SOW_Attachment_C_--_Critical_Safety_Item_(CSI)_List.pdf

PDF 106 KB Posted

Attached to
T-38 Wing Acquisition Federal contract opportunity
Solicitation number
FA8208-19-R-0001
Issued by
Department of the Air Force Materiel Command Lifecycle Management Center Hill Air Force Base

About this file

Written by GovTribe AI ·

This document contains a Critical Safety Item list for T-38 wing components. It identifies over 100 part numbers as Critical Safety Items and references their engineering drawings for significant characteristics requirements. The parts include wing spars, ribs, skins, and various structural and flight control components. Compliance with the engineering drawings is required to ensure the structural integrity and safe operation of the aircraft. The federal contract opportunity notice indicates the Air Force is seeking to acquire new T-38 wings and lists an anticipated solicitation number and point of contact. The replacement of aging aircraft wings is important for maintaining military readiness.

From the source

SOW Attachment C Critical Safety Item (CSI) List

View the file

Other files for this federal contract opportunity

Other files attached to T-38 Wing Acquisition, newest first.
File Type Posted
T-38_Wing_RFP_-_Industry_Questions_and_Answers_V4.pdf PDF
EDL_Revision_31_Updated_28Mar2019_T-38_Wing_NSN_1560-01-527-3968XE.pdf PDF
FA820819R0001_Revised_27_March_2019.pdf PDF
Section_L_Revised_27_March_2019.pdf PDF
SOW_Attachment_C_-_Critical_Safety_Item_(CSI)_List_Rev_F.pdf PDF
T-38_Wing_RFP_-_Industry_Questions_and_Answers_V3.pdf PDF
T-38_Wing_RFP_-_Industry_Questions_and_Answers_V2.pdf PDF
Section_L_Attachment_7_Cross_Reference_Table_(v2).pdf PDF
FA820819R0001_Revised_20_Feb_19.pdf PDF
Section_L_Revised_21_Feb_2019.pdf PDF
SOW_Attachment_C_-_Critical_Safety_Item_(CSI)_List_(21_Feb_2019).pdf PDF
Section_L_Attachment_6_-TEP_Pricing_Matrix_Revised_14_Feb_19.xlsx XLSX spreadsheet
Section_L_Attachment_4_Past_Performance_Questionaire_Rev_14_Feb_19.pdf PDF
T-38_Wing_RFP_-_Industry_Questions_and_Answers_V1.pdf PDF
FA820819R0001.pdf PDF
Section_L_Attachment_7_--_Cross_Reference_Table.pdf PDF
Section_L_Attachment_5_--_Past_Performance_Information_Sheet_Supplement.pdf PDF
Source_Qualification_Statement.pdf PDF
SOW_Attachment_D_--_Interchangeability_and_Replaceability_List.pdf PDF
462.pdf PDF
Section_L_Attachment_3_--_Past_Performance_Client_Authorization_Letter.pdf PDF
Section_L.pdf PDF
Packaging.pdf PDF
SOW_Attachment_B_--_CDRL_Distribution_List.pdf PDF
Section_M.pdf PDF
Special_Packaging_Instructions_(SPI).pdf PDF
Section_L_Attachment_2_--_Past_Performance_Consent_Letter.pdf PDF
SOW_Attachment_F_--_Master_Tool_List.pdf PDF
SOW_for_Packaging.pdf PDF
Section_L_Attachment_4_--_Past_Performance_Questionaire.pdf PDF
SOW.pdf PDF
Section_L_Attachment_6_--_TEP_Pricing_Matrix.xlsx XLSX spreadsheet
FA820819R0001.pdf PDF
EDL_Revision_29.pdf PDF
ppi_tool.accdb MDB file
SOW_Attachment_E_--_Analysis_Requirements_for_Non-Conformances_MRB_Process.pdf PDF
Section_L_Attachment_--_1_EZ_Source_Instructions.pdf PDF
SOW_Attachment_A_--_Contract_Data_Requirements_List.pdf PDF
RFP_QAs.pdf PDF
Synopsis_18_Jan_2019.pdf PDF
Show all 40

