FSC 1560 Airframe Structural Components: 1560-00-109-9726, 1560-00-109-9767, 1560-00-110-2908
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1560-00-109-9726 1560001099726 | 3P21525-101 | Rod Assembly, Cowling Support | General Characteristics Item Description: Cres, MIL-T-8808, 7.860 in. lg | Lockheed Martin Corporation (98897) Space AGE MFG Corp. (32483) E. W. Packaging Corporation Inc. (6M161) | |
| 1560-00-109-9758 1560001099758 | 65752-07004-081 | Strut, Armor, Servo, Tail Rotor | General Characteristics Item Description: Steel MIL-S-6736 MIL-S-18729, 16.030 in. lg, heat treat to 125000 psi, rockwell hardness C26 to C33 | Sikorsky Aircraft Corporation (78286) | |
| 1560-00-109-9759 1560001099759 | 65752-07004-082 | Strut, Armor, Servo, Tail Rotor | General Characteristics Item Description: Steel MIL-S-6736 MIL-S-18729, 15.570 in. lg, heat treat to 125000 psi, rockwell hardness C26 to C33 | Sikorsky Aircraft Corporation (78286) | |
| 1560-00-109-9764 1560001099764 | 3F31710-103 | Bracket, Restraint Rail, Ramp | General Characteristics Item Description: Aluminum alloy, 7075-T6, QQ-A-200/11, applicable to C141 acft | Lockheed Martin Corporation (98897) | |
| 1560-00-109-9766 1560001099766 | 65200-08027-045 65200-08027-041 | Sponson Assembly, F | General Characteristics Item Description: Complete assy less fuel cell and lines | Sikorsky Aircraft Corporation (78286) | |
| 1560-00-109-9767 1560001099767 | 65200-08027-042 65200-08027-046 | Sponson Assembly, F | General Characteristics Item Description: Complete assy less fuel cell and lines | Sikorsky Aircraft Corporation (78286) | |
| 1560-00-109-9768 1560001099768 | 65200-08001-045 | Sponson Assy, Aft | Sikorsky Aircraft Corporation (78286) | ||
| 1560-00-109-9769 1560001099769 | 65200-08001-046 | Sponson Assy, Aft | Sikorsky Aircraft Corporation (78286) | ||
| 1560-00-109-9862 1560001099862 | 88-54840 | Tube Assy, Battery V | Boeing Company, The (43999) | ||
| 1560-00-109-9966 1560001099966 | 4114029-33 | Cable Assy, Left Han | Boeing Company, The (18355, 88277) | ||
| 1560-00-109-9971 1560001099971 | 4114029-5 | Cable Assy, Left Han | Boeing Company, The (88277, 18355) | ||
| 1560-00-109-9972 1560001099972 | 4114029-7 | Cable Assy, Left Han | Boeing Company, The (18355, 88277) | ||
| 1560-00-110-1475 1560001101475 | S6290-62050-1 | Table Assy Tilt | Sikorsky Aircraft Corporation (78286) | ||
| 1560-00-110-2617 1560001102617 | 16585-1 | Key and Ring | ITT Cannon Electric (08718) | ||
| 1560-00-110-2618 1560001102618 | 16584-1 | Key and Ring | ITT Cannon Electric (08718) ITT Corporation (71468) | ||
| 1560-00-110-2892 1560001102892 | 4F11890-101A | Lever, cam, Windshield | III End Item Identification: Acft model C5A General Characteristics Item Description: Aluminum alloy, 7075-T651, QQ-A-225/9, 3.250 in. lg, 1.569 in. W, 1.035 in. O/a H | Aero Components Inc. (59213) Lockheed Martin Corporation (98897) Tect Aerospace Inc. (34336) | |
| 1560-00-110-2893 1560001102893 | 4F11890-102A | Lever, cam, Windshield | III End Item Identification: Acft model C5A General Characteristics Item Description: Aluminum alloy, 7075-T651, QQ-A-225/9, 3.250 in. lg, 1.569 in. W, 1.035 in. O/a H | Lockheed Martin Corporation (98897) | |
| 1560-00-110-2895 1560001102895 | 4F11892-102A | Plate, Cover, Latching | General Characteristics Item Description: Aluminum alloy 7075-T651, QQ-A-250/12 T6, 21.640 in. lg, 1.020 in. W, 0.100 in. thk, 15 ea 0.271 in. min, 0.278 in. max dia holes, 2 ea 0.343 in. min, 0.350 in. max dia holes counterbored 0.438 in. nom dia, 0.063 in. deep 14.750 in. C to C | Lockheed Martin Corporation (98897) | |
| 1560-00-110-2898 1560001102898 | 4J22068-102C 4J22068-102B 4J22068-102D 4J22068-102A | Skin, Aircraft | III End Item Identification: Aircraft model C5A Material: Aluminum alloy Material Document and Classification: QQ-A-250/13 fed spec single material response | Lockheed Martin Corporation (98897) | |
| 1560-00-110-2908 1560001102908 | 4F11879-102A | Housing, Bushing | III End Item Identification: Aircraft model C5A General Characteristics Item Description: Aluminum alloy, QQ-A-225/9 comp 7075 cond T651, 5.850 in. O/a lg, 2.850 in. O/a W, 2.553 in. O/a H, bushing hole 1.5625 in. min, 1.5630 in. max dia after plating | Lockheed Martin Corporation (98897) |