Attachment 0003 - Critical Characteristics.pdf

162 KB Posted

Attached to
Head, Rotary Wing for the Apache AH-64
Solicitation number
W58RGZ-25-B-0014
Issued by

About this file

Written by GovTribe AI ·

This document is an Army Aviation Critical Item Management (CIM) Subcomponent Report for a Head Assembly (Part Number 7-311411003-625) used in a Rotary Wing Aircraft, specifically the Apache AH-64. The report details multiple subcomponents including bearings, links, pins, hubs, and housings, all of which are tracked and have specific critical characteristics related to manufacturing, heat treatment, surface finish, hardness, and inspection requirements.

The report identifies The Boeing Company as the primary source for most components, with additional sources including Professional Aircraft Accessories Inc, AAR Aircraft Component Services-New York, and PCX Aerostructures. The assembly requires engineering tests, fatigue testing, and specific quality control measures, with a verification date of 05/08/2004 and a report generation date of 04/15/2025. The Head Assembly is classified as a tracked, critical safety item (CSI) with multiple manufacturing and installation critical characteristics that must be carefully monitored throughout its lifecycle.

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Other files

File Type Posted
W58RGZ25B0014-0003.pdf PDF
Attachment 0012 - QE-STD-2_81996__D.pdf PDF
W58RGZ25B0014-0002.pdf PDF
Attachment 0011 - QE-STD-1_81996__F.pdf PDF
Attachment 0010 - Technical Data Package List (TDPL).pdf PDF
Attachment 0002 - Document Summary List (DSL).pdf PDF
W58RGZ25B0014-0001.pdf PDF
W58RGZ25B0014.pdf PDF
Attachment 0008 - GFP.xlsx XLSX spreadsheet
Attachment 0007 - AMC AUP for TAV-C.pdf PDF
Exhibit E - CDRL A005_Cost and Hour RPT (FlexFile).pdf PDF
Exhibit B - CDRL A002_ROD.pdf PDF
Attachment 0006 - Contractor Overhaul TAV-C Requirements and TAV-C Portal User Access.pdf PDF
Exhibit D - CDRL A004_Logistics Product Data.pdf PDF
Exhibit A - CDRL A001_GP Inventory Report.pdf PDF
Exhibit F - CDRL A006_Maint Repair Parts Data RPT.pdf PDF
Exhibit C - CDRL A003_MO Process Plan.pdf PDF
Attachment 0001 - MO Packaging Requirements.pdf PDF
Attachment 0004 - DD2794 CSDR.xls XLS spreadsheet
Attachment 0003 - MO CSI.pdf PDF
Attachment 0002 - Document Summary List (DSL).pdf PDF
Attachment 0005 - DD2794 Sustainment CSDR Standard Plan 23-B-0037.cplan.XML_Finalized.pdf PDF
Attachment 0009 - AH-64 Head Rotary Wing Pricing Template.xlsx XLSX spreadsheet
Show all 23

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7-311411003-625Part Number:

Army Aviation CIM Subcomponent Report Date: 04-15-2025

7-114110011 (subcomponent of 7-311411003-625)

Part Details:

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-114110011 3110 011797335 Bearing, Roller, Tapered N Y Yes Tracked 08/02/2011 N N N

Critical Characteristic: No Data Available

Current Sources:

Source Cage

Source Corporation MFG Cage

MFG Corporation Tested Add Date

Remove Date

Reason Code

T8V613 The Boeing Company

Page: 1/48

Testing Requirements:

Engineering Test (NST) Fatigue Endurance Interchange Other

Y Y N N Check Drawing

Page: 2/48

7-211411089-3 (subcomponent of 7-311411003-625)

Part Details:

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-211411089-3 5340 016721981 Pin, Link Attach, M/R Y Y Yes Not Tracked 05/08/2004 Y Y N

Critical Characteristic: (Manufacture / Depot/ Installation) Critical)

M D I Description

N Y N Visual inspection for heat oxidation (discoloration)

Y N N Heat treat and Age per AMS5844

Current Sources: CAGE: 8V613 Company: The Boeing Company

Testing Requirements:

Engineering Test (NST) Fatigue Endurance Interchange Other

Page: 3/48

7-211411155-29 (subcomponent of 7-311411003-625)

