ILS-420 Section C.pdf

C.1 SCOPE OF CONTRACT

C.2 ORDER OF PRECEDENCE

C.3 APPLICABLE DOCUMENTS

C.3.2 Federal, DoD, Military Standards and Specifications

C.3.3 Other Documents

C.4 REQUIREMENTS

C.4.1 Equipment Configurations

C.4.1.1 CLIN X001 – Complete Dual Equipment Dual Frequency (DEDF) Instrument Landing System. 8

C.4.1.2 CLIN X002 – Complete Dual Equipment Dual Frequency Localizer System (DEDF

LOC). 9

C.4.1.3 CLIN X003 – Complete Dual Equipment Dual Frequency Glide Slope System (DEDF

CEGS). 10

C.4.1.4 CLIN X004 – Single Equipment Single Frequency Localizer Cabinet with Spares

(SESF LOC). 11

C.4.1.5 CLIN X005 – Single Equipment Dual Frequency Localizer Cabinet with Spares (SEDF

LOC). 11

C.4.1.6 CLIN X006 – Dual Equipment Single Frequency Localizer Cabinet with Spares (DESF

LOC). 11

C.4.1.7 CLIN X007 – Dual Equipment Dual Frequency Localizer Cabinet with Spares (DEDF

LOC). 11

C.4.1.8 CLIN X008 – 8 Element Single Frequency Localizer Antenna Array (LOC 8 Element SF Ant; DUCU Enclosure)

C.4.1.9 CLIN X009 – 14 Element Single Frequency Localizer Antenna Array (LOC 14 Element SF Ant; DUCU Enclosure)

C.4.1.10 CLIN X010 – 14/10 Dual Frequency Localizer Antenna Array (14/10-EL DF LOC; DUCU Enclosure). 12

C.4.1.11 CLIN X011 – 20/10 Dual Frequency Localizer Antenna Array (20/10, DF LOC; DUCU Enclosure). 12

C.4.1.12 CLIN X012 – Dual Equipment Dual Frequency Capture Effect Glide Slope Cabinet with Spares (DEDF CEGS)

C.4.1.13 CLIN X013 – Single Equipment Dual Frequency Capture Effect Glide Slope Cabinet with Spares (SEDF CEGS)

C.4.1.14 CLIN X014 – Dual Equipment Single Frequency Null Reference Glide Slope Cabinet with Spares (DESF NRGS)

C.4.1.15 CLIN X015 – Single Equipment Single Frequency Null Reference Glide Slope Cabinet with Spares (SESF NRGS)

C.4.1.16 CLIN X016 – Dual Equipment Single Frequency Side-Band Reference Glide Slope Cabinet with Spares (DESF SBRGS)

C.4.1.17 CLIN X017 - Single Equipment Single Frequency Side-Band Reference Glide Slope Cabinet with Spares (SESF SBRGS)

C.4.1.18 CLIN X018a – Fall Prevention System for 45’ Glide Slope Tower – FAA Approved (aka Fall Prevention Kit, 45')

C.4.1.19 CLIN X018b – Glide Slope Tower Working Platform (3 Piece)

C.4.1.20 CLIN X019 – Radio Guardian – 400 (analog)

C.4.1.21 CLIN X020 – Portable ILS Receiver (PIR)

C.4.1.22 CLIN X021 – Remote Maintenance Monitor (RMM) Set

C.4.1.23 CLIN X022 – RMM Tower Computer

C.4.1.24 CLIN X023 – RMM LED Monitor

C.4.1.25 CLIN X024 – Serial Interface Adapter

C.4.1.26 CLIN X025 – X028 – Reserved

C.4.1.27 CLIN X029 – One Glide Slope Tower Middle Section, 5 ft. Painted White

C.4.1.28 CLIN X030 – One Glide Slope Tower Middle Section, 10 ft. Painted White

C.4.1.29 CLIN X031 – One Glide Slope Tower Middle Section, 5 ft. Painted Aviation Orange . 15

C.4.1.30 CLIN X032 – One Glide Slope Tower Middle Section, 10 ft. Painted Aviation Orange 15

C.4.1.31 CLIN X033 – One Glide Slope Tower Top Section, 5 ft. Painted White

C.4.1.32 CLIN X034 – One Glide Slope Tower Top Section, 10 ft. Painted White

C.4.1.33 CLIN X035 – One Glide Slope Tower Top Section, 5 ft. Painted Aviation Orange

C.4.1.34 CLIN X036 – One Glide Slope Tower Top Section, 10 ft. Painted Aviation Orange

C.4.1.35 CLIN X037 – X046 – Reserved

C.4.1.36 CLIN X047 – Log-Periodic Dipole Snow Cover Kit

C.4.1.37 CLIN X048 - Log-Periodic Dipole Antenna (single antenna)

C.4.1.38 CLIN X049 – Dual Equipment Receiver FFM with Dual YAGI Antenna

C.4.1.39 CLIN X050a – Single Glide Slope Antenna, without Removable Tray

C.4.1.40 CLIN X050b – Single Glide Slope Antenna, with Removable Tray

C.4.1.41 CLIN X051 – Localizer Antenna (Single Antenna)

C.4.1.42 CLIN X052 – 14/20 Instrument Landing System Conversion Kit

C.4.1.43 CLIN X053 – Capture Effect Glide Slope Antenna System (Removable Tray)

C.4.1.44 CLIN X054 – Null Reference (NR) Glide Slope Antenna System (Removable Tray). .. 17

C.4.1.45 CLIN X055 – Side-Band Reference Glide Slope Antenna System (Removable Tray). 17

C.4.1.46 CLIN X056 – Glide Slope Antenna Heater Kit

C.4.1.47 CLIN X057 – Reserved

C.4.1.48 CLIN X058 – Remote Control Subsystem with Spares

C.4.1.49 CLIN X059 – Remote Status Control Unit

C.4.1.50 CLIN X060 – Remote Status and Interlock Control

C.4.1.51 CLIN X061 – Base Modem Kit with Spares

C.4.1.52 CLIN X062 – Site Modem Kit with Spares

C.4.1.53 CLIN X063 – Modem/Radio 19” Rack Shelf

C.4.1.54 CLIN X064 – Communication Display Interface Circuit Card Assembly

C.4.1.55 CLIN X065 – Universal Local Control Status Unit

C.4.1.56 CLIN X066 – ILS Monitor Receiver

C.4.1.57 CLIN X067-X068 – Reserved

C.4.1.58 CLIN X069 – Base Radio Kit with Spares (One to multilink, Digital)

C.4.1.59 CLIN X070 – Site Radio Kit with Spares (One to multilink, Digital)

C.4.1.60 CLIN X071 – Localizer Leg Extension Kit (3 ft.)

