helicopter electromagnetic system

50
/- od/z f , C HEMLO PROJECT SUNEXCO ENERGY CORP ELECTROMAGNETIC PROFILE MAP COAXIAL SCALE 1/15,000 O K i lorn* t r* 1/2 1/2 Mil* AERODAT LIMITED DATE' March-June 1 983 N.T.S. No' 48-45' Marathon 86*00' 42C13SE0055 4 2C13SE00I2 WHITE LAKE (NORTH) 200 HELICOPTER E LECTROMAGNETIC SYSTEM Coil Configuration -Coaxial Separation ^7 metres Frequency - 45OO Hz. Mean Sensor Altitude -30 metres Horizontal Positioning- MRS m radar positioning l p.p.m. 30 i 20 - . 10 i O -N- In-phase Quadrature

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Page 1: HELICOPTER ELECTROMAGNETIC SYSTEM

/-

od/z f , C

HEMLO PROJECT

SUNEXCO ENERGY CORP

ELECTROMAGNETIC PROFILE MAP COAXIAL

SCALE 1/15,000 O K i lorn* t r*

1/2 1/2 Mil*

AERODAT LIMITED

DATE' March-June 1983

N.T.S. No'

48-45'

Marathon

86*00'

42C13SE0055 42C13SE00I2 WHITE LAKE (NORTH) 200

HELICOPTER E LECTROMAGNETIC SYSTEM

Coil Configuration -CoaxialSeparation ^7 metresFrequency - 45OO Hz.

Mean Sensor Altitude -30 metresHorizontal Positioning- MRS m radar positioning l

p.p.m. 30 i

20 -.

10 i

O

-N-In-phase

Quadrature

Page 2: HELICOPTER ELECTROMAGNETIC SYSTEM

42 4te if

HEMLO PROJECT

SUNEXCO ENERGY CORR

ELECTROMAGNETIC PROFILE MAP COPLANAR

SCALE 1/15,000 O l Kilometre

1/2 1/2 Mil*

AERODAT LIMITED

DATE: March-June 1983

N, T. S. No '

'AP No'

86*00'

48-45'

HELICOPTER ELECTR6MAGNETIC SYSTEM

Coil Configuration -CoplflnorSeparation - 7 metresFrequency -4100 Hz.

Mean Sensor Altitude -30 metresHorizontal Positioning-MRS IE radar positioning

p.p.m. 120 q

80 :

40 \

O

-N-

In-phase

Quadrature

*2C13SEa055 4 2CI3SE0812 WHITE LAKE (NORTH)

Page 3: HELICOPTER ELECTROMAGNETIC SYSTEM

\

HEMLO PROJECT

SUNEXCO ENERGY CORR

VLF-EM TOTAL FIELD

SCALE 1/15,000 Q Kilometre

1/2 1/2 Mile

AERODAT LIMITED

DATE' March-June 1983

N.T.S. No-'

1AP No-- 3

46*45'

86'00'

VLF-EM

Instrument 1 Herz Totem 2AStation; NAA Cutler, Maine-17.8 kHz.

Mean Sensor Altitude' 45 metresHorizontal Positioning- MRS UT radar positioning

-HJ-contour interval 2*Vo

NOTE : The total field will usually indicate a local maximum over the upper edge of a steeply dipping conductor.

42C13SEe655 42C53SE0812 WHITE LAKE (NORTH)

Page 4: HELICOPTER ELECTROMAGNETIC SYSTEM

\

HEMLO PROJECT

SUNEXCO ENERGY CORP

TOTAL MAGNETIC FIELD

SCALE 1/15,000 1 P 1 K i lorn* t r*

1/2 0 1/2 Mil*

^ DATE; March-June

VAEROOAT LIMITED N TS No1AP No: 4

mn minium li muni minium ii m ———————————————————

1983

86-00'MAGNETOMETERInstrument -- Geometrics 6-803Mean Sensor Altitude : 45 metresHorizontal Positioning-- MRS HI radar positioning

250 gammas.

5O gammas.

10 gammas. contour interval 10 gammas

fN

42C13SE0055 4aC13SE0*12 WHITE LAKE ( NORTH) 230

Page 5: HELICOPTER ELECTROMAGNETIC SYSTEM

HEMLO PROJECT

SUNEXCO ENERGY CORP

INTERPRETATION

SCALE 1/15,000 O Kilometre

1/2 1/2 Mile

AERODAT LIMITED

March-June 1983

IM. T. S. No :

^P No- 5

SUPERIOR

B6 0OO' INTERPRETATION

Interpreted conductive axis within bedrockPossible conductive axis within bedrock

- . Probable cultural conductor

AERODAT HEM SYSTEM RESPONSE VERTICAL HALF-PLANE

-N-

Frequency (Hf) 1 - Cooduclonce (Siemens)

100IN- PHASE (ppm]

