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For many years, the words Power-By-Victor
on the cowling of an aircraft have come to
represent the ultimate in quality, the best in
aviation piston engine technology. Victor
Aviations unique, down-to-earth attention to
personal service, meticulous detail and reliable
high performance have become recognized
across the U.S. and around the world as the
standard by which other overhaul facilities and
manufacturers are measured.
Legendary Quality
Legendary Air Show Pilot Bob Hoover chose Victor engines for his Shrike
Commander aircraft because he wanted performance, reliability and endurance.
Since 1983 Bob ew in over 570 air shows around the world and ew his
Power-By-Victor engines to T.B.O. several times with 5,000 hours of trouble
free use. No one else in the world can attest to this accomplishment, not
even the original engine manufacturer. Bobs Shrike Commander
can now be found at the Smithsonian Air & Space Museum
in Washington, D.C.
In my career, I couldnt
afford anything less than
the best. Victor engines are
the best in the business
Since 1977 the Victor organization has earned a worldwide reputation for quality
and excellence, utilizing innovative design techniques to improve performance
and advance the state-of-the-art of piston engine technology. Several pilots have
successfully own single engine aircraft Powered by Victor around the world setting
speed and endurance records.
Victor offers three levels of engine remanufacturing processes, depending upon the
customers individual needs: The Black Edition IITM, Limited Edition IITM, and the
Gold Edition IITM.
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X-15 Rocket Pilot Scott Crosseld ChoosesPower-By-Victor Black Edition IITM Engine.
Whether its Mach 2.0 or Mach .2
it is all a function of power.
Former X-15 research test pilot and propulsion engineer for
the National Advisory Committee for Aeronautics and North
American Aviation, Scott Crosseld, selected Victor Aviation
because he wanted an engine that he could count on. Scott
relied on his Power-By-Victor Black Edition IITM engine
throughout his career, ying his Cessna 210 to T.B.O. twice
with over 3,000 hours of reliable performance.
Scott was the rst to y successfully to Mach 2.0 and Mach
3.0 in the X-15 rocket plane and knew propulsion systems
intimately. Scott knew and appreciated Victors attention to
detail and trusted his life to his engine. Throughout Scotts
heavily decorated aviation career, Victor Aviation was the
only company that he ever endorsed, and became an advisor
and mentor to Victor Aviation. Victor and Scott pioneered
the technology used in Victors thrust velocity load cell
development and cryogenic engine technology.
Some of the experimental rocket planes that Scott ew were
the X-1, XF-92, X-4, X-5, X-15, Douglas D-558-1 Skystreak
and the Douglas D-558-II Skyrocket, which can now be found
at the Smithsonian Air & Space Museum in Washington, D.C.
Scott Crosseld 1921-2006
B-52 Launch Aircraft
X-15 Rocket Plane
Painted By: W.J Reynolds
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BLACK EDITION IITM
Valve train mid-lift geometry improved.
Volumetric efficiency balanced and flow tested.
Cylinder combustion chambers uniformity tested.
Inertia supercharging air flow optimization.
Real-time reciprocating and rotational balanced.
Iron manganese phosphate internal corrosion coated.
Premium formulated electrostatic black powder coated.
Crankcase three axis centerline machined.
Effective compression ratio balanced.
Thrust velocity load cell tested.
Full domain frequency vibration tested.
Extended limited workmanship warranty protection.
The Power-By-Victor Black Edition IITM Engine is designed for the pilot who demands the maximum operating potential from
his engine without sacricing safety or reliability. The benets of the Black Edition II TM Engine are improved safety, enhanced
reliability, proven endurance, and maximum performance. Victor Black Edition IITM Engines achieve their goal through an industry
unique, comprehensive twelve-point program:
Old-Time Craftsmanship Combined with State-of-the-Art
Technology Makes Victor Engines Better, Guaranteed.
