Q A_for_Amendment_0002.docx
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- Attached to
- T-38C Avionics Component Integration and Contractor Logistics Support Federal contract opportunity
- Solicitation number
- FA8211-15-R-0001
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Question and Answer for Amendment 0002
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Text version
23 February 2015
List of Questions Contractor #1
Doc Name
| Section |
| Description |
| Page # |
| Question / Comment / Recommendation |
| 1 |
| Solicitation FA8211-15-R-0001 & Amendment -0001 |
| Section B |
| N/A |
| N/A |
| Two sets of CLS Services/PBL CLINs are provided, based on the base and option five year ordering periods: |
0005, 1005 0006, 1006 0007, 1007 0009, 1009 0011, 1011 0012, 1012 0013, 1013
The base ordering period CLINs (00xx) can be used to exercise up to four (4) years of services, yet the CLIN quantities are for 12 months only. Where are the additional three years to be proposed?
The option ordering period CLINs (10xx) can be used to exercise up to five (5) years of services, yet the CLIN quantities are also for 12 months only. Where are the additional four years to be proposed?
Government Response: The offeror is to complete pricing information in the TEP Attachment 6B only. This revised instruction has been added to Section B of the RFP/Amendment 0002 and is located on page 4. This instruction has also been clarified in Attachment 12 Section L paragraph 10.3.
| 2 |
| Attachment 6B, Total Evaluated Price Worksheet Revision 1 |
| N/A |
| N/A |
| N/A |
| The revised worksheet shows the addition of a 9th services ordering period (01 April 2025 - 31 March 2026, FY-25); however, the Record of Revision tab states "the eight (8) CLS Delivery Orders" and "Blacked-out the CLS CLINS for FY-25". We want to confirm if the direction is to price a 9th ordering period? This same question applies to the Attachment 6A labor rate table? |
Government Response: The offeror is to fill in all yellow cells within the TEP Attachment 6B. This would include pricing the 9th and 10th years of the ordering period.
Contractor #2
Doc Name
| Section |
| Description |
| Page # |
| Question / Comment / Recommendation |
| 1 |
| Attachment 2 MDP SOO and Attachment 6B Total Evaluated Price Worksheet |
| SOO 2.1 |
| If install time is over 25 hours |
| 1, 1 |
| As discussed at the Site visit at Randolph Air Force Base, CLINs X001AD (Contractor Field Team) is a request for installation of the Group A and Group B equipment into the T-38C jets. Government suggested that the contractor go ahead and provide a bid for the installation cost in the event contractor cost is cheaper than government installation estimates. Contractors are concerned that this requested installation cost, which may not be required due to an estimated modification time less than 25 hours, may count against the contractor during the Total Evaluated Price (TEP) assessment made by the government. If the government would like an estimate for contractor installation, contractor request that CLINs X001AD be removed from the TEP evaluation. |
Government Response: The Government requires all CLINs to be evaluated.
| 2 |
| Attachment 1 AvCI CLS PWS |
| Appx. D |
| Contractor Provided Test Equipment |
| 90 |
| In Appx D of the PWS, there is a requirement to have equipment available in the COMBs facility, but on our trip of 2-11-15, some of this equipment (Ramp Tester) was not found at Randolph COMBs. Please either remove the requirement or confirm that this is a new requirement, or advise otherwise. |
Government Response: The requirements have changed from the current contract. Please refer to the requirements documentation for this effort.
| 3 |
| MDP SOO (all SOOs) |
| 4.1.10 |
| T2 and TCTO |
| 8 |
| In the MDP SOO, actually in all the LRU SOOs, section 4.1.9, isn’t a T-2 modification required to support temporary installation of the Group A and Group B kits into the flight test jets in support of flight test? The only reference for kit installation was made to the TCTOs which are normally only for the permanent modification of the fleet. Request clarification on T-2 requirement. Also, how many test jets will be required to be modified to support flight test as well as the test jet locations? |
Government Response: Test requirements will vary greatly based on the solution set proposed. Test plans and requirements will be developed accordingly, and in conjunction with the Engineering Change Proposal.
Kit installation required for testing will be accomplished by the Government with on-site Contractor support. Number of aircraft will be determined by the test plan. The contractor should plan for 2 aircraft to be modified depending on the complexity of the solution proposed.
DT will be accomplished at Edwards AFB and FDE at Randolph AFB. Please refer to section 5.3.
| 4 |
| FA821115R0001 section 52.222-49, & Attachment 12, Section L, (8) |
| 52.222-49, and Paragraph 8 |
| Collective Bargaining Agreements and DOL wage determinations |
| 73, 16 |
| For wage determination, from document FA821115R0001, section 52.222-49, & Section L (8), the wage determination section implies this Collective Bargaining agreement applies to all COMBS facilities. Contractor is requesting a copy of the current Collective Bargaining Agreement in order to access/develop cost for these facilities. |
Government Response: The current Collective Bargaining Agreement has been posted to FBO as part of this amendment.
There was not a question #5 provided.
| 6 |
| NA |
| NA |
| NA |
| NA |
| Based on discussions at the Site Visit at Randolph AFB, Contractor would like to request aircraft photos show the locations of the existing avionics components and harnesses to facilitate the bid for the installation cost associated with CLINs X001AD for the CFT installations. |
Government Response: Another revision of the bidder’s library will be made available.
| 7 |
| NA |
| NA |
| Per conversation at Randolph COMBS tour |
| NA |
| Based on discussions at the T-38C TSSC facility at Randolph AFB, Contractor request a copy of the re-competition Support Package (RSP) developed in support of the T-38C trainer solicitation coming out of Wright Patterson AFB. The package will contain a detailed list of software delivered by the Aircraft Prime to the TSSC facility. |
Government Response: Please see Appendix C of the CLS PWS for a list of software applications. It is a complete list of all software applications.
| 8 |
| Attachment 1 AvCI CLS PWS |
| Appx. C |
| Application Software |
| 84-89 |
| What GFE/GFD is provided from this Appx? Will all licensed rights be transferred? For example, will a computer with Red Hat 9 (A customized Red Hat 9 OS configured to support a diskless real-time PC)already installed be made available as GFP? Another example is the Silicon Graphics Computer mentioned in the “Automatic Software Documentation” line item. |
Government Response: Please refer to attachment 8a & 8b of the solicitation for the list GFE. Attached to this document is the attachment 8 provided with the draft solicitation. This list is in a different format than the solicitation however, the content is the same.
| 9 |
| 1T-38C-556 |
| NA |
| Missing Document |
| NA |
| Please provide document 1T-38C-556 “MODIFICATION OF MISSION DISPLAY PROCESSOR (MDP) P/N 623700-4 TO INCORPORATE BLOCK 8 OPERATIONAL FLIGHT PROGRAM (OFP) SOFTWARE UPGRADE ON T-38C AIRCRAFT” |
Government Response: TCTO 1T-38C-567C MODIFICATION OF MISSION DISPLAY PROCESSOR (MDP) P/N 623700-4 TO INCORPORATE BLOCK 9 SOFTWARE AND MODIFICATION OF ELECTRONIC ENGINE DISPLAY (EED) P/N 640-915-02-02 TO INCORPORATE FIRMWARE UPGRADE IN T-38C AIRCRAFT will be provided.
