Attachment 0009_M and O Critical Characteristics.pdf

PDF 30 KB Posted

Attached to
Solicitation for the Overhaul of the Rotor, Turbine Aircraft
Solicitation number
W58RGZ-20-R-0074
Issued by

About this file

Written by GovTribe AI ·

This document contains details for a solicitation seeking the overhaul of rotor turbines for aircraft. The Army Materiel Command Contracting Command at Redstone Arsenal is soliciting offers for a five-year indefinite delivery indefinite quantity contract to overhaul a minimum of five and maximum of 414 rotor turbines per year. The rotor turbines have national stock numbers 2840-01-515-3538 and part number 3048T90G01. Offerors must be approved sources according to defense regulations for overhauling this critical safety item. The only currently approved source is GE Engine Services, LLC with CAGE code 99207. Proposals are due by the estimated closing date in accordance with Federal Acquisition Regulation clause 52.215-1. Award will be contingent upon available funding.

View the file

Other files

File Type Posted
Attachment 0011_MEO_B3301.pdf PDF
Exhibit F_CDRL A006_Technical Report - Study and Services-Process Plan_2016CT315_02Dec19.pdf PDF
Attachment 0019_MEO_P7029.pdf PDF
Attachment 0014_MEO_B3413.pdf PDF
Attachment 0007_DD Form 1348-1A Template.pdf PDF
Exhibit E_CDRL A005_CDM Production Report_2016CT315_02Dec19.pdf PDF
Exhibit B_CDRL A002_Report of Shipping and Packaging Discrepancy_2016CT315_02Dec19.pdf PDF
Attachment 0013_MEO_B3390A.pdf PDF
Exhibit A_CDRL A001_TAMMS-A_2016CT315_02Dec19.pdf PDF
Attachment 0005_M and O Plan Guidance.pdf PDF
Attachment 0002_Document Summary List_2016CT315_02Dec19.pdf PDF
Attachment 0012_MEO_B3315.pdf PDF
Attachment 0016_MEO_P7003.pdf PDF
Attachment 0018_MEO_P7028.pdf PDF
Attachment 0017_MEO_P7009.pdf PDF
W58RGZ20R0074_15Jul20.pdf PDF
Attachment 0008_HQAMC-Level Protest Procedures.pdf PDF
Attachment 0010_MEO_B3182.pdf PDF
Exhibit D_CDRL A004_Technical Report - Study and Services-DD Form 1348-1_2016CT315_02Dec19.pdf PDF
Exhibit C_CDRL A003_Quality Deficiency Report_2016CT315_02Dec19.pdf PDF
Attachment 0021_ROD Guidance.pdf PDF
Attachment 0004_Depot Maintenance Production Report Template.xlsx XLSX spreadsheet
Attachment 0001_M and O Packaging Requirements_2016CT315_02Dec19.pdf PDF
Attachment 0020_MEO_P7081.pdf PDF
Attachment 0003_SF 364 (ROD Template).pdf PDF
Attachment 0006 - Form 1379.pdf PDF
Attachment 0015_MEO_B3414.pdf PDF
Show all 27

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.

12/02/2019

3048T90G01 2840 01 515 - 3538

Y

Y

N

N

Y

Y

Assembly contains CSI subcomponents

Visual Inspection Verification that all cooling air passages are clear after machining

24113 GE Engine Services Inc DBA GE

CAGE

Critical CharacteristicsM ID

Part No NSN

Matched Assy, H Pres TurbineNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved M&O Sources

11/03/2005CSI Date

Approved Date

M&O CRITICAL SAFETY ITEMS

3056T17P09 2840 01 509 - 0348

Y

Y

N

N

N

N

N

N

Y

Dovetail Contour per drawing Note 2

FPI per drawing note 6

No Cracks beyond DMWR Limits via White Light Inspection

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Stage 1 Turbine Rotor BladeNoun YCritical Safety

NSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

11/03/2005CSI Date

3056T17P11 2840 01 509 - 0348

Y

Y

N

N

N

N

N

N

Y

Dovetail Contours per Drawing 3056T17P11, Note 3

FPI per Drawing 3056T17P11, Note 6

No Cracks beyond DMWR Limits via White Light Inspection

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Stage 1 Turbine Rotor BladeNoun YCritical Safety

NSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

07/01/2014CSI Date

3056T94P02 2840 01 509 - 0325

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Stage 1 ShroudNoun NCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

4106T80P01 2840 01 509 - 0315

N

Y

Y

N

N

N

Y

N

N

Absence of cracks via FPI per DMWR Requirements

Bolt hole dimensions per drawing (Sheet 2, Zones A4, A5 and A6)

FPI per drawing

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Stage 2, Fwd Cooling PlateNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

