch in height, 12 inches +/- 1 inch in width, and

13 inches +/- 1 inch in depth.

(b) The new Jumper Cable Assembly shall be 360 inches +/- 3 inches in length.

3.10.4 WEIGHT

The new PITS shall have a weight limit of 37 pounds or less for one lifter in accordance with MIL-STD-1472G Paragraph 5.8.6.3.1 and Table XXXVIII.

3.10.5 COLOR

The color of the new PITS shall be in accordance with FED-STD-595C. Use color number 17925 for white.

3.11 CALIBRATION

The new PITS shall not require calibration.

3.12 ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (E3)

3.12.1 ELECTROMAGNETIC INTERFERENCE (EMI)

The new PITS and new Jumper Cable Assembly shall comply with the following requirements of MIL-STD-461F when operating and testing the upgraded ARS above deck in the F/A-18 electromagnetic environment (EME) on U.S. Navy (USN) aircraft carriers.

(a) CE102 Conducted Emissions, Power Leads, 10 kHz to 10 MHz

(b) CS114 Conducted Susceptibility, Bulk Cable Injection, 10 kHz to 200 MHz

(c) CS115 Conducted Susceptibility, Bulk Cable Injection, Impulse Excitation

(d) CS116 Conducted Susceptibility, Damped Sinusoid Transients, 10 kHz to 100 MHz

(e) RE102 Radiated Emissions, Electric Field, 2 MHz to 18 GHz

(f) RS103 Radiated Susceptibility, Electric Field, 2 MHz to 40 GHz, 200 V/m

3.12.2 ELECTROMAGNETIC COMPATIBILITY (EMC)

The new PITS and new Jumper Cable Assembly shall comply with the following sections of MIL-STD-464C when operating and testing the upgraded ARS above deck in the F/A-18 EME on USN aircraft carriers.

(a) Paragraph 5.3 for external radio frequency (RF) EME.

(b) Paragraph 5.9 for Electromagnetic Radiation Hazards (EMRADHAZ).

(c) Paragraph 5.9.1 for Hazards of Electromagnetic Radiation to Personnel (HERP).

(d) Paragraph 5.9.2 for Hazards of Electromagnetic Radiation to Fuel (HERF).

(e) Paragraph 5.9.3 for Hazards of Electromagnetic Radiation to Ordnance (HERO).

3.13 ENVIRONMENTAL REQUIREMENTS

3.13.1 TEMPERATURE

3.13.1.1 OPERATING TEMPERATURE

The new PITS and new Jumper Cable Assembly shall meet the requirements of this Specification without loss of function or reliability during and after exposure to temperatures from -31 to 49 degrees Celsius (°C) when operating.

3.13.1.2 STORAGE TEMPERATURE

The new PITS and new Jumper Cable Assembly shall meet the requirements of this Specification without loss of function or reliability during and after exposure to temperatures from -46 to 71°C when in storage.

3.13.2 RAIN

The new PITS and new Jumper Cable Assembly shall meet the requirements of this Specification without loss of function or reliability, when operating during and after exposure to rainfall with a rate of 0.2 inch per minute.

3.13.3 SALT FOG

The new PITS and new Jumper Cable Assembly shall meet the requirements of this Specification without loss of function or reliability, when operating during and after exposure to a salt fog atmosphere with a 5% salt (sodium chloride) solution.

3.13.4 DUST

The new PITS and new Jumper Cable Assembly shall meet the requirements of this Specification without loss of function or reliability, during and after exposure to dust encountered during troubleshooting and repair in the ARS maintenace environment. Dust particle size, particle composition, and concentration shall be in accordance with MIL-STD-810G, Method 510.5, Paragraphs 4.1.1.4 and 4.1.1.5.

3.13.5 EXPLOSIVE ATMOSPHERE

The new PITS and new Jumper Cable Assembly shall not be a source for ignition when operated in an explosive atmosphere which contains a fuel vapor mixture.

