Appendix J - FCP 25 October 2009.xls

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Sustainment, Modification, and Installation Program in support of P-3 Aircraft (all T/M/S)
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N00019-09-R-0216
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Appendix J FCP dtd 25Oct09

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Q A 176 for FedBizOps 9-22-2010.doc DOC document
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Appendix B - SSI-K —
Appendix D - SSI-K —
Attch_(1)_SOW_for_P-3_Aircraft_Sustainment_dtd_09_Sept_2010.doc DOC document
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Appendix L - CWA BOM 09 September 2010.xls XLS spreadsheet
Amendment 0007.pdf PDF
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Appendix U -ALD-9 Reqs 25 October 2009.xls XLS spreadsheet
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Appendix V - P-3 IDP 25 October 2009.pdf PDF
Appendix G - SSI-K Zone 5 BOM 09 June 2010.xls XLS spreadsheet
Appendix E - SSI-K BOM 09 June 2010.xls XLS spreadsheet
Attch —
Appendix C - Zone 5 Drawings 09 June 2010.xls XLS spreadsheet
Appendix R - Misc BOM 16 Mar 2010.xls XLS spreadsheet
Appendix Q - Misc Drawings 09 June 2010.xls XLS spreadsheet
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Appendix H - DIMPLE Ch 2 19 July 2010.pdf PDF
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Appendix M - OW Drawings 09 June 2010.xls XLS spreadsheet
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Appendix K - CWSR Drawings 09 June 2010.xls XLS spreadsheet
Appendix S - P-3 Shoring Guide 25 October 2009.xls XLS spreadsheet
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N00019-09-R-0216-0004.pdf PDF
Q As posted 19 Mar 2010.pdf PDF
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Fatigue Critical Parts

