Purchase Specification C-17 Pneumatic 5_24_12.pdf

HILL AIR FORCE BASE

Ogden Air Logistics Center

PURCHASE SPECIFICATION

C-17 PNEUMATIC COMPONENT TEST STAND

February 2012 “Rev 1 24 May 2012”

Hill Air Force Base

Ogden Air Logistics Center

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Purchase Specification

Pneumatic Component Test Stand

1.0 Scope

1.1 This specification is for the purchase of one (1) universal pneumatic component test stand (self contained) with equipment, fixtures, software and accessories as described herein. The units to be tested consist of C-17 auxiliary power unit (APU) load valves. This is a total-turnkey project; the contractor shall provide all equipment, adapters, tools, supplies, labor, and management necessary. Any defects or non-compliance with the applicable Technical Orders (T.O.) shall be repaired and brought into T.O. compliance. The contractor shall deliver all technical data necessary to manufacture, test, maintain, reproduce, procure, and modify the test stand and all components related to the test stand. Full rights of ownership for all technical data, including software source code, shall be transferred to the United States Air Force upon final acceptance of the test stand. This specification lists minimum requirements and is not intended to restrict or limit design improvements that the Supplier has either available or under development.

2.0 Basic Requirements

2.1 The contractor shall use the Air force Technical Order (T.O.) test requirements as the primary design criteria of the test stand. Any deviations from T.O. requirements shall be approved in writing by the

Air Force process engineers. The applicable T.O.’s for the items being tested are listed below (The latest revision when contract is awarded shall be used). Contact the contract negotiator to have the T.O.’s distributed via CD. The Contractor must provide a current DD Form

2345 and must comply with AFI 61-204 (NOTICE TO ACCOMPANY

THE DISSEMINATION OF EXPORT-CONTROLLED TECHNICAL

DATA) and verify the DD Form 2345 through the Joint Certification

Program http://www.dlis.dla.mil/JCP/ . Project manager will provide the needed CDs with the T.O. information to the Contract Negotiator on an as needed basis. The C17 Pneumatic Component Test Stand shall be capable of measuring any of the parameters listed in the Technical orders below to an accuracy of at least four times better than each tolerances range in the test unit technical order.

2.1.1 T.O. 7J6-6-17-3 Section 3

P/N: 3290408-1

Engine Models: GTCP331-250G

2.1.2 T.O. 7J6-21-3 Section 3

http://www.dlis.dla.mil/JCP/

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P/N: 979806-11 & -12

Engine Models: GTCP331-250G

2.1.3 T.O. 7J14-9-3 Section 6

P/N: 3614409-1, 3290594-1, 328918-1, 3876085-3, -4, -6, 3876084-1, -2

Engine Model: GTCP331-250G

2.2 The contractor shall host the capability to functionally test the workload listed in section 2.1 above on the new test stand. The government anticipates Test Program Set (TPS) development will be completed consecutively as opposed to completing all the tasking for all TPSs concurrently.

2.3 A TPS consists of all elements required to test the items listed in section 2.1 above, including test program software Computer Software

Configuration Item (CSCI), ITA and cables Configuration Item (CI), test documentation, and holding fixtures. Each TPS, when used in conjunction with the target test station, shall provide all facilities required for testing and fault diagnosing one or more Unit Under Test

(UUT) configurations.

2.4 Test stand software shall be programmed using LabVIEW 2010 or newer. The licensed copy of LabVIEW 2010 Professional (or newer) shall remain with the test stand to allow future modifications to the software.

2.5 Size Restrictions: The test stand footprint shall not exceed 120 inches long. The test stand must fit through a door measured 43 inches wide by 79 inches high. It is acceptable for the test stand to be in segments.

2.6 The test stand shall have permanent industry standard fork lift slots to facilitate relocation.

2.7 Equipment shall be designed for accessibility and ease of change for frequently replaced components. In general, such components should have a mean time to repair of one (1) hour or less, to minimize system downtime. Parts and/or devices prone to high maintenance shall be designed so as to be quickly changed within twenty (20) minutes.

Accessibility means that components shall be mounted in such a way that major disassembly is not required to replace a frequently changed item. This also means that such components will be in an easily reached position and not require special tools.

