Quickie Q2 Lite Instructions for use

Q2 Quickie Construction Manual
The QUICKIE Q2 kit, properly constructed, will reproduce the successful
original QUICKIE Q2 designed, and tested by QUICKIE AIRCRAFT CORPORATION.
QUICKIE AIRCRAFT CORPORATION is not responsible, and makes no warranties,
express or implied whatsoever, regarding the structural integrity,
performance, flight characteristics, or safety of the Buyer's completed
aircraft and its component parts. QUICKIE AIRCRAFT CORPORATION has no control
and assumes no control over the Buyer's ability to successfully construct and
test the QUICKIE Q2 AIRCRAFT. Buyer expressly waives any and all claims
arising from structural integrity, performance, flight characteristics,
mechanical failures, and safety against QUICKIE AIRCRAFT CORPORATION. Buyer
acknowledges awareness of the risks of flying a homebuilt aircraft. Buyer
acknowledges that the FAA must inspect the aircraft at construction intervals,
as well as the completed project, prior to flight and should work with his
local FAA representative regarding the construction and licensing of the
aircraft.
..
QUICKIE AIRCRAFT CORPORATION reserves the right to make recommended revisions
in the plans and construction of the aircraft at any time without liability to
QUICKIE AIRCRAFT CORPORATION, as such revisions or changes may be deemed
advisable from time to time.

Q2 Plans – Appendix Page i
TABLE OF CONTENTS
CHAPTER TITLE NO. OF PAGES NO. OF SHEETS
SECTION I
1 DESCRIPTION AND INTRODUCTION 3 2
2 BILL OF MATERIALS 1 1
3 COMPOSITE MATERIALS EDUCATION 23 12
4 INDIVIDUAL PART CONSTRUCTION 2 1
5 HOT-WIRING 4 2
6AILERONS, RUDDER, AND
ELEVATORS CONSTRUCTION 3 2
7 VERTICAL FIN CONSTRUCTION 2 1
8 BASIC FUSELAGE ASSEMBLY 5 3
9 MAIN WING CONSTRUCTION 9 5
10 CANARD CONSTRUCTION 10 5
11 WHEEL PANT/TIRE/WHEEL/BRAKE
ASSEMBLY 6 3
12 MAIN WING AND CANARD MOUNTING 3 2
13 CANOPY ASSEMBLY AND MOUNTING 4 2
14 FUSELAGE DETAIL ASSEMBLY 10 5
- APPENDIX SHEETS 1 THRU 6 6 6
SECTION II
15 MAKING YOUR Q2 TRAILERABLE 2 1
16 ENGINE INSTALLATION 6 3
17 FUEL SYSTEM INSTALLATION 3 2
18 INSTRUMENT AND PITOT-STATIC
SYSTEM INSTALLATION 1 1
19 ELECTRICAL SYSTEM 1 1
20 COMPLETING YOUR Q2 5 3

ADDITIONAL Q2 DOCUMENTATION
TITLE CONTENTS DATE OF FIRST
PUBLICATION
Q2 Pilot's Manual Flight and maintenance manual includes
normal and emergency procedures, weight
and balance, check lists, detailed flying
qualities descriptions, operating
limitations, performance charts, first
flight test procedures, pilot checkout
procedures, and systems descriptions.
1 May, 1981
Quickie Newsletter Published quarterly (Jan, April, July,
and October); includes plans changes,
builder tips, options, current and future
developments, and dates and information
on future seminars.
25 May, 1978
Q2 Information
Package Provides general information on the Q2, including performance, construction
techniques, and a poster.
9 February,
1981
Quickie & 'Q2
Composite Materials
Introductory
Package
Provides an education in the techniques
required in the building of a Q2.
Includes a booklet, and sufficient
materials for several suggested projects.
Somewhat redundant with Chapter 3 of the
Q2 Construction Plans.
8 April,
1981
Q2 Plans - Appendix Page ii
Q2 PLANS ADDENDUM