C.4.1.61 CLIN X072 – Installer Workshop

C.4.1.62 CLIN X073 – End Fire Glide Slope Interface for ILS-420

C.4.1.63 CLIN X074 - Enlarged Distribution Unit, Controller Unit (DUCU), Wattmeter Interface Card (WIC), and Guide Rail Enhancement

C.4.1.64 CLIN X075 – X076 – Reserved

C.4.1.65 CLIN X077– Engineering Support Service

C.4.1.66 CLIN X078 – Customer Support Services

C.4.1.67 CLIN X079 – CDLS

As described in Section C.4.9.3

C.4.1.68 CLIN X080a – Program Management, Conferences, Reviews, Meetings

C.4.1.69 CLIN X080b – Technical Interchange Meetings

C.4.1.70 CLIN X081 – ILS-420 Installation Support Service

C.4.2 Program Management

C.4.2.1 Program Management Organization and Plan

CDRL 001: Program Management Plan

C.4.2.2 Meetings, Conferences and Reviews

C.4.2.3 Post Award Conference

C.4.2.4 Technical Interchange Meetings

C.4.3 Quality Assurance

CDRL 002: Quality System Plan

C.4.4 Configuration Management

C.4.4.1 Configuration Management (CM) Planning

CDRL 003: Configuration Management Plan

C.4.4.2 Configuration Item (CI) Identification

C.4.4.3 Software Configuration Items

C.4.4.4 Configuration Change Control

C.4.4.5 Engineering Change Proposals (ECP)

CDRL 004: Engineering Change Proposals

C.4.4.6 Class I and II Change Definition

CDRL 005: Requests for Deviations

C.4.4.7 Configuration Status Accounting (CSAR)

C.4.4.8 Configuration Validation and Audits

CDRL 006: Configuration Audit Plan

CDRL 007: Functional Configuration Audit Traceability Matrix

CDRL 008: Functional Configuration Audit Report

CDRL 009: Physical Configuration Audit (PCA) Report

C.4.5 SYSTEM TEST AND EVALUATION

C.4.5.1 Production Acceptance Test

CDRL 010: PAT Reports

C.4.5.2 Type Test

CDRL 011: Type Test Report

C.4.5.3 Installation and Checkout Support

C.4.5.4 Contractor Test Coordination

C.4.5.5 Test Logs

C.4.5.6 Problem Reporting

C.4.5.7 Re-testing

C.4.5.8 Regression Testing

CDRL 012: Regression Test Plan

C.4.5.9 Test Equipment

C.4.6 System Safety Requirements

CDRL 013: Software Configuration Management Plan

CDRL 014: Personnel Safety Hazard Analysis Report

C.4.7 System Software Support

CDRL 015: Software Development Plan

C.4.8 INTERFACE REQUIREMENTS DOCUMENTS

CDRL 016: Interface Control Document for the Remote Monitoring Logging System

CDRL 017: Interface Control Document for the Maintenance Data Terminal (MDT)

CDRL 018: Interface Control Document for the Remote Control Subsystem (RCS)

C.4.9 National Airspace Integrated Logistics Supports (NAILS)

C.4.9.1 NAILS Management

C.4.9.2 Provisioning

CDRL 019: Logistics Management Information (LMI) Data Product

CDRL 020: DMSMS Health Assessment Report

C.4.9.3 Depot Level Maintenance

CDRL 021: CDLS Activity and Repair Status Report

CDRL 022: Depot Maintenance Transition Plan

C.4.9.4 Technical Instruction Books

CDRL 023: Technical Instruction Book

C.4.9.5 Technical Data Package

CDRL 024: Technical Data Package

C.4.10 ILS Program Support Services

C.4.10.1 Customer Support Services

C.4.10.2 Engineering Support Service

C.4.10.3 ILS-420 Installation Support Service

C.4.10.4 Installation Workshop

Section C – Statement of Work

C.1 SCOPE OF CONTRACT

The Contractor must deliver commercial/non-developmental item (NDI) or modified commercial/NDI Category I/II/III Instrument Landing Systems (ILS) meeting the requirements of FAA specification FAA-E-2970. The Contractor must deliver all equipment, spare parts, documentation, and services in accordance with the requirements of this Statement of Work (SOW) and all other terms and conditions of the contract at the prices listed in Section B thereof.

C.2 ORDER OF PRECEDENCE

In case of conflict between provisions of this contract, the following order of precedence is established.

a. Schedule – Sections A – H

b. Contract Clauses - Section I

c. Attachments – Section J, including J-3 (FAA specification FAA-E-2970) and J-4 (Corrections and Tailoring: FAA-E-2970)

d. Other FAA Specifications

e. Other FAA Documents (other than Specifications)

f. FAA Standards and Orders

g. DoD Standards and Orders

h. Other documents incorporated by reference

C.3 APPLICABLE DOCUMENTS

a. The following specifications, handbooks, orders, standards, and drawings form a part of this SOW and are applicable to the extent specified herein. Unless otherwise stated, the latest version of these documents as of the contract date must apply. Changes to any applicable document during this contract period of performance will not impact or affect this contract unless the FAA issues a contractual modification. In the event of conflict between this SOW and any of the applicable documents cited below, the provisions of this SOW must apply.

b. Copies of FAA specifications and interface documents may be obtained from the Federal Aviation Administration, Headquarters Public Inquiry Center APA-230, 800 Independence Avenue SW, Washington, DC 20591, 202-267-3484. Requests should fully identify material desired and cite the solicitation or contract number.

c. Requests for copies of documents not covered in the preceding paragraph should be addressed to the Contracting Officer. Requests should fully identify material desired and cite the solicitation or contract number.

d. Military Standards and Specifications can be ordered from the Department of Defense Single Stock Point (DODSSP), Building 4/Section D, 700 Robbins Avenue, Philadelphia, PA 19111-5098. Information is available at their website, http://www.dodssp.daps.mil

e. Copies of ANSI/ASQC-Q-9001-2000 can be obtained from the following source: American Society for Quality Control 611 East Wisconsin Avenue P.O. Box 3005; Milwaukee, Wisconsin 53201-3005. Phones: (414) 272-8575 or (800) 248-1946. The Fax is: (414) 272-1734.

f. Copies of the Acquisition Management System Test and Evaluation Process Guidelines are http://www.dodssp.daps.mil/ available in the FAA Acquisition System Toolset (FAST). The on-line internet address of FAST is: http://FAST.faa.gov

C.3.1 FAA Documents

FAA-D-2494 Rev. B Technical Instruction Book Manuscript: Electronic, Electrical, and Mechanical Equipment

FAA-E-2970

Performance Specification Category I/II/III Instrument Landing System (ILS)

FAA-G-2100G Electronic Equipment, General Requirement

FAA-STD-002E Standard Engineering Drawing Preparation

FAA-STD-025E Preparation of Interface Documents

FAA-STD-026A

Software Development for the National Airspace System, (NAS)

