Exhibits.pdf

DATA ITEM DESCRIPTION

Title: PRODUCT ENGINEERING DESIGN DATA AND ASSOCIATED LISTS Number: DI-SESS-81000F Approval Date: 20190417 AMSC Number: 10017 Limitation:

DTIC Applicable: GIDEP Applicable:

Preparing Activity: AR Project Number: SESS-2019-023 Applicable Forms:

Use/relationship: Product Engineering Design Data and Associated Lists provide engineering data adequate to serve as an authoritative and complete technical description of an item. This data, when authorized, is adequate to support competitive procurement and maintenance for items interchangeable with the original items. This data represents the highest level of design disclosure.

a. This Data Item Description (DID) contains the format and content preparation instructions for Product Engineering Design Data and Associated Lists resulting from the work task described in 5.4.1.3 of MIL-STD-31000.

b. This DID is applicable to acquisitions of military systems, equipment, and components. It is intended for acquiring Product Engineering Design Data and Associated Lists at the end of the Engineering and Manufacturing Development Phase and during subsequent phases of the DoD materiel life cycle.

c. It is not intended that all the requirements contained herein should be applied to every program. This DID should be tailored to the minimum data requirements of the applicable contract or purchase order.

d. This DID is related to DI-SESS-81001F, DI-SESS-81002F, and DI-SESS-81003F. This DID supersedes DI-SESS-81000E.

e. A purchased item, as defined by ASME Y14.24, an item which is sold or traded in the course of conducting normal business operations, is used by commercial industry, or is a specialized version of a supplier's general product line which he routinely customizes. Purchased items as used herein have also been referred to as vendor items or vendor-developed items.

Requirements:

1. Reference documents. The applicable issue of the documents cited herein, including their approval dates and dates of any applicable amendments, notices, and revisions, shall be as specified in the contract.

2. General. Product Engineering Design Data and Associated Lists shall meet the requirements of MIL- STD-31000. Product Engineering Design Data and Associated Lists shall provide the design disclosure information necessary to serve as a clear, complete and accurate technical description of an item sufficient to enable a manufacturer of similar products at the same or similar state of the art to produce and maintain quality control of item(s) so that the resulting physical and functional characteristics duplicate those of the specified item. These design data shall:

a. Reflect the end product at its current level of design maturity.

This data, when authorized, is adequate to support competitive procurement and maintenance for items interchangeable with the original items. This data repre

Design Data and Associated Lists resulting from the work task described in 5.4.1.3 of MIL-STD-31000.

components. It is intended for acquiring Product Engineering Design Data and Associated Lists at the end of the Engineering and Manufacturing Development Phase and during subsequent phases of the DoD materiel life cycle. of

c. It is not intended that all the requirements contained herein should be applied to every program. This DID should be tailored to the minimum data requirements of the applicable contract or purchase order.

This DID is related to DI-SESS-81001F, DI-SESS-81002F, and DI-SESS-81003F.

e. A purchased item, as defined by ASME Y14.24, by an item whichan is sold or traded in the in course of conducting normal business operations, is used by commercialby industry, or is a specialized version of a supplier's general product line which he routinely customizes. Purchased items as used herein have also been referred to as vendor items or vendor-developed items.

General. Product Engineering Design Data and Associated Lists shall meet the requirements of MIL-

STD-31000.

sufficient to enable a manufacturer of similar products at the same or similar state of the art to produce and maintain quality control of item(s) so that the resulting physical and functional characteristics duplicate those of the specified item. of the specified item. of

DI-SESS-81000F

b. Provide the engineering data for logistics support products.

c. Provide the necessary data to permit competitive acquisition and manufacture of the original item(s).

3. Format. Product Engineering Design Data and Associated Lists shall be in either the contractor's format or the Government's format as specified on the TDP Option Selection Worksheet incorporated into the contract or purchase order.