3.13.6 VIBRATION

The new PITS and new Jumper Cable Assembly shall meet the requirements of this Specification without loss of function or reliability, during and after exposure to Category 20 and 21 vibration environments described in MIL-STD-810G, Table 514.6-I.

3.13.7 MECHANICAL SHOCK

3.13.7.1 TRANSIT DROP

The new PITS and new Jumper Cable Assembly shall physically and functionally withstand the shocks defined in MIL-STD-810G for Procedure IV.

3.13.7.2 BENCH HANDLING

The new PITS and new Jumper Cable Assembly shall physically and functionally withstand the shocks defined in MIL-STD-810G for Procedure VI.

3.14 MATERIALS

3.14.1 HAZARDOUS MATERIALS

Hazardous materials shall be avoided at all times in the design, manufacture, testing, operation, maintenance, and disposal of the new PITS and new Jumper Cable Assembly. Where hazardous materials cannot be avoided, their use shall be justified by the Contractor and approved by the Government. A hazardous material is any material that due to its chemical, physical, or biological nature causes safety, public health, or environmental concerns. This includes but is not limited to the following materials:

(a) Materials regulated as a hazardous material per 49 CFR 173.2.

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

(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.

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

(e) Materials identified in the Clean Air Act as a Hazardous Air Pollutant per 40 CFR 63.

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

A and B.

(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.

(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.

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

3.14.2 RESTRICTED MATERIALS

The following hazardous materials are prohibited in the design, manufacture, testing, operation, and maintenance of the new PITS and new Jumper Cable Assembly: Asbestos, Class I ODS, Class II ODS, Hexavalent Chromium, and Polychlorinated Biphenyls (PCBs).

3.14.3 TARGETED MATERIALS

The following hazardous materials will require NAVAIR approval for use in the new PITS and new Jumper Cable Assembly: Arsenic & Arsenic Compounds, Benzene, Beryllium & Beryllium Compounds, Cadmium & Cadmium Compounds, Chloroform, Chromium & 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 the Contractor can document that no technically feasible alternative is viable.

3.14.4 METAL ALLOYS

Chromium or nickel as a constituent of metal alloys is exempted.

3.14.5 LEAD

Lead as a constituent of lead solder is exempted.

3.14.6 PROTECTIVE COATINGS

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. On components where powder coating is not employed, the unit shall be finished and coated using a MIL-DTL-53022 Type II epoxy primer and a MIL-PRF-85285 Type II polyurethane topcoat.

3.14.7 OTHER RESTRICTED MATERIALS AND GASES

The new PITS and new Jumper Cable Assembly shall not contain materials that promote the premature failure of the equipment or that present a health hazard under normal use or storage conditions as specified below.

3.14.7.1 FLAMMABLE MATERIALS

The new PITS and new Jumper Cable Assembly shall not contain materials that are combustible at operating or storage temperatures.

3.14.7.2 EXPLOSIVE MATERIALS

The new PITS and new Jumper Cable Assembly shall not contain materials that explode at operating or storage temperatures.

3.14.8 FUNGUS RESISTANCE

The new PITS and new Jumper Cable Assembly shall not contain materials that provide nutrients for the growth of fungus. General moisture or fungus resistance coating of assembled part, wire, or solder joints is not acceptable.

3.15 NAMEPLATES AND PRODUCT MARKING

3.15.1 PLACARDS

Placards shall be constructed in accordance with MIL-STD-130N and MIL-DTL-15024F. Each identification device shall be either Type A, B, or L with color style III.

3.15.2 ITEM UNIQUE IDENTIFICATION (IUID) MARKING

The new PITS and new Jumper Cable Assembly shall be marked per MIL-STD-130N and in a manner that does not adversely affect safety or performance.

3.15.3 REFERENCE DESIGNATIONS

Reference designations shall be used to identify each part for its particular circuit application.

Sub-miniaturized and non repairable assemblies need not be marked with reference designators.

Reference designator usage shall be in accordance with IEEE-STD-315 as applicable.