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-211411155-29 3040 014338522 Link, Lead Lag Y Y Yes Not Tracked 07/13/2010 Y Y N

Critical Characteristic: (Manufacture / Depot/ Installation) Critical)

M D I Description

Y Y N Shot peening

Current Sources:

Source Cage

Source Corporation MFG Cage

MFG Corporation Tested Add Date

Remove Date

Reason Code

8V613 The Boeing Company T

Testing Requirements:

Engineering Test (NST) Fatigue Endurance Interchange Other

N N N N N

Page: 5/48

7-211411155-31 (subcomponent of 7-311411003-625)

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-211411155-31 3040 014338523 Link Assy, Lead Lag Y Y Yes Not Tracked 07/13/2010 Y Y N

Critical Characteristic: (Manufacture / Depot/ Installation) Critical)

M D I Description

Y Y N Shot peening

Current Sources:

Source Cage

Source Corporation MFG Cage

MFG Corporation Tested Add Date

Remove Date

Reason Code

8V613 The Boeing Company

Testing Requirements:

Engineering Test (NST) Fatigue Endurance Interchange Other

Page: 7/48

7-211411186-5 (subcomponent of 7-311411003-625)

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-211411186-5 3120 011705299 Bearing, Plain, Rod End N Y Yes Tracked 04/07/2009 N N N

Critical Characteristic: No Data Available

Current Sources:

Source Cage

Source Corporation MFG Cage

MFG Corporation Tested Add Date

Remove Date

Reason Code

09455 RBC Transport Dynamics Corporation

8V613 The Boeing Company T

8V613 The Boeing Company T

8V613 The Boeing Company T

8V613 The Boeing Company T

97613 Sargent Aerospace & Defense, LLC

T

Testing Requirements:

Engineering Test (NST) Fatigue Endurance Interchange Other

Page: 9/48

7-211411199-3 (subcomponent of 7-311411003-625)

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-211411199-3 1615 011634514 Pin Assy, Link Attach Y Y Yes Tracked 05/08/2004 Y Y N

Critical Characteristic: (Manufacture / Depot/ Installation) Critical)

M D I Description

Y Y N Assembly contains CSI. See P/N 7-211411089-3 for CCs.

Current Sources:

Source Cage

Source Corporation MFG Cage

MFG Corporation Tested Add Date

Remove Date

Reason Code

8V613 The Boeing Company T

Testing Requirements:

Engineering Test (NST) Fatigue Endurance Interchange Other

Page: 11/48

7-311411009-3 (subcomponent of 7-311411003-625)

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-311411009-3 1615 014338517 Hub, M/R Y Y Yes Not Tracked Y N N

Critical Characteristic: (Manufacture / Depot/ Installation) Critical)

M D I Description

Y N N Heat treat

Current Sources:

Source Cage

Source Corporation MFG Cage

MFG Corporation Tested Add Date

Remove Date

Reason Code

8V613 The Boeing Company 8V613

Testing Requirements:

Engineering Test (NST) Fatigue Endurance Interchange Other

Page: 13/48

7-311411009-5 (subcomponent of 7-311411003-625)

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-311411009-5 1615 014335594 Hub, M/R Y Y Yes Not Tracked 07/24/2006 Y Y N

Critical Characteristic: (Manufacture / Depot/ Installation) Critical)

M D I Description

Y N N Heat treat

Y N N Conductivity

Y N N Hardness

N Y N Visual inspection for heat oxidation (discoloration)

Current Sources: CAGE: 8V613 Company: The Boeing Company

Testing Requirements:

Engineering Test (NST) Fatigue Endurance Interchange Other

Page: 15/48

7-311411015-5 (subcomponent of 7-311411003-625)

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-311411015-5 1615 013234381 Hub Sub-Assy, M/R Y Y Yes Tracked 05/13/1997 Y Y N

Critical Characteristic: (Manufacture / Depot/ Installation) Critical)

M D I Description

Y Y N Assembly contains Critical Safety Items

N Y N Visual inspection for heat oxidation (discoloration)

Current Sources:

Source Cage

Source Corporation MFG Cage

MFG Corporation Tested Add Date

Remove Date

Reason Code

8V613 The Boeing Company T

8V613 The Boeing Company T

Testing Requirements:

