CH-53K_CNI PERFORMANCE SPECIFICATION_DRAFT_11-25-24.docx

PRF 230007B

22 November 2024

SUPERSEDING

PERFORMANCE SPECIFICATION

FOR

UNITED STATES MARINE CORPS

CH-53K Communication, Navigation and Instrumentation (CNI) Maintenance Trainer

NAVAL AIR WARFARE CENTER

TRAINING SYSTEMS DIVISION

12211 SCIENCE DRIVE

ORLANDO, FL 32826

APPROVED BY: _________________________________ DATE:

Jenny Barriger (PMA-205, Level II IPTL) H-53 Training Systems of designee

APPROVED BY: _________________________________ DATE:

Lynn Rau (APME designee) APEO (E) or designee

APPROVED BY: _________________________________ DATE:

Chad Guillet (PSM designee) APEO (L) or designee

APPROVED BY: _________________________________ DATE:

Ryan Schmidt (APMT&E designee)

Distribution Statement D: Distribution authorized to Department of Defense and U.S. DoD contractors only; Controlled Technical Information (CTI); 8 November 2019. Other requests for this document must be referred to Program Executive Officer Air (PEO(A)), PMA-261, 47123 Buse Rd., Building 2272 RM 155, Patuxent River, MD 20670.

Controlled by: Department of Navy Controlled by: NAWCTSD CUI Category: CTI Distribution/Dissemination Control: FEDCON

CUI

POC: Cattien.T.Nguyen.civ@us.navy.mil

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REVISIONS

A

Revision A Changes Accepted

Michael Miller USMC APMSE

iii

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Table of Contents

Table of Contents

Section Title Page xiv

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xiii

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Tables

Table of Contents

Figures

Performance Specification for CH-53K CNI Training Device

SCOPE

This specification establishes the functional, performance, and verification requirements for a new United States Marine Corps (USMC) CH-53K Communication, Navigation and Instrumentation (CNI) maintenance trainer that will be at the Center for Naval Aviation Technical Training Marine Unit (CNATT MARU) facilities building AS235 located at Marine Corps Air Station (MCAS) New River, Jacksonville, North Carolina.

System Identification The CH-53K CNI is designated as Device 11B112. The CNI will be used as a full-size training device to aid in the development of maintenance skills and support first-level maintenance training of the CH-53K cockpit and avionics areas to maintenance personnel as described herein, see section 3.1 and subsequent paragraphs.

System Overview The primary use of the CNI training device will be to train cockpit and avionics system familiarization, component identification, the performance of function tests and all variations of Built-In Tests, fault isolation and remove and installs of selected Weapons Repairable/Replaceable Assemblies or Line Replaceable Assemblies.

Document Overview For purposes of this specification, the terms CNI, device, trainer, training system, and training device are equivalent. The terms “shall”, “will”, and “objective” are used with specific intent throughout this document. All requirements are threshold requirements except those specified as objective. The threshold requirements represent the minimum acceptable value necessary to satisfy the training need. The use of “shall” denotes a threshold. Requirements defined using “shall” are considered to be binding and require formal verification. Requirements defined using “will” express intent, are not binding, and therefore do not require formal verification. The term “objective” expresses capabilities beyond the threshold requirement. Objectives present an opportunity to exceed the threshold requirement if a cost effective implementation is achievable.

APPLICABLE DOCUMENTS

General The documents listed in this section are cited in sections 3, 4, and 5 of this specification. This section does not include documents cited in other sections of this specification or recommended for additional information or as examples. While every effort has been made to ensure the completeness of this list, document users are cautioned that they must meet the specified requirements of documents cited in sections 3, 4, and 5 of this specification, whether or not they are listed.

Government Documents Specifications, Standards, and Handbooks The following specifications, standards, and handbooks of the exact revision listed below form a part of this specification to the extent specified herein.

Department of Defense Standards

(Copies of these documents are available online at https://quicksearch.dla.mil or from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094)

Department of Defense Handbooks

(Copies of these documents are available online at https://quicksearch.dla.mil or from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094)

Other Government Documents, Drawings, and Publications The following Government documents, drawings, and publications of the exact revision level shown form a part of this document to the extent specified herein.