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Unique BLACK EDITION IIEngine OVERHAUL Processes
The camshaft is precision ground or replaced with
matched tappet bodies for optimum fuel efciency.
Inertia supercharging helps maximize the volume of
air trapped in the cylinder for combustion by precisely
timing and delivering the proper charge of air. This
phenomenon takes advantage of the natural dynamiceffects and inertia of the air during the intake cycle.
RPM, cubic inch displacement, and air ow are related
factors that are evaluated to help determine proper
engine performance and horsepower which contribute
to the inertia supercharging effect. By maximizing the
kinetic energy of the air ow into the cylinders with the
inertia supercharging effect, the volumetric efciency
is improved and also engine power.
Valve Train Geometry
and Inertia Supercharging Optimization
Extracting maximum performance from the valve train is essential for best power
smoothness and longevity. As an engines valves open and close, the contact
angle between the valve and the rocker arm becomes critical to proper valve
operation and engine performance. Any valve side loading can decrease cylinder
efciency and reduce available horsepower. Victors Black Edition II TM Engines
are machined for minimum valve side loading at mid-lift geometry for improved
power, performance and reliability. To help achieve consistency, valve spring
pressures and heights are matched for more efcient engine operation.
Similarly, hydraulic lifters are matched for identical bleed-down rates to assure
uniformity of independent valve overlap timing and maximum throttle response.
Valve clearances are also set to consistent Power-By-Victor specications.
Rocker Arm
Valve
Intake Air
Hydraulic
Lifter
Camshaft
Connecting Rod
Crankshaft
90
Volumetric EfciencyBalancing and Flow Testing
Volumetric efciency testing measures airow into
each cylinder and allows Victor Aviation to match
cylinders for maximum power so that the pilot can
have the benet of using all available power uniformly
with all cylinders.
Horsepower of an engine is directly proportional to
the volume of air drawn into the cylinders and retained
until ignition occurs. With this F.A.A. accepted
process of polishing and removal of surface ashings
of the intake and exhaust systems, a signicant
improvement in volumetric efciency is available.
Its quite common to nd airow volume variations
as great as 15 percent between independent cylinders
which causes inconsistent cylinder horsepower
outputs. After cylinders are volumetrically balanced
all cylinders produce uniform airow to provide for
improved uniformity of power distribution.
Cylinder chamber and intake port volumes are also
cubic centimeter tested for uniformity by uid test
methods for improved engine power. Such precision
tests are virtually unique in the aircraft industry to
Power-By-Victor Black Edition IITM Engines.
Surface Flashings
Surface
Flashings
Cylinder Chamber
Air Flow
VOLUMETRIC EFFICIENCY =3456 X C.F.M.
C.I.D X R.P.M.
Tappet
Body
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Iron Manganese Phosphate Corrosion Coating
Internal engine parts are verysensitive to the effects of
corrosion which can cause
premature failure of the
engines camshaft, hydraulic
lifters, gears and other parts.
Iron manganese phosphate
coating is a F.A.A. accepted
process of acid etching a
lubricant into steel parts to
reduce friction and provide
for corrosion protection while
improving fuel efciency.
This chemical conversion treatment forms a crystalline coated surface which provides
for a signicant improvement in contact fatigue strength and can greatly improveengine parts life.
Full Domain Frequency Vibration Testing
Internal engine parts move at varying rates of motion and produce different
frequency signatures. Parts that move at different rates of motion can be identied
using a full domain frequency analyzer
and their respective amplitude of
vibration can be detected using a triaxialpiezoelectric accelerometer. This F.A.A.
accepted testing process enables Victors
technicians to not only test for complete
engine balance but isolate exactly what
internal parts are in need of balance
correction. This level of balancing
correction capability by far exceeds
industry standards and allows for a
smoother and more efcient engine.
Black Electrostatic
Powder Coating
This F.A.A. accepted process is a dry organic compound coating in whichelectrostatically charged particles of special resins and pigments are applied onto
the crankcase, sub-assemblies, intake system, housings and related components.