Engineering Test (NST) Fatigue Endurance Interchange Other

Page: 17/48

7-311411015-7 (subcomponent of 7-311411003-625)

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-311411015-7 1615 013234381 Hub Sub-Assy, M/R Y Y Yes Tracked 09/10/2019 Y Y N

Critical Characteristic: (Manufacture / Depot/ Installation) Critical)

M D I Description

Y Y N Assembly contains Critical Safety Items

N Y N Visual inspection for heat oxidation (discoloration)

Current Sources:

Source Cage

Source Corporation MFG Cage

MFG Corporation Tested Add Date

Remove Date

Reason Code

8V613 The Boeing Company T

Testing Requirements:

Engineering Test (NST) Fatigue Endurance Interchange Other

Page: 19/48

7-311411045-3 (subcomponent of 7-311411003-625)

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-311411045-3 5307 011634676 Stud, Plain Y Y Yes Tracked 05/08/2004 Y Y N

Critical Characteristic: (Manufacture / Depot/ Installation) Critical)

M D I Description

Y N N Verify hardness of 45 HRC per notes 17 and 18 of the parts list.

Y N N Heat treat per note 16 of the parts list.

N Y N Visual inspection for heat oxidation (discoloration)

Current Sources:

Source Cage

Source Corporation MFG Cage

MFG Corporation Tested Add Date

Remove Date

Reason Code

8V613 The Boeing Company T

Testing Requirements:

Engineering Test (NST) Fatigue Endurance Interchange Other

Page: 21/48

7-311411080-7 (subcomponent of 7-311411003-625)

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-311411080-7 1615 011643848 Plate Assy, Lwr, Hub, M/R Y Y Yes Tracked 09/10/2019 Y Y N

Critical Characteristic: (Manufacture / Depot/ Installation) Critical)

M D I Description

Y N N Hardness

Y N N Heat treat

Y Y N Assembly contains CSI

Current Sources:

Source Cage

Source Corporation MFG Cage

MFG Corporation Tested Add Date

Remove Date

Reason Code

8V613 The Boeing Company T

Testing Requirements:

Engineering Test (NST) Fatigue Endurance Interchange Other

Page: 23/48

7-311411080-9 (subcomponent of 7-311411003-625)

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-311411080-9 1560 014335599 Plate, Lwr, Hub, M/R Y Y Yes Not Tracked 10/03/2017 Y Y N

Critical Characteristic: (Manufacture / Depot/ Installation) Critical)

M D I Description

Y N N Hardness (Notes 22, 23 & 24)

N Y N Visual inspection for heat oxidation (discoloration)

Y Y N Magnetic particle inspection

Y N N Heat treat

Current Sources: CAGE: 8V613 Company: The Boeing Company

Testing Requirements:

Engineering Test (NST) Fatigue Endurance Interchange Other

Page: 25/48

7-311411088-9 (subcomponent of 7-311411003-625)

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-311411088-9 1615 012459826 Shoe Assy, Lower, M/R Y Y Yes Tracked 09/10/2019 Y Y N

Critical Characteristic: (Manufacture / Depot/ Installation) Critical)

M D I Description

Y N N Hardness (forging)

Y N N Heat treat and conductivity (forging)

N Y N Visual inspection for heat oxidation (discoloration)

Current Sources:

Source Cage

Source Corporation MFG Cage

MFG Corporation Tested Add Date

Remove Date

Reason Code

8V613 The Boeing Company T

Testing Requirements:

Engineering Test (NST) Fatigue Endurance Interchange Other

Page: 27/48

7-311411096-3 (subcomponent of 7-311411003-625)

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-311411096-3 1615 011643847 Load Plate, Upper, Hub, M/R

Y Y Yes Tracked 09/10/2019 Y Y N

Critical Characteristic: (Manufacture / Depot/ Installation) Critical)

M D I Description

Y N N Heat treat

Y N N Hardness

Y Y N Magnetic particle inspection

N Y N Visual inspection for heat oxidation (discoloration)

Current Sources:

Source Cage

Source Corporation MFG Cage

MFG Corporation Tested Add Date

Remove Date

Reason Code

8V613 The Boeing Company T

Testing Requirements:

Engineering Test (NST) Fatigue Endurance Interchange Other

Page: 29/48

7-311411110 (subcomponent of 7-311411003-625)