| 10 |
| Attachment 1 AvCI CLS PWS |
| Paragraph 4.1.5 and Appx C. |
| Software and Documentation |
| 17, and 84-89 |
| It is our understanding that the current Prime will continue to host this software at their SIL facility during the initial 2-year period of this contract. Competing contractors will require access to these software tools and licenses shortly after contract award to support the design/development/fabrication/flight test effort for the form fit function replacements for the MDP and other associated avionics LRUs. Can the government confirm access to these tools within 60 day ARO of this contract or will a duplicate set of development tools be provided to the winning bidder to support the development effort over the initial 2.5-year development effort? |
Government Response: A complete library of software will be provided upon contract award. Any commercial software licenses that do not transfer will be the responsibility of the contractor to obtain.
| 11 |
| Attachment 1 AvCI CLS PWS |
| Paragraph 4.1.5, 5.14.4, and Appx C. |
| SIL Software and Documentation |
| 17, 27, 84 |
| Contractor upgrades SIL and maintains SIL Avionics, However no SW, model or associated documentation are listed in appendix C applies to the SIL other than MDP software. Please confirm that 4.1.5 (second sentence) refers to complete library including SIL SW and is not necessarily limited to software in Appendix C list. Otherwise, please provide a list of SIL SW and documentation and the rights declared. |
Government Response: All software will be provided to the contractor upon award. Instructions on how to schedule a software library review is posted on FBO.
The applications listed in Appendix C under the ATD section that are also used with the SIL are identified below:
T-38 MDP OFP (runs in the MDP, installed in the SIL)
The applications listed under ATD IOS, referred to as "Model Operating System (MOS)" that are used in the SIL.
· T-38 Host DIS Adapter (listed under ATD Host)
· T-38 Host Models (listed under ATD Host)
| 12 |
| T-38 SIL-2 H/W Maintenance Manual, & Attachment_8A_GFP_List |
| Table 3.1.4, All |
| Airborne Equipment in SIL, GFP List |
| 0.28 |
| Document "T-38_SIL-2_Hardware_Maintenance_Manual_Rev_A[1]" has Part Numbers for equipment list in table 3.1.4 and other tables. There is a separate "GFP List" document giving a list of parts. How are these part lists related, and which takes precedence or does winning contractor receive both? During the site visit several of the computers and manuals were not identified. Please identify and list the hardware and software operating on the SIL and describe the rights. |
Government Response: The Government furnished property is attachment 8a & 8b of the solicitation. The Government does not have rights to any other equipment or processes.
Parts list or tables in Document "T-38_SIL-2_Hardware Maintenance Manual – Rev A[1]" are not current.
| 13 |
| CDRL-0026 Prod. Drawings/Models & Associated Lists and 71J267013 MDP Envelope Drawing |
| 16, All |
| Remarks and MDP Envelope Drawing |
| 1, 1 |
| The drawing CDRL has requirements such as ANSI-14.100 not met by drawing that exist in libraries provided by the Government. Please confirm the requirements of CDRL do not apply to revisions of existing drawings; only to new drawings or revise CDRL accordingly. |
Government Response: For revised drawings refer to ASME Y14.35 “Revision of Engineering Drawings and Associated Documents” as cited in the CDRL.
| 14 |
| Attachment 1 AvCI CLS PWS |
| Paragraph 4.4.1, and Appx. C |
| Data Analysis Application for Flight Data from Data Cartridge |
| 18, 88 |
| The Data Analysis application is a PC-based program used to display, export, and print flight data recorded on the Data Transfer Cartridge. Data may be debriefed after each flight and maintenance and operational data is displayed in tabular format using menu-driven windows. Question is, will the data analysis software be provided as GFP? Can a listing of the Data Analysis documents be made available as part of the RFP package? Can the documents be made available as part of the RFP package? |
Government Response: All software will be provided to the contractor upon award.
Offerors will be given the opportunity to review software library. Instructions on how to schedule a software library review is posted on FBO.
| 15 |
| Attachment 1 AvCI CLS PWS |
| Paragraph 4.5.1 |
| Mission Debrief Application |
| 19 |
| Will all of the components of the mission debrief system application be provided as GFP? Will a listing of the Mission Debrief document(s) be made available as part of the RFP package? Will the documents be made available as part of the RFP package? As discussed at the site visit at Randolph AFB, contactor noted that there were not any Boeing representatives located at the Ops facilities supporting mission planning or post mission debriefing. What role does the contractor perform in support of both the mission debrief and mission planning applications at the COMBS sites? Will contractor also be required to support baseline updates to either system? It was our understanding that the Government maintains these baselines. Is there a variant of these applications that the current Prime has developed that are unique to the T-38C? |
Government Response: All software will be provided to the contractor upon award. Offerors will be allowed to review software library.
The contractor is required to keep the software functioning IAW Section 4 of the PWS and specifically 4.1.3.
The contractor does not have an active role in the mission planning or post mission debriefing. However the contractor provides the necessary on-site support to assist in correcting anomalies with the software.
Most of the software listed in Appendix C of the PWS was developed specifically for the T-38C program. The software is updated, via Government or systematic requirements, periodically through the Block Upgrade process.
| 16 |
| Attachment 1 AvCI CLS PWS |
| Paragraph 4.6.1, 4.7.1, 4.8.2, 4.9.1 |
| Various applications and data |
Will a listing of all the documents and software and the associated rights be made available as part of the RFP package? Will the documents and software be made available as part of the RFP package? As the SIL and documentation is identified with IAI, please identify IAI proprietary software or models or documentation that are integral to operational and software management of the SIL.
Government Response: The Government is unaware of any proprietary information related to operation or maintenance of the SIL.
Please see answer to question 11 for SIL software models.
Offerors will be given the opportunity to review software library. Instructions on how to schedule a software library review is posted on FBO.
| 17 |
| Attachment 1 AvCI CLS PWS |
| Paragraph 5.13.5, 5.14.1 |
| ATD and SIL Support |
| 27 |
| Can a listing of the ATD and SIL test bench equipment and hardware and software/application tools be made available as part of this RFP package? |
Will the ATD and SIL test bench equipment and hardware/software support tools be provided to the successor contractor as GFP? See questions 12 & 13 from above.