Code of Federal Regulations

(Copies of this document are downloadable from http://www.ecfr.gov)

DOD Security/Cybersecurity Documents

ISO/IEC 11889-2:2015

Information Technology – Trusted Platform Module Library – Part 2: Structures, Second Edition, dated 15 December 2015

ISO/IEC 11889-3:2015

Information Technology – Trusted Platform Module Library – Part 3: Commands, Second Edition, dated 15 December 2015

(Copies of the above documents are downloadable from https://www.esd.whs.mil/directives/issuances/, https://csrc.nist.gov/publications, https://www.dcsa.mil/portals/91/documents/ctp/nao/CNSSI_No1253.pdf, https://standards.iso.org/ittf/PubliclyAvailableStandards/index.html)

DoD Unified Facilities Criteria (UFC)

(Copies of the above documents are downloadable from https://www.wbdg.org/ffc/dod/unified-facilities-criteria-ufc)

Naval Air Systems Command (NAVAIR) Documents

(Copies of the above documents will be delivered as Government-furnished information)

Office of the Law Revision Counsel United States Code

(Copies of this document are downloadable from http://uscode.house.gov/)

United States (US) Army Corp of Engineers – Engineer Manuals

(Copies of these documents are downloadable from https://www.publications.usace.army.mil/USACE-Publications/Engineer-Manuals/)

Non-Government Publications American National Standards Institute (ANSI)/National Electrical Manufacturers Association (NEMA)

(Copies of these documents are available from www.ansi.org)

American Society of Mechanical Engineers (ASME)

(Copies of this document are available from http://www.asme.org)

JEDEC Solid State Technology Association

(Copies of this document are available from http://www.jedec.org)

National Fire Protection Association (NFPA)

(Copies of the above documents are downloadable from http://www.nfpa.org and are available from are available from NFPA 1 Batterymarch Park Quincy, Massachusetts USA 02169-7471)

Order of Precedence Unless otherwise noted herein or in the contract, in the event of a conflict between the text of this specification and the references cited herein, the text of this specification takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained.

REQUIREMENTS

The CNI device functional and performance characteristics shall be in accordance with (IAW) the following subordinate paragraphs, based on procedures/tasks identified in the latest version of CH-53K Interactive Electronic Technical Manual (IETM) (A1-CH53K-IETM-MMO-000), and aligned to the latest aircraft Bureau Number (BUNO) # XXXXXX with IETM lockdown to occur NLT 30 days prior to PDR and provided to seller.

Subsystem Functional Requirements Training Tasks and Objectives The trainer shall

1. be a stand-alone, full-size, high fidelity (see 6.1.7) maintenance task trainer replicating the CH-53K nose, cockpit, and forward cabin section to Station 282 on the System Demonstration Test Article (SDTA) 6 airframe (provided as GFE located at NAS Patuxent River, MD) including but not limited to the overhead and instrument panels, consoles, avionics bays and shelves, flight controls, Multifunctional Displays (MFDs) and Control Display Units (CDUs);

only include CH-53K cockpit through forward Station 282;

have the components necessary to accomplish the maintenance procedures listed in 3.1.3;

have embedded simulated or stimulated functionality, with a separate instructor operator station (IOS) for fault insertion/isolation/correction;

represent the latest version CH-53K aircraft BUNO represented by CH-53K design basis aircraft (DBA) (see 6.1.5) available 30 days prior to PDR;

be comprised of components, panels and avionics replicating the form and fit as the CH-53K DBA (see 6.1.5);

present the trainees with realistic operational checkout, troubleshooting situations, and component replacement tasks; and function IAW latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, demonstrating the operation, testing, fault identification and isolation, adjustment, diagnostics, and replacement of the aircraft systems and components.

Trainer Tasks and Objectives Precedence The training system shall not require wire repair except as explicitly stated in the tables within subsections of 3.1.3. The tables within the subsections of 3.1.3 correspond with A1-CH53K-IETM-MMO-000 available 30 days prior to PDR.

