CR | Aircraft Wing Repair Application and Parts List

CR - Tooling 3

CR Tooling Detail

Nominal Hole Size 1/4
Mandrel Tool Code R40
Start Hole Max 0.232
Start Hole Min 0.236
Final Hole Min 0.2460
Final Hole Max 0.2490
Start Drill 1 WCI-SD-R40
Start Reamer 2 WCI-SR-R40
Combination Gage WCI-CBG-R40
Mandrel Wear Gage WCIS-WG-R40
Mandrel3 WCI-CRM-R40-1-XX
Extension Nosecap 4 WCI-1700NE-R40-XX-F
Flush Nosecap 5 WCI-1700OAJ-R40
Sleeve 6 CRS-R40-XX *
Finish Reamer 7 WCI-FR-R40-2460
Optional Tooling
Start Hole Gage WCI-SHG-R40
Final Hole Gage 8 WCI-FHG-2460-2490

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1 Start Drill Add -C if cobalt
2 Start Reamer Add -C if cobalt
3 Mandrel
* = Attachment callout
1 = 7/16-20 used with 1700 puller to 16-3-N
2
= 5/8-18 used with 1800 puller, 10-3-N - 30-3-N
3 = .960 tang used with 1900 puller 32-0-N - 56-3-N
4 = 7/8-14 used with 1900 puller, 32-0-N - 56-3-N, 2 piece
5 = 7/8-14 used with 1800 puller
XX = Mandrel length in 1/10". Available in ½" increments
Add -V2 for high strength steel and titanium application

4 Extension Nosecap
XX = Extension length in 1/10". Available in ½" increments
**** = (Overlap between 1700 and 1800 pullers. Please specify)
5 Flush Nosecap
X = (F)lared or (S)traight sleeve
**** = (overlap between 1700 and 1800 pullers. Please specify)
6 Sleeve
XX = Sleeve length in 1/16"
* = (F)lared or (S)traight sleeve
7 Finish Feamer
XXXX = Final hole size in 1/10,000". Add -C if Cobalt
8 Final Hole Gage
**** = Go diameter
XXXX = No-Go diameter