Airframe Structural Components: 5HF42538-119, 5HF42553-105, 5HF42714-101
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 5HF42538-119 5HF42538119 | 1560-01-559-6014 | Panel, Structural, Aircraft | III End Item Identification: F-22 raptor Aircraft Mission Design Series: F-22A III Part Name Assigned BY Controlling Agency: Panel | Lockheed Martin Corporation (81755) | |
| 5HF42538-120 5HF42538120 | 1560-01-559-6020 | Panel, Structural, Aircraft | III End Item Identification: F-22 raptor Aircraft Mission Design Series: F-22A Material: Titanium alloy | Lockheed Martin Corporation (81755) | |
| 5HF42538-121 5HF42538121 | 1560-01-559-6018 | Panel, Structural, Aircraft | III End Item Identification: F-22RAPTOR Aircraft Mission Design Series: F-22A Material: Titanium alloy | Lockheed Martin Corporation (81755) | |
| 5HF42538-122 5HF42538122 | 1560-01-559-6019 | Panel, Structural, Aircraft | III End Item Identification: F-22RAPTOR Aircraft Mission Design Series: F-22A Material: Titanium alloy | Lockheed Martin Corporation (81755) | |
| 5HF42546-111 5HF42546111 | 1560-01-535-6756 | Pan Assembly | III End Item Identification: F/A-22 raptor Special Features: F-22 emd | Lockheed Martin Corporation (81755) | |
| 5HF42546-121 5HF42546121 | 1560-01-488-1713 | Panel, Structural, Aircraft | III End Item Identification: F-22 raptor Aircraft Mission Design Series: F-22A Special Features: Fracture/durability critical item; C/o: 123 cap, -125 & -126 stiffener, and -127 & -129 floor; m/f: titanium, 6AL-4V ann | Lockheed Martin Corporation (81755) | |
| 5HF42553-103 5HF42553103 | 1560-01-486-9208 | Panel, Canopy, Aircraft | III End Item Identification: F-22A raptor Aircraft Mission Design Series: F-22A Special Features: C/o: 920574001 pps; m/f: composite material: 5PTMKG64-1-1 thermoplastic pps moulding unreinforced; wind swept surface critical item | Lockheed Martin Corporation (81755) | |
| 5HF42553-105 5HF42553105 | 1560-01-509-2236 | Panel, Canopy, Aircraft | III End Item Identification: F-22A raptor Aircraft Mission Design Series: F-22A Special Features: C/o: 920574001 pps; m/f: composite material: 5PTMKG64-1-1 thermoplastic pps moulding unreinforced; wind swept surface critical item | Lockheed Martin Corporation (81755) | |
| 5HF42702-103 5HF42702103 | 1560-01-488-4563 | Bracket, Structural Component, Air | III End Item Identification: F-22 raptor Aircraft Mission Design Series: F-22 Special Features: Heat treat T8151 | Lockheed Martin Corporation (81755) | |
| 5HF42702-104 5HF42702104 | 1560-01-549-0283 | Bracket, Structural Component, Air | III End Item Identification: F-22 raptor Aircraft Mission Design Series: F-22A III Part Name Assigned BY Controlling Agency: Bracket | Lockheed Martin Corporation (81755) | |
| 5HF42710-105 5HF42710105 | 1560-01-488-1718 | Fitting, Structural Component, Air | III End Item Identification: F-22 raptor Aircraft Mission Design Series: F-22 acft Material: Titanium | Lockheed Martin Corporation (81755) | |
| 5HF42710-107 5HF42710107 | 1560-01-524-2134 | Fitting, Structural Component, Air | Lockheed Martin Corporation (81755) | ||
| 5HF42710-109 5HF42710109 | 1560-01-526-1008 | Fitting, Structural Component, Air | Lockheed Martin Corporation (81755) | ||
| 5HF42710-115 5HF42710115 | 1560-01-566-8199 | Fitting, Structural Component, Air | III End Item Identification: F-22 raptor Special Features: C/O 1 -113 fitting and 1 MS14103-10 bearing;located at FS443;USED as lh/rh main weapons bay power hinge fitting | Lockheed Martin Corporation (81755) | |
| 5HF42711-109 5HF42711109 | 1560-01-488-1715 | Fitting, Structural Component, Air | III End Item Identification: F/A-22 raptor Special Features: 2124 -T8151 al 5.000 plate width 11, length 9 Material: Aluminum alloy 2124 | Lockheed Martin Corporation (81755) | |
| 5HF42711-111 5HF42711111 | 1560-01-526-2759 | Fitting, Structural Component, Air | Lockheed Martin Corporation (81755) | ||
| 5HF42712-117 5HF42712117 | 1560-01-488-1717 | Fitting, Structural Component, Air | III End Item Identification: F-22 raptor Aircraft Mission Design Series: F-22 acft Special Features: Heat treat T8151 | Lockheed Martin Corporation (81755) | |
| 5HF42712-118 5HF42712118 | 1560-01-488-1719 | Fitting, Structural Component, Air | III End Item Identification: F-22 raptor Aircraft Mission Design Series: F-22 Special Features: Heat treat T8151 | Lockheed Martin Corporation (81755) | |
| 5HF42713-105 5HF42713105 | 1560-01-488-1721 | Fitting, Structural Component, Air | III End Item Identification: F-22 raptor Aircraft Mission Design Series: F-22A Special Features: Fracture/durability critical part; dim. are stock material; m/o: 2024-T8151 aluminum plate | Lockheed Martin Corporation (81755) | |
| 5HF42714-101 5HF42714101 | 1560-01-535-8598 | Fitting, Structural Component, Air | III End Item Identification: F/A-22 raptor Aircraft Mission Design Series: F/A-22 raptor | Lockheed Martin Corporation (81755) |