BushCaddy LSA Owner's manual

BushCADDY LSA Pilot Operating Handbook Rev.03 5 March, 2008
Page 1 of 52
CANADIAN LIGHT AIRCRAFT SALES & SERVICE INC.
177-179 Joseph Carrier
Vaudreuil-Dorion, Qc. J7V 5V5
Canada
PILOT
OPERATING
HANDBOOK
MODEL: BushCaddy LSA

BushCADDY LSA Pilot Operating Handbook Rev.03 5 March, 2008
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CAUTION
THIS AIRCRAFT WAS
MANUFACTURED IN
ACCORDANCE WITH LIGHT
SPORT AIRCRAFT
AIRWORTHINESS STANDARDS
AND DOES NOT CONFORM TO
STANDARD CATEGORY
AIRWORTHINESS
REQUIREMENTS.
NO AEROBATIC MANOEUVRES
ARE ALLOWED.
This manual is integral and part of the airplane documents. To ensure a safe flight,
read carefully, follow instructions and pay particular attention to aircraft limitations.
It is strictly prohibited to alter this manual in any way.

BushCADDY LSA Pilot Operating Handbook Rev.03 5 March, 2008
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Contents
CAUTION........................................................................................................................... 2
OWNER IDENTIFICATION............................................................................................................. 6
MANUFACTURER............................................................................................................................. 6
OPTIONS:........................................................................................................................................... 6
DESCRIPTION OF THE AIRCRAFT AND SYSTEMS........................................................... 8
1.1Aircraft ............................................................................................................................. 8
1.2Landing Gear.................................................................................................................... 8
1.3Flaps ................................................................................................................................. 8
1.4Floats ................................................................................................................................ 8
1.5Dimensions....................................................................................................................... 8
1.6Airframe ........................................................................................................................... 8
1.7Engine............................................................................................................................. 10
1.8Propeller ......................................................................................................................... 10
1.9Fuel and Fuel Capacity................................................................................................... 10
1.10Oil and Lubrication ........................................................................................................ 11
1.11Electrical System............................................................................................................ 11
ELECTRICAL SCHEMATIC.................................................................................................... 11
1.12Specifications ................................................................................................................. 12
WING ......................................................................................................................................... 12
CONTROL SURFACES............................................................................................................ 12
SECTION 2........................................................................................................................................ 13
WEIGHT AND BALANCE......................................................................................................... 13
2.1General ........................................................................................................................... 13
2.2Airplane weighing procedure ......................................................................................... 13
WHEELS.................................................................................................................................... 15
FLOATS..................................................................................................................................... 16
SKIS ........................................................................................................................................... 17
Weight and Balance Examples................................................................................................... 18
GRAPH ......................................................................................................................................... 22
INSTALLED EQUIPMENT LIST............................................................................................. 23
MODIFICATION EQUIPMENT LIST..................................................................................... 24
SECTION 3........................................................................................................................................ 25
OPERATING LIMITATIONS................................................................................................... 25
3.1.General ........................................................................................................................... 25
3.2Airspeed Limitations ...................................................................................................... 25
3.3Crosswind Limitations ................................................................................................... 25
3.4Service Ceiling ............................................................................................................... 25
3.5Loading........................................................................................................................... 25

