SkyReach BushCat User manual


Issue 8, Revision 1
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MAINTENANCE MANUAL
BushCat
NOSE-WHEEL AND TAIL-DRAGGER
FITTED WITH ROTAX 912UL/ULS ENGINE
APPROVED FLIGHT MANUAL PART NUMBER:
BCMM-NT-008-001
AIRCRAFT TYPE:
CHEETAH –BUSHCAT*
DATE OF ISSUE:
28 JUNE 2017
NOTE: THIS DOCUMENT MUST BE KEPT IN THE AIRCRAFT DURING OPERATION
*Refer to the POH for more information on aircraft type.

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ISSUES AND REVISIONS
This operating manual may be revised and amended periodically and as a result new issues and
revisions will be made and published. Revisions will be made to rectify small changes or errors with
this manual which do not change page numbering. Corrected pages simply replace existing pages.
New issues will be released if major changes to this manual are made and page many or all page
numbers change. If this manual has been shipped with an aircraft it will be suitable for the aircraft
and subsequent issues will not be required for it to be complete - i.e., a later issue operating manual
will only be applicable to aircraft shipped after that particular issue. If revisions are published you
will be notified by SkyReach or by your distributer as they will apply to the correctness of your
manual. It should be noted that all revisions and revisions are available on the SkyReach website as
downloadable PDF files. The part number of your manual (shown on the front cover) will have the
following format:
BCMM-NT-aaa-bbb
The first two parts show that it is a BushCat maintenance manual for nose-wheel and tail-dragger
variants. The numbers replacing 'aaa' show the issue number of your manual, and the numbers
replacing 'bbb' indicate the latest revision which has been included in this manual. If you receive a
revision to your manual, your manual number will change in the 'bbb' section.
A record of issues and revisions are given on the following page.

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RECORD OF ISSUES AND REVISIONS
The following issues have led to this current issue:
Issues Number
Date Published
Notable Changes
001
28/10/2013
Original
002
05/12/2013
Electrical system schematic moved to A/C supplement
003
07/07/2014
New Zealand distributer address added
004
08/07/2014
Several changes
005
19/11/2014
Fuel line inspection added
006
01/04/2015
MTOW increased to 600kg
007
19/07/2016
Canada distributor address added
008 (Current)
01/04/2017
Multiple
The following revisions have been included in this issue. Please document further amendments in
the blank spaces provided:
Revision Number
Date Published
Notable Changes
000
Original (No revisions)
001
28/06/2017
Multiple

Issue 8, Revision 1
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FEEDBACK FORM
Please use the following form to notify us of any improvements or corrections needed, as well as for
continued operational safety reporting or for an owner’s change of address notice. After completing
the form please fax or email it to the relevant contact shown on the next page. In addition, please
keep a copy of the completed form in your Maintenance Manual.
Name:
Email:
Phone Number:
Date:
BushCat Serial Number:
Registration number:
Feedback information:

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Email or fax to:
South African Address:
Rainbow SkyReach (PTY) Ltd
P.O. Box 3408,
Dalview 1544,
Gauteng,
South Africa.
Tel: +2711 817 2298
Fax: +2711 817 2297
USA Address:
AeroSport, LLC
198 Lynne Drive,
Twin Lakes,
WI 53181,
USA.
Tel/Fax: +1 (262) 448-1122
New Zealand Address:
BushCat Aviation NZ LTD
Ngaruawahia,
Waikato,
3720,
New Zealand.
Tel: +64 7 824 8747
Canadian Address:
Sport Aircraft Brokers Ltd
60 Starrview Crescent,
Mono,
Ontario,
L9W 3W9,
Canada.
Toll free: +1 866 733 8432
Mobile: +1 416 918 6569
Israeli Address:
BushCat Israel
12 Havradim,
Haifa,
Israel.
Tel: +972-52-5639049
Tel: +972-50-6599890
Ecuadorian Address:
Use South African contact
details
Polish Address:
Use South African contact
details
Namibian Address:
Use South African contact
details
Brazilian Address:
Use South African contact
details