FAA-STD-028C Contract Training Program

FAA-STD-1293C

Servicing Standard and Test Requirements for Ground Electronics Equipment

FAA Order 1800.66 Configuration Management Policy

FAA Order 3900.19 FAA Occupational Safety and Health (OSH) Policy

Order JO 6750.49A Maintenance of Instrument Landing Systems (ILS) Facilities

Order 8040.4 Safety Risk Management Policy

ASD-100-SSE-1 Rev 9.0 NAS Modernization System Safety Program

* New to the Bridge Contract

C.3.2 Federal, DoD, Military Standards and Specifications

MIL-DTL-31000B Technical Data Packages

MIL-STD-882D Standard Practice for System Safety

MIL-HDBK-781A

Reliability Test Methods, Plans and Environments for Engineering Development, Qualification, and Production

MIL-STD-2073-1D DOD Standard Practice for Military Packaging

MIL-HDBK-61A Configuration Management

MIL-PRF-49506 Logistics Management Information http://fast.faa.gov/

C.3.3 Other Documents

ANSI/EIA-649

National Consensus Standard for Configuration Management

*AS9100

Quality Management Systems-Requirements for Aviation, Space and Defense Organizations

ASTM D3951-98 Standard Practice for Commercial Packaging

ISO/IEC 15438 Bar Code Symbology Specifications 2015

29 CFR 1910 Occupational Safety and Health Standards

RTCA DO-178C

Software Considerations in Airborne Systems and Equipment Certification

RTCA DO-278

Software Integrity Assurance Considerations for Communication, Navigation, Surveillance, and Air Traffic Management (CNS/ATM) Systems

SAE ARP-4754

Aerospace Recommended Practice: Certification Considerations for Highly Integrated or Complex Aircraft Systems, Society of Automotive Engineers (SAE)

SAE ARP-4761

Aerospace Recommended Practice: Guidelines and Methods for Conducting the Safety Assessment Process on Civil Airborne Systems and Equipment, SAE

* New to the Bridge Contract

C.4 REQUIREMENTS

C.4.1 Equipment Configurations

C.4.1.1 CLIN X001 – Complete Dual Equipment Dual Frequency (DEDF) Instrument Landing System.

Includes the following:

Localizer Electronic Subsystem Dual Equipment Dual Frequency - Electronic Subsystem, Shelter Environmental Sensor Kit, Battery Kit without Battery, Spare Localizer-Specific Modular Power Amplifier (MODPA), and two Localizer and Thales Maintenance Data Terminal Instruction Books, Wattmeter Test Panel;

14/10 Localizer Antenna Subsystem Medium Aperture Dual Frequency Capture Effect – Antennas, Antenna Shelter J-box, Installation Kit, and two Antenna Instruction Books;

Note: Civil kits are not supplied (i.e. concrete anchor bolts, leveling nuts, washers, etc.);

Full Spares for Localizer & Glide Slope Dual Equipment Configuration - Synthesizers, Localizer/Glide Slope Uncommitted Cards (LGX), Interface Assemblies, Executive Combining Units (ECU), Stand-By On-Air Combiners (SOAC), Local Control Panels (LCP), AC-DC Converters, DC- DC Converters, Low Voltage Sensors (LVS), Transient Suppressors, Wattmeter Interface Cards (WIC), Fuses, and Transfer Switches;

Unique Spares – Localizer MODPA, Glide Slope MODPA and a Cable Fault Board;

Glide Slope Electronic Subsystem Dual Equipment Dual Frequency Capture Effect - Electronic Subsystem, Shelter Environmental Sensor Kit, Battery Kit without Battery, Spare Glide Slope – Specific Modular Power Amplifier, and two Glide Slope and Thales Maintenance Data Terminal Instruction Books, Wattmeter Test Panel;

Note: Sensor kit does not include wiring

Glide Slope Antenna Subsystem Capture Effect Configuration - Three Antennas of the ‘Removable Tray Type’, one Tower (45 Ft.), three Platform Kits, one Fall Prevention System (Dyna Glide), three Antenna Installation and Mounting Kits, one Interior Shelter J-Box with three Trombone Phasers, one Interior Shelter Installation Kit (including Antenna Attenuator Kit), one 420° Test (Phasing) Cable;

Note: Fall Prevention System does not include personal safety harness

Remote Control Subsystem - Remote Control Status Unit, Remote Status and Interlock Control (capable of supporting Localizer and Glide Slope), and two Remote Control Status Instruction Books;

Base Modem Kit (X4) - Modem, Interface Cables for Remote Monitoring Subsystem or Remote Control Subsystem inside the Base Shelf, Power Interface Cable, Hardware, and Installation Drawing, and labeling for Base modem;

Note: RS-232 Interface Modem Kit for Remote Maintenance Monitor or Remote Control Subsystem Communication at the Air Traffic Control Tower (or other control site), and two Modems will be used for the Remote Control Status Unit link and two Modems will be used for the Remote Monitoring Subsystem link to Concentrator.

Site Modem Kit (X4) - Modem, Mounting Bracket, Specialized Interface Cables for Remote Monitoring Subsystem or Remote Control Subsystem, Power Interface Cable with inline Fuse, Hardware, Installation Drawing, and labeling for Site modem.;

Note: RS-232 Interface Modem Kit for Remote Maintenance Monitor or Remote Control Subsystem Communication at the Localizer/Glide Slope site, and two Modems will be used for the Remote Control Status Unit link and two Modems will be used for the Remote Monitoring Subsystem link to Concentrator.

Base Station Shelf Kit (for Radio Link/Modem Link) - Slides, Cable Retractor, and Spare Power Supply;

Note: Base Station Mounting Plate (for 19-inch Rack, C Panel Height) and Installation Kit (capable of being populated with eight Radio or Modem Positions used for Remote Control Subsystem or Remote Monitoring Subsystem Function);

Remote Control System Spares - Remote Status Control Unit Battery Charger/Power Supply, DC- DC Converter, Controller Card, Localizer/Glide Slope Communication/Display Card, Spare Fuse, and Spare Remote Status Interlock Control.

Modem Link Spares - Fuse, Cable, Modem, Software, Hardware, Installation Drawing, Schematic, and Users Guide.

Maintenance Data Terminal (MDT)- Two Instruction Manuals for Remote Monitoring Subsystem Concentrator Function, Maintenance Data Terminal Host Instruction Book, Instrument Landing System 420 Plug-In Instruction Book, and FAA Software Kit in CD format.

C.4.1.2 CLIN X002 – Complete Dual Equipment Dual Frequency Localizer System

(DEDF LOC).

Includes the following:

Localizer Electronic Subsystem Dual Equipment Dual Frequency - Electronic Subsystem, Shelter Environmental Sensor Kit, Battery Kit without Battery, Spare Localizer-Specific MODPA, and two Localizer & Thales Maintenance Data Terminal Instruction Books, Wattmeter Test Panel.