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
Try for free Login

Text version

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

T38 -33 Wing Finalized CSI LIST

28 April 2010

PN Description Significant Characteristics System

2-23203-509

RIB INSTL, WING TO FUS

ATTACH, LH

See drawing (Rev K) for CSI requirements STRUCTURAL

2-23203-510

RIB INSTL, WING TO FUS

ATTACH, RH

See drawing (Rev K) for CSI requirements STRUCTURAL

2-23204-19

FORGING, RIB, WING TO FUS

ATTACH, LH

See drawing (Rev V) for CSI requirements STRUCTURAL

2-23204-20

FORGING, RIB, WING TO FUS

ATTACH, RH

See drawing (Rev V) for CSI requirements STRUCTURAL

2-23204-21

MACHINED RIB, WING TO FUS

ATTACH, LH

See drawing (Rev V) for CSI requirements STRUCTURAL

2-23204-22

MACHINED RIB, WING TO FUS

ATTACH, RH

See drawing (Rev V) for CSI requirements STRUCTURAL

2-23204-511

RIB ASSY, WING TO FUS

ATTACH, LH

See drawing (Rev V) for CSI requirements STRUCTURAL

2-23204-512

RIB ASSY, WING TO FUS

ATTACH, RH

See drawing (Rev V) for CSI requirements STRUCTURAL

2-23207-517 RIB INSTL, WS 64.8, LH See drawing (Rev R) for CSI requirements STRUCTURAL 2-23207-518 RIB INSTL, WS 64.8, RH See drawing (Rev R) for CSI requirements STRUCTURAL

2-23208-31

RIB, MACHINED, MLG

TRUNNION, W.S. 64.8, LH

See drawing (Rev K) for CSI requirements STRUCTURAL

2-23208-32

RIB, MACHINED, MLG

TRUNNION, W.S. 64.8, RH

See drawing (Rev K) for CSI requirements STRUCTURAL

2-23208-505

RIB ASSY, MLG TRUNNION, WS

64.8 ASSY, LH

See drawing (Rev K) for CSI requirements STRUCTURAL

2-23208-506

RIB ASSY, MLG TRUNNION, WS

64.8 ASSY, RH

See drawing (Rev K) for CSI requirements STRUCTURAL

2-23220-501

RIB INSTL, TIP ATTACH, W.S.

125, LH

See drawing (Rev M) for CSI requirements STRUCTURAL

2-23220-502

RIB INSTL, TIP ATTACH, W.S.

125 RH

See drawing (Rev M) for CSI requirements STRUCTURAL

2-23221-21

RIB, ROUGH FORGING, TIP

ATTACH, W.S. 125, LH

See drawing (Rev N) for CSI requirements STRUCTURAL

2-23221-22

RIB, ROUGH FORGING, TIP

ATTACH, W.S. 125, RH

See drawing (Rev N) for CSI requirements STRUCTURAL

2-23221-23

RIB, MACHINED FITTING, TIP

ATTACH, W.S. 125, LH

See drawing (Rev N) for CSI requirements STRUCTURAL

2-23221-24

RIB, MACHINED FITTING, TIP

ATTACH, W.S. 125, RH

See drawing (Rev N) for CSI requirements STRUCTURAL

2-23221-25

RIB, ASSEMBLY, TIP ATTACH,

W.S. 125, LH

See drawing (Rev N) for CSI requirements STRUCTURAL

2-23221-26

RIB, ASSEMBLY, TIP ATTACH,

W.S. 125, RH

See drawing (Rev N) for CSI requirements STRUCTURAL

2-23229-507

SPAR INSTL, WING CENTER

SECTION, F.S. 330.021

See drawing (Rev M) for CSI requirements STRUCTURAL

2-23230-7

SPAR, WING CENTER SECTION,

F.S. 330.021

See drawing (Rev J) for CSI requirements STRUCTURAL

2-23239-513

SPAR INSTL, WING CENTER

SECTION, F.S. 361.572

Revision R; Note 1 (PS: FH-114); Note 6 STRUCTURAL

2-23240-9

SPAR, WING CENTER SECTION,

F.S. 361.572

See drawing (Rev N) for CSI requirements STRUCTURAL

T-38 (-33) Wing CSI List: Rev F (11 May 2017)