3.15.4 WARNING MARKINGS

Warning markings shall warn of the location, the nature, and the extent of a hazard. Letters of warning markings shall be clearly legible gothic capitals. Warning labels shall have high contrast between the letter and background colors. The markings shall be as permanent as normal life expectancy of the test equipment, and located as close as possible to the point of danger.

3.15.5 EQUIPMENT IDENTIFICATION

An equipment identification plate shall be permanently affixed to the equipment and shall contain the information provided in (a) through (h) in accordance with MIL-STD-130.

Equipment identification shall include the items as specified below.

(a) Nomenclature

(b) Manufacturer's Commercial And Government Entity (CAGE) code

(c) Serial number

(d) Part number

(e) Enterprise identifier for IUID (DODACC: N68335)

(f) Acquisition instrument identification number- Contract Number

(g) National Stock Number (NSN)

(h) IUID marking

3.16 WORKMANSHIP

3.16.1 CLEANING

After fabrication, parts and assembled equipment shall be cleaned of smudges; loose, spattered, or excess solder, weld metal; metal chips and mold release agents; or any other foreign material, which might impair intended operation, function, appearance, or service life of the equipment.

3.16.2 THREADED PARTS OR DEVICES

(a) Screws, nuts, bolts and fittings shall show no evidence of cross threading, mutilation, or detrimental or hazardous burrs, and shall be firmly secured.

(b) All threaded devices shall be U.S. and/or metric thread sizes only.

(c) Fasteners used for general assembly shall have positive locking features, or shall be used in conjunction with a thread locking compound.

3.16.3 SOLDERING

Soldering shall be in accordance with ANSI/J-STD-001A.

3.16.4 CONNECTORS

(a) Each connector shall be identified by appropriately numbered and designated "J" or "P" reference designators in accordance with IEEE-Std-200.

(b) Each connector shall have a removable endcap. To avoid misplacing it when it is removed from a connector, each endcap shall be securely tethered to the connector's backshell or mounting plate using a lanyard.

(c) Special tools required for connector repair that are not available at the operational maintenance facility shall be identified.

3.16.5 WIRES AND CABLE ASSEMBLIES

(a) Wires and cables shall be secured and insulated to avoid causing shorts in exposed current carrying parts, and prevent contact with rough or irregular surfaces and sharp edges.

(b) Each cable assembly shall be completely repairable using standard tools.

(c) A continuous EMI shield shall be applied over the entire wire assembly in each cable assembly.

(d) The EMI shield shall be secured to prevent fraying.

(e) The EMI shield shall be electrically grounded to the backshell of each connector in the cable assembly.

(f) Neither the outer EMI shield nor the connector assembly shall be used as a signal ground path in the cable assemblies.

(g) A strain relief shall be used with each connector to prevent it from separating from the cable during normal usage.

3.16.6 GROUNDING

Electrical grounding shall be in accordance with MIL-STD-704 and the following:

(a) Provide effective shielding for signal circuits.

(b) Minimize EMI.

(c) Protect personnel from electrical hazards.

3.17 SAFETY

(a) Design shall be in accordance with MIL-STD-882E System Safety Program Requirements.

(b) Design shall comply with safety guidelines defined in MIL-HDBK-454B Guideline 1.

(c) Design shall contain no single point failures which would result in a MIL-STD-882

Category I or II hazard (NAVSEAINST 8020.6E).

3.18 MEAN TIME BETWEEN FAILURE (MTBF)

The new PITS shall have a MTBF of 3500 hours or greater in a Naval Unsheltered (NU) environment as defined in MIL-HDBK-217.

4.0 VERIFICATION

The Contractor shall be responsible for the performance of all inspection requirements specified herein. The Contractor may use his or any other facilities suitable for the performance of the inspection requirements specified herein. The Government reserves the right to witness or separately perform all tests specified or otherwise inspect any or all tests. The absence of any verification requirement in this Specification shall not relieve the Contractor of the responsibility of ensuring all deliverables submitted to the Government for acceptance comply with all the requirements of Section 3 herein or the requirements of the contract.