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3.6Prohibited Manoeuvres .................................................................................................. 25
3.7Airspeed Indicator Markings.......................................................................................... 25
3.8Oil Pressure Markings - Rotax 912 UL......................................................................... 26
3.9Oil Temperature Makings - Rotax 912UL .................................................................... 26
3.10RPM – Rotax 912UL...................................................................................................... 26
3.11Cylinder Head Temperature Markings – Rotax 912UL................................................. 26
SECTION 4........................................................................................................................................ 27
PERFORMANCE (Standard Air Conditions) 80 hp Engine................................................... 27
NOTE: These performance figures are specific to the Rotax 80 hp Engine, and may vary
according to equipment installed, loading and engine installation. Please refer to the Appendix
for alternative performance data specific to the optional engine installation of your model..... 27
SECTION 5 FLIGHT TRAINING................................................................................................... 28
NORMAL PROCEDURES......................................................................................................... 28
5.1Pre-flight......................................................................................................................... 28
5.2Pre-Start.......................................................................................................................... 30
5.3Start ................................................................................................................................ 30
5.4Before Take-off .............................................................................................................. 30
5.5Taxiing ........................................................................................................................... 31
5.6Take-off.......................................................................................................................... 31
5.6.1 Normal........................................................................................................................... 31
5.6.2 Short Field, Obstacle Clearance .................................................................................... 31
5.6.3 Short Field, No Obstacle Clearance .............................................................................. 31
5.6.4 Soft Field, Obstacle Clearance ...................................................................................... 31
5.6.5 Soft Field, No Obstacle Clearance ................................................................................ 31
5.7Cruise ............................................................................................................................. 32
5.8Pre-Landing.................................................................................................................... 32
5.9Landing........................................................................................................................... 32
5.9.1 Normal........................................................................................................................... 32
5.9.2 Over an Obstacle ........................................................................................................... 32
5.9.3 Short Field over an Obstacle ......................................................................................... 32
5.9.4 Balked Landing ............................................................................................................. 32
5.10Shutting down ................................................................................................................ 32
5.11Turbulent Air Operations ............................................................................................... 33
SECTION 6........................................................................................................................................ 34
EMERGENCY PROCEDURES................................................................................................. 34
6.1General ........................................................................................................................... 34
6.2Engine Fire During Start ................................................................................................ 34
6.3Engine Fire in Flight ...................................................................................................... 34
6.4Electrical Fire in Flight .................................................................................................. 35
6.5Loss of Oil Pressure ....................................................................................................... 35
6.6High Oil Temperature .................................................................................................... 35
6.7Engine Failure on Take-off ............................................................................................ 36
6.8Engine failure in Flight .................................................................................................. 36
6.9Power off Landing.......................................................................................................... 36
SECTION 7........................................................................................................................................ 37

BushCADDY LSA Pilot Operating Handbook Rev.03 5 March, 2008
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GROUND HANDLING AND SERVICING.............................................................................. 37
7.1Towing and Repositioning ............................................................................................. 37
7.2Parking ........................................................................................................................... 37
7.2Landing Gear.................................................................................................................. 37
7.3Propeller ......................................................................................................................... 38
7.4Oil................................................................................................................................... 38
7.5Fuel................................................................................................................................. 38
7.5.1.Fuel grades ............................................................................................................. 38
7.5.2.Filling Fuel Tanks .................................................................................................. 38
7.5.3.Draining Fuel Strainer, sumps and lines ................................................................ 38
7.5.4.Draining fuel system .............................................................................................. 38
CAUTION!............................................................................................................................. 38
When draining any amount of fuel care should be taken to ensure that no fire hazard exists
before starting the engine. Each quick drain should be checked after closing to make sure that it
has closed completely and is not leaking. .................................................................................... 38
7.6Tire Inflation .................................................................................................................. 39
7.7Battery Service ............................................................................................................... 39
7.8Brakes............................................................................................................................. 39
7.9Shock Cords ................................................................................................................... 39
7.10Cleaning ......................................................................................................................... 39
7.10.1Exterior Surfaces .................................................................................................... 39
7.10.2Windshield and Windows ...................................................................................... 39
7.10.3Interior.................................................................................................................... 40
7.11Lubrication ..................................................................................................................... 41
SECTION 8........................................................................................................................................ 42
SUPPLEMENTARY INFORMATION..................................................................................... 42
8.1Familiarization Flight Procedures: ................................................................................. 42
SECTION 9........................................................................................................................................ 43
SAFETY TIPS.............................................................................................................................. 43
APPENDIX A.................................................................................................................................... 45
JABIRU ENGINE........................................................................................................................ 45
JABIRU ENGINE INSTALLED PERFORMANCE (Standard Air Conditions) ................. 51
References:
BushCaddy LSA Maintenance Manual.
Rotax Operators Manual for Rotax Engine Type 912 Series
Jabiru Operators Manual for Jabiru Engines.