42C13SE0055 42C13SEOai2 WHITE LAKE t NORTH) 240 r*

Page 6: HELICOPTER ELECTROMAGNETIC SYSTEM

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LAKE (NORTH) 010

REPORT ON

COMBINED HELICOPTER-BORNE

MAGNETIC AND ELECTROMAGNETIC

SURVEY

HEMLO, ONTARIO

RECEIVED•ji-'l o 1933

MINING LANDS SECTION

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B SUNEXCO ENERGY CORPORATION

by

AERODAT LIMITED

September, 1983

Page 7: HELICOPTER ELECTROMAGNETIC SYSTEM

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•n

1 i•1

Mi

Hi

1 B•i

I riE

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1 i1 ;11111111i11i

0 Q TABLE OF CONTENTS Q ———————————————————

••••••••••B

uHuMuMHHi

———— 5 1. INTRODUCTION^— — — t~——————— Of

* 2 . SURVEY AREA AND LOCATION"•""••1 Lil————. v

-' 3. AIRCRAFT EQUIPMENT AND PERSONNELz^HvZZiBM i~-

* 3.1 Aircraft•••••H ™ ~—————— 8

5 3.2 Equipment^^^^n n

2 3.2.1 Electromagnetic System*"^^"^!? LO

——— 1 3.2.2 VLF-EM System^^M-~~ 10""•^"M n

k] 3.2.3 Magnetometer

3.2.4 Magnetic Base Station

3.2.5 Radar Altimeter

3.2.6 Tracking Camera

3.2.7 7inalog Recorder

3.2.8 Digital Recorder

3.2.9 Radar Positioning System

4. DATA PRESENTATION

4.1 S'.ase Map and Flight Path Recovery

4.2 Electromagnetic Profile Maps

4.3 Magnetic Contour Maps

4.4 VLF-EM Contour Maps

5. INTERPRETATION

6. RECOMMENDATIONS

7. DISCUSSION OF RESULTS

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APPENDIX I - General Interpretive Considerations

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LIST OF MAPS

l(Scale: 1:15,000)

lMaps

l ~l Airborne Electromagnetic Survey Profiles

m 4 500 Hz (coaxial)

2 Airborne Electromagnetic Survey ProfilesI 4100 Hz (coplanar)

II 3 Total Field VLF-EM

m A Total Field Magnetic Map

5 Interpretation Map

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m 1 . INTRODUCTION

lH During the period of March 2 to June 14 , 1983

Aerodat carried out an airborne geophysical survey

l of approximately 1,570 square kilometers in the Hemlo

area of Ontario. Equipment operated include a 3

l frequency HEM and VLF electromagnetic systems, a

B magnetometer and a radar positioning device. At a

nominal line spacing of 100 meters a total of

l 15,770 line kilometers of data was acquired.

M This report, on behalf of Sunexco Energy Corporation

refers to a part of the overall survey, consisting of

K 44 line; kilometers, flown during the period of April 15

to April 30, 1983.

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2.

2-1

SURVEY AREA AND LOCATIONS

The index map below outlines the overall survey and

the location of the property to which this report

refers. The property outline and related mining

claim numbers are indicated on the maps accompanying

the report.

66'OO'

*8"*5!*fK—-*

LMKf

SUFffTIOf!

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.•*, ...-.j. - ...SP. ....

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3 -

ll al 3' AIRCRAFT EQUIPMENT

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3.1 Aircraft

The helicopter used for the survey was an Aerospatial

Astar 350D owned and operated by North Star Helicopters,

Installation of the geophysical and ancillary equipment

l was carried out by Aerodat. The survey aircraft was

flown at a nominal altitude at 60 meters.

3.2 Equipment

3.2.1 Electromagnetic System

* The electromagnetic system was an Aerodat/

l Geonics 3 frequency system. Two vertical

coaxial coil pairs were operated at 950 and

l 4500 Hz and a horizontal coplanar coil pair

at 4100 Hz. The transmitter-receiver separa-

* tion was 7 meters. In-phase and quadrature

M s ignals were measured simultaneously for the

3 frequencies with a time-constant, of 0.1

l seconds. The electromagnetic bird was towed

30 meters below the helicopter.

3 - 2 - 2 VLF-EM SystemaThe VLF-EM System was a Herz 1A. This instru-

I ment measures the. total field and vertical

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Page 13: HELICOPTER ELECTROMAGNETIC SYSTEM

l l 3-2

quadrature component of the selected frequency.

The sensor was towed in a bird 15 meters belowH

the helicopter. The station used was NAA,

l Cutler Maine, 17.8 KHz or NLK, Jim Creek

Washington, 24.8 KHz.

l3.2.3 Ma gne tome te r

l The magnetometer was a Geometrics G-803 proton

8 precession type. The sensitivity of the

instrument was l gamma at a 0.5 second sample

l rate. The sensor was towed in a bird 15 meters

— below the helicopter.

B3.2.4 Magnetic Base Stationl ————————

An IFG proton precession type "lagnetometer was

l operated at the base of operations to record

— diurnal variations of the earths magnetic

' field. The clock of the base station was

l synchronized with that of the airborne system.

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3-3

3.2.5 Radar Altimeter

A Hoffman HRA-100 radar altimeter was used to

record terrain clearance. The output from the

instrument is a linear function of altitude

for maximum accuracy.l3.2.6 Tracking Camera

A Geocam tracking camera was used to record

fi flight path on 35 mm film. The camera was

m operated in strip mode and the fiducial numbers

for cross reference to the analog and digital

l data were imprinted on the margin of the film.

B 3.2.7 Analog Recorder

M A RMS dot-matrix recorder was used to display

the data during the survey. A sample record

fi with channel identification and scales is

presented on the following page.

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ll^ft

ANALOG CHART

c AMP: RAFIDUCIAL ;*" .

VLF QUAD.