Q2 Builder Tip Notices (Q2BT9) are intended to provide clarification,
guidance, improved construction methods, and helpful hints of a non-
mandatory nature. The builder, at his discretion may use or discard
any Q2BT. Most are a result of work accomplished at Quickie Aircraft
Corporation building a Q2 from the Q2 Construction Plans. Any
questions on a Q2BT notice should be referred to Quickie Aircraft
Corporation. Each Q2BT has a number and a publication date along with
a description of the builder tip.
NUMBER DATE DESCRIPTION
Q2BT9 1 July, 1981 Q2 CONSTRUCTION PLANS -
SECTION I: Some plan sets sent
out may have faint re-
production on parts of pages
9-8, 10-1, 10-2, 10-3, 11-4,
14-2, and Appendix Sheet 4. We
intend to have those sections
reprinted within 30 days. We
will send the reprinted sheets
to any builder who reports
this problem.
Q2 Plans Change Notices (Q2PC9 & Q2PC10) are mandatory revisions to
the Q2 plans. Each Q2PC has a number and a publication date along
with a description of the change. All Q2PC notices should be
incorporated into the builder's set of Q2 Construction Plans
immediately upon receipt by the builder. Any questions on a Q2PC
notice should be referred to Quickie Aircraft Corp.
NUMBER DATE DESCRIPTION
Q2PC9 1 July, 1981 Q2 GROUND ANGLE OF ATTACK:
With the aircraft assembled
and WL15 level, and with the
aircraft on a reasonable level
floor, take a measurement
vertically between the floor
and the bottom of the
tailwheel. The nominal
measurement should be 27". A
range from 25" to 28.6" should
be Acceptable. This limitation
is to assist tailwheel first
landings and
three point takeoffs at
mid/forward c.g. Small change
can be effected by changing
the tailwheel diameter. It is
a good idea to delay mounting
the tailspring until the
aircraft is assembled, so that

the proper height can be
achieved.
Q2PC10 1 July, 1981 ENGINE MOUNT INSTALLATION, P-
16-2 does not indicate the
required spacer. The material
is 4130 steel, or mild steel
of 1/2" 0.0. x 3/8" 1.0. The
sketch indicates the location
of this QEM5 spacer (4
required).
ii
Q2 Plans - Appendix Page iii
NUMBER DATE DESCRIPTION

Q2BT11 21 August,
1981 MASS BALANCING ELEVATORS. In preparation for testing on
turbocharged Revmasters and
possible A-65 thru C-85
installations, we have further
explored the very high speed area
of the Q2 operating envelope. We
have found that mass balancing the
elevators improves the ride
qualities at high speed. Therefore,
we are supplying to all builders
the drawings and hardware to mass
balance all Q2 elevators, and
recommend this before first flight.
See pages...for details.
ELEVATOR MASS BALANCING
.....Locate the two Q2CSA11 arms and the molded lead weights.
.....These elevator mass balance arms can be retrofitted to the elevator
control system even after the canard has been mounted to the fuselage.
This will allow a closer clearance with the fuselage sides and maximize
the available legroom. If the mass balance arms are installed prior to
mounting the canard, careful measurements must be made to assure
clearance with the fuselage sides.
.....Begin by attaching a molded lead weight to each Q2CSA11 as shown.
.....Next, remove the two bolts holding CS20 in position, and slide it
outboard through the CS14 phenolic bearing until a Q2CSA11 arm can be
slid onto the tube with the lead weight projecting forward. Reinstall the
bolts holding CS20 in position.
.....Then remove the three bolts securing Q2CSA8 and slip it inboard
until the second Q2CSA11 arm can be slid on the outboard end inward with
the lead weight projecting forward. Reinstall the bolts holding Q2CSA8 in
place.
.....Locate the Elevator Rigging template and jig the elevator in the
full trailing edge up position. With the elevator in this position, each
Q2CSA11 should be almost resting on the canard upper surface just inboard
of the fuselage. Note the piece of felt called out as a bumper stop. The
Q2CSA11's are located as far outboard as practical so as not to interfere
with pilot or passenger legroom. Verify that when the elevator is rotated
to full trailing edge down position, that the arc of each Q2CSA11 clears
the fuselage and all other components.
.....Finally, return the elevator to the full trailing edge up position
with each Q2CSA11 resting almost on the canard, and drill in the one AN3-
12A bolt per side to attach the Q2CSA11's to Q2CSA8 and CS20.
.....Leave the CS13 pitch control arm unattached from Q2CSA8, and remove
the two AN4-11A bolts attaching the universal joint to Q2CSA8 and CS20.
Remove the universal joint so that each elevator can rotate independently
of the other. Make sure that you have lubricated all of the bearing and
hinge points to reduce the system friction to a minimum. It is desirable
for each elevator to balance at 0 degrees to 2 degrees trailing edge up
with all painting and finishing complete. Remove lead, as necessary from
the molded lead weight until that position is reached. Each elevator
should rotate freely about the hinge points when given a slight nudge.