Part NumberNomenclatureTesting Method
OUTER WING
938811-***PANEL - OW LOWER # 1
981811-***PANEL - OW LOWER # 1*FTT
938812-***PANEL - OW LOWER # 2
981812-***PANEL - OW LOWER # 2*FTT
938813-***PANEL - OW LOWER # 3
981813-***PANEL - OW LOWER # 3*FTT
938814-***PANEL - OW LOWER # 4
981814-***PANEL - OW LOWER # 4*FTT
938815-***PANEL - OW LOWER # 5*FTT required for -107/-108
938816-***PANEL - OW LOWER # 6*FTT required for -107/-108
938817-***PANEL - OW LOWER # 7*FTT required for -107/-108
938818-***PANEL - OW LOWER # 8*FTT required for -107/-108
938819-***PANEL - OW LOWER # 9*FTT required for -107/-108
938801-***PANEL - OW UPPER # 1*FTT required for -201/-202
938802-***PANEL - OW UPPER # 2*FTT required for -201/-202
938803-***PANEL - OW UPPER # 3*FTT required for -201/-202
938804-***PANEL - OW UPPER # 4*FTT required for -201/-202
938805-***PANEL - OW UPPER # 5*FTT required for -201/-202
938806-***PANEL - OW UPPER # 6*FTT required for -201/-202
938807-***PANEL - OW UPPER # 7*FTT required for -201/-202
938808-***PANEL - OW UPPER # 8*FTT required for -201/-202
938809-***PANEL - OW UPPER # 9*FTT required for -201/-202
939202-***CAP - OW AFT UPPER
939203-***CAP - OW AFT LOWER
939204-***WEB - OW AFT
938320-***CAP - OW FWD UPPER**Tensile Test
938321-***CAP - OW FWD LOWER
981321-***CAP - OW FWD LOWER**Tensile Test
938322-***WEB - OW FWD
982195-***WEB - OW FWD
939192-***FITTING - OW FWD LWR FWD
939193-***FITTING - OW FWD LWR AFT
939196-***FITTING - OW FWD UPPER FWD
939191-***FITTING - OW FWD UPPER AFT
939194-***FITTING - OW AFT UPPER
939198-***FITTING - OW AFT LWR
939329-***#2 & 3 Nacelle Attach Plate
982121-***#2 & 3 Nacelle Attach Plate
810053-***#2 & 3 Nacelle Attach Plate
982120-***#2 & 3 Nacelle Attach Plate
810052-***#2 & 3 Nacelle Attach Plate
982123-***#2 & 3 Nacelle Attach Plate
810051-***#2 & 3 Nacelle Attach plate
982122-***#2 & 3 Nacelle Attach plate
810055-***#1 & 4 Nacelle Attach Plate
982128-***#1 & 4 Nacelle Attach Plate
810056-***#1 & 4 Nacelle Attach Plate
982129-***#1 & 4 Nacelle Attach Plate
919144-***#1 & 4 Nacelle Attach Plate
919139-***#1 & 4 Nacelle Attach Plate
902529-***RIB - MLG TRUSS, WS 167
SKT-P3-301-00*RIB - MLG TRUSS, WS 167
902530-***RIB - MLG TRUSS, WS 209
606A0102-00*RIB - MLG TRUSS, WS 209
939515-***CAP - BL 65 WING RIB, LOWER
E10-23433-*CAP - BL 65 WING RIB, LOWER**Tensile Test
939516-***PLATE - WING BL65 LOWER SPLICE
CENTER WING
938831-***PANEL - CW UPPER # 1*FTT required for -105
938832-***PANEL - CW UPPER # 2*FTT required for -105
938833-***PANEL - CW UPPER # 3*FTT required for -105
938834-***PANEL - CW UPPER # 4*FTT required for -105
938835-***PANEL - CW UPPER # 5*FTT required for -105
938836-***PANEL - CW UPPER # 6*FTT required for -105
938837-***PANEL - CW UPPER # 7*FTT required for -105
938838-***PANEL - CW UPPER # 8*FTT required for -105
938839-***PANEL - CW UPPER # 9*FTT required for -105
938821-***PANEL - CW LOWER # 1*FTT required for -115
938822-***PANEL - CW LOWER # 2*FTT required for -115
938823-***PANEL - CW LOWER # 3*FTT required for -115
938824-***PANEL - CW LOWER # 4*FTT required for -117
938825-***PANEL - CW LOWER # 5*FTT required for -115
938826-***PANEL - CW LOWER # 6*FTT required for -115
938827-***PANEL - CW LOWER # 7*FTT required for -115
938828-***PANEL - CW LOWER # 8*FTT required for -115
938829-***PANEL - CW LOWER # 9*FTT required for -115
901606-***CAP - CW FWD UPPER
925251-***CAP - CW FWD LOWER**Tensile Test
925498-***WEB - CW FWD
900906-***CAP - CW AFT UPPER
900907-***CAP - CW AFT LOWER
900908-***WEB - CW AFT
939195-***FITTING - CW FWD LWR
939197-***FITTING - CW AFT LWR
901721-***RING FITTING - FORWARD
901722-***RING FITTING - AFT
* The fracture toughness test specimen shall be taken from the parent extrusion and tested in the L-T direction. The L-T direction means that the specimen is loaded in the longitudinal direction and the crack orientation is the transverse direction.
Specimen thickness shall be maximized within the section. Contractor shall perform testing in accordance with the requirements of ASTM E 399. The data obtained from these tests shall be plane strain fracture toughness KIc.
Test results failing to meet the validity requirements of ASTM E 399 shall be interpreted in accordance with the requirements of ASTM B 645. Contractor shall maintain specimen identity throughout specimen fabrication and testing.
** Tensile specimens shall be machined to ASTM E8 and ASTM B 557 from final tempered product with acceptance values per AMS 4293. The data required from these test are tensile strength (Ftu), yield strength at 0.2% offset (Fty), and percent elongation (e%). The Contractor shall maintain specimen identity throughout specimen fabrication and testing.
NOTE -- The parts with a blank under the Testing Method column are not manufactured from 7249 material and do not require any special testing to verify material properties.

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