TM-G84 Rev.

: H DCR# 15-0406 DATE: 5/5/15 Federal Identification Code: 11815 © 2015 Cherry Aerospace

Original Instructions

G84
Lockbolt Power Tool

1224 E. Warner Ave,

Santa Ana, Ca 92705
Tel: 1-714-545-5511
Fax: 1-714-850-6093
www.cherryaerospace.com
 TM-G84 Rev.: H DCR# 15-0406 DATE: 5/5/15 Federal Identification Code: 11815 © 2015 Cherry Aerospace

T H E G 8 4 TO O L

TABLE OF CONTENTS
Description .........................................................................................................................................................................................3
Specifications for G84 ........................................................................................................................................................................3
Safety Warnings .................................................................................................................................................................................3
Putting the tool in service ............................................................................................................................................................... …4
How to Use the G84 ...........................................................................................................................................................................4
Lockbolt Pulling Pulling-Heads ............................................................................................................................................5
Maxibolt Pulling Pulling-Heads .............................................................................................................................................5
Adaptors and Cherrymax Pulling-Heads...............................................................................................................................5
Maintenance and Repair / Fluid Safety Data .....................................................................................................................................6
Fill and Bleed Instructions ..................................................................................................................................................................6
Tool Overhaul .....................................................................................................................................................................................7
Air Valve ..............................................................................................................................................................................7
Head Sub-Assembly ............................................................................................................................................................7
Handle Sub-Assembly .........................................................................................................................................................8

Troubleshooting .................................................................................................................................................................................8
Cross Section Drawing .......................................................................................................................................................................9
Parts List ...........................................................................................................................................................................................10
Exploded View of G84 .....................................................................................................................................................................11
Declaration of Conformity ................................................................................................................................................. Back Cover

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 ONE (1) YEAR AFTER INITIAL USE BY BUYER OF ANY POWER RIVETER OR NINETY (90) DAYS AFTER INITIAL USE OF
ANY OTHER PRODUCT.

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.

For more information please contact our Technical Services Department at Tel. 714-850-6022

LOCTITE® is a registered trademark of Henkel Corporation

DEXRON® is a registered trademark of GM corporation.
PARKER® is a trademark of Parker Hannifin Corporation
LUBRRIPLATE® is a trademark of Fiske Brothers Refining Co.

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 TM-G84 Rev.: H DCR# 15-0406 DATE: 5/5/15 Federal Identification Code: 11815 © 2015 Cherry Aerospace

DESCRIPTION
The Cherry® G84 pneumatic-hydraulic Lockbolt™ installation tool is
a heavy duty production tool designed for high speed, reliable
installation of the most popular sizes of aircraft Lockbolts™.
This powerful tool has been designed with many ergonomic
features: light weight (7.70 lb.), (3.5 kg), low recoil and noise, a
comfortable fit in the operator’s hand. The piston returns with a
force of 1200 Lbs., force necessary when used for Lockbolt™
swaging.
This tool can also be used to install blind bolts and rivets.

SPECIFICATIONS FOR G84A

Cherry® Aerospace (CHERRY®) policy is one of continuous
development. Specifications shown in this document may be
subject to change which may be introduced after publication. For
the latest information always consult CHERRY®.
AIR PRESSURE RANGE 90 psi (6.2 bar) / 100 psi (6.89 bar)
(use P1505 regulator pre-set at 100 psi)
STROKE 9/16 inch (14.3 mm)
PULLING FORCE 5,750 lbs. (25.6 kN) @ 100 psi,
1200 lbs. (5.34 kN) on return stroke
WEIGHT 7.70 lbs. (3.5 kg)
NOISE LEVEL less than 80 dB (A)
VIBRATION less than 2.5 m/s2
AIR CONSUMPTION 0.29 SCF/cycle (8.21 L/cycle)