VLF TOTAL

1 VLF QUAD.*" ——— -™-, ____ ^

1 VLF TOTAL

|COPIJVNAR

1

1 COPLANAR . __ - —————— -^S—— , —— v-^——— ~—— ——— —— - ———

(ORTHO)^^,

1(LINE) ,.

QUA B., jt" ~~ .4

IIjj-PHASE ,,

25i

TVV,--'

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A

7,CX

*\MANUAL FIDUCIAL

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3-4

3.2.8 Digital Recorder

A Perle DAC/NAV data system recorded the survey

data on cassette magnetic tape. Information

recorded was as follows:

Equipment

EM

VLF-EM

magnetometer

altimeter

fiducial (time)

fiducial (manual)

Interval

0.1 second

0.5 second

0.5 second

l.O second

1.0 second

0.2 second

Page 17: HELICOPTER ELECTROMAGNETIC SYSTEM

13-5

3.2.9 Radar Positioning System

l

lA Motorola Mini-Ranger (MRS III) radar

navigation system was utilized for both

•j navigation and track recovery. Transponders

located at fixed known locations were inter-

Jj rogated several times per second and the ranges

from these points to the helicopter measured

™ to several meter accuracy. A navigational

Ij computer triangulates the position of the

helicopter and provides the pilot with naviga-

|| tion information. The range/range data was

recorded on magnetic tape for subsequent flightB" path determination.

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4-1

4. DATA PRESENTATION

4.1 Base Map and Flight Path Recovery

* maps

The base map, at a scale of 1/15,000 is an

enlargement of published 1/50,000 topographic

The flight path was derived from the Mini Ranger

radar positioning system. The distance from the

helicopter to two established reference locations

l was measured several times per second and the

position of the helicopter mathematically calcu-

I lated by triangulation. It is estimated that the

m flight path is generally accurate to about 30

meters, with respect to the topographic detail of

l the base map.

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l 4.2 Electromagnetic Profile Maps

l The electromagnetic data was recorded digitally at

a high sample rate of 10/second with a small time

" constant of 0.1 second. A two stage digital filtering

l process was ccirried out to reject major sferic events,

and reduce system noise.

Local atmospheric activity can produce sharp, large

H amplitude events that cannot be removed by conventional

filtering procedures. Smoothing or stacking will reduce

m their amplitude but leave a broader residual response

m that can be confused with a geological phenomenon. To

avoid this possibility, a computer algorithm searches

l out and rejects the major "sferic" events.

l The signal to noise was further enhanced by the

application of a low pass filter. The filter was

l applied digitally. It has zero phase shift which

M prevents any lag or peak displacement from occurring

and it suppresses only variation with a wavelength

l less than about 0.25 seconds. This low effective time

constant permits maximum profile shape resolution.

lFollowing the filtering processes, a base level

H correction was made. The correction applied is a linear

function of time that ensures that the corrected

™ amplitude of the various inphase and quadrature components

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Page 20: HELICOPTER ELECTROMAGNETIC SYSTEM

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4-3

is zero when no conductive or permeable source is

present. This filtered and levelled data was then—

am presented in profile map form.

The in-phase and quadrature responses of the coaxial

B 4500 Hz and the coplanar 4100 Hz configuration are

presented with flight path on the topographic base

map .lB 4.3 Magnetic Contour Maps

m The aeromagnetic data was corrected for diurnal

variations by subtraction of the digitally recorded

l base station magnetic profile. No correction for

regional variation is applied.

lThe corrected profile data was interpolated onto a

l regular grid at a 2.5 mm interval using a cubic

spline technique. The grid provided the basis for

™ threading the presented contours at a 10 gamma

M interval.

m 4 * 5 VLF-EM Contour Maps

The VLF-EM signal, was compiled in map form. The

B mean response level of the total field signal was

removed and the data was gridded and contoured at

an interval of 2?,.

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Page 21: HELICOPTER ELECTROMAGNETIC SYSTEM

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5. INTERPRETATION

B The electromagnetic profile maps and VLF contour

map were analysed and conductor axes interpreted.

The axes identified are divided into 2 classific

ations; "probable bedrock conductors" and "possible

bedrock conductors".

In the first category are those conductors that

l display relatively clear characteristics of a thin,

steeply dipping conductive source. A discussion

( of the HEM response shape is provided in the

H Appendix. Anomalies with less distinctive charac

teristics were also included in this category if

associated with a magnetic feature.

H The second category, "possible bedrock conductor"

were not adequately distinguished by HEM response

l shape or magnetic association to rule out a

conductive overburden source.

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6. RECOMMENDATIONS

l The "Hemlo" gold deposit is a very weak electro

magnetic conductor. Cultural interference along

B the road prevented reliable evaluation of electro-

m magnetic data over the main zone; however, weak

HEM and VLF-EM responses are noted along strike.

l The magnetic t-'ntour map clearly showed an assoc

iated linear magnetic anomaly of about 150 gammas

l amplitude.

l Gold mineralization, disseminated in the rock

cannot be expected to produce a measureable elect-

™ romagnetic anomaly. The associated geologic

B formation may become measureably conductive due to

accessory sulphide or graphite mineralization or

l even electrolytic conduction within faults and

shears.