2.8 The test stand shall be designed ergonomically correct for a test operator in a standing position. The unit under test shall be easily

3 | P a g e visible while the operator is standing at the control console.

2.9 The test stand shall be of rugged construction and shall be designed to have a service life of at least ten (10) years with proper maintenance.

Test stand components subject to corrosion shall be properly coated or treated.

2.10 Order of Precedence. In the event of a conflict between the text of this

Purchase Specification and the references cited herein, the text of this

Purchase Specification shall take precedence. Nothing in this Purchase

Specification shall supersede applicable laws and regulations unless a specific exemption has been obtained.

2.11 An additional small roll-away cabinet such as a Vidmar, Lista or equivalent will be provided and shadowed for tooling and parts. The contractor is to allow for storage space beneath the test stand for spare harnesses, fittings, parts, etc.

2.12 Test stand is to have a desktop area with sufficient space for a large binder such as a T.O. that the operator can refer to while testing.

2.13 Test stand work space is to be enclosed with clear Lexan that is easily accessible with smooth free moving doors.

3.0 Special Requirements

3.1 Automation

3.1.1 The test stand shall be automated by computer, with an

appropriate user interface. The computer system must have at least 500 GB hard drive with sufficient memory and processor speed to accurately control the test sequences and collect and store data. Two (2) new Liquid Crystal Display (LCD) displays shall be provided with a minimum nineteen (19) inch screen size each. Monitors are to be setup in a side by side position not a top to bottom. Data acquisition to be done using National

Instruments, Compact RIO.

3.1.2 The test program shall require the following user inputs: operator name, part number tested (Per programming drop down menu), serial number and final disposition (pass/fail).

3.1.3 The test stand shall have three (3) modes of operation:

Manual: whereby the required test conditions are achieved manually by making adjustments on the test

4 | P a g e stand control panel. The operator commands the computer to record the data.

Semi-Automatic: whereby the operator steps through each test point and the test stand automatically adjusts the computer controlled parameters to achieve the desired conditions. The operator commands the computer to record the data.

Automatic: whereby the computer automatically advances through test points, sets the conditions and records the data. Some units require physical adjustments of the unit under test. While in automatic mode the computer will advance to the test point where the adjustments are required and hold the settings until commanded by the operator to continue with the test.

3.1.4 The final test report for each unit shall display the part number, serial number, date/time, operator name and if test parameters are in or out of tolerance.

3.1.5 A new laser printer (HP LaserJet 4050N or equivalent) shall be included for report publication. Final test report shall fit on one side of a single sheet of letter sized (8.5” x 11”) paper.

3.1.6 Final test reports shall be saved to the hard drive. The file path shall contain the part number, serial number and the date of test.

Tests that are redone shall overwrite the previous data file(s).

3.1.7 Computer system shall have a CD-R/W drive and at least one (1) free USB port to facilitate data transfer.

3.2 The contractor shall supply all adapters, fixtures, hoses and cables required to test each item listed in section 2.1. All special tooling/adapters developed for the test stand shall have a part number engraved or etched into the part.

3.3 The contractor is to label on both end of all

wires/cables/terminals/junctions to match the electrical diagrams of the test stand.

3.4 A work light strategically located (without interfering with machine operation) to illuminate the work area shall be provided. It shall have an individual on/off control switch and protective shields. The light will be capable of 6000 lumens or better.

3.5 Caps, plugs and covers for all openings shall be provided.

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3.6 Software

All Software, including but not limited to, operating system, Test

Executive, and Test Development, that are required by the Test Station shall either be commercially available or available by license to the government with unlimited rights. The contractor shall demonstrate that the software can be installed from an image, or equivalent, to a blank hard drive, and verify that all the Directories and Files have been installed and operate correctly. Instructions in the T.O.s shall be written so that government operators/technicians are able to follow them step by step and successfully install the operating system and tester software, then successfully run self test and calibration software end to end without any discrepancies.

