1224 East Warner Ave,
Santa Ana, Ca 92705
Tel: 1-714-545-5511
www.cherryaerospace.com
TS-H753A-456 Rev: B Date: 17 Aug 10 DCR#: 10-0928
H753A-456
RIGHT ANGLE PULLING HEAD
INSTRUCTION SHEET
REF.
NO.
PART
NUMBER
DESCRIPTION
QTY
1 753B12
Sleeve
1
2 G6JN
Jam
Nut
1
3* 753A13A Collet
1
4 701B18
Jaws
1
set
5 753A14A Jaw
Follower
1
6 P293
0-ring 1
7 P-1003 Spring
1
8 753A15
Stem
Stop
1
9 P706
0-ring 2
10 753C2-3 Frame
1
11 753A4
Shoe
Bearing
2
12* 753B3
Collet
Bolt
1
13 753B5
Lever
1
14 P-413
Button Head Screw
1
15 P-930 Set
Screw
2
16 753A16
Guard
1
17 753A10
Pivot
Pin
2
18 P954
Link
8
19 753A9
Link
Pin
4
20 753B6
Bell
Crank
1
21 753A11
Guide
Pin
1
22 753A7
Drawbolt
1
23 753B8
Adapter
Fitting
1
24 671A16
Jam
Nut
1
MAINTENANCE AND REPAIR
Keep the pulling head clean, especially around the
riveting end, as adhesives, chips, sealants, etc., may
cause slippage of the rivet stem.
To disassemble pulling head: Loosen jam nut (2) and
remove sleeve (1). Unscrew collet (3) which contains jaws
(4), jaw follower (5), 0-ring (6), spring (7), stem stop (8)
and 0-rings (9) from collet bolt (12).
Remove screw (14) and guard (16). Remove 2 set
screws (15) and push out 2 pivot pins (17) to permit
removal of linkage. Shoe bearings (11) and collet bolt
(12) will disengage from lever (13).
Remove 4 link pins (19) to disassemble lever (13), links
(18), bell crank (20) and drawbolt (22).
Remove guide pin (21) from frame (10). Adapter fitting
(23) is secured to frame with Loctite and need not be
removed unless damaged.
To re-assemble: Reverse the procedure. Linkage,
consisting of lever (13), links (18), link pins (19), bell
crank (20) and drawbolt (22) should be assembled as a
sub- assembly before inserting lever (13) into shoe
bearings (11) and collet bolt (12). This complete sub-
assembly may then be inserted into frame (10) and
retained by guide pin (21) and pivot pins (17).
*Use Loctite 242 or equivalent when assembling items 3 and 12
WARRANTY
Seller warrants the goods conform to applicable specifications and drawings and will be manufactured and inspected according to generally accepted practices of companies manufacturing industrial or aerospace
fasteners. In the event of any breach of the foregoing warranty, Buyer’s sole remedy shall be to return defective goods (after receiving authorization from Seller) for replacement or refund of the purchase price, at
the Seller’s option. Seller agrees to any freight costs in connection with the return of any defective goods, but any costs relating to removal of the defective or nonconforming goods or installation of replacement
goods shall be Buyer’s responsibility. SELLER’S WARRANTY DOES NOT APPLY WHEN ANY PHYSICAL OR CHEMICAL CHANGE IN THE FORM OF THE PRODUCT IS MADE BY BUYER. THE
FOREGOING EXPRESS WARRANTY AND REMEDY ARE EXCLUSIVE AND ARE IN LIEU OF ALL OTHER WARRANTIES AND REMEDIES; ANY IMPLIED WARRANTY AS TO QUALITY, FITNESS FOR PURPOSE, OR
MERCHANTABILITY IS HEREBY SPECIFICALLY DISCLAIMED AND EXCLUDED BY SELLER. This warranty is void if seller is not notified in writing of any rejection of the goods within ninety (90) days after receipt of
the goods by buyer.
Seller shall not be liable under any circumstances for incidental, special or consequential damages arising in whole or in part from any breach by Seller, AND SUCH INCIDENTAL, SPECIAL, OR CONSEQUENTIAL
DAMAGES ARE HEREBY EXPRESSLY EXCLUDED.
Our policy is one of continuous development. Specifications shown in this document may be subject to changes introduced after publication.
NOTE: The properties, strength, dimensions, installed characteristics and all other information in these materials are for guidance only to aid in the correct selection
of the products described herein and is not intended or implied as part of the above warranty. All applications should be evaluated for functional stability and available
samples of the described parts can be requested for installed tests, suitability and evaluations.
For more information please contact our Technical Services Department at tel. 714-850-6022