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B Interpreted bedrock conductor axes indicate zones

potentially favourable to gold mineralization and

™ deserve ground follow-up investigation. Those

fl most familiar with the detailed geology of the area

can best evaluate the potential significance of the

jl conductors and magnetic features and assign relative

follow up priority.

lRespectfully submitted,

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" August. 24. 1983 R. L. Scott Flog

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7. DISCUSSION OF RESULTS

expression.

l The conductor locations are numbered for ident

ification cind discussion, cind do not imply priority.

(1) Moderate conductor, nuignetic low, vest of

l diabase dyke.

l (2) High amplitude, moderate conductor, no magnetic

l(3) Poor conductor, west of diabase dyke, on trend

l with (2).

l (4) Weak conductor, possibly surficial effect.

M ( 5) Modereite conductor, some magnetic response.

m ( 6) Weak conductor, on flank of magnetic trend.

— (7) Fair to good conductor, on trend with (2) and

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(8) Weak conductor, north contact of serpentinite.

g (9) Weak conductor, centre of serpentine body,

l (10) Fair, short conductor, south contact of serpen

tine .

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(11) Good conductor, contains associated magnetic

minerals.

(12) Weak conductor, on geological trend with (10)

Fenton Scott, P.Eng.

Page 26: HELICOPTER ELECTROMAGNETIC SYSTEM

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APPENDIX

GENERAL INTERPRETIVE CONSIDERATIONSlE le c t r om a g n et i c

l The Aerodat 3 frequency system utilizes 2 different

g transmitter-receiver coil geometries. The traditional

coaxial coil configuration is operated at 2 widely

l separated frequencies and the horizontal coplanar coil

pair is operated at a frequency approximately aligned

l with one of the coaxial frequencies.

l The electromagnetic response measured by the helicopter

system is a function of the "electrical" and "geometrical"

B properties of the conductor. The "electrical" property

M o f a conductor is determined largely by its conductivity

and its size and shape; the "geometrical" property of the

l response is largely a function of the conductors shape and

orientation with respect to the measuring transmitter and

recever .

Electrical Considerations

l For a given conductive body the measure of its conductivity

or conductance is closely related to the measured phase

l shift between the received and transmitted electromagnetic

m f ield. A small phase shift indicates a relatively high

conductance, a large phase shift lower conductance. A

l small phase shift results in a large in-phase to quadrature

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- 2 - APPENDIX I

ratio and a large phase shift a low ratio. This relation

ship is shown quantitatively for a vertical half-plane

model on the phasor dicigram. Other physical models will

show the same trend but different quantitative relation

ships.

The conductance and depth values as determined are correct

only as far as the model approximates the real geological

situation. The actual geological source may be of limited

length, have significant dip, its conductivity and thickness

may vary with depth and/or strike and adjacent bodies and

overburden may have modified the response. In general the

conductance estimate is less affected by these limitations

than the depth estimate but both should be considered a

relative rather than absolute guide to the anomalies

properties.

AERCCAT HEM SYSTEM RESPONSE VERTICAL HALF-PLANE

Page 28: HELICOPTER ELECTROMAGNETIC SYSTEM

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H

- 3 - APPENDIX

Conductance in mhos is the reciprocal of resistance in

ohms and in the case of narrow slab-like bodies is themm

product of electrical conductivity and thickness.

Most, overburden will have an indicated conductance of less

than 2 mhos; however, more conductive clays may have an

apparent conductance of say 2 to 4 mhos. Also in the low

l conductance range will be electrolytic conductors in

faults and shears.

The higher ranges of conductance, greater than 4 mhos,

indicate that a significant fraction of the electrical

n conduction is electronic rather than electrolytic in

nature. Materials that conduct electronically are limited

l to certain metallic sulphides and to graphite. High

conductance anomalies, roughly 10 mhos or greater, are

l generally limited to sulphide or graphite bearing rocks.

B Sulphide minerals with the exception of sphalerite, cinnabar

and stibnite are good conductors; however, they may occur

™ in a disseminated manner that inhibits electrical conduction

•j through the rock mass. In this case the apparent conductance

can seriously underrate the quality of the conductor in

l geological terms. In a similar sense the relatively non

conducting sulphide minerals noted above may be present in

™ significant concentration in association with minor conductive

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l^ - 4 - APPENDIX

1

l sulphides, and the electromagnetic response only relate

m to the minor associated mineralization. Indicated conductance

is also of little direct significance for the identification

B of gold mineralization. Although gold is highly conductive

it would not be expected to exist in sufficient quantity

l to create a recognizable anomaly, but minor accessory sulphide

m mineralization could provide a useful indirect indication.

H In summary, the estimated conductance of a conductor can

™ provide a relatively positive identification of significant

•j sulphide or graphite mineralization; however, a moderate

to low conductance value does not rule out the possibility

J of significant economic mineralization.

