Airframe Structural Components: 5HF43767-105, 5HF43767-109, 5HF44328-107
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 5HF43767-105 5HF43767105 | 1560-01-535-7199 | Fitting, Structural Component, Air | III End Item Identification: F/A-22 raptor Aircraft Mission Design Series: F/A-22 emd | Lockheed Martin Corporation (81755) | |
| 5HF43767-107 5HF43767107 | 1560-01-488-1665 | Fitting, Structural Component, Air | III End Item Identification: F-22 raptor Aircraft Mission Design Series: F-22A Special Features: Fracture critical catagory 2 item; thickness dim. is stock material; C/o: -101 fitting, CA2210-4R ring (4), CA2290-4-20-16 screw (4); m/o: 6AL-4V eli titanium beta ann plate | Lockheed Martin Corporation (81755) | |
| 5HF43767-109 5HF43767109 | 1560-01-515-4968 | Fitting, Structural Component, Air | III End Item Identification: F/A-22 raptor Aircraft Mission Design Series: F/A-22 raptor Special Features: Consists of 1 5HF43767-101 fitting | Lockheed Martin Corporation (81755) | |
| 5HF43769-105 5HF43769105 | 1560-01-488-5854 | Bracket, Structural Component, Air | III End Item Identification: F-22 raptor Aircraft Mission Design Series: F-22 raptor Special Features: Opposite -106 nsn 1560-01-488-5859 | Lockheed Martin Corporation (81755) | |
| 5HF43769-106 5HF43769106 | 1560-01-488-5859 | Bracket, Structural Component, Air | III End Item Identification: F-22 raptor Aircraft Mission Design Series: F-22A Special Features: Opposite -105; overall width & thickness dim. are stock material; m/o: 2024-0 aluminum sheet, final cond T62 | Lockheed Martin Corporation (81755) | |
| 5HF43775-103 5HF43775103 | 1560-01-535-6760 | Fitting, Structural Component, Air | III End Item Identification: F/A-22 raptor Special Features: F-22 emd III Part Name Assigned BY Controlling Agency: Fitting | Lockheed Martin Corporation (81755) | |
| 5HF43775-107 5HF43775107 | 1560-01-488-1667 | Fitting, Structural Component, Air | III End Item Identification: F-22 raptor Aircraft Mission Design Series: F-22A Special Features: Fracture critical / durability critical item; thickness dim. is stock material; C/o: -101 fitting, ring (4), screw (4); m/o: 6AL-4V eli titanium beta ann plate | Lockheed Martin Corporation (81755) | |
| 5HF43775-109 5HF43775109 | 1560-01-515-8577 | Fitting, Structural Component, Air | III End Item Identification: F-22A raptor Aircraft Mission Design Series: F-22A Special Features: Fracture/durability critical item, cat 2; dim are stock material; m/f: 6AL-4V eli titanium beta ann plate; C/o: -101 fitting & FT1761-12PT RING(4) | Lockheed Martin Corporation (81755) | |
| 5HF43781-103 5HF43781103 | 1560-01-537-5418 | Fitting, Structural Component, Air | III End Item Identification: F-22 raptor Aircraft Mission Design Series: F-22 Material: Aluminum alloy 2124 | Lockheed Martin Corporation (81755) | |
| 5HF43781-107 5HF43781107 | 1560-01-537-5421 | Fitting, Structural Component, Air | III End Item Identification: F-22 raptor Aircraft Mission Design Series: F-22 Material: Aluminum alloy 2124 | Lockheed Martin Corporation (81755) | |
| 5HF43782-103 5HF43782103 | 1560-01-537-6301 | Fitting, Structural Component, Air | III End Item Identification: F-22 raptor Aircraft Mission Design Series: F-22 Special Features: C/O 1 fitting, 1 bearing | Lockheed Martin Corporation (81755) | |
| 5HF43782-111 5HF43782111 | 1560-01-559-5722 | Fitting, Structural Component, Air | III End Item Identification: F-22 raptor Aircraft Mission Design Series: F-22 Material: Aluminum alloy | Lockheed Martin Corporation (81755) | |
| 5HF43821-105 5HF43821105 | 1560-01-488-1668 | Fitting, Structural Component, Air | III End Item Identification: F/A-22 raptor Aircraft Mission Design Series: F/A-22 raptor Special Features: Stock size is 5 inches wide; 3 inches long by 3 inch thick plate | Lockheed Martin Corporation (81755) | |
| 5HF43821-107 5HF43821107 | 1560-01-526-9871 | Fitting, Structural Component, Air | Lockheed Martin Corporation (81755) | ||
| 5HF43821-109 5HF43821109 | 1560-01-526-3850 | Fitting, Structural Component, Air | Lockheed Martin Corporation (81755) | ||
| 5HF44314-103 5HF44314103 | 1560-01-486-9222 | Frame, Aircraft | III End Item Identification: F/A-22 raptor Special Features: 2124-T8151 al, 1.500 plate Material: Aluminum alloy 2124 | Lockheed Martin Corporation (81755) | |
| 5HF44314-105 5HF44314105 | 1560-01-528-7410 | Frame, Aircraft | Aircraft Mission Design Series: F-22 Special Features: Dim. are stock material; heat treat to T8151 Material: Aluminum alloy 2124 | Lockheed Martin Corporation (81755) | |
| 5HF44314-107 5HF44314107 | 1560-01-528-8227 | Frame, Aircraft | III End Item Identification: F-22 Aircraft Station Number: FS443 Part Name Assigned BY Controlling Agency: FRAME-FS443, upper center | Lockheed Martin Corporation (81755) | |
| 5HF44328-105 5HF44328105 | 1560-01-486-9215 | Frame, Aircraft | III End Item Identification: F-22 raptor Aircraft Mission Design Series: F-22A Part Name Assigned BY Controlling Agency: Frame | Lockheed Martin Corporation (81755) | |
| 5HF44328-107 5HF44328107 | 1560-01-528-7935 | Frame, Aircraft | Aircraft Mission Design Series: F-22 Special Features: Matl al aly 2124-T8161 Material: Aluminum alloy 2124 | Lockheed Martin Corporation (81755) |