DI-MISC-81454B, Automated Computer Program Identification

Number (ACPIN), CDRL A002

DI-IPSC-81488, Computer Software Product, CDRL A004

3.7 Station Selftest

The contractor shall develop and deliver software for the Test Station that enables the technician to troubleshoot and repair faults in the Test

Station. The contractor shall demonstrate Fault Detection & Fault

Isolation (FD/FI) capabilities by inserting faults into the Test Station.

The contractor shall provide the government with a fault list containing up to 25 fault insertion candidates, and conforming to guidelines set forth in the Acceptance Test Procedure (ATP). During Functional

Configuration Audit (FCA), the government will select up to 10 different independent non-destructive faults from the fault list. The government also reserves the right to increase the number of fault insertions up to 25, and may include non-destructive faults outside the contractor’s list of 25. The contractor shall insert these faults into the test station as prescribed in the ATP. The faults shall be detected and isolated in accordance with the Following:

a. FD/FI capability shall be provided to the next replaceable level of the Test Station.

b. Ability to determine if the test station is performing within its specified set of operational parameters. (i.e. application of functional or diagnostic testing)

c. Fault isolation capability shall apply to those faults for which isolation is allowed by both the physical and electrical design of the unit

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d. Faults shall be considered individually and shall be permanent.

(Intermittent faults shall not be included). After the successful completion of the fault detection/isolation routines, the faults shall be removed and the selftest software shall be re-run commencing at the point of failed test entry point at the operator and government discretion. After the successful completion of the fault detection/isolation routines the selftest software shall be re-run successfully end-to-end. The WR- ALC/GRNEB system engineer is the acceptance authority for the station selftest software.

3.8 The contractor will provide a 120 VAC mechanical convection oven

Cole-Parmer 5200-00 or equivalent.

3.9 Any clamps that are to be used to connect components for testing should be a quick disconnect type similar to the Clampco or equivalent pictured below.

4.0 Spare Parts

4.1 The contractor shall provide one additional spare of the following parts.

Spare parts shall include spare cables, hoses, connectors, fittings, relays, fuses, caps, plugs, covers and pressure transducers. A list of spare parts will be approved by the government process engineer before factory acceptance. The spare parts list shall include the following information:

Name of manufacturer component

Manufacturer’s part number

Detailed catalog description

Lead time to acquire long lead items

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4.2 Standard off-the-shelf components and spare parts shall be used whenever possible (for example, switches, relays, data acquisition cards, etc).

DI-ILSS-80134A, Proposed Spare Parts List, CDRL A010

5.0 Calibration

5.1 The Contractor shall ensure the developed system is capable of being calibrated and its calibration is verified IAW AFMETCAL requirements. Calibration and measurement traceability shall be identified and documented IAW MIL-STD-1839D. MIL-HDBK-1839A will be used for interpretive guidance to clarify requirements invoked by MIL-STD-1839D. The Contractor shall provide a means to perform calibration to meet these requirements. The Contractor shall provide with each C17 Pneumatic Component Test Stand all software and hardware peculiar to the Test Stand, required to perform calibration and calibration verification. The Contractor shall deliver the Calibration

Measurement Requirements Summary (CMRS)) in accordance with

DID DI-QCIC-80278B and Contractor Data Requirements List (DD

Form 1423).

DI-QCIC-80278B Calibration/Measurements Requirements

Summary CDRL A008

DI-QCIC-80798B CALIBRATION CERTIFICATE CDRL A007

6.0 Acceptance Test Procedure

6.1 The Acceptance Test Procedure (ATP) shall be performed at the contractor’s location at least 45 calendar days prior to test station delivery and shall include FCA (Functional Configuration Audit), PCA

(Physical Configuration Audit) and Technical Data verification and

Technical Order verification. The contractor shall deliver an ATP, CMRS, Engineering Drawing package, and draft T.O.’s 15 calendar days prior to the FCA/PCA.

DI-ATTS-80282B, Test Program Set (TPS) and Operational Test

Program Set (OTPS) Acceptance Test Procedures (ATPS), CDRL

A001

DI-ATTS-80283B, Test Program Set (TPS) Acceptance Test Report

(ATR), CDRL A003

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7.0 Safety and Health Requirements

7.1 The test stand shall be equipped with an emergency stop button at the operator console. Emergency stop switch shall be located in front of the test stand unobstructed. Emergency stop switches are not to be located in a place that they can be accidentally bumped while working in front of the test stand. The test stand shall return to a safe condition in the event of an emergency stop or an unexpected power outage.

