Product Information

QR
Structural Panel Fasteners
The QR Strucutral Panel Fastener qualifies to MIL-F-22978 and meets
MS17731 and MS17732. The QR fastening system is lightweight, has
a small envelope and is fast operating. Most versions lock and unlock
in less than two turns. Positive stud retention is featured. Flush or
protruding head styles and various recess configurations are available. Optional stud hold-out grommet is available which provides
bottom flush condition. Receptacle provides .020 inch minimum radial
float. There are other QR Panel Fastener styles and types which are
not featured in this catalog; contact Fairchild Fasteners for details.
Typical QR Fastening System:
Stud assembly is retained in retracted position
by sprint-loaded grommet and retaining ring.
The QR Fastening System has a high-strength-to-weight ratio.
Quick operating, it locks and unlocks in less than two turns.
Optional stud hold-out grommet is available which provides
bottom flush condition.
Stud assembly is automatically ejeted free
from sub-structure during unlocking cycle.
Fairchild Fasteners
Tridair Products 64
QR
‘MS’ Version
To Install FX10-1525 Retaining Ring:
1. Slide retaining ring
onto mandrel (Figures A
and B).
2. Slide handle onto
mandrel (Figure C).
Retaining Ring
Standard Version
FX10-1525
Material:
18-8 Type 300 Series CRES per
AMS 7245 or QQ-W-423.
Heat Treat:
Stressed relieved.
Finish:
Passivated per QQ-P-35.
Weight:
.033 lbs./100, approximate.
3. Place anvil on top side of panel to brace stud assembly.
Installation Tool for FX10-1525 Retaining Ring:
FX10-1530T
Material: Alloy Steel
Finish: Black Oxide per MIL-C-13924
4. Align tool assembly onto stud
assembly and push on handle until
retaining ring is captivated to the
stud assembly (Figures D and E).
5. Remove tool.
Retaining Ring
Oversize Version.
FX10-1576
Material: 17-7Ph CRES per AMS 5528.
Heat Treat: Rc 44-48.
Finish: Passivated per QQ-P-35.
Weight: .043 lbs./100, approximate.
Notes:
1. Ring is designed to be used when hole in substructure is
.391 or greater. See hole preparation on Page 69.
2. FX10-1576 retaining ring is hand installed.
Fairchild Fasteners
Tridair Products 65
QR
Standard Version
Stud Assemblies
Flush Head Style.
FX10-1558-( )( ) Series
Protruding Head Style.
FX10-1559-( )( ) Series
Material:
Screw: 8740 Alloy Steel per MIL-S-6049.
Grommet: 4140 Alloy Steel per MIL-S-5626.
Spring: 17-7PH CRES per AMS 5673.
Heat Treat:
Screw and Grommet: 160 K.S.I. minimum ultimate tensile
strength per MIL-H-6875.
Spring: Condition CH900 per MIL-H-6875.
Finish:
Screw and Grommet: Cadmium Plated per QQ-P-416, Type
II, Class 3.
Spring: Passivated per QQ-P-35.
Specifications: See Page 2.
B a si c
Stud Assembly
Part No.
A
Ref.
FX10-1558-1( )
FX10-1558-2( )
Grip Range
B
Ref.
Min.
.35
.41
.150
.220
.010
.42
.48
.221
.290
.013
Max.
Weight
lbs./ea.
FX10-1558-3( )
.49
.55
.291
.360
.015
FX10-1558-4( )
.56
.62
.361
.430
.017
.019
FX10-1558-5( )
.63
.69
.431
.500
FX10-1558-6( )
.70
.76
.501
.570
.021
FX10-1558-7( )
.77
.83
.571
.640
.023
FX10-1558-8( )
.84
.90
.641
.710
.025
FX10-1558-9( )
.91
.97
.711
.780
.027
FX10-1558-10( )
.98
1.04
.781
.850
.029
FX10-1558-11( )
1.05
1.11
.851
.920
.031
B a si c
Stud Assembly
Part No.
A
Ref.
B
Ref.
Min.
Max.
Weight
lbs./ea.
FX10-1559-1( )
.35
.53
.116
.185
.015
Grip Range
FX10-1559-2( )
.42
.60
.186
.255
.017
FX10-1559-3( )
.49
.67
.256
.325
.019
FX10-1559-4( )
.56
.74
.326
.395
.021
FX10-1559-5( )
.63
.81
.396
.465
.023
FX10-1559-6( )
.70
.88
.466
.535
.025
FX10-1559-7( )
.77
.95
.536
.605
.027
FX10-1559-8( )
.84
1.02
.606
.675
.029
FX10-1559-9( )
.91
1.10
.676
.745
.031
Notes:
1. Anti-seize compound per MIL-A-907 applied to thread.
2. For retaining ring information see Page 65.
How to Order:
FX10 — 1558 — 4 P
Recess options:
p = recess per MS9006,
No. 10 size
TS = recess per NAS1078,
No. 10 size
Grip range: (see stud part number
selection Page 8 for grip range
requirements)
FX10-1558-4 = .361 to .430
FX10-1559-4 = .326 to .395
Head style:
FX10-1558 = Flush head style
FX10-1559 = Protruding head style
Fairchild Fasteners
Tridair Products 66
QR
Standard Version
Stud Assembly
Receptacle Assemblies
Fully Retractable Flush Head Style.
FX10-15010-( )P Series
FX10-1502( ) Series
FX10-1510( ) Series
Stud Assembly
Part No.
A
Ref.
B
Ref.
FX10-15010-1P
.42
FX10-15010-2P
.49
Grip Range
Weight
lbs./ea.
Min.
Max.
.41
.230
.290
.013
.48
.291
.360
.015
FX10-15010-3P
.56
.55
.361
.430
.017
FX10-15010-4P
.63
.62
.431
.500
.019
FX10-15010-5P
.70
.69
.501
.570
.021
Material:
Screw: 8740 Alloy Steel per MIL-S-6049.
Grommet: 4140 Alloy Steel per MIL-S-5626.
Heat Treat:
Screw and Grommet: 160 K.S.I. minimum ultimate tensile
strength per MIL-H-6875.
Finish:
Screw and Grommet: Cadmium Plated per QQ-P-416, Type
II, Class 3.
Specifications: See Page 2.