Government Response: All of the program software listed in Appendix C of the PWS. GFE is attachment 8a & 8b. Also see attachment to question 8.
| 18 |
| Attachment 1 AvCI CLS PWS |
| Paragraph 9.4.6 |
| Transition to Successor |
| 38 |
| At a minimum, The Contractor shall prepare and deliver updates to the following: System Change Description (SCD); identify changes to the Operational Concept Description (OCD), avionics and ATD performance specifications, and F3I specifications; and prepare related requirements change documentation (e.g. Requirement Change Notices, Built-in-Test (BIT) Concept Document, Interface Control Documents (ICD), and vendor specifications). (CDRLA019). If the incumbent contractor is presently bound to a similar requirement will CDRL A019 be made available to the successor contractor? |
Government Response: Yes. The “transition” section of the CLS PWS is almost identical to the existing contract.
| 19 |
| Solicitation FA821115R0001 |
| Part I-Schedule, Section B |
| CLINs X0001AA, X1001AA |
The current notional development schedule for each of the SOOs indicated a 2.5-year development period of performance (POP) to include 1-year of flight test. This issue is the existing solicitation on page 3 of 96 indicated CLIN 0001 is labeled a Base Year yet the development CLIN 0001AA for development indicates a 54 month POP along with 0001AB- AE. The associated CLINs 1001AA-AE have the same exact POP. A note on page 3 of 96 for CLIN 0001 also states that you can only use either 0001 or 1001 CLINs but not both during this program. What is the intent of the overlapping CLINs for development and delivery of the Kits? What is the Government’s definition of a Base Year and Base Period? On page 3 of 96 you define BASE PERIOD CLINs at both 0001-0026 and 1001-1004. Was it the intent of the Government for the contractor to use 0001AA, 0002AA, 0003AA, and 0004AA to support the initial 12 month development effort in support of the SOOs and use CLINs 1001thru 10026 for year 2 thru the remainder of the program to support development through flight test as well as fielding of all KITs and all other CLS support requested in the PWS for the T-38C AvCI program?
Government Response: Updates to TEP and Section L&M have been made.
| 20 |
| Attachment 6B TEP Excel Worksheet |
| N/A |
| CLIN Discrepancies |
The TEP worksheet provided in the attached file indicated you only want the contractor to identify all development cost and kit cost in the Base Year and Year 2? Is that a correct assessment? Or, does the Government only intending to access the NRE cost for X001 through X004 on the TEP worksheet? Also note that the development POP will most likely be 2.5 years based on your notional development schedule in the MDP SOO. Is the intent of the government to reduce flight test to 6-months to meet the 2-year development?
Government Response: The development CLINS should be priced as a complete effort.
Example: If CLIN 0001 is exercised the pricing for all 0001 sub-CLINs are applicable and CLIN 1001 pricing will not be used.
The notional schedule is not meant to prevent the contractor’s from developing a realistic schedule based on the complexity of the proposed solution. The intent is to complete development, integration and test with in the 54 month timeframe. If CLIN X001AD is exercised 18-months will added to complete installations.
| 21 |
| Solicitation FA821115R0001, and Attachment 6B Total Evaulated Price Worksheet |
| Part I |
| Period Of Performance |
| 3 of 96, 1 |
| Part I, paragraph 1, last sentence says : “The total Period of Performance for this contract is to be completed within eleven years” Please reconcile this with the Attachment 6B Total Evaluated Price, which only shows 10 years of effort. |
Government Response: See the notes above Section B in the RFP. The 11th year is for performance only.
| 22 |
| MDP SOO |
| 5.3 |
| DT and FDE Flight Test |
| 9 of 21 |
| The SOO states the contractor will be required to support flight test at both Edwards and Randolph AFB. Will the contractor be required to install both the Group A and B kits on jets at both facilities in support of flight test? If so, how many jets will need to be modified at each facility. |
Government Response: Test requirements will vary greatly based on the solution set proposed. Test plans and requirements will be developed accordingly.
Kit installation required for testing will be accomplished by the Government with on-site Contractor support.
| 23 |
| T-38C AvCI PWS |
| 4.1.2 |
| ATD software support |
| 17 of 109 |
| Based on discussions had with the TSSC chief engineer at Randolph AFB during the site visit, he indicated all ATD software, other than the Aircraft OFP software, was maintained by the TSSC facility and their contractor used to sustain the simulators. It is our understanding that under a separate solicitation out of Wright Patterson AFB, the TSSC facility will award a separate 5-year contract to maintain and support the TSSC trainer software. If this is the case, then what role will the winning prime assume with respect to support of the ATD software? Please clarify roles and responsibilities between the TSSC contractor and the T-38C AvSIP contractor. |
Government Response: The TSSC chief engineer misinformed the site visit participants. Please refer to the documents for this solicitation for contractor requirements related to the ATD systems.
Note: All documents available to the Government have been provided in the Bidder’s Library dated 28 January 2015.
Missing and found drawings for MDP
| Document Number |
| Title/Description |
| Status |
| Provided in latest Release |
| 71A262111 |
| MDP Shelf Drawing |
| Missing from package. Contractor requests this document. |
| Yes |
| T38-004-960461 |
| IAI T38 MDP Subsystem Spec |
| Missing from package. Contractor requests this document. |
| Unavailable |
71D264002 Rev A
| T-38C MDP Breakout Box |
| Missing from package. Contractor requests this document. |
| Yes |
| 71D263805 |
| MDP Breakout Box |
| Missing from package. Contractor requests this document. |
| Yes |
| 71D263813 |
| Shorting Plug MDP Software Loader |
| Missing from package. Contractor requests this document. |
| Yes |
| 71A262001 |
| Nose Equip Bay Instl |
| Missing from package. Contractor requests this document. |
| Yes |
All Missing Drawings
Drawing Number/ Document Number
| Description |
| Release Date/Rev |
| Note |
| Provided in latest Release |
| T-38C System Performance Specification, Rev H |
| 14-Feb-11 |
| specified in MDP SOO |
The latest revision is revision “I”. Revision I is provided as part of the Bidder’s Library.
Yes
| AETC 001-94-III |
| Operational Requirements Document |
| 13-Feb-01 |
| specified in MDP SOO |
This has been deleted from the SOOs. Please ensure work is being accomplished IAW the correct revision of the document.