14/10 Localizer Antenna Subsystem Medium Aperture Dual Frequency Capture Effect – Antennas, Interior Shelter J-box, Installation Kit, and two Antenna Instruction Books;

Note: Civil kits are not supplied (i.e. concrete anchor bolts, leveling nuts, washers, etc.).

Spares for Localizer/Glide Slope Dual Equipment Configuration - Synthesizer, LGX.

Interface Assembly, ECU, SOAC, LCP, AC-DC Converter, DC- DC Converter, LVS, Transient Suppressor, WIC, Fuse, and Transfer Switch.

Unique Spares – Localizer MODPA and a Cable Fault Board.

Remote Control Subsystem - Remote Status and Interlock Control (capable of supporting Localizer and Glide Slope) and two Remote Control Status Instruction Books.

Remote Control System Spares - Remote Status Control Unit Battery Charger/Power Supply, DC-DC Converter, Controller Card, Localizer/Glide Slope Communication/Display Card, Spare Fuse, and Spare Remote Status Interlock Control.

Maintenance Data Terminal (MDT) - Two Instruction Manuals for Remote Monitoring Subsystem Concentrator Function, Maintenance Data Terminal Host Instruction Book, Instrument Landing System 420 Plug-In Instruction Book and FAA Software Kit in CD format.

C.4.1.3 CLIN X003 – Complete Dual Equipment Dual Frequency Glide Slope System

(DEDF CEGS).

Includes the following:

Glide Slope Electronic Subsystem Dual Equipment Dual Frequency Capture Effect - Electronic Subsystem, Shelter Environmental Sensor Kit, Battery Kit without Battery, Spare Glide Slope – Specific Modular Power Amplifier, and two Glide Slope & Thales Maintenance Data Terminal Instruction Books, Wattmeter Test Panel.

Glide Slope Antenna Subsystem Capture Effect Configuration - Three Antennas of the ‘Removable Tray Type’, one Tower (45 Ft.), three Platform Kits, one Fall Prevention System (Dyna Glide), three Antenna Installation & Mounting Kits, one Interior Shelter J-Box with three Trombone Phasers, one Interior Shelter Installation Kit (including Antenna Attenuator Kit), one 420° Test (Phasing) Cable.

Note: Civil kits are not supplied (i.e. concrete anchor bolts, leveling nuts, washers, etc.);

Note: No Climbing Harness or Safety Lanyard to be provided.

Spares for Localizer/Glide Slope Dual Equipment Configuration - Synthesizer, LGX.

Interface Assembly, ECU, SOAC, LCP, AC-DC Converter, DC- DC Converter, LVS, Transient

Suppressor, WIC, Fuse, and Transfer Switch.

Unique Spares – Glide Slope MODPA; and

Maintenance Data Terminal (MDT) - Two Instruction Manuals for Remote Monitoring Subsystem Concentrator Function, Maintenance Data Terminal Host Instruction Book, Instrument Landing System 420 Plug-In Instruction Book, and FAA Software Kit in CD format.

C.4.1.4 CLIN X004 – Single Equipment Single Frequency Localizer Cabinet with

Spares (SESF LOC).

Includes the following:

Localizer Electronic Subsystem Single Equipment Single Frequency - Electronic Subsystem, Shelter Environmental Sensor Kit, Battery Kit without Battery, Spare Localizer- Specific MODPA, and two Localizer & Thales Maintenance Data Terminal Instruction Books, Wattmeter Test Panel.

Spares for Localizer/Glide Slope Single Equipment Configuration - Synthesizer, LGX.

Interface Assembly, ECU, SOAC, LCP, AC-DC Converter, DC- DC Converter, LVS, Transient Suppressor, WIC, and Fuse.

Unique Spares – Localizer MODPA.

C.4.1.5 CLIN X005 – Single Equipment Dual Frequency Localizer Cabinet with Spares

(SEDF LOC).

Includes the following:

Localizer Electronic Subsystem Single Equipment Dual Frequency - Electronic Subsystem, Shelter Environmental Sensor Kit, Battery Kit without Battery, Spare Localizer-Specific MODPA, and two Localizer & Thales Maintenance Data Terminal Instruction Books, Wattmeter Test Panel.

Spares for Localizer/Glide Slope Single Equipment Configuration - Synthesizer, LGX.

Interface Assembly, ECU, SOAC, LCP, AC-DC Converter, DC- DC Converter, LVS, Transient Suppressor, WIC, and Fuse.

Unique Spares – Localizer MODPA.

C.4.1.6 CLIN X006 – Dual Equipment Single Frequency Localizer Cabinet with Spares

(DESF LOC).

Includes the following:

Localizer Electronic Subsystem Dual Equipment Single Frequency - Electronic Subsystem, Shelter Environmental Sensor Kit, Battery Kit without Battery, Spare Localizer-Specific MODPA, and two Localizer & Thales Maintenance Data Terminal Instruction Books, Wattmeter Test Panel;

Spares for Localizer/Glide Slope Dual Equipment Configuration - Synthesizer, LGX.

Interface Assembly, ECU, SOAC, LCP, AC-DC Converter, DC- DC Converter, LVS, Transient Suppressor, WIC, and Fuse, and Transfer Switch; and

Unique Spares – Localizer MODPA.

C.4.1.7 CLIN X007 – Dual Equipment Dual Frequency Localizer Cabinet with Spares

(DEDF LOC).

Localizer Electronic Subsystem Dual Equipment Dual Frequency - Electronic Subsystem, Shelter Environmental Sensor Kit, Battery Kit without Battery, Spare Localizer-Specific MODPA, and two Localizer & Thales Maintenance Data Terminal Instruction Books, Wattmeter Test Panel;

Spares for Localizer/Glide Slope Dual Equipment Configuration - Synthesizer, LGX. Interface Assembly, ECU, SOAC, LCP, AC-DC Converter, DC- DC Converter, LVS, Transient Suppressor, WIC, and Fuse, Transfer Switch; and

Unique Spares – Localizer MODPA.

C.4.1.8 CLIN X008 – 8 Element Single Frequency Localizer Antenna Array (LOC 8 Element SF Ant; DUCU Enclosure).

Includes the following:

8 Element Localizer Antenna Subsystem Single Frequency – Antennas, J-box, Installation Kit, and two Antenna Instruction Books; and

8 Element Localizer Spare - Cable Fault Board.

Note: Civil kits are not supplied (i.e. concrete anchor bolts, leveling nuts, washers, etc.).

C.4.1.9 CLIN X009 – 14 Element Single Frequency Localizer Antenna Array (LOC 14 Element SF Ant; DUCU Enclosure).

Includes the following:

14 Element Localizer Antenna Subsystem Medium Aperture Single Frequency – Antennas, J-box, Installation Kit, and two Antenna Instruction Books; and

14 Element Localizer Spare - Cable Fault Board.

Note: Civil kits are not supplied (i.e. concrete anchor bolts, leveling nuts, washers, etc.).