Failure of this check means that the pivots are too tight and must be
adjusted for minimum friction.
.....Once the amount of lead weight on each elevator has been adjusted,
bolt the entire pitch control system together and check for friction,
excess play, and interferences.
iii
Q2 Plans - Appendix Page iv
NUMBER DATE DESCRIPTION

Q2BT12 21 August, 1981 IMPROVED BRAKING EFFECTIVNESS. We
have determined that a single pull
brake handle modulating both main
gear brakes simultaneously is
superior in nearly all situations
to the standard toe brakes.
Materials and drawings are
available for retrofit for all
builders returning their unused
Q2BSW1's & two AN210-1A pullies to
QAC. Current kit shipments
incorporate this modification as
standard.
Development work continues on a
set of retrofittable hydraulic
disc brakes, which may be
available as early as October,
1981. Those builders not ready to
fly before then may wish to wait
and decide whether they wish to
retrofit that system instead.
SINGLE PULL BRAKE HANDLE INSTALLATION
.....This section replaces the original section on installing the Brake
Pedals (Q2BSW1's) and four inboard pulleys. In place of the individually
controlled toe brakes, a single pull handle has been incorporated on the
left side of the cockpit.
.....Begin by fabricating BS3 and BS5 from the 0.125" thick Aluminum and
BS4 from 1/4" plywood.
(see next page for drawing)

.....BS4
is mounted in position with flox and 2 BID tapes to the top of the fuel
tank near the left side console. Position the BS4 so that the handle
will be an easy and comfortable reach for the pilot and so it will not
interfere unnecessarily with pilot comfort.
.....Next, install the Brake Handle as shown in the sketch.
.....The Brake Equalizer is used to help proportion braking
effectiveness equally. The turnbuckle assembly on the left side must be
attached directly to BS5 because of the proximity of the cable to the
left elevator slot foam core. The turn buckle for the right side can be
mounted in the system outboard of the Canard shear web pulley.
The two BS3 Canard shear web pulley mounts shown on page 11-4 must be
modified in location for the proper angles.
The cable routing is from the BS5 Brake Equalizer around the two pulleys
on the canard shear web, and then outboard through the Elevator slot
foam cores as originally indicated.....
The turnbuckles are adjusted to provide equal braking on each wheel.
iv

Q2 Plans - Appendix Page v
Q2 Plans - Chapter 1 - Page 1-1

DESCRIPTION AND INTRODUCTION
DESCRIPTION AND INTRODUCTION: The Q2 is a high performance, homebuilt
aircraft. Its compact external size and extremely efficient design
results in superb performance and unequalled fuel economy using a low
horsepower engine. Inside, it provides side-by-side seating comfort
for a pilot up to 6'8" tall and 250 lbs, plus passenger, as well as
some baggage in the roomy compartment behind the seat. Its canard
configuration was designed not only for performance, but to provide
improved flying qualities and safety as compared to the conventional
light plane.
.....The origin of the Q2 dates back to 1977. Although the Q2 has
much in common with the QUICKIE, considerable progress has been made
since that earlier effort. As a result, the Q2 has lower drag than
any other two place aircraft available to the public. Likewise, it
has proven to be the most fuel efficient two-place aircraft ever
offered to the public.
.....The Q2's high-lift canard (forward wing) is fitted with a plain
elevator that controls the aircraft's pitch attitude. The canard also
serves as the main landing gear spring since the main gear is mounted
on the tips of the canard. This feature results in a remarkably
smooth ride as well as outstanding ground stability during taxiing,
takeoff, and landing.
.....Roll capability is provided by ailerons on the inboard position
of the main wing.
.....Yaw control is provided by a rudder mounted on the vertical fin,
and is actuated by conventional rudder pedals.
.....The pitch and roll capability is provided by a side stick
controller in the center of the cockpit. This feature permits precise
control of the Q2 while reducing pilot fatigue and cockpit clutter.
.....Optional dual controls provide the option of pilot checkout and
instruction.
.....The tail wheel is actuated directly from the rudder pedals,
without any springs, thus providing positive steering at all times
while on the ground.
.....Since the tail wheel is not raised on takeoff roll like other
tail draggers, this positive steering is available until the aircraft
is airborne, making for very safe takeoff and landing
characteristics.
.....Even though the Q2 has low horsepower, it can outperform most
general aviation aircraft while retaining unequalled fuel economy.
The maximum speed is actually faster than most retractable gear
aircraft, such as the Piper Arrow, and the fuel economy exceeds
60 miles per gallon.
.....The Q2 obtains this remarkable performance without resorting to
retractable landing gear, without flaps, without turbochargers, and
without variable pitch propellers.
.....Further, the Q2 was designed to be built by the inexperienced
builder, so these Q2 Construction Plans and the Q2 kit contents have
been developed for ease of construction. Construction time should
require only 500 man hours spread over less than one year of the
builders spare time, with no special tools required.