BushCADDY LSA Pilot Operating Handbook Rev.03 5 March, 2008
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AIRCRAFT IDENTIFICATION
MODEL BushCaddy LSA
SERIAL NUMBER
REGISTRATION
DATE OF PURCHASE
OWNER IDENTIFICATION
NAME
ADDRESS
TELEPHONE
MANUFACTURER
NAME Canadian Light Aircraft Sales & Service (CLASS) Inc.
ADDRESS 177-179 Joseph Carrier
Vaudreuil, Dorion, Qc.
J7V 5V5, Canada
TEL: [phone]
OPTIONS:
The BUSHCADDY LSA is offered in several configurations as described below. Refer to the
Aircraft Serial Number and Appendix to determine the configuration of your particular aircraft.
BCLSA (A) Rotax Engine Model 912 – 80 hp
BCLSA (B) Rotax Engine Model 912S – 100 hp
BCLSA (C) Rotax Engine Model 914 – 115 hp
BCLSA (D) Jabiru 3300 Engine
BCLSA (T) Nosewheel Landing Gear.
BCLSA (F) Floats
Typical Serial Number : BCLSA-001(B)(T) means a BushCaddy BUSHCADDY LSA aircraft
equipped with Rotax Engine Model 912S – 100 hp engine, Nosewheel Landing Gear.

BushCADDY LSA Pilot Operating Handbook Rev.03 5 March, 2008
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BushCaddy LSA Taildragger Version
BushCaddy Tricycle Gear Option

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SECTION 1
DESCRIPTION OF THE AIRCRAFT AND SYSTEMS.
1.1 Aircraft
The BushCaddy LSA is a single-engine, high wing, monoplane of all metal construction. It has a
two place side-by-side configuration.
1.2 Landing Gear
The aircraft landing gear is conventional configuration with an optional tricycle configuration. The
Landing gear is constructed from 4130-chromoly steel. Shock absorption is by means of 2 # 1380
shock chords.
1.3 Flaps
TheBushCaddy LSA model may be equipped with flaps. (Optional)
1.4 Floats
The following size floats are approved for installation on the BushCaddy LSA
Full Lotus 1400 and 1650
Straight Metal Floats 1400 and 1500
Amphibs 1400 and 1500
1.5 Dimensions
The following diagrams give the general dimensions of the aircraft.
1.6 Airframe
The airframe is constructed of 6061 T6 aluminium alloy. Hard points are 2024 T-3 aluminium
allow and of 4130 chromoly steel. The nose bowl and trim are of fibreglass.
The fuselage is a monocoque structure. Access to the cabin is through two upward opening doors.
Fig. 1 Dimensions of BushCaddy LSA
22ft. 1in.
65in

BushCADDY LSA Pilot Operating Handbook Rev.03 5 March, 2008
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Fig. 2 Dimensions of BUSHCADDY LSA
32ft.
90 inc
h
80 inches
72 in.
40 in
63
100 inches
52 in.
35 in.
Cabin width at elbows
44 inches
BushCaddy Model BUSHCADDY LSA

BushCADDY LSA Pilot Operating Handbook Rev.03 5 March, 2008
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1.7 Engine
The following engines are approved for installation in the BUSHCADDY-LSA
i) Rotax 912 UL – 80 hp
ii) Rotax 912 ULS – 100 hp
iii) Rotax 914 – 115 hp
iv) Jabiru 3300 - 120 hp
Standard engine for the BUSHCADDY-S-LSA.is the ROTAX-BOMBARDIER 912 ULS 4 stroke, 4
cylinder engine - liquid/air cooled.
1.8 Propeller
The BUSHCADDY LSA is fitted with a ground adjustable propeller. The hub is of aircraft grade
aluminium alloy.
1.9 Fuel and Fuel Capacity
Fuel is stored in two 10-IMPERIAL (12 US) gallon tanks installed in the wings, gravity fed to the
engine, which is equipped with a mechanical pump.
Fig. 3 Fuel Lines
An electric standby fuel pump may be installed.

