Order Description_TH-1H Standby Turn Rate Indicator Battery Backup (04 Aug 2023).pdf

PR FD2060-23-31231 Page 1 of 2

Multiple Award Contract for Modifications (MACM)

ORDER DESCRIPTION

Modification Upgrade of the

TH-1H Standby Turn Rate Indicator and Battery Backup Source

04 August 2023

1. BACKGROUND: The subject modification upgrade is a validated requirement from 1067 AETC 20-027, Standby Turn Rate Indicator and Source with Battery Backup and AETC 20-030, Standby Attitude Indicator Battery Backup. The TH-1H only has one source of turn rate: the Attitude and Heading Reference System (AHRS). The Standby Instrumentation located between the Pilot and Center Multi- Functional Displays contain all necessary flight instruments (Attitude Indicator, Airspeed Indicator, Barometric Altimeter, Vertical Speed Indicator, and Magnetic Heading Indicators [located outboard of the instrument panel at both pilot and co-pilot's stations]) except for rate of turn indication. The addition of a standby rate of turn indication would provide critical turn rate information while operating in Instrument Meteorological Conditions (IMC) conditions with a failed AHRS. In addition, there is no dedicated backup power source providing power to this standby instrumentation, including the attitude indicator and backlighting, in the event of electrical failure.

2. SCOPE:

a. Standby Rate of Turn Indication. The contractor shall provide and install a Standby Rate of Turn Indication in the form of a Commercial-off-the-Shelf (COTS), combination attitude/rate-of-turn/slip indicator, capable of replacing the existing standby attitude indicator. Due to space concerns, the indicator size must not exceed the size of other standby instrumentation already installed and which meets the requirements of AETC 20-027 Appendix A – Air Education and Training Command (AETC), TH-1H Aircraft – Standby Rate of Turn Indication.

b. Battery Backup Source. The contractor shall provide and install an emergency standby power/battery backup system capable of supporting the standby instrumentation, associated backlighting, and which meets the requirements of AETC 20-030 Appendix A – Air Education and Training Command (AETC), TH-1H Aircraft – Emergency Battery Backup System for an objective period of 1 hour.

c. This effort will require the Contractor to perform non-recurring engineering (NRE) for integration, development of modification Time Compliance Technical Order (TCTO), Technical Data Package (TDP), Technical Order (TO) updates, prototype and verification installations, prototype manufacturing/delivery, TO validation/verification, and testing and delivery of Production Kits, and provisioning.

d. There are 28 TH-1H aircraft affected by this modification located at Cairns Army Airfield, Fort Novosel (formerly Fort Rucker), AL. This effort includes installation of 28 kits (1 trial install kit, 1 kit proof kit, and 26 production install kits), consisting of an upgraded standby attitude indicator with rate of turn indication and battery backup source. In addition, this effort includes the procurement of 5 each initial spares (1 indicator + 1 battery backup system, when combined, constitutes a single spare).

3. DESCRIPTION OF REQUIREMENT TASKS: This order does not require specific delineation from the baseline SOW Revision B, as written (dated 27 Sep 2021).

PR FD2060-23-31231 Page 2 of 3

a. The SOW paragraphs listed below are applicable for this delivery order and must be addressed in the proposal:

TABLE OF CONTENTS

1 Description of Supplies/Services

1.1 Objective(s)

1.1.1 Support

1.2 Benefit to the United States Air Force (USAF)

2 Government Property and Services

2.1 Government Property

2.2 Government Property to be Provided

2.3 Government Furnished Information (GFI)

2.4 Reporting of Government Property

2.5 Loss of Government Property

2.6 Return/Retention of Government Property

2.7 Government Systems

3 Technical Requirements

3.1 Period and Place of Performance

3.1.1 Contract/Order Period of Performance

3.1.2 Place of Performance

3.2 Item Unique Identification (IUID)

3.3 Kit Packaging, Handling, Shipping, and Transportation

3.3.1 Packaging and Handling

3.3.2 Shipping/Transportation

3.4 Counterfeit Electronic Parts

3.5 Government-Industry Data Exchange Program (GIDEP)

3.6 Travel

3.7 Diminishing Manufacturing Sources/Material Shortages (DMS/MS)

3.8 Cybersecurity Implementation

3.8.1 Cybersecurity Workforce

3.8.2 Reserved

3.9 Engineering

3.9.1 Engineering Data

3.9.1.1 Restrictions on use of Proprietary Material

3.9.1.2 Reserved

3.9.2 System Integration

3.9.3 Proof of Concept Fabrication

3.9.4 Airworthiness

3.9.5 Validation and Verification

3.9.6 Trial Installation (TI) Kit

3.9.7 Kit Proof (KP)/Production Kits

3.9.8 Production Installation

3.9.9 Test Procedures

3.9.9.1 Ground and Flight Testing

3.9.9.2 System and Component Testing

3.9.10 Software

3.9.10.1 Software Requirements and Feasibility Analysis

3.9.10.2 Software Process

3.9.10.3 Software Design

3.9.10.4 Software Implementation

3.9.10.5 Software Test and Evaluation

3.9.10.6 Software Validation

3.9.10.7 Software Verification

3.9.10.8 Software Documentation

3.9.10.9 Software Configuration Management

3.9.10.10 Software Ownership and Rights

PR FD2060-23-31231 Page 3 of 4

3.9.10.11 Development of New Software

3.9.10.12 Modification of Existing Software

3.9.10.13 Software Sustainment

3.9.11 Systems Engineering

3.9.12 Human Factors Engineering

3.10 Technology Insertion and Systems Integration

3.11 Systems Installation and Integration

3.12 Standard Items

3.13 Producibility

3.14 Source Qualification

3.15 Laboratory Services

3.16 Certifications

3.17 Product Data Management

3.18 Configuration Management (MIL-STD-973)

3.19 Configuration Data Management

3.20 Contractor Requirements

3.21 Program Management

3.22 Subcontractor Management

3.22.1 Associated Contractor Agreement (ACA)

3.22.2 Reserved

3.23 Multi-functional Team (MFT)

3.24 Contractor Furnished Materials and Equipment

3.25 Facilities Requirement

3.26 Management Meetings and Reviews

3.26.1 Post Contract Award Conferences

3.26.2 Technical Interchange Meetings (TIM)

3.26.3 Design Reviews/Audits

3.26.4 Performance Reviews

3.26.5 Provisioning

3.26.6 Engineering Data Guidance Conference

3.26.7 In-Process Review (IPR) of the TDP

3.26.8 Relationship of Contractor with Subcontractors/Vendors

3.26.9 Engineering Data Updates and Revisions

3.27 Order Requirements

3.27.1 Conflicting Requirements

3.27.2 Administration

3.28 Order Deliverables

3.28.1 Data Requirements

3.28.1.1 Documentation

3.28.1.2 Time Compliance Technical Order (TCTO)

3.28.1.3 Technical Orders (TOs)

3.28.2 Funds Status Report

3.28.3 Integrated Master Schedule (IMS)

3.28.4 Monthly Status Reports

3.28.5 Final Report

3.29 Risk Management

3.30 Field Representation

3.30.2 Reserved

3.31 Publications

3.32 Quality Control Provisions

PR FD2060-23-31231 Page 4 of 5

3.33 Program Protection Plan (PPP)

3.34 Non-Development Items (NDIs)

3.35 Commercial Processes and Technologies

3.36 Over and Above (O&A)

3.36.1 O&A Non-Mod Related

3.36.2 Engineering Configuration Mod Related Changes

4 General Information

4.1 Continuation of Mission-Essential Services During a Crisis