4.1 VERIFICATION COMPLIANCE

The Contractor shall be considered compliant with the requirements upon written approval from the Government. The Contractor shall be considered non-compliant upon failure of a unit to meet any of the requirements specified therein. In the event of verification non-compliance, the Contractor shall: 1) document the failure, and 2) identify and provide to the Government in writing the root cause for the failure, the associated effects the failure has on the unit’s ability to comply with the requirements of this document, and the corresponding corrective action needed to correct the failure in the affected units. Unless specifically authorized in writing by the Government, deliverables will not be accepted by the Government until: (1) concurrence has been received from the designated Government Inspector that the proposed corrective action has been implemented; (2) a unit incorporating the resultant remedies has passed verification; and (3) the applicable verification report has been submitted and approved IAW the corresponding

CDRL.

4.2 TEST MODES

4.2.1 OPERATING

When the test mode is "Operating", the top section of the PITS shall be detached from the bottom section; all cables required for the test shall be attached to the PITS; and the PITS shall be powered in accordance with this Specification.

4.2.2 STORAGE

When the test mode is "Storage", the top section of the PITS shall be attached to the bottom section, and the PITS Cable Set stored in the top section as described in this Specfication.

4.3 SYSTEM OPERATIONAL TEST

Following each environmental test, the PITS Self-Test function and a voltmeter shall be used to verify the unit is operational, and the PITS internal power supply is providing 28 VDC power to the J3 port and the Control Panel cavity. Any failure of this test shall result in a failure of the environmental test which it follows.

4.4 SPECIAL TESTS AND EXAMINATIONS

4.4.1 SYSTEM INSPECTION

This test shall involve inspection of the new PITS and new Jumper Cable Assembly for physical characteristic and workmanship requirements, as well as processing accumulated data obtained from separately prepared documents/reports.

Paragraph Requirement/Description

3.2 Switches and Circuit Breakers

3.3 Indicators

3.4 Ports

3.5 PITS Cable Set

3.6 Jumper Cable Assembly

3.7.2 Aircraft Wiring

3.10 Physical Characteristics

3.10.1 Electronics Enclosure (Bottom Section)

3.10.2 Storage Lid (Top Section)

3.10.3 Dimensions

3.10.4 Weight

3.10.5 Color

3.14.1 Hazardous Materials

3.14.2 Restricted Materials

3.14.3 Targeted Materials

3.14.4 Metal Alloys

3.14.5 Lead

3.14.6 Protective Coatings

3.14.7 Other Restricted Materials and Gases

3.14.7.1 Flammable Materials

3.14.7.2 Explosive Materials

3.14.8 Fungus Resistance

3.15.1 Placards

3.15.2 Item Unique Identification (IUID) Marking

3.15.3 Reference Designations

3.15.4 Warning Markings

3.15.5 Equipment Identification

3.16.1 Cleaning

3.16.2 Threaded Parts or Devices

3.16.3 Soldering

3.16.4 Connectors

3.16.5 Wires and Cable Assemblies

3.16.6 Grounding

4.4.2 SYSTEM PERFORMANCE TEST

This test shall verify the operation and performance of the new PITS and new Jumper Cable Assembly. Testing shall involve operation using instrumentation or other special test equipment to collect data for subsequent review.

3.0 Requirements

3.1 Test Capabilities

3.1.1 Aircraft Fuel To/From Test

3.1.2 Lamp Test

3.1.3 Self Test

4.4.3 FUNCTIONAL TEST (DEMONSTRATION)

The functional test shall demonstrate overall functionality of the new PITS and new Jumper Cable Assembly. Demonstration shall rely on observable functional operation.

3.2.1 Circuit Breaker (CB1)

3.2.2 Power Switch

3.2.3 Lamp Test Switch

3.3.1 Aircraft Fuel To/From Indicators

3.3.2 115 VAC Power Indicator

3.3.3 28 VDC Power Indicator

3.3.4 15 VDC Power Indicator

3.3.5 Drogue Stowed Indicator

3.3.6 Self Test Fault Indicator

3.3.7 Hi-Level Float Switch Indicator

3.4.1 J1 Ground Stud

3.4.2 J2 Power Port

3.4.3 J3 UUT Port

3.7.1 External Cables

3.7.3 ARS

3.7.4 Control Panel

3.8 Input Power

3.9 Output Power

3.11 Calibration

4.4.4 RELIABILITY ANALYSIS

The mean-time between failure of the new PITS shall be verified by reliability prediction analysis.