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TABLE OF CONTENTS
ISSUES AND REVISIONS ...........................................................................................................................3
RECORD OF ISSUES AND REVISIONS .......................................................................................................4
FEEDBACK FORM.....................................................................................................................................5
TABLE OF CONTENTS...............................................................................................................................7
CHAPTER 1. GENERAL .......................................................................................................................12
1.1. INTRODUCTION TO THE MANUAL ........................................................................................12
1.2. INTRODUCTION TO THE CHEETAH SERIES ............................................................................12
1.3. A NOTE ON STAND UNITS .....................................................................................................12
1.4. REFERENCE DOCUMENTATION.............................................................................................12
1.5. SUPPLIED DOCUMENTATION................................................................................................13
1.6. TERMINOLOGY ......................................................................................................................14
CHAPTER 2. AUTHORISATIONS .........................................................................................................16
CHAPTER 3. GENERAL SPECIFICATIONS ............................................................................................17
3.1. DIMENSIONS .........................................................................................................................17
3.2. BAGGAGE SPACE ...................................................................................................................20
3.3. CABIN AND ENTRY DIMENSIONS ..........................................................................................20
3.4. SPECIFIC LOADINGS...............................................................................................................20
3.5. GROUND TURNING CLEARANCE ...........................................................................................21
3.6. EQUIPMENT LIST ...................................................................................................................21
3.7. SOURCES TO PURCHASE PARTS ............................................................................................21
3.8. LIST OF DISPOSABLE REPLACEMENT PARTS..........................................................................22
3.9. ENGINE SPECIFICATIONS.......................................................................................................23
3.9.1. POWER AND SPEED LIMITATIONS: ...............................................................................23
3.9.2. LOAD FACTOR LIMITATIONS: ........................................................................................23
3.9.3. OIL PRESSURE:...............................................................................................................23
3.9.4. OIL TEMPERATURE:.......................................................................................................23
3.9.5. EXHAUST GAS TEMPERATURE: .....................................................................................24
3.9.6. CYLINDER HEAD TEMPERATURE: ..................................................................................24
3.9.7. COOLANT TEMPERATURE: ............................................................................................24
3.9.8. FUEL PRESSURE: ............................................................................................................24
3.9.9. STARTING & OPERATING TEMPERATURE: ....................................................................24
3.9.10. ENGINE INSTRUMENTATION.........................................................................................24

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3.9.11. CARBURETTOR HEAT.....................................................................................................24
3.9.12. ENGINE PERFORMANCE CURVES ..................................................................................24
3.10. PROPELLER ............................................................................................................................28
3.11. IGNITION SYSTEM .................................................................................................................29
3.12. ELECTRICAL SYSTEM..............................................................................................................33
3.13. WEIGHT AND BALANCE INFORMATION................................................................................41
3.13.1. MAXIMUM GROSS MASS ..............................................................................................41
3.13.2. CENTRE OF GRAVITY POSITION.....................................................................................42
3.13.3. MASS AND BALANCE FORM ..........................................................................................43
3.14. TYRE INFLATION PRESSURES.................................................................................................44
3.15. AIRCRAFT BATTERY ...............................................................................................................44
3.16. FUEL SYSTEM.........................................................................................................................45
3.16.1. FUEL SYSTEM DESCRIPTION ..........................................................................................45
3.16.2. FUEL SYSTEM CAPACITIES .............................................................................................48
3.16.3. APPROVED FUELS..........................................................................................................48
3.17. OIL COOLING AND LUBRICATION SYSTEM ............................................................................49
3.18. LIQUID COOLING SYSTEM .....................................................................................................51
3.19. BRAKING SYSTEM..................................................................................................................53
3.20. RECOMMENDED FASTENER TORQUE VALUES......................................................................55
3.21. GROUND HANDLING .............................................................................................................56
3.22. TIE DOWN INSTRUCTIONS ....................................................................................................56
3.23. GENERAL SAFETY INSTRUCTIONS..........................................................................................56
3.24. INSTRUCTIONS FOR REPORTING POSSIBLE SAFETY OF FLIGHT CONCERNS FOUND DURING
INSPECTION / MAINTENANCE...........................................................................................................57
CHAPTER 4. SCHEDULED MAINTENANCE INSPECTION / SERVICE ITEMS .........................................58
4.1. AIRFRAME PERIODIC INSPECTIONS / SERVICES ....................................................................60
4.1.1. AIRFRAME 100 HOUR / ANNUAL INSPECTION..............................................................61
4.1.2. AIRFRAME ADDITIONAL ITEM / 500 HOUR INSPECTION ..............................................66
4.1.3. AIRFRAME 100 HOUR / ANNUAL SERVICE ....................................................................67
4.2. ENGINE PERIODIC INSPECTIONS ...........................................................................................68
4.2.1. ENGINE 100 HOUR CHECK.............................................................................................68
4.2.2. ENGINE 25 HOUR CHECK...............................................................................................68
4.2.3. ENGINE ADDITIONAL ITEM 200 HOUR CHECK ..............................................................74
4.2.4. ENGINE ADDITIONAL ITEM 600 HOUR CHECK ..............................................................76