28 April 2010

PN Description Significant Characteristics System

2-23251-513

SPAR INSTL 44%, WING OUTER

PANEL, W.S. 25.231 TO 64.8,

LH

See drawing (Rev P) for CSI requirements STRUCTURAL

2-23251-514

SPAR INSTL 44%, WING OUTER

PANEL, W.S. 25.231 TO 64.8,

RH

See drawing (Rev P) for CSI requirements STRUCTURAL

2-23252-15

SPAR, MACHINED, WING

OUTER PANEL, W.S. 25.231 TO

64.8, LH

See drawing (Rev V) for CSI requirements STRUCTURAL

2-23252-16

SPAR, MACHINED, WING

OUTER PANEL, W.S. 25.231 TO

64.8, RH

See drawing (Rev V) for CSI requirements STRUCTURAL

2-23252-509

SPAR ASSY, WING OUTER

PANEL, W.S. 25.231 TO 64.8,

LH

See drawing (Rev V) for CSI requirements STRUCTURAL

2-23252-510

SPAR ASSY, WING OUTER

PANEL, W.S. 25.231 TO 64.8,

RH

See drawing (Rev V) for CSI requirements STRUCTURAL

2-23263-507

SPAR INSTL 44%, WING OUTER

PANEL, W.S. 64.8 TO 82.368,

LH

See drawing (Rev N) for CSI requirements STRUCTURAL

2-23263-508

SPAR INSTL 44%, WING OUTER

PANEL, W.S. 64.8 TO 82.368,

RH

See drawing (Rev N) for CSI requirements STRUCTURAL

2-23264-13

SPAR ASSY, WING OUTER

PANEL, W.S. 64.8 TO 82.368,

LH

See drawing (Rev J) for CSI requirements STRUCTURAL

2-23264-14

SPAR ASSY, WING OUTER

PANEL, W.S. 64.8 TO 82.368,

RH

See drawing (Rev J) for CSI requirements STRUCTURAL

2-23264-15

SPAR, WING OUTER PANEL,

W.S. 64.8 TO 82.368, LH

See drawing (Rev J) for CSI requirements STRUCTURAL

2-23264-16

SPAR, WING OUTER PANEL,

W.S. 64.8 TO 82.368, RH

See drawing (Rev J) for CSI requirements STRUCTURAL

2-23265-505 SPAR Installation - 44%, WING

OUTER PANEL, W.S. 82.368 TO

101.0, LH

See drawing (Rev J) for CSI requirements STRUCTURAL

2-23265-506 SPAR Installation - 44%, WING

OUTER PANEL, W.S. 82.368 TO

101.0, RH

See drawing (Rev J) for CSI requirements STRUCTURAL

2-23270-503

SPAR INSTL, WING OUTER

PANEL, W.S. 101.0 TO 125.0,

LH

See drawing (Rev J) for CSI requirements STRUCTURAL

2-23270-504

SPAR INSTL, WING OUTER

PANEL, W.S. 101.0 TO 125.0,

RH

See drawing (Rev J) for CSI requirements STRUCTURAL

2-23271-17

SPAR, WING OUTER PANEL,

W.S. 101.0 TO 125.0, LH

See drawing (Rev H) for CSI requirements STRUCTURAL

2-23271-18

SPAR, WING OUTER PANEL,

W.S. 101.0 TO 125.0, RH

See drawing (Rev H) for CSI requirements STRUCTURAL

2-23271-505

SPAR ASSY, WING OUTER

PANEL, W.S. 101.0 TO 125.0,

LH

See drawing (Rev H) for CSI requirements STRUCTURAL

28 April 2010

PN Description Significant Characteristics System

2-23271-506

SPAR ASSY, WING OUTER

PANEL, W.S. 101.0 TO 125.0,

RH

See drawing (Rev H) for CSI requirements STRUCTURAL

2-23296-7

ROUGH FORGING, 15% SPAR,

WING OUTER PANEL, W.S.

