Airframe Structural Components: C3FS515-9, C4287-1, C4810065-3
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| C3FS515-9 C3FS5159 | 1560-00-520-4513 | Window Panel, Aircraft | Material: Plastic Material Document and Classification: MIL-P-5425 mil spec single material response Thickness: 0.080 inches nominal | Bombardier Aerospace Aerospace Div. (71867) | |
| C3N98-3 C3N983 | 1560-00-861-7276 | Tab, Locking Battery | General Characteristics Item Description: Steel, MIL-S-18729, cadmium plated, 0.875 in.lg, 0.600 in. W, 0.300 in. H, 1 mtg hole 0.257 in. dia | Bombardier Aerospace Aerospace Div. (71867) DE Havilland Inc. (0HWZ3) | |
| C3UT102-3 C3UT1023 | 1560-00-525-9406 | Housing Assy, Steeri | Bombardier Aerospace Aerospace Div. (71867) | ||
| C4040 | 1560-00-335-6945 | Support, Roller | III End Item Identification: Aircraft model H19 General Characteristics Item Description: Aluminum alloy, AN-A-12, 1.687 in. O/a lg, 0.750 in. min, 0.755 in. max O/a W, 0.344 in. O/a H | COX Machine Inc. (16413) | |
| C404-15 C40415 | 1560-00-895-2981 | Cap Assembly, Filler | General Characteristics Item Description: Aluminum alloy, 12 holes, 0.281 in. dia spaced equally | Lockheed Martin Corporation (81755) | |
| C404-2 C4042 | 1560-00-012-3609 | Adapter, Filler cap | General Characteristics Item Description: Aluminum alloy, 10.590 in. dia, 3.001 in. dia of opening, 24 mtg HOLES0.250 in. min, 0.255 in. max dia | Lockheed Martin Corporation (81755) | |
| C404&3 C4043 | 1560-00-929-6973 | Adapter, Fuel Filler | General Characteristics Item Description: Aluminum alloy, 8.080 in. dia, 0.553 in. H, 3.001 in. dia of opening, 19 mtg holes 0.250 in. min, 0.255 in. max dia | Lockheed Martin Corporation (81755) | |
| C412-1 C4121 | 1560-00-997-3625 | Housing, Slip Joint | General Characteristics Item Description: Aluminum alloy, 6061-T6, QQ-A-207, rubber seal, per MIL-R-25988, 125 microinches, anodized finish | Lockheed Martin Corporation (81755) | |
| C413-1 C4131 | 1560-00-853-7000 | Housing, Slip Joint | General Characteristics Item Description: Aluminum alloy, QQ-A-200-8 | Lockheed Martin Corporation (81755) | |
| C4245-11 C424511 | 1560-00-410-3668 | Insulation Pipe Covering, Thermal, Special Purpose | Lockheed Martin Corporation (81755) | ||
| C4245-13 C424513 | 1560-00-410-3669 | Insulation Pipe Covering, Thermal | Lockheed Martin Corporation (81755) | ||
| C4245-15 C424515 | 1560-00-410-3670 | Insulation Pipe Covering, Thermal | Lockheed Martin Corporation (81755) | ||
| C4245-17 C424517 | 1560-00-410-3671 | Insulation Pipe Covering, Thermal | Lockheed Martin Corporation (81755) | ||
| C4277-1 C42771 | 1560-00-465-7473 | Insulation, Thermal, Special Purpo | Lockheed Martin Corporation (81755) | ||
| C4277-2 C42772 | 1560-00-482-0081 | Insulation, Thermal, Special Purpo | Special Features: Aircraft model FB-111;INSULATION felt Thickness: 0.190 inches nominal Length: 14.220 inches nominal | Lockheed Martin Corporation (81755) | |
| C4287-1 C42871 | 1560-00-249-9530 | Strut Assembly, Door Stop | III End Item Identification: Aircraft model F111 General Characteristics Item Description: 11.375 in. min, 11.499 in. max O/a lg | Lockheed Martin Corporation (81755) | |
| C442-2 C4422 | 1560-00-997-3746 | Seal, Fuel Tank Unit | Lockheed Martin Corporation (81755) | ||
| C442-6 C4426 | 1560-00-994-5271 | Seal, Tank unit, Fuel Quantity | III End Item Identification: Acft model F111 General Characteristics Item Description: 0.090 in.thick, 3.50 in.outside dia hex, 2.30 in.inside dia, 1 hole 0.312 to 0.320 in.dia, 5 holes 0.266 to 0.274 in.dia, 3.187 in.dbc, 2.660 in.dia groove C/l | Lockheed Martin Corporation (81755) | |
| C4581RM1 | 1560-01-127-5252 | Latch Assembly, Togg | Tecnotec Sarl (F6033) | ||
| C4810065-3 C48100653 | 1560-00-034-1008 | Floor, Aircraft | Aircraft Mission Design Series: C-7A | Bombardier Aerospace Aerospace Div. (71867) DE Havilland Inc. (0HWZ3) |