Airframe Structural Components: H3270-3, H3348-1, H3441-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| H3270-3 H32703 | 1560-01-392-7149 | Latch Assembly, Aircraft | Hartwell Corporation (83014) | ||
| H3274-3 H32743 | 1560-01-454-8953 | Latch Assembly, Aircraft | III End Item Identification: Preprovisioning support navicp is poe Special Features: Essential to weapon system performance or operation, or the preservation of life or safety of operating personnel Criticality Code Justification: FEAT | Hartwell Corporation (83014) | |
| H3274-9 H32749 | 1560-01-454-8961 | Latch Assembly, Aircraft | III End Item Identification: Preprovisioning support navicp is poe Special Features: Essential to weapon system performance or operation, or the preservation of life or safety of operating personnel Criticality Code Justification: FEAT | Hartwell Corporation (83014) | |
| H3293-9 H32939 | 1560-01-444-7105 | Latch Assembly, Aircraft | III End Item Identification: Preprovisioning support navicp is poe Special Features: Essential to weapon system performance or operation, or the preservation of life or safety of operating personnel Criticality Code Justification: FEAT | Hartwell Corporation (83014) | |
| H3345-1 H33451 | 1560-01-392-7147 | Strut, Aircraft | Hartwell Corporation (83014) | ||
| H3348-1 H33481 | 1560-01-580-7050 | Hinge, Door, Aircraft | III End Item Identification: KC-135 acft Aircraft Mission Design Series: KC-135(K) acft Special Features: Used on 527-12528-1 door | Hartwell Corporation (83014) The Boeing Company (82918) | |
| H3382-1 H33821 | 1560-01-476-3651 | Rod Assembly, Cover, Aircraft | Hartwell Corporation (83014) | ||
| H3383-1 H33831 | 1560-01-476-3653 | Rod Assembly, Cover, Aircraft | Hartwell Corporation (83014) | ||
| H339-1 H3391 | 1560-00-885-8679 | Latch Assembly, Cockpit | III End Item Identification: Aircraft model no. C-47 | Hartwell Corporation (83014) | |
| H3391-5 H33915 | 1560-01-474-4394 | Strut Assembly, Access Door | III End Item Identification: SH-2G(A) seasprite helicopter Special Features: Mounting bushings at each end have 0.312-0.314 in. inside dia.; adjustable spherical male end with jam nut on rod end; opposite end is cone shaped, integral with housing; when extended overall length of strut is 19.950 in. on bushing centers, plus or minus 0.250 in.; when retracted overall length is 10.000 in. on bushing centers plus or minus 0.250 in.; maximum diameter for locking collars with circular cross section is 1.630 in. III Part Name Assigned BY Controlling Agency: Forward self-locking strut assembly, engine access door | Hartwell Corporation (83014) | |
| H3393-33 H339333 | 1560-01-445-8370 | Latch Assembly, Aircraft | Boeing Company, The (88277) Hartwell Corporation (83014) | ||
| H3393-33K3911 H339333K3911 | 1560-01-445-8370 | Latch Assembly, Aircraft | Hartwell Corporation (83014) | ||
| H3393-34 H339334 | 1560-01-445-8379 | Latch Assembly, Aircraft | Boeing Company, The (88277) | ||
| H3393-34 H339334 | 1560-01-446-5823 | Latch Assy, Aircraft | Hartwell Corporation (83014) | ||
| H3393-34K3911 H339334K3911 | 1560-01-445-8379 | Latch Assembly, Aircraft | Hartwell Corporation (83014) | ||
| H3393-7 H33937 | 1560-01-415-7552 | Latch Assembly, Aircraft | III End Item Identification: C-17 aircraft | Hartwell Corporation (83014) | |
| H3397-5 H33975 | 1560-01-474-4390 | Strut Assembly, Access Door | III End Item Identification: SH-2G(A) seasprite helicopter Special Features: Mounting bushings at each end have 0.312-0.314 in. inside dia.; adjustable spherical male end with jam nut on rod end; opposite end is cone shaped, integral with housing; when extended overall length of strut is 19.950 in. on bushing centers, plus or minus 0.250 in.; when retracted overall length is 10.000 in. on bushing centers plus or minus 0.250 in.; non-locking strut III Part Name Assigned BY Controlling Agency: Aft strut assembly, engine access door | Hartwell Corporation (83014) | |
| H3402-1 H34021 | 1560-01-474-4392 | Strut Assembly, Engine Door | III End Item Identification: SH-2G(A) seasprite helicopter Special Features: Maximum retracted length 7.690 in. dia; inside of mounting bushings is 0.1895-0.1900 in. dia. both ends; width at each mounting end across bushing is 0.276-0.281 in. Overall Length: 11.970 inches maximum | Hartwell Corporation (83014) | |
| H3425-1 H34251 | 1560-01-475-5157 | Latch Assembly, Aircraft | III End Item Identification: SH-2G Special Features: Latch rotates 180 degrees; 4 mounting holes, one in each corner; holes are 0.218 in min and 0.223 in max Overall Length: 3.000 inches nominal | Hartwell Corporation (83014) | |
| H3425-11 H342511 | 1560-01-475-5159 | Keeper Assembly, Latch, Rotary | III End Item Identification: SH-2G Special Features: Nha pn K870359-001, latch assy-rotary hook; 2 mounting holes 0.218 in min 0.223 in max; distance between mounting hole center to hole center 1.000 in | Hartwell Corporation (83014) | |
| H3441-1 H34411 | 1560-01-475-6735 | Hinge, Aircraft | III End Item Identification: SH-2G Special Features: Nha pn K870302; assy consists of K870360-011 support and K870360-003 hinge assy; support stock size casting, material A356.0 Material Document and Classification: AMS4218 assn std single material response | Hartwell Corporation (83014) |