DID_DI-SESS-80255A.pdf
PDF 30 KB Posted
- Attached to
- Overhaul of B-2 Flight Control Actuators Federal contract opportunity
- Solicitation number
- FA8118-20-R-0009
About this file
This solicitation seeks proposals for the overhaul of seven hydraulic servomechanisms used on the B-2 bomber aircraft. The Air Force Sustainment Center is contemplating awarding a firm fixed price, indefinite delivery requirements contract for a one-year base period and two one-year options. The contractor shall provide all labor, facilities, equipment and materials to overhaul the servomechanisms. Estimated quantities for each part number are provided for the base year and options. Delivery of six units per month is required beginning 30 days after order receipt. The response deadline is January 30, 2020 and award is estimated for September 26, 2020. Qualification requirements apply and interested vendors must request approval. The incumbent is Moog, Inc. Export control and set-aside provisions do not apply.
This document provides the part numbers, dimensions, and materials for the seven hydraulic servomechanisms requiring overhaul. It also lists the applicable technical orders and manuals to be followed, DoD forms to be used, and contractor documents for assembly and test procedures.
View the file
Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| CDRLS.pdf | ||
| B-2_PWS_v4_1_FINAL.pdf | ||
| FA811820R0009_______0001.pdf | ||
| Wage_Determination_NewYork.pdf | ||
| DID_DI-PSSS-81656B.pdf | ||
| DID_DI-ADMN-81250B.pdf | ||
| DID_DI-MGMT-80555A.pdf | ||
| SPI_1089.pdf | ||
| SPI_5488.pdf | ||
| DID_DI-PSSS-81534A.pdf | ||
| CAVAF.pdf | ||
| DID_DI-MGMT-80441C.pdf | ||
| B-2_PWS_v4_1_FINAL.pdf | ||
| DID_DI-MGMT-80969.pdf | ||
| SGFP.pdf | ||
| DID_DI-MGMT-81178.pdf | ||
| DID_DI-QCIC-80798C.pdf | ||
| FA811820R0009 (Updated).pdf | ||
| DID_DI-MGMT-81255.pdf | ||
| Wage_Determination.pdf | ||
| DID_DI-ADMN-81249B.pdf | ||
| DID_DI-MGMT-80503.pdf | ||
| DID_DI-MGMT-81838.pdf | ||
| TRNSPDATA_REPORT.pdf | ||
| PKGRQMT_REPORT.pdf | ||
| CDRL_CAV_Reporting.pdf | ||
| DID_DI-PSSS-81995.pdf |
Show all 27
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Text version
DATA ITEM DESCRIPTION
Title: FAILURE SUMMARY & ANALYSIS REPORT
Number: DI-SESS-80255A Approval Date: 20141219 AMSC Number: 9506 Limitation: No DTIC Applicable: Yes GIDEP Applicable: Yes http://www.dtic.mil/dtic/submit http://www.gidep.org/data/submit.htm Preparing Activity: AS Applicable Forms: N/A
Use/relationship:
This report presents a summary of the individual failures that occur prior to and during the reporting period and describes the analysis and corrective actions performed. This report is used to evaluate the contractor’s failure reporting, analysis, and corrective action efforts in accordance with the solicitation. This Data Item Description (DID) contains the format, intended use information, and content preparation instructions for the data product generated by the specific and discrete task described in the solicitation, and should be tailored appropriately.
This DID supersedes DI-RELI-80255.
Requirements:
1. Format. The Failure Summary and Analysis Report shall be in contractor’s format.
2. Content. The report shall summarize the results of the contractor’s Failure Reporting, Analysis, and Corrective Action System (FRACAS) implementation required by the statement of work, and shall include a cumulative tabulation of failure data. Failures which occurred during the latest report period shall be identified by suitable notation. The report shall include the following elements at a minimum:
1. Failure number
2. Failure analysis number
3. Failure date
4. Name of engineer responsible for failure analysis
5. Failed part name
6. Failed part number (e.g. national stock number (NSN), logistics control number, work unit code)
7. Manufacturer of failed part
8. Subassembly name and number
9. Major assembly name and number
10. Equipment name and serial number
11. Failed part’s accumulated test or field operational life data
12. Test or mission being performed when the failure occurred
13. Test or mission mode of operation and environmental and use conditions when the failure occurred
Source: http://assist.dla.mil -- Downloaded: 2019-02-04T20:20Z Check the source to verify that this is the current version before use.
http://www.dtic.mil/dtic/submit http://www.gidep.org/data/submit.htm
DI-SESS-80255A
14. Failure symptoms and description of detection or diagnosis methods (e.g. Built In Test)
15. Failure effects (e.g. none, degradation, abort)
16. Repair action (e.g. remove/replace)
17. Failure mode description
18. Description of engineering analysis method employed in failure analysis
19. Failure mechanism/cause of failure
20. Contributing factors, including multiple factor interactions, or secondary effects of the failure
21. Categorization of failure (e.g. equipment design, equipment manufacturing workmanship, part design, part manufacturing workmanship software errors, unverified, intermittent, non-relevant)
22. Information on previous corrective actions for the same part and/or failure mode
23. Corrective action required to mitigate the failure mode, including:
i. Identification of the failure mode
ii. The recommended process or process control changes, when the failure cause is due to workmanship defects
iii. Proposals for retrofit of all equipment already delivered or assembled, including recommended effectivity, in accordance with the contract
iv. Disposition of all defective material and material rendered obsolete because of any necessary redesign, to assure their exclusion from production items
v. Identification of previous functional and environmental qualification tests, if any, invalidated by the corrective action changes and recommendation of those tests that should be repeated, in accordance with the terms of the contract, to demonstrate the corrective action’s effectiveness
vi. Effect on operational and diagnostic software programs and plan for changes, if necessary
24. Corrective action status
25. The recommended fix effectiveness factor (FEF) to be applied to the failure mode based on the proposed corrective action
26. Rationale for any open failure analyses past the contract-specified closeout time
27. Severity criticality ranking of the failure modes. The severity classification categories are:
i. Category I - Catastrophic - A failure which may cause death or system loss (i.e., aircraft, tank, missile, ship)
ii. Category II - Critical - A failure which may cause severe injury, major property damage, or major system damage resulting in mission loss.
iii. Category III - Marginal - A failure which may cause minor injury, minor property damage, or minor system damage which will result in delay or loss of availability or mission degradation.
iv. Category IV - Minor - A failure not serious enough to cause injury, property, or system damage, but which results in unscheduled maintenance or repair.
End of DI-SESS-80255A.
Source: http://assist.dla.mil -- Downloaded: 2019-02-04T20:20Z Check the source to verify that this is the current version before use.
File details come from the government source that posted it. Updated .