Notes:
1. Use with FX10-15009 hold-out grommet (see Page 6) to
provide flush condition on bottom side of panel in retracted
position, and with FX10-1502( ) Series or FX10-1510( )
Series receptacle. Retaining ring is not required.
2. Anti-seize compound per MIL-A-907 applied to thread.
3. For stud part number selection see Page 8.
4. For other head styles and recesses, contact Fairchild
Fasteners.
Fairchild Fasteners
Locking
Feature
Part No.
A*
Ref.
High**
Prevailing
Torque
FX10-1502
None
FX10-1502-05
.03
FX10-1502-08
.08
FX10-1510
None
Eliptical
FX10-1510-05
.03
FX10-1510-08
.08
Lubricant
Coating
Per MIL-L-25681
Per MIL-A-907
*“A” dimension, when .03 or .08, provides extra jackout to allow
stud hold-out spring to engage panel.
**Locking feature maintains 5 inch pounds minimum running torqueout after 200 complete cycles.
Material:
Receptacle: 1050 Steel per ASI C1050.
Nut: 8740 Alloy Steel per MIL-S-6049.
Insert: 4140 Alloy Steel per MIL-S-5626.
Heat Treat:
Receptacle: Ftu 150 K.S.I. minimum per MIL-H-6875.
Nut: Ftu 180 K.S.I. minimum per MIL-H-6875.
Insert: Ftu 160 K.S.I. minimum MIL-H-6875.
Finish:
Receptacle, Nut, and Insert: Cadmium Plated per QQ-P416, Type II, Class 3.
Weight: .016 lbs. each, approximate.
Tridair Products 67
QR
Structural Panel Fasteners
Hold-Out Grommet
FX10-15009-( ) Series
Material:
Grommet: 18-8 Type 300 Series
CRES per ASTM-A-582.
Spring: 17-7PH CRES per AMS 5673.
Notes:
1. Use grommet with FX10-15010-( )P Series stud
assembly and FX10-1502 Series or FX10-1510
Series receptacles.
2. First and second oversize styles are designed to
provide greater strength or replacement of basic style
due to panel damage.
3. See Page 71 for hole preparation and installation
information.
Heat Treat:
Grommet: None.
Spring: Condition CH900.
Finish:
Grommet and Spring: Passivated
per QQ-P-35.
D escri pti on
Part No.
A
Theo.
Sharp
D
D i a.
E
Ref.
.630
Max.
.500
Ref.
.050
.655
Max.
.515
Ref.
.056
.692
Max.
.530
Ref.
.066
FX10-15009-1
B a si c
FX10-15009-2
1 st
Oversi ze
2nd
Oversi ze
FX10-15009-3
FX10-15009-4
FX10-15009-5
FX10-15009-6
Flari ng Tool
Back-up
Tool
Stud
Installati on Tool
FX10-15009-T10
FX10-15009-T12
FX10-15009-T13
FX10-15009-T14
FX10-15009-T15
FX10-15009-T16
.159
.128
FX10-15009-T11
.159
.128
.159
Back-Up Tool
FX10-15009-T( ) Series
Part No.
A
D i a.
FX10-15009-T10
.469
.467
FX10-15009-T13
.484
.482
FX10-15009-T15
.500
.498
Stud Assembly Installation Tool
FX10-15009-T11
Used to install FX10-15010-( )P Series stud assembly into
FX10-15009-( ) grommet assembly.
Fairchild Fasteners
G
Ref.
.128
Flaring Tool
FX10-15009-T( ) Series
Material:
Tool Steel
Heat Treat:
Rc45 min. per
MIL-H-6875
Finish:
Black Oxide per
MIL-C-13924
Installati on Tools (see below)
Material:
Tool Steel
Heat Treat:
Rc45 min. per MIL-H-6875
Finish:
Black Oxide per MIL-C-13924
Part No.
A
D i a.
Ref.
FX10-15009-T12
.610
.590
FX10-15009-T14
.640
.620
FX10-15009-T16
.665
.645
Material:
Tool Steel
Heat Treat:
Rc45 min. per MIL-H-6875
Finish:
Black Oxide per MIL-C-13924
Tridair Products 68
QR
Structural Panel Fasteners
Panel/Substructure Preparation and Installation Data.
Protruding Head Styles.
Flush Head Styles.
Notes:
1. Refer to table at left.
Application
A D i a.
B D i a.
Retaining Ring
Part No.
Basic Installation
.378
.375
.536
.526
FX10-1525
2. Locate and drill “A” diameter hole through panel and
substructure.
When curvature of
panel is 18 inches
or less*
.395
.391
.630
.620
FX10-1576
3. Counterbore to “B” diameter backside of panel or
*Subject to approval of structures group.
.035
frontside of substructure to .030
deep. Location is optional
when “T1” = .065 or greater. Otherwise counterbore substructure (Panel is preferred location).
Notes:
1. Locate and drill “A” diameter hole through panel and
substructure.
101°
.540
2. Countersink panel 99 to .530 diameter.
°
4. Locate, drill and countersink two holes for rivets (not
supplied).
5. Shim is required when total thickness (“T1”+”T2” plus any
compressed gasketing material, paint or other finishes)
equals .155 or less. Contact Fairchild Fasteners for details.
3. Counterbore to “B” diameter backside of panel or
frontside of substructure to .035 deep. Location is
.030
optional when “T1” = .125 or greater. Otherwise
counterbore substructure (panel is preferred location).
4. Locate, drill and countersink two holes for rivets (not
supplied).
5. Shim is required when total thickness (“T1” + “T2” plus
any compressed gasketing material, paint or other finishes)
equals .155 or less. Contact Fairchild Fasteners for details.
Basic Installation.
Notes:
1. Place stud assembly into panel.
2. Install retaining ring (see Page 3).
3. Rivet receptacle in place.
Fairchild Fasteners
Tridair Products 69
QR
Structural Panel Fasteners
Panel/Substrucutre
Preparation and Installation Data (cont’d.).
°
Grommet
FX10-15010-( )P Series.
Grommet Assembly
Part No.
Ref.
T1
Panel
Thickness
FX10-15009-1
.125
FX10-15009-2
.156
FX10-15009-3
.125
FX10-15009-4
.156
FX10-15009-5
.125
FX10-15009-6
.156
Notes:
1. Select grommet dash number to panel “T1” thickness.
2. Locate and drill “H” diameter hole through panel.
3. Countersink top of panel 99 °° to “J” diameter.
101
H
J
K
.5020
.4995
.635
.630
.146
.5175
.5150
.660
.655
.146
.5335
.5310
.697
.692
.146
5. Locate and drill .378
.375
.110
.110
.110
diameter hole through substructure.