3.18 Mean Time Between Failure (MTBF)

4.4.5 ELECTROMAGNETIC INTERFERENCE (EMI)

The new PITS and new Jumper Cable Assembly shall pass the tests listed in the table below without suffering permanent damage or an interruption in operation.

Category Method Requirement

Conducted Emissions MIL-STD-461F, CE102 Power Leads, 10 kHz to 10 MHz

Conducted Susceptibility

MIL-STD-461F, CS101 Power Leads, 30 Hz to 150 kHz

MIL-STD-461F, CS114

Bulk Cable Injection, 10 kHz to 200 MHz, Curve 5

MIL-STD-461F, CS115 Bulk Cable Injection, Impulse Excitation

MIL-STD-461F, CS116

Cables and Power Leads, Damped Sinusoidal Transients, 10 kHz to 100 MHz

Radiated Emissions MIL-STD-461F, RE101 Magnetic Field, 30 Hz to 100 kHz

MIL-STD-461F, RE102 Electric Field, 10 kHz to 18 GHz

Radiated Susceptibility

MIL-STD-461F, RS101

Magnetic Field, 30 Hz to 100 kHz, Figure

RS101-1

MIL-STD-461F, RS103 Electric Field, 2 MHz to 40 GHz, 200 V/m

3.12.1 Electromagnetic Interference (EMI)

4.4.6 ELECTROMAGNETIC COMPATIBILITY (EMC)

The new PITS and new Jumper Cable Assembly shall pass the tests listed in the table below without suffering permanent damage or an interruption in operation.

Category Method Requirement

External RF EME MIL-STD-464C, Paragraph 5.3

F/A-18 above deck EME on USN aircraft carrier

Electromagnetic Radiation Hazards (EMRADHAZ)

MIL-STD-464C, Paragraph 5.9

Hazards of Electromagnetic Radiation to Personnel (HERP)

MIL-STD-464C, Paragraph 5.9.1

Hazards of Electromagnetic Radiation to Fuel (HERF)

MIL-STD-464C, Paragraph 5.9.2

Hazards of Electromagnetic Radiation to Ordnance (HERO)

MIL-STD-464C, Paragraph 5.9.3

3.12.2 Electromagnetic Compatibility (EMC)

4.4.7 HIGH TEMPERATURE

The new PITS and new Jumper Cable Assembly shall pass MIL-STD-810G, Method 501.5, Procedure I (Storage) when exposed (unsheltered) to temperatures from 33 to 71°C for two (2) 8-hour cycles. The new PITS and new Jumper Cable Assembly shall pass MIL-STD-810G, Method 501.5, Procedure II (Operating) when exposed (unsheltered) to temperatures from 32 to 49°C for two (2) 8-hour cycles.

3.13.1.1 Operating Temperature

3.13.1.2 Storage Temperature

4.3.9 LOW TEMPERATURE

The new PITS and new Jumper Cable Assembly shall pass MIL-STD-810G, Method 502.5, Procedure I (Storage) when exposed (unsheltered) to temperatures from -37 to -46°C for 8 hours.

The new PITS and new Jumper Cable Assembly shall pass MIL-STD-810G, Method 502.5, Procedure II (Operating) when exposed (unsheltered) to temperatures from -21 to -31°C for 8 hours.

3.13.1.1 Operating Temperature

3.13.1.2 Storage Temperature

4.3.10 RAIN

The new PITS and new Jumper Cable Assembly shall pass MIL-STD-810G, Method 506.5, Procedure I (Blowing Rain).

