Airframe Structural Components: C4PM10312-6, C4PM10313-4, C4PM1424-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| C4PM10312-6 C4PM103126 | 1560-00-968-4734 | Hinge, Engine Cowling | III End Item Identification: Acft model C7A General Characteristics Item Description: Steel, bar, MIL-S-6758 4130 | Bombardier Aerospace Aerospace Div. (71867) | |
| C4PM10313-3 C4PM103133 | 1560-00-075-3369 | Arm Assembly, Cowl | General Characteristics Item Description: Aluminum alloy, QQ-A-367 | Bombardier Aerospace Aerospace Div. (71867) | |
| C4PM10313-4 C4PM103134 | 1560-00-075-3381 | Arm Assembly, Cowl | General Characteristics Item Description: Aluminum alloy, QQ-A-367, 6.025 in. lg | Bombardier Aerospace Aerospace Div. (71867) | |
| C4PM10314-6 C4PM103146 | 1560-00-073-0321 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-7A Material Document and Classification: QQ-A-225 fed spec single material response | Bombardier Aerospace Aerospace Div. (71867) | |
| C4PM10315-2 C4PM103152 | 1560-00-073-9796 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-7A | Bombardier Aerospace Aerospace Div. (71867) | |
| C4PM10315-4 C4PM103154 | 1560-00-073-9796 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-7A | Bombardier Aerospace Aerospace Div. (71867) DE Havilland Inc. (0HWZ3) | |
| C4PM10319-1 C4PM103191 | 1560-00-475-1991 | Spacer, Engine Control | III End Item Identification: Acft C-7A General Characteristics Item Description: Aluminum alloy QQ-A-267; outside dia. 2.250; aperture min dia 0.6245, max dia 0.6255; 0.250 W | Bombardier Aerospace Aerospace Div. (71867) | |
| C4PM10332-1 C4PM103321 | 1560-00-531-9847 | Holder, Heat Control | III End Item Identification: Acft model C7A General Characteristics Item Description: Aluminum alloy, bar 2024, T4, QQ-A-267, 1.200 in. W | Bombardier Aerospace Aerospace Div. (71867) | |
| C4PM1034-1 C4PM10341 | 1560-00-093-0224 | Plate, Seal, Oil Tank | General Characteristics Item Description: Aluminum alloy 2024, QQ-A-200/3 T4, 9.200 in. od, 0.045 in. thk O/a | Bombardier Aerospace Aerospace Div. (71867) | |
| C4PM10353-1 C4PM103531 | 1560-00-021-8993 | Block Swivel, Cowl Strut | General Characteristics Item Description: 0.375 in. dia hole thru center, 0.191 in. dia hole thru base 4 places, 1.360 in. W, 2.000 in. lg | Bombardier Aerospace Aerospace Div. (71867) | |
| C4PM10355-3 C4PM103553 | 1560-00-979-7525 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-7A Special Features: Matl:tap 0.312-24 UNF-2B thd thruend, 0.290IN. dia. hole thru side two places Aircraft Location: Strut top cowl | Bombardier Aerospace Aerospace Div. (71867) | |
| C4PM10355-5 C4PM103555 | 1560-00-979-7525 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-7A Special Features: Matl:tap 0.312-24 UNF-2B thd thruend, 0.290IN. dia. hole thru side two places Aircraft Location: Strut top cowl | Bombardier Aerospace Aerospace Div. (71867) | |
| C4PM10542-1 C4PM105421 | 1560-00-019-7984 | Tee Block | General Characteristics Item Description: Aluminum plate, QQ-A-200/3-T4, 2.00 in. lg, 1.500 in. W | Bombardier Aerospace Aerospace Div. (71867) | |
| C4PM10615-3 C4PM106153 | 1560-00-133-3908 | Plunger, Switch Operating, Propell | General Characteristics Item Description: Plastic, 0.500 in. lg, 0.250 in. dia head, 0.123 in. dia shank 0.400 in. lg | Bombardier Aerospace Aerospace Div. (71867) | |
| C4PM10689-1 C4PM106891 | 1560-00-442-9133 | Adapter, Engine Control | General Characteristics Item Description: Steel, MIL-S-6758, chrome-plated, 1.960 in. min, 1.970 in. max lg, 1.500 in. O/a dia, 0.6245 in. min, 0.6255 in. max dia of bore | Bombardier Aerospace Aerospace Div. (71867) DE Havilland Inc. (0HWZ3) | |
| C4PM1080-1 C4PM10801 | 1560-00-707-6897 | Connector Assembly | III End Item Identification: Aircraft model C-7 General Characteristics Item Description: First end, steel plate, 4130, MIL-S-18729, condition N, 0.150 in. thk, W/2 holes 0.199 in. dia, second end, steel tube, 4130, MIL-S-6758, condition D, 1.00-8N-2A thread on one end, other end welded to plate, 0.765 in. dia hole through center of assembly | Bombardier Aerospace Aerospace Div. (71867) | |
| C4PM1191-1 C4PM11911 | 1560-00-439-3698 | Adapter, Pressure Fuel Servicing | III End Item Identification: C-7A | Bombardier Aerospace Aerospace Div. (71867) DE Havilland Inc. (0HWZ3) | |
| C4PM1363-3 C4PM13633 | 1560-00-735-4470 | Hinge, Engine Cowling | III End Item Identification: Acft model C7A General Characteristics Item Description: 7.300 in. lg, 3 holes 0.562 in. dia | Bombardier Aerospace Aerospace Div. (71867) | |
| C4PM1363-5 C4PM13635 | 1560-00-859-2727 | Hinge, Engine Cowling | III End Item Identification: Acft model C7A General Characteristics Item Description: 7.300 in. lg, 3 holes 0.562 in. dia | Bombardier Aerospace Aerospace Div. (71867) | |
| C4PM1424-1 C4PM14241 | 1560-00-442-9141 | Cowling | Aircraft Mission Design Series: C-7A Special Features: U/a: cowling, hinge, support Overall Length: 6.200 inches nominal | Bombardier Aerospace Aerospace Div. (71867) |