Airframe Structural Components: 4P51102-105A, 4P51131-103A, 4P52000-117
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 4P51102-105A 4P51102105A | 1560-00-001-6885 | Lock, Eccentric Bushing, Pylon to | General Characteristics Item Description: Cres, 17-4PH, AMS5604, temper H1025, 3.000 in. lg, 3.000 in. W, 0.312 in. thk, W/NAS580-16-35 spline, 2 mtg holes 0.280 in. min, 0.287 in. max dia spaced 1.250 in. center to center | A and M Aerospace Inc. (6Z800) ADK Machine Inc. (0TFG3) Aero Components Inc. (59213) Aero Engineering & Manufacturing (17772) CAL-MIL Plastic Products Inc. (22557) Caprice Engineering Company Inc. (52916) Essner Precision Manufacturing LLC (92037) Falcon Manufacturing Corp. (0HM72) Lockheed Martin Corporation (98897) Mercer Products & Manufacturing (30205) Skyspares Parts Inc. (6M132) | |
| 4P51105-101A 4P51105101A | 1560-01-094-9367 | Strap, Fail Safe | III End Item Identification: C5 acft General Characteristics Item Description: Matl spec STM05-602; heat treatment 200 ksi min; matl size 0.250 by 3.750 by 23.000 in.; used to attach aft outboard pylon to wing | Lockheed Martin Corporation (98897) | |
| 4P51105-103A 4P51105103A | 1560-01-500-9501 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-5 Special Features: Requested name-plate(failsafe); material PH13-8MO; heat treat to 200 ksi cond H1000 Material: Steel | Lockheed Martin Corporation (98897) | |
| 4P51110-101A 4P51110101A | 1560-01-500-9649 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-5 Special Features: Material spec LS37666-1 X23.00, dim are stock material;heat treat to 200KSI min, cond H1000;PENETRANT insp per stp 53-201, mach per ds 30003, id per stp 63-001, heat treat and process per 54-013, finish code see ds 30000, finish, M-54 Material: Steel | Lockheed Martin Corporation (98897) | |
| 4P51115-101A 4P51115101A | 1560-01-498-4613 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-5 Special Features: Requested name spacer; nha 4P51096 Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 4P51120-101A 4P51120101A | 1560-01-498-3851 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-5 Special Features: M/0 PH13-8M0 steel per ST05-602 Material: Steel corrosion resisting | Lockheed Martin Corporation (98897) | |
| 4P51120-102A 4P51120102A | 1560-01-498-4612 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-5 Special Features: M/O PH13-8MO steel per STO5-602 Material: Steel corrosion resisting | Lockheed Martin Corporation (98897) | |
| 4P51131-101A 4P51131101A | 1560-01-498-3857 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-5 Special Features: M/O PH13-8MO steel Material: Steel corrosion resisting | Lockheed Martin Corporation (98897) | |
| 4P51131-103A 4P51131103A | 1560-01-498-3856 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-5 Special Features: M/O PH13-8MO steel Material: Steel corrosion resisting | Lockheed Martin Corporation (98897) | |
| 4P51137-109A 4P51137109A | 1560-01-126-0073 | Pylon Assembly, Airc | Lockheed Martin Corporation (98897) | ||
| 4P51137-113A 4P51137113A | 1560-01-118-8001 | Stiffener | III End Item Identification: C-5A acft General Characteristics Item Description: Matl al alloy QQ-A-250/4 2024-T3, matl size .160 by 2 by 3 part of heat cap truss, inboard and out board pylon | A and M Aerospace Inc. (6Z800) Aero Components Inc. (59213) CPI Aerostructures Inc. (9U679) Lockheed Martin Corporation (98897) Rohr Inc. (51563) Tect Aerospace Inc. (34336) | |
| 4P51155-117A 4P51155117A | 1560-01-217-3551 | Retainer, web | Lockheed Martin Corporation (98897) | ||
| 4P51165-101A 4P51165101A | 1560-01-161-0557 | Support, Structural Component, Air | III End Item Identification: C-5 acft Special Features: C/O boot and retainer; boot matl rubber buna fuel resistant, MIL-S-6855, cli, grade 60; used as boot upper truss sealing, aft pylon attach point | Lockheed Martin Corporation (98897) | |
| 4P51166-103A 4P51166103A | 1560-01-041-8552 | Strap, Bonding, Inboard Pylon to W | III End Item Identification: Acft model C5A General Characteristics Item Description: Alum. alloy 6061-1 per QQ-A-250711, 0.040 in. thk 7.000 in. W, 12.000 in. lg | Lockheed Martin Corporation (98897) Rohr Inc. (51563) | |
| 4P51167-109A 4P51167109A | 1560-01-529-4767 | Support, Structural Component, Air | Aircraft Mission Design Series: C-5 Special Features: Electrical bond faying surfaces; matl al 6061-0; dim are stock matl Material: Aluminum alloy 6061 | Lockheed Martin Corporation (98897) | |
| 4P51167-115B 4P51167115B | 1560-00-001-5570 | Strap, Bonding, Outboard Pylon | General Characteristics Item Description: 17.800 in. lg, 3.620 in. W | Lockheed Martin Corporation (98897) | |
| 4P51168-101A 4P51168101A | 1560-01-501-8136 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-5 Special Features: PH13-8MO, spec stm 05-602 may be used in lieu of LS37666-1, PH13-8MO is not to be used when the preferred matl is available;heat treat 200 ksi min, cond H1000 per stp 54-013;DIM are stock material Material: Steel | Lockheed Martin Corporation (98897) | |
| 4P52000-101A 4P52000101A | 1560-00-732-2789 | Leading Edge, Pylon | III End Item Identification: Aircraft model C-5 | Lockheed Martin Corporation (98897) | |
| 4P52000-103B 4P52000103B | 1560-01-579-9765 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-5 Material: Aluminum alloy 2024 Aircraft Location: Leading edge, forward, pylon | Lockheed Martin Corporation (98897) Warner Robins Air Logistics Center (98752) | |
| 4P52000-117 4P52000117 | 1560-00-732-2789 | Leading Edge, Pylon | III End Item Identification: Aircraft model C-5 | Lockheed Martin Corporation (98897) |