7.2 One or more methods of machine guarding shall be provided to protect the operator and other employees in the machine guarding area from hazards such as those created by point of operation, ingoing nip points, rotating parts, flying chips and sparks. Examples of guarding methods are—barrier guards, two-hand tripping devices, electronic safety devices, etc. OSHA 1910

7.3 Guards shall be affixed to the machine where possible or secured elsewhere if for any reason attachment to the machine is not possible.

The guard shall be such that it does not present an accident hazard itself.

7.4 Guards shall be provided to cover all belts, gears, electric motors and any other mechanical moving parts. Safety interlocks, over-travel limit stops and warning devices shall protect the machine, controls and operator from damage. Guards to protect the operator from injury due to contact with possible broken parts of units under test while the test stand is in operation shall be provided.

7.5 Hazardous electrical connections shall be shielded from the test operator. The test stand shall incorporate appropriately sized fuses/breakers to prevent an overload condition. The stand frame shall be appropriately grounded. The machine shall comply with OSHA’s standard, 29 CFR 1910

7.6 The manufacturer shall furnish a corrosion-resistant plate(s) securely attached to the test stand console in a visible location with all important safety cautions to be observed by the operator.

7.7 High pressure equipment i.e.: air and hydraulic will have guarding and secure lines.

7.8 The machine shall not exceed 84 dBA maximum noise level.

7.9 Mercury Prohibition. The use of mercury, mercury compounds or mercury based instruments on or in the machine is prohibited.

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7.10 Asbestos Prohibition. The use of asbestos and materials containing asbestos on or in the machine is prohibited.

7.11 Lockout/Tagout: OSHA’s Lockout/Tagout standard, 29 CFR 1910.147 and 1910.269 and Hill AFB Instruction 91-302, Control of Hazardous

Energy shall be required to protect contract employees, as well as, Government employees from electrical harm.

8.0 Lubrication.

8.1 All mechanisms requiring lubrication including gears, slide ways, and bearings (except sealed-for-life type) shall be provided with means for lubrication. All oil holes, grease fittings, and filler caps shall be easily accessible. The contractor shall provide all Material Safety Data Sheets

(MSDS) for all oils or lubricants required the machine operation. All lubrication must be on the Hill AFB approved hazardous materials list.

FED-STD -313D , Federal Standard Material Safety Data, Transportation Data and Disposal Data for Hazardous Furnished to Government, CDRL A011

9.0 Plates

9.1 All markings on the plates shall be permanent and legible on a contrasting non-glare background.

9.2 Lubrication chart or plate.

9.2.1 A Lubrication chart or plate shall be permanently and securely attached to the machine. The following information shall be furnished on the chart or plate:

Points of application

Service interval

Type and viscosity of lubricant

9.3 Nameplate

9.3.1 A Corrosion-resistant nameplate shall be securely attached to the machine. The nameplate shall contain the information listed below:

Name of Test Stand (i.e. C-17 Pneumatic Component

Tester)

Manufacturer’s name

Manufacturer’s serial number

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Manufacturer’s model number

Power input (volts, total amperage, phases, frequency)

Contract number or order number

Date of manufacture (day month and year)

9.3.2 To include DFAR 252.211-7003: UID reference solicitation

10.0 Documentation Requirements

10.1 The contractor shall provide manuals in accordance with CDRL A005 for the new test system that provides the necessary data for operation, troubleshooting, repair and maintenance of the test system. The manual shall include a calibration procedure as outlined in CDRL A009.

TM-86-01N Technical Manual Contract Requirements CDRL

A005

TM-86-01 M Technical Manual Contract Requirements CDRL

A009

11.0 Installation

11.1 The test stand is to be located in Building 240, 5816 D Ave, Hill AFB, UT 84056-5015

11.2 The contractor shall ship, off-load, install and test the machines and at its final location. The contractor shall instruct the carrier that the machine shall be off-loaded only under the supervision of a representative of the contractor.