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4.2.5. ENGINE ADDITIONAL ITEM 1000 HOUR CHECK ............................................................77
CHAPTER 5. UNSCHEDULED MAINTENANCE INSPECTION / SERVICE ITEMS ....................................78
5.1. WING STRIKE INSPECTION ....................................................................................................79
5.2. TAIL STRIKE INSPECTION .......................................................................................................80
5.3. HARD LANDING INSPECTION ................................................................................................81
5.4. EXCEEDANCE OF OPERATING LIMITATIONS OF THE ENGINE ...............................................82
5.4.1. RETURNING ENGINE TO SERVICE AFTER SUBMERGING IN WATER ..............................82
5.4.2. EXTREME CLIMATIC CONDITIONS.................................................................................82
5.4.3. RETURNING ENGINE TO SERVICE AFTER EXPOSURE TO FIRE .......................................82
5.4.4. EXCEEDANCE OF MAXIMUM PERMISSIBLE ENGINE RPM.............................................83
5.4.5. EXCEEDANCE OF MAXIMUM PERMISSIBLE COOLING SYSTEM TEMPERATURE............85
5.4.6. EXCEEDANCE OF MAXIMUM PERMISSIBLE OIL TEMPERATURE ...................................89
5.5. PROPELLER SUDDEN STOPPAGE ...........................................................................................91
5.6. EXCEEDANCE OF AIRCRAFT G-LIMITATIONS / SPEED LIMITATIONS .....................................93
CHAPTER 6. DETAILED MAINTENANCE PROCEDURES ......................................................................94
6.1. PROCEDURE FOR WEIGHING AND DETERMINING THE CENTRE OF GRAVITY POSITION......95
6.2. WING.....................................................................................................................................98
6.2.1. REMOVAL AND INSTALLATION......................................................................................98
6.3. LANDING GEAR....................................................................................................................107
6.3.1. TAIL WHEEL INSTALLATION PROCEDURE –TAIL-DRAGGER VARIANTS ONLY.............107
6.3.2. SPRING GEAR ATTACHMENT INSTALLATION ..............................................................110
6.3.3. MATCO WHEEL ASSEMBLY..........................................................................................116
6.3.4. AXLE, CALLIPER, AND MAIN WHEEL INSTALLATION ...................................................122
6.3.5. NOSE WHEEL ASSEMBLY –NOSE-WHEEL VARIANTS ONLY ........................................127
6.3.6. FRONT FORK AND WHEEL ASSEMBLY –NOSE-WHEEL VARIANTS ONLY ....................131
6.3.7. FRONT FORK INSTALLATION (PART 1) –NOSE WHEEL VARIANTS ONLY ....................134
6.3.8. FRONT FORK INSTALLATION (PART 2) –NOSE WHEEL VARIANTS ONLY ....................136
6.3.9. FRONT FORK INSTALLATION (PART 3) –NOSE WHEEL VARIANTS ONLY ....................138
6.3.10. BRAKE BLEEDING PROCEDURE....................................................................................141
6.4. CONTROL SURFACES ...........................................................................................................143
6.4.1. FLAP AND AILERON INSTALLATION / REMOVAL PROCEDURE ....................................143
6.4.2. ELEVATOR INSTALLATION / REMOVAL PROCEDURE...................................................146
6.4.3. ELEVATOR TRIM TAB INSTALLATION / REMOVAL PROCEDURE..................................150
6.4.4. RUDDER INSTALLATION / REMOVAL PROCEDURE......................................................153