No
| 71A260202 |
| Weight And Balance Procedures |
| C |
Yes
| 71A263768 |
| Embedded GPS/ INS - System Wiring Diagram |
| E |
Yes
| 71A263776 |
| Communications - System Wiring Diagram |
| H |
Yes
| 71A263778 |
| Mode S Transponder/TCAS - System Wiring Diagram |
| G |
Yes
| 71A263779 |
| HUD and UFC - System Wiring Diagram |
| E |
Yes
| 71A263783 |
| Mission & Display Proc - System Wiring Diagram |
| E |
Yes
| 71D263803 |
| EGI Boresight Extension Cable |
| N/C |
| contractor supplied test equipment |
| Yes |
| 71D263804 |
| SAS/Boresight Data Load Cable |
| N/C |
| contractor supplied test equipment |
| Yes |
| 71D263808 |
| EED Fuel Quantity Test Cable |
| N/C |
| contractor supplied test equipment |
| Yes |
| 71D263814 |
| Cable Assembly - Fuel Crossfeed |
| N/C |
| contractor supplied test equipment |
| Yes |
| 71D264000 |
| Pitot Static System Adapter Kit |
Yes
| D-55089-500000 |
| Interface Specification for VDTS |
| 02/23/10 |
Yes
| 90A020009 |
| Parts List, T-38 Operational Flight Trainer |
| 01/08/2010 - H |
Yes
| 90A020014 |
| Parts List, T-38 Unit Training Device |
| 01/08/2010 - D |
Yes
| 90A020023 |
| Parts List, T-38 Weapons Trainer |
| 01/04/2010 - D |
Yes
| PS4453-0000-00 |
| El-Op T-38 Avionics Upgrade Program PDU Specification |
Yes
| PS4453-0000-00 |
| El-Op T-38 Avionics Upgrade Program UFCP Specification |
Yes
| 970578 |
| Serial Data Communication Protocol |
Yes
| T38/004/960461 |
| IAI T38 Mission and Display Processor Subsystem Specification |
| 2-Apr-98 |
Unavailable
| 71A260100 |
| T-38 Top Installation Drawing |
| E |
Yes
| 71A261308 |
| MIP Installation, Fwd |
| E |
Yes
| 71A261311 |
| MIP Installation, Aft |
| G |
Yes
| 71A261802 |
| HUD Installation |
| E |
Yes
| 71A263201 |
| Cable Assy L Avion Bay |
| F |
Yes
| 71A263202 |
| Cable Assy R Avion Bay |
| E |
Yes
| 71A263301 |
| Cable Assy Fwd MIP |
| C |
Yes
| 71A263401 |
| Cable Assy Aft MIP |
| E |
Yes
Software Requirements Specification (MDP)
Unavailable
MDP Prime Item Development Specification
Unavailable
HUD Prime Item Development Specification
Unavailable
HUD Power Supply Unit Prime Item Development Specification
Unavailable
UFCP Prime Item Development Specification
Unavailable
Mode S Transponder Prime Item Development Specification
Unavailable
TCAS II Processor Prime Item Development Specification
Unavailable
| 047-09406-0014 |
| Mounting Rack (Transponder Mode-S) |
Yes
| 047-09855-0004 |
| Mounting Rack (TCAS II) |
Yes
| 71A263102-1001 |
| Drawing for Electrical Installation, Right Hand Forward Fuselage |
Yes
| 200733822 |
| Reverse Polarity Tee |
Yes
| 200733823 |
| Coaxial Tee Shorting Adapter |
Yes
| 906309 |
| T-38C Interface Control Document |
| latest |
| version we have is very old and out of date |
A revision dated 12/11/12 has been provided in the latest version of the Bidder’s Library.
Yes
T-38 Weapons System Capability Roadmap
Will be provided post award (See Avionics System Roadmap provide in Bidder’s Library)
508th Aircraft Sustainment Wing Operating Instructions (ASWOI)
508th Aircraft Sustainment Wing does not exist. OIs are not valid. The T-38 SPO is assigned to AFLCMC/Mobility Directorate/Mature and Proven Aircraft Division.
Operational Safety Suitability and Effectiveness (OSS&E) Implementation Plan
This document is no longer required to be maintained.
OSS&E Internal Management Plan
This document is no longer required to be maintained.
T-38 Life-Cycle Sustainment Plan
Will be provided post award
T-38C Data Quality Requirements (DQR) Block 9
Yes
CNS/ATM Data Compliance Plan for the T-38C
In Coordination
| 906309 |
| T-38C TCAS II/ Mode-S Transponder Physical Interface Control Document |
Yes
| 16-1898-1 |
| BEZEL ASSY |
| Group A Part Drawing |
| Unavailable |
| 71A261102 |
| TUBE ASSY |
| Group A Part Drawing |
| Yes |
| 71A261117 |
| PANEL, REMOVABLE |
| Group A Part Drawing |
| Yes |
| 71A261122 |
| BUSHING |
| Group A Part Drawing |
| Yes |
| 71A261133 |
| ROD ASSY |
| Group A Part Drawing |
| Yes |
| 71A261135 |
| TRAY ASSY |
| Group A Part Drawing |
| Yes |
| 71A261137 |
| BRACKET ASSY |
| Group A Part Drawing |
| Yes |
| 71A261140 |
| MARKER |
| Group A Part Drawing |
| Yes |
| 71A261141 |
| STRAP, FWD |
| Group A Part Drawing |
| Yes |
| 71A261201 |
| SUB INSTRUMENT PANEL ASSY, FWD |
| Group A Part Drawing |
| Yes |
| 71A261202 |
| DP PLATE |
| Group A Part Drawing |
| Yes |
| 71A261203 |
| SUB INSTRUMENT PANEL ASSY, FWD |
| Group A Part Drawing |
| Yes |
| 71A261206 |
| GLARESHIELD ASSY |
| Group A Part Drawing |
| Yes |
| 71A261208 |
| PANEL ASSY |
| Group A Part Drawing |
| Yes |
| 71A261212 |
| SUB INSTRUMENT PANEL ASSY, AFT CREW |
| Group A Part Drawing |
| Yes |
| 71A261213 |
| SUB INSTRUMENT PANEL ASSY, AFT CREW |
| Group A Part Drawing |
| Yes |
| 71A261218 |
| PANEL, WOW |
| Group A Part Drawing |
| Yes |
| 71A261220 |
| ADAPTER ASSY |
| Group A Part Drawing |
| Yes |
| 71A261811 |
| SUPPORT ASSY |
| Group A Part Drawing |
| Yes |
| 71A262031 |
| PANEL, DC CB |
| Group A Part Drawing |
| Yes |
| 71A262032 |
| PANEL, DC POWER |
| Group A Part Drawing |
| Yes |
| 71A262033 |
| PANEL, GPS CRYPTO |
| Group A Part Drawing |
| Yes |
| 71A262110 |
| TRAY ASSY |
| Group A Part Drawing |
| Yes |
| 71A262110 |
| TRAY, TACAN |
| Group A Part Drawing |
| Yes |
| 71A262111 |
| TRAY, MISSION DISPLAY PROCESSOR |
| Group A Part Drawing |
| Yes |
| 71A262113 |
| BOX, CIRCUIT BREAKER, FWD STRUCTURAL |
| Group A Part Drawing |
| Yes |
| 71A262113 |
| COVER, CIRCUIT BREAKER BOX |
| Group A Part Drawing |
| Yes |
| 71A262114 |
| ADAPTER ASSY, STATIC INVERTER, FUEL FLOW |
| Group A Part Drawing |
| Yes |
| 71A262114 |
| MOUNT PLATE, FUEL FLOW P/S |
| Group A Part Drawing |
| Yes |
| 71A262115 |
| TRAY, AVIONICS |
| Group A Part Drawing |
| Yes |
| 71A262115 |
| ADAPTER |
| Group A Part Drawing |
| Yes |
| 71A262120 |
| SHELF, VOR-ILS-RCVR, VHF COMM |
| Group A Part Drawing |
| Yes |
| 71A262121 |
| TRAY ASSY, TRU |
| Group A Part Drawing |
| Yes |
| 71A262122 |
| BRACKET, MODE S RACK |
| Group A Part Drawing |
| Yes |
| 71A262122 |
| PANEL, BATTERY HOLD-DOWN |
| Group A Part Drawing |
| Yes |
| 71A262123 |
| ADAPTER, TCAS ANTENNA PANEL |
| Group A Part Drawing |
| Yes |
| 71A262125 |
| BRACKET, ASSEMBLY |
| Group A Part Drawing |
| Yes |
| 71A262125 |
| SUPPORT |
| Group A Part Drawing |
| Yes |
| 71A262125 |
| DOUBLER ASSY |
| Group A Part Drawing |
| Yes |
| 71A262126 |
| SHELF, NAVIGATION UNIT |
| Group A Part Drawing |
| Yes |
| 71A262130 |
| BRACKET |
| Group A Part Drawing |
| Yes |
| 71A262130 |
| TRAY, MOUNT, BATTERY |
| Group A Part Drawing |
| Yes |
| 71A262133 |
| SCREEN |
| Group A Part Drawing |
| Yes |
| 71A262135 |
| SUPPORT |
| Group A Part Drawing |
| Yes |
| 71A262136 |
| DOUBLER |
| Group A Part Drawing |
| Yes |
| 71A262140 |
| COVER, FUSE |
| Group A Part Drawing |
| Yes |
| 71A262151 |
| MARKER |
| Group A Part Drawing |
| Yes |
| 71A262152 |
| MARKER |
| Group A Part Drawing |
| Yes |
| 71A262153 |
| MARKER |
| Group A Part Drawing |
| Yes |
| 71A262210 |
| SPACER, BAY DOORS |
| Group A Part Drawing |
| Yes |
| 71A262230 |
| SHIELD ASSY, TCAS |
| Group A Part Drawing |
| Yes |
| 71A262321 |
| TUBE ASSY |
| Group A Part Drawing |
| Yes |
| 71A262322 |
| TUBE ASSY |
| Group A Part Drawing |
| Yes |
| 71A262323 |
| TUBE ASSY |
| Group A Part Drawing |
| Yes |
| 71A262330 |
| MANIFOLD ASSY |
| Group A Part Drawing |
| Yes |
| 71A262331 |
| SHIELD ASSY, WATER |
| Group A Part Drawing |
| Yes |
| 71A262332 |
| CONTACTOR |
| Group A Part Drawing |
| Yes |
| 71A263000 |
| CABLE ASSY |
| Group A Part Drawing |
| Yes |
| 71A263201 |
| MARKER |
| Group A Part Drawing |
| Yes |
| 71A263202 |
| MARKER |
| Group A Part Drawing |
| Yes |
| 71A263203 |
| MARKER |
| Group A Part Drawing |
| Yes |
| 71A263210 |
| CABLE ASSY, UHF COMM RADIO |
| Group A Part Drawing |
| Yes |
| 71A263211 |
| CABLE ASSY |
| Group A Part Drawing |
| Yes |
| 71A263211 |
| CABLE ASSY, VHF LOWER ANTENNA |
| Group A Part Drawing |
| Yes |
| 71A263212 |
| CABLE ASSY, UHF LOWER ANTENNA |
| Group A Part Drawing |
| Yes |
| 71A263213 |
| CABLE ASSY, MODE S UPPER ANTENNA |
| Group A Part Drawing |
| Yes |
| 71A263214 |
| CABLE ASSY |
| Group A Part Drawing |
| Yes |
| 71A263216 |
| CABLE ASSY |
| Group A Part Drawing |
| Yes |
| 71A263216 |
| CABLE ASSY, ILS/GLIDESLOPE ANTENNA |
| Group A Part Drawing |
| Yes |
| 71A263217 |
| CABLE ASSY |
| Group A Part Drawing |
| Yes |
| 71A263218 |
| CABLE ASSEMBLY |
| Group A Part Drawing |
| Yes |
| 71A263220 |
| CABLE ASSY, TCAS UPPER ANTENNA |
| Group A Part Drawing |
| Yes |
| 71A263221 |
| CABLE ASSY, TCAS LOWER ANTENNA |
| Group A Part Drawing |
| Yes |
| 71A263222 |
| CABLE ASSY |
| Group A Part Drawing |
| Yes |
| 71A263223 |
| CABLE, RADAR ALTIMETER |
| Group A Part Drawing |
| Yes |
| 71A263223 |
| CABLE ASSY |
| Group A Part Drawing |
| Yes |
| 71A263224 |
| CABLE ASSY |
| Group A Part Drawing |
| Yes |
| 71A263225 |
| CABLE ASSY |
| Group A Part Drawing |
| Yes |
| 71A263302 |
| MARKER |
| Group A Part Drawing |
| Yes |
| 71A263303 |
| MARKER |
| Group A Part Drawing |
| Yes |
| 71A263304 |
| MARKER |
| Group A Part Drawing |
| Yes |