SAFETY WARNINGS
• Do not use beyond the design intent; do not use substitute components for repair.
• Use the tool with a pressure regulator; if one is not available, use the Cherry P-1505.
• Operating this tool with a damaged or missing stem deflector, or using the deflector as a handle, may result in
severe personal injury. Rotate the pin deflector facing away from the operator
• Wear proper PPE when operating, repairing, or overhauling this tool ( .)
• Any modification will void warranty and shall be at the customer's entire responsibility.
• Maintain the tool in a safe working condition at all times and examined at regular intervals for damage.
• Before disassembling the tool for repair, refer to the maintenance instructions. All repairs shall be undertaken
only by personnel trained in Cherry installation tools.
• Disconnect the air line from the tool inlet before servicing, adjusting, fitting or removing any accessory.
• Ensure that the vent holes do not become blocked or clogged and the hoses are in good condition.
• Wash thoroughly after handling the fluid; excessive contact could cause rashes.
• Operating air pressure not to exceed 110 psi (7.6 bar); use of a pre-set regulator (P1505) is recommended
• Do not operate the tool without the pulling head in place.
• All retaining rings, screwed end caps, air fittings, trigger valves and pulling heads should be attached securely
and examined at the end of each working shift.
• Do not pull rivet in the air or directed at any person.
• Do not pound on the rear of the tool head to force rivets into holes as this will damage the tool.
• Safety warnings must be explained all operators as part of training.

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 TM-G84 Rev.: H DCR# 15-0406 DATE: 5/5/15 Federal Identification Code: 11815 © 2015 Cherry Aerospace

PUTTING THE TOOL IN SERVICE

The tool must be used with an air pressure regulator. Even if your shop air pressure is below the maximum recommended
range, pressure spikes in your airlines could cause serious damage to the tool or cause safety concerns.

Tools with an integral Air Tools without an integral Air Pressure Regulator (P-1505),
Pressure Regulator (P-1505), MUST be connected to a dedicated, regulated airline.
may be attached to any shop airline.

HOW TO USE THE G84

LOCKBOLT INSTALLATION
After selecting the proper pulling head and attaching it securely to the G84, connect the air line to the tool.

Lockbolts: Place the lockbolt pin into the workpiece and place the collar over the pintail.
While holding the back end of the lockbolt in place, push the pulling head onto the serrated area of the stem.

• Caution: When using a non-self-releasing pulling head once the tool is placed onto the serrated end, it cannot be removed unless
going through the installation cycle which breaks the serrated end of the bolt.
The broken part (pintail) will eject through the rear of the riveter when using a straight pulling head and through the rear of the active
area of the tool for when using offset pulling heads.

If the tool does not release the swaged collar after installation, it can be adjusted by adding shims behind the pulling head collet. If
the tool still does not release, see troubleshooting instructions on page:
See pulling head installation instructions.

BLIND BOLTS AND RIVETS

• Insert the blind fastener into the prepared hole and place the tool onto the serrated stem.

• Pull the trigger to activate the tool. Upon release of the trigger, the stem will eject to the rear of the riveter when using straight pulling
heads, and from the rear of the active area of the tool when using offset pulling head. Right angle pulling heads eject the stems
through the front..

PULLING HEADS
Pulling heads are not furnished and must be ordered separately. All Huck nose assemblies suitable for the 352 and 230 style tools will fit
directly on this tool.

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 TM-G84 Rev.: H DCR# 15-0406 DATE: 5/5/15 Federal Identification Code: 11815 © 2015 Cherry Aerospace

CHISEL SHAPE
SWIVEL NOSE
L O C K B O L T P U L L I N G H E AD S TYPE
DIA
BASIC MODEL
SWIVEL NOSE
SELF-RELEASING
SWIVEL NOSE
CODE TYPE SELF-RELEASING
TYPE
H513 SERIES STRAIGHT PULLING TYPE.
H513-04-20*
HEADS -4 H513-04-35* - - -
H513-04-60*
The H513 series pulling heads are for 1/8" through 1/4"
H513-05-35* H5135-05-20* H513SR-05-20* H513SRC-05-20*
diameter lockbolts (see table below). -5
H513-05-60* H513S-05-35 H513SR-05-35 H513SRC-05-35*

STRAIGHT H513S-06-20* H513SR-06-20*

H562/H563 OFFSET PULLING HEADS -6
H513-06-20*
H513-06-60*
H513S-06-24
H513S-06-35*
H513SR-06-24
H513SR-06-35*
H513SRC-06-20*
H513SRC-06-35*
The H562 and H563 series offset pulling heads can be H513S-06-48 H513SR-06-48

used in limited access areas. H513S-08-24

H513SR-08-24
-8 H513-08-35* H513S-08-35* H513SRC-08-48
H513SR-08-48
H513S-08-48
NOTES: H563-4B*
-4
H563SP-4B*
• No letter after P/N indicates basic head; "S" code - - -
H563-5B*
indicates swivel nose; "SR" code indicates self- -5
H563SP-5B* - - -
OFFSET
releasing swivel nose;
H563-6B*
"SRC" code indicates chisel shape, self-releasing, -6 - - -
H563SP-6B*
swivel nose; "SP" code indicates it intended for short
-8 H562-8B - - -
pintail lockbolts.
• Part numbers with an asterisk fit directly on the Cherry® G84 tool; the rest require adapter 744-100to fit onto the G84 tool.