11.3 The machine shall remain the property of the contractor until it is accepted by the Government at Hill AFB.

11.4 All costs associated with the manufacture, shipping, installation, testing and preparation of the machine for final acceptance at Hill AFB shall be the responsibility of the contractor.

11.5 The contractor shall be responsible to furnish all tools and equipment required to install the machine and perform the tests specified in this specification. The Government shall furnish no tools or equipment.

11.6 Special equipment, measuring equipment, and machine alignment equipment etc., required by the contractor to align the machine and

11 | P a g e perform the tests specified herein shall be furnished by the contractor and shall remain the property of the contractor.

11.7 The contractor shall be required to provide and install all necessary fusible disconnects, circuit breakers, circuit breaker boxes, and conduit to hard wire the machine into the buss duct. Once the equipment is connected to power, it shall be disabled during the installation process and only unlocked by the contractor when required. Hill AFB

Instruction 91-302, Control of Hazardous Energy shall be required to protect contract employees, as well as, Government employees from electrical harm.

12.0 Security Requirements

12.1 The contractor will not be required to obtain a Controlled Area Badge.

The contractor will be escorted at all times within a controlled area.

13.0 Training

13.1 The contractor shall provide the following training upon installation of the test stand at Hill AFB:

Forty (40) hours for training two (2) operators on the software/hardware

Sixteen (16) hours for training two (2) technicians on test stand calibration

Eight (8) hours for training two (2) maintenance technicians on repair and preventative maintenance

Eight (8) hours for training one (1) process engineer on function of test software (source code)

14.0 Facilities

14.1 The Air Force shall provide a source of 208 VAC (3-phase) power and

110/120VAC power within ten (10) feet of the test stand location. A source of 90 PSI shop air will be provided. Any other facility requirements must be agreed upon in writing during the post-award conference at Hill AFB and will be the responsibility of the contractor to fund the facility modifications.

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15.0 Performance Summary

15.1 Schedule/Design Review. To ensure that work is progressing on schedule and that the requirements defined in this specification are being properly addressed, the contractor shall participate in the following events and take minutes as needed:

Event Timeline Location

Post Award

Conference

Engineering Data

Guidance Conference

(EDGC)

<1 month ARO

See para 15.1.1 &

18.2

Hill AFB

Building 240

Preliminary Design

Review (PDR)

3 month ARO

See para 15.1.2 Teleconference

Critical Design

Review (CDR)

In Process Review

(IPR)

5 month ARO

See para 15.1.3 &

18.3

Teleconference

Final Integration

Acceptance

Test(FIAT)

8 month ARO

See para 6.0 and15.1.4

Contractor Facility

Installation and

Commissioning

10 month ARO

See para 15.1.7

Hill AFB

Building 240

Reliability Testing

2 months after commissioning

See para 15.1.8

Hill AFB

Building 240

Final Acceptance

Upon completion of reliability testing

See 15.1.9

Teleconference

Warranty

Starts upon final acceptance

See para 15.1.10

Hill AFB

Building 240

Note: Schedule is tentative and may be adjusted by written agreements between contractor and Hill AFB process engineers.

15.1.1 Post Award Conference. The purpose of this conference will be to review the requirements of this purchase specification and the applicable technical orders, tour the facility where the new test stand will be installed, inspect the existing test stand, and provide the opportunity for the contractor to ask questions. This

13 | P a g e conference also allows the contractor to present possible design options. The duration of this conference should not exceed eight

(8) hours. The contractor’s lead designer of the test stand shall be present for the meeting. At the conclusion of the conference, both the contractor and Hill AFB should have a clear understanding of how the project is to proceed.

15.1.2 Preliminary Design Review. The purpose of the preliminary design review is to allow Hill AFB personnel to review the preliminary mechanical, electrical and pneumatic test stand diagrams (and any other documentation provided by the contractor) and provide early feedback to the contractor. This early feedback is valuable to ensure that the project is heading in the right direction. Any questions or feedback will be resolved via teleconference or e-mail. Hill AFB will require approximately one (1) week for performing the preliminary design review.

15.1.3 Critical Design Review. The purpose of the critical design review is to perform a thorough review of technical data in preparation for Air Force approval. Any questions or feedback will be resolved via teleconference or e-mail. Hill AFB will require approximately three (3) weeks for performing the critical design review.