.....The composite structure of your Q2 provides some important
advantages over conventional metal, wood, or fabric construction. It
has been tested to loads far in excess of those required for FAA
certification. Fatigue margins are higher. Contour is maintained
under load, the structure does not "oil can," buckle, or distort. It
provides excellent insulation and damps noise. It has no hidden
joints, no water traps, and is far less susceptible to corrosion.
It is easier to inspect, more redundant and easier to repair. It is
not susceptible to thermal stress due to temperature changes.
Properly protected from UV, it has an unlimited life.
Perspective
.....The builder of an amateur-built aircraft is the manufacturer; he
is responsible for quality control on all parts, all construction,
and the conduct of his flight tests. While Quickie Aircraft
Corporation is not the manufacturer of your aircraft, we do, through
these plans and services, provide you with information about how our
Q2 was built and what we feel is the best way for you to build a
safe, reliable airplane. We do encourage you. to build the airplane
as shown on the plans because we have found that our airplane
provides us with reliability and safety, and any problems that we
experience with our aircraft are documented and reported in "The
Quickie Newsletter". We have gone to a considerable effort in
developing the design, the structure, and the systems, and proving
their adequacy with appropriate tests.
.....If you modify the airplane and then ask us if your modification
will work, we cannot give you an answer without conducting the
appropriate tests and totally qualifying the modification. This would
obviously be quite expensive. Our concern then, is that if your
modification is not successful, and causes an incident or accident,
this would be attributed to our design, the Q2. Because of this, we
must insist that if you modify the airplane with any major change
such as an aerodynamic change, primary structural change, or using a
non-approved engine installation, that you call your airplane a
different name, rather than a Q2. If you make a major change, you
must consider yourself involved in basic aircraft design and
development, an extremely risky business. As such it is not fair for
us to be associated with any results of your development. We state
this, not to discourage inventiveness and progress, but to release
any connection of your new development efforts with our proven
design, the Q2.
.....We are particularly concerned about individuals using alternate
engines to power their Q2's. The Q2 was designed around the engine;
any change would require an exhaustive test program to determine not
only the new engine's suitability as an aircraft power plant, but
also its suitability as a Q2 power plant.
.....These Q2 Construction Plans have been specifically designed to
educate you in the construction materials, their use, and to guide
you through each step of assembly in the most efficient manner
possible. It is our intent to drastically reduce the non-completion
rate* common to homebuilt aircraft. With that in mind, we have:
1. Preceded the plans with an education section intended to

thoroughly acquaint you with the tools and materials, and
how to use them.
2. Laid out the plans in a detailed, step-by-step format to
answer the questions of "what do I do next?"
3. Provided all appropriate information to each step
adjacent to the words.
4. Provided full-size templates, ready to cutout and use, to
avoid the work and confusion associated with scaling up
drawings.
5. Provided a complete kit from one source to eliminate time
spent looking for materials.
6. Identified the difficult to build items, and included
them (prefabricated and ready to install) with the basic
Q2 Kit.
7. Set up our newsletter, "The Quickie Newsletter" as a
continuing plans updating/correcting system.**
*..Over 80% of homebuilt airplane construction projects
started, are never finished and flown.
** Because plans updates occasionally are of a mandatory
nature, a subscription to "The Quickie Newsletter" is
mandatory for those building a Q2.
PAGE
1-1
Q2 Plans - Chapter 1 - Page 1-2