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6.4.5. AILERON BALANCE TABS INSTALLATION / REMOVAL .................................................157
6.4.6. CONTROL SURFACE RIGGING......................................................................................159
6.4.7. ELEVATOR SETUP ........................................................................................................167
6.4.8. RUDDER SETUP............................................................................................................173
6.4.9. AILERON SETUP...........................................................................................................177
6.4.10. FLAP SETUP .................................................................................................................181
6.5. ROTAX 912 ENGINE.............................................................................................................184
6.5.1. ENGINE CLEANING ......................................................................................................184
6.5.2. AIR FILTER INSPECTION ...............................................................................................186
6.5.3. AIR FILTER REPLACEMENT...........................................................................................188
6.5.4. ENGINE INITIAL PREPARATION ...................................................................................189
6.5.5. STARTER MOTOR ROTATION ......................................................................................192
6.5.6. MAGNETO BOX REMOUNT .........................................................................................197
6.5.7. ENGINE MOUNTING ATTACHMENT............................................................................203
6.5.8. ENGINE REMOVAL AND INSTALLATION ......................................................................211
6.5.9. REPLACEMENT OF ENGINE EXHAUST..........................................................................217
6.5.10. FUEL PUMP INSPECTION / MAINTENANCE PROCEDURE............................................225
6.5.11. MAGNETIC PLUG INSPECTION ....................................................................................229
6.5.12. BING CONSTANT DEPRESSION CARBURETTOR INSPECTION ......................................231
6.5.13. ENGINE TEST RUN .......................................................................................................244
6.6. FUEL SYSTEM.......................................................................................................................246
6.6.1. REFUELLING PROCEDURE............................................................................................246
6.6.2. FUEL FILTER INSPECTION / REPLACEMENT .................................................................247
6.6.3. INSPECTION OF THE FUEL PUMP, CARBURETTOR, FUEL LINES, AND DRIP TRAY .......250
6.6.4. FUEL TANK, FUEL LINES, AND FUEL SHUT-OFF VALVE INSTALLATION........................255
6.7. OIL SYSTEM .........................................................................................................................260
6.7.1. REPLENISHMENT OF OIL .............................................................................................260
6.7.2. OIL FILTER REPLACEMENT...........................................................................................263
6.7.3. OIL FILTER INSPECTION ...............................................................................................266
6.7.4. OIL CHANGES...............................................................................................................270
6.8. PROPELLER ..........................................................................................................................272
6.8.1. INSTALLATION OF THE PROPELLER AND ADJUSTMENT OF THE PROPELLER PITCH
ANGLE 272
6.9. UTILITY SYSTEMS.................................................................................................................278

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6.9.1. HEATING AND VENTILATION SYSTEMS .......................................................................278
6.10. INSTRUMENTS AND AVIONICS............................................................................................279
6.10.1. INSTRUMENT PANEL INTALLATION.............................................................................279
6.10.2. INSPECTION OF THE PITOT STATIC SYSTEM................................................................282
6.11. IGNITION SYSTEM ...............................................................................................................285
6.11.1. IGNITION SYSTEM INSPECTION...................................................................................285
6.12. ELECTRICAL SYSTEM............................................................................................................286
6.12.1. REPLACEMENT OF THE BATTERY ................................................................................286
6.12.2. OVERHAUL OF ELECTRIC STARTER ..............................................................................288
6.13. STRUCTURAL INSTALLATION / REPLACEMENT / MINOR REPAIR........................................303
6.13.1. SEAT INSTALLATION ....................................................................................................303
6.13.2. SEAT BELT NSTALLATION ............................................................................................307
6.13.3. CABIN DOOR REPLACEMENT.......................................................................................310
6.13.4. REPLACEMENT OF THE BALLISTIC RECOVERY SYSTEM ...............................................313
6.13.5. REMOVAL AND REPLACEMENT OF THE WINDSCREEN ...............................................315
6.14. PAINTING AND COATINGS ..................................................................................................327
6.14.1. TRI-LAMINATE REPAIR ................................................................................................327
6.14.2. PLACARD AND INSTRUMENT MARKING IDENTIFICATION AND REPLACEMENT .........328
6.14.3. AIRCRAFT PAINTING....................................................................................................336
6.14.4. AIRCRAFT WASHING....................................................................................................337
APPENDIX 1: EQUIPMENT CHANGE REQUEST ................................................................................338