15.1.4 FIAT The purpose of this acceptance test is to ensure that the completed test stand meets all requirements of this purchase specification. As part of this test, the contractor will demonstrate the test stand’s capability of testing the components listed in paragraph 2.1 per the applicable T.O. requirements. Any deficiencies identified at the factory inspection by Air Force process engineers shall be corrected prior to installation at Hill

AFB.

15.1.5 Functional Configuration Audit (FCA)

The FCA shall be performed to verify all developed or modified software for the Test System. The FCA shall be performed jointly by the government and the contractor (at contractor’s facility) with the government chairing the audit. The contractor shall document the results of the FCA after the audit and shall correct all audit discrepancies documented in the Acceptance Test Report prior to

Test Set delivery. The functional baseline shall be established upon completion of and government acceptance of the FCA.

15.1.6 Physical Configuration Audit (PCA)

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The government and the contractor shall conduct a PCA jointly (at contractor’s facility) with the government chairing the audit. The

PCA will verify the drawings reflect the "as built" configuration of all developed or modified portions of the hardware. The contractor shall document the results of the PCA after the audit. A product baseline will be established upon completion of and government acceptance of the PCA.

DI-ATTS-80282B, Test Program Set (TPS) and Operational

Test Program Set (OTPS) Acceptance Test Procedures

(ATPS), CDRL A001

DI-ATTS-80283B, Test Program Set (TPS) Acceptance Test

Report (ATR), CDRL A003

15.1.7 Installation and Commissioning. Upon delivery at Hill AFB, the contractor shall ensure successful installation of the test stand.

(Hill AFB can provide fork lift services for unloading if requested in advance by the contractor) After installation, the contractor shall ensure proper function of the test stand and provided training to Hill AFB personnel. The contractor shall run selftest and calibration to verify that the tester is still working properly.

15.1.8 Reliability Testing. After installation and commissioning, Hill

AFB personnel shall verify test stand reliability by testing the shorter of a total of thirty (30) components or for a two (2) month period. Any failures of the test stand during this period will be repaired at the expense of the contractor and will restart the reliability testing period.

15.1.9 Final Acceptance. Upon successful completion of the reliability testing, Hill AFB will verify that the conditions of this purchase specification have been met and then take ownership of the test stand.

15.1.10 Warranty. The contractor shall provide a written warranty for the test stand, which shall cover two (2) years from the date of final acceptance.

16.0 GOVERNMENT FURNISHED PROPERTY.

16.1 The government shall provide one (1) of each serviceable asset as outlined in Appendix A. These assets shall be stored in a secured location by the contractor. Absolutely no changes/alterations shall be made to the assets by the contractor or sub-contractor. A log shall be kept by the contractor of each occurrence of removal of the assets from

15 | P a g e the secured location along with description of what the assets were used for and how many hours they were run. The contractor shall be responsible for any damage to the assets which occur while they are in possession of the assets. Any damage to the assets shall be reported immediately to the Process Engineer at HAFB along with written documentation of what, how, and why the asset was damaged.

16.2 Shipping of Government Furnished Equipment. The contractor shall be responsible for picking up assets referenced in Appendix A of this document from Hill AFB, shipping them to the factory for testing and buy-off, and returning the assets to Hill AFB. The contractor shall assume full responsibility for these assets during transportation. The contractor shall obtain written permission via e-mail from the Air Force process engineers.

17.0 GENERAL INFORMATION

17.1 Information Disclosure. Any developments, devices, or technical information furnished in connection with this equipment or resulting from development of this equipment shall not be disclosed to other than authorized Hill AFB personnel.

17.2 Physical Security. The contractor shall be responsible for safeguarding all government property provided for contractor use. At the close of each work period, government facilities, property, and materials shall be secured.