Building Sequence
.....The nature of the Q2 structure requires that a part be left alone
to cure for a longer period of time than that required to build it.
Thus, you will find that when following the step-by-step order, you will
often find yourself out of work, waiting for a cure. In most cases you
can skip to another chapter and build another part while waiting. With a
little planning and familiarity with the entire manual, you should be
able to use all of your time productively.
Questions?
.....Please use the procedure detailed here if you do not understand
something and need an answer. First of all, do not be concerned if you
do not understand everything the first time you read through the plans.
Many things that may not be obvious just reading the drawings, will be
obvious when you have that portion of the airplane in front of you or
have built a similar part in a previous chapter. Also, we will be able
to help you better if you are looking at that portion of your airplane.
So, do not ask for clarification until you are really working-on that
particular chapter. We have found through our Quickie and Q2 experience
that the majority of questions that the homebuilder asks are already
answered somewhere in the plans. We have made considerable effort in the
Q2 Construction Plans to make the information visible. If you do not
understand something, study the words in the step, study the sketches
and all related sections/views/ photos, then look through the full size
drawings and components that show that portion of the airplane. If the
answer is still not found, it may be that the item is covered in detail
in another chapter (there is some necessary overlap). It is possible
that a question related to the operation of a part of the airplane or
its maintenance is answered in your Q2 Pilot's Manual. Also, check your
back issues of "The Quickie Newsletter" for plans updates or
clarifications. OK, if you have checked everything and you are still
stumped, you can do one of three things:
1. Ask a friend. Often a description of an item is unclear to one
individual and clear to another.
2. Write to Quickie Aircraft Corporation, leaving room on the paper
under each question for our answer. INCLUDE A SELF-ADDRESSED,
STAMPED ENVELOPE and INCLUDE YOUR AIRCRAFT SERIAL NUMBER. We do
our best to answer all such questions within two days of receipt.
We cannot answer questions regarding the application of non-
recommended materials or regarding non-approved modifications.
Quickie Aircraft Corporation
P.O. Box 786
Mojave, CA 93501
.....
Also, let us know if you have found a better way of doing something. If
we agree, we'll publish it in "The Quickie Newsletter" so that all

Quickie builders can benefit. If it is not a good idea, we'll tell you
why, if you include a self-addressed stamped envelope.
.....Do keep us up to date on the progress of your project. Send us a
black and white snap shot of your airplane for publication in "The
Quickie Newsletter". Photos in the newsletter are particularly
beneficial if they are of an area of the airplane that's not clearly
shown with photos or sketches in the plans. Remember, the primary
purpose of "The Quickie Newsletter" is to support your airplane project.
.....If you are not a member of The Experimental Aircraft Association
(EAA), do join. This is the only organization who looks out for the
homebuilder as far as FAA regulations are concerned. Membership in your
local EAA can be extremely beneficial both in building your airplane and
in meeting people who share your interests. Their monthly publication,
"Sport Aviation" is worth the membership fee in itself.
EAA
Box 229
Hales Corners, Wisconsin 53130
EAA often publishes reports on builder's projects, so send them photos
and some words on your progress.
FAA LICENSING PROCEDURES
This procedure applies in the U.S.A. only. The Federal Aviation
Administration (FAA) has a definite procedure for registering and
licensing homebuilt aircraft. There is nothing complicated about it, but
they insist that you follow each step carefully.
1. Contact your local FAA Engineering and
Manufacturing District Office or FAA General Aviation District
Office. Tell them you are building a Q2 homebuilt. Give them the
following information:
3-View drawing of the Q2
Aircraft serial number
Aircraft registration number, if available
(see step #2)
Approximate date of starting construction
Engine-type
FAA will then answer you, and tell you when they want to inspect
your airplane, where the approved test areas are, etc.
2. This step is optional, and applies only if you want to reserve a
specific registration number (the number you will paint on the
tail). You can ask for all numbers, numbers followed by a single
letter, or numbers followed by two letters. They are preceded by
the letter "N". (For example, N77Q, N8490P, etc.). Be sure to give
them your second and third choice, in case the number you want is
already taken. Send $10 to reserve your special number to:

FAA Aircraft Registry
Box 25082
Oklahoma City, OK. 73125
Do not register your aircraft yet, since you don't need to pay
registration fees, property taxes, etc., until your airplane is
ready to fly. If you do not desire a special number, then the FAA
will assign you a random number.
3. When you are ready for inspection* contact your local FAA office.
Be sure you have an airframe log book (available from EAA) so that
FAA can make an inspection entry.
4. To prepare for your final inspection, be sure you have: The "N"
number painted on, the "Experimental" sign (2" high letters) on
the canopy frame, the ID plate, and an airframe log book and an
engine log book.
Before final inspection, fill out an application for registration
(FAA form #AC8050-1), a notarized affidavit that you built the
airplane from parts that you bought yourself, and include $5
registration fee, along with copies of your sales agreement and
invoice signed by Quickie Aircraft Corporation. Send those things
to:
FAA Registry
Box 25082
Oklahoma City, OK 73125
5. After you have made a final inspection of your aircraft, run the
engine, etc., but prior to any taxi tests or flights, contact your
local FAA office and tell them you are ready to fly. They will
have you fill out an application for airworthiness (form #8130-6),
inspect your airplane, and issue you an airworthiness certificate
and a list of operating limitations. When you have completed your
initial test period, contact FAA to get your operating limitations
amended so you can fly outside your test area.
•Refer to education section - inspection is done to major areas
(wing, canard, and fuselage) after the glass is applied, but
before the area is painted with any primer, etc., so that the
glass structure can be inspected. The FAA office has been supplied
with the same inspection criteria that you are given in your
Composite Materials Education Chapter.
PAGE
1-2

Q2 Plans - Chapter 1 - Page 1-3

PAGE 1-3
Q2 Plans - Chapter 2 - Page 2-1
BILL OF MATERIALS
TOOLS
.....There are certain tools which are necessary to complete the
aircraft. Three lists of tools are provided here. The first is the
absolute bare minimum required, sacrificing efficiency; the second is a
recommended list for the best compromise of cost and work efficiency; the
third is a list for the "Cadillac" of shops where ease of construction is
more important than money. The non-common items are stocked by Aircraft
Spruce and Specialty.
FIRST LIST - BASIC REQUIRED TOOLS
•Common household butcher knife
•Coping saw
•1/4" drive socket set
•Small open-end wrenches
•Sandpaper.
50 sheets, 40-grit, 3M Production Paper D-wt.
50 Sheets, 80-grit, 3M Production Paper D-wt. 20 sheets, 240-grit,
3M Wet or Dry Tri-M-Ite Paper
A-wt. Silicon Carbide Waterproof.
20 sheets, 320-grit, 3M Wet or Dry Tri-M-Ite Paper
A-wt. Silicon Carbide Waterproof.
•Small Weights - Approx. 150 lbs in 5-15 lb pieces
•6 - 6" C-Clamps
•Square and half-round files
•Pliers
•1" putty knife
•Hacksaw
•Blade & Phillips screwdrivers
•Box of single-edge razor blades
•24" carpenter's level
•Carpenter's square
•Felt marking pens
•3-ft straightedge
•12-ft decimal steel tape (Stanley #61-112)
•1/4" drill with set of fraction and number bits,

#30, #32, #10, 1/4" and #12 bits
•Taps; 1/4-28, 10-32, 1/8 NPT (Pipe Tap)
•Roll of grey duct tape
•Saber saw
•Cheap hole saw set or flycutter
•Pop rivet puller
•Homemade balance for rationing epoxy
•Wall thermometer 50 to 100°F
•6-ft straightedge
•Small set of X-Acto knives
•Dremel-type miniature high-speed hand grinder with saw and router
bits
SECOND LIST - RECOMMENDED TOOLS
(In addition to those in the first list
•6" to 9" disc-type hand sander
•Set of 1/4",1/2" and 1" chisels (wood)
•1/2"-dia 100° counter sink (piloted)
•6" machinist steel ruler
•X-Acto razor saw
•3/8" variable-speed hand drill
•Hand broom/brush
•Bench-mounted belt sander
•Stanley surform plane
•Vacuum cleaner (shop type)
•Dovetail saw
•Epoxy Ratio Pump
•Plumb bob
THIRD LIST - FOR THE FIRST CLASS SHOP
(In addition to those in the first and second list)
•Drill press
•18-inch band saw
•Vernier Caliper
•90° drill adapter
•Air compressor with blow nozzle
•Orbital sander
•NICO press sleeve tool
•Clecos - one dozen 1/8"
•Hotwire Voltage Control
ITEMS USED ONLY OCCASIONALLY AND CAN BE BORROWED
•1 dozen 1/8" Clecos
•Hotwire Voltage Control