6. Locate and drill two holes for rivets (not supplied).
4. Counersink bottom of panel 99 ° to “K” depth.
°
101
Stud Assembly and Grommet Assembly
Installation
6. Rivet receptacle in place.
7. Installation is complete.
Notes:
1. Place correct size grommet assembly in panel.
2. Place correct size flaring
tool and back-up tool in place
and apply sufficient pressure
to flare grommet.
3. Insert pilot of stud installation tool into thread end of stud
assembly.
4. Push tool and stud assembly through grommet until stud
is captivated by hold-out spring.
5. Remove tool.
Fairchild Fasteners
Stud Part Number Selection
Notes:
1. Determine grip range thickness. Note: Grip range
thickness equals “T1” + “T2” plus the compressed
thickness of any gasket (if used). Also allow for paint or
other finish thickness.
2. Refer to appropriate table for stud type and style
(see Pages 2, 4 or 5).
3. Locate grip range in table and find the corresponding
part no.
Tridair Products 70
QR
Structural Panel Fasteners
Panel/Substrucutre
Preparation and Installation Data (cont’d.).
°
Grommet
FX10-15009-( )P Series.
Grommet Assembly
Part No.
Ref.
T1
Panel
Thickness
FX10-15009-1
.125
FX10-15009-2
.156
FX10-15009-3
.125
FX10-15009-4
.156
FX10-15009-5
.125
FX10-15009-6
.156
Notes:
1. Select grommet dash number to panel “T1” thickness.
2. Locate and drill “H” diameter hole through panel.
3. Countersink top of panel 99 °° to “J” diameter.
101
H
J
K
.5020
.4995
.635
.630
.146
.5175
.5150
.660
.655
.146
.5335
.5310
.697
.692
.146
5. Locate and drill .378
.375
.110
.110
.110
diameter hole through substructure.
6. Locate and drill two holes for rivets (not supplied).
4. Counersink bottom of panel 99 ° to “K” depth.
°
101
Stud Assembly and Grommet Assembly
Installation
6. Rivet receptacle in place.
7. Installation is complete.
Notes:
1. Place correct size gromet assembly in panel.
2. Place correct size flaring
tool and back-up tool in place
and apply sufficient pressure
to flare grommet.
3. Insert pilot of stud installation tool into thread end of stud
assembly.
4. Push tool and stud assembly through grommet until stud
is captivated by hold-out spring.
5. Remove tool.
Fairchild Fasteners
Stud Part Number Selection
Notes:
1. Determine grip range thickness. Note: Grip range
thickness equals “T1” + “T2” plus the compressed
thickness of any gasket (if used). Also allow for paint or
other finish thickness.
2. Refer to appropriate table for stud type and style
(see Pages 2, 4 or 5).
3. Locate grip range on stud assembly drawing and find the
corresponding part dash no.
Tridair Products 71
THIS PAGE INTENTIONALLY LEFT BLANK
72
D RAWING BY
LTWH
D ATE:
3-4-80
APPROVED BY
D ATE:
3-31-80
APPROVED BY
D ATE:
4-1-80
APPROVED BY: D ATE:
PROJEC T
NUMBER
.345
-2[ ]
MAX.
.530
.116
.185
.015
.415
.600
.186
.255
.017
-3[ ]
.485
.670
.256
.325
.019
-4[ ]
.555
.740
.326
.395
.021
-5[ ]
.625
.810
.396
.465
.023
-6[ ]
.695
.880
.466
.535
.025
-7[ ]
.765
.950
.536
.605
.027
-8[ ]
.835
1.020
.606
.675
.029
-9[ ]
.905
1.100
.676
.745
.031
11/18/80
-1[ ]
WEIGHT
LBS/EA
MIN.
EC O
11-258
NUMBER
B
2-4-80
E
JWN
GRIP RANGE
A
REVISION R RED RAWN
D ASH
TITLE
SC REW ASSY, QR
UNLESS OFHER RANGE SPEC IFIED
TOLERANC ES
D EC IMALS
XX = .02
XXX = .020
ANGLES
= 2°
Fairchild Fasteners
MILLIMETERS
.050
.025
SURFAC E FINISH
125 MIC ROINC HES
3016 West Lomit Boulevard
Torrance, CA 90505 USA
909-947-3366
FX10-1559-00
F S C : 29372
SHEET 1 OF
2
Tridair Products 73
INSTALLATION
HOLD-OUT POSITION
PANEL PREPARATION
NOTES:
MATERIAL:
SCREW: 8740 ALLOY STEEL PER MIL-S-6049.
GROMMET: 4140 ALLOY STEEL PER MIL-S-5626
SPRING: 17-7 PH CRES PER AMS 5673.
2.
2.1
2.2
HEAT TREAT:
SCREW AND GROMMET: 160 K.S.I. MINIMUM ULTIMATE TENSILE STRENGTH PER
MIL-H-6875.
SPRING: CONDITION CH900 PER MIL-H-6875.
3.
3.1
3.2
FINISH:
SCREW AND GROMMET: CADMIUM PLATE PER QQ-P-416, TYPE II, CLASS 3.
SPRING: PASSIVATE PER QQ-P-35.
4.
.375 DIAMETER HOLE IN T2 MAY BE ENLARGED TO .390 DIAMETER (MAXIMUM) TO ALLOW FOR HOLE
MISALIGNMENT.
5.
5.1
5.2
RECESS OPTIONS AND CALLOUTS:
MS9006 RECESS: ADD “P” AFTER DASH NUMBER. EXAMBLE: FX10-1559-2P
NAS1078 RECESS: ADD “TS” AFTER DASH NUMBER. EXAMPLE: FX10-1559-2TS.
6.
ANTI-SEIZE COMPOUND PER MIL-A-907 APPLIED TO THREAD.
D RAWING BY
JWH
D ATE:
3-4-80
APPROVED BY
D ATE:
3-31-80
APPROVED BY
D ATE:
4-1-80
APPROVED BY: D ATE:
PROJEC T
NUMBER
REVISION D RED RAWN
DRAWING PROVIDES FORM, FIT
AND FUNTION DATA. DO NOT
ATTEMPT TO MANUFACTURE
PRODUCT USING THIS DRAWING.
