Airframe Structural Components: 912267-1, 912267-2, 91262
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 912267-1 9122671 | 1560-00-821-4071 | Leading Edge | Lockheed Martin Corporation (98897) | ||
| 912267-101 912267101 | 1560-00-621-4318 | Leading Edge, Aircraft | Lockheed Martin Corporation (98897) | ||
| 912267-102 912267102 | 1560-00-621-4319 | Wing Section, Outer | Lockheed Martin Corporation (98897) | ||
| 912267-107 912267107 | 1560-01-346-2770 | Leading Edge, Aircraft | Specification/Standard Data: 36659-912267-107 manufacturers standard | Lockheed Martin Corporation (98897) | |
| 912267-108 912267108 | 1560-01-346-2769 | Leading Edge, Aircraft | Specification/Standard Data: 36659-912267-108 manufacturers standard | Lockheed Martin Corporation (98897) | |
| 912267-2 9122672 | 1560-00-821-4075 | Leading Edge | Lockheed Martin Corporation (98897) | ||
| 912288-1 9122881 | 1560-00-802-4162 | Cover, Bladder Cell | Aero Engineering & Manufacturing (17772) Lockheed Martin Corporation (98897) | ||
| 91236-11 9123611 | 1560-00-789-4972 | Crossover, Fuel, Standard | III End Item Identification: Aircraft model UH-1D General Characteristics Item Description: Internal proof pressure test 5 psig, burst pressure test 10 psig, flexible section resistant to hydraulic oil to 160.0 deg F, flanged ends, 11.440 in. lg, 4.890 in. W connecting distance, 3 ea auxiliary connections, 2 per MS33656-8, 1 style g, 1 style E, 1 per AND10050-12 | Arrowhead Products Corporation (70628) | |
| 91236-13 9123613 | 1560-00-789-4947 | Crossover, Fuel, Standard | III End Item Identification: Aircraft model UH-1D General Characteristics Item Description: Internal proof pressure test 5 psig, burst pressure test 10 psig, flexible section resistant to hydraulic oil to 160.0 deg F, flanged ends, 11.440 in. lg, 4.890 in. W connecting distance, 2 ea auxiliary connections per MS33656-8, 1 style g, 1 style E | Arrowhead Products Corporation (70628) | |
| 91236-15 9123615 | 1560-00-789-4946 | Crossover, Fuel, Standard | III End Item Identification: Aircraft model UH-1D General Characteristics Item Description: Internal proof pressure test 5 psig, burst pressure test 10 psig, flexible section resistant to hydraulic oil to 160.0 deg F, flanged ends, 6.000 in. lg, 5.020 in. W connecting distance, 1.250 in. od end tubes | Arrowhead Products Corporation (70628) | |
| 91236-17 9123617 | 1560-00-789-4966 | Crossover, Fuel, Standard | III End Item Identification: Aircraft model UH-1D General Characteristics Item Description: Internal proof pressure test 5 psig, burst pressure test 10 psig, flexible section resistant to hydraulic fluid to 160.0 deg F, flanged ends, 6.000 in. lg, 5.020 in. W, 1.710 in. offset connecting distance, 1.250 in. od end tubes | Arrowhead Products Corporation (70628) | |
| 91236-19 9123619 | 1560-00-789-4965 | Crossover, Fuel, Standard | III End Item Identification: Aircraft model UH-1D General Characteristics Item Description: Internal proof pressure test 5 psig, burst pressure test 10 psig, flexible section resistant to hydraulic fluid to 160.0 deg F, 1 end flanged connection, 2ND end flared W/nut and sleeve, 5.600 in. lg, 3.900 in. W connecting span, 0.750 in. od end tubes | Arrowhead Products Corporation (70628) | |
| 91236-21 9123621 | 1560-00-789-4964 | Crossover, Fuel, Standard | III End Item Identification: Aircraft model UH-1D General Characteristics Item Description: Internal proof pressure test 5 psig, burst pressure test 10 psig, flexible section resistant to hydraulic fluid to 160.0 deg F, 1 end flanged connection, 2ND end flared W/nut and sleeve, 9.200 in. lg, 7.220 in. connecting span, 0.750 in. od end tubes | Arrowhead Products Corporation (70628) | |
| 912364-1 9123641 | 1560-00-802-4172 | Fitting Assembly | Lockheed Martin Corporation (98897) | ||
| 9123962-10 912396210 | 1560-01-358-6993 | Panel, Structural, Aircraft | Aircraft Mission Design Series: A-10A Material: Glass fiber Aircraft Location: Engine nacelle lower inner panel | Northrop Grumman Systems Corporation (26512) | |
| 91240-1 912401 | 1560-01-541-5172 | Mechanism Opening, a | III End Item Identification: Arr list code; first pbl; radome assembly III Part Name Assigned BY Controlling Agency: (Drawing) radome push mechanism; (inavy) mechanism opening | Avibank Mfg. Inc. (84256) | |
| 912413-1 9124131 | 1560-00-802-4988 | Cartridge Assembly | Aero Engineering & Manufacturing (17772) Lockheed Martin Corporation (98897) | ||
| 912459-1 9124591 | 1560-00-802-3054 | Straightener, E, Haus | Lockheed Martin Corporation (98897) | ||
| 912538-1 9125381 | 1560-00-802-4911 | Panel Assembly | Lockheed Martin Corporation (98897) | ||
| 91262 | 1560-00-694-6871 | Terminal Assembly, Door | General Characteristics Item Description: Brass stud, 0.125 in. spherical radius on one end, 10-32NF-2A thds on opposite end, O/a lg 1.281 in., mounted through center of phenolic mounting plate 1.500 in. dia, 0.125 in. thk | Northrop Grumman Systems Corporation (26512) |