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The fuel selector control is located on cross frame immediately below and in front of pilot. Optional
position is on the centre of instrument panel.
Note: For firewall forward schematic, see engine operator’s manual.
1.10 Oil and Lubrication
Please refer to engine operator’s manual for more details.
Rotax engines are dry sump engines. Oil is drawn from the firewall mounted tank through an oil
cooler by engine mounted oil pump, through the engine lubricating points and returns to oil tank via
hose mounted on the base of the engine.
Jabiru engines are wet sump internal oil pump and external oil cooler.
1.11 Electrical System
A 12-volt battery to the master, from the master to firewall mounted relay, supplies power and then
to a fuse equipped buss bar for distribution to gauges, instruments radios etc.
For ignition system, see engine operator’s manual.
ELECTRICAL SCHEMATIC

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1.12 Specifications
(May vary depending on optional configurations and equipment installed) Refer to Form WB-1
specific to this model and configuration. Jabiru Engine performances may vary from those shown
below.
ENGINE ROTAX 912 – 80 h.p. ROTAX 914 –115 h.p. FLOATS
LENGTH 22 ft. 1in. 22ft.1in. 22 ft. 1in.
HEIGHT 6 ft 6 ft 6 ft
AILERON Left wing travel up 22 Left wing travel up 22 Left wing travel up 22
AILERON Left wing travel down 21 Left wing travel down 21 Left wing travel down 21
AILERON Right wing travel up 25 Right wing travel up 25 Right wing travel up 25
AILERON Right wing travel down 19 Right wing travel down 19 Right wing travel down 19
ELEVATOR Travel down 31.5 Travel down 31.5 Travel down 31.5
ELEVATOR Travel up 22 Travel up 22 Travel up 22
RUDDER Right 15.25” Right 15.25” Right 15.25”
RUDDER Left 18” Left 18” Left 18”
WING SPAN 32 feet 32 feet 32 feet
WING AREA 168 sq. ft. 168. Sq. ft 168. Sq. ft.
CEILING 10,000 ft. 12,,000 ft. 10,000 ft.
MAX WEIGHT 1320 lbs. 1320 lbs` 1430 lbs
EMPTY WEIGHT 751. 751 lbs. 835
USEFUL LOAD 569. 569 lbs. 595
CRUISE 75% 95 MPH 105 MPH 84 – 96 MPH
VNE 130 MPH 130 MPH` 130 MPH
VA 58 MPH 58 MPH 58 MPH
STALL power off 34 MPH 34 MPH 34 MPH
Power/weight ratio 15 lb/BHP 10.43 lb/BHP 14.8 lb/BHP
WING LOADING 7.3 lb per sq. ft. 7.3 lb. Per. Sq. ft. 7.3 lb. Per sq. ft.
TAKE OFF 1332 lb. 266 ft. concrete
282 ft. short grass
300 ft. tall grass
305 ft. soft ground
266 ft. concrete
270 short grass
300 tall grass
300 soft ground
15-30 seconds at gross
RATE OF CLIMB 850 f.p.m. 1000 f.m.p. 600 f.p.m.
WING
A) Average Aerodynamic Line 63.5”
B) Line of Incidence 0.05
C) Dihedral 1.125” at the tip of the wing
CONTROL SURFACES
A) Wings and Ailerons 168 sq.ft.
B) Ailerons 17.94 sq.ft.
C) Horizontal Stabilizer 15.68 sq.ft.
D) Elevator 11.0 sq.ft.
E) Vertical Stabilizer 8.3 sq. ft.
F) Rudder 4.5 sq.ft.

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SECTION 2
WEIGHT AND BALANCE.
2.1 General
In order to achieve the performance, safety and optimal flying characteristics, which are designed,
into the aircraft, it must be flown with the weight and centre of gravity (C.G.) position within the
approved operating range (envelope). The pilot must ensure that the aircraft is loaded within the
loading envelope before takeoff. A weight and balance calculation can be helpful in determining
how much fuel or baggage can be boarded so as to keep within the allowable limits. Check
calculations prior to adding fuel to ensure against over loading.
2.2 Airplane weighing procedure
At the time of delivery, CLASS Inc. provides each airplane with the basic empty weight and centre
of gravity location. This data is supplied on Form WB-1
WARNING!
Misloading carries serious safety consequences for any aircraft. If the C.G. is too far forward, it
may be difficult to rotate for takeoff or landing. If the C.G. is too far aft, the aircraft may rotate
prematurely on takeoff or tend to pitch up during climb. Longitudinal stability will be reduced.
This can lead to inadvertent stalls and even spins; and spin recovery becomes more difficult as
the center of gravity moves aft of the approved limit.

