SOW.pdf
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- Solicitation number
- FA853826R0020
About this file
This is a Statement of Work (SOW) for the inspection, overhaul, and repair of C-5 Aft Center Cargo Doors "C" Model, part numbers 4F69010-101A/102A with NSNs 1560-01-296-6316 and 1560-01-297-9975. The SOW was prepared by Samuel Stockton Jr at Warner Robins Air Logistics Complex (WR-ALC) and dated May 12, 2025.
The work scope includes a comprehensive inspection and overhaul process to return the cargo doors to serviceable condition. WR-ALC must conduct detailed visual inspections per Technical Order 1C-5M-3 to identify cracks, corrosion, dents, punctures, loose and missing fasteners, and unauthorized repairs. Honeycomb skin panels must be replaced at 100 percent. Frames and fittings require corrosion inspection and evaluation per TO 1C-5M-23. Repair limitations authorize no more than two repairs and three negligible damages per frame; components exceeding these limits require replacement. The work includes removal and replacement of all perimeter rub strips, rubber seals (part 4F61417-246A), and centerline seals (4F69025-101A) per Lockheed drawings 4F69010 and 4F61419. The doors must undergo paint removal and repainting per TO 1C-5M-23 and USAF Drawing 201211891, followed by application of Corrosion Preventive Compound. A final visual inspection must be completed before items are returned to supply as "A condition" assets with appropriate packaging per Special Packaging Instructions. The point of contact is Samuel Stockton Jr at DSN 497-5131.
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Other files
| File | Type | Posted |
|---|---|---|
| GFP_FA853826R0020.pdf | ||
| CDRL_2600641.pdf | ||
| FA8538-26-R-0020_W_ATTACHMENTS.pdf | ||
| TRNSPDATA_REPORT.pdf | ||
| PKGRQMT_REPORT.pdf |
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Text version
SOW:
Revision: Basic Date: 5-12-2025
Prepared by Samuel Stockton Jr/SCMS/GUEAC/ (478) 497-5131
Statement of Work
C-5 Aft Center Cargo Door “C” Model P/N-4F69010-
101A/102A NSN’s
1560-01-296-6316 1560-01-297-9975
SECTION I: SCOPE
1.1 This SOW will allow for an inspection and overhaul of C-5 Aft Center Cargo Doors
“C” Model, P/N 4F69010-101A/102A and NSN’s 1560-01-296-6316/1560-01-297- 9975 and satisfy existing MICAPs. This SOW was also developed to provide the most updated and accurate engineering data for the purpose of repairing, maintaining and fabricating the Aft Center Cargo Doors.
1.2 The separate NSN’s MUST be overhauled as a single assembly set and must have previously been assembled together on the same aircraft (“A-to-A” assembly).
SECTION II: APPLICABLE DOCUMENTS AND REFERENCE DATA
2.1 The following Technical Orders (T.O.) form a part of this document to the extent specified herein.
2.2 Technical Documents: T.O. 1C-5M-3, Structural Repair Instructions
T.O. 1C-5M-23, Corrosion Control Manual T.O. 33B-1-2, Nondestructive Inspection T.O. 1C-5M-4-1, Illustrated Parts Breakdown
Airframe Group T.O. 1C-5M-4-5, Illustrated Parts Breakdown
Flight Control and Instrument Systems
2.3 JEDMICS drawings: 4F69010, 201211891
SECTION III: WORK REQUIREMENTS
3.1 All work performed under this SOW shall be accomplished in accordance with the information listed in section II above.
3.2 WR-ALC shall have available for fabrication or repair work any applicable and necessary material, parts, and/or equipment listed on the face of drawings for part numbers 4F69010-101A/102A.
3.3 Work performed under this SOW includes all actions necessary to return a reparable item to a serviceable condition that will offer the user a maximum amount of trouble-free service.
3.4 If de-painting is deemed necessary, de-painting according to T.O. 1C-5M-23, Section
2, Paint Removal and Repainting.
3.5 The C-model Aft Center Cargo Doors shall be visually inspected IAW 1C-5M-3 para 1.23.2, Detailed Visual Inspection, for cracks, corrosion, dents, punctures, loose and missing fasteners, and unauthorized or nonconforming repairs.
3.5.1 Do NOT inspect any honeycomb skin panels, as these are all 100% replacement parts.
3.5.2 Inspect all frames and fittings for corrosion IAW TO 1C-5M-23 para 1.7.1.1, Optical Inspection.
3.5.3 Evaluate and repair corrosion damage and corrosion prevention measures including all plating requirements in accordance with Lockheed drawing 4F69010 and T.O. 1C-5M-
23. Remove and replace the honeycomb skin panels at 100%.
3.5.4 Perform a detailed visual inspection (DVI) of the LHS and RHS Lock Installations (4F69200-101A/-103A) IAW 1C-5M-3 para 1.23.2.
3.6 No more than two repairs and no more than three negligible damages on any one frame are authorized, at completion of component repair. Replace individual components that fall outside of these limits. For damage, other than listed above or beyond limits stated herein, contact program office via AFMC Form 202 for disposition.
3.6.1. Damages that fall within repair limitations according to this SOW, Section 3.6, shall be accomplished in accordance with T.O. 1C-5M-3 and T.O. 1C-5M-23.
3.6.2. Provide per Lockheed drawing 4F69010.
3.7 Remove and replace all perimeter rub strips and rubber seals (i.e., 4F61417-246A) and all centerline seals (4F69025-101A) IAW Lockheed Dwgs 4F69010 and 4F61419.
3.8 The C-Model Aft Center Cargo Doors shall be finished in accordance with TO 1C- 5M-23 Sections 2, Paint Removal and Repainting, and USAF Drawings 201211891 and 4F69010-101A/102A, Latest Revisions.
3.9 Following finish system application and full cure, apply Corrosion Preventive Compound (CPC) IAW TO 1C-5M-23 para 1.8.2, Areas for Application of Corrosion Preventive Compound, and 1.8.3, Application of Corrosion Preventive Compound.
3.10 Perform a final visual inspection IAW 1C-5M-3 para 14.8.4, Visual Inspections, of subject item. If no unresolved defects are noted, turn into supply as an A condition asset after packaging per relevant Special Packaging Instructions (SPI).
SECTION V: POINT OF CONTACT
4.0 Point of contact for this SOW is Samuel Stockton Jr, 409 SCMS / GUEA; DSN 497- 5131.
AFLCMC/WLSEBA Approval x______________________
Jonathan R Harrison C-5 Structures Chief x_______________________
| Statement of Work |
| P/N-4F69010-101A/102A |
| NSN’s |
| 1560-01-296-6316 |
| 1560-01-297-9975 |
| SECTION I: SCOPE |
| SECTION II: APPLICABLE DOCUMENTS AND REFERENCE DATA |
| SECTION III: WORK REQUIREMENTS |
| SECTION V: POINT OF CONTACT |
| 2025-05-13T12:47:10-0400 | |
| FAIRBANKS.SCOTT.M.1391459416 |
| 2025-05-13T13:23:58-0400 | |
| HARRISON.JONATHAN.R.1397218623 |
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