3-4-80
E
JWH
EC O
16258
11/18/86
1.
1.1
1.2
1.3
TITLE
SC REW ASSY, QR
UNLESS OFTHER RANGE SPEC IFIED
TOLERANC ES
D EC IMALS
XX = .02
XXX = .020
ANGLES
= 2°
Fairchild Fasteners
MILLIMETERS
.050
.025
SURFAC E FINISH
125 MIC ROINC HES
3016 West Lomit Boulevard
Torrance, CA 90505 USA
909-947-3366
FX10-1559-00
F S C : 29372
SHEET 2 OF
2
Tridair Products 74
D RAWING BY
JWH
D ATE:
2-28-80
APPROVED BY
D ATE:
3-31-80
APPROVED BY
D ATE:
4-1-80
APPROVED BY: D ATE:
PROJEC T
NUMBER
-2[ ]
MAX.
.41
.150
.220
.010
.42
.48
.221
.290
.013
-3[ ]
.49
.55
.291
.360
.015
-4[ ]
.56
.62
.361
.430
.017
-5[ ]
.63
.69
.431
.500
.019
-6[ ]
.70
.76
.501
.570
.021
-7[ ]
.77
.83
.571
.640
.023
-8[ ]
.84
.90
.641
.710
.025
-9[ ]
.91
.97
.711
.780
.027
-10[ ]
.98
1.04
.781
.850
.029
-11[ ]
1.05
1.11
.851
.920
.031
11/18/86
.35
WEIGHT
LBS/EA
MIN.
EC O
16614
-1[ ]
B
2-28-80
E
JWH
A
REVISION G RED RAWN
DRAWING PROVIDES FORM, FIT
AND FUNTION DATA. DO NOT
ATTEMPT TO MANUFACTURE
PRODUCT USING THIS DRAWING.
GRIP RANGE
D ASH
NUMBER
TITLE
SC REW ASSY, QR
UNLESS OTHER RANGE SPEC IFIED
TOLERANC ES
D EC IMALS
XX = .02
XXX = .020
ANGLES
= 2°
Fairchild Fasteners
MILLIMETERS
.050
.025
SURFAC E FINISH
125 MIC ROINC HES
3016 West Lomit Boulevard
Torrance, CA 90505 USA
909-947-3366
FX10-1558-00
F S C : 29372
SHEET
1 OF 2
Tridair Products 75
INSTALLATION
HOLD-OUT POSITION
PANEL PREPARATION
NOTES:
MATERIAL:
SCREW: 8740 ALLOY STEEL PER MIL-S-6049.
GROMMET: 4140 ALLOY STEEL PER MIL-S-5626
SPRING: 17-7 PH CRES PER AMS 5673
2.
2.1
2.2
HEAT TREAT:
SCREW AND GROMMET: 160 K.S.I. MINIMUM ULTIMATE TENSILE STRENGTH PER
MIL-H-6875.
SPRING: CONDITION CH900 PER MIL-H-6875.
3.
3.1
3.2
FINISH:
SCREW AND GROMMET: CADMIUM PLATE PER QQ-P-416, TYPE II, CLASS 3.
SPRING: PASSIVATE PER QQ-P-35.
4.
USE WITH FX10-1510 OR FX10-1502 RECEPTACLE AND FX10-1525 RETAINING RING.
5.
.375 DIAMETER HOLE IN T2 MAY BE ENLARGED TO .390 DIAMETER (MAXIMUM) TO ALLOW FOR HOLE
MISALIGNMENT.
6.
6.1
6.2
RECESS OPTIONS AND CALLOUTS:
MS9006 RECESS: ADD “P” AFTER DASH NUMBER. EXAMBLE: FX10-1558-2P.
NAS1078 RECESS: ADD “TS” AFTER DASH NUMBER. EXAMPLE: FX10-1558-2TS.
7.
ANTI-SEIZE COMPOUND PER MIL-A-907 APPLIED TO THREAD.
D RAWING BY
JWH
D ATE:
2-28-80
APPROVED BY
D ATE:
3-31-80
APPROVED BY
D ATE:
4-1-80
APPROVED BY: D ATE:
PROJEC T
NUMBER
REVISION G RED RAWN
2-28-80
H
JWH
EC O
16614
11-18-86
1.
1.1
1.2
1.3
TITLE
SC REW ASSY, QR
UNLESS OTHER RANGE SPEC IFIED
TOLERANC ES
D EC IMALS
XX = .02
XXX = .020
ANGLES
= 2°
Fairchild Fasteners
MILLIMETERS
.050
.025
SURFAC E FINISH
125 MIC ROINC HES
3016 West Lomit Boulevard
Torrance, CA 90505 USA
909-947-3366
FX10-1558-00
F S C : 29372
SHEET 2 OF
2
Tridair Products 76
MAX.
.41
.230
.290
.013
.49
.48
.291
.360
.015
-3P
.56
.55
.361
.430
.017
-4P
.63
.62
.431
.500
.019
-5P
.70
.69
.501
.579
.021
-1P
.42
-2P
D RAWING BY
JWH
D ATE:
3-6-80
APPROVED BY
D ATE:
3-31-80
APPROVED BY
D ATE:
4-1-80
APPROVED BY: D ATE:
PROJEC T
NUMBER
REVISION D RED RAWN
DRAWING PROVIDES FORM, FIT
AND FUNTION DATA. DO NOT
ATTEMPT TO MANUFACTURE
PRODUCT USING THIS DRAWING.
3-6-80
JWH
E
B
OMJ
11/18/86
MIN.
A
EC O
16100
GRIP RANGE
WEIGHT
LBS/EA
D ASH
NUMBER
TITLE
SC REW ASSY, QR
UNLESS OTHER RANGE SPEC IFIED
TOLERANC ES
D EC IMALS
XX = .02
XXX = .020
ANGLES
= 2°
Fairchild Fasteners
MILLIMETERS
.050
.025
SURFAC E FINISH
125 MIC ROINC HES
3016 West Lomit Boulevard
Torrance, CA 90505 USA
909-947-3366
FX10-15010-[]P
F S C : 29372
SHEET
1 OF 2
Tridair Products 77
NOTES:
MATERIAL:
SCREW: 8740 ALLOY STEEL PER MIL-S-6049.
GROMMET: 4140 ALLOY STEEL PER MIL-S-5626
2.