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CHAPTER 1. GENERAL
1.1. INTRODUCTION TO THE MANUAL
Thank you for purchasing a BushCat Light Sport Aircraft.
The BushCat represents the best value in a light sport aircraft without any compromise in quality and
safety.
In order to extract maximum safety and performance from your BushCat please familiarize yourself
with the entire contents of this Maintenance Manual.
This manual conforms to ASTM F2483 standards –Standard Specifications for Maintenance Manuals
(MM) for Light Sport Airplanes.
This aircraft is equipped with a non-certified engine which meets the ASTM F2339-06 engine
standard.
All factory-built aircraft have been manufactured by Rainbow SkyReach (PTY) LTD –a part 148
approved manufacturing organisation, approved by the South African Civil Aviation Authority.
1.2. INTRODUCTION TO THE CHEETAH SERIES
It should be noted that the term ‘BushCat’ refers to the third (and most current) variant of Cheetah
aircraft; The Cheetah-BushCat. Original production acceptance certification with the SACAA was
obtained under the name of ‘Cheetah’. The two main upgrades to the aircraft were approved as
‘Cheetah-XLS’ and ‘Cheetah-BushCat’. For certification in foreign countries which was based on the
South African approval the term ‘BushCat’ was used in place of ‘Cheetah-BushCat’. This manual
applies only to the Cheetah-BushCat and not to the Cheetah-Standard or Cheetah-XLS aircraft.
1.3. A NOTE ON STAND UNITS
Aircraft manufacturers traditionally present figures in the standard units adopted by the country of
manufacturer. The BushCat is a South African designed and manufactured aircraft and as such it
presents metric units as default. However, Rainbow SkyReach (PTY) LTD makes efforts to present
both Metric and Imperial units in all published documentation where practical. The operator should
bear this in mind to avoid errors from using figures with incorrect units.
1.4. REFERENCE DOCUMENTATION
The following documents are referenced within this manual:
1. ASTM 2245 –Specifications for the design and performance of a Light Sport Aircraft
2. The BushCat assembly manual.
3. The BushCat pilot operating handbook.
4. Line Maintenance Manual for ROTAX engine type 912 series.
5. Heavy Maintenance Manual for ROTAX engine type 912 and 914 series.
6. Installation Manual for ROTAX engine type 912 series.
7. Operators Manual for ROTAX engine type 912.

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1.5. SUPPLIED DOCUMENTATION
The following manuals are supplied in either hardcopy or electronic format as part of your BushCat
aircraft in addition to any pertinent avionics and equipment manuals
1. The Rotax 912 ULS engine operators manual
2. The BushCat Pilots Operating Handbook
3. The BushCat Quick Reference Handbook
4. The BushCat Maintenance Manual
5. The BushCat Assembly Manual (for kit build option)

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1.6. TERMINOLOGY
Annual Condition Inspection
Detailed inspection accomplished once a year in accordance with
instructions provided in the maintenance manual supplied with the
aircraft to ensure continued safe operation.
A&P
Airframe and Power plant mechanic as defined by 14 CFR Part 65 in
the U.S. or equivalent certification in other countries.
Heavy Maintenance
Any maintenance, inspection, repair or alteration a manufacturer
has designated that requires specialized training, equipment or
facilities. Level 3 authorization as per the table in chapter 2 is
required to accomplish heavy maintenance.
Line Maintenance
Any repair, maintenance, scheduled checks, servicing, inspections