C.4.1.10 CLIN X010 – 14/10 Dual Frequency Localizer Antenna Array (14/10-EL DF LOC; DUCU Enclosure).

Includes the following:

14/10 Localizer Antenna Subsystem Medium Aperture Dual Frequency Capture Effect – Antennas, J-box, Installation Kit, two Antenna Instruction Books; and

14/10 Localizer Spare - Cable Fault Board.

Note: Civil kits are not supplied (i.e. concrete anchor bolts, leveling nuts, washers, etc.).

C.4.1.11 CLIN X011 – 20/10 Dual Frequency Localizer Antenna Array (20/10, DF LOC;

DUCU Enclosure).

Includes the following:

20/10 Localizer Antenna Subsystem Dual Frequency Capture Effect – Antennas, J-box, Installation Kit, two Antenna Instruction Books; and

20/10 Localizer Spare - Cable Fault Board.

Note: Civil kits are not supplied (i.e. concrete anchor bolts, leveling nuts, washers, etc.).

C.4.1.12 CLIN X012 – Dual Equipment Dual Frequency Capture Effect Glide Slope Cabinet with Spares (DEDF CEGS).

Includes the following:

Glide Slope Electronic Subsystem Dual Equipment Dual Frequency Capture Effect - Electronic Subsystem, Shelter Environmental Sensor Kit, Battery Kit without Battery, Spare Glide Slope – Specific Modular Power Amplifier, and two Glide Slope & Thales Maintenance Data Terminal Instruction Books Wattmeter Test Panel; and

Spares for Localizer/Glide Slope Dual Equipment Configuration - Synthesizer, LGX.

Interface Assembly, ECU, SOAC, LCP, AC-DC Converter, DC- DC Converter, LVS, Transient Suppressor, WIC, and Fuse, and Transfer Switch.

Unique Spares – Glide Slope (MODPA.

C.4.1.13 CLIN X013 – Single Equipment Dual Frequency Capture Effect Glide Slope Cabinet with Spares (SEDF CEGS).

Includes the following:

Glide Slope Electronic Subsystem Single Equipment Dual Frequency Capture Effect - Electronic Subsystem, Shelter Environmental Sensor Kit, Battery Kit without Battery, Spare Glide Slope – Specific Modular Power Amplifier, and two Glide Slope & Thales Maintenance Data Terminal Instruction Books, Wattmeter Test Panel;

Spares for Localizer/Glide Slope Single Equipment Configuration - Synthesizer, LGX.

Interface Assembly, ECU, SOAC, LCP, AC-DC Converter, DC- DC Converter, LVS, Transient Suppressor, WIC, and Fuse; and

Unique Spares – Glide Slope MODPA.

C.4.1.14 CLIN X014 – Dual Equipment Single Frequency Null Reference Glide Slope Cabinet with Spares (DESF NRGS).

Includes the following:

Glide Slope Electronic Subsystem Dual Equipment Single Frequency Null Reference (NR) - Electronic Subsystem, Shelter Environmental Sensor Kit, Battery Kit without Battery, Spare Glide Slope – Specific Modular Power Amplifier, and two Glide Slope & Thales Maintenance Data Terminal Instruction Books, Wattmeter Test Panel;

Spares for Localizer/Glide Slope Dual Equipment Configuration - Synthesizer, LGX.

Interface Assembly, ECU, SOAC, LCP, AC-DC Converter, DC- DC Converter, LVS, Transient Suppressor, WIC, and Fuse, and Transfer Switch; and

Unique Spares – Glide Slope MODPA.

C.4.1.15 CLIN X015 – Single Equipment Single Frequency Null Reference Glide Slope Cabinet with Spares (SESF NRGS).

Includes the following:

Glide Slope Electronic Subsystem Single Equipment Single Frequency Null Reference (NR) - Electronic Subsystem, Shelter Environmental Sensor Kit, Battery Kit without Battery, Spare Glide Slope – Specific Modular Power Amplifier, and two Glide Slope & Thales Maintenance Data Terminal Instruction Books, Wattmeter Test Panel;

Spares for Localizer/Glide Slope Single Equipment Configuration - Synthesizer, LGX. Interface

Assembly, ECU, SOAC, LCP, AC-DC Converter, DC- DC Converter, LVS, Transient Suppressor, WIC, and Fuse; and

Unique Spares – Glide Slope MODPA.

C.4.1.16 CLIN X016 – Dual Equipment Single Frequency Side-Band Reference Glide Slope Cabinet with Spares (DESF SBRGS).

Includes the following:

Glide Slope Electronic Subsystem Dual Equipment Single Frequency Side-Band Reference - Electronic Subsystem, Shelter Environmental Sensor Kit, Battery Kit without Battery, Spare Glide Slope – Specific Modular Power Amplifier, and two Glide Slope & Thales Maintenance Data Terminal Instruction Books, Wattmeter Test Panel.

Spares for Localizer/Glide Slope Dual Equipment Configuration - Synthesizer, LGX. Interface Assembly, ECU, SOAC, LCP, AC-DC Converter, DC- DC Converter, LVS, Transient Suppressor, WIC, Fuse, and Transfer Switch.

Unique Spares – Glide Slope MODPA.

C.4.1.17 CLIN X017 - Single Equipment Single Frequency Side-Band Reference Glide Slope Cabinet with Spares (SESF SBRGS).

Includes the following:

Glide Slope Electronic Subsystem Dual Equipment Single Frequency Side-Band Reference - Electronic Subsystem, Shelter Environmental Sensor Kit, Battery Kit without Battery, Spare Glide Slope – Specific Modular Power Amplifier, and two Glide Slope & Thales Maintenance Data Terminal Instruction Books, Wattmeter Test Panel.

Spares for Localizer/Glide Slope Dual Equipment Configuration - Synthesizer, LGX. Interface Assembly, ECU, SOAC, LCP, AC-DC Converter, DC- DC Converter, LVS, Transient Suppressor, WIC, and Fuse, and Transfer Switch; and

Unique Spares – Glide Slope MODPA.

C.4.1.18 CLIN X018a – Fall Prevention System for 45’ Glide Slope Tower – FAA Approved (aka Fall Prevention Kit, 45').

Includes the following:

Glide Slope Tower Fall Prevention System- Climbing Rail (Dyna-Glide), Climbing Trolley (Dyna-Glide) for a 45’ GS tower.

Note: No Climbing Harness or Safety Lanyard to be provided.

C.4.1.19 CLIN X018b – Glide Slope Tower Working Platform (3 Piece)

Includes the following:

See Section B.4.1.

C.4.1.20 CLIN X019 – Radio Guardian – 400 (analog).

See Section B.4.1.

C.4.1.21 CLIN X020 – Portable ILS Receiver (PIR).

Portable Receiver - At the FAA’s election, a Portable Receiver must be comprised of one of the following:

Portable ILS Receiver (PIR) - Portable ILS Receiver with Accessories Kit, Power Supply/Charger Uni-Pod, Localizer and Glide Slope Antennas, Cables, Battery Assembly, and Portable ILS Receiver Instruction Book; or

Note: No spares included with PIR.

