Attachment_0023_Critical_Characteristics_W58RGZ-19-R-0050.pdf

PDF 458 KB Posted

Attached to
Solicitation for the Overhaul/Repair of the UH-60 Tail Rotor Blade with Pitch Horn Replacement
Solicitation number
W58RGZ-19-R-0050
Issued by

About this file

From the source

Attachment 0023_Critical Characteristics_W58RGZ-19-R-0050.pdf

View the file

Other files

File Type Posted
Solicitation_W58RGZ-19-R-0050.pdf PDF
Exhibit_C_Data_Item_A003_W58RGZ-19-R-0050.pdf PDF
Attachment_0004_MEO_B1576A_W58RGZ-19-R-0050.pdf PDF
Attachment_0019_DD_Form_1348-1A_Example_W58RGZ-19-R-0050.pdf PDF
Attachment_0017_Report_of_Discrepancy_(ROD)_Guidance_W58RGZ-19-R-0050.pdf PDF
Attachment_0013_MEO_B2469_W58RGZ-19-R-0050.pdf PDF
Attachment_0012_MEO_B2142_W58RGZ-19-R-0050.pdf PDF
Attachment_0003_MEO_B1389_W58RGZ-19-R-0050.pdf PDF
Exhibit_B_Data_Item_A002_W58RGZ-19-R-0050.pdf PDF
Attachment_0018_Frozen_Plan_Description_and_Guidance_W58RGZ-19-R-0050.pdf PDF
Attachment_0021_HQAMC-Level_Protest_Procedures_(October_2015)_W58RGZ-19-R-0050.pdf PDF
Attachment_0007_MEO_B1739A_W58RGZ-19-R-0050.pdf PDF
Exhibit_F_Data_Item_A006_W58RGZ-19-R-0050.pdf PDF
Exhibit_D_Data_Item_A004_W58RGZ-19-R-0050.pdf PDF
Attachment_0011_MEO_B2059_W58RGZ-19-R-0050.pdf PDF
Attachment_0014_MEO_B2474_W58RGZ-19-R-0050.pdf PDF
Exhibit_A_Data_Item_A001_W58RGZ-19-R-0050.pdf PDF
Attachment_0016_MEO_T1356D_W58RGZ-19-R-0050.pdf PDF
Attachment_0002_MEO_B1295_W58RGZ-19-R-0050.pdf PDF
Attachment_0008_MEO_B1754A_W58RGZ-19-R-0050.pdf PDF
Attachment_0006_MEO_B1613_W58RGZ-19-R-0050.pdf PDF
Attachment_0005_MEO_B1586_W58RGZ-19-R-0050.pdf PDF
Attachment_0015_MEO_B2481_W58RGZ-19-R-0050.pdf PDF
Attachment_0009_MEO_B1887_W58RGZ-19-R-0050.pdf PDF
Exhibit_E_Data_Item_A005_W58RGZ-19-R-0050.pdf PDF
Attachment_0010_MEO_B2033_W58RGZ-19-R-0050.pdf PDF
Attachment_0022_Packaging_Requirements_W58RGZ-19-R-0050.pdf PDF
Attachment_0024_Document_Summary_List_W58RGZ-19-R-0050.pdf PDF
Attachment_0020_CDM_Production_Report_Sample_W58RGZ-18-R-0067.pdf.xlsx XLSX spreadsheet
Show all 29

On GovTribe

Work with this file

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

Text version

The file's text, extracted by GovTribe without its formatting.

06/07/2017

70101-11201-041 1560 01 432 - 9242

Y NN Inspection acceptance of interlaminar shear strength of each fabricated spar (Note 21)

78286 Sikorsky Aircraft Corp

CAGE

Critical CharacteristicsM ID

Part No NSN

Blade Assy, T/RNoun YCritical Safety

YSerial Number Req'd NEngineering Test Req'd NFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

04/01/1987CSI Date

Approved Date

M&O CRITICAL SAFETY ITEMS

W58RGZ-17-R-0237

Attachment 0023

70101-11201-042 1560 01 432 - 9241

Y NN Inspection acceptance of interlaminar shear strength of each fabricated spar (Note 21)

78286 Sikorsky Aircraft Corp

CAGE

Critical CharacteristicsM ID

Part No NSN

Blade Assy, T/RNoun YCritical Safety

YSerial Number Req'd NEngineering Test Req'd NFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

09/19/1988CSI Date

Approved Date

M&O CRITICAL SAFETY ITEMS

70101-11220-042 1615 01 105 - 8714

N NN

78286 Sikorsky Aircraft Corp

CAGE

Critical CharacteristicsM ID

Part No NSN

Horn Assy, T/RNoun NCritical Safety

NSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

Approved Date

M&O CRITICAL SAFETY ITEMS

70101-31000-043 1615 01 113 - 8188

Y

Y

Y

Y

Y

Y

Assembly contains CSIs

Bond skin assembly along trailing edge tab per note 39. Inspection acceptance of the bond within the final production trim, from R station 15.062 to R station 35.00, to the requirements of the bond control, 70101-11267, para. 10.0, is a CC.

78286 Sikorsky Aircraft Corp

CAGE

Critical CharacteristicsM ID

Part No NSN

Blade Assy, T/RNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved M&O Sources

04/01/1987CSI Date

Approved Date

M&O CRITICAL SAFETY ITEMS

70101-31002-041 -

Y NN Assembly Contains Critical Safety Items P/N 70101-11201-041/042

78286 Sikorsky Aircraft Corp

CAGE

Critical CharacteristicsM ID

Part No NSN

Spar Assy, TR BladeNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

11/09/2015CSI Date

Approved Date

M&O CRITICAL SAFETY ITEMS

70101-31002-042 -

Y NN Assembly Contains Critical Safety Items P/N 70101-11201-041/042

78286 Sikorsky Aircraft Corp

CAGE

Critical CharacteristicsM ID

Part No NSN

SPAR ASSY, TR BLADENoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

Approved Date

M&O CRITICAL SAFETY ITEMS

SB7301-103 1560 01 100 - 1701

N NN

76005

78286

Lord Corporation (Aerospace/Mechanical Products Division)

Sikorsky Aircraft Corp

CAGE

Critical CharacteristicsM ID

Part No NSN

Pivot Assy, T/RNoun NCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

Approved Date

M&O CRITICAL SAFETY ITEMS

File details come from the government source that posted it.