| 71A263402 |
| MARKER |
| Group A Part Drawing |
| Yes |
| 71A263403 |
| MARKER |
| Group A Part Drawing |
| Yes |
| 71A263514 |
| CABLE ASSY, GPS |
| Group A Part Drawing |
| Yes |
| 71A263515 |
| GPS, ANTENNA CABLE |
| Group A Part Drawing |
| Yes |
| 71A263521 |
| CABLE ASSY, TCAS |
| Group A Part Drawing |
| Yes |
| 71A26352 |
| CABLE ASSY, TACAN |
| Group A Part Drawing |
| Yes |
| 71A263523 |
| COAX, TACAN LOWER |
| Group A Part Drawing |
| Yes |
| 71A263524 |
| COAX, TACAN UPPER |
| Group A Part Drawing |
| Yes |
| 71A263612 |
| MARKER |
| Group A Part Drawing |
| Yes |
| 71A263620 |
| CABLE ASSY |
| Group A Part Drawing |
| Yes |
| 71B261507 |
| LIGHT PLATE |
| Group A Part Drawing |
| Yes |
| 71B261507 |
| PANEL |
| Group A Part Drawing |
| Yes |
| 71R261807 |
| BRACKET (SPEED BRAKE) |
| Group A Part Drawing |
| Yes |
| 71R263100 |
| TACAN CTRL HD HARNESS W/CANNON |
| Group A Part Drawing |
| Yes |
| 71R263808 |
| BANDMARKER (SPEED BRAKE) |
| Group A Part Drawing |
| Yes |
| 71R263810 |
| BOX, CIRCUIT BREAKER, FWD |
| Group A Part Drawing |
| Yes |
| 74A800741 |
| ADAPTER ASSY |
| Group A Part Drawing |
| Yes |
| 71A262001 |
| Nose Equip Bay Instl |
| N |
| specified in MDP SOO |
| Yes |
| 71A262111 |
| MDP Shelf Assy |
| C |
| specified in MDP SOO |
| Yes |
| 71D263805 |
| MDP Breakout Box |
| N/C |
| contractor supplied test equipment |
| Yes |
| 71D263813 |
| Shorting Plug MDP Software Loader |
| N/C |
| contractor supplied test equipment |
| Yes |
| 71D264002 |
| T-38C MDP Breakout Box |
| A |
Yes
ATTACHMENT_8_GFE_List.pdf
List of Government Furnished Equipment (GFE) as Suppliers/Vendors
ASSET ID P/N Nomenclature S/N Supplier Location Manufacturer
506292 10400-640 MULTI-FUNCTION DISPLAY 0003 VENSC705 (IAI) L-3 COMM DISPLAY SYSTEMS 506293 10400-640 MULTI-FUNCTION DISPLAY 0006 VENSC705 (IAI) L-3 COMM DISPLAY SYSTEMS
Material 640120-917 LCD ASSEMBLY 0431 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-917 LCD ASSEMBLY 0548 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-917 LCD ASSEMBLY 0559 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-917 LCD ASSEMBLY 0602 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-917 LCD ASSEMBLY 0673 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-917 LCD ASSEMBLY 0676 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-917 LCD ASSEMBLY 0755 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-917 LCD ASSEMBLY 0832 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-917 LCD ASSEMBLY 0845 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-917 LCD ASSEMBLY 0858 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-917 LCD ASSEMBLY 0895 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-918 LCD ASSEMBLY 1078 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-918 LCD ASSEMBLY 1079 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-918 LCD ASSEMBLY 1082 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1202 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1203 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1320 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1334 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1349 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1367 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1378 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1427 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1514 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1519 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1548 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1567 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1570 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1665 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1682 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1698 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1714 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1721 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1723 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1772 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1779 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1781 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1784 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1785 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1791 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1792 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1797 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1809 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1813 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1815 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1817 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1821 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1822 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1825 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1834 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1836 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1837 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1839 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS
DRAFT
Material 640120-919 LCD ASSEMBLY 1842 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1844 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1847 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1848 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1849 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1851 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1854 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1856 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1857 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1858 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1859 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1863 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1866 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1867 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1869 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1884 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1887 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1888 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1892 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1899 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1900 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1908 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1926 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1927 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1929 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1930 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1932 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1933 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1934 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1936 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1940 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1941 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1942 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1943 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1944 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1945 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1948 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1949 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1951 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1952 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1953 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1954 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1955 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1956 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1957 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1958 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1959 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1960 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1961 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1962 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1963 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1964 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1965 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1966 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1967 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS
Material 640120-919 LCD ASSEMBLY 1968 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1969 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1970 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1971 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1972 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1973 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1975 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1976 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1977 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1981 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1982 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS Material 640120-919 LCD ASSEMBLY 1983 T38L3DS-ATLANTA L-3 COMM DISPLAY SYSTEMS