Geometrical Considerations

•j Geometrical information about, the geologic conductor can

often be interpreted from the profile shape of the anomaly,

f The change in shape is primarily related to the change in

m inductive coupling among the transmitter, the target, and

* the receiver.

m In the case of a thin, steeply dipping, sheet-like conductor,

m the coaxial coil pair will yield a near symmetric peak over

the conductor. On the other hand the coplanar coil pair will

l pass through a null couple re:lationship and yield a minimum

over the conductor, flanked by positive side lobes. As the

dip of the conductor decreases from vertical, the coaxial

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Page 30: HELICOPTER ELECTROMAGNETIC SYSTEM

l"~ - 5 - APPENDIX

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l anomaly shape changes only slightly, but in the case of

the coplanar coil pair the side lobe on the down dip side

l strengthens relative to that on the up dip side.

l As the thickness of the conductor increases, induced

current flow across the thickness of the conductor becomes

™ relatively significant and complete null coupling with the

H coplanar coils is no longer possible. As a result, the

apparent minimum of the coplanar response over the conductor

l diminishes with increasing thickness, and in the limiting

case of a fully 3 dimensional body or a horizontal layer

™ or half -space, the minimum disappears completely.

l A horizontal conducting layer such as overburden will produce

. a response in the coaxial and coplanar coils that is a

function of altitude (and conductivity if not uniform) . The

B profile shape will be similar in both coil configurations

with an amplitude ratio (copl anar/coaxial) of cibout 4/1.*

lIn the case of a spherical conductor, the induced currents

l are confined to the volume of the sphere, but not relatively

restricted to any arbitrary plane as in the case of a sheet-

9 like form. The response of the coplanar coil pair directly

m over the sphere may be up to 8* times greater than that of

the coaxial coil pair.

Page 31: HELICOPTER ELECTROMAGNETIC SYSTEM

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Jj In summary a steeply dipping, sheet-like conductor will

— display a decrease in the coplanar response coincident

* with the peak of the coaxial response. The relative

fl strength of this coplanar null is related inversely to

the thickness of the conductor; a pronounced null indicates

l a relatively thin conductor. The dip of such a conductor

— can be inferred from the relative amplitudes of the side-lobes.

Massive conductors that could be approximated by a conducting

" sphere will display a simple single peak profile form on both

B coaxial and coplanar coils, with a ratio between the coplanar

to coaxial response amplitudes as high as 8.*

Overburden anomalies often produce broad poorly defined

l anomaly profiles. In most cases the response of the coplanar

coils closely follows that of the coaxial coils with a

l relative amplitude ratio of 4.*

B Occasionally if the edge of an overburden zone is sharply

defined with some significant depth extent, an edge effect

* will occur in the coaxial coils. In the case of a horizontal

D conductive ring or ribbon, the coaxial response will consist

of two peaks, one over each edge; whereas the coplanar coil

g will yield a single peak.

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- 7 - APPENDIX

l ll * It should be noted at this point that Aerodat's definition

of the measured ppm unit is related to the primary field

l sensed in the receiving coil without normalization to the

. maximum coupled (coaxial configuration). If such normal-

ization were applied to the Aerodat units, the amplitude

l of the coplcinar coil pair would be halved.

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- 8 - APPENDIX

The Total Field Magnetic Map shows contours of thel

total magnetic field, uncorrected for regional varia-

I tion. Whether an EM anomaly with a magnetic correla

tion is more likely to be caused by a sulphide deposit

than one without depends on the type of mineralization.

An apparent coincidence between an EM and a magnetic

anomaly may be caused by a conductor which is also

l magnetic, or by a conductor which lies in close proximity

to a magnetic body. The majority of conductors which are

also magnetic are sulphides containing pyrrhotite and/or

n magnetite. Conductive and magnetic bodies in close

association can be, and often are, graphite and magnetite.

l It is often very difficult to distinguish between these

cases. If the conductor is also magnetic, it will usually

l produce an EM anomaly whose general pattern resembles

m that of the magnetics. Depending on the magnetic perme

ability of the conducting body, the amplitude of the

l inphase EM anomaly will be weakened, and if the conduc

tivity is also weak, the inphase EM anomaly may even be

l reversed in sign.

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l VLF Electromagnetics

l The VLF-EM method employs the radiation from powerful

military radio transmitters as the primary signals.

l The magnetic field associated with the primary field

M is elliptically polarized in the vicinity of electrical

conductors. The Herz Totem uses three orthogonal coils

C to measure the total field and vertical quadrature

component of the polarization ellipse.

lM The relatively high frequency of VLF 15-25 kHz provides

high response factors for bodies of low conductance.

l Relatively "disconnected" sulphide ores have been found

to produce measurable VLF signals. For the same reason,

y poor conductors such as sheared contacts, breccia zones,

I narrow faults, alteration zones and porous flow tops normally

produce VLF anomalies. The method can therefore be used

l effectively for geological mapping. The only relative dis

advantage of the method lies in its sensitivity to conductive

l overburden. In conductive ground the depth of exploration

M is severely limited.

The effect of strike direction is important in the sense

H of the relation of the conductor axis relative to the

H energizing electromagnetic field. A conductor aligned

along a radius drawn from a transmitting station will be

l

l

Page 35: HELICOPTER ELECTROMAGNETIC SYSTEM

l l

l

- 10 - APPENDIX I

l in a maximum coupled orientation and thereby produce a

stronger response than a similar conductor at a different

H strike angle. Theoretically it would be possible for a

l conductor, oriented tangentially to the transmitter to

produce no signal. The most obvious effect of the strike

l angle consideration is that conductors favourably oriented

with respect to the transmitter location and also near

" perpendicular to the flight direction are most clearly

B rendered and usually dominate the map presentation.

H The total field response is an indicator of the existence

ond position of a conductivity anomaly. The response will

l be a maximum over the conductor, without any special filtering,

and strongly favour the upper edge of the conductor even in

H the case of a relatively shallow dip.

l The vertical quadrature component over steeply dipping sheet

like conductor will be a cross-over type response with the

cross-over closely associated with the upper edge of the

conductor.

