Airframe Structural Components: 7-211654003, 7-211660009-3, 7-211660023
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
7-211654003 7211654003 | 1560-01-174-7283 | No Item Name Available | III End Item Identification: AH-64 airframe | Boeing Company, The (8V613) McDonnell Douglas Helicopter Co. Inc. (02731) | |
7-211654005 7211654005 | 1560-01-475-9830 | Cover Assy-Upr Otbd | III End Item Identification: AH-64 longbow | Boeing Company, The (8V613) | |
7-211654005-23 721165400523 | 1560-01-249-4012 | Doubler, Enclosure | Boeing Company, The (8V613) McDonnell Douglas Helicopter Co. Inc. (02731) | ||
7-211654005-25 721165400525 | 1560-01-186-4081 | Guide, Cover | Boeing Company, The (8V613) McDonnell Douglas Helicopter Co. Inc. (02731) | ||
7-211654005-27 721165400527 | 1560-01-249-8472 | Doubler, Enclousure | Boeing Company, The (8V613) McDonnell Douglas Helicopter Co. Inc. (02731) | ||
7-211654005-31 721165400531 | 1560-01-249-4013 | Doubler, Enclosure | Boeing Company, The (8V613) McDonnell Douglas Helicopter Co. Inc. (02731) Swift-COR Tool Engineering (21227) W and G Machine Company Incorporated (33682) | ||
7-211654005-37 721165400537 | 1560-01-249-4014 | Doubler, Enclosure | Boeing Company, The (8V613) McDonnell Douglas Helicopter Co. Inc. (02731) | ||
7-211654005-71 721165400571 | 1560-01-475-9830 | Cover Assy-Upr Otbd | III End Item Identification: AH-64 longbow | Boeing Company, The (8V613) | |
7-211654005-73 721165400573 | 1560-01-249-6714 | Cover Assy, top Encl | III End Item Identification: AH-64 airframe, rotary wing aircraft | Boeing Company, The (8V613) McDonnell Douglas Helicopter Co. Inc. (02731) | |
7-211654005-75 721165400575 | 1560-01-257-5779 | Cover Assy, Enclosur | Boeing Company, The (8V613) McDonnell Douglas Helicopter Co. Inc. (02731) | ||
7-211660009-3 72116600093 | 1560-01-170-7413 | Support, cable, Engine | General Characteristics Item Description: Al alloy, comp 2024-T351, spec QQ-A-25014, per mil A11-21180, wall thk 0.080 | Boeing Company, The (8V613) McDonnell Douglas Helicopter Co. Inc. (02731) | |
7-211660014 7211660014 | 1560-01-186-4071 | Bracket Assy, Suppor | Boeing Company, The (8V613) McDonnell Douglas Helicopter Co. Inc. (02731) | ||
7-211660016 7211660016 | 1560-01-170-6918 | Support Assy, Bell C | Boeing Company, The (8V613) McDonnell Douglas Helicopter Co. Inc. (02731) | ||
7-211660017-3 72116600173 | 1560-01-188-4523 | Support, Engine Air | General Characteristics Item Description: Sh al alloy, comp 6061-0, spec QQ-A-250/11, O/a width 1.950 in. O/a lg 2.840 in. | Boeing Company, The (8V613) McDonnell Douglas Helicopter Co. Inc. (02731) | |
7-211660018-13 721166001813 | 1560-01-186-4072 | Flange Assy, Bracket | Boeing Company, The (8V613) McDonnell Douglas Helicopter Co. Inc. (02731) | ||
7-211660018-15 721166001815 | 1560-01-186-4073 | Flange Assy, Bracket | Boeing Company, The (8V613) McDonnell Douglas Helicopter Co. Inc. (02731) | ||
7-211660018-19 721166001819 | 1560-01-186-4074 | Support Assy, Bracke | Boeing Company, The (8V613) McDonnell Douglas Helicopter Co. Inc. (02731) | ||
7-211660019 7211660019 | 1560-01-172-5037 | Support, Engine Disconnect | General Characteristics Item Description: Al alloy, comp 6061-0, spec QQ-A-250/11, 0.040 in. thk, O/a lg. 3.970 | Boeing Company, The (8V613) McDonnell Douglas Helicopter Co. Inc. (02731) | |
7-211660022 7211660022 | 1560-01-172-5077 | Support, Engine Control | General Characteristics Item Description: Aluminum alloy, QQ-A-250/4, comp 2024-0;0.040 in. wall THICKNESS;4.860 in. O/a LG;2.320 in. O/a w; 2 holes drilled 0.193 in. min, 0.203 in. max dia, spaced 1.200 in. C to C along W Test Data Document: 02731-7-211660022 drawing (this is the basic governing drawing, such as a contractor drawing, original equipment manufacturer drawing, etc.; excludes any specification, standard or other document that may be referenced in a basic governing drawing) | Boeing Company, The (8V613) McDonnell Douglas Helicopter Co. Inc. (02731) | |
7-211660023 7211660023 | 1560-01-172-8051 | Bracket Assy, Engine | General Characteristics Item Description: Base measurements 3.310 in. lg; 1.000 in. W;1 hole ea end drilled 0.203 to 0.209 in. deep;plate measurement 2.350 in. lg;w 2 holes drilled 0.570 to 0.586 in. deep;w rivet holes spaced 0.400 in. C to c;matl aluminum alloy, QQ-A-250/4, comp 2024-T3 Test Data Document: 02731-7-211660023 drawing (this is the basic governing drawing, such as a contractor drawing, original equipment manufacturer drawing, etc.; excludes any specification, standard or other document that may be referenced in a basic governing drawing) | Boeing Company, The (8V613) McDonnell Douglas Helicopter Co. Inc. (02731) |