T-38 System Integration Lab - Avionics
ASSET ID P/N Nomenclature S/N Manufacturer
455759 T38-100.1000 SYSTEM INTEGRATION LAB (SIL-2) TEST 0001 ISRAEL AEROSPACE INDUSTRIES LTD.
455759-001 9021720200-1 STICK GRIP 151 ESSEX MFG DIVISION
455759-002 071-1377-02 VHF NAV BACKUP CONTROL HEAD 3858 ALLIED SIGNAL INC
455759-003 064-1047-01 VHF TRANSCEIVER 4053 ALLIED SIGNAL INC
455759-004 064-01076-0101 UHF TRANSCEIVER 1034 ALLIED SIGNAL INC
455759-005 066-01101-00 VHF NAV (VOR/ILS) RECEIVER 4215 ALLIED SIGNAL INC
455759-006 066-01101-00 VHF NAV (VOR/ILS) RECEIVER 3830 ALLIED SIGNAL INC
455759-007 066-01143-0601 TRANSPONDER MODE S TCAS XP 2541 ALLIED SIGNAL INC
455759-008 34200602-3SRB EMBEDDED GPS/INS 1520 HONEYWELL-MINNEAPOLIS (SENSORS)
455759-009 34200602-3SRB EMBEDDED GPS/INS 1072 HONEYWELL-MINNEAPOLIS (SENSORS)
455759-010 4477-1000-80 HUD POWER SUPPLY UNIT 2004 ELBIT SYSTEMS ELECTRO OPTICS E
455759-011 D55000-550000 DATA TRANSFER UNIT 891 VECTOP
455759-012 D-33062-000-550000 VIDEO AND DATA TRANSFER SYSTEM 359 VECTOP
455759-013 9021720400-3 THROTTLE GRIP (I/B) 00003 ESSEX MFG DIVISION
455759-014 9021720400-1 THROTTLE GRIP (I/B) 0001 ESSEX MFG DIVISION
455759-015 HG1140AA01 AIR DATA COMPUTER 0004 HONEYWELL-MINNEAPOLIS (SENSORS)
455759-027 4453-1000-00 UP FRONT CONTROL PANEL 1008 ELBIT SYSTEMS ELECTRO OPTICS E 455759-028 MT89030100-30 ANTENNA OVERRIDE RELAY MODULE 0530 BAE SYSTEMS MFG TECHNOLOGY INC
455759-029 AL-15-1289-3 AUDIO INTERFACE UNIT 0003 ORBIT COMMUNICATION SYSTEM LTD
455759-030 104-642-02-01 MULTI-FUNCTION DISPLAY 0106 L-3 COMM DISPLAY SYSTEMS
455759-033 623700-4 MISSION AND DISPLAY PROCESSOR 13705 ASTRONAUTICS CORP OF AMERICA
455759-034 4A0235 RF SPLITTER 0003 ANAREN CERAMICS INC
455759-038 064-1047-01 VHF TRANSCEIVER 4034 ALLIED SIGNAL INC
455759-042 640-915-02-01 ELECTRONIC ENGINE DISPLAY 0102 L-3 COMM DISPLAY SYSTEMS
455759-043 104-642-02-01 MULTI-FUNCTION DISPLAY 0107 L-3 COMM DISPLAY SYSTEMS
455759-044 104-642-02-01 MULTI-FUNCTION DISPLAY 0610 L-3 COMM DISPLAY SYSTEMS
455759-045 104-642-02-01 MULTI-FUNCTION DISPLAY 2306 L-3 COMM DISPLAY SYSTEMS
455759-046 4453-1000-00 UP FRONT CONTROL PANEL 1004 ELBIT SYSTEMS ELECTRO OPTICS E
455759-047 AL-15-1290-2 AUDIO CONTROL PANEL 0006 ORBIT COMMUNICATION SYSTEM LTD
455759-048 RY673 YSAS CONTROL ASSEMBLY J4521 ELECTRONIC SPECIALTY COMPANY
455759-050 4452-1000-01 HEAD-UP DISPLAY 1004 ELBIT SYSTEMS ELECTRO OPTICS E
455759-051 T38-118-02 CTVS (HUD VIDEO CAMERA) 1157 VECTOP
455759-052 4453-1000-00 UP FRONT CONTROL PANEL 1007 ELBIT SYSTEMS ELECTRO OPTICS E
455759-053 AL-15-1290-2 AUDIO CONTROL PANEL 0001 ORBIT COMMUNICATION SYSTEM LTD
455759-054 805D0663-31 TACAN BACKUP CONTROL PANEL 80005 L3 COMM AVIONICS SYSTEMS
455759-055 71B261504-101 AVIONICS ACTIVATION PANEL 002 THE BOEING CO. - SAINT LOUIS
455759-056 071-1377-00 VHF NAV BACKUP CONTROL HEAD 3852 ALLIED SIGNAL INC
455759-057 071-01576-1201 UHF BACKUP CONTROL HEAD 1006 ALLIED SIGNAL INC
455759-058 D-33062-000-550000 VIDEO AND DATA TRANSFER SYSTEM 5 VECTOP
455759-059 D55000-550000 DATA TRANSFER UNIT 136 VECTOP
455759-060 V-80AB-FD VIDEO TAPE RECORDER 622235 TEAC AMERICA INC
455759-061 9021720400-2 THROTTLE GRIP (O/B) 0006 ESSEX MFG DIVISION
455759-062 9021720400-3 THROTTLE GRIP (I/B) 00001 ESSEX MFG DIVISION
455759-076 402JST-6301 RF SWITCH 168 DOW-KEY MICROWAVE CORP
455759-077 9021720200-1 STICK GRIP 0009 ESSEX MFG DIVISION
455759-078 805D0602-45 TACAN RECEIVER/TRANSMITTER 80011 L3 COMM AVIONICS SYSTEMS
455759-079 064-01076-0101 UHF TRANSCEIVER 1033 ALLIED SIGNAL INC
455759-080 071-00097-1000 CM 67A TCAS CONFIG. MODULE 1424 ALLIED SIGNAL INC
455759-081 HG1140AA01 AIR DATA COMPUTER 0003 HONEYWELL-MINNEAPOLIS (SENSORS)
455759-090 AL-15-1289-3 AUDIO INTERFACE UNIT 0001 ORBIT COMMUNICATION SYSTEM LTD
455759-100 4477-1000-80 HUD POWER SUPPLY UNIT 1001 ELBIT SYSTEMS ELECTRO OPTICS E
455759-103 M25708/3-03 DME ANTENNA 4267 SENSOR SYSTEMS INC
455759-104 S67-1575-49 GPS ANTENNA 1522 SENSOR SYSTEMS INC
455759-105 D-33062-000-550000 VIDEO AND DATA TRANSFER SYSTEM 110 ISRAEL AEROSPACE INDUSTRIES LTD.