The response is a cross-over type due to the fact that it

is the vertical rather than total field quadrature component

l that is measured. The response shape is due largely to

geometrical rather than conductivity considerations and

l the distance between the maximum and minimum on either side

m of the cross-over is related to target depth. For a given

target geometry, the larger this distance the greater the

l

Page 36: HELICOPTER ELECTROMAGNETIC SYSTEM

l- 11 - APPENDIX I

I depth.

B The amplitude of the quadrature: response, as opposed

to shape, is a function of target conductance and depth

g as well as the conductivity of the overburden and host

g rock. As the primary field travels down to the conductor

through conductive material, it is both attenuated and

l phase shifted in a negative sense. The secondary field

produced by this altered field at the target also has an

l associated phase shift. This phase shift is positive and

H is larger for relatively poor conductors. This secondary

field is attenuated and phase shifted in a negative sense

B during return travel to the surface. The net effect of

these 3 phase shifts determine the phase of the secondary

l field sensed at the receiver.

l A relatively poor conductor in resistive ground will yield

a net positive phase shift. A relatively good conductor

" in more conductive ground will yield a net negative phase

fl shift. A combination is possible whereby the net phase shift

is; zero and the response is purely in-phase with no quad-

1 rature component.

l A net positive phase shift combined with the geometrical

cross-over shape will lead to a positive quadrature response

l on the side of approach and a negative on the side of

m departure. A net negative phase shift would produce the

re;verse. A further sign reversal occurs with a 180 degree

l

Page 37: HELICOPTER ELECTROMAGNETIC SYSTEM

l| 4b - 12 - APPENDIX I —————————

— change in instrument orientation as occurs on reciprocal

™ line headings. During digital processing of the quad-

I rature data for map presentation this is corrected for

by normalizing the sign to one of the flight line headings,

l

l

l

l

l

l

l

l

l

l

l

l

l

l l

Page 38: HELICOPTER ELECTROMAGNETIC SYSTEM

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Page 39: HELICOPTER ELECTROMAGNETIC SYSTEM

Ontario

Ministry of Natural Resources

GEOPHYSICAL - GEOLOGICAL - GEOCHEMICAL TECHNICAL DATA STATEMENT

File.

TO BE ATTACHED AS AN APPENDIX TO TECHNICAL REPORTFACTS SHOWN HERE NEED NOT BE REPEATED IN REPORT

TECHNICAL REPORT MUST CONTAIN INTERPRETATION, CONCLUSIONS ETC.

w u*—iu, u. O

Type of Survcy(s)___ALrJjor.ne Klcc.troma^netic , Fa^nctie, VLF-KK Township or Area^.^JVjn.to. .Lake, .(north part)______Claim Holder(s). . .. .. ,,-j u n c x c o K n c fly Corporation—

Survey Co.-npany- ....,..

Author of Report .. . ... ...Ke.ij ton ...Sco.t ,t.,— . -—-———-———

Address of Author ...,,...l,Z..b.albar, Place . Don Ml 11s

Covering Dates of Survey,. j'LarcJl ^ to Jubc l/i , 19.6(linrcutting to office)

Total Miles of Line Cut...... ....-......-..^.-.18.*^-. __ -.——-—

SPECIAL PROVISIONSCREDITS REQUESTED

KNTKR 40 days (includes line cutting) for first survey.

KNTKR 20 days for each additional survey using same grid.

Geophysical

-Electromagnetic

-Magnetometer

- Radiometric

- Other..

Geological.

Georhrmiral

DAYS per claim

PF^i * i* i

—— rt

MINING

CI TV

LA?AIRBORNE CRE1)1TS (Special proviiion crcditi do not apply to airborne iiirveyi)

VI. F

Magnetometer __ .Electromagnetic ^^2-~—— Radiometric(enter days per claim)

or of Report or Agent

Res. Gcol..

Previous SurveysFile No. 'I 'ype

... Qualifications . ..

Date Claim Holder

MINING CLAIMS TRAVERSED List numerically

1 e t al(prefix) (number)

A7TD'

S S ECTiOl;

TOTAL CLA1MS-

Page 40: HELICOPTER ELECTROMAGNETIC SYSTEM

Mining Claims Traversed (List in numerical sequence)Mining Culm

Prefix Number

660671

— -74- 660679—

...——8266068^__ 88

^ ^B9-......--90.......91

92

-Y .94"-95-

.96.

.9.7

1SL

ixptnd. Days Cr.

Total numbtr of mining claim* covsf*d by thit rapOM of work.

Page 41: HELICOPTER ELECTROMAGNETIC SYSTEM

SKI,I ..POTKNTjA.l.

Instrument^ .——.————.___-.._-._.____......-_________._________ Range.

Survey Method__.................__....—.___________________________

Corrections m ade.

RAMIOMKTRIC

Instrument............

Values measured -

Energy w indows ( levels)-.. ....^.....................,..,.__ __ ——————.^——^—^——^.^.^..

Height of i nstrument........ .... . ...........________________Background Count.

Size of detector... . ... ..........- .. ^_.______.—^.^-^^—^__.__^__________

Overburden.-- .. , _......^....___._____________________________(type, depth - include outcrop map)

01 I1KKS (SKISM1C, DRil.!. WKl.l. IXKKHNC; i.JC:.)

Type of survey. ................. ....._. _._..________..

