Physical Properties Testing and Inspection: 17G110079-1, 17G110659-1, 17G110854-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 17G110079-1 17G1100791 | 6635-01-458-4540 | Reference Standard, Physical Prop | Special Features: Reference standard finish is A similar elastomer erosion coating and paint that closely matches the aircraft design finish; operating temperature -40 to 125 deg F END Item Identification: C-17 ndi support Part Name Assigned BY Controlling Agency: Reference standard carbon epoxy to syncore | Boeing Company, The (88277) | |
| 17G110433-1 17G1104331 | 6635-01-458-5339 | Reference Standard, Physical Prop | Special Features: Reference standard finish, A similar elastomer erosion coating and paint that closely matches the aircraft design finish; operating temperature -40 to 125 deg F END Item Identification: C-17 ndi support Part Name Assigned BY Controlling Agency: Reference standard, carbon skin to nomex core | Boeing Company, The (88277) | |
| 17G110483-1 17G1104831 | 6635-01-458-4538 | Reference Standard, Physical Prop | Special Features: Reference standard finish, A similar lastomer erosion coating and paintthat closely matches the aircraft design finish; operating termperature -40 to 125 degree F END Item Identification: C-17 ndi support Part Name Assigned BY Controlling Agency: Kit, reference standard, solid laminate, carbon epoxy | Boeing Company, The (88277) | |
| 17G110484-1 17G1104841 | 6635-01-458-4537 | Reference Standard, Physical Prop | Special Features: Reference standard finish, A similar elastomer erosion coating and paint that closely matches the aircraft design finish; operating temperature -40TO 125 deg F END Item Identification: C-17 ndi support Part Name Assigned BY Controlling Agency: Reference standard, solid laminate, aramid epoxy | Boeing Company, The (88277) | |
| 17G110485-1 17G1104851 | 6635-01-458-4543 | Reference Standard, Physical Prop | Special Features: Reference standard finish, A similar elastomer erosion coating and paint that closely matches the aircraft design finish; operating temperature -40 to 125 deg F END Item Identification: C-17 ndi support Part Name Assigned BY Controlling Agency: Reference standard carbon epoxy secondary bond | Boeing Company, The (88277) | |
| 17G110486-1 17G1104861 | 6635-01-458-4545 | Reference Standard, Physical Prop | Special Features: Reference standard finish, A similar elastomer erosion coating and paint that closely matches the aircraft design finish; operating temperature -40 to 125 deg F END Item Identification: C-17 ndi support Part Name Assigned BY Controlling Agency: Reference standard glass skin to nomex core | Boeing Company, The (88277) | |
| 17G110487-1 17G1104871 | 6635-01-458-4539 | Reference Standard, Physical Prop | Special Features: Reference standard finish, A similar elastomer erosion coating and paint that closely matches the aircraft design finish; operating temperatures -40 to 125 deg F END Item Identification: C-17 ndi support Part Name Assigned BY Controlling Agency: Reference standard carbon skin torohacell | Boeing Company, The (88277) | |
| 17G110488-1 17G1104881 | 6635-01-458-4541 | Reference Standard, Physical Prop | Special Features: Reference standard finish, A similar elastomer erosion coating and paint that closely matches the aircraft design finish; operating temperature -40 to 125 deg F END Item Identification: C-17 ndi support Part Name Assigned BY Controlling Agency: Reference standard carbon skin patch/paste adhesive | Boeing Company, The (88277) | |
| 17G110489-1 17G1104891 | 6635-01-458-4542 | Reference Standard, Physical Prop | Special Features: Reference standard finish, A similar elastomer erosion coating and paint that closely matches the aircraft design finish; operating temperature -40 to 125 deg F END Item Identification: C-17 ndi support Part Name Assigned BY Controlling Agency: Reference standard carbon dry fabric/paste adhesive | Boeing Company, The (88277) | |