1.1.1 IOS Subsystem

The IOS shall

1. identify the designated training scenario with reference to applicable maintenance task in the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, including Fault Code, Fault Condition, and failed component if applicable;

have controls to monitor and display system status;

have instructor controls to initiate, and stop training events;

assign functional test and insert fault training scenarios;

manually insert and reset system fault conditions; and monitor and fault trainer system circuit breakers;

b. have controls to turn on and off electrical power to support tasks in the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR;

c. perform Diagnostic analysis of the trainer (Daily Operational Readiness Test (DORT)); and have controls to insert up to three, unrelated tasks (not cascading faults), simultaneously.

Training System or Subsystem Functional Requirements The CNI shall

1. replicate system functional testing with no failure IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR;

replicate system functional testing with failures IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR;

have the failures defined as a single combination of Fault Code and Fault Condition per training exercise as defined per the tables within subsections of 3.1.3;

have fault isolation and troubleshooting defined as the same;

have the failures display the associated failure indicators for that combination of Fault Code and Fault Condition on the CNI MFD;

replicate system troubleshooting and failure identification IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, with the following fidelity:

1. high fidelity (see 6.1.7) physical interface connectors;

high fidelity (see 6.1.7) physical components;

replicate component location, obstructions and accessibility IAW CH-53K DBA (see 6.1.5);

replicate component interfaces and attachments with training device IAW CH-53K DBA (see 6.1.5);

replicate component attachments to the training device IAW CH-53K DBA (see 6.1.5);

replicate wiring harnesses, routing, and interfacing IAW CH-53K DBA (see 6.1.5); and replicate continuity or voltage reading for specified fault IAW CH-53K DBA (see 6.1.5);

receive the inserted fault from the IOS IAW the tables within subsections of 3.1.3;

have the fidelity and functionality required to repair the fault by replacement of failed high fidelity (see 6.1.7) replica or actual component;

receive the command from the IOS, and to clear the inserted fault manually; and have sounds and aural cues associated to normal operation and faults within the latest version A1-CH53K-IETM-MMO-000 tasks available 30 days prior to PDR identified in this specification (e.g. inter-communication system (ICS), radios, Auxiliary Power Unit (APU), engine start, audio master caution warnings, etc.), to support training outcome IAW latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR.

Integrated Vehicle Health Management System (IVHMS) Integrated Built-In-Test (IBIT) The CNI shall

1. replicate the CH-53K IVHMS IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR;

have an IVHMS comprised of actual and/or simulated components, with the fidelity required to facilitate system component identification and perform function tests, fault isolation procedures, removal, repairs, and installations associated with the components IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR;

contain the components, subcomponents, and hardware to execute the IVHMS Function Test with no failure indication IAW the latest version available A1-CH53K-IETM-MMO-000, 30 days prior to PDR, procedure 19-10-00-01A-340A-A, excluding steps 5-6;

have IOS controls to insert and remove Fault Codes and Fault Conditions (if applicable) listed in TABLE I for IVHMS functional IBIT test;

perform IVHMS IBIT with the indicated Fault Codes and Fault Conditions (if applicable) listed in TABLE I IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, procedure 19-10-00-01A-340A-A;

perform fault isolation procedures per the Fault Codes and Fault Conditions (if applicable) listed in TABLE I IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, procedure 19-10-00-01A-421A-A;

remove and reinstall the failed components IAW the Repair IETM column listed in TABLE I; and execute the IVHMS Function Test with no failure indications after the failed component has been repaired.

TABLE I IVHMS failed components

Environmental Control System (ECS) IBIT The CNI shall

1. replicate the CH-53K ECS IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR;

have an ECS comprised of actual and/or simulated components, with the fidelity required to facilitate system component identification and perform function tests, fault isolation procedures, removal, repairs, and installations associated with the components IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR;

contain the components, subcomponents, and hardware to execute the ECS Function Test with no failure indication IAW the latest version A1-CH53K-IETM-MMO-000, available 30 days prior to PDR, procedure 21-90-00-01A-340A-A, excluding steps 6-10;

have IOS controls to insert and remove the Fault Codes and Fault Conditions listed in TABLE II for ECS functional IBIT test;

perform ECS functional IBIT Function Test with the indicated Fault Codes and Fault Conditions listed in TABLE II IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, procedure 21-90-00-01A-340A-A;

perform fault isolation procedures per the Fault Codes and Fault Conditions listed in TABLE II IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, procedure 21-90-00-01A-421A-A, excluding Fault Codes 21-90-00-31, 21-90-00-32 and 21-90-00-37;

remove and reinstall the failed components IAW the Repair IETM column listed in TABLE II, excluding Fault Codes 21-90-00-31, 21-90-00-32 and 21-90-00-37; and execute the ECS Function Test with no failure indications after the failed component has been repaired.