4.2 Security Requirements

4.2.1 Security Regulations

4.2.2 Operations Security (OPSEC)

4.2.3 Communications Security (COMSEC)

4.2.4 Security Clearances

4.2.5 Security Incidents and Violations

4.2.6 Security of Contractor System(s)

4.2.7 Release and Removal of Documentation

4.2.8 Access to Government Facility or Military Installation

4.2.9 Prohibitions against Unauthorized Disclosures

4.3 Environmental Management System (EMS)

4.3.1 Safety and Environmental

4.3.2 System Safety and Health Hazards

4.3.3 Hazardous Materials

4.4 Affirmative Procurement Programs (APP)

4.4.1 Contractor’s Purchasing Systems

4.4.2 Contractor’s Purchasing System Reviews (CPSR)

4.5 Safety Requirements

4.5.1 Contractor Compliance

4.5.2 Mishap Notification/Investigation

4.5.3 Safety and Health Plan

4.6 Inspection of Services

4.7 Trafficking in Persons

4.8 Invoicing/Payment and Receipt/Acceptance

5 Appendices

5.1 Appendix A: References

5.2 Appendix B: Acronyms

5.3 Appendix C: Sample Contract Data Requirements List (CDRL)

5.4 Appendix D: SOF/PR and Rotary Systems Engineering Plan (SEP)

5.5 Appendix E: SOF/PR and Rotary Technical Manual Contract Requirements (TMCR)

b. The SOW paragraphs listed below are not applicable for this delivery order:

1.1.2 Quality Assurance Surveillance Plan (QASP)

3.30.1 Interim Contract Support/Contractor Logistics Support (ICS/CLS)

4.9 Earned Value Management (EVM)

4. TRAVEL: The Contractor may be required to travel during the performance of this effort. Travel will be executed and authorized IAW paragraph 3.6 Travel of the MACM SOW Revision B, as written (dated 27 Sep 2021).

PR FD2060-23-31231 Page 5 of 6

5. DELIVERABLES:

a. The following CDRLS from the Basic IDIQ are required for this delivery order (TBD CDRLs at the bottom of this list will be identified on MACM SOW Rev B):

Sequence Number Title Data Item

Description

SOW

Paragraph Basic/Option Deliverable Send To

A001 Conference Agenda DI-ADMN-81249B 3.21, 3.26,

3.26.7 Both ABC

A002 Conference Minutes DI-ADMN-81250B 3.21, 3.26,

3.26.7 Both ABC

A005

Final System Security Plan - Naval Aviation Cybersecurity Risk Management Framework (RMF) Assessment And Authorization Products, And CYBERSAFE Objective Quality Evidence, Assessment & Authorization (A&A) Products

DI-MGMT-82135 3.8 Basic AELM

A006 Time Compliance Technical Order (TCTO) Supply Data DI-ALSS-81531 3.28.1.2 Basic ADGH

A007 Validation Report DI-CMAN-80792A 3.9.5 Basic ADE

A009 Security Control Traceability Matrix (SCTM) - Dod Risk Management Framework (RMF) Package Deliverables

DI-MGMT-82001 3.8 Basic AELM

A00C Program Environmental Safety And Health Evaluation (PESHE) DI-ENVR-81840 4.3.1, 4.3.2 Basic ADEFGH

A00K System/Subsystem Specification (SSS) DI-IPSC-81431A 3.9.10 Basic ADE

A00M Software Requirement Specification (SRS) DI-IPSC-81433A 3.9.10.1 Basic ADEL

A00N Interface Requirements Specification (IRS) DI-IPSC-81434A 3.9.10 Basic ADE

A00P Software Design Description (SDD) DI-IPSC-81756 3.9.10.3 Basic ADEL A00U Software Version Description (SVD) DI-IPSC-81442A 3.9.10.9 Basic ADEL A00V Software Users Manual (SUM) DI-IPSC-81443A 3.9.10 Basic ADEL

A00Z

Final Security Assessment Plan - Naval Aviation Cybersecurity Risk Management Framework (RMF) Assessment And Authorization Products, And CYBERSAFE Objective Quality Evidence, Assessment & Authorization (A&A) Products

DI-MGMT-82135 3.8 Basic AELM

A010 Management Plan DI-MGMT-80004A 3.21 Basic ABC

A011 Site Preparation Requirements And Installation Plan DI-MGMT-80033A 3.9.6, 3.9.8 Both ADEFGH

A012 Engineering And Technical Services Accomplishment Report DI-MGMT-80061A 3.9.11 Both ADEF

A014 Status Of Government Furnished Equipment (GFE) Report DI-MGMT-80269 2.2, 3.21 Both ABCDEG