| 17G110496-1 17G1104961 | 6635-01-496-0946 | Reference Standard, Physical Prop | Boeing Company, The (88277) | ||
| 17G110627-1 17G1106271 | 6635-01-522-5880 | Reference Standard, Physical Prop | Special Features: Material stitched; carbon epoxy; painted finish; color gray; operating temperature minus 40 degrees F to 125 degrees F END Item Identification: C17-A aircraft General Characteristics Item Description: Used to establish calibration of the baseline that represents the material thickness being inspected | Boeing Company, The (88277) | |
| 17G110645-1 17G1106451 | 6635-01-535-4582 | Reference Standard, Physical Prop | Special Features: Material aluminum, finish painted gray, operating temps -40 deg F to 125 deg f; manufacturers name reference standard, metal to core - aluminum END Item Identification: C-17 aircraft Overall Length: 6.000 inches nominal | Boeing Company, The (88277) | |
| 17G110650-1 17G1106501 | 6635-01-535-4583 | Reference Standard, Physical Prop | Special Features: Material aluminum, finish painted, gray, operating temps -40 deg F to 125 deg f; manufacturer name reference standard, metal to metal - aluminum END Item Identification: C-17 aircraft Overall Length: 6.000 inches nominal | Boeing Company, The (88277) | |
| 17G110659-1 17G1106591 | 6635-01-573-2014 | Reference Standard, Physical Prop | Special Features: Material stitched carbon epoxy;painted gray;operating temp -40DEG F to 125DEG f;weight 1LBS END Item Identification: C-17 aircraft Part Name Assigned BY Controlling Agency: Reference standard | Boeing Company, The (88277) | |
| 17G110828-1 17G1108281 | 6635-01-407-6272 | Reference Standard, Physical Prop | END Item Identification: C-17 ndi support Part Name Assigned BY Controlling Agency: Reference standard carbon epoxy to syncore Overall Length: 25.000 inches nominal | Boeing Company, The (88277) | |
| 17G110841-1 17G1108411 | 6635-01-407-1501 | Reference Standard, Physical Prop | END Item Identification: C-17 ndi support Part Name Assigned BY Controlling Agency: Reference standard carbon epoxy secondary bond Overall Length: 25.000 inches nominal | Boeing Company, The (88277) | |
| 17G110842-1 17G1108421 | 6635-01-407-1504 | Reference Standard, Physical Prop | END Item Identification: C-17 nid support Part Name Assigned BY Controlling Agency: Reference standard glass skin to nomex core Overall Length: 21.000 inches nominal | Boeing Company, The (88277) | |
| 17G110843-1 17G1108431 | 6635-01-407-1502 | Reference Standard, Physical Prop | General Characteristics Item Description: Uainreference standard, glass skin; reference standard consists of two blocks of composite material; each block is contructed of laminate skins bonded to each side of approximately 0.5 in. thick glass honeycomb core material; one block top skin is contructed of steps 4 & 5 plies and A bottom skin of 3 plies; second block constructed of top skin 7 & 8 plies and bottom skin 6 plies; 5 in. H, 15 in. W, 15 in. d; 5 lbs. | Boeing Company, The (88277) | |
| 17G110853-1 17G1108531 | 6635-01-407-1505 | Reference Standard, Physical Prop | General Characteristics Item Description: Uain reference stamdard, solid laminate; reference standard is constructed from glass epoxy solid laminate in the form stepped wedge ranging from 2 to 28 pliesof glass cloth and epoxy adhesive cured together to form solid rectangular block maeterial; block contains six steps starting with two plies and then 4, 8, 12, 16, 20, 24 and 28; 0.5 in. H, 5 in. W, 20 in. w; 20 lbs. | Boeing Company, The (88277) | |
| 17G110854-1 17G1108541 | 6635-01-407-6271 | Reference Standard, Physical Prop | END Item Identification: C-17 ndi support Part Name Assigned BY Controlling Agency: Reference standard carbon skin to rohacell Overall Length: 21.000 inches nominal | Boeing Company, The (88277) |