4. Content. Product Engineering Design Data and Associated Lists shall conform to the requirements of ASME Y14.100, or, if applicable, ASME Y14.100 and Appendices B through E, as required, ASME Y14.34, ASME Y14.41 and/or ASME Y14.41.1. They shall document directly or by reference the following, as applicable:

a. Details of unique processes, i.e., not published or generally available to industry, when essential to design and manufacture.

b. Performance ratings.

c. Dimensional and tolerance data

d. Critical manufacturing processes and assembly sequences.

e. Toleranced input and output characteristics.

f. Diagrams.

g. Mechanical and electrical connections.

h. Physical characteristics, including form, finishes, and protective coatings.

i. Details of material identification, including material condition, and mandatory treatments and coatings.

j. Inspection, test and evaluation criteria.

k. Equipment calibration requirements.

l. Quality assurance requirements.

m. Hardware marking requirements.

n. Requirements for reliability, maintainability, environmental conditioning, shock and vibration testing and other operational or functional tests.

o. Vendor substantiation data when required by the contract or purchase order.

c. Provide the necessary data to permit competitive acquisition and manufacture of the original item(s).

or the Government's format as specified on the TDP Option Selection Worksheet incorporated into the contract or purchase order.

shall conform to the requirements of ASME Y14.100, or, if applicable, ASME Y14.100 and Appendices B through E, as required, ASME Y14.34, ASME Y14.41 and/or ASME Y14.41.1. They

d. Critical manufacturing processes and assembly sequences.

e. Toleranced input and output characteristics.

Details of material identification, including material condition, and mandatory treatments and coatings.

k. Equipment calibration requirements.

l. Quality assurance requirements.

m. Hardware marking requirements.

Requirements for reliability, maintainability, environmental conditioning, shock and vibration shock testing and other operational or functional tests.

DI-SESS-81000

p. Requirements for programming software into devices or assemblies including a description of the input media and the procedures for validating that the software has been installed correctly.

q. Special consideration items and processes.

5. Item definition. All parameters required to define each unit, assembly, subassembly, part or material shall be presented on the applicable design data document. This includes data such as:

a. All necessary mechanical dimensions to fully define fabrication, acceptance, interface or installation of the item depicted.

b. All necessary electrical parameters to fully define fabrication, acceptance, interface or installation of the item depicted.

c. All other necessary physical parameters to fully define fabrication, acceptance, interface or installation of the item depicted, i.e., weight, pressure, viscosity, etc.

d. All necessary environmental conditions which units, assemblies, subassemblies, parts and materials must meet to perform effectively in the end item, such that the end item will meet its specification requirements.

6. CAGE code and document numbers. Product Engineering Design Data and Associated Lists shall be identified with the contractor's CAGE code and contractor document numbers or with a Government CAGE code and document numbers as specified in the TDP Option Selection Worksheet incorporated in the contract or purchase order.

7. Selection of design data. The types of design data (e.g. drawings, models, 3Di viewables, etc.) required shall be as stated in the TDP Option Selection Worksheet incorporated in the contract or purchase order.

7.1. Vendor Item Control Documents. Vendor Item Control Documents shall be used to specify the requirements for purchased items when such items have been approved for use in the design and are used without alteration, selection or source qualification (testing of an item prior to procurement action to ensure that it satisfies the specified requirements).

7.2. Source Control Documents. Source Control Documents shall be used to specify the requirements for purchased items only when such items have been approved for use in the design and:

a. the item is for a critical application and

b. the requirements can be met by an item from one or more sources and

c. the application required source qualification (testing of an item prior to procurement action to ensure that it satisfies the specified requirements).

7.3. Standard Microcircuit Drawings. Standard Microcircuit Drawings (MIL-HDBK-780) shall be used to specify the requirements of microcircuits.

End of DI-SESS-81000F.

p. Requirements for programming software into devices or assemblies including a description of the input media and the procedures for validating that the software has the procedures for validating that been installed correctly.

q. Special consideration items and processes.

c. All other necessary physical parameters to fully define fabrication, acceptance, interface or installation of the item depicted, i.e., weight, pressure, viscosity, etc.

d. All necessary environmental conditions which units, assemblies, subassemblies, parts and materials must meet to perform effectively in the end item, such that the end item will meet its specification requirements.

or with a Government CAGE code and document numbers as specified in the TDP Option Selection Worksheet incorporated in the contract or purchase order.