17.3 Plans and Schedules. The contractor shall prepare a program plan that coordinates all activities related to this PS to assure successful and timely completion. The program plan shall be presented to the government for review and approval, and shall illustrate an overall accomplishment plan, allocating responsibilities, and identifying interdependencies and agreements with all parties involved. A master milestone chart for the program shall be generated as part of the plan, detailing major events and reviews to include time involvement criteria for all participants. This chart will serve as the basis for future work scheduling and will provide a reference to track progress. Program success shall be measured by comparing the milestone chart to actual accomplishment dates. Any major discrepancies shall be brought to the attention of the CO along with a plan to get the project back on schedule.

17.4 Subcontractor Requirements. A list of all intended subcontractors that will be used for any part of the design, build, installation, and testing shall be provided with the proposal. Hill AFB reserves the right to approve/disapprove all subcontractors’ access to work on this project.

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Contractors are responsible to insure all subcontractors meet the same specifications and agreements as the prime contractor.

17.5 Reports. The contractor shall prepare and submit to government personnel a monthly status report, due by close of business on the last day of the month. This report shall summarize tasks or activities concluded during the month, the tasks started, the tasks in progress, percentage complete, and the tasks that are planned to be started during the next reporting period. A breakdown by individual tasks shall be used to best reflect progress as it relates to each development. Any project concerns or issues that are or may impact resources, schedule, or cost shall be reported along with the projected impact to the schedule. In addition to presenting impacts, the contractor shall present a plan to correct or mitigate these impacts.

DI-MGMT- 80368A, Status Report, CDRL A012

17.5.1 Meeting Minutes. The contractor shall take meeting minutes on all teleconferences and meetings and submit a copy to government personnel.

DI-ADMIN-81505, Report, Record of Meeting/Minutes, CDRL

A013

18.0 Engineering Data

18.1 Engineering Data: The contractor shall develop/produce/maintain and deliver a Technical Data Package (TDP) that accurately depicts the final product. The TDP shall represent the approved, tested, and accepted configuration of the defined delivered item(s). TDP data includes, but is not limited to, Computer Aided Design (CAD) data, CAD models, model based definition data sets, Gerber data and Master

Bill of Materials (BOM). The TDP shall provide the necessary design, engineering, manufacturing, testing and quality assurance requirements information necessary to enable the procurement or manufacture of an interchangeable item that duplicates the physical and performance characteristics of the original product without additional design engineering effort or recourse to the original design activity or any third party. All engineering product definition data created as a result of this contract shall be considered a part of the TDP. The TDP shall be delivered in accordance with Air Force Product Data Specification drawing 9579776 (CAGE 98752), reference attached DD Form 1423

Block 16.

[DI-SESS-81000D/T], Production Drawings/Models and Associated

Lists, CDRL A006

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18.2 Engineering Data Guidance Conference: The contractor shall support and co-chair a Guidance Conference with WR-ALC/ENGLDC for engineering data within 30 days after contract award. The Conference shall be convened at a site and on a date agreed upon by the

Government contracting officer and the contractor. The contractor shall prepare an agenda and record the minutes of the Guidance

Conference. The contractor shall address, discuss, and provide status on the following:

a. Understanding of all CDRL requirements, applicable DIDs, specifications and standards.

b. TDP review requirements and schedules.

c. TDP delivery requirements and schedules.

d. Contractor’s drafting practices/procedures/TDP drawing formats/CAD programs.

e. The contractor's quality assurance procedures relating to TDP documents, including quality control of subcontractor and vendor data.

f. The role of subcontractors and vendors who may deliver TDP documents under this contract.

g. The contractor's configuration management system, including methods for releasing documents, approving documents, and incorporating changes into documents.

h. Digital Technical Data Package (TDP) deliverables.

Note: Guidance Conference may be held in conjunction with other meetings or conferences.

18.3 In-Process Review (IPR) of the TDP: The contractor shall host, support, and co-chair an IPR of the engineering drawings and associated lists and other documentation to be included in the TDP.

The IPR shall be conducted only after the contractor's quality assurance personnel have completely reviewed the data and determined that data are of sufficient quality that Government time will be effectively utilized during the review. IPR may be scheduled when data has reached the 50% percent completion point and shall be held, when possible, in conjunction with other reviews (i.e., PDR, CDR). The contractor shall notify WR-ALC/ENGLDC a minimum of 30 days prior

18 | P a g e to the anticipated date of completion point. The IPR shall focus on the contractor's progress in the preparation of the TDP. The contractor shall support and provide the necessary resources, i.e., meeting agenda, conference room, applicable data, minutes, and appropriate personnel available to answer any questions to perform the IPR effectively. The contractor shall correct all discrepancies identified in the IPR. All subcontractor/vendor data shall be made available for review. If the quantity of subcontractor/vendor data is of sufficient magnitude, the

Government may schedule a separate IPR at the subcontractor's/vendor's facility.

