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HL10

The document contains specifications and details regarding the HI-LOK™ pin and collar assembly, including dimensions, material requirements, and coating options. It lists various licensees and their corresponding CAGE numbers, as well as general notes on manufacturing and quality standards. Additionally, it outlines how to order the pins with specific part numbers and variations.

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cyril.daraujo
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0% found this document useful (0 votes)
214 views2 pages

HL10

The document contains specifications and details regarding the HI-LOK™ pin and collar assembly, including dimensions, material requirements, and coating options. It lists various licensees and their corresponding CAGE numbers, as well as general notes on manufacturing and quality standards. Additionally, it outlines how to order the pins with specific part numbers and variations.

Uploaded by

cyril.daraujo
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF, TXT or read online on Scribd
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.IS).

LISI AEROSPACE – Please refer to Central Documentation Website to check validity


H!-~~~~~~o"s~6~t~n~P~~YA
Design Holder CAGE No. 73197 SPS TECHNOLOGIES. USA
SPS TECHNOLOGIES. UK
Licensee
Licensee
CAGE No. 56878
CAGE No. K5673

l
BLANC AERO INDUSTRIES UK Ltd Licensee CAGE No. U6300 MINEBEA. Japan Licensee (Japan) CAGE No. SB962
a USJ AEROSPACE Company WEST COAST AEROSPACE. USA (WW for oversize. USA & CAGE No. 60516
AEROSPACE BLANC AERO INDUSTRIES SA,France Licensee CAGE No. F0188-C Canada for nominal)

@1 L~~~~~~;~~~EE~~~~DA, Canada Licensee CAGE No. L4528


AFS Hildesheim, Germany
AFS City of lndustry,USA
Licensee
Licensee
CAGE No. C4293
CAGE No. 1 AC86
a USI AEROSPACE Company CAGE No. 06950
h;·•heor corporation ANKIT FASTENERS Ltd, India Licensee (India) CAGE No. SEM10 AFS Carson. USA Licensee CAGE No.17446
2100 SKYPARK DRIVE, TORRANCE, CALIFORNIA i06ot U.S.A. Air Industries CO., USA Licensee (USA, Canada) CAGE No. 06725

INDENTED HEAD MARKING .010 MAX DEPTH. REMAINING PORTION OF HI·LOKTM


MANUFACTURER'S TRADEMARK "hs" PER 1------ (MAX GRIP+ B) ±.010 -------1 COLLAR AFTER ASSEMBLY
SPEC 363. THE NUMBER(S) FOLLOWING
TRADEMARK INDICATES FIRST DASH NO.
ARRANGEMENT OPTIONAL. RMAX GRIP ±.005 ~
S CHAMFER
RAD I