C.4.1.22 CLIN X021 – Remote Maintenance Monitor (RMM) Set.

Includes all equipment from CLINs X022, X023 and X024 (RMM Set, Concentrator Set).

C.4.1.23 CLIN X022 – RMM Tower Computer

Includes the following:

RMM Tower Computer - Windows based and the following minimum requirements: 3 GHz Core I5 CPU, 8 GB RAM, and 500 GB Internal Disk Drive.

C.4.1.24 CLIN X023 – RMM LED Monitor

Includes the following:

A RMM LED or LCD Monitor with Minimum requirements: 19” screen with 800x600 or better resolution.

C.4.1.25 CLIN X024 – Serial Interface Adapter.

Includes the following:

Serial Interface Adapter - USB to 4-Port RS-232 DB9 serial interface adapter, FTDI Driver Compatible; or equivalent.

C.4.1.26 CLIN X025 – X028 – Reserved

C.4.1.27 CLIN X029 – One Glide Slope Tower Middle Section, 5 ft. Painted White

C.4.1.28 CLIN X030 – One Glide Slope Tower Middle Section, 10 ft. Painted White

C.4.1.29 CLIN X031 – One Glide Slope Tower Middle Section, 5 ft. Painted Aviation Orange

C.4.1.30 CLIN X032 – One Glide Slope Tower Middle Section, 10 ft. Painted Aviation Orange

C.4.1.31 CLIN X033 – One Glide Slope Tower Top Section, 5 ft. Painted White

C.4.1.32 CLIN X034 – One Glide Slope Tower Top Section, 10 ft. Painted White

C.4.1.33 CLIN X035 – One Glide Slope Tower Top Section, 5 ft. Painted Aviation Orange

C.4.1.34 CLIN X036 – One Glide Slope Tower Top Section, 10 ft. Painted Aviation Orange

C.4.1.35 CLIN X037 – X046 – Reserved

C.4.1.36 CLIN X047 – Log-Periodic Dipole Snow Cover Kit

Includes the following:

Log-Periodic Dipole Snow Covers – 8 Sleeve Assemblies and Installation Drawings.

Note: Kit is for one Log-Periodic Dipole Antenna. Example: If a 14 Element Array is installed, then 14 Kits would need to be purchased. No spares included.

C.4.1.37 CLIN X048 - Log-Periodic Dipole Antenna (single antenna).

Includes the following:

Log-Periodic Dipole Antenna – One Log-Periodic Dipole Antenna with welded rods.

Note: This CLIN does not include installation hardware. Example: If the site requires 14 Antennas, then 14 Log-Periodic Dipoles would need to be purchased.

C.4.1.38 CLIN X049 – Dual Equipment Receiver Far Field Monitor (FFM) with Dual YAGI Antenna.

Includes the following:

Far Field Monitor – Dual Equipment Monitor Receiver Electronic Subsystem in Desktop Enclosure, two YAGI Antennas with Supports, one Installation Kit, one Battery Kit without Battery, one Transient Suppressor Assembly, and two Far Field Monitor Instruction Manuals.

Far Field Monitor Spares - Support Circuit Card Assembly, Receiver Circuit Card Assembly, Control Panel and AC-DC Power Supply, and Battery Charger/Power Supply Fuses.

C.4.1.39 CLIN X050a – Single Glide Slope Antenna, without Removable Tray

Includes the following:

A single GS antenna element without the removable tray.

C.4.1.40 CLIN X050b – Single Glide Slope Antenna, with Removable Tray

See Section B.4.1.

C.4.1.41 CLIN X051 – Localizer Antenna (Single Antenna)

Single Log-Periodic Dipole (LPD) Antenna.

C.4.1.42 CLIN X052 – 14/20 Instrument Landing System Conversion Kit.

Log-Periodic Dipole Antennas with Supports, Antenna Raceway, Distribution Unit Combining Unit (DUCU), Cables.

C.4.1.43 CLIN X053 – Capture Effect Glide Slope Antenna System (Removable Tray).

See Section B.4.1.

C.4.1.44 CLIN X054 – Null Reference (NR) Glide Slope Antenna System (Removable Tray).

See Section B.4.1.

C.4.1.45 CLIN X055 – Side-Band Reference Glide Slope Antenna System (Removable Tray).

See Section B.4.1.

C.4.1.46 CLIN X056 – Glide Slope Antenna Heater Kit.

Includes the following:

Glide Slope Antenna Heater Kit – Two Glide Slope Antenna Heater Thermostats (low and high), three nine-foot Terminated Flexible SJW 600V Heater Cables.

Note: This kit can be used with all three types of the Contractor’s conventional Antenna Systems.

No spares included.

C.4.1.47 CLIN X057 – Reserved

C.4.1.48 CLIN X058 – Remote Control Subsystem with Spares.

Includes the following:

Remote Control Subsystem – Remote Status Control Unit, Remote Status, and Interlock Control (capable of supporting Localizer and Glide Slope), and two Remote Control Status Instruction Books.

Remote Control System Spares - Remote Status Control Unit Battery Charger/Power Supply, DC-DC Converter, Controller Card, Localizer/Glide Slope Communication/Display Card, Spare Fuse, and Spare Remote Status Interlock Control.

C.4.1.49 CLIN X059 – Remote Status Control Unit.

Includes the following:

Remote Status Control Unit - Remote Status Control Unit (capable of supporting Localizer and Glide Slope), and two Remote Control Status Instruction Books; and

Remote Control System Spares - Remote Status Control Unit Battery Charger/Power Supply, DC-DC Converter, Controller Card, Localizer/Glide Slope Communication/Display Card, Spare Fuse, and Spare Remote Status Interlock Control.

C.4.1.50 CLIN X060 – Remote Status and Interlock Control.

Includes the following:

Remote Status and Interlock Control - Remote Status and Interlock Control Module and two

Remote Control Status Instruction Books.

Note: Available for retrofit of Remote Status and Interlock Units to provide the additional features of Subsystem On-Battery Indication, Daisy Chain Installation, and Positive Interlock Control. No spares included.

C.4.1.51 CLIN X061 – Base Modem Kit with Spares.

Includes the following:

Base Modem Kit (X2) – Each Base Modem Kit includes Modem, Interface Cables for Remote Monitoring Subsystem or Remote Control Subsystem inside the Base Shelf, Power Interface Cable, Hardware, Installation Drawing, and labeling for Base modem.

Base Modem Kit Spare - Modem, Power Supply, and Fuse.

Note: RS-232 Interface Modem Kit for Remote Maintenance Monitor or Remote Control Subsystem Communication at the Air Traffic Control Tower (or other control site). One Modem will be used for the Remote Status Control Unit link and one Modem will be used for the Remote Monitoring Subsystem link to Concentrator.