TDP Option Selection Worksheet incorporated in the contract or

7.1. Vendor Item Control Documents. Vendor Item Control Documents shall be used to specify the requirements for purchased items when such items have been approved for use in the design and are used without alteration, selection or source qualification (testing of an item prior to procurement action to ensure that it satisfies the specified requirements).

7.2. Source Control Documents. Source Control Documents shall be used to specify the requirements for purchased items only when such items have been approved for use in the design and:

a. the item is for a critical application and

b. the requirements can be met by an item from one or more sources and

c. the application required source qualification (testing of an item prior to procurement action to ensure that it satisfies the specified requirements).

Title: ANALYTICAL CONDITION INSPECTION (ACI) REPORT

Number: DI-MISC-81391A Approval Date: 20180326

AMSC Number: F9914 Limitation: N/A

DTIC Applicable: No GIDEP Applicable: No

Preparing Activity: 11 (AFLCMC/EZFS) Project Number: MISC-2018-008

Applicable Forms: N/A

Use/Relationship: The Analytical Condition Inspection (ACI) Report will be used to reveal damage (flaw, defect, crack, corrosion, disbond, delamination, discontinuity, or other type that degrades or has the potential to degrade the performance of the affected component) that may not otherwise be detected through normal technical order (TO) and programmed depot maintenance (PDM) inspections and to provide data for engineering and technical evaluations of the relative condition of the mission, design and series (MDS) aircraft. Data generated through ACI Reports is used to refine mandatory aircraft inspection programs (field and depot).

This DID contains the format, content and intended use information for the data deliverable resulting from the technical requirements described in Task V of MIL-STD-1530, Aircraft Structural Integrity Program (ASIP), and Subtask 3 of MIL-STD-1798, Mechanical Equipment and Subsystems Integrity Program.

(Copies of these documents are available online at http://quicksearch.dla.mil.)

Requirements:

1. Reference Documents. The applicable issue of the documents cited herein, including their approval dates and dates of any applicable amendments, notices, and revisions, shall be as specified in the contract.

2. Format. The ACI Report shall be in the contractor’s format.

3. Content. The ACI Report shall include the following information:

3.1 ACI Work Instructions - for each inspection/inspection location:

a. Identification number.

b. Part name/description of article to be inspected.

c. Part number(s).

d. Part criticality – safety or fracture critical, durability or maintenance (Mx) critical, normal controls, etc.

e. Area/location of inspection.

f. Reason for inspection.

DISTRIBUTION STATEMENT A. Approved for public release. Distribution is unlimited.

inspections and to provide data for engineering and technical evaluations and series (MDS) aircraft. Data generated condition of the mission, design (MDS) aircraft. Data generated through ACI Reports is used to refine mandatory aircraft inspection programs (field and through ACI depot).

degrades or has the potential to degrade the performance of the affected component) and programmed depot may not otherwise be detected through normal technical order maintenance (PDM) format, resulting from the technical requirements described in Task V of MIL-STD-1530, resulting requirements

Aircraft Structural Integrity Program (ASIP), and Subtask 3 of MIL-STD-1798, Mechanical Aircraft Structural Integrity Program (ASIP), and Subtask 3 of MIL Equipment and Subsystems Integrity Program.

(Copies of these documents are available online at http://quicksearch.dla.mil.)

c. Part number(s).

d. Part criticality – safety or fracture critical, durability or maintenance (Mx) critical, Part criticality safety or fracture critical, durability or normal controls, etc.

f. Reason for inspection.

DI-MISC-81391A

g. Frequency of inspection.

h. Type of inspection.

i. Instructions for accessing article to be inspected.

j. Inspection procedures and potential/anticipated damage.

3.2 ACI Inspection Results:

a. Pertinent aircraft identifying information:

(1) Aircraft mission design series (MDS).

(2) Aircraft serial number (SN).

(3) Base assignment history.

(4) Planned ACI start and end date.

(5) Actual ACI start and end date.

(6) Actual flight hours.

(7) Equivalent flight hours.

