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
Issued by
Department of the Air Force Materiel Command Air Force Sustainment Center

About this file

This notice provides details for a federal contract opportunity to overhaul B-2 flight control actuators. The United States Air Force through the Air Force Sustainment Center is seeking to award a firm fixed price, indefinite delivery requirements contract for a one-year base period and two one-year options to overhaul seven different part numbers for B-2 aircraft flight control actuators. The contractor shall provide all labor, facilities, equipment and materials to overhaul the actuators on a monthly delivery schedule of up to six units. The pre-solicitation anticipates release of solicitation FA8118-20-R-0009 on December 31, 2019 with responses due January 30, 2020 and award by September 26, 2020. Qualification is required and incumbent Moog, Inc. is the only approved source. The technical data and orders listed provide requirements for overhaul, repair, testing and quality assurance of the flight control actuators.

View the file

Other files for this federal contract opportunity

Other files attached to Overhaul of B-2 Flight Control Actuators, newest first.
File Type Posted
SPI_5488.pdf PDF
Wage_Determination_Oklahoma.pdf PDF
B-2_PWS_v4_1_FINAL.pdf PDF
SGFP.pdf PDF
Wage_Determination_NewYork.pdf PDF
SPI_1089.pdf PDF
PKGRQMT_REPORT.pdf PDF
DID_DI-MGMT-81178.pdf PDF
FA811820R0009 (Updated).pdf PDF
2904059_CDRL1_REPORT.pdf PDF
TRNSPDATA_REPORT.pdf PDF
DID_DI-PSSS-81656B.pdf PDF
DID_DI-MGMT-80503.pdf PDF
DID_DI-ADMN-81249B.pdf PDF
DID_DI-ADMN-81250B.pdf PDF
DID_DI-MGMT-81255.pdf PDF
CAVAF.pdf PDF
DID_DI-PSSS-81534A.pdf PDF
DID_DI-MGMT-80969.pdf PDF
DID_DI-MGMT-80555A.pdf PDF
DID_DI-MGMT-80441C.pdf PDF
DID_DI-QCIC-80798C.pdf PDF
DID_DI-PSSS-81995.pdf PDF
Show all 23

On GovTribe

Work with this file on GovTribe

  • Download the original file
  • Contacts named in this file
  • Similar government files
  • Ask GovTribe AI about this file

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 .