29.677 TO 125.0, LH

See drawing (Rev T) for CSI requirements STRUCTURAL

2-23297-15

ROUGH FORGING, SPAR - 66%,

WING OUTER PANEL, W.S. 25.1

TO 125, LH

See drawing (Rev N) for CSI requirements STRUCTURAL

2-23297-16

ROUGH FORGING, SPAR - 66%,

WING OUTER PANEL, W.S. 25.1

TO 125, LH

See drawing (Rev N) for CSI requirements STRUCTURAL

2-23306-5 Rough Forging - RIB-MLG

TRUNNION, W.S. 64.80

Rev D; Note 7, 8, 9, 10; material Hy-tuf steel, spec NAI-1275, STRUCTURAL

2-23311-5

SPAR, FORGING, WING OUTER

PANEL, W.S. 25.231 TO 64.8,

RH

See drawing (Rev L) for CSI requirements STRUCTURAL

2-23316-11

SPAR - 44%, ROUGH FORGING,

WING OUTER PANEL, W.S.

82.368 TO 101.0, LH

See drawing (Rev J) for CSI requirements STRUCTURAL

2-23316-12

SPAR - 44%, ROUGH FORGING,

WING OUTER PANEL, W.S.

82.368 TO 101.0, RH

See drawing (Rev J) for CSI requirements STRUCTURAL

2-23316-13

SPAR - 44% ASSY, WING OUTER

PANEL, W.S. 82.368 TO 101.0,

LH

See drawing (Rev J) for CSI requirements STRUCTURAL

2-23316-14

SPAR - 44% ASSY, WING OUTER

PANEL, W.S. 82.368 TO 101.0,

RH

See drawing (Rev J) for CSI requirements STRUCTURAL

2-74153-10

SUPPORT - AILERON,

MACHINED, OPERATING

MECHANISM, RH

Revision J; Material A356-T6 CSTG AL, MATL SPEC NAI-1296;

Note 7, Note 12, Note 14

FLIGHT CONTROLS

2-74153-11

SUPPORT - AILERON ASSY,

OPERATING MECHANISM, LH

Revision J; Dimensions: Zone 2: .2500, .3750; Zone 4: .312; FLIGHT CONTROLS

2-74153-12

SUPPORT - AILERON ASSY,

OPERATING MECHANISM, RH

Revision J; Dimensions: Zone 2: .2500, .3750; Zone 4: .312; FLIGHT CONTROLS

2-74153-7

SUPPORT - AILERON, ROUGH

CASTING, OPERATING

MECHANISM, LH

Revision J; Material A356-T6 CSTG AL, MATL SPEC NAI-1296;

Note 7, Note 12

FLIGHT CONTROLS

2-74153-8

SUPPORT - AILERON, ROUGH

CASTING, OPERATING

MECHANISM, RH

Revision J; Material A356-T6 CSTG AL, MATL SPEC NAI-1296;

Note 7, Note 12

FLIGHT CONTROLS

2-74153-9

SUPPORT - AILERON,

MACHINED, OPERATING

MECHANISM, LH

Revision J; Material A356-T6 CSTG AL, MATL SPEC NAI-1296;

Note 7, Note 12, Note 14

FLIGHT CONTROLS

28 April 2010

PN Description Significant Characteristics System

2-74154-10

QUADRANT - AILERON, ROUGH

CASTING, OPERATING

MECHANISM, RH

Revision F; Material A356-T6; MATL SPEC NAI-1296; Note 8 FLIGHT CONTROLS

2-74154-11

QUADRANT - AILERON,

MACHINED, OPERATING

MECHANISM, LH

Revision F; Material A356-T6; MATL SPEC NAI-1296; Note 8, Note 18; Dimensions: Zone 4: A .0005, .6243, .6238; Zone 5:

.6265, .6255, .1900; Zone 6: .1900;