18.4 Relationship of Contractor with Subcontractors/Vendors: The contractor shall levy on sub-contractors and sub-vendors the same requirements for Technical Data Packages (TDPs) as are levied on them by this contract. This requirement shall apply at all tiers of sub-contractor/vendor levels associated with the program.

18.5 Engineering Data Updates and Revisions: The contractor shall (and shall cause subcontractors and vendors to) update and maintain engineering data for the item(s) designed/ developed/modified/produced under this contract for the life of this contract and shall incorporate all changes in accordance with the following:

a. All engineering changes shall be incorporated into the applicable engineering data within 90 days after engineering release/Air Force concurrence or at intervals of five changes, whichever occurs first, except a change involving safety, which shall be incorporated immediately.

b. All engineering changes shall be incorporated into the applicable engineering data prior to delivery of data for review.

c. All engineering changes shall be incorporated into the applicable engineering data prior to delivery of final media (this includes all

Engineering Orders EO’s generated as a result of the preliminary data review.)

d. Revisions to existing drawings when the contractor is the current design activity shall result in the delivery of the entire document with no regards to how minor or major the revision.

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Appendix A Government Furnished Equipment (GFE)

The following aircraft components will be available for the contractor to use in the development and testing of the pneumatic component test stand. These components shall be controlled per paragraph 14.0 of the purchase specification.

Nomenclature Part Number NSN T.O. Replacement

Cost

Surge Valve 979806-11, -12 4810013346399

4810015279435

7J6-21-3

Section 3

$10,514.54

Load Valve 3290408-1 4810013341961 7J6-6-17-3

Section 3

$6588.16

Diff. Pressure

Transducer

3876085-3, -4, -6 4820015160123

6695014687645

6695015227590

7J14-9-3

Section 6

$7,550.00

$8,626.88

Total Pressure

Transducer

3876084-1, -2 6685013617594

6685014748326

7J14-9-3

Section 6

$3,988.94

$10,066.00

Flow Sensor

Housing

3614409-1 4820013577910 7J14-9-3

Section 6

$4617.50

Variable Volume

Chamber

328918-1

3290594-1

6620013603453

6620013603453

7J14-9-3

Section 6

$2,365.23

$2,365.23

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Appendix B

Summary of Data Item Deliverables

CDRL

Item

No#

Data Item Title Sow

Para.

Ref.

Data Item Description

Authority

A001 Test Program Set (TPS) and

Operational Test Program (OTPS)

Acceptance Test Procedures

(ATPS)

6.0,15.1.6 DI-ATTS-80282B

A002 Automated Computer Program

Identification Number (ACPIN)

Data and Control Record

3.6 DI-MISC-81454B/T

A003 Test Program Set (TPS)

Acceptance Test Report (ATR)

6.0,15.1.6 DI-ATTS-80283B

A004 Computer Software Product 3.6 DI-IPSC-81488

A005 Technical Manual Contract

Requirements (TMCR)

10.0 TM-8601N (TMCR)

A006 Product Drawings/Models and

Associated Lists

18.0 DI-SESS-81000D/T

A007 Calibration Certificate 5.0 DI-QCIC-80798B

A008 Calibration and Measurement

Requirements Summary

5.0 DI-QCIC-80278B

A009 Technical Manual Contract

Requirements (TMCR)

10.0 TM-86-01M (T)

A010 Proposed Spare Pares List 4.0 DI-ILSS-80134A

A011 Material Safety Data, Transportation Data and Disposal

Data for Hazardous Material

Furnished to Government Activities

8.0 FED-STD-313D

A012 Status Report 17.5 DI-MGMT 80368A

A013 Report, Record of

Meetings/Minutes

17.5.1 DI-ADMN-81505