TABLE II ECS failed components

Flight Control System (FCS) IBIT

1. replicate the CH-53K FCS IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR;

have a FCS comprised of actual and/or simulated components, with the fidelity required to facilitate system component identification and perform function tests, fault isolation procedures, removal, repairs, and installations associated with the components IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR;

contain the components, subcomponents, and hardware to execute the FCS Function Test with no failure indication IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, procedure 22-10-00-01A-340A-A, excluding steps 4.6.5 -16;

have IOS controls to insert and remove Fault Codes and Fault Conditions listed in TABLE III for FCS functional IBIT test;

perform FCS functional IBIT Function Test with the indicated Fault Codes and Fault Conditions listed in TABLE III IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, procedure 22-10-00-01A-340A-A, excluding steps 4.6.5 through 4.6.8;

fault isolation procedures per the Fault Codes and Fault Conditions listed in TABLE III IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, procedure 22-10-00-01A-421A-A;

remove and reinstall the failed components IAW the Repair IETM column listed in TABLE III; and execute the FCS Function Test with no failure indications after the failed component has been repaired.

TABLE III FCS failed components

Communication (Comm) 1 AN/ARC-210(V) System IBIT

1. replicate the CH-53K Comm 1 AN/ARC-210(V) System IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR;

have a Comm 1 AN/ARC-210(V) System comprised of actual and/or simulated components, with the fidelity required to facilitate system component identification and perform function tests, fault isolation procedures, removal, repairs, and installations associated with the components IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR;

contain the components, subcomponents, and hardware to execute the Comm 1 AN/ARC-210(V) System Function Test with no failure indication IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, procedure 23-10-01-01A-340A-A, excluding step 5;

have IOS controls to insert and remove the Fault Code and Fault Condition listed in TABLE IV for Comm 1 AN/ARC-210(V) System functional IBIT test;

perform Comm 1 AN/ARC-210(V) System functional IBIT Function Test with the indicated Fault Code and Fault Condition listed in TABLE IV IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, procedure 23-10-01-01A-340A-A;

perform fault isolation procedures per the Fault Code and Fault Condition listed in TABLE IV IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, procedure 23-10-01-01A-421A-A;

remove and reinstall the failed components IAW the Repair IETM column listed in TABLE IV; and execute the Comm 1 AN/ARC-210(V) System Function Test with no failure indications after the failed component has been repaired.

TABLE IV Comm 1 AN/ARC-210(V) System failed components

Comm 2 AN/ARC-210(V) System IBIT

1. replicate the CH-53K Comm 2 AN/ARC-210(V) System IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR;

have a Comm 2 AN/ARC-210(V) System comprised of actual and/or simulated components, with the fidelity required to facilitate system component identification and perform function tests, fault isolation procedures, removal, repairs, and installations associated with the components IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR;

contain the components, subcomponents, and hardware to execute the Comm 2 AN/ARC-210(V) System Function Test with no failure indication IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, procedure 23-10-02-01A-340A-A, excluding step 5;

have IOS controls to insert and remove the Fault Code and Fault Condition listed in TABLE V for Comm 2 AN/ARC-210(V) System functional IBIT test;

perform Comm 2 AN/ARC-210(V) System functional IBIT Function Test with the indicated Fault Code and Fault Condition listed in TABLE V IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, procedure 23-10-02-01A-340A-A;

perform fault isolation procedures per the Fault Code and Fault Condition listed in TABLE V IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, procedure 23-10-02-01A-421A-A;

remove and reinstall the failed components IAW the Repair IETM column listed in TABLE V; and execute the Comm 2 AN/ARC-210(V) System Function Test with no failure indications after the failed component has been repaired.