THREAD ROLLED PER AS8879


(MODIFIED). MAJOR DIA SHALL COLLAR WRENCH
BE PER "TD" DEVICE AUTOMATICALLY
HI-LOK'M PIN SHEARS OFF

HI-LOK'M PIN AND COLLAR AFTER ASSEMBLY


v -
SOCKET SEE COLLAR STANDARDS
DDIA DOUBLE
FIRST
DASH
PIN
NOM
A B WITHOUT AFTER TO G H R s THREAD SHEAR
TENSION
POUNDS
FOR COLLAR STRENGTHS.
LOWER STRENGTH (PIN OR
NO. DIA DIA REF COATING COATING
OR SOLID OR SOLID
DIA REF RAD
CHAMFER
REF MODIFIED w
HEX
T
DEPTH
y
DIA
POUNDS
MINIMUM COLLAR) DETERMINES
MINIMUM SYSTEM STRENGTH
FILM FILM
4 1/8
.240
.225
.294
.1375
.1370
.1375
.1365
.1335
.1310
.020
.042
.032
.020
.010
1/32 x3r
.1380-32
UNJC-3A
.0645
.0635
.100
.085 rn 2,840 1,350
.262 .1635 .1635 .1595 .047 .025 .1640-32 .0645 .135 .090
5 5/32 .312 .020 1/32 X 37' 4,010 1,940
.242 .1630 .1625 .1570 .037 .015 UNJC-3A .0635 .115 .075
.315 .1895 .1895 .1840 .055 .025 .1900·32 .0806 .135 .119
6 3/16 .325 .025 1/32 X 37' 5,380 2,500
.295 .1890 .1885 .1810 .045 .015 UNJF-3A .0791 .115 .104
.412 .2495 .2495 .2440 .069 .025 .2500·28 .0967 .150 .142
8 1/4 .395 .030 1/32 X 37' 9,300 4,300
.387 .2490 .2485 .2410 .059 .015 UNJF·3A .0947 .130 .122
.505 .3120 .3120 .3060 .078 .030 .3125·24 .1295 .170 .180
10 5/16 .500 .035 3/64 X 37' 14,600 6,300
.475 .3115 .3110 .3020 .068 .020 UNJF-3A .1270 .150 .160
.600 .3745 .3745 .3680 .088 .030 .3750-24 .1617 .200 .217
12 3/8 .545 .040 3/64 X 37' 21,000 8,700
.565 .3740 .3735 .3640 .078 .020 UNJF-3A .1582 .180 .197
.676 .4370 .4370 .4310 .105 .030 .4375·20 .1930 .230 .253
14 7/16 .635 .045 3/64 X 37' 28,600 12,100
.641 .4365 .4360 .4260 .093 .020 UNJF·3A .1895 .210 .233
.770 .4995 .4995 .4930 .115 .030 .5000·20 .2242 .260 .289
16 1/2 .685 .050 3/64 X 37' 37,300 15,300
.735 .4990 .4985 .4880 .103 .020 UNJF-3A .2207 .240 .269
.864 .5615 .5615 .5550 .127 .040 .5625·18 .2555 .290 .326
18 9/16 .770 .055 1/16x3r 47,200 19,000
.829 .5610 .5605 .5500 .112 .025 UNJF·3A .2520 .270 .306
.953 .6240 .6240 .6180 .137 .040 .6250·18 .2555 .330 .326
20 5/8 .825 .060 1/16 X 37' 58,300 23,000
.918 .6235 .6230 .6120 .122 .025 UNJF·3A .2520 .305 .306
1.108 .7490 .7490 .7430 .151 .045 .7500-16 .3185 .395 .398
24 3/4 1.050 .070 1/16x3r 83,900 30,700
1.066 .7485 .7480 .7370 .136 .030 UNJF-3A .3150 .365 .378
1.285 .8740 .8740 .8680 .187 .050 .8750-14 .3820 .455 .471
28 7/8 1.210 .090 5/64 X 37' 114,000 45,000
1.241 .8735 .8730 .8610 .172 .035 UNJF·3A .3780 .425 .451
1.468 .9990 .9990 .9930 .218 .060 1.0000·12 .5100 .580 .618
32 1 1.390 .110 5/64 X 37' 149,000 60,900
1.424 .9985 .9980 .9860 .203 .045_ UNJF-3A .5040 -- -
.55Q_ .598 -

"HI-LOK", "HL", and "HI-KOTE",


are Trademarks of Hi-Shear Corporation
DRAWN BY DATE TITLE
Brlej 11-26·62 HI-LOK™ PIN
J.F.Obispo 7-29-14

:I: DATE
PROTRUDING SHEAR HEAD

•......
APPROVED
TITANIUM
Cessna 11-26-62 1/16 GRIP VARIATION

REVISION DATE DRAWING NUMBER

0 @ JFO
7-29-14 HL10 1 of 2

@ 2014 Hi-Shear Corporation

LISI AEROSPACE – Please refer to Central Documentation Website to check validity


.IS). LISI AEROSPACE – Please refer to Central Documentation Website to check validity

l AEROSPACE

hl·•hear corporation
21500 SKYPAAK DRIVE, TORRANCE, CALIFORNIA 10501 U.S.A.

GENERAL NOTES: 1. Concentricity: "A" to "D" diameter within .010 FIM.


2. Dimensions to be met afterfinish. CODE: First dash number indicates nominal diameter in 1/32nds.
3. Surface texture per ANSI B46.1. Second dash number indicates maximum grip in 1/16ths.
4. Hole preparation per NAS618. See Finish note for explanation of code letters.
rn:J Maximum "D" diameter may be increased by .0002 to allow
for solid film or aluminum coating application.
rn:J Broach petals removed. HOW TO ORDER
EXAMPLE: Pin Part Number
1IJ Dimensions to be met before finish for "VY" code only. HL10VAP8-8

1JU
liD Evidence of broken edge across points.
[l!] Non-lubed pins must be used with lubed collars or wet sealant. TL 8/16 or 1/2 Maximum Grip Length
L 8/32 or 1/4 Nominal Diameter Pin
10. Use HL 110 for oversize replacement.
HI-KOTETM 1 Aluminum Coating
Pin Basic Part Number
MATERIAL: 6AL-4V titanium alloy per AMS4928 or AMS4967.

@ HEAT TREAT: 160,000 psi tensile minimum (95,000 psi shear minimum for sizes up to 3/4;
90,000 psi shear minimum for 7/8 and larger).

FINISH: HL 10V()-() = Cetyl alcohol lube per Hi-Shear Spec. 305.