C.4.1.52 CLIN X062 – Site Modem Kit with Spares.

Includes the following:

Site Modem Kit (X2) – Each Site Modem Kit includes Modem, Mounting Bracket, Specialized Interface Cables for Remote Monitoring Subsystem or Remote Control Subsystem, Power Interface Cable with Inline Fuse, Hardware, Installation Drawing, and labeling for Site modem.

Site Modem Kit Spare - Modem, Power Supply, and Fuse.

Note: RS-232 Interface Modem Kit for Remote Maintenance Monitor or Remote Control Subsystem Communication at Localizer/Glide Slope Site, and one Modem will be used for the Remote Control Status Unit link and one Modem will be used for the Remote Monitoring Subsystem link to Concentrator.

C.4.1.53 CLIN X063 – Modem/Radio 19” Rack Shelf.

Includes the following:

Base Station Shelf Kit (for Radio Link/Modem Link) - Base Station Mounting Plate (for 19-inch Rack, C Panel Height), Installation Kit (capable of being populated with eight Radio or Modem Positions (used for Remote Control Subsystem or Remote Monitoring Subsystem Function), Slides, Cable Retractor, and Spare Power Supply.

Note: Radio Kit or Modem Kit Ordered Separately. No spares included.

C.4.1.54 CLIN X064 – Communication Display Interface Circuit Card Assembly.

Communication Display Interface Circuit Card Assembly - Communication Display

Assembly Interface (with Integrated Modem) for Remote Control Status Unit/Remote Status Control Unit.

Note: Used in conjunction with Universal Local Control Status Unit (CLIN 1059) to interface additional subsystems into a MK-20 Remote Control Status Unit or ILS-420 Remote Status Control Unit. No spares included.

C.4.1.55 CLIN X065 – Universal Local Control Status Unit

Universal Local Control Status Unit.

Note: Universal Local Control Status Unit provides interface capability to Remote Status Control Unit (CLIN 1051) for legacy systems and ancillary equipment. No spares included.

C.4.1.56 CLIN X066 – ILS Monitor Receiver

ILS Monitor Receiver – ILS Monitor Receiver consisting of Receivers and Pre-Selector Filter for Localizer and Glide Slope (within a “C” panel 19” Rack Mount Enclosure). Unit includes Antennas for the Localizer and Glide Slope sites, Remote Status Indicator Unit, and two ILS Monitor Receiver Instruction Books.

ILS Monitor Receiver Spare - Remote Status Unit.

Note: Pre-Selector for Localizer and Glide Slope are passive devices and are not included in the spares.

C.4.1.57 CLIN X067-X068 – Reserved

C.4.1.58 CLIN X069 – Base Radio Kit with Spares (One to multilink, Digital).

Includes the following:

Base Radio Kit with Spare – Radio, Programming Kit, Omni-Directional Antenna, Interface Cables for Remote Monitor System or Remote Control System inside the Base Shelf, 100’ RF Antenna Cable with Type N Connectors, and Installation Drawing.

Base Radio Spare - Spare Radio, DC/DC Power Supply (DIN Rail Mount), and Fuse.

Note: Antenna Mount and Conduit are determined based on installation and are not supplied in this kit.

C.4.1.59 CLIN X070 – Site Radio Kit with Spares (One to multilink, Digital).

Includes the following:

Site Radio Kit with Spare – Radio, Programming Kit, Antenna, Mounting Bracket, 15' Specialized Interface Cables for Remote Monitor System or Remote Control System, DIN Rail DC/DC Converter Power Supply and Power Interface Cable with Inline Fuse, Hardware, 4’ RF Interface Cable between Radio and Bulkhead Plate, 25’ RF Antenna Cable with Type N Connectors, Type N Bulkhead Feedthrough (UG 30 D/U), and Installation Drawing.

Site Radio Spare - Spare Radio, DC/DC Power Supply (DIN Rail Mount), and Fuse.

Note: Antenna Mount and Conduit are determined based on installation and are not supplied in this kit.

C.4.1.60 CLIN X071 – Localizer Leg Extension Kit (3 ft.).

Includes the following:

LPD Leg Extension – One front Leg extension and one rear leg extension for LPD antenna, each being 3 feet in length. Mounting hardware, installation instructions, and data package to be provided in the kit. Kits will include 14 extensions for a 14-element antenna array.

C.4.1.61 CLIN X072 – Installer Workshop

As described in section C.4.10.4

C.4.1.62 CLIN X073 – End Fire Glide Slope Interface for ILS-420

See Section B.4.1.

C.4.1.63 CLIN X074 - Enlarged Distribution Unit, Controller Unit (DUCU), Wattmeter Interface Card (WIC), and Guide Rail Enhancement

Includes the following:

Enlarged DUCU enclosure, Quantity 2 guide rail enhancements, 1 GS wattmeter interface card, 1 LOC wattmeter interface card.

C.4.1.64 CLIN X075 – X076 – Reserved

C.4.1.65 CLIN X077– Engineering Support Service

As described in Section C.4.10.2

C.4.1.66 CLIN X078 – Customer Support Services

As described in Section C.4.10.1

C.4.1.67 CLIN X079 – CDLS

As described in Section C.4.9.3

CLIN 1079a – Spares

CLIN 1079b – Repairs

CLIN 1079c – Monthly Management and Reports (CDRL 021)

C.4.1.68 CLIN X080a – Program Management, Conferences, Reviews, Meetings

This CLIN is to capture all Programmatic work and various meetings listed in Section C.4.2.1, 4.2.2, 4.2.3, 4.9.1.2, 4.9.2.4.

C.4.1.69 CLIN X080b – Technical Interchange Meetings

This CLIN is to capture the requirements in Section C.4.2.4.

C.4.1.70 CLIN X081 – ILS-420 Installation Support Service

This CLIN is to capture the requirements in Section C.4.10.3

C.4.2 Program Management

C.4.2.1 Program Management Organization and Plan

The Contractor must maintain the organization to manage the contract and subcontracts, including program control, quality assurance, configuration management, management of FAA furnished resources, risk management, and security. The management organization, techniques, tasks and procedures must be documented in a Program Management Plan (PMP). The contractor must deliver a PMP on the current Program Management Organization.

The contractor must deliver a quarterly “Contractor's Progress, Status and Management Report”.

The report is due the 15th day of the month, starting the third month after contract award.

Contractor format is acceptable. The content of the report must include at a minimum; a cover sheet; system delivery status and schedule; description of the progress made against milestones during the reporting period; any FAA trips and significant results; Summary of Engineering Change Proposal (ECP) status, including identification of proposed ECPs, approved ECPs, and implemented ECPs; and plans for activities during the following reporting period.