TABLE V Comm 2 AN/ARC-210(V) System failed components

Multifunctional Information Distribution System (MIDS) IBIT

1. replicate the CH-53K MIDS IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR;

have a MIDS comprised of actual and/or simulated components, with the fidelity required to facilitate system component identification and perform function tests, fault isolation procedures, removal, repairs, and installations associated with the components IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR;

contain the components, subcomponents, and hardware to execute the MIDS Function Test with no failure indication IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, procedure 23-11-00-01A-340A-A, excluding steps 6-7;

have IOS controls to insert and remove Fault Codes and Fault Conditions listed in TABLE VI for MIDS functional IBIT test;

perform MIDS functional IBIT Function Test with the indicated Fault Codes and Fault Conditions listed in TABLE VI IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, procedure 23-11-00-01A-340A-A;

perform fault isolation procedures per the Fault Codes and Fault Conditions listed in TABLE VI IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, procedure 23-11-00-01A-421A-A;

remove and reinstall the failed components IAW the Repair IETM column listed in TABLE VI; and execute the MIDS Function Test with no failure indications after the failed component has been repaired.

TABLE VI MIDS failed components

Satellite Communications (SATCOM) System IBIT

1. replicate the CH-53K SATCOM System IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR;

have a SATCOM System comprised of actual and/or simulated components, with the fidelity required to facilitate system component identification and perform function tests, fault isolation procedures, removal, repairs, and installations associated with the components IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR;

contain the components, subcomponents, and hardware to execute the SATCOM System Function Test with no failure indication IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, procedure 23-15-00-01A-340A-A;

have IOS controls to insert and remove Fault Codes and Fault Conditions listed in TABLE VII for SATCOM System functional IBIT test;

perform SATCOM System functional IBIT Function Test with the indicated Fault Codes and Fault Conditions listed in TABLE VI IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, procedure 23-15-00-01A-340A-A;

have ability to perform fault isolation procedures per the Fault Codes and Fault Conditions listed in TABLE VI IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, procedure 23-15-00-01A-421A-A;

remove and reinstall the failed components IAW the Repair IETM column listed in TABLE VI; and execute the SATCOM System Function Test with no failure indications after the failed component has been repaired.

TABLE VII SATCOM System failed components

Inter-Communication System (ICS) IBIT

1. replicate the CH-53K ICS IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR;

have an ICS comprised of actual and/or simulated components, with the fidelity required to facilitate system component identification and perform function tests, fault isolation procedures, removal, repairs, and installations associated with the components IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR;

contain the components, subcomponents, and hardware to execute the ICS Function Test with no failure indication IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, procedure 23-50-00-01A-340A-A, excluding steps 5-11;

have IOS controls to insert and remove Fault Codes listed in TABLE VIII for ICS functional IBIT test;

perform ICS functional IBIT Function Test with the indicated Fault Codes listed in TABLE VIII IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, procedure 23-50-00-01A-340A-A;

perform fault isolation procedures per the Fault Codes listed in TABLE VIII IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, procedure 23-50-00-01A-421A-A;

remove and reinstall the failed components IAW the Repair IETM column listed in TABLE VIII; and execute the ICS Function Test with no failure indications after the failed component has been repaired.

TABLE VIII ICS failed components

Alternating Current (AC) Power System IBIT

1. replicate the CH-53K AC Power System IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR;

have an AC Power System comprised of actual and/or simulated components, with the fidelity required to facilitate system component identification and perform function tests, fault isolation procedures, removal, repairs, and installations associated with the components IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR;

contain the components, subcomponents, and hardware to execute the AC Power System Function Test with no failure indication IAW the latest version A1-CH53K-IETM-MMO-000 available 30 days prior to PDR, procedure 24-20-00-01A-340A-A, excluding steps 6-7;

have IOS controls to insert and remove Fault Codes and Fault Conditions listed in TABLE IX for AC Power System functional IBIT test;

perform AC Power System functional IBIT Function Test with the indicated Fault Codes and Fault Conditions listed in TABLE IX IAW the latest version A1-CH53K-IETM-MMO-000 available 30…