The engines crankcase and components are meticulously prepared, pre-assembled
by Victors technicians, then heated and degassed in preparation for powder coat
application. Then the positive charged particles are pneumatically sprayed and
adhere to the negatively charged parts surfaces and nish baked in a curing oven
at 400 degrees Fahrenheit to form an extremely tough, durable surface. In effect
this fuses the premium formulated powder to the components filling the
rough, porous surfaces to prevent aluminum oxide corrosion and reduces surface
fatigue cracking. Due to the special nature of Victors special black powder coat
engine heat emissivity is also improved. Emissivity is a measure of the efciency in
which a surface emits thermal energy and can result in improved parts life.
AccelerationAmplitude
DisplacementAmplitude
Frequency
100
m/s2
10
0.1
0.01
0 50 100 150 200
10-7
10-6
10-5
10-4
10-3
m
Hz
dx
ax
az
ay
Positive Electrostatic
Charged Pigments
and Resins
Original Aluminum Part Surface Emissivity Rating 0.07
Black Powdercoat Emissivity Rating 0.95
Thermal Emissivity
Coefcient Improved
Precision Crankshaft Balancing
Real-Time Reciprocatingand Rotational Engine Balancing
Engine thrust also may be increased by reducing
the amount of power wasted in attempting to offset
counterbalancing forces induced by out-of-balance
internal components. Improving parts balance allows
the engine to deliver more power to the propeller
and the engine becomes more efcient with less
wear on internal moving parts. Power-By-Victor
Black Edition IITM Engines are uniquely real-time
motion balanced by Victors A.S.E certied master
machinists to within one gram. With this F.A.A.
accepted process, individual parts and cumulative
reciprocating mass weights are balanced, to provide
for the best longevity and smoothness of the engine.
To illustrate the importance of proper balance, a
typical six-cylinder engine connecting rod travels
four inches. If a connecting rod were only 35
grams out of balance at a takeoff rpm of 2700, theresulting centrifugal force imbalance would be
approximately 255 pounds. Over a period of time, such
an imbalance could crack engine and accessory
mounts, crankcases, exhaust systems, cause premature
bearing failure, cause accelerated fatigue to sensitive
aircraft electronics, propeller, and structural members
of the aircraft. Additionally, an engine imbalance can
introduce unwanted vibration harmonics in ight
controls, navigational and ight instruments, and is
one of the leading causes for premature system fatigue.
Balancing not only improves thrust but also reduces
pilot and passenger fatigue by lowering the amplitude
of various vibration frequencies generated by theengine. The vibration that most pilots feel in an aircraft
is generally low frequency vibration, often unrelated to
propeller balance. Propeller dynamic balancing alone
will not remedy an internal engine vibration and may
only mask the symptoms of a larger problem. At Victor
Aviation, engine vibration is reduced as a cumulative
result of rotational, reciprocating and airow
balancing, improved valve train geometry, inertia
supercharging, friction reduction and fuel distribution.
Phosphate Corrosion Coating
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Cylinder EffectiveCompression Ratio Balancing
Black Edition IITM Engines include Power-By-Victors
volumetric efcient new cylinder process for improved
cylinder efciency, and are further enhanced by
improving the cylinder effective compression ratio
balance by selective cylinder positioning.
As the temperature of the inlet air to each cylinder
changes, so does the effective compression ratio of the
cylinder. When the intake air gets hotter, the effective
compression ratio decreases and when it gets colder the
effective compression ratio increases. This is similar
to the basic principle of how most intercooler systems
work. When these changes occur, the indicated mean
effective pressure of each cylinder changes, producing
inconsistent horsepower from cylinder to cylinder.
Engine cylinders are tested for combustion chamber
volume area and are very carefully positioned on each
engine. This maximizes the positive effects of enginetemperature, chamber volume and cylinder installation
position to improve effective compression balance and
uniformity of engine power.
