Airframe Structural Components: LS1569-20-7, LS173-4, LS2130-5-7
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| LS1569-20-7 LS1569207 | 1560-00-821-0857 | Blanket, Insulation | III End Item Identification: T-33 aircraft General Characteristics Item Description: For general use only;for high velocity air, use LS3839;MATERIAL-COVER-CHLOROPRENE covered fiberglass cloth, lining-no. 108 owens corning fbrgls cloth, filler- 1 in., 1/20 density fiberglass insulation | Lockheed Martin Corporation (98897) | |
| LS1569-20-9 LS1569209 | 1560-00-613-4514 | Blanket, Thermo | General Characteristics Item Description: Fiberglass filler, MIL-B-5924, type 2, 1.000 in. thk, 8.875 in. min, 8.125 in. max lg | Lockheed Martin Corporation (98897) | |
| LS1569-28-15 LS15692815 | 1560-00-630-5261 | Blanket Assy, Insula | Lockheed Martin Corporation (98897) | ||
| LS1569-28-2 1-4 LS156928214 | 1560-00-310-1128 | Blanket, Thermo | General Characteristics Item Description: Fiberglass filler, MIL-B-5924, type 2, 1.000 in. thk, 2.125 in. min, 2.375 in. max lg, 7.690 in. min, 8.070 in. max W, fiberglass cloth cover, and fiberglass cloth lining, MIL-G-11404 | Lockheed Martin Corporation (98897) | |
| LS1569-28-8 LS1569288 | 1560-00-630-5518 | Blanket, Thermo | General Characteristics Item Description: Fiberglass filler, MIL-B-5924, type 2, 1.000 in. thk, 7.875 in. min, 8.125 in. max lg | Lockheed Martin Corporation (98897) | |
| LS1569-32-17-1/2 LS1569321712 | 1560-01-140-2230 | Insulation Blanket, Thermal | Special Features: Material-cover-chloroprene covered fiberglass cloth, LINING-108 owens corning fiberglass cloth, filler- 1 in. 1/2 density fiberglass insulation;tan color Length: 17.500 inches nominal Mounting Facility: Strip | Lockheed Martin Corporation (98897) | |
| LS1569-32-21 LS15693221 | 1560-00-703-0878 | Insulation, Thermal, Special Purpo | Special Features: T-33 | Lockheed Martin Corporation (98897) | |
| LS1569-48-14 LS15694814 | 1560-00-620-4957 | Blanket Assy, Insula | Lockheed Martin Corporation (98897) | ||
| LS1569-8-12 LS1569812 | 1560-00-697-9739 | Blanket, Thermo, Airc | Lockheed Martin Corporation (98897) | ||
| LS15782KT24-22P LS15782KT2422P | 1560-01-289-0076 | Connector | Lockheed Martin Corporation (98897) | ||
| LS15798-110 LS15798110 | 1560-01-314-9868 | Cup Panel Hole | Lockheed Martin Corporation (98897) | ||
| LS15798-145 LS15798145 | 1560-01-432-1905 | Cup, Panel Hole, Reinforcement | General Characteristics Item Description: Matl al alloy, 6061-T6; finished anodized; height 0.145 in; outside diameter 0.750 in min and 0.760 in max | Lockheed Martin Corporation (98897) | |
| LS159-2 LS1592 | 1560-01-483-4822 | Stiffener, Aircraft | III End Item Identification: Used on C-130 aircraft Material: Aluminum | Lockheed Martin Corporation (98897) | |
| LS1636-2 LS16362 | 1560-00-629-9211 | End, Shock Cord | General Characteristics Item Description: Cres, AMS5566, 1.562 in. lg | Lockheed Martin Corporation (98897) | |
| LS1669-31D72 LS166931D72 | 1560-00-986-2698 | Filler, Split, Tubula | Aero Engineering & Manufacturing (17772) Lockheed Martin Corporation (98897) | ||
| LS173-4 LS1734 | 1560-01-483-4824 | Stiffener, Aircraft | III End Item Identification: Used on C-130 aircraft Material: Aluminum Material Document and Classification: QQ-A-250 fed spec single material response | Lockheed Martin Corporation (98897) | |
| LS1812-12 LS181212 | 1560-00-650-5942 | Coupling, Flanged | General Characteristics Item Description: Aluminum alloy, 2.038 in. lg, 0.75 in. od, 3.10 in. max 2.90 in. min flange dia | Lockheed Martin Corporation (98897) | |
| LS181-7 LS1817 | 1560-01-345-1957 | Stiffener, Aircraft | Specification/Standard Data: 98897-LS181-7 manufacturers standard | Lockheed Martin Corporation (98897) | |
| LS2130-5-10 LS2130510 | 1560-00-986-2699 | Transition Piece, Fl | Lockheed Martin Corporation (98897) | ||
| LS2130-5-7 LS213057 | 1560-00-986-2700 | Transition Piece, Fl | Lockheed Martin Corporation (98897) |