Airframe Structural Components: 199C6630G7, 199C6630G8, 1AGM10845
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 199C6630G7 | 1560-01-471-8443 | Post, Spacer | BAE Systems Controls Inc. (89954) | ||
| 199C6630G8 | 1560-01-471-8439 | Post, Spacer | BAE Systems Controls Inc. (89954) | ||
| 19E50-1 19E501 | 1560-01-451-9944 | Diaphragm | III End Item Identification: E-3A awacs, grimes aerospace co | Grimes Aerospace Company (72914) | |
| 19E57-1 19E571 | 1560-01-245-2838 | Diaphragm | III End Item Identification: Acft model E-3A III Functional Description: Used on modulator assembly | Grimes Aerospace Company (72914) Honeywell International Inc. (59364) | |
| 19E83-2ACL53 19E832ACL53 | 1560-00-989-6805 | Shaft Assembly, Interconnecting | End Item Identification: Acft model T38 | Goodrich Corporation (99551) | |
| 19E83-2ACL54 19E832ACL54 | 1560-00-989-6800 | Guard Assy, Drive Sh | Goodrich Corporation (99551) | ||
| 19M1016-101 19M1016101 | 1560-01-389-6423 | Insulation, Thermal, Special Purpo | Width: 4.750 inches nominal Temp Rating: 200.0 deg fahrenheit Thickness: 0.050 inches nominal | HI-Temp Insulation Inc. (25167) | |
| 19M1016-103 19M1016103 | 1560-01-343-1651 | Insulation, Thermal, Special Purpo | Width: 8.500 inches nominal Thickness: 1.020 inches nominal Length: 23.300 inches nominal | HI-Temp Insulation Inc. (25167) | |
| 19M1016-105A 19M1016105A | 1560-01-341-7712 | Cover, Access | Material: Steel END Item Identification: C-5A aircraft Outside Diameter: 10.200 inches minimum and 10.300 inches maximum | HI-Temp Insulation Inc. (25167) | |
| 19M1017-101 19M1017101 | 1560-01-340-1942 | Panel, Structural, Aircraft | III End Item Identification: Aircraft, hercules C-130 | HI-Temp Insulation Inc. (25167) | |
| 19M1017-107 19M1017107 | 1560-01-339-9722 | Panel, Structural, Aircraft | III End Item Identification: B-1B aircraft Aircraft Location: WING | HI-Temp Insulation Inc. (25167) | |
| 19M1017-109 19M1017109 | 1560-01-340-1943 | Panel, Structural, Aircraft | III End Item Identification: Aircraft, hercules C-130 | HI-Temp Insulation Inc. (25167) | |
| 19M1017-111 19M1017111 | 1560-01-340-1944 | Panel, Structural, Aircraft | III End Item Identification: Aircraft, hercules C-130 | HI-Temp Insulation Inc. (25167) | |
| 19M1018-101 19M1018101 | 1560-01-343-1650 | Insulation, Thermal, Special Purpo | Temp Rating: 250.0 deg fahrenheit Special Features: C-5 aircraft | HI-Temp Insulation Inc. (25167) | |
| 19M1018-102 19M1018102 | 1560-01-352-1648 | Insulation, Thermal, Special Purpo | Width: 18.450 inches nominal Temp Rating: 250.0 deg fahrenheit Thickness: 4.400 inches nominal | HI-Temp Insulation Inc. (25167) | |
| 19P2A5730-5 19P2A57305 | 1560-01-468-9191 | Support, Structural Component, Air | III End Item Identification: C-17A acft Aircraft Mission Design Series: C17A Aircraft Location: Center fuselage | Boeing Company, The (88277) | |
| 19SRF240-1 19SRF2401 | 1560-01-240-0000 | Plate, Structural, Aircraft | Ogden Air Logistics Center (98747) | ||
| 19X21 1-2WIRE 19X2112WIRE | 1560-00-682-8137 | Former | Reference Number Differentiating Characteristics: For national wire stitcher model no. 9 | Gitzendanner Muller Co. Inc. (24985) | |
| 1A6587-8 1A65878 | 1560-00-422-2973 | Armor, Supplemental, Small Arms-Fr | Special Features: Model A-37 | Safe Car Inc. (0WPV0) | |
| 1AGM10845 | 1560-00-771-8259 | Shroud, Exhaust | Piper Aircraft Inc. (77294) |