Precision Three Axis Crankcase Machining
A common misconception is that conventional lapping and line honing alone always
results in a properly aligned and sized crankcase. This is untrue as line honing merely
follows existing discontinuities and lapping can create uneven thicknesses. Gear mesh
and bearing heat transfer problems may also occur. When necessary, crankcases are
straightened, then precision milled to avoid high metal loss, and nal machine boredutilizing precision boring equipment to assure proper alignment and size. Crankcase
journals are nish tested for size and journal geometry by airow differential
procedures to assure proper t. This minimizes piston side loading, reduces bearing
wear and provides equal loading on crankshaft main journals. Unlike line honing
which follows or changes the existing axis, line boring reestablishes the centerline of
the crankshaft axis, thereby insuring the centerline is parallel and equidistant to the
cylinder deck planes for enhanced engine performance.
Extended Warranty Protection
Black Edition IITM Engines are covered by a two
year or 750 hour limited warranty for workmanship
and prorated up to seven years or the manufacturers
recommended T.B.O. Accessories and new parts are
warranted by the original parts manufacturer. The
benet of this outstanding limited warranty saves you
money in the long run and covers most of an average
pilots years of ownership. In other words, when other
engine warranties expire, Victors is still going strong.
Precision Cylinder Machining
Precision Crankcase Alignment
Engine Thrust Velocity Load Cell Testing
Engine testing at Victor Aviation is the most extensive procedure used in the industry
and performed over a several day cycle process. Victors state-of-the-art mobile
engine testing apparatus, incorporates a thrust velocity load cell that measures
the actual thrust force of the propeller. Engines are installed into a hydraulicallyactivated engine mount, with engine accessories, induction system and exhaust
system installed, to simulate real-time engine test parameters. Using an electronic
load cell wafer, the engines real-time thrust velocity is recorded at all engine
speeds. Internal engine parts are vibration monitored using triaxial piezoelectric
accelerometers and a full domain frequency analysis to determine real-time internal
engine parts balance. During the test process, special dyes are put into the oil system
and examined under a black light canopy to detect for any discrepancies. Engines
are tested at maximum power and must meet Victors rigid test standards.
Thrust Velocity Load Test Cell
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LIMITED EDITION IITM
The Limited Edition IITM Engine is by far the most advanced engine remanufacturing technology available for the piston aircraft
industry. This engine series is designed to meet maximum engine durability, power and fuel efciency demands. With Victors
unique Limited Edition IITM modied engine processes and patents pending, we are able to advance engine reliability, longevity and
fuel efciency while adding signicant aircraft value. The Limited Edition IITM
engine series is valued by the Aircraft BluebookPrice Digest as a 100% added value to aircraft.
In addition to the twelve unique processes used on the Black Edition II TM Engine, the Limited Edition IITM Engine includes ten
additional state-of-the-art features and unique processes:
Cryogenic liquid nitrogen stress relieved.
Acoustic ultrasound spectroscopy tested.
Isotropic surface finished gears.
Vibratory stress relief tested.
Part surfaces pneumatic shot peened.
Multiple angle machined valves and seats.
Custom color electrostatic powder coated.
Ultrasonic high speed velocity tested.
Eddy current electromagnetic induction tested.
Extended limited workmanship warranty.
Victor Engines Go The Distance.
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Impact EnergySignal during th
period of impac
Noise
Microphone
Force
Cryogenic Liquid Nitrogen Stress Relieving
To reduce residual parts stress and improve engine performance, Victor
Aviation has a unique F.A.A. accepted patent pending process to test
parts over a 600 degree range in temperature from -300 to +300 degrees
Fahrenheit. This non destructive testing process is performed in a
computer controlled vacuum insulated cryogenic processing chamber
over a several day period in a Liquid Nitrogen atmosphere.