MAXIBOLT PULLING HEADS

PART NO. MAXIBOLT DIA. DESCRIPTION ADAPTER

H83B-5MB/5MBU -5
H83B-6MB/6MBU -6 FOR SINGLE ACTION MAXIBOLT. USE "MBU" FOR
STRAIGHT H84A-8MB/8MBU "U" TYPE FASTENERS
-8
PULLING
HEADS H84C-8MB -8 N/A
H84CE6-8MB -8 EXTENDED REACH (6" LONGER)
H84HL-5 OR 6 OR 8 -5 OR -6 OR -8 PREVENTS HEAD LIFT ON 130 HEAD FASTENERS
H84B-568 -5, -6, -8 MB Plus FOR MAXIBOLT PLUS FASTENERS
OFFSET H856-6MB -6 744-200
H828-5MB -5 744-200
H828-6MB -6 FOR SINGLE ACTION MAXIBOLT. 744-200
RIGHT ANGLE
H828-8MB -8 744-200
H828-56MBP -8 FOR MAXIBOLT PLUS FASTENERS 744-200

CHERRYMAX ® PULLING HEADS STEP 1 STEP 2 STEP 3

AND ADAPTERS
PULLING CHERRYMAX®
PART NO. ADAPTER
HEAD DIAMETER
H701B-456 -4, -5, -6 744-300
STRAIGHT
H84A-8 -8 —
H781-456 -4, -5, -6 744-300
OFFSET H782 -4, -5, -6 744-300
H827-8 -8 744-200

RIGHT H753A-456 -4, -5, -6 744-300

ANGLE H828-8 -8 744-200

ADAPTOR MOUNTING INSTRUCTIONS

STEP 1 Remove Bayonet mount with square shank screwdriver. Use even force to turn the bayonet mount free from the thread locking compound.
Do not hammer on the screw driver or bayonet mount. We recommend placing the tool carefully in a vise equipped with soft jaws. Store it for future use.
STEP 2 Attach Drawbolt Adapter to head piston and tighten securely.
STEP 3Attach the Sleeve Adapter and tighten securely

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 TM-G84 Rev.: H DCR# 15-0406 DATE: 5/5/15 Federal Identification Code: 11815 © 2015 Cherry Aerospace

MAINTENANCE AND REPAIR

This riveter has been manufactured to give maximum service with minimum care. For optimum function:
1. The hydraulic system to be full of oil and free from air at all times.
2. Use clean and dry air to prevent premature wear and clogging of the air components.
3. Inspect the riveter for fluid leaks routinely
Use automatic transmission fluid (ATF ) type “A” (no substitutes). Cherry® Aerospace recommends using, Dexron® III ATF.

FIRST AID
Skin: Wash thoroughly with soap and water as soon as possible. Casual contact requires no immediate
attention. If irritation develops, consult a physician.
Ingestion: Seek medical attention immediately. DO NOT INDUCE VOMITING.
Eyes: Flush with copious amounts of water. If irritation develops, consult a physician.
Inhalation: No significant adverse health effects are expected to occur on short term exposure.
Remove from contaminated area. Apply artificial respiration if needed. If unconscious, consult physician.
FIRE
Suitable extinguishing media: CO2, dry powder, foam or water fog. DO NOT use water jets.
ENVIRONMENT
Waste Disposal: In accordance with local, state and federal regulations.
Spillage: Prevent entry into drains, sewers and water courses. Soak up with diatomaceous earth or
other inert material.
Store the spent fluid in appropriate containers for disposal.
HANDLING
Eye protection required. Protective gloves recommended. Chemically resistant boots and apron
recommended. Use in well-ventilated area.
COMBUSTIBILITY
It is slightly combustible when heated above flash point. It will release flammable vapors which can
burn in open or be explosive in confined spaces if exposed to source of ignition.
STORAGE
Avoid storage near open flame or other sources of ignition.