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CENTER OF GRAVITY
Example
Calculation of Center of Gravity
The datum line is situated at the leading edge of the wing
Horizontal distance “D” between the main wheel balance point and the datum line------6.5in.
Horizontal distance “L” between the main wheel balance point and the tail wheel balance point ----174 INS.
EMPTY WEIGHT
Scale weight Lbs. Tare weight Net weight
Right 280 0 280
Left 280 0 280
Tail 67 27 40
TOTAL WEIGHT 600
RECORD THE WEIGHT ON EACH WHEEL, DEDUCT THE TARE FROM EACH
READING.
FORMULA FOR CALCULATING THE CENTER OF GRAVITY POINT
C.G = D+ Rx L = 6in. + 40 x 174 = 11.6 IN + 6.5 IN. = 18.1 in.
W 600
WARNING! Chock Main wheels to prevent aircraft movement during weighing
procedure.
C of G
To be calculated
Datum line (leading edge of wing)
Weight 280lbs(left and right) Rearscale 67lb
L m e a su re d
Sup p o rt 2 7 lb s.
Weighing point
tail wheel
Weighing point main wheels
D measured
(Tare)

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WEIGHT AND BALANCE Form WB-1
WHEELS
DATE: MODEL:
SERIAL NO: DATUM: Leading edge of wing
REGISTRATION: USEFUL LOAD
LANDING GEAR CONFIGURATION: Wheels
Aircraft must be placed level on scales, hangar doors closed, fuel tanks drained and engine oil included.
WEIGHT (LBS)
Right wheel
Left wheel
Tail wheel
TOTAL WEIGHT
Net empty weight
Centre of Gravity
Max. Gross 1320 lbs
Useful load
Weight Total empty
weight Arm Moment
Aircraft
Passenger
Fuel
Luggage
TOTAL
NOTE
The limits of the centre of gravity must be within 15 – 22 inches.
Centerof Gravity Datum
Sc a le Sc a le
C.G. =
NOTE: RECORD THE WEIGHT ON EACH WHEEL; DEDUCT THE TARE FROM EACH
READING
WARNING! Chock main wheels to prevent aircraft movement during weighing
procedure. Raise tail carefully, the higher the tail is lifted, the lighter it becomes. Aircraft
can nose over.

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WEIGHT AND BALANCE
FLOATS
DATE: SERIAL NO:
SERIAL NO: DATUM: Leading edge of wing
REGISTRATION: MAX GROSS: 1430 lbs.
LANDING GEAR CONFIGURATION: Floats USEFUL LOAD
Aircraft must be placed level on scales, hangar doors closed, fuel tanks drained and engine oil included
WEIGHT (LBS)
Right float
Left float
Tail
TOTAL WEIGHT
Weight Total empty
weight Arm Moment
Aircraft
Passenger
Fuel
Luggage
TOTAL
Net empty weight
Centre of Gravity
Max. Gross 1430 lbs
Useful load
NOTE
The limits of the center of gravity must be within 15 – 22 inches.
C.G. =
NOTE: RECORD THE WEIGHT ON EACH FLOAT; DEDUCT THE TARE FROM EACH
READING

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WEIGHT AND BALANCE
SKIS
DATE: SERIAL NO:
SERIAL NO: DATUM: Leading edge of wing
REGISTRATION: MAX GROSS: 1320 lbs.
LANDING GEAR CONFIGURATION: Floats USEFUL LOAD
Aircraft must be placed level on scales, hangar doors closed, fuel tanks drained and engine oil included
WEIGHT (LBS)
Right ski
Left ski
Tail ski
TOTAL WEIGHT
Net empty weight
Centre of Gravity
Max. Gross 1320 lbs.
Useful load
NOTE
The limits of the center of gravity must be within 15 – 22 inches.
Weight Total empty
weight Arm Moment
Aircraft
Passenger
Fuel
Luggage
TOTAL
C.G. =
NOTE: RECORD THE WEIGHT ON EACH SKI; DEDUCT THE TARE FROM EACH
READING
WARNING!Prevent aircraft movement during weighing procedure. Raise tail carefully, the
higher the tail is lifted, the lighter it becomes. Aircraft can nose over