FLIGHT CONTROLS

2-74154-12

QUADRANT - AILERON,

MACHINED, OPERATING

MECHANISM, RH

Revision F; Material A356-T6; MATL SPEC NAI-1296; Note 8, Note 18; Dimensions: Zone 4: A .0005, .6243, .6238; Zone 5:

.6265, .6255, .1900; Zone 6: .1900;

FLIGHT CONTROLS

2-74154-9

QUADRANT - AILERON, ROUGH

CASTING, OPERATING

MECHANISM, LH

Revision F; Material A356-T6; MATL SPEC NAI-1296; Note 8 FLIGHT CONTROLS

2-74155-3

LINK - AILERON, OPERATING

MECHANISM

Revision E; Material Plate-AL Alloy 7075-T6; MATL SPEC AMS- QQ-Q-250/12; Note 3

FLIGHT CONTROLS

2-74155-5

STOP, LINK - AILERON,

OPERATING MECHANISM

Revision E; Material Sheet ALCLAD 7075-T6; MATL SPEC AMS-

QQ-Q-250/13;

FLIGHT CONTROLS

2-74155-501

LINK - AILERON ASSY,

OPERATING MECHANISM

Revision E; Dimensions: Zone 3: .6243, .6238, .6243, .6238; FLIGHT CONTROLS

2-74156-7

BEAM - VALVE WALKING,

MACHINED, AILERON

OPERATING MECHANISM

Revision E; MATERIAL: PERM MOLD AL 356-T6; MATL SPEC:

ASTM B108; Note 8, DIMENSION: ZONE 3: .6243, .6238, .9007, .9002, + .0005

FLIGHT CONTROLS

2-74197-1

ROD END - FORWARD SURFACE

FOLLOW UP, AILERON

Revision G; MATERIAL: MAKE FROM RE4S10 OR EQUIV; MATL

SPEC: FAFNIR BRG CO. NEW BRITAIN CONN; DIMENSIONS:

.5130 + .0005; NOTE 2, NOTE 4;

FLIGHT CONTROLS

2-74198-1

ROD END - AFT SURFACE

FOLLOW UP, AILERON

REVISION B; MATL: MAKE FROM RA3M5 OR EQUIV.; MATL

SPEC: FAFNIR BRG CO. NEW BRITAIN, CONN;

FLIGHT CONTROLS

2-74199-1

SLEEVE - SURFACE FOLLOW UP

ROD, AILERON

REVISION E; MATERIAL: BAR-STEEL 4130-F4; MATL SPEC: MIL-S-

6758; Nickel Plate .0005 to .0008 thick all over per AMS 2404.

Solid Film lube .00035 + .00015 thick on O.D. only; Note 4;

FLIGHT CONTROLS

3-23241-507

SPAR INSTL, 15%, WING OUTER

PANEL, W.S. 29.677 TO 125.0,

LH

See drawing (Rev K) for CSI requirements STRUCTURAL

3-23241-508

SPAR INSTL, 15%, WING OUTER

PANEL, W.S. 29.677 TO 125.0,

RH

See drawing (Rev K) for CSI requirements STRUCTURAL

3-23242-11

SPAR, 15%, WING OUTER

PANEL, W.S. 29.677 TO 125.0,

LH

See drawing (Rev L) for CSI requirements STRUCTURAL

3-23242-12

SPAR, 15%, WING OUTER

PANEL, W.S. 29.677 TO 125.0,

RH

See drawing (Rev L) for CSI requirements STRUCTURAL

3-23242-507 15% SPAR (WING) See drawing (Rev L) for CSI requirements STRUCTURAL 3-23242-508 15% SPAR (WING) See drawing (Rev L) for CSI requirements STRUCTURAL