CDRL 001: Program Management Plan

C.4.2.2 Meetings, Conferences and Reviews

The Contractor must conduct meetings, conferences, and reviews in accordance with the approved PMP and this statement of work at the Contractor’s site or virtually at a mutually agreed upon time between the FAA and the contractor. The FAA shall prepare and submit agendas and minutes. When meetings or conferences are held at the Contractor’s site, the Contractor must provide facilities and office equipment (e.g., access to internet, telephone), sub-Contractor personnel when requested, and appropriate presentation materials, mockups, and technical data. Copies of presentation materials must be prepared for all meeting participants.

C.4.2.3 Post Award Conference

A post award conference will be held at the Contractor’s facility or conducted virtually within one (1) month after contract award. The agenda will be developed jointly between the Contractor and the FAA. The FAA will provide minutes from each meeting. The duration of the conference may be two full working days.

C.4.2.4 Technical Interchange Meetings

If ordered by the FAA, the Contractor must host and conduct a Technical Interchange Meetings (TIMs) at the Contractor’s facility to discuss specific technical activities, including but not limited to:

studies, test plans, risk, test results, design issues including human engineering, technical problems, training issues, logistics issues, implementation concerns, verification audit, and to monitor the technical progress of the contract. The CO or COR will determine the meeting location.

The meeting duration, attendees, and agenda will be determined by the issues brought up or by the discussions during the meeting. The Contractor must prepare and submit for FAA review, a meeting agenda at least 10-calendar days prior to the TIM. The FAA may, as a result of this review, direct the Contractor to add additional items to the agenda. The TIM must be planned for no more than 2-calendar days in length. The FAA will provide minutes from each meeting.

C.4.3 Quality Assurance

The Contractor must maintain a documented quality system compliant with the requirements of AS9100D, Quality Management Systems - Requirements for Aviation, Space, and Defense Organizations. Third party certification of International Standards Organization ISO standards is not required nor does such certification relieve the Contractor of the requirement in the QSP.

The contractor must deliver a Quality System Plan on the current Quality System program and procedures.

CDRL 002: Quality System Plan

C.4.4 Configuration Management

C.4.4.1 Configuration Management (CM) Planning

The Contractor must maintain a CM program using MIL-HDBK-61A and ANSI/EIA-649 for guidance. The CM program must be documented using MIL-HDBK-61A, Appendix A, focusing on Phase II and III, as described in Table A-3. The CM program must cover the Contractor’s CM organizational structure and methods of configuration identification, change control, configuration status accounting, and configuration auditing for documentation, physical media and physical parts representing or comprising the ILS 420. The Contractor must maintain configuration control of hardware, software, firmware, and developmental/ commercial documentation until delivery of the last ordered production unit, subject to configuration change control requirements specified below.

The Contractor must identify the single focal point, under the Program Manager, who will serve as the primary point of contact for all communication on CM-related issues. The contractor must deliver a Configuration Management Plan on the current CM Program, organization, and procedures.

CDRL 003: Configuration Management Plan

C.4.4.2 Configuration Item (CI) Identification

The Contractor must identify, establish, and maintain the configuration of the ILS 420 and its subordinate CIs. This configuration must include the following:

a. Selecting developmental and commercial CIs at appropriate levels of the product structure to facilitate the control and support of the items;

b. Determining the types of configuration documentation required for each CI to define its performance, functional, and physical attributes, including internal and external interfaces;

c. Determining the appropriate configuration control authority for each configuration document consistent with logistic support planning for the associated CI;

d. Issuing identifiers for the CIs and the configuration documentation.

e. Maintaining the configuration identification of CIs to facilitate effective logistics support of items in service;

f. Releasing configuration documentation;

g. Establishing configuration baselines for the configuration control of CIs.

C.4.4.3 Software Configuration Items

The Contractor must assign a discrete version/release number to each software product released to include; medium (e.g., magnetic tape, disk) containing release-or build-type software executables. The medium thus identified must be inclusive and contain all software segments; thereby providing easy identification of software releases.

C.4.4.4 Configuration Change Control

The Contractor must maintain and demonstrate a systematic life cycle configuration change management process for the ILS 420 as described in the CM Plan (CDRL 003). This change management process, using MIL-HDBK-61A, Section 6, and ANSI/EIA-649, as guidance, must manage the preparation, justification, evaluation, coordination, disposition, and implementation of proposed engineering changes and deviations to the ILS 420 system hardware, software and firmware, and baselined configuration documentation.

C.4.4.5 Engineering Change Proposals (ECP)

Engineering Change Proposals (ECPs) required to be submitted to the FAA are classified as either Class I or Class II. If Contractor initiated Class I or Class II ECP changes are approved by the FAA, they are developed and implemented at no additional cost to the FAA. Items like code, part lists, drawings and procedures will be provided to the FAA for operational systems implementation.

If the FAA initiates an ECP Class I change, the Contractor will not incur the cost to implement the change. Implementation will start after the release of the FAA modification. A Class II change is reviewed for concurrence in classification by the FAA Quality Reliability Officer (QRO). As part of the ECP, the Contractor must provide history, detailed change information, estimated costs, schedules, benefits and risks associated with the ECPs.

CDRL 004: Engineering Change Proposals

C.4.4.6 Class I and II Change Definition

The contractor must classify ECPs as either Class I or II in accordance with the definitions in MIL- HDBK-61A. For detailed classification criteria, see DD Form 1692 instruction sheet.

C.4.4.6.1 Class I Changes

The Contractor must submit all Class I ECPs to the CO or his/her designated Contracting Officer’s Representative (COR), with a copy to the FAA QRO. The FAA will have 30 calendar days to review the subsequent ECP. If approved, the Contractor must proceed with the engineering change. The Contractor must submit to the CO and COR all changes to documentation resulting from the approved ECP. The documentation includes, at a minimum, all affected assembly drawings and TIB change pages within 30 calendar days of FAA approval. All changed documentation must have all changes within it highlighted by change bars and was/now annotations. ECPs will be applicable and required for all equipment procured throughout the life of the contract, including option years. If the change is not approved, the Contractor must withdraw it or resubmit with further clarification of the proposed change(s).

C.4.4.6.2 Class II Change

The Contractor must submit all Engineering Change Requests (ECRs) or Class II ECPs to the FAA QRO for classification concurrence and approval. The FAA has 21 calendar days to review and approve all ECRs or Class II ECPs. If approved, the Contractor must submit to the CO and COR all changes to documentation resulting from the approved ECRs/Class II ECPs within 30 calendar days of FAA approval. The documentation includes, at a minimum, all affected assembly drawings, and TIB change pages. All changed documentation must have all changes within it highlighted by change bars and was/now annotations.

If the QRO does not concur in the classification of a Class II engineering change, the Contractor must prepare a Class I ECP and submit it to the CO or COR and QRO for approval by following the procedures outlined in this contract.

C.4.4.6.3 FAA Configuration Changes

The Contractor Depot Level Support (CDLS Services) set forth in Section C.4.9.3 may not be utilized, in the event that any portion of the ILS 420 system is configured and operated in combination with…