When metal castings cool and solidify during manufacturing, compressive
stresses develop in lower volume areas, which cool rst and tensilestresses develop in areas of greater volume, which are last to cool. Shear
stresses can develop between the different volume areas. The surface
cools rst and the core last. In such cases, residual stresses develop as a
result of the phase volume change between those layers that transform
rst and the center portion which transforms last. This testing process
can relieve these residual stresses, detect for improperly machined or
heat treated parts by measuring material volume changes, provide
for longer engine life, better fuel efciency, and improve engine
performance. Cryogenics is widely used by the NASA Space
Program, Aerospace Industry, NASCAR, and high performance engine
builders to improve parts durability, stability, and performance.
Resonant Ultrasound Spectroscopy Testing
The principle of acoustic resonance inspection is used to determine
the vibration signature of a part when exposed to an external force
or striker. Every part has its unique vibration signature or resonant
frequency. If there is an internal or external change or imperfection
to a part, the frequency of the part will change. Resonant inspection
can detect imperfections such as cracks, porosity, material density
or heat treating problems.
To determine a parts vibration signature, a striker will contact
the part and a microphone will record the resonant frequencies
generated on a full domain spectrum analyzer. These frequencies
can then be compared to
a known good part, and
in sets of similar part
numbers be matched for
frequency response and
quality control.
Advanced LIMITED EDITION II
Engine OVERHAUL Processes
Cryogenic Processing Chamber
Resonant Frequency Analysis
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Ultrasonic High Speed Velocity Testing
Using high frequency high speed sound waves, parts are scanned to gauge their integrity
and check for aws and material characterization. A pulse-echo ultrasonic measurement
can determine the location of a discontinuity within a part or structure by accurately
measuring the time required for a short ultrasonic pulse generated by a transducer to
travel through a thickness of the material. The pulse then reects from the back or surface
of the discontinuity and is returned to the transducer and can identify aws internally in
a part. Using ultrasonic high speed velocity testing can signicantly improve engine
longevity by detecting sub surface
aws that could have developed
into future parts failure.
_ 1- - -1
-
1
1
1
1
1
- 1- -
1 - _1
Multiple Angle Valve and Seat Machining
Engine intake air ows in and out of the combustion chamber through the intake
and exhaust system by the opening and closing of the valves. As the air passes
through the cylinder intake and exhaust ports, the ow of air can be affected by thecurvature or radius of the openings
caused by the shape of the valve
and seat angles. Using specialized
equipment, Victors technicians
can shape these openings and
improve the airow and venturi
characteristics by blending an
improved curvature radius into
the airow path. Multiple angle
valve and seat machining is
very effective in making the air
ow more efcient. As a result
improved engine performance and
fuel efciency can be obtained.
Isotropic Gear Surface Finishing
Engine parts are manufactured using grinding and cutting
methods that can cause high surface roughness or irregularities
in metal surfaces causing an anisotropic surface. This means that
the surface irregularities of the parts all run in the same direction.
These grinding marks can also interfere with non destructive
testing of a parts surface. This F.A.A. accepted process enables
technicians more reliable test indications when testing parts.
Isotropic surface nishing means that the part has been surfacenished, or honed, to obtain a surface that has no discernible
pattern thereby reducing friction, heat, noise, and reduces
contact fatigue. By exposing internal engine parts to a series of
improved optional surface nishing techniques utilizing media
in a specialized vibratory process, these surface roughness
problems are reduced, resulting in longer parts life, smoother
parts operation, improved lubrication and better fuel efciency.
Port Cylinder Head
Valve
Chamber
FlowDirection
45- 60Throat Angle
30Seat
15Top Cut
15Back Cut30Face (Seat In Middle)
Radius
Metal Surface Shot Peening
Engine parts are pneumatically shot peened by
impingement of metallic, glass, or plastic shot for
the purpose of increasing parts fatigue strength and
resistance to stress corrosion cracking. This F.A.A.
accepted process is accomplished by inducing residual
compressive stress in specied parts surfaces. As a
result of this unique process, critical stressed surface
areas prone to stress corrosion cracking are shot
peened to provide for longer lasting more durable
parts life.
