Airframe Structural Components: AE94900Z, AE98516R, AEA24917D720A
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| AE94900Z | 1560-00-350-0590 | Fitting, Starter Return | III End Item Identification: Aircraft model C5A | Eaton Corporation (00624) | |
| AE94913G | 1560-00-435-0898 | Fitting and Coupling | III End Item Identification: Aircraft model C5A | Eaton Corporation (00624) | |
| AE95620G | 1560-01-423-0208 | Support, Structural Component, Air | III End Item Identification: Aircraft E-3 Special Features: Nut, actuator and swivel joint installation, spoiler. | Eaton Corporation (00624) | |
| AE96300Z | 1560-00-350-0590 | Fitting, Starter Return | III End Item Identification: Aircraft model C5A | Eaton Corporation (00624) | |
| AE97829K | 1560-01-012-8109 | Cap, Fuel Tank | General Characteristics Item Description: Aluminum QQ-A-225/6 composition 2024-T351 and 2024-T4, and cres 304 QQ-W-423, 1.640 in. O/a lg, 1.590 in. O/a dia | Eaton Corporation (00624) | |
| AE98516R | 1560-01-228-5064 | Adapter, Pressure Fuel Servicing | Eaton Corporation (00624) | ||
| AE99748H | 1560-01-481-2981 | Adapter, Straight, Tu | III End Item Identification: Fighter aircraft - first (F18 E/f) Criticality Code Justification: AGAV | Eaton Corporation (00624) | |
| AE-A249-13AKIT AEA24913AKIT | 1560-01-329-6481 | Modification kit, Airframe | End Item Identification: CH-47D cargo hel | Pall Aeropower Corp. (60047) | |
| AE-A249-13B AEA24913B | 1560-01-329-6482 | Modification kit, Airframe | End Item Identification: CH-47D, air particle separator instl | Pall Aeropower Corp. (60047) | |
| AE-A249-13D628A AEA24913D628A | 1560-01-353-0831 | Cover, Access | Material: Aluminum alloy END Item Identification: Helicopter, chinook, CH-47 Surface Treatment: Anodize and primer | Pall Aeropower Corp. (60047) Pall Aeropower Corporation (18350) | |
| AEA24913KT3D160 | 1560-01-530-1460 | Plate, Structural, Aircraft | III End Item Identification: CH47D helicopter, cargo-transport nsn 1520-01-088-3669 Material: Aluminum alloy Aircraft Location: Left side | Pall Aeropower Corporation (18350) | |
| AEA24913KTA | 1560-01-473-7720 | Modification kit, Me | III End Item Identification: CH-47 rotary wing aircraft | Pall Aeropower Corporation (18350) | |
| AEA24913KTB | 1560-01-473-7719 | Modification kit, Me | III End Item Identification: CH-47 rotary wing aircraft | Pall Aeropower Corporation (18350) | |
| AEA24914KT3D159 | 1560-01-530-1475 | Plate, Structural, Aircraft | III End Item Identification: CH47D helicopter, cargo-transport nsn 1520-01-088-3669 Material: Aluminum alloy Aircraft Location: Right side | Pall Aeropower Corporation (18350) | |
| AEA24914KT3D160 | 1560-01-530-1467 | Plate, Structural, Aircraft | III End Item Identification: CH47D helicopter, cargo-transport nsn 1520-01-088-3669 Material: Aluminum alloy Aircraft Location: Right side | Pall Aeropower Corporation (18350) | |
| AEA24917D7109A | 1560-01-561-0944 | Latch Assembly, Aircraft | Aircraft Mission Design Series: CH-47 chinook Special Features: Used to retain the cross shaft seal assembly- has an angle of 20 degrees and a U shaped groove cut into one end Material: Steel comp 304 | Pall Aeropower Corporation (18350) | |
| AEA24917D7111A | 1560-01-561-2758 | Hinge, Aircraft | Pall Aeropower Corporation (18350) | ||
| AEA24917D7112A | 1560-01-561-4155 | Plate, Structural, Aircraft | III End Item Identification: CH-47 helicopter | Pall Aeropower Corporation (18350) | |
| AEA24917D7113A | 1560-01-561-3487 | Pad, Chafe | III End Item Identification: 1520-01-088-3669 | Pall Aeropower Corporation (18350) | |
| AEA24917D720A | 1560-01-561-3104 | Latch Assembly, Aircraft | III End Item Identification: 1520010883669 Overall Length: 5.390 inches nominal | Pall Aeropower Corporation (18350) |