Airframe Structural Components: 53L580001, 540-001-307-1, 540-011-014-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 53L580001 | 1560-00-231-9209 | Foam Assembly | III End Item Identification: Aircraft model F4 | Boeing Company, The (76301) | |
| 53L580003 | 1560-00-204-6264 | Foam Assembly, Fuel Tank | III End Item Identification: Aircraft model F4 | Boeing Company, The (76301) | |
| 53L580004 | 1560-00-204-6273 | Foam Assembly, Fuel Tank | III End Item Identification: Aircraft model F4 | Boeing Company, The (76301) | |
| 53L580005 | 1560-00-204-6266 | Foam Assembly, Fuel Tank | III End Item Identification: Aircraft model F4 | Boeing Company, The (76301) | |
| 53L580006 | 1560-00-204-6267 | Foam Assembly, Fuel Tank | III End Item Identification: Aircraft model F4 | Boeing Company, The (76301) | |
| 53L580007 | 1560-00-204-6269 | Foam Assembly, Fuel Tank | III End Item Identification: Aircraft model F4 | Boeing Company, The (76301) | |
| 53S79006D287 | 1560-01-061-6463 | Wire Bundle | Boeing Company, The (76301) | ||
| 53SB11423-4 53SB114234 | 1560-01-091-4811 | Plate, Structural, Aircraft | III End Item Identification: Acft model F4C Special Features: Do not use cadmium plated tools on this item, titanium 6AL-4V AMS-4911 annealed per MIL-T-9046 type 3, 0.437 in.thk, 4.860 in.W, 4.950 in.lg, right hand; Criticality Code Justification: FEAT | Boeing Company, The (76301) | |
| 53SB3905-3 53SB39053 | 1560-00-780-7753 | Angle, Cover Access | General Characteristics Item Description: Aluminum alloy, QQ-A-250/15 | Boeing Company, The (76301) | |
| 53SB3908-3 53SB39083 | 1560-00-776-0110 | Former, Aircraft | Material: Aluminum alloy Material Document and Classification: QQ-A-250/12 fed spec single material response | Boeing Company, The (76301) | |
| 53SCC787-101 53SCC787101 | 1560-00-705-8421 | Brace Assy, Anti Swa | Sacramento Air Logistics Center (98749) | ||
| 5400010100-5 54000101005 | 1560-00-798-5687 | Heater, Venturi | III End Item Identification: Aircraft model F-4C General Characteristics Item Description: Aluminum alloy, QQ-A-596, 256 T6, 9.230 in. min, 9.311 in. max lg | Essex Industries Inc. (83533) | |
| 5400010200-2 54000102002 | 1560-00-570-7917 | Tube Assembly, Probe | General Characteristics Item Description: Aluminum alloy | Essex Industries Inc. (83533) | |
| 5400010400-1 54000104001 | 1560-00-759-2222 | Heater Assembly, Probe | General Characteristics Item Description: 41.810 in. min, 41.890 in. max lg | Essex Industries Inc. (83533) | |
| 540-001-300-1 5400013001 | 1560-00-872-1138 | Support Assembly, Cy | Bell Helicopter Textron Inc. (97499) Lockheed Martin Corporation (80070) | ||
| 540-001-301-1 5400013011 | 1560-00-872-1139 | Support Assembly, Cy | Bell Helicopter Textron Inc. (97499) Lockheed Martin Corporation (80070) | ||
| 540-001-307-1 5400013071 | 1560-00-918-2685 | Counterweight, Fore | Bell Helicopter Textron Inc. (97499) Lockheed Martin Corporation (80070) | ||
| 540-001-905-1 5400019051 | 1560-00-871-8679 | Support, Structural Component, Air | III End Item Identification: Used on AH-1 series helicopters Aircraft Mission Design Series: AH-1 Material: Steel | Bell Helicopter Textron Inc. (97499) Lockheed Martin Corporation (80070) Textron Systems Corporation (04614) | |
| 540-001-907-1 5400019071 | 1560-00-872-1114 | Bell Crank | Bore Diameter: 0.7488 inches minimum and 0.7493 inches maximum Bore Length: 0.750 inches minimum and 0.760 inches maximum Center to Center Distance Between Fulcrum and Arm End Hole/Slot/Ball: 2.996 inches nominal 1ST end | Bell Helicopter Textron Inc. (97499) Lockheed Martin Corporation (80070) | |
| 540-011-014-1 5400110141 | 1560-00-907-5139 | Tip cap, Rotor Blade | Bell Helicopter Textron Inc. (97499) Lockheed Martin Corporation (80070) |