H

A015 Status Report DI-MGMT-80368A 2.4, 3.28.3,

3.28.4 Both ABCL

A017 Weight And Balance Report for Aircraft DI-MGMT-81501A 3.9 Both ADEF A018 Project Planning Chart DI-MGMT-80507C 3.21 Both ABCDE A01F Contractor's Risk Management Plan DI-MGMT-81808 3.29 Both ABCDE

A01P Final System Authorization Boundary Diagram - Dod Risk Management Framework (RMF) Package Deliverables

DI-MGMT-82001 3.8 Basic AEL

A01S Technical Report - Study/Services DI-MISC-80508B 3.28.1.1 Basic ADEFGH

PR FD2060-23-31231 Page 6 of 7

A01T Scientific And Technical Reports DI-MISC-80711A 3.9, 3.9.4, 3.9.9.2, 3.9.12, 3.10 Basic ADE

A01W Final Information Technology (IT) Determination-DoD Risk Management Framework (RMF)Package Deliverables

DI-MGMT-82001 3.8 Basic AEL

A01Z Test/Inspection Report DI-NDTI-80809B 3.9.9 Both ADE

A020 Test and Evaluation Program Plan

(TEPP) DI-NDTI-81284 3.9.9 ADE

A028 Installation Specification DI-QCIC-80510 3.25 Both ADEGH A029 Acceptance Test Plan DI-QCIC-80553A 3.9.9 Basic ADEFGH

A02L System Safety Hazard Analysis Report (SSHAR) DI-SAFT-80101C 4.5.3 Basic ADEGH

A02M Safety Assessment Report (SAR) DI-SAFT-80102C 4.5.3 Basic ADEGH

A02P Accident/Incident Report DI-SAFT-81563 4.5.2 Both ABCDEG H

A02Q Parts Management Plan DI-SDMP-81748 3.26.5 Basic ADEGHI A02R Failure Summary And Analysis Report DI-SESS-80255A 3.9 Basic ADEGH A02T Engineering Change Proposal (ECP) DI-SESS-80639D 3.9.11 Both ABCDEF

A02X Product Drawing/Models and Associated Lists DI-SESS-81000F 3.17 ADE

A02Y Configuration Audit Summary Report DI-SESS-81022D 3.18 Basic ADEF A02Z Reliability And Maintainability Report DI-SESS-81497A 3.1 Basic ADEGH

A030 Reliability And Maintainability (R&M) Program Plan DI-SESS-81613A 3.1 Basic ADEGH

A033 Airworthiness Certification Criteria Report DI-SESS-81768 3.9.4 Basic ADEF

A034 System Engineering Management Plan (SEMP) DI-SESS-81785A 3.9.11 Basic ADEF

A035 Engineering Data for Provisioning (EDFP) DI-SESS-81874 3.26.5 Both ADEGH

A038

Technical Manual (TM) Contractor Furnished Aeronautical Equipment Or Contractor Furnished Equipment (CFAE/CFE) Notices

DI-TMSS-80067C 3.24 Basic ADE

A039 Commercial Off-The-Shelf (COTS) Manual And Associated Supplemental Data

DI-TMSS-80527C 3.10, 3.27 Basic ADEFGH

A03A Technical Manual TM-86-01N 3.28.1.3 Basic ADEFGH

A03C Failure Modes, Effects And Criticality Analysis Report (FMECA) DI-SESS-81495B 3.9.11 Basic ADE

A03D System Subsystem Design Description DI-IPSC-81432A 3.9 Basic ADE A03E Still Photo Coverage DI-MISC-80169 3.18 Both ADE

A03F Engineering Documentation Product Drawings, Modified (Maintenance) DI-DRPR-81681A 3.9 Basic ADEFGH

A03H Technical Manual Research and Analysis Source Data DI-TMSS-81354 3.9, 3.28.1 Basic ADEGH

A03J Test Plan DI-NDTI-80566A 3.8, 3.9 Basic ADEF A03M Interface Control Document DI-SESS-81248B 3.9 Basic ADE A03N Software Documentation DI-IPSC-81756 3.9.10.8 Basic ADEL