3.13.2 Rain

4.3.11 SALT FOG

The new PITS and new Jumper Cable Assembly shall pass MIL-STD-810G, Method 509.5 while operating in an atmosphere with a salt solution concentration of 5% +/- 1%. The salt fog exposure shall be in accordance with MIL-STD-810G, Method 509.5, Paragraph 2.2.3 with alternating 24-hour periods of salt fog exposure and drying conditions for a minimum of four 24-hour periods (two wet and two dry).

3.13.3 Salt Fog

4.3.12 DUST

The new PITS and new Jumper Cable Assembly shall pass MIL-STD-810G, Method 510.5, Procedure I (Blowing Dust) while operating when exposed to a dust concentration, particle size, and particle composition in accordance with MIL-STD-810G, Method 510.5, Paragraphs

4.1.1.4 and 4.1.1.5.

3.13.4 Dust

4.3.13 EXPLOSIVE ATMOSPHERE

The new PITS and new Jumper Cable Assembly shall pass MIL-STD-810G, Method 511.5, Procedure I (Explosive Atmosphere) while operating in an explosive atmosphere which contains a fuel vapor mixture.

3.13.5 Explosive Atmosphere

4.3.14 VIBRATION

The new PITS and new Jumper Cable Assembly shall pass MIL-STD-810G, Method 514.6 for Category 20 and 21 vibration environments described in MIL-STD-810G, Table 514.6-I.

3.13.6 Vibration

4.3.15 TRANSIT DROP

The new PITS and new Jumper Cable Assembly shall pass MIL-STD-810G, Method 516.6, Procedure IV. Any damage that affects the functionality of the unit shall be considered a failure of this test. After completion of this test, the operational test specified in paragraph 4.3 shall be performed without any failures.

3.13.7.1 Transit Drop

4.3.16 BENCH HANDLING

The new PITS and new Jumper Cable Assembly shall pass MIL-STD-810G, Method 516.6, Procedure VI. After completion of this test, the operational tests specified in paragraph 4.3 shall be performed without any failures.

3.13.7.2 Bench Handling

4.3.17 SAFETY ASSESSMENT

Verify that the safety design requirements and considerations have been met by performing a Safety Compliance Assessment in accordance with MIL-STD-882E, Task 402.

3.17 Safety

4.4 REQUIREMENTS CROSS REFERENCE

Appendix A contains the Verification Cross Reference Matrix (VCRM) which establishes the test stage at which each requirement specified in this document is to be verified. The test stages are Qualification Test (QT) and Acceptance Test (AT). Refer to the Statement of Work for the definitions of these stages.

5.0 PRESERVATION, PACKAGING, AND MARKING

Preservation and packaging methods shall be in accordance with MIL-STD-2073 to prevent corrosion, deterioration, and physical damage during storage, multiple handling and shipments associated with the military distribution system. Markings shall be in accordance with MIL-

STD-129P.

1 June 2015

APPENDIX A

Requirements Verification Cross Reference Matrix (VCRM)