(8) Last programmed depot Mx date.

b. Information for each inspection location:

(1) ACI work instruction identification number.

(2) Date of inspection.

(3) Description of inspected article condition.

(4) If damage found, damage classification (minor, major, or critical):

(a) Detailed description, sketches, drawings, and photographs documenting damage, for damage types, sizes, locations, and orientations.

(b) Part number and criticality classification.

(c) Work Unit Code for item with defect.

(d) How malfunction codes/root cause determination.

(e) Engineering and nondestructive inspection records.

(f) Action taken code/damage disposition (no action required, repair, replace, etc.)

with documentation.

(5) Record of inspection:

(a) Date and time of inspection.

(b) Name and organization of inspector.

(c) Location of inspection (e.g., RAFB (Robins Air Force Base), HAFB (Hill Air Force Base), TAFB (Tinker Air Force Base), location of contractor facility, etc.).

c. Summary of results and recommendations.

(1) Summary of inspection findings.

g. Frequency of inspection.

i. Instructions for accessing article to be inspected.

j. Inspection procedures and potential/anticipated damage.

a. Pertinent aircraft identifying information:

(1) Aircraft mission design series (MDS).

(2) Aircraft serial number (SN).

(3) Base assignment history.

(4) Planned ACI start and end date.

(5) Actual ACI start and end date.

(6) Actual flight hours.

(7) Equivalent flight hours.

(8) Last programmed depot Mx date.

(b) Part number and criticality classification.

(c) Work Unit Code for item with defect.

(d) How malfunction codes/root cause determination.

(f) Action taken code/damage disposition (no action required, repair, replace, etc.) (f) with documentation.

(e.g., RAFB (Robins Air Force Base), HAFB (Hill Air (c) inspection (e.g., (Robins Air Force Base), HAFB (Hill Air Force Base), TAFB (Tinker Air Force Base), location of contractor facility, etc.).

DI-MISC-81391A

(2) Prioritized list of critical and major findings.

(3) Recommendations for revisions to maintenance requirements at the depot and/or field levels.

End of DI-MISC-81391A.

(3) Recommendations for revisions to maintenance requirements at the depot and/or field levels.

Title: STATIC TEST REPORTS

Number: DI-SESS-82038 Approved Date: 20160412

AMSC Number: F9648 Limitation: N/A

DTIC Applicable: No GIDEP Applicable: No

Preparing Activity: 11 (AFLCMC/EZFS) Project Number: SESS-2016-012

Applicable Forms: N/A

Use/Relationship: The static test reports consist of a static test plan, static test progress and static test final reports. These reports will be used by the procuring agency to evaluate the suitability of the planned static test, to assess static test progress, and to verify the actual static strength as well as to document the data collected to substantiate the contractor’s strength analysis.

a. This document contains preparation instructions for data resulting from the technical requirements described in MIL-STD-1530, Aircraft Structural Integrity Program (ASIP).

(Copies of this document are available online at http://quicksearch.dla.mil.)

b. This Data Item Description (DID) contains the format, content, and intended use information for the data deliverable resulting from the work task described in the solicitation.

Requirements:

1. Reference documents. The applicable issue of the documents cited herein, including their approval dates and dates of any applicable amendments, notices, and revisions, shall be as specified in the contract.

2. Format. The reports shall be in the contractor’s format.

3. Content. The Static Test Reports shall contain the following:

3.1 Static Test Plan - For each static test, this report shall contain schedule information as well as detailed information on the: test article configuration, test article instrumentation, load introduction and control system, environmental control system, data acquisition system, and critical load conditions. The report shall include:

a. Test objectives and entrance/exit criteria. The test objectives shall include obtaining data necessary to verify the structural analysis and demonstrating compliance with strength requirements. The entrance criteria shall include evaluation of test loading accuracy and pre-test predictions of strains and deflections at all critical locations. The exit criteria shall include test conditions and load levels that must be completed and data that must be acquired.

b. Processes for selection of the critical test conditions and the associated flight condition and critical structure for each condition selected for testing. Describe comparisons of test loads and environment with corresponding design analyses loads and environment.