3-23279-509

SPAR INSTL - 66%, WING

OUTER PANEL, W.S. 25.1 TO

125, LH

See drawing (Rev R) for CSI requirements STRUCTURAL

3-23279-510

SPAR INSTL - 66%, WING

OUTER PANEL, W.S. 25.1 TO

125, RH

See drawing (Rev R) for CSI requirements STRUCTURAL

28 April 2010

PN Description Significant Characteristics System

3-23282-7

SPAR - 66%, WING OUTER

PANEL, W.S. 25.1 TO 125, LH

See drawing (Rev P) for CSI requirements STRUCTURAL

3-23282-8

SPAR - 66%, WING OUTER

PANEL, W.S. 25.1 TO 125, RH

See drawing (Rev P) for CSI requirements STRUCTURAL

3-23301-7 SKIN, UPPER MAIN WING See drawing (Rev H) for CSI requirements STRUCTURAL 3-23502-11 SKIN, LOWER MAIN WING See drawing (Rev K) for CSI requirements STRUCTURAL 3-23502-9 SKIN, LOWER MAIN WING See drawing (Rev K) for CSI requirements STRUCTURAL

3-74157-10

ARM, MACHINED, FOLLOW-UP,

AILERON OPERATING

MECHANISM, RH

REVISION C; MATL: AL EXTR. BAR 7075-T73511; MATL SPEC:

AMS-QQ-A-200/11; NOTE 4

FLIGHT CONTROLS

3-74157-7

ARM, ASSY, FOLLOW-UP,

AILERON OPERATING

MECHANISM, LH

REVISION C; NOTE 7; DIMENSIONS: ZONE 3: .7493, .7510,

.2480, .2500;

FLIGHT CONTROLS

3-74157-8

ARM ASSY, MACHINED,

FOLLOW-UP, AILERON

OPERATING MECHANISM, RH

REVISION C; NOTE 7; DIMENSIONS: ZONE 3: .7493, .7510,

.2480, .2500;

FLIGHT CONTROLS

3-74157-9

ARM, MACHINED, FOLLOW-UP,

AILERON OPERATING

MECHANISM, LH

REVISION C; MATL: AL EXTR. BAR 7075-T73511; MATL SPEC:

AMS-QQ-A-200/11; NOTE 4

FLIGHT CONTROLS

51B221-11H BOLT - BRAZIER HEAD

REVISION AG; Note Finish paragraph; See material specs; Note heat treat parameters

FLIGHT CONTROLS

51B221-9H BOLT - BRAZIER HEAD

REVISION AG; Note Finish paragraph; See material specs; Note heat treat parameters

FLIGHT CONTROLS

51B333-10H BOLT - CLOSE TOLERANCE

REVISION V; Note Finish paragraph; See material specs; Note heat treat parameters

FLIGHT CONTROLS

51B333-9H BOLT - CLOSE TOLERANCE

REVISION V; Note Finish paragraph; See material specs; Note heat treat parameters

FLIGHT CONTROLS

51B464-3-11 BOLT - BRAZIER HEAD

REVISION AG; Note Finish paragraph; See material specs; Note heat treat parameters

FLIGHT CONTROLS

51B464-3-13 BOLT - CLOSE TOLERANCE

REVISION AG; Note Finish paragraph; See material specs; Note heat treat parameters

FLIGHT CONTROLS

51B464-3-27 BOLT - CLOSE TOLERANCE

REVISION AG; Note Finish paragraph; See material specs; Note heat treat parameters

FLIGHT CONTROLS

51B464-3A2 BOLT - CLOSE TOLERANCE

REVISION AG; Note Finish paragraph; See material specs; Note heat treat parameters

FLIGHT CONTROLS

51B464-4-15 BOLT - CLOSE TOLERANCE

REVISION AG; Note Finish paragraph; See material specs; Note heat treat parameters

FLIGHT CONTROLS

51B464-4-20 BOLT

REVISION AG; Note Finish paragraph; See material specs; Note heat treat parameters

FLIGHT CONTROLS

51B464-4-22 BOLT - CLOSE TOLERANCE

REVISION AG; Note Finish paragraph; See material specs; Note heat treat parameters

FLIGHT CONTROLS

NAS1303-12 BOLT

Rockwell C, 36.0 min and 40.0 max overall; Material: Steep Comp E4340 or Steel Comp 8740 overall

LANDING GEAR

CSI List for -33 Wing

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