2.1
HEAT TREAT:
SCREW AND GROMMET: 160 K.S.I. MINIMUM ULTIMATE TENSILE STRENGTH PER
MIL-H-6875.
3.
3.1
FINISH:
SCREW AND GROMMET: CADMIUM PLATE PER QQ-P-416, TYPE II, CLASS 3.
4.
USE WITH FX10-15009 OR CA17064 HOLD-OUT GROMMET TO PROVIDE FLUSH
CONDITION ON BOTTOM SIDE OF PANEL IN RETRACTED POSITION, AND FX10-1502
RECEPTACLE. SEE GROMMET DRAWING FOR PANEL PREPARATION AND INSTALLATION.
5.
AN FX10-1579-T11 INSTALLATION TOOL MUST BE USED TO INSTALL SCREW ASSEMBLY
INTO FX10-15009 GROMMET.
6.
ANTI-SEIZE COMPOUND PER MIL-A-907 APPLIED TO THREAD.
DRAWING PROVIDES FORM, FIT
AND FUNTION DATA. DO NOT
ATTEMPT TO MANUFACTURE
PRODUCT USING THIS DRAWING.
D RAWING BY
JWH
D ATE:
3-6-80
APPROVED BY
D ATE:
3-31-80
APPROVED BY
D ATE:
4-1-80
APPROVED BY: D ATE:
PROJEC T
NUMBER
REVISION D RED RAWN
JWH
E
3-6-80
1.
1.1
1.2
TITLE
SC REW ASSY, QR
UNLESS OTHER RANGE SPEC IFIED
TOLERANC ES
D EC IMALS
XX = .02
XXX = .020
ANGLES
= 2°
Fairchild Fasteners
MILLIMETERS
.050
.025
SURFAC E FINISH
125 MIC ROINC HES
3016 West Lomit Boulevard
Torrance, CA 90505 USA
909-947-3366
FX10-15010-[]P
F S C : 29372
SHEET 2 OF
2
Tridair Products 78
NOTES:
1.
1.1
1.2
1.3
MATERIAL:
RECEPTACLE: 1050 STEEL PER AISI C1050 OR AMS 5085.
NUT: 4140 OR 8740 ALLOY STEEL PER MIL-S-5626 OR MIL-S-6049.
INSERT: 4140 ALLOY STEEL PER MIL-S-5626.
2.
2.1
2.2
2.3
HEAT TREAT:
RECEPTACLE: FTU 150ksi MINIMUM PER MIL-H-6875.
NUT: FTU 180 KSI MINIMUM PER MIL-H-6875.
INSERT: FTU 160 KSI MINIMUM PER MIL-H-6875.
3.
3.1
FINISH:
RECEPTACLE, NUT AND INSERT: CADMIUM PLATE PER QQ-P-416, TYPE II, CLASS 3.
4.
TO BE USED WITH FX10-1500 AND FX10-15000 SERIES, 4 LEAD SCREW ASSEMBLIES.
5.
SHIMS FOR THIS RECEPTACLE: SEE FX10-1550 DRAWING.
6.
RECEPTACLE MAINTAINS 5 IN-LBS (MINIMUM) RUNNING TORQUE-OUT AFTER 200 COMPLETE CYCLES.
UNLESS OTHERWI SE SPECI FI ED
TOLERANCE: .XX = .±.02
.XXX = .010
ANGLE = ±2°
SURFACE FINISH: 125 M ICROINCHES
APPROVED DATE
31 M A R 80
REV LETTER AND DATE
S43022
J
AEROSPACE FASTENER DI VI SI ON
ENGI NEERI NG R&D CENTER
CAGE CODE 92215
I CIVIC PLAZA, SUITE 500
CARSON, CA 90745
FX10-1502
16 OCT 92
ECN NUMBER
E C N 31 574
Fairchild Fasteners
Q.R. RECEPTACLE ASSEM BLY
.190-32 UNF-3B, 4 LEAD
SHEET
1 OF 1
Tridair Products 79
NOTES:
1.
1.1
1.2
1.3
MATERIAL:
RECEPTACLE: 1050 STEEL PER AISI C1050 OR AMS 5085.
NUT: 4140 OR 8740 ALLOY STEEL PER MIL-S-5626 OR MIL-S-6049.
INSERT: 4140 ALLOY STEEL PER MIL-S-5626.
2.
2.1
2.2
2.3
HEAT TREAT:
RECEPTACLE: FTU 150 KSI MINIMUM PER MIL-H-6875.
NUT: FTU 180 KSI MINIMUM PER MIL-H-6875.
INSERT: FTU 160 KSI MINIMUM PER MIL-H-6875.
3.
3.1
FINISH:
RECEPTACLE, NUT AND INSERT: CADMIUM PLATE PER QQ-P-416, TYPE II, CLASS 3.
4.
TO BE USED WITH FX10-1500 AND FX10-15000 SERIES, 4 LEAD SCREW ASSEMBLIES.
5.
SHIMS FOR THIS RECEPTACLE: SEE FX10-1550 DRAWING.
UNLESS OTHERWI SE SPECI FI ED
TOLERANCE: .XX = .±.02
.XXX = .±..010
ANGLE = ±2°
SURFACE FINISH: 125 M ICROINCHES
APPROVED DATE
19 M A R 80
REV LETTER AND DATE
S43023
T
AEROSPACE FASTENER DI VI SI ON
ENGI NEERI NG R&D CENTER
CAGE CODE 92215
I CIVIC PLAZA, SUITE 500
CARSON, CA 90745
FX10-1510
16 OCT 92
ECN NUMBER
E C N 31 573
Fairchild Fasteners
Q.R. RECEPTACLE ASSEM BLY
.1900-32 UNF-3B, 4 LEAD
SHEET
1 OF 1
Tridair Products 80
NOTES:
1.
THIS RING DESIGNED FOR USE ON FX10-1500 SERIES SCREW ASSEMBLIES AND
CA1797 TYPE STUD NUTS.
2.
INSTALLATION TOOL:
A.) USE FX10-1530T TO INSTALL RINGS ON FX10-1500 SERIES SCREW ASSEMBLYS.
B.) USE CA1797-T10 TO INSTALL RINGS ON CA1795-( ) AND CA17036-( ) STUD NUTS.
3.
PANEL PREPARATION DATA:
A.) RETAINING RING RECESS: C’BORE .531 DIA X .030-.035 DEEP.