PROPERTIES Specific gravity 0.863

Weight per gallon 7.18 lbs.
Open flash point >200°C (392°F)

FILL AND BLEED INSTRUCTIONS

• To replace a small amount of oil in the tool, remove cap screw (21) from side of head cylinder and attach the
700A77 Air Bleeder (see picture). Connect the tool to the air line and cycle several times.
• To completely refill the tool (after the tool has been dismantled and re- assembled) take the following steps:
1. With the tool upright, connected to an air source, hold trigger down and disconnect the air. The Head
Piston (10) should have moved back; if it hasn’t push it back manually, using a press
2. Remove the screw (21) from the side of the head cylinder (13). Connect a pressurized fluid source
filled with automatic transmission fluid Type “A”.
3. Remove the screw (21) from the rear of the head cylinder (13). Force the fluid into the tool until it flows
out the rear hole. Position the tool so the rear hole is the highest point. Keep pumping fluid until all air
bubbles are out. Place the Screw (21) and the Seal (22) into the rear hole and tighten.
4. Remove the screw (21) from the top of the head cylinder (13). Force the fluid into the tool until it flows
out the top hole. Position the tool in such a way that the top hole is the high point. Keep pumping the
oil until all air bubbles are out.
5. Disconnect the pressure oil can from the side hole of the head cylinder (13). Replace screw (21) and
Stat-O-Seal (22) and tighten.
6. Holding a cloth over the top hole, attach tool to an air source. Excess fluid and will be discharged into
the cloth. Place the Screw (21) with the Seal (22) onto the top hole and tighten.
NOTE: For the purpose of bleeding, it is not necessary to remove the pressure relief valve (77). Do not
remove any of the hex set screws from the head or the handle.

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 TM-G84 Rev.: H DCR# 15-0406 DATE: 5/5/15 Federal Identification Code: 11815 © 2015 Cherry Aerospace
TO O L O V E R H AU L
Tool overhaul is needed in case of tool malfunction, massive fluid loss or as part of your routine maintenance program.
TOOLS NEEDED: G740KT – tool kit, Needle Nose Pliers,
G84KS – service kit:

836B740
Valve Spring Installation 744-104
Tool Seal Guide

837B740
Valve Sleeve Removal
700A61 Tool
Piston Rod
Wrench

700B65
Packing Plug Wrench 740A43
Power Cylinder Tool 700A77
Air Bleeder
G740KT TOOL KIT

OVERHAUL PROCEDURE
Caution:
• Maintenance and repair to be conducted only by trained personnel.
• Prior to attempting any repair or maintenance work, make sure the air is disconnected.
• Follow these instructions. Use special care handling sealing surfaces to avoid damage.
•
®
Replace all seals; before re-assembly, apply an O-ring lubricant (Parker silicone lube or equivalent) on all O-rings
• Apply a small amount of Loctite® 242 on the threaded components; curing time about 30 to 60 minutes.
• After tool overhaul, fill and bleed per instructions on page 6.

AIR VALVE SUB-ASSEMBLY

Disassembly Instructions:
• Remove retaining ring (55) and muffler (54).
• Pull the valve plug (53) and spool subassembly (80) out with the help of tool P1178;
• If necessary, pull the valve sleeve (46) with l tool 837B740 after dislodging the spring (47) with a needle-nose pliers and pulling it out.
Assembly Instructions:
• Reverse the above procedures. Use Install tool 836B740 to push spring (47) into its groove.

HEAD SUB-ASSEMBLY
Disassembly:
• Remove end cap (4). Thread tool 744-103 onto head piston (10) and push it out of the head cylinder (13).
• O-rings and back-up ring can be removed using a bent hook. Replace all seals.
• Remove the pressure relief valve sub-assembly (78); unscrew the ball seat (24) carefully from the spring seat (29) using soft jaws.
When all components have been removed, clean and dry thoroughly
Re-assembly:
• Reverse the above directions; before re-attaching, fill the handle with fluid to the top.