455759-106 640-915-02-01 ELECTRONIC ENGINE DISPLAY 0104 L-3 COMM DISPLAY SYSTEMS
455759-107 D-35029-00-550000 VIDEO AND DATA TRANSFER UNIT 28 ISRAEL AEROSPACE INDUSTRIES LTD.
455759-108 D-35029-00-550000 VIDEO AND DATA TRANSFER UNIT 18 ISRAEL AEROSPACE INDUSTRIES LTD.
455759-109 623700-4 MISSION AND DISPLAY PROCESSOR 11705 ASTRONAUTICS CORP OF AMERICA
506286 640-915-02-02 ELECTRONIC ENGINE DISPLAY 2042 L-3 COMM DISPLAY SYSTEMS
506287 640-915-02-02 ELECTRONIC ENGINE DISPLAY 2130 L-3 COMM DISPLAY SYSTEMS
T-38 System Integration Lab - Test Equipment
ASSET ID Model or P/N Nomenclature S/N Manufacturer
455759-037 82872 HEADSET NONE ASTROCOM ELECTRONICS INC
455759-035 10253B HEADSET 0809 ASTROCOM ELECTRONICS INC
455759-036 10253B HEADSET 9620 ASTROCOM ELECTRONICS INC
232964 361-015-001 TEST SET ELECTRONIC 762 GULL ELECTRONIC SYSTEMS DIV
455759-084 375BNM RF TERMINATOR 28 NARDA MICROWAVE CORP
455759-085 376BNM TERMINATOR RF 9502 NARDA MICROWAVE CORP
271264 4304A WATTMETER 073700344 BIRD ELECTRONIC CORP
455759-089 765-10 RF ATTENUATOR 8409 NARDA MICROWAVE CORP
455759-087 766-20 RF ATTENUATOR 04517 NARDA MICROWAVE CORP
455759-086 768-30 RF ATTENUATOR 8308 NARDA MICROWAVE CORP
271263 MPS31C TEST SET AIR DATA 6311 DMA-AERO
237867 NAV2000R GENERATOR SIGNAL 286 JCAIR INC
233236 NC4280E REFERENCE JUNCTION HADES MFG CORP
235305 NPN235305 CAABLE DISCRETE BOEING COMPANY THE
455759-071 NPN455759-071 CONTROL BOX T38 AUP RADIO THE BOEING CO. - SAINT LOUIS
506237 NPN506237 BREAKOUT BOX PSU/HUD THE BOEING CO. - SAINT LOUIS
235302 PVM8044Q DISPLAY VTC 2515071 SONY CORP OF AMERICA
236901 SDX2000 GENERATOR SIGNAL 138 JCAIR INC
506236 T-0060550 YSAS BREAKOUT BOX THE BOEING CO. - SAINT LOUIS
235301 T-60B POWER SUPPLY ASSEMBL MICROSYSTEMS ENGINEERING CORP
455759-101 10355-B HEADSET ASTROCOM ELECTRONICS INC
506235 PVM-8045Q MONITOR COLOR 2000340 SONY CORP OF AMERICA
506238 PVM-8045Q MONITOR COLOR 2000338 SONY CORP OF AMERICA
455759-098 PVM-20N1U COLOR MONITOR 6002510 SONY CORP OF AMERICA
455759-041 5040 X-Y MONITOR 1614 ELECTRO STATIC FINISHING INC
455759-049 5114R X-Y MONITOR (INSTALLED IN BEN 1463 ELECTRO STATIC FINISHING INCDRAFT
T-38 System Integration Lab - Computing Equipment
ASSET ID Model or P/N Nomenclature S/N Manufacturer
455759-063 2007FPB FLAT PANEL MONITOR G324H-74262-891-1YML DELL
455759-064 2007FPB FLAT PANEL MONITOR G324H-74262-891-1YJL DELL
455759-065 2007FPB FLAT PANEL MONITOR C9536-74262-7BM-1T0S DELL
455759-067 O2 TALON COMPUTER (SG) 0800690CA652 SILICON GRAPHICS FEDERAL INC
455759-072 NPN455759-072 COMPUTER SIL MODELS HOST 108698 COLFAX INTERNATIONAL
455759-082 RAW-USB2.0 COMPACT FLASH DRIVE USB 2.0 NONE CAT-API
455759-083 NO MODEL NUMBER DVD DUPLICATOR LC321591 PIONEER COMPUTER
455759-091 TH3BA-EU BACKUP DRIVE CX72101485 QUANTUM3D INC
455759-092 064-0003-001 BACKUP DRIVE DS0HWAT SEAGATE TECHNOLOGY
455759-096 GDM-20E21 TRAINER MONITOR 2075449 SGI
455759-097 SLGR-002-01 ZIP DRIVE 980215305418 SILICON GRAPHICS FEDERAL INC
506239 HP7550 ALPHA MONITOR CNC4020QLR HEWLETT PACKARD CO
506241 4350XT BACKUP DRIVE YAA63756 ARCHIVE CORP
506297 FB47H-AA COMPUTER ALPHA NI65201OYJ DIGITAL
455759-039 VT420 DUMMY MONITOR HK14004452 VECMAR CORPORATION INC
455759-040 VT420 DUMMY MONITOR TA242B4666 VECMAR CORPORATION INC
455759-066 90B20084-101 PC BOEING TRAINING SYSTEMS
455759-068 LS902UT TALON MONITOR 9GGG41B205351 SGI
455759-073 90B200067-117 PC 121894-1 COLFAX INTERNATIONAL
455759-074 90B200067-117 PC 121894-2 COLFAX INTERNATIONAL
455759-075 DESKJET 5850 PRINTER MY3AG1N2DB HEWLETT-PACKARD CO
455759-099 NPN455759-099 SIL MODELS MOS PC S000020748 SYS TECHNOLOGY
455759-102 SUPERSERVER 6013P-8 SIL MODELS PC S6013P814302124 SUPERMICRO COMPUTER
455759-110 SLGR-002-01 ZIP DRIVE 746N220407 SILICON GRAPHICS FEDERAL INC
506296 CHRG01LF0075 BATTERY CHARGER 37H0002012AD DELL
455759-088 GS608 V2 MBPS SWITCH 1FK1715U01CB8 NETGEAR INC.