A-1

Section 3 Section 4

Paragraph Requirement PITS Verification

Method Paragraph

3.0 Requirements QT Test 4.4.2

3.1 Test Capabilities QT Test 4.4.2

3.1.1 Fuel Transfer Test QT Test 4.4.2

3.1.2 Lamp Test QT Test 4.4.2

3.1.3 Self Test QT Test 4.4.2

3.2 Switches and Circuit Breakers QT Inspect 4.4.1

3.2.1 Circuit Breaker (CB1) QT Test 4.4.3

3.2.2 Power Switch QT Test 4.4.3

3.2.3 Lamp Test Switch QT Test 4.4.3

3.3 Indicators QT Inspect 4.4.1

3.3.1 Aircraft Fuel To/From Indicators QT Test 4.4.3

3.3.2 115 VAC Power Indicator QT Test 4.4.3

3.3.3 28 VDC Power Indicator QT Test 4.4.3

3.3.4 15 VDC Power Indicator QT Test 4.4.3

3.3.5 Drogue Stowed Indicator QT Test 4.4.3

3.3.6 Self Test Fault Indicator QT Test 4.4.3

3.3.7 Hi-Level Float Switch Indicator QT Test 4.4.3

3.4 Ports QT Inspect 4.4.1

3.4.1 J1 Ground Stud QT Test 4.4.3

3.4.2 J2 Power Port QT Test 4.4.3

3.4.3 J3 UUT Port QT Test 4.4.3

3.5 PITS Cable Set QT Inspect 4.4.1

3.6 Jumper Cable Assembly QT Inspect 4.4.1

3.7 Connectivity N/A

3.7.1 External Cables QT Test 4.4.3

3.7.2 Aircraft Wiring QT Inspect 4.4.1

3.7.3 ARS QT Test 4.4.3

3.7.4 Control Panel QT Test 4.4.3

3.8 Input Power QT Test 4.4.3

3.9 Output Power QT Test 4.4.3

3.10 Physical Characteristics QT Inspect 4.4.1

3.10.1 Electronics Enclosure (Bottom Section) QT Inspect 4.4.1

3.10.2 Storage Lid (Top Section) QT Inspect 4.4.1

1 June 2015

A-2

Paragraph Requirement PITS Verification

Method Paragraph

3.10.3 Dimensions QT Inspect 4.4.1

3.10.4 Weight QT Inspect 4.4.1

3.10.5 Color QT Inspect 4.4.1

3.11 Calibration QT Test 4.4.3

3.12 Electromagnetic Environmental Effects (E3) N/A

3.12.1 Electromagnetic Interference (EMI) QT Test 4.4.6

3.12.2 Electromagnetic Compatibility (EMC) QT Test 4.4.7

3.13 Environmental Requirements N/A

3.13.1 Temperature N/A

3.13.1.1 Operating Temperature QT Test 4.4.8 & 4.4.9

3.13.1.2 Storage Temperature QT Test 4.4.8 & 4.4.9

3.13.2 Rain QT Test 4.4.10

3.13.3 Salt Fog QT Test 4.4.11

3.13.4 Sand and Dust QT Test 4.4.12

3.13.5 Explosive Atmosphere QT Test 4.4.13

3.13.6 Vibration QT Test 4.4.14

3.13.7 Mechanical Shock N/A

3.13.7.1 Transit Drop QT Test 4.4.15

3.13.7.2 Bench Handling QT Test 4.4.16

3.14 Materials N/A

3.14.1 Hazardous Materials QT Inspect 4.4.1

3.14.2 Restricted Materials QT Inspect 4.4.1

3.14.3 Targeted Materials QT Inspect 4.4.1

3.14.4 Metal Alloys QT Inspect 4.4.1

3.14.5 Lead QT Inspect 4.4.1

3.14.6 Protective Coatings QT Inspect 4.4.1

3.14.7 Other Restricted Materials and Gases QT Inspect 4.4.1

3.14.7.1 Flammable Materials QT Inspect 4.4.1

3.14.7.2 Explosive Materials QT Inspect 4.4.1

3.14.8 Fungus Resistance QT Inspect 4.4.1

3.15 Nameplates and Product Marking N/A

3.15.1 Placards QT Inspect 4.4.1

1 June 2015

A-3

Paragraph Requirement PITS Verification

Method Paragraph

3.15.2 Item Unique Identification (IUID) Marking QT Inspect 4.4.1

3.15.3 Reference Designations QT Inspect 4.4.1

3.15.4 Warning Markings QT Inspect 4.4.1

3.15.5 Equipment Identification QT Inspect 4.4.1

3.16 Workmanship N/A

3.16.1 Cleaning QT Inspect 4.4.1

3.16.2 Threaded Parts or Devices QT Inspect 4.4.1

3.16.3 Soldering QT Inspect 4.4.1

3.16.4 Connectors QT Inspect 4.4.1

3.16.5 Wires and Cable Assemblies QT Inspect 4.4.1

3.16.6 Grounding QT Inspect 4.4.1

3.17 Safety QT Analysis 4.4.17

3.18 Mean Time Between Failure (MTBF) QT Analysis 4.4.4

3.19 Design for Maintainability QT Analysis 4.4.5