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Weight and Balance Examples
Maximum Gross Weight - Example
Weight Arm Moment US Gal
(Lbs) (Inches) (in/lbs)
Empty (684.0 lbs) 684.0 16.0 10944.0
Pilot (190 lbs) 190.0 26.0 4940.0
Pax (190 lbs) 190.0 26.0 4940.0
Luggage 50.0 45.0 2250.0
Fuel (max 20 US gal) (gals) 134.0 24.0 3216.0 20
Total 1248.0Lbs
Maximum Allowable Gross 1320.0Lbs
Margin 72.0Lbs
Calculated CG Position 21.07Inches
Max Allowable CG = 22"
Min Allowable CG = 15"
Maximum Gross Weight - 1/2 hour fuel remaining-
Example
Weight Arm Moment US
Gal
(Lbs) (Inches) (in/lbs)
Empty (751 lbs) 751 16 12016
Pilot (190 lbs) 190 26 4940
Pax (190 lbs) 190 26 4940
Luggage 50 45 2250
Fuel (max 20 US gal) (gals) 10.1 24 241.2 1.5
24387.2
Total 1191.1 Lbs
Maximum Allowable Gross 1320 Lbs
Margin 128.9 Lbs
Calculated CG Position 20.47 Inches
Max Allowable CG = 22"
Min Allowable CG = 15"

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Pilot and Passenger - Example
Weight Arm Moment (Us
gals)
(Lbs) (Inches) (in/lbs)
Empty (751 lbs) 751 16 12016
Pilot (190 lbs) 190 26 4940
Pax (190 lbs) 190 26 4940
Luggage 0 45 0
Fuel (max 20 US gal) (gals) 134 24 3216 20
25112
Total 1265 Lbs
Maximum Allowable Gross 1320 Lbs
Margin 55 Lbs
Calculated CG Position 19.85 Inches
Max Allowable CG = 22"
Min Allowable CG = 15"
Pilot and Passenger - 1/2 hour fuel remaining
- Example
Weight Arm Moment
(Lbs) (Inches) (in/lbs)
Empty (751 lbs) 751 16 12016
Pilot (190 lbs) 190 26 4940
Pax (190 lbs) 190 26 4940
Luggage 0 45 0 (Us gals)
Fuel (max 20 US gal) (gals) 10.1 24 241.2 1.5
22137.2
Total 1141.1 Lbs
Maximum Allowable Gross 1320 Lbs
Margin 178.9 Lbs
Calculated CG Position 19.40 Inches
Max Allowable CG = 22"
Min Allowable CG = 15"

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Pilot with Baggage - Example
Weight Arm Moment
(Lbs) (Inches) (in/lbs)
Empty (751 lbs) 751 16 12016
Pilot (190 lbs) 190 26 4940
Pax (190 lbs) 0 26 0
Luggage 50 45 2250 (Us gals)
Fuel (max 20 US gal) (gals) 134 24 3216 20
22422
Total 1125 Lbs
Maximum Allowable Gross 1320 Lbs
Margin 195 Lbs
Calculated CG Position 19.93 Inches
Max Allowable CG = 22"
Min Allowable CG = 15"
Pilot with Baggage - 1/2 hour fuel remaining -
Example
Weight Arm Moment
(Lbs) (Inches) (in/lbs)
Empty (751lbs) 751 16 12016
Pilot (190 lbs) 190 26 4940
Pax (190 lbs) 0 26 0
Luggage 50 45 2250 (Us gals)
Fuel (max 20 US gal) (gals) 10.1 24 241.2 1.5
19447.2
Total 1001.1 Lbs
Maximum Allowable Gross 1320 Lbs
Margin 318.9 Lbs
Calculated CG Position 19.43 Inches
Max Allowable CG = 22"
Min Allowable CG = 15"