Instrument-.^.... -.-.. ....... ., ...-.-...^-..^,..—-—

Accuracy—- .—..—. - -.-........,....... —-. ,......__—.,-——-

Parameters measured———. ^.——.... ..-^s..— .-..—.^

Additional information (for understanding results).

KlGctromagne ti c ______ VLK-EMof survey(s)- - : a^nc -?.. Instrument(s) - Gcornotroi csGK AcrodaY To t ci:. #6 2 A

(specify for each type of survey)

Accuracy-... ........... .....?..Gam(,prcifyfore.chlypcofiui*ty)

Aircraft us* d _ ...

Sensor altmulc

Navigation and night path recovery method

Aircraft altitude____...... ...?iP.OL..______.-.._______Line SpacingMiles flown over total arca..—.-jyZ2.2-..__... — ____.______Over claims only

Page 42: HELICOPTER ELECTROMAGNETIC SYSTEM

"I he r ".inirvj Act fV["io'"sI.rvtsur '

Airborne !-:3 octroir.a^notic , 1'arnot ic , VhF - J-XClaim HoUUi(i)

Sunexco Knorgy Corporation

V.'hite Lake CO'Pti-%; i en." 5 ! -. i- -.t s No.

T /. :s/

Suite 2603 ^'9i; Burrard St. p. 0. Box/^130 Vancouvor V'/X 1JS.'K'V Coi'.|.rt!W |fl..rtu' Sjt.ty i', c ,,,, ft, iol . i ' :f ' .' './s r..* :,r. c Cut

Aorodat Liir.itcdN'*n.e ino Addrfil o* Aulho' (o( Geo Tec hn.cal t enon

18.5

Complnc ifvi-ijc si Jc and enter lotalls) here

Airborne C'.•.till

Noto S.-t-c^ 1 , '('visions i f li'LifoM,^!

credits do cot apply to Airborne Surveys.

, —QlM'Xi!?™1 jSQJLExpenditures (excludes power stripping)f ype of Wo: k Pa

R*yi |.e. C'o.'ii

26.66

26.66

126.66

M in ri g ri,"r i us Tin vi 'i'.'li ! l. lit in ni.i.'iii/i seal ','. r;:.'-, iic.el

Fenton Scott 17 Kalabar Place Don Kills Ontario K3B 1 A/ttS Rft'i'.n.'SH'ii pt-'i r.'n.li Clcdril in C'jl^nris ot i ivjht

cu " 10 '" n,.i.i.nt:t*i i r' iMS ;; Cld.iT

For dist suivcy: j

Enitr 40 days. (This : inclui!t-s l int C ulling) i. t.,. , , ,, i

For tiocli o'.iiiitlO'idl suivcy: u^ing the Sbr:it- j'id:

Enter ?0 days ((or each)

C-1-oi.lif.'iiiitjl

on Citinilt)

Toul Ei

[s n D*yf

Total O*v* C'tcl'U may Le apportioned *' .ne clairr, f.ol tnO'C* Enitf numb*' of ctayi cieu-ts j-e' t lauri veluci*d in colunini at right.

M, rung C'iiiiTi

P'o'.K \'urr.l.*r

SSM . 66067.1.

73

6606798081

\ 82l . 66063? .

88 89

9192

i . . 93.

959697

' V 98660717

18 -M 9

Dj-,-1 C'.

-

. . .

t

--

-

^.M

rl

- 1m

F - c-t ix i *1 -. -,rt,[,er

S SK j 660729 .

i i

ji

i

j

SAULT STE. MARIEW;f.'!NG DIV.

E C E 1 V F. f)

SEPi ^1983Oilft.11 10 i ^ o j . * vjly|JljJ^j ] 1, i-Ij'Ji ( (

i |

\ E c ^r^l i

•!. i . ' *" . .

!i?^?iJM.2ji :.:\ .;,'i "~ " — ~

ToTti* nufnt't' O mining j Ct2"nii cOvt'bO ti^ Jhil l 1 frtJO' I O* i-VO'h. 1 '

L kf.tNd.

Days O.

- - - -

-

l \

J

V)

j. ;;- j

?.4

l—————— , -^-—. ——.J ...,--—..--.-...l-- :—— ——.....^J4r--4~t-r-l^v—l *i*irtnf-i.t^Ctft'fiCct'On VcrifyinQ Rti'on of work

For Office Use- Only ""

^ i r^TJ j i ' /j

TZmrT

*/. /'-

l hereby certily O,at l h* ve n (x-rsonal and intitule knov.'li clje of the Ions se! (oil h in iht Report o* Work ir.-.e x c! hi" t lo. r;,., i r.g p^rf, r mi d the work

or rt.messed strr* dur.nj e:id,'ur Et.^r its tonu-Vnon ind tht , r . r, t j ed report is true.

mt and Post*' Aoclrest o ( Ptrfcor. Ortily np

Fenton Scott 17 Kalabar Place.....Don MlUe__K.jr.

Page 43: HELICOPTER ELECTROMAGNETIC SYSTEM

. Geotechnicali Natural t,

*J Resources R e POrt

Dntano Approval

Filt

loMining Lends Comments

: Geophysics

j Approved Q J Wish to tee nQBin with corrections

To: Geology- Expenditures

Comment*

j j Approved j ] With to see egaln with correction!Date Signature

To: Geochemistry

Comment!

