Part Number : R-TBD-696 | Manufacturer : Boeing Company The | ||
NSN : 4920-01-168-1312 (4920011681312) | |||
Item Name : Tester Load Applica | CAGE Code : 43999 | ||
NIIN : 01-168-1312 (011681312) | |||
FSC Code : 4920 Aircraft Maintenance And Repair Shop Specialized Equipment | |||
FSG Code : 49 Maintenance And Repair Shop Equipment | |||
INC Code : 77777 | |||
NCB Code : 01 | Country : USA | ||
Alternate P/N: RTBD696 |
Thank you for taking an interest in part number R-TBD-696, that of which is listed with the description Tester Load Applica; Manufactured by Boeing Company The and listed alongside the NSN 4920011681312, part number R-TBD-696 is available for immediate purchase on our website. As such, to learn more about this offering while receiving a competitive quote for your comparisons, be sure to fill out and submit the RFQ form presented on this page. Within 15 minutes of us receiving and reviewing a completed form, a member of our staff will contact you to present a tailored solution for your comparisons.
Part Number : R-TBD-696 | Manufacturer : Boeing Company The | ||
NSN Number : 4920-01-168-1312 (4920011681312) | |||
Item Name : Tester Load Applica | CAGE Code : 43999 | ||
NIIN : 011681312 | |||
FSC CODE : 4920 Aircraft Maintenance And Repair Shop Specialized Equipment |
Thank you for taking an interest in part number R-TBD-696, that of which is listed with the description Tester Load Applica; Manufactured by Boeing Company The and listed alongside the NSN 4920011681312, part number R-TBD-696 is available for immediate purchase on our website. As such, to learn more about this offering while receiving a competitive quote for your comparisons, be sure to fill out and submit the RFQ form presented on this page. Within 15 minutes of us receiving and reviewing a completed form, a member of our staff will contact you to present a tailored solution for your comparisons.
MRC | Criteria | Characteristic |
---|---|---|
FTLD | Functional Description | USED TO PERFORM HATCH UNLATCH LOADING TEST PRIOR TO INSTALLING THE AFT HATCH REMOVER; APPLICATOR WILL PROVIDE A MAXIMUM FORCE OF 100.000 LBS TO IDLER ARM AT THE THRUSTER ATTACH POINT,TO UNLATCH AFT ESCAPE HATCH LOCKING SYSTEM |
AGAV | End Item Identification | B-1B AIRCRAFT AGE. |
CXCY | Part Name Assigned By Controlling Agency | LOAD APPLICATOR TESTER |
MRC | Decoded Requirement | Clear Text Reply |
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