Vibratory Stress Relief Testing
Vibratory parts testing is used to provide for more
reliable magnetic test indications during non
destructive testing of engine parts as a result of
any shifting of material composition. This F.A.A.
accepted process is also used to remove residual
stress of parts for improved parts durability. Vibratory
stress relief testing is performed by vibrating the parts
at a specic sub-harmonic vibration frequency while
monitoring with a vibration transducer and domain
spectrum analyzer to measure changes in residualstress concentrations. Using this process can improve
parts longevity by removing residual stress in parts.
Pulse Echo
TransducerFlaw
Immersion Ultrasonic Testing
Phased Array Ultrasonic Scan
Example Valve/Seat Multiple Angle Machining
Vibratory Testing
Shot Peening
Isotropic Finishing
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Extended LimitedWorkmanship Warranty
Limited Edition IITM Engines are covered by a ve
year or 1,000 hour limited warranty for workmanship
and then prorated up to ten years or the manufacturers
recommended T.B.O.
Accessories and new parts are warranted by the
original parts manufacturer. Warranty repairs are
available at any Victor Aviation preferred installationfacility or other pre-approved locations.
Custom Color Electrostatic
Powder Coatings
Victor Aviation has several high
performance custom color powder
coatings available. Customer maychoose select colors to meet their
aircraft design requirements.
Eddy Current Electromagnetic Induction Testing
Engine electrically conductive parts are tested using an electromagnetic induction
process. This process is very effective especially on aluminum castings such as
crankcases and housings. The advantage of this method is that it can detect fractures
or porosity problems beneath the surface of the material that are not detectable by
surface dye penetrant inspection techniques.
Eddy current uses alternating electrical current owing through a coil at a chosen
frequency and generates a magnetic eld around a coil or probe. When the coil is
placed next to a conductive material, eddy current is included in the material. If a aw
in the conductive material
disturbs the eddy current
circulation such as a crack
or porosity problem, the
magnetic coupling with
the probe is changed and
a defect signal can be read
by measuring the coil
impedance variation. This
process is an advancedparts inspection procedure
and can detect hidden
aws in materials before
they reveal themselves by
structural failure.
Preferred Installation Facilities
Victor Aviation can direct you to a Power-By-Victor
preferred installation facility near you. Our experience
indicates that engine operational problems can occur
as a result of improper engine installation techniques
or improper break-in. The benet of having an aircraft
engine changed by a Power-By-Victor preferred
installation facility is the extra condence and peace
of mind you receive by knowing the job is done right.
If you elect to y your aircraft to a Power-By-Victor
preferred installation facility, they can provide
engine removal and reinstallation, aircraft
inspection, propeller and accessory replacement
and avionics upgrade services.
a - The alternating current owing through the coil
at a chosen frequency generates a magnetic eld
around the coil.
b - When the coil is placed close to an electricallyconductive material, eddy current is included in the
material.
c - If a aw in the conductive material disturbs the
eddy current circulation, the magnetic coupling with
the probe is changed and a defect signal can be read
by measuring the coil impedance variation.
Eddy Current Non Destructive Testing
a cb
The term remanufactured is used to describe a Victor category or
process. The denition is not intended to contradict any authorized
manual, publication or an F.A.R. or F.A.A. authorized publication.
Processes, specications, warranty terms and conditions, subject to
change without notice at anytime.
Copyright 1993, Victor Aviation Service, Inc. 03/11
Custom Powder Coatings
IO-720 Limited Edition IITM
Engine Installation
Eddy Current Testing
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GOLD EDITION IITM
A Power-By-Victor Gold Edition IITM Engine is designed
for the high performance, experimental aircraft builder or
owner who wants the benets of a zero-time factory engine
that will perform like a Power-By-Victor engine.