With to tee 'jaln with correction!Dete Bigxeiure

~"~To: f/'ning L.mds Section, P.oom 6462, Whitney Dlock. (Tel: 5-1380)

503 (61/10)

Page 44: HELICOPTER ELECTROMAGNETIC SYSTEM

1983 10 13 2.5866]

Mrs. M.V. St. OulesMining RecorderMinistry of Natural Resources875 Queen Street EastP.O. Box 669Sault Ste. Marie, OntarioP6A 5N2

Dear Madam:

Ue have received reports and naps for an Airborne Geophysical (Electromagnetic, Magnetometer and YLF) survey submitted on mining claims SSM 660671 in the Area of White Lake.

This material will be examined and assessed and a statement of assessment work credits will be Issued.

Yours very truly,

E.F. AndersonDirectorLand Management Branch

Whitney Block, Room 6610Queen's Park , ~Toronto, OntarioH7A 1W3Phone: (416)965-1380 . ;;

R. P1chette:dvg

cc: Sunexco Energy Corporation Suite 2803* 595 Burrard Street P.O. Box 49130 Vancouver, B.C. V7X 105

Fenton Scott 17 Malabar Place Don MHls, Ontario M3B 1A4

Page 45: HELICOPTER ELECTROMAGNETIC SYSTEM

<A-

0\U

IU

li!

G:0

i

H

CM

19

FOo

x01o(^

Page 46: HELICOPTER ELECTROMAGNETIC SYSTEM

od/z

HEMLO PROJECT

SUNEXCO ENERGY CORR

ELECTROMAGNETIC PROFILE MAP COAXIAL

SCALE 1/15,0009^-—. l Kilometre

1/2 Mil*

T LIMITED

DATE: March-June 1983

N. T. S. No -

P No'

86*00'

48-45",

Marathon

HELICOPTER ELECTROMAGNETIC ;t'~j'

Coil Configuration -CoaxialSeparation " 7 m etres Frequency -43OO Hz.

Mean Sensor Altitude -30 metresHorizontal Positioning-MRS m radar positioning

p.p.m, 30 320 -

10-

0

N-In-phase

Quadrature

4aC13SE6*55 42CI3SE0812 WHITE LAKE (NORTH) 200

Page 47: HELICOPTER ELECTROMAGNETIC SYSTEM

x

HEMLO PROJECT

SUNEXCO ENERGY CORP

ELECTROMAGNETIC PROFILE MAP COPLANAR

SCALE 1/15,000 O K i lorn* t r*

1/2 1/2 Mil*

iT LIMITED

DATE: March-June 1983

N. T. S. No :

'AP

86-OO'

48-45

HELICOPTER EL^CTf^felAGNEtlC SYSTEMCoil Configuration -CoplOnar

Septet Ion - 7 metresFrequency - 4100 Hz.

Mean Sensor Altitude - 30 metresHorizontal Positioning-MRSHE radar positioning

pp.m. 130 q

80 :

N-In-phase

Quadrature

42C13SE0eS5 42C13SE0012 WHITE LAKE (NORTH) 21O

Page 48: HELICOPTER ELECTROMAGNETIC SYSTEM

A\\

c

HEMLO PROJECT

SUNEXCO ENERGY CORR

VLF-EM TOTAL FIELD

SCALE 1/15,000 O l K t lo m* r re

1/2 1/2 Mil*

AERODAT LIMITED

DATE' March-June 1983

N. T. S. No :

1AP N o-' 3

48*45'

86*00'

VLF-EM

Instrument: Herz Totem 2AStation^ NAA Cutler, Maine-17.8 kHz.

Mean Sensor Altitude: 45 metresHorizontal Positioning: MRS IE radar positioning

500/0........ \-N-20/0 ........

contour interval 2*VoNOTE: The total field will usually indicate

a local maximum over the upper edge of a steeply dipping conductor,

4aci3SEa055 42ci3seaai2 WHITE LAKE 230

Page 49: HELICOPTER ELECTROMAGNETIC SYSTEM

HEMLO PROJECT

SUNEXCO ENERGY CORR

TOTAL MAGNETIC FIELD

SCALE 1/15,000 P l K i lorn* t r*

1/2 Mil*

J LIMITED

DATE' March-June 1983

N. T. S. No :

IAP

86*00'MAGNETOMETERInstrument - Geometrics Q-803Mean Sensor Altitude: 45 metresHorizontal Positioning- MRS m radar positioning

250. gammas.

50 gammas.

10 gammas, contour interval 10 gammas

fN

4SC13SE005S 42C13SE00I2 WHITE LAKE C NORTH) 230

Page 50: HELICOPTER ELECTROMAGNETIC SYSTEM

HEMLO PROJECT

SUNEXCO ENERGY CORP

INTERPRETATION

SCALE 1/15,000 O Kilometre

1/2 1/2 Mile

AERODAT LIMITED

DATE' March-June 1983

N. T. S. No '

\P

48*45

66 INTERPRETATION

Interpreted conductive axis within bedrockPossible conductive axis within bedrockProbable cultural conductor

AERODAT HEM SYSTEM RESPONSE VERTICAL HALF-PLANE

-N-

100

IN-PHASE (ppmj

42CI3SE0B55 42C13SE00I2 WHITE LAKE (NORTH) 2-40