A03P Deficiency Report (DR) DI-PSSS-81535 3.9, 3.10,

3.11 Basic ADE

PR FD2060-23-31231 Page 7 of 8

b. The contractor shall provide a list of hardware and software with the information listed in Table 1:

Hardware components list and Table 2: Software components list.

c. The contractor shall answer questions about the configuration and security implementation of the indicator during the period of performance reportable as part of the monthly status report. (CDRL

A015 DI-MGMT-80368A).

d. Diminishing Manufacturing Sources/Material Shortage (DMS/MS) (MACM SOW Rev B, paragraph 3.7): Results of DMSMS efforts shall be reported as part of the monthly status report. (CDRL A015

DI-MGMT-80368A)

e. Electronic distribution for each CDRL will be emailed to the following addresses as indicated:

A - shawn.drake.3@us.af.mil B – tarha.mazyck.2@us.af.mil C - gregory.hendricks.3@us.af.mil D - johnny.mangum@us.af.mil E - AFLCMC.WIUE.RotaryWing@us.af.mil F - thuydan.ngo@us.af.mil

G - john.mims.4@us.af.mil H - wendell.peavy.1@us.af.mil J - jarius.jones@us.af.mil K - keonne.ross@us.af.mil L - michelle.osborne.1@us.af.mil mailto:tarha.mazyck.2@us.af.mil mailto:johnny.mangum@us.af.mil mailto:thuydan.ngo@us.af.mil mailto:john.mims.4@us.af.mil mailto:wendell.peavy.1@us.af.mil mailto:jarius.jones@us.af.mil mailto:cheryl.walker.3@us.af.mil mailto:michelle.osborne.1@us.af.mil

Appendix A:

Air Education and Training Command (AETC), TH-1H Aircraft Standby Rate of Turn Indication and Emergency Battery Backup System

References:

FAR 14 CFR 29.1303 – Flight and Navigation Instruments FAA AC 29-2C – Certification of Transport Category Rotorcraft FAA AC 20-184 – Guidance on Testing and Installation of Rechargeable Lithium Battery Systems FAA AC 20-192 – Lithium Batteries TSO C4c – Attitude Indicator TSO C3b – Turn and Slip Indicator TSO C113a – Airborne Multipurpose Electronic Instruments TSO C179b – Lithium Batteries MIL-HDBK-516 – Airworthiness

General

AETC 20-027:

The TH-1H only has one source of turn rate, a single Attitude and Heading Reference System (AHRS) that displays rate of turn on the Pilot and Copilots Multi-Function Control Displays (MFCD). If the AHRS fails, there is no backup turn rate source or indication. Turn rate information is critical to maintaining aircraft control in IMC. The Standby Instrumentation located between the Pilot and Center Multi- Functional Displays contains all necessary flight instruments (Attitude, Airspeed, Barometric Altimeter, and Vertical Speed) except for a Rate of Turn Indicator. According to 14 Code of Federal Regulations § 29.1303(g), Flight and Navigation Instruments, a gyroscopic rate-of-turn indicator combined with an integral slip-skid indicator is a required flight instrument. The addition of a standby rate of turn indication would provide critical turn rate information for Instrument Meteorological Conditions (IMC) flight with a failed AHRS turn rate source/indication.

AETC 20-030:

There is no dedicated backup power source that provides emergency power to the standby instrumentation, including any standby instrumentation backlighting, in the event of complete electrical failure. The standby attitude indicator is powered by the same electrical bus as the AHRS system which provides primary attitude information to the Pilot and Copilots MFCD. In the event of electrical failure in IMC, there is a complete loss of required flight instrumentation. Loss of attitude reference in IMC would lead to loss of aircraft control, resulting in the loss of aircraft and crew.

AETC 20-027, Rate of Turn Indication

The contractor shall provide a standby attitude indicator with rate-of-turn indication that possesses, at minimum, the following salient characteristics, features or capabilities:

1. Integrate a replacement standby attitude indicator that contains an integral rate of turn indicator, slip-skid indicator and holds a Federal Aviation Administration (FAA) Technical Standard Orders (TSO) of TSO-C3e, TSO-C4c and TSO-113a.