(1) Describe the intermediate and maximum test loads to be applied to the test article, including loading sequence. Include estimated dates for attainment of intermediate and maximum test loads.

DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.

a. This document contains preparation instructions for data resulting from the technical This document contains preparation instructions for data resulting from the technical requirements described in MIL-STD-1530, Aircraft Structural Integrity Program (ASIP).

(Copies of this document are available online at http://quicksearch.dla.mil.)

3.1 Static Test Plan - For each static test, this report shall contain schedule information as well For each static test, this report shall contain schedule information as well as detailed information on the: test article configuration, test article instrumentation, load test article configuration, test article instrumentation, load introduction and control system, environmental control system, data acquisition system, and introduction and control system, environmental control system, data acquisition system, and critical load conditions. The report shall include:

a. Test objectives and entrance/exit criteria. The test objectives shall include obtaining data Test objectives and entrance/exit criteria. The test objectives shall include obtaining data necessary to verify the structural analysis and demonstrating compliance with strength necessary to verify the structural analysis and demonstrating compliance with strength requirements. The entrance criteria shall include evaluation of test loading accuracy and pre-requirements. The entrance criteria shall include evaluation of test loading accuracy and pre test predictions of strains and deflections at all critical locations. The exit criteria shall include test predictions of strains and deflections at all critical locations.

test conditions and load levels that must be completed and data that must be acquired.

b. Processes for selection of the critical test conditions and the associated flight condition and Processes for selection of the critical test conditions and the associated flight condition and critical structure for each condition selected for testing. Describe comparisons of test loads and ted for testing. Describe comparisons of test loads and environment with corresponding design analyses loads and environment.

(1) Describe the intermediate and maximum test loads to be applied to the test article, Describe the intermediate and maximum test loads to be applied to the test article, including loading sequence. Include estimated dates for attainment of intermediate and including loading sequence. Include estimate maximum test loads.

DI-SESS-82038

(2) Describe all major component static test loads including shear, bending and torsion compared to design analyses.

(3) Describe the distributed and inertia loads compared to the design analyses. Describe which loads are not properly represented and any unbalanced loads that must be reacted and their associated magnitudes and impacts.

(4) For each test condition, summarize all applicable test parameters such as, but not limited to, aircraft weight, load factor, speed, altitude, and the critical stress points of the structure for that particular test loading condition.

(5) Describe the temperature, moisture, etc., requirement for each test condition and the method to achieve, control, and verify the environment.

c. Test article configuration, test article instrumentation, test fixture, load introduction and control system (including test article protection and safety), environmental control system, and data acquisition system. For instrumentation, include drawings and photographs documenting the exact location and orientation for each.

d. Predicted and allowable parameters (stress or strain, deflection, temperature, pressure, load, etc.) for all measurements for each test condition.

3.2 Static Test Progress Report - This report shall contain details for static testing progress and include the following:

a. Test article configuration changes made since the last progress report to include drawings and photographs.

b. Deviations from the test plan.

c. Events to date which affect the progress of the test program (premature failures, inability to sustain load, delays in the planned test schedule, etc.).

d. Test loading conditions completed since the last progress report and results.

e. Inspection results including any elastic buckling, permanent buckling, and failures with photographs for each.

f. Schedule estimates for remaining test conditions.

3.3 Final Static Test Report - This report shall describe each test condition and data obtained and shall include the following:

a. Details of test results and conclusions and necessary changes to production and delivered aircraft.

b. Load versus deflection plots at locations throughout the test article and any location with permanent deformation.

c. Instrumentation measurements compared to predictions for each location and condition.

d. Final inspection results including any elastic buckling, permanent buckling, and failures with photographs for each.

End of DI-SESS-82038

(2) Describe all major component static test loads including shear, bending and torsion Describe all major component static test loads including shear, bending and torsi compared to design analyses.

(3) Describe the distributed and inertia loads compared to the design analyses. Describe Describe the distributed and inertia loads compared to the design analyses. Describe which loads are not properly represented and any unbalanced loads that must be which loads are not properly represented and any unbalanced loads that must reacted and their associated magnitudes and impacts.