HL10VAP( )-() = HI-KOTPM 1 aluminum pigmented coating per Hi-Shear Spec. 294, and cetyl alcohol lube
per Hi-Shear Spec. 305.
HL10VAZ( )-() = HI-KOTETM 1 aluminum pigmented coating per Hi-Shear Spec. 294, with color black on
thread end, and cetyl alcohol lube per Hi-Shear Spec. 305.
HL 1OVBJ( )-( ) = I.V.D. aluminum coating per MIL-DTL-83488, Type II, Class 3, and cetyl alcohol lube per
Hi-Shear Spec. 305.
HL10VBR( )-() = Color code white on thread end, and cetyl alcohol lube per Hi-Shear Spec. 305.
[l!]HL 10VBU( )-() = I.V.D. aluminum coating per MIL-DTL-83488, Type I, Class 3, with color yellow on thread end.
[l!]HL 10VBV( )-() = I.V.D. aluminum coating per MIL-DTL-83488, Type II, Class 3, with color blue on thread end.
HL10VCB( )-() = I.V.D. aluminum coating per MIL-DTL-83488, Type I, Class 3, with color black on thread end,
and cetyl alcohol lube per Hi-Shear Spec. 305.
rn:J HL 1OVDK()-() =Solid film lube per "KaiGardTM" FA. "KALGARD" is a trademark of Metal Improvement Company.
HL10VF( )-() =Surface coating per Hi-Shear Spec. 306, Type I, color blue, and cetyl alcohol lube per Hi-Shear Spec. 305.
HL10VHD()-() = I.V.D. aluminum coating per BAC5315, with color red on thread end, and cetyl alcohol lube per
Hi-Shear Spec. 305.
rn:JHL10VK( )-() = Solid film lube per Lubeco 905.
H L 1OVLJ()-() =Surface coating per Hi-Shear Spec. 306, Type II, and solid film lube per AS5272.
HL10VLV()-() = Phosphate fluoride treat and Esna-Lube No. 382 (Everlube Corp).
HL10VR( )-() =Surface coating per Hi-Shear Spec. 306, Type II, and solid film lube per "Eiectrofilm" 4396.
HL 10VRA( )-() = Phosphate fluoride treat with color red on thread end and cetyl alcohol lube per Hi-Shear Spec. 305.
HL10VSY( )-() =Phosphate fluoride treat, solid film lube per AS5272, Type I, and color red on thread end.
HL 10VT( )-() =Surface coating per Hi-Shear Spec. 306, Type I, color pink, and cetyl alcohol lube per Hi-Shear
Spec. 305.
HL10VTA()-() =Anodize Ti-Shield Ill and HI-KOTETM 2 solid film lube per Hi-Shear Spec. 292, and cetyl alcohol
lube per Hi-Shear Spec. 305.
HL 10VTB( )-() = HI-KOTETM 2 solid film lube per Hi-Shear Spec. 292, and cetyl alcohol lube per Hi-Shear Spec. 305.
HL10VTF( )-() = HI-KOTETM 2 solid film lube per Hi-Shear Spec. 292.
HL10VTL( )-() = Anodize Ti-Shield Ill, solid film lube per DAG-258, and cetyl alcohol lube per Hi-Shear Spec. 305; or
anodize per Tiodize Type II, solid film lube per TI-0-LUBE': TAL-58, and cetyl alcohol lube per
Hi-Shear Spec. 305.
HL10VTT{ )-() = Translube.
HL 10VUE( )-() =Surface coating per Hi-Shear Spec. 306, Type II, and cetyl alcohol lube per Hi-Shear Spec. 305.
HL10VUU( )-() =Surface coating per Hi-Shear Spec. 306, Type II, and solid film lube per "Lubeco" 2123, Type II.
HL10VV( )-() =Solid film lube per "Lubeco" 2123, Type II.
IIJHL10VY( )-() = Surface coating per Hi-Shear Spec. 306, Type I, color blue, and solid film lubricant per M88.
(British Aircraft Corporation Spec. MP-1071).
HL 10VNKJ( )-() = HI-KOTETM 1 NC aluminum pigmented coating per Hi-Shear Spec. 294, with color siilver on thread
end, and cetyl alcohol lube per Hi-Shear Spec. 305.
HL 10VNKK( )-() = Sulfuric acid anodizing per IS08080 and HI-KOTETM 1 NC aluminum pigmented coating per Hi-Shear
Spec. 294 on threads only, with color silver on thread end, and cetyl alcohol lube per Hi-Shear Spec. 305.
HL 1OVNKL( )-( ) = HI-KOTETM 1 NC aluminum pigmented coating per Hi-Shear Spec. 294 on threads only, with color silver
::1: on thread end, and cetyl alcohol lube per Hi-Shear Spec. 305.

r..... SPECIFICATION: HI-LOKTM Product Specification 342.


DRAWING NUMBER

0 I
©
HL10
2014 Hi-Shear Corporation
2 of 2

_ _ _ _. . . . , , . . . . , _ . . . , _ _ _ _ _ _ _ _ _ _ _ _ _ _ LISI AEROSPACE – Please refer to Central Documentation Website to check validity


,_...--------~- --~- ... W>i~~"'-"""'~

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