B.) MAX SUBSTRUCTURE HOLE: .390 DIA.
4.
MATERIAL: 18-8 TYPE 300 SERIES CRES, PER MIL-S-5059 AND/OR QQ-S-766 (CHEMISTRY ONLY).
5.
HEAT TREAT: STRESS RELIEVE.
6.
FINISH: PASSIVATED PER QQ-P-35.
7.
WEIGHT: .312 LBS/1000 PIECES (APPROXIMATE).
U N LESS OTH ER WI SE SPEC I FI ED
TOLER AN C E:
D EC IM ALS
. XX = .±.02
XXX = .010
AN GLE = ±2°
SU R FAC E FIN ISH : 125 M IC R OIN C H ES
APPROVED D ATE
29 M AY 73
REV LETTER AND D ATE
S42840
T
A ER OSPA C E FA STEN ER D I VI SI ON
EN GI N EER I N G R & D C EN TER
I C IVIC PLAZA, SU ITE 500
C AR SON , C A 90745
2 7 JU L 9 3
EC N NUMBER
E C N 33937
Fairchild Fasteners
R ETAIN IN G R IN G
OR FASTEN ER
TR ID AIR PR OD U C T
FX10-1525
SHEET
1 OF 1
Tridair Products 81
5-6-69
DATE
F
E
HEV
3.00 3.12
REDRAWN.
CHANGE
UNLESS OTHERWISE SPECIFIED
FINISH:
BLACK OXIDE
PER MIL-C-13924, CL I.
WEIGHT: .23 LB/EA
HEAT TREAT:
S C A LE
ENGN
ENGN
APP'D
E.E.
F JC
ALLOY STEEL
10/9/68
MATERIAL OR NAME
10/25/68
10-31-68
MFR'S OF NEWTON INSERTS AND CALFAX FASTENERS
3000 W. LOMITA BLVD., TORRANCE, CALIFORNIA, 90505, PHONES: 213-775-3636
OF
1
F
FX10-1530T
SPECIFICATION
INSTALLATION TOOL
- RETAINING RING -
1
FX10-1530T
SHEET
Tridair Products 82
Fairchild Fasteners
10-10-68
FEDERAL SUPPLY
CODE 29372
ANGLES ±
TOLERANCES:
DECIMALS:
.XX ± .015
.XXX ± .010
DRAWING PROVIDES FORM, FIT
AND FUNCTION DATA. DO NOT
ATTEMPT TO MANUFACTURE
PRODUCT USING THIS DRAWING.
REV
CHANGE
F
REVISED & REDRAWN
12-11-70
G
CORRECTED TOLERANCES
DRAWING PROVIDES FORM, FIT
AND FUNCTION DATA. DO NOT
ATTEMPT TO MANUFACTURE
PRODUCT USING THIS DRAWING.
FX10-1576
G
Tridair Products 83
DATE
9-30-70
UNLESS OTHERWISE SPECIFIED
TOLERANCES:
DECIMALS:
.XX ± .010
.XXX ± .005
ANGLES ± 1°
FEDERAL SUPPLY
CODE 29372
FINISH:
ENGN
HEAT TREAT:
PASSIVATED
PER QQ-P-35
Rc 44-48
17-7 PH CRES
AMS 5528
MATERIAL OR NAME
SPECIFICATION
9-30-70
ENGN
APP'D
10-4-70
RETAINING RING
FX10-1576
WEIGHT: .043 LBS/100
S C A LE :
4: 1
MFR'S OF NEWTON INSERTS AND CALFAX FASTENERS
3000 W. LOMITA BLVD., TORRANCE, CALIFORNIA, 90908, PHONES: 213-775-3626
SHEET
1
OF
1
Fairchild Fasteners
NOTES:
1.
TO BE USED WITH FX10-1502, FX10-1520, FX10-1570
FX10-1540 SCREW ASSEMBLIES.
2.
C’BORE .625 +.010 DIA. x .031 DEEP IN
-.000
OUTER PANEL, OR INNER STRUCTURE
FOR RETAINING RING RECESS.
CHANGE
6-24-70
B
10-16-70
C
6-11-80
D
E C O - 6480
12-15-80
E
E C O - 7404
4-24-82
F
DRAWING PROVIDES FORM, FIT
AND FUNCTION DATA. DO NOT
ATTEMPT TO MANUFACTURE
PRODUCT USING THIS DRAWING.
E C O - 9390
NOTES:
1.
2.
3.
SELECT DASH NO. ACCORDING TO PANEL THICKNESS T
USE FX10-19009-T11 TOOL TO INSTALL STUD IN GROMMET AS
SHOWN ON SHT 2
SEE SHT 2 FOR GROMMET & PANEL PREPARATION
DIMENSIONS.
GROMMET - 18-8 TYPE 300 SERIES CRES
UNLESS OTHERWISE SPECIFIED
TOLERANCES:
DECIMALS:
.XX ± .015
.XXX ± .010
ANGLES ± 1°
FINISH:
PASSIVATED
PER QQ-P-35
FEDERAL SUPPLY
CODE 29372
WEIGHT:
75-292
ENGN
HEAT TREAT:
ENGN
SPRING:
COND
CN900
APP'D
S C A LE : 4: 1
AMS56T5
MATERIAL OR NAME
SPECIFICATION
2-25-70
F JC
ASTM-A-582
SPRING - 17-7 PN CRES
3-4-70
GROMMET ASSY
STUD HOLD-OUT
FX10-15009
MFR'S OF NEWTON INSERTS AND CALFAX FASTENERS
3000 W. LOMITA BLVD., TORRANCE, CALIFORNIA, 90908, PHONES: 213-775-3626
SHEET
1
OF
2
Tridair Products 84
A
Fairchild Fasteners
REV
FX10-5009
DATE
1-20-70
C HANGE
FX10-15009
SEE SHEET 1
F
GROMMET D IMENSIONS
SIZE
BASIC
1S T
OVERSIZE
2ND
OVERSIZE
PART NO.