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 TM-G84 Rev.: H DCR# 15-0406 DATE: 5/5/15 Federal Identification Code: 11815 © 2015 Cherry Aerospace

HANDLE SUB-ASSEMBLY
Disassembly:
• Remove parts (65) through (69). Remove screws (76). Lift head assembly from the handle (33); empty and dispose of fluid
according to environmental regulations.
• Unthread the locknut (64) with a 1/2" socket wrench and then remove the air piston (63) by using wrench 700B65; hold the top
of the piston with tool 700A61 to prevent from turning. Push piston out when completely unthreaded
• Push the power piston (79) all the way up and remove packing plug (59) with the help of wrench 700B65.
• Tap the power cylinder (37) from the top; when loosened, it will fall through the bottom.
• Remove all the seals using a bent hook tool.
Assembly:
• The re-assembly sequence is the opposite of disassembly; to prevent damage to piston threads, the tightening torque for the
locknut (64) must be between 50 and 59 in.-lb. (5.65 and 6.67 N-m).

TROUBLESHOOTING GUIDE
PROBLEM POSSIBLE REASONS / SOLUTIONS

- No air supply is connected:

Connect to a clean, filtered air source at 90 to 110 psi (6,2 to 7,6 bar).
Piston does not move after depressing Trigger - Faulty trigger: Remove and replace trigger assembly.
- Broken power piston: Service the Handle Subassembly.

- Significant fluid loss: Bleed the system to purge the air out.
Short stroke or low pull force
If performance doesn’t improve, or excessive leakage continues, see below.
- Leaks around the seals or fittings indicate that they are not tightened to seal
properly: Tighten until no more leaks are observed.
Head Cylinder Fluid leakage
- Leaks at the front or back of head cylinder indicate worn/ damaged seals
Service head cylinder per instructions provided herein
- Broken or dislodged valve spring.
Air leakage at the spool valve - Worn or damaged valve spool seals: Disassemble and service air valve per Air
Sub-Assembly Overhaul Instructions.
- Piston or seal damage: Service head cylinder.
- Oil bypassing due to power piston displacement off its seat: Service Handle
Head piston is slow or seizes Subassembly per instructions provided below.
- Clogged air muffler or filter Clean thoroughly with solvent and back-blow with
compressed air.
- Pressure relief valve (78) malfunction: Remove, inspect and clean components
Head Piston (64) does not return fully forward thoroughly. Replace seals and damaged components.
even after system bleeding - Return Cylinder Spring (34) is damaged or broken: Remove head assembly and
replace the damaged spring. Re-assemble, fill and bleed per page 6.

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 TM-G84 Rev.: H DCR# 15-0406 DATE: 5/5/15 Federal Identification Code: 11815 © 2015 Cherry Aerospace

CROSS SECTION OF G84

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 TM-G84 Rev.: H DCR# 15-0406 DATE: 5/5/15 Federal Identification Code: 11815 © 2015 Cherry Aerospace