2. The indicator form factor shall be the 3” bezel/case style.

3. The indicator shall provide a 2-minute turn (3 degree/sec) rate of turn indication.

4. The indicator shall operate independently of any other attitude indicating systems.

5. The indicator shall be NVIS compatible.

6. The indicator shall be powered from the STBY INST circuit breaker common to the existing standby instrumentation (See Figure 3).

7. The indicator shall replace the existing standby attitude indicator (See Figures 1 & 7).

8. The contractor shall include information about known cyber vulnerabilities and evidence of cyber hardening of the rate-of-turn indicator.

AETC 20-030 Emergency Standby Power/Battery Backup

The contractor shall integrate an emergency standby/battery backup system capable of powering the standby flight instrumentation and the associated instrument backlighting, for up to one (1) hour during a total loss of aircraft electrical power. The emergency standby/battery backup system shall possess, at minimum, the following salient characteristics, or capabilities:

1. The battery backup shall be capable of suppling +28VDC emergency power to the standby attitude indicator with rate-of-turn indication (See Figures 1, 5, 6 & 7):

2. The battery backup shall be capable of suppling emergency power for backlighting for the following standby instrumentation (See Figures 1, 5 & 6):

(a) Standby attitude indicator w/ rate of turn indication

(b) Standby airspeed indicator

(c) Standby barometric altimeter

(d) Standby vertical velocity indicator

3. The battery backup shall be capable of supplying emergency power for backlighting the following instruments (See Figures 1, 5 & 6):

(a) Pilot and Copilot – Clocks

(b) Pilot and Copilot – Compasses

4. The emergency standby/battery backup shall hold an FAA Technical Standard Order (TSO)

TSO-C179a (or greater).

5. The emergency standby/battery backup shall be environmentally certified to DO-160F (or greater).

6. The battery backup shall be charged from the existing +28VDC Essential DC bus when not providing emergency standby power.

7. The battery backup system shall be designed so that following the loss of electrical power the battery backup will automatically provide emergency power without the need for flight crew action.

8. The battery backup system shall be designed so that emergency power is only provided in the event of:

(a) Total loss of aircraft electrical power, or

(b) When intentionally selected ON by the flight crew

9. The battery backup system shall be designed such that the failure of the primary electrical generation system does not interfere with the proper supply of power from the battery backup system.

10. The battery backup system shall provide an indication to the flight crew any time emergency power is discharging or supplying power to the standby instrumentation.

11. The battery backup system shall provide the flight crew with the ability to determine the battery’s current state of charge either through a system self-test or direct indication.

12. The battery backup system shall provide a means for the flight crew to turn the system OFF manually.

13. The existing instrument panel lighting circuit, as controlled by the INST PANEL lighting rheostat and the STBY INST rheostat, shall be modified so that the circuit is powered from the emergency standby/battery backup bus when emergency power is in use (See Figure 2).

Figure 1 – TH-1H Instrument Panel Layout

Figure 2 – TH-1H Instrument Panel Layout (Con’t)

Figure 3 – TH-1H Center Console Layout

Figure 4 – TH-1H Overhead Circuit Breaker Panel

Figure 5 – TH-1H Power Generation System Block Diagram

Figure 6 – TH-1H 5VDC Lighting Wiring Diagram

Figure 7 – TH-1H 5VDC Lighting Wiring Diagram (Cont’d)

Figure 8 – TH-1H Standby Attitude Indicator Characteristics

Table 1: Hardware Components List

Hardware Components Manufacturer Highest Classification Memory Removable Media Front Panel Interface Maintenance Interface

<name of indicator component>

<Who manufactures the component?>

<Does the hardware process classified information?>

<Is memory used?

What type?>

<Is removable media used? What type?> <Is there a front panel or other user interface?> <Is there a maintenance panel or other maintainer interface?>

Table 2: Software Components List

Hardware Component Software (with version) Developer Loading Highest Classification

<What part of the indicator uses software?> <Name of software and current approved version?> <Who developed the software?> <How is the software loaded and/or updated?>

<Is the software classified?>