Weapon System - Hardware: 1288-228-01, 128B10514-21, 128B10514-22
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
1288-228-01 128822801 | 5342-00-894-3428 | Clamp, Mounting | Barry Wright Corporation (81860) | ||
128827 | 5342-00-313-3597 | Bracket, E, Ternal Hy | Curtiss-Wright Controls Inc. (0AHP5) | ||
12883 | 5342-01-237-4129 | Clip, Special | Tennant Company (59500) | ||
128836C W 128836CW | 5342-01-250-2237 | Cover Assembly, Special | Oshkosh Corporation (45152) | ||
12893052 | 5342-01-401-3725 | Mount, Resilient, Weapon System | Stewart & Stevenson Power Products (81381) | ||
1289520-101 1289520101 | 5342-00-302-9291 | Bracket, Duct | General Characteristics Item Description: 347 investment casting, C03-508, fscm 36659, 2.370 in. min, 2.430 in. max, tapered to 2.080 in. min, 2.110 in. max, base, 0.760 in. O/a H, 2 mtg slots thru base, 1.765 in. min, 1.775 in. max, dia id, counterbored, 1.950 in. min, 1.990 in. max, by 0.420 in. deep, penetrant inspect LCP1068, fscm 36659, 125 aa finish, arithmetic average surface roughness | Lockheed Martin Corporation (98897) | |
128AB10388-611 128AB10388611 | 5342-01-259-4616 | Bracket, Landing Gear Control | General Characteristics Item Description: Aluminum alloy, QQ-A-250/5, alloy 2024, chromate, MIL-C-5541; 0.040 in. thk | Northrop Grumman Systems Corporation (26512) | |
128AB10388-612 128AB10388612 | 5342-01-259-4170 | Bracket, Landing Gear Control | General Characteristics Item Description: Aluminum alloy, QQ-A-250/5, alloy 2024, chromate, MIL-C-5541; 0.040 in. thk | Northrop Grumman Systems Corporation (26512) | |
128AB10388-613 128AB10388613 | 5342-01-259-7968 | Bracket, Landing Gear Control | General Characteristics Item Description: Aluminum alloy, QQ-A-250/5, alloy 2024, chromate, MIL-C-5541; 0.040 in. thk; two holes, 0.098 in. dia | Northrop Grumman Systems Corporation (26512,61174) | |
128AB10553-3 128AB105533 | 5342-01-266-3873 | Door, Access, Weapon System | Material: Aluminum alloy 2024 Cross-Sectional Shape Style: 26 flat Material Document and Classification: QQ-A-250/5 T42 fed spec single material response | Northrop Grumman Systems Corporation (26512,61174) | |
128AB10793-11 128AB1079311 | 5342-01-270-8160 | Bracket, Sequencer unit | General Characteristics Item Description: Aluminum alloy 2024, QQ-A-250/5 T3 or T42; gloss acrylic white finish; 4 mounting holes 0.233 in. min and 0.239 in. max; distance between mounting holes along lg 5.245 in. min and 5.255 in. max; distance between mounting holes along W 3.245 in. min and 3.255 in. max; 1.000 in. H | Northrop Grumman Systems Corporation (26512,61174) | |
128ABM10006-1 128ABM100061 | 5342-00-970-9554 | Crank, Control | Northrop Grumman Systems Corporation (26512) | ||
128ABM10169-1 128ABM101691 | 5342-00-966-9901 | Crank | Northrop Grumman Systems Corporation (26512) | ||
128ABP1006-15 128ABP100615 | 5342-01-239-0692 | Bracket, Special | General Characteristics Item Description: Plastic | Northrop Grumman Systems Corporation (61174) | |
128ABP10066-13 128ABP1006613 | 5342-01-270-4342 | Bracket, foot Guard | General Characteristics Item Description: Plastic abs | Northrop Grumman Systems Corporation (26512) | |
128ABP10066-15 128ABP1006615 | 5342-01-239-0692 | Bracket, Special | General Characteristics Item Description: Plastic | Northrop Grumman Systems Corporation (26512) | |
128ABP10066-603 128ABP10066603 | 5342-01-256-4590 | Bracket, Protective Panel | General Characteristics Item Description: Includes flame resistant plastic bracket, 2 seals, 2 doublers, 4 nut plates and 8 eyelets; color dark gull gray | Northrop Grumman Systems Corporation (26512,61174) | |
128AV10976-1 128AV109761 | 5342-01-220-2314 | Bracket | Northrop Grumman Systems Corporation (26512) | ||
128B10514-21 128B1051421 | 5342-01-259-7966 | Clip, Fuselage Tail Section | General Characteristics Item Description: Aluminum alloy, QQ-A-250/3, alloy 2014, chromate, g.s.s. 9.010, grumman aerospace corp; 0.063 in. thk; four holes, 0.127 in. min 0.133 in. max dia | Northrop Grumman Systems Corporation (26512) | |
128B10514-22 128B1051422 | 5342-01-259-7967 | Clip, Fuselage Tail Section | General Characteristics Item Description: Aluminum alloy, QQ-A-250/3, alloy 2014, chromate, g.s.s. 9.010, grumman aerospace corp; 0.063 in. thk; four holes, 0.127 in. min 0.133 in. max dia; opposite of 128B10589-17 | Northrop Grumman Systems Corporation (26512) |