PART LIST
Model No.: G84 (P/N 744-090)
PART ITEM NO. PART NO. DESCRIPTION QTY
ITEM NO. DESCRIPTION QTY
NO. 37 744-089 CYLINDER. POWER 1
744-092 SUB-ASSEMBLY- HEAD
38 P-833** O-RING. DISOGRIN 1
1 530A16 DEFLECTOR. PIN 1 39 P-892** O-RING, DISOGRIN 1
2 560A17 FITTING, DEFLECTOR 1 40 P-908 RING. BACK-UP 1
3 530A20-1 SPRING 1 79 744-088 SUB-ASSEMBLY, POWER PISTON AND ROD
4 744-083 CAP, END 1 41 744-087 CAP. PISTON ROD 1
5 P-1252 O-RING 1 42 740A9 PISTON. POWER 1
6 P-1389 RING. QUAD 1 43 740A12 STOP. PISTON 1
7 P-1390 RING. BACK-UP 2 44 744-086 ROD. POWER PISTON 1
8 P-196 O-RING 1 45 P-268 O-RING 4
9 P-300 RING. RETAINING 1 46 740B14 SLEEVE. VALVE 1
10 744-093 PISTON, HEAD 1 47 740A18 SPRING 1
11 P-568 O-RING 2 48 P-891** 0-RING, DISOGRIN 3
12 P-242 RING. BACK-UP 1 80 740A15 SUB-ASSEMBLY. VALVE SPOOL
13 744-096 CYLINDER. HEAD 1 49 740B15-1* SPOOL. VALVE 1
14 700-258 SHIM. STEEL A/R 50 700A18* FILTER 1
77 700-211 SUB ASSEMBLY, ADAPTER 51 700A69* SCREW. METERING 1
15 P-699 RING. RETAINING 1 52 P-848 O-RING 2
16 700-257 SPACER. ADAPTER 3 53 740B16 PLUG. VALVE 1
17 P-957 RING. RETAINING 1 54 740A17 MUFFLER 1
18 P-1372 SPRING 1 55 P-321 RING RETAINING 1
19 700-255 EXTENSION. HEAD 1 56 P-838** O-RING. DISOGRIN 2
20 700-256 SLEEVE, LOCKING 1 57 P-115 RING. BACK-UP 2
21 P-573 SCREW. BUTTON HD CAP, 10.32 X 1/4 3 58 P 889
- O-RING 1
22 P-572 STAT-O-SEAL 3 59 740B13 PLUG. PACKING 1
78 700-214 SUB-ASSEMBLY. RELIEF VALVE 60 P-909 RING. BACK-UP 2
23 P-111 O-RING 1 61 P-887 RING. QUAD 1
24 700-215 SEAT. BALL 1 62 744-095* WASHER (inc w/Air Piston) 1
25 P-688 BALL (3/32) 1 63 744-094 PISTON. AIR 1
26 700-217 PISTON. VALVE 1 64 P-1392 NUT. CONELOK. 5/16-18 1
27 P-383 O-RING 1 65 P-890 O-RING 1
28 P-1366 SPRING 1 66 740C4 BASE. HANDLE 1
29 700-218 SEAT SPRING 1 67 P-886 RING. RETAINING 1
30 744-085 CYLINDER. RETURN 1 68 740B5 COVER. BASE 1

744-091 SUB-ASSEMBLY. HANDLE 69 P-884 RING. RETAINING 1

1 70 530A34 SWIVEL 1
31 703A33 SUB-ASSEMBLY. TRIGGER (includes P-223)
1 71 P-195 O-RING 2
32 P-223 O-RING
1 72 530A35 BOLT. SWIVEL 1
33 740R3 HANDLE
1 73 P-1505 PRESSURE REGULATOR 1
34 P-1391 SPRING
2 74 P-832** O-RING. DISOGRIN 1
35 P-508 O-RING
75 700A22 GASKET 1
36 744-084 PISTON, RETURN 1
76 P-73 SCREW, SOC HD CAP. 10-24 X 5/8 4

* NOT SOLD SEPARATELY

**NO SUBSTITUTIONS

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TM-G84 Rev.: H DCR# 15-0406 DATE: 5/5/15 Federal Identification Code: 11815 © 2015 Cherry Aerospace
EXPLODED VIEW OF G84

11
 Declaration of Conformity

We, Cherry Aerospace

Located at 1224 East Warner Avenue, Santa Ana, CA 92705-0157, USA,
In accordance with the provisions of
Machine Directive 2006/42/EC
Hereby declare under our sole responsibility that:
Equipment: Pneumatic Hydraulic Hand Riveter
Model Number: G-84
Serial Number: _____________________
Is in conformity with the applicable requirements of the following standards:
EN ISO 12100:2010 Safety of Machinery; General Principles for design; Risk Assessment and Reduction
ISO/TR 14121-1&2:2007 Safety of Machinery, Risk assessment
EN 792-1:2000 + A1:2008 Safety requirements; Assembly power tools for non-threaded mechanical fasteners
ISO 8662-11 Hand-held portable power tools -- Measurement of vibrations at the handle
ISO 3744 Acoustics – Determination of sound power levels of noise sources
ISO 4413:2010. Hydraulic fluid power - General Rules of safety
ISO 4414:2010. Pneumatic fluid power - General Rules of safety

Signed by: ________________________________

Cris Cobzaru,
Master of Science in Mechanical Engineering

Sr. Technical Services / Installation Tooling Engineer

The Technical documentation for the machinery is available from:

Name: Karl-Heinz Beckers
Position: CE Representative and Western Europe Sales Manager
Address: Maternusstrasse 14, D-52538, Gangelt, Germany
Mobile Phone +49 –(0) 171 31 88020