235300 PC104 COMPUTER PROCESSOR MICROSYSTEMS ENGINEERING CORPDRAFT
ATD Equipment at Contractor
455758 90A020009 TRAINER, T-38 001 BOEING TRAINING SYSTEMS
455771 DGS-1224T SWITCH NONE D-LINK TAIWAN
455772 DGS-1224T SWITCH N/A D-LINK TAIWAN
455780 CX-24831 ATD SERVER COLFAX INTERNATIONAL
455781 CX-23783 ATD WINDOWS BUILD PC 112724 COLFAX INTERNATIONAL
455782 90B200084-101 COMPUTER (HOST PROTOTYPE) 125504 COLFAX INTERNATIONAL
455787 ACE-R1U ASTI RIU 39737 ASTI
455788 ACE-R1U ASTI RIU 39351 ASTI
455789 SUA1000 UPC POWER BACKUP AS0811346595 AMERICAN POWER CORP
455790 SUA1000 UPC POWER BACKUP AS0523311866 AMERICAN POWER CORP
506233 10704-016 BLOWER, EXHAUST 381-500 SCHROFF INC
506234 60713-013 FAN 97153122 SCHROFF INC
506240 EV-C200 VIDEO PLAYER HI-8 SONY ELECTRONICS INC.
506298 V-80AB-FD RECORDER AIRBORNE VIDEO 622450 TEAC AMERICA INC
455758-001 VTD15-850M POWER SUPPLY, +/-15 VDC ACOPIAN CORP
455758-010 AIU-1-A AIU 23328 ASTI
455758-011 AIU-1-A AIU 18889 ASTI
455758-013 AB1150 AVIONICS BUS BOX 1155B BALLARD TECHNOLOGY
455758-014 OMNIVIEW PRO KVM 100701036422 BELKIN COMPONENTS
455758-019 90A410422-1001 SITE SERVER 6 BOEING TRAINING SYSTEMS
455758-022 90B410145-101 IG CHANNEL 116438-1 COLFAX INTERNATIONAL
455758-024 90B410145-101 IG CHANNEL 116438-11 COLFAX INTERNATIONAL
455758-025 90B410145-101 IG CHANNEL 116438-20 COLFAX INTERNATIONAL
455758-026 CX-16805 SERVER PCVSC 117660-2 COLFAX INTERNATIONAL
455758-027 CX-16805 SERVER PCVSC 117660-1 COLFAX INTERNATIONAL
455758-028 90B20066-103 COMPUTER IG 126910-1 COLFAX INTERNATIONAL
455758-029 2007FP MONITOR DELL
455758-031 CX-38417 COMPUTER PERSONAL 122505 COLFAX INTERNATIONAL
455758-033 CX-31794 COMPUTER IOS 117662-2 COLFAX INTERNATIONAL
455758-034 CX-31794 COMPUTER IOS 117662-1 COLFAX INTERNATIONAL
455758-036 2007FP MONITOR DELL
455758-037 2007FP MONITOR DELL
455758-038 2007FP MONITOR DELL
455758-042 CAU97028 STICK PITCH/ROLL C/L ACTUATOR 618 MOOG FCS BV
455758-043 CAU97028 STICK PITCH/ROLL C/L ACTUATOR 063 MOOG FCS BV
455758-044 CAU97028 STICK PITCH/ROLL C/L ACTUATOR 837 MOOG FCS BV
455758-045 CPS98037 CONTROL LOADER POWER SUPPLY 90240085 MOOG FCS BV
455758-046 CPS98037 CONTROL LOADER POWER SUPPLY 805460039 MOOG FCS BV
455758-047 CPS98037 CONTROL LOADER POWER SUPPLY 805460020 MOOG FCS BV
455758-048 CPS98037 CONTROL LOADER POWER SUPPLY 805460021 MOOG FCS BV
455758-049 D55000-550000 DATA TRANSFER UNIT 217 VECTOP
455758-050 D55000-550000 DATA TRANSFER UNIT 102 VECTOP
455758-051 CIA100 COMPUTER VIDEO INTERFACE 634308037E1189 INLINE INC
455758-052 LZS-1000-3 POWER SUPPLY, +28 VDC 43821028347 LAMBDA ELECTRONICS INC
455758-053 640-915-02-02 ELECTRONIC ENGINE DISPLAY 0804 L-3 COMM DISPLAY SYSTEMS
455758-054 640-915-02-02 ELECTRONIC ENGINE DISPLAY 0887 L-3 COMM DISPLAY SYSTEMS
455758-055 RGB190F INTERFACE COMPUTER VIDEO RGB SYSTEMS INC. (DBA EXTRON)
455758-056 351-900052-001 MULTIFUNCTION DISPLAY 12 SYMBOLIC DISPLAYS INC.
455758-057 85913153 REV F 810 BOARD 869019 GENERAL ELECTRIC
455758-058 351-900052-001 MULTIFUNCTION DISPLAY 24 SYMBOLIC DISPLAYS INC.
455758-059 351-900053-002 UP FRONT CONTROL (UFCP) 10 SYMBOLIC DISPLAYS INC.
455758-060 351-900053-002 UP FRONT CONTROL (UFCP) 11 SYMBOLIC DISPLAYS INC.
455758-061 18283G-05 HEADSET/AVIATION/MODEL NO. H10-66 DAVID CLARK COMPANY INC
455758-062 18284G-01 HEADSET/AVIATION/MODEL NO. H10-66 5965-01-390-9240 DAVID CLARK COMPANY INC 455758-063 B020-008-17 SWITCH KVM RACK MOUNT 9921ACPCB715-10044 TRIPP LITE MFG CO
455758-069 MIXER 221 WESTAR EZ BLEND 0021 WESTAR DISPLAY TECH, INC.
455758-078 90A200019-1003 COMPUTER (GSS) LEADING TECHNOLOGY MICRO INC.
455758-079 90A200019-1001 COMPUTER (HOST) LEADING TECHNOLOGY MICRO INC.
455758-089 DFE-530TX+ CCA, ETHERNET B22924C009083 D-LINK SYSTEMS INC
455758-090 81389-02 CCA, MODULAR FOCAS C0228-08 COMMUNITRONICS CORP
ATD Equipment at Contractor
455758-091 90A410028-1001 CCA, BIT CONTROLLER 035 THE BOEING CO. - SAINT LOUIS
455758-092 90A410028-1001 CCA, BIT CONTROLLER 0068 THE BOEING CO. - SAINT LOUIS
455758-093 VMIVME-4132-011 ANALOG OUTPUT CIRCUIT CARD 470661 VMIC
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