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-311411110 1615 012198658 Damper Assy, Lead Lag N Y Yes Tracked 06/17/2002 N N N

Critical Characteristic: No Data Available

Current Sources:

Source Cage

Source Corporation MFG Cage

MFG Corporation Tested Add Date

Remove Date

Reason Code

8V613 The Boeing Company T

Testing Requirements:

Engineering Test (NST) Fatigue Endurance Interchange Other

Page: 31/48

7-311411155-11 (subcomponent of 7-311411003-625)

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-311411155-11 3040 013521531 Link Assy, Lead Lag Y Y Yes Tracked 06/08/2018 Y Y N

Critical Characteristic: (Manufacture / Depot/ Installation) Critical)

M D I Description

Y Y N Assembly contains Critical Safety Items

Current Sources:

Source Cage

Source Corporation MFG Cage

MFG Corporation Tested Add Date

Remove Date

Reason Code

8V613 The Boeing Company T

Testing Requirements:

Engineering Test (NST) Fatigue Endurance Interchange Other

Page: 33/48

7-311411155-9 (subcomponent of 7-311411003-625)

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-311411155-9 3040 014328240 Link Assy, Lead Lag Y Y Yes Tracked 07/29/2010 Y Y N

Critical Characteristic: (Manufacture / Depot/ Installation) Critical)

M D I Description

Y Y N Assembly contains Critical Safety Items

Current Sources: CAGE: 8V613 Company: The Boeing Company

Testing Requirements:

Engineering Test (NST) Fatigue Endurance Interchange Other

Page: 35/48

7-311411164-7 (subcomponent of 7-311411003-625)

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-311411164-7 3120 015099129 Bearing, Lead Lag Link Y Y No Not Tracked 04/30/2024 Y Y N

Critical Characteristic: (Manufacture / Depot/ Installation) Critical)

M D I Description

Y N N Fluorescent penetrant inspection per HP6-13

Y Y N Shot Peen as noted per HP4-36, 200% coverage, intensity .006-.010A, Shot size S230-S330.

Y Y N Surface finish should be RMS 32 on I.D. (1.5025 - 1.5015) of the stem to be kept as the final minimum acceptable surface finish after all operations.

Y N N Surface finish should be RMS 16 on O.D. (2.4980-2.4965) of, the stem to be kept as the final minimum acceptable surface, finish after all operations.

N Y N Surface finish shall be RMS 20 or less on O.D. (2.4980-, 2.4965) of the stem.

N Y N Eddy Current Inspection IAW TM 1-1520-264-23

Current Sources:

Source Cage

Source Corporation MFG Cage

MFG Corporation Tested Add Date

Remove Date

Reason Code

8V613 The Boeing Company

Testing Requirements:

Engineering Test (NST) Fatigue Endurance Interchange Other

Page: 37/48

7-311411187 (subcomponent of 7-311411003-625)

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-311411187 1615 011705243 Trunnion, Damper M/R N Y Yes Tracked 08/12/2011 N N N

Critical Characteristic: No Data Available

Current Sources:

Source Cage

Source Corporation MFG Cage

MFG Corporation Tested Add Date

Remove Date

Reason Code

09455 RBC Transport Dynamics Corporation

T

50632 Kamatics Corporation (Sub of Kaman Corp)

T

8V613 The Boeing Company T

97613 Sargent Aerospace & Defense, LLC T

Testing Requirements:

Engineering Test (NST) Fatigue Endurance Interchange Other

Page: 39/48

Page: 40/48

7-311411193-15 (subcomponent of 7-311411003-625)

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-311411193-15 3110 012493982 Bearing Assy, Feathering Y Y Yes Tracked 11/18/2008 Y Y N

Critical Characteristic: (Manufacture / Depot/ Installation) Critical)

M D I Description

Y N N Hardness

Y N N Heat treat

Y N N Conductivity

N Y N Visual inspection for heat oxidation (discoloration)

Current Sources:

Source Cage

Source Corporation MFG Cage

MFG Corporation Tested Add Date

Remove Date

Reason Code

30061 Lord Corp Mechanical Products Division

T

76005 Lord Corporation (Aerospace/Mechanical Products Division)

T

Page: 41/48

Page: 42/48

7-311411202-5 (subcomponent of 7-311411003-625)

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-311411202-5 3110 012154794 Bearing, Roller, Tapered Y Y Yes Tracked 11/03/2005 Y Y N

Critical Characteristic: (Manufacture / Depot/ Installation) Critical)

M D I Description

Y N N Heat treat

Y N N Maximum surface roughness (per Parts List note 1G of Revision E)

Y N N Profile of all Rollers shall be inspected (per Parts List note 8 of Revision E)

N Y N Visual inspection for heat oxidation (discoloration)

Y N N Hardness

Y N N Magnetic Particle Inspection

Y N N Nital Etch Inspection

Current Sources:

Source Cage

Source Corporation MFG Cage

MFG Corporation Tested Add Date

Remove Date

Reason Code

32828 Kaydon Corporation T

8V613 The Boeing Company T

Page: 43/48

Y N Y N Check Drawing

Page: 44/48

7-311411215-19 (subcomponent of 7-311411003-625)

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-311411215-19 1615 015075295 Housing Assy, Pitch, M/R Y Y Yes Tracked 05/08/2004 Y Y N

Critical Characteristic: (Manufacture / Depot/ Installation) Critical)

M D I Description

Y N N Hardness & conductivity verification per drwg note 39

Y N N Heat treat

Y Y N Shot peen

N Y N Visual inspection for heat oxidation (discoloration)

Current Sources:

Source Cage

Source Corporation MFG Cage

MFG Corporation Tested Add Date

Remove Date

Reason Code

8V613 The Boeing Company T

Testing Requirements:

Engineering Test (NST) Fatigue Endurance Interchange Other

Page: 45/48

7-611411146-103 (subcomponent of 7-311411003-625)

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification Date M D I

7-611411146-103 1615 016874905 Strap Pack Assy, M/R Y Y Yes Tracked 06/21/2021 Y Y N

Critical Characteristic: (Manufacture / Depot/ Installation) Critical)

M D I Description

Y N N Bolt elongation process as defined on engineering drawing.

Y N N Bolt elongation dimension as defined on engineering drawing.

Y Y N Fixed process control for finishing holes, edges, and surfaces of stainless steel laminates.

Y Y N Assembly contains CSIs.

N Y N Measured ID: 1.515 inch maximum ID measured in 3 locations: 1) 0.5 inches into the bore from the Top.,

2) 0.5 inches into the bore from the Bottom., 3) Center of the Bore from the Top and Bottom.

Current Sources:

Source Cage

Source Corporation MFG Cage

MFG Corporation Tested Add Date

Remove Date

Reason Code

8V613 The Boeing Company T

Testing Requirements:

Engineering Test (NST) Fatigue Endurance Interchange Other

Y Y N N N

Page: 47/48

7-311411003-625Part Number:

Army Aviation CIM Part Report Date:

Part Details:

Part Number FSC NIIN Noun CSI CAI

SN

Required Tracked Status Verification

Date M D I

7-311411003-625 1615 015120889 Head Assy, M/R Y Y Yes Tracked 05/08/2004 Y Y N

Critical Characteristic: (Manufacture / Depot/ Installation)

M D I Description

Y Y N Assy contains CSI. See PN 7-211411199, 7-311411015-7, 7-311411045-3, 7-311411080-7, 7- 311411088-9, 7-311411096-3, 7-311411146-7, 7-311411155-9/-11, 7-311411193-15, 7-311411215-19, 7-311411202-5, 7-311411045-3 for CC.

Testing Requirements:

Engineering Test (NST) Fatigue Endurance Interchange Other PLT Req

Y Y N N Check Drawing N

Maintenance and Overhaul Sources:

Source Cage

Source Corporation MFG Cage

MFG Corporation Add Date Remove Date

Reason Code

08XL0 Professional Aircraft Accessories Inc

3Y015 AAR Aircraft Component Services-New York

82001 PCX Aerostructures, LLC - Newington

8V613 The Boeing Company

Unclassified - For Official Use Only

04-15-2025

Page: 1/1

7-311411003-625_CIMSubcomponentReport_15 April 2025.pdf
7-311411003-625_CIMPartReport_15 April 2025.pdf

File details come from the government source that posted it. Updated .