(4) For each test condition, summarize all applicable test parameters such as, but not For each test condition, summarize all applicable test parameters such as, but not limited to, aircraft weight, load factor, speed, altitude, and the critical stress points of the limited to, aircraft weight, load factor, speed, altitude, and the critical stress points of the structure for that particular test loading condition.

(5) Describe the temperature, moisture, etc., requirement for each test condition and the Describe the temperature, moisture, etc. requirement for each test condition and the method to achieve, control, and verify the environment.

c. Test article configuration, test article instrumentation, test fixture, load introduction and Test article configuration, test article instrumentation, test fixture, load control system (including test article protection and safety), environmental control system, and control system (including test article protection and safety), environmental control system, and data acquisition system. For instrumentation, include drawings and photographs documenting data acquisition system. For instrumentation, include drawings and photographs documenting the exact location and orientation for each.

d. Predicted and allowable parameters (stress or strain, deflection, temperature, pressure, cted and allowable parameters (stress or strain, deflection, temperature, pressure, load, etc.) for all measurements for each test condition.

f. Schedule estimates for remaining test conditions.

d. Test loading conditions completed since the last progress report and results.

c. Events to date which affect the progress of the test program (premature failures, inability to Events to date which affect the progress of the test program (premature failures, inability to sustain load, delays in the planned test schedule, etc.).

a. Test article configuration changes made since the last progress report to include drawings Test article configuration changes made since the last progress report to include drawings and photographs.

Title: Equipment Installation Instructions

Number: DI-MISC-81321A Approval Date: 20130419 AMSC Number: N9364 Limitation: N/A DTIC Applicable: N/A GIDEP Applicable: N/A Office of Primary Responsibility: AS/PMA-207 Applicable Forms: N/A

Use/Relationship:

This Document provides equipment installation, operation, and maintenance instructions.

This Data Item Description (DID) contains the format, content, and intended use information, and content preparation instructions for the data product resulting from the work task described in the contract Statement of Work or Performance Work Statement.

This DID supersedes DI-MISC-81321.

Requirements:

1. Format: The data shall be in Contractor format or if a commercial commodity as designated per FAA regulations.

2. Content: The Equipment Installation Instructions shall have a title page containing the title, date, application, and document number.

Section 1. Installation Instructions. The equipment installation instructions include step-by-step assembly, mounting and connection procedures, and grounding and bonding procedures and procedures to demonstrate that the equipment is operating correctly. The instructions shall include the information necessary for personnel to properly engineer the installation of the system. The instruction shall include dimensions of the equipment, mounting brackets, consoles/panels, wiring and pictures to assist in the location of wiring runs. The instructions are in sufficient detail to enable a technician with little or no formal training on the equipment to perform installation functions.

Section 2. Operations Instructions. The operations instructions contain the complete, step-by-step description

Statement of Work or Performance Work Statement.

or if a or if a commercial commodity as designcommercial commodity as designated per FAA regulations.

and connection grounding and bonding procedures and

The instructions shall include the information necessary for personnel to properly engineer the installation of the system.

mounting brackets, consoles/panels, wiring to assist in the location of wiring runs.

DI-MISC-81321A

of all operating procedures. The instructions are in sufficient detail to enable a technician with little or no formal training on the equipment to perform operational functions.

Section 3. Maintenance Instructions. The maintenance instructions contain the complete, step-by-step description of the following for each subsystem and assembly:

a. All maintenance procedures and adjustments performed during installation.

b. All maintenance procedures and actions required to diagnose and locate any fault of any part of the system during and after installation.

c. All test equipment required to inspect, test, calibrate, service, repair, overhaul and end items shall be identified. This information shall include the identification of test cables, connectors, extender kits, and adapters required.

3. The instructions are in sufficient detail to enable a technician with little or no formal training on the equipment to perform maintenance functions.

4. END OF DI-MISC-81321A.

c. All test equipment required to inspect, test, calibrate, service, repair, overhaul and end items shall be identified. This information shall include the identification of test cables, connectors, extender kits, and adapters required.