We start by taking a zero-time factory new Textron Lycoming
or Teledyne Continental Motors engine and testing the engine in
our specially engineered load cell for thrust velocity, vibration
harmonics, and complete engine performance characteristics.
Using a spectrum analyzer and piezoelectric accelerometers, our
technicians can determine the frequencies and amplitudes of
internal moving parts to determine real-time internal motion
balancing prior to engine disassembly.
The engine is then completely disassembled, inspected and the
unique Power-By-Victor processes used in Victors Limited
Edition IITM Engine, are applied to the zero-time factory new
Textron Lycoming or Teledyne Continental Motors engine.
When we have completed the Power-By-Victor engineprocesses, the engine is then re-tested in our engine load cell
to assure that we have extracted the maximum performance
potential from the engine without sacricing engine reliability
or safety. By comparing the incoming and completed engine
test run data, Victors technicians are able to document the
improvement in engine performance.
Engines can be nished to customer specications and
custom powder coat colors are available. For experimental
aircraft applications, we work closely with the aircraft
builder and have several engine performance modications
and processes available.
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Power By Victor Engine Process Comparison
POWER BY VICTOR ENGINE PROCESSESBlack
Edition II
Limited
Edition II
Gold
Edition II
Factory
Engines*
Cryogenic Liquid Nitrogen Stress Relieved O X X N/A
Resonant Ultrasound Spectroscopy Tested O X X N/A
Isotropic Surface Finished Gears O X X N/A
Isotropic Surface Finished Crankshaft O O O N/A
Vibratory Stress Relief Tested O X X N/A
Metal Surfaces Shot Peened O X X N/A
Multiple Angle Machined Valves and Seats O X X N/A
Custom Color Electrostatic Powder Coated O X X N/A
Ultrasonic High Speed Velocity Tested X X X N/A
Eddy Current Electromagnetic Induction Tested X X X N/A
Valve Train Mid-Lift Geometry Improved X X X N/A
Matched Hydraulic Lifter Bleed Down Rates X X X N/A
Volumetric Efciency Balanced and Flow Tested X X X N/A
Uniformity Tested Cylinder Combustion Chambers X X X N/A
Inertia Supercharging Air Flow Optimization X X X N/A
Real-Time Reciprocating and Rotational Balanced X X X N/A
Iron Manganese Phosphate Corrosion Coated X X X N/A
Premium Electrostatic Black Powder Coated X X X N/A
Three Axis Centerline Machined Crankcase X X X X
Effective Compression Ratio Balanced X X X N/A
Thrust Velocity Load Cell Tested X X X N/A
Full Domain Frequency Vibration Tested X X X N/A
Express Limited Workmanship Warranty 7yrs 10yrs 10yrs 1-5yrs
Limited Warranty T.B.O. Prorated Coverage TBO TBO TBO N/A
O Optional
X Available
N/A Inapplicable
Processes, specications, and limited workmanship warranty coverage subject to
change without notice. Other terms and conditions apply. *Factory engine process
specications and details may vary.
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N*- Gold Edition IITM Exchange
N - Factory New Exchange
Prices subject to change without notice. Other terms and conditions apply.