FX10-15009-1
FX10-15009-2
FX10-15009-3
FX10-15009-4
FX10-15009-5
FX10-15009-6
A
THEO
SHARP
B
MIN
D IA
C
C 'SMALL
D IA
D
GROM
D IA
.629
.590
.590
.499
.496
.090
.650
.625
.590
.514
.511
.096
.657
.690
.590
.530
.527
.066
PANEL AREA
F
E
(REF)
G
INSTALLATION TOOLS
LENGTH
LENGTH
T
PANEL
THIC
H
HOLE
SIZE
J
C ' SINC
D IA
.129
.128
.125
14999
.630
.110
.154
.199
.196
.5020
.633
.146
.129
.128
.125
.5150
.695
.110
.194
.199
.196
.5175
.660
.146
.129
.128
.125
.5310
.692
.110
.156
.199
.196
.9999
.697
.146
HOLLST. GROMMET GROMMET
K
C 'SMIL
D EPTH
L
FLARING
TOOL
M
STUD INST.
TOOL
N
BAC K-UP
TOOL
FX10-15009-T10
FX10-15009-T11
FX10-15009-T12
FX10-15009-T19
FX10-15009-T11
FX10-15009-T14
FX10-15009-T15
FX10-15009-T11
FX10-15009-T16
DRAWING PROVIDES FORM, FIT
AND FUNCTION DATA. DO NOT
ATTEMPT TO MANUFACTURE
PRODUCT USING THIS DRAWING.
MATERIAL OR NAME
UNLESS OTHERWISE SPECIFIED
TOLERANCES:
DECIMALS:
.XX ± .015
.XXX ± .010
ANGLES ± 1°
FINISH:
FEDERAL SUPPLY
CODE 29372
WEIGHT:
75-292
HEAT TREAT:
ENGN
2-25-70
ENGN
APP'D
F JC
3-4-70
SPECIFICATION
GROMMET ASSY
STUD HOLD-OUT
FX10-15009
S C A LE : 4: 1
Tridair Products 85
REV
MFR'S OF NEWTON INSERTS AND CALFAX FASTENERS
3000 W. LOMITA BLVD., TORRANCE, CALIFORNIA, 90908, PHONES: 213-775-3626
SHEET
2
OF
2
Fairchild Fasteners
D ATE
2.
HEAT TREAT: Rc 45 MINIMUM PER MIL-H-6875.
3.
FINISH: BLACK OXIDE PER MIL-C-13924A, CLASS I.
4.
THIS TOOL IS TO BE USED WITH A FX10-15009-T12 BACK-UP TOOL
TO INSTALL FX10-15009-1 AND FX10-15009-2 GROMMET.
5.
TOOL SHALL HAVE PART NUMBER ETCHED OR STAMPED IN AREA SHOWN.
DRAWING PROVIDES FORM, FIT
AND FUNTION DATA. DO NOT
ATTEMPT TO MANUFACTURE
PRODUCT USING THIS DRAWING.
D RAWING BY
D ATE:
11-28-79
APPROVED BY
D ATE:
12-6-79
APPROVED BY
D ATE:
12-6-79
APPROVED BY: D ATE:
PROJEC T
NUMBER
REVISION
NOTES:
1.
MATERIAL: TOOL STEEL, AISI TYPE06.
TITLE
FLARING TOOL
UNLESS OFTHER RANGE SPEC IFIED
TOLERANC ES
D EC IMALS
.XX = .02
. XXX = .020
ANGLES
= 2°
Fairchild Fasteners
MILLIMETERS
.050
.025
SURFAC E FINISH
125 MIC ROINC HES
3016 West Lomit Boulevard
Torrance, CA 90505 USA
909-947-3366
FX10-15009-T10
F S C : 29372
SHEET
1 OF 1
Tridair Products 86
FX10-15010-[ ] SCREW ASSEMBLY
(REF.)
FX10-15009-[ ] GROMMET ASSEMBLY
(REF.)
FX10-15009-T11 TOOL
(REF.)
NOTE:
INSERT TOOL AND SCREW ASSEMBLY AS SHOWN
THROUGH TOP SIDE OF GROMMET.
HEAT TREAT: Rc 45 MINIMUM PER MIL-H-6875.
3.
FINISH: BLACK OXIDE PER MIL-C-13924A, CLASS 1.
4.
TOOL SHALL HAVE DASH NUMBER, (-T11) ETCHED OR STAMPED ON
.374-.369 DIA.
DRAWING PROVIDES FORM, FIT
AND FUNTION DATA. DO NOT
ATTEMPT TO MANUFACTURE
PRODUCT USING THIS DRAWING.
D RAWING BY
RSR
D ATE:
11-27-79
APPROVED BY
D ATE:
12-3-79
APPROVED BY
RLW
D ATE:
12-4-79
APPROVED BY: D ATE:
PROJEC T
NUMBER
REVISION A
2.
ELO#
6156
LTWH
12-30-79
NOTES:
1.
MATERIAL: TOOL STEEL.
TITLE
INSTALLATION TOOL
SC REW ASSY.
UNLESS OFTHER RANGE SPEC IFIED
TOLERANC ES
D EC IMALS
XX = .02
XXX = .020
ANGLES
= 2°
Fairchild Fasteners
MILLIMETERS
.050
.025
SURFAC E FINISH
125 MIC ROINC HES
3016 West Lomit Boulevard
Torrance, CA 90505 USA
909-947-3366
FX10-15009-T11
F S C : 29372
SHEET
1 OF 1
Tridair Products 87
3.
FINISH: BLACK OXIDE PER MIL-C-13924A, CLASS I.
4.
THIS TOOL IS TO BE USED WITH A FX10-15009-T10 FLARE TOOL TO
INSTALL FX10-15009-1 AND FX10-15009-2 GROMMETS.
5.
TOOL SHALL HAVE PART NUMBER ETCHED OR STAMPED IN
AREA SHOWN.
12-30-79 B
HEAT TREAT: Rc 62-67 PER MIL-H-6875.
DRAWING PROVIDES FORM, FIT
AND FUNTION DATA. DO NOT
ATTEMPT TO MANUFACTURE
PRODUCT USING THIS DRAWING.
D RAWING BY
RSR
D ATE:
11-27-79
APPROVED BY
D ATE:
12-3-79
APPROVED BY
RLW
D ATE:
12-4-79
APPROVED BY: D ATE:
PROJEC T
NUMBER
REVISION A
JWH
2.
ECO#
7924
JWT
4-21-81
NOTES:
1.
MATERIAL: TOOL STEEL.