11/03/2005CSI Date

5066T16G25 2840 01 509 - 0308

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Segment Assy, Stage 2 NozzleNoun NCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

6058T99G07 2840 01 509 - 0321

Y

Y

N

N

N

N

N

N

Y

Dovetail Contour per drawing Note 5

FPI per Drawing Note 20

No Cracks beyond DMWR Limits via White Light Inspection

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Stage 2 BladeNoun YCritical Safety

NSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

11/03/2005CSI Date

6064T06P01 2840 01 305 - 2446

N

N

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

Y

Y

N

N

N

N

Absence of cracks with eddy current inspection

Absence of cracks, per DMWR limits, with FPI

Bore/rim diameter

Fluorescent penetrant inspection per drawing note 3

Hardness

Non-conventional machining material removal, no recast layer, no intergranular attack as required, per notes 5 and 11 Ultrasonic Inspection of raw material forging

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Disc, TurbineNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

08/29/1991CSI Date

6064T06P03 2840 01 461 - 3433

N

N

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

Y

Y

N

N

N

N

Absence of cracks with eddy current inspection

Absence of cracks, per DMWR limits, with FPI

Bore/rim diameter

Fluorescent penetrant inspection per drawing note 3

Hardness on raw material forging drwg (see zone A11 of drwg for forging)

Non-conventional machining material removal, no recast layer, no intergranular attack as required, per notes 5 and 11 Ultrasonic Inspection of raw material forging (see zone A11 for forging drwg)

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Disc, TurbineNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

10/25/1999CSI Date

6064T07P06 2840 01 509 - 0304

N

Y

N

N

Y

N

Absence of cracks via FPI per DMWR Requirements

Absence of cracks with FPI

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Stage 2, Aft Cooling PlateNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

11/03/2005CSI Date

6064T08P01 2840 01 299 - 2236

Y

Y

Y

N

N

N

Y

N

N

Absence of cracks with FPI

Air hole diameter 0.032/0.037

Flange radius fillet .050/.060 (zone D12)

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Plate, Cooling, FwdNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

07/18/1996CSI Date

6064T08P03 2840 01 526 - 4971

N

Y

Y

Y

Y

N

N

N

N

N

Y

N

N

N

N

Absence of cracks via FPI per DMWR requirements

Air Hole diameter all within 0.032 to 0.037 except up to three airholes may exceed 0.037 by 0.002

Bolt hole diameter 0.540 to 0.550

Flange Radius fillet 0.050/0.060 (zone D12)

Radius 0.040 to 0.050 (View W, Zone D14)

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Stage 1 Fwd Cooling PlateNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

12/01/2005CSI Date

6064T09P01 2840 01 314 - 6657

N

Y

Y

N

N

N

Y

N

N

Absence of cracks via FPI per DMWR requirements

Absence of cracks with FPI

Scallop radius 0.26/0.24 (10 places)

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Plate, Cooling, AftNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

07/18/1996CSI Date

6064T12P01 2840 01 306 - 1800

N

Y

N

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

Y

Y

N

N

N

Absence of cracks via FPI per DMWR Requirements

Absence of cracks with FPI

Absence of cracks with eddy current inspection

Bore/rim diameter

Hardness

Non-conventional machining material removal, no recast layer, no intergranular attack as required, per notes 5 and 11 Ultrasonic Inspection of raw material forging

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Turbine Disc, Stage 2Noun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

10/07/1993CSI Date

6064T12P03 2840 01 460 - 3583

Y

N

Y

Y

Y

N

N

N

N

N

Y

Y

Y

N

N

Absence of cracks with FPI

Absence of cracks with eddy current inspection

Bore and Rim Diameters

Non-conventional machining/material removal, no recast layer and no intergranular attack (drawing notes 5 and 11) Ultrasonic Inspection of raw material forging

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Turbine Disc, Stage 2Noun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

06/16/1999CSI Date

6064T94P01 2840 01 280 - 9860

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Shroud Segment, TurbineNoun NCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

6068T26G14 2840 01 527 - 9917

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Hanger, Stage 1 ShroudNoun NCritical Safety

NSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

6068T35G15 2840 01 509 - 0327

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Support, Stg 1&2 Turbine ShdNoun NCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

6068T40G03 5330 01 506 - 0258

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Seal, Stage 2 Turbine NozzleNoun NCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

6068T57G22 -

Y

Y

N

N

Y

Y

Assembly contains CSIs. See turbine disks, blades, dampers, and cooling plates for CCs

Installation of Dampers

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

GGT Rotor AssyNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

11/03/2005CSI Date

6080T32P21 2840 01 509 - 0326

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Damper, Stage 1 BladeNoun NCritical Safety

NSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

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