Engine Pricing Comparison ExamplesManufacturers Suggested Retail Base Pricing Effective 1/1/11
Black Edition IITM Limited Edition IITM Factory New Gold Edition IITM
BEECHCRAFT BONANZA G36T.C.M. IO-550-B (33) 300HP Platinum
$41,853 $47,103 $47,525N $74,103N*
BEECHCRAFT BARON G58T.C.M. IO-550-C (46) 300HP Platinum
$41,853 $47,103 $47,499N $73,921N*
CESSNA CORVALIS 400 TTT.C.M. TSIO-550-C (11) 350HP Platinum
$64,628 $69,878 $80,492N $121,278N*
CESSNA STATIONAIR 206HTextron Lycoming IO-540-AC1A 300HP
$57,450 $63,950 $73,966N $106,450N*
CESSNA TURBO STATIONAIR T206HTextron Lycoming TIO-540-AJ1A 310HP
$68,302 $75,802 $106,204N $145,802N*
CIRRUS SR 22T.C.M. IO-550-N (22) 310HP Platinum
$42,272 $47,372 $48,495N $73,772N*
MOONEY OVATION 3T.C.M. IO-550-G (7) 310HP Platinum
$42,272 $47,372 $49,333N $73,772N*
MOONEY ACCLAIMT.C.M. TSIO-550-G (4) 280HP Platinum
$64,550 $71,050 $84,161N $125,422N*
PIPER SENECA VT.C.M. TSIO/LTSIO-360-RB (2) 220HP
$48,892 $55,392 $63,148N $92,392N*
PIPER MIRAGETextron Lycoming TIO-540-AE2A 350HP
$69,142 $76,642 $116,377N $159,642N*
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Aircraft values are representative averages and will vary based on equipment installed and condition of aircraft.
Prices subject to change without notice. Other terms and conditions apply.
Aircraft Value Comparison ExamplesAircraft Bluebook Price Digest - Spring 2011 Volume 11-1
AIRCRAFT MODELAdded
Aircraft Value
Average
Retail Value
Average
Retail Value @1,000hrs
2006 Beechcraft Bonanza G36
Zero-Time Rebuilt Engine $33,000 $406,501 $387,091
Black Edition IITM
Engine $49,242 $422,743 $412,893 Limited Edition IITM Engine $54,492 $427,993 $418,143
2006 Beechcraft Baron G58
Zero-Time Rebuilt Engine $33,000 $721,501 $702,091
Black Edition IITM Engine $49,641 $738,142 $728,292
Limited Edition IITM Engine $54,891 $743,392 $733,542
2006 Columbia 400
Zero-Time Rebuilt Engine $60,000 $370,000 $340,000
Black Edition IITM Engine $74,360 $384,360 $369,360
Limited Edition IITM Engine $79,610 $389,610 $374,610
2006 Cessna Stationair 206H Zero-Time Rebuilt Engine $45,000 $307,500 $285,000
Black Edition IITM Engine $64,530 $327,030 $315,780
Limited Edition IITM Engine $71,030 $333,530 $322,280
2006 Cessna Turbo Stationair T206H
Zero-Time Rebuilt Engine $52,000 $346,000 $320,000
Black Edition IITM Engine $76,081 $370,081 $357,081
Limited Edition IITM Engine $83,581 $377,581 $364,581
2006 Cirrus SR 22
Zero-Time Rebuilt Engine $33,000 $231,500 $215,000
Black Edition IITM Engine $48,531 $247,031 $238,781 Limited Edition IITM Engine $53,631 $252,131 $243,881
2008 Mooney Ovation 3
Zero-Time Rebuilt Engine $37,000 $371,000 $350,000
Black Edition IITM Engine $50,693 $384,693 $375,443
Limited Edition IITM Engine $55,793 $389,793 $380,543
2006 Mooney Acclaim
Zero-Time Rebuilt Engine $70,000 $444,000 $409,000
Black Edition IITM Engine $75,911 $450,911 $433,411
Limited EditionTM II Engine $82,411 $457,411 $439,911
2006 Piper Seneca V
Zero-Time Rebuilt Engine $45,000 $487,500 $465,000
Black Edition IITM Engine $57,797 $500,297 $487,797
Limited Edition IITM Engine $64,297 $506,797 $494,297
2006 Piper Mirage
Zero-Time Rebuilt Engine $75,000 $727,500 $690,000
Black Edition IITM Engine $83,291 $735,792 $717,042
Limited Edition IITM Engine $90,791 $743,291 $724,541
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P.O. Box 50608, Palo Alto, CA 94303-0608
TEL: (650) 354-1399 - FAX: (650) 354-1395
www.victor-aviation.com
Approved FAA Repair Station #BJ3R399L