TITLE
TOOL, BAC KUP
UNLESS OTHER RANGE SPEC IFIED
TOLERANC ES
D EC IMALS
XX = .02
XXX = .020
ANGLES
= 2°
Fairchild Fasteners
MILLIMETERS
.050
.025
SURFAC E FINISH
125 MIC ROINC HES
3016 West Lomit Boulevard
Torrance, CA 90505 USA
909-947-3366
FX10-15009-T12
F S C : 29372
SHEET
1 OF 1
Tridair Products 88
NOTES:
1.
MATERIAL: TOOL STEEL.
HEAT TREAT: Rc 45 MINIMUM PER MIL-H-6875.
3.
FINISH: BLACK OXIDE PER MIL-C-13924A, CLASS I.
4.
THIS TOOL IS TO BE USED WITH A FX10-15009-T14 BACK-UP TOOL
TO INSTALL FX10-15009-3 AND FX10-15009-4 GROMMETS
5.
TOOL SHALL HAVE PART NUMBER ETCHED OR STAMPED IN AREA SHOWN.
DRAWING PROVIDES FORM, FIT
AND FUNTION DATA. DO NOT
ATTEMPT TO MANUFACTURE
PRODUCT USING THIS DRAWING.
D RAWING BY
D ATE:
11-28-79
APPROVED BY
D ATE:
12-3-79
APPROVED BY
RLW
D ATE:
12-4-79
APPROVED BY: D ATE:
PROJEC T
NUMBER
REVISION A
12-20-79
JWH
2.
TITLE
FLARING TOOL
UNLESS OFTHER RANGE SPEC IFIED
TOLERANC ES
D EC IMALS
XX = .02
XXX = .020
ANGLES
= 2°
Fairchild Fasteners
MILLIMETERS
.050
.025
SURFAC E FINISH
125 MIC ROINC HES
3016 West Lomit Boulevard
Torrance, CA 90505 USA
909-947-3366
FX10-15009-T13
F S C : 29372
SHEET
1 OF 1
Tridair Products 89
NOTES:
1.
MATERIAL: TOOL STEEL.
HEAT TREAT: Rc 45 PER MIL-H-6875.
3.
FINISH: BLACK OXIDE PER MIL-C-13924A, CLASS I.
4.
THIS TOOL IS TO BE USED WITH A FX10-15009-T16 BACKUP TOOL TO
INSTALL FX10-15009-5 AND FX10-15009-6 GROMMET.
5.
TOOL SHALL HAVE PART NUMBER ETCHED OR STAMPED IN AREA SHOWN.
DRAWING PROVIDES FORM, FIT
AND FUNTION DATA. DO NOT
ATTEMPT TO MANUFACTURE
PRODUCT USING THIS DRAWING.
D RAWING BY
D ATE:
11-28-79
APPROVED BY
D ATE:
12-3-79
APPROVED BY
RLW
D ATE:
12-4-79
APPROVED BY: D ATE:
PROJEC T
NUMBER
REVISION A
12-28-79
JWH
2.
TITLE
FLARING TOOL
UNLESS OFTHER RANGE SPEC IFIED
TOLERANC ES
D EC IMALS
XX = .02
XXX = .020
ANGLES
= 2°
Fairchild Fasteners
MILLIMETERS
.050
.025
SURFAC E FINISH
125 MIC ROINC HES
3016 West Lomit Boulevard
Torrance, CA 90505 USA
909-947-3366
FX10-15009-T15
F S C : 29372
SHEET
1 OF 1
Tridair Products 90
NOTES:
1.
MATERIAL: TOOL STEEL.
HEAT TREAT: Rc 45 MINIMUM PER MIL-H-6875.
3.
FINISH: BLACK OXIDE PER MIL-C-13924A, CLASS I.
4.
THIS TOOL IS TO BE USED WITH A FX10-15009-T16 BACK-UP TO
INSTALL FX10-15009-3 AND FX10-15009-4 GROMMETS.
5.
TOOL SHALL HAVE PART NUMBER ETCHED OR STAMPED IN AREA SHOWN.
DRAWING PROVIDES FORM, FIT
AND FUNTION DATA. DO NOT
ATTEMPT TO MANUFACTURE
PRODUCT USING THIS DRAWING.
D RAWING BY
D ATE:
11-27-79
APPROVED BY
D ATE:
12-3-79
APPROVED BY
MSC
D ATE:
12-4-79
APPROVED BY: D ATE:
RLW
PROJEC T
NUMBER
REVISION A
12-20-79
JWH
2.
TITLE
TOOL, BAC K-UP
UNLESS OFTHER RANGE SPEC IFIED
TOLERANC ES
D EC IMALS
XX = .02
XXX = .020
ANGLES
= 2°
Fairchild Fasteners
MILLIMETERS
.050
.025
SURFAC E FINISH
125 MIC ROINC HES
3016 West Lomit Boulevard
Torrance, CA 90505 USA
909-947-3366
FX10-15009-T15
F S C : 29372
SHEET
1 OF 1
Tridair Products 91
NOTES:
1.
MATERIAL: TOOL STEEL.
HEAT TREAT: Rc 62-67 PER MIL-H-6875.
3.
FINISH: BLACK OXIDE PER MIL-C-13924A, CLASS I.
4.
THIS TOOL IS TO BE USED WITH A FX10-15009-T15 FLARE TOOL TO
INSTALL FX10-15009-5 AND FX10-15009-6 GROMMETS.
5.
TOOL SHALL HAVE PART NUMBER ETCHED OR STAMPED IN AREA SHOWN.
DRAWING PROVIDES FORM, FIT
AND FUNTION DATA. DO NOT
ATTEMPT TO MANUFACTURE
PRODUCT USING THIS DRAWING.
D RAWING BY
RSR
D ATE:
11-27-79
APPROVED BY
D ATE:
12-3-79
APPROVED BY
RLW
D ATE:
12-4-79
APPROVED BY: D ATE:
PROJEC T
NUMBER
REVISION A
12-28-79
JWH
2.
TITLE
TOOL, BAC K-UP
UNLESS OFTHER RANGE SPEC IFIED
TOLERANC ES
D EC IMALS
XX = .02
XXX = .020
ANGLES
+
= 2°
Fairchild Fasteners
MILLIMETERS
+.050
+.025
SURFAC E FINISH
125 MIC ROINC HES
3016 West Lomit Boulevard
Torrance, CA 90505 USA
909-947-3366
FX10-15009-T16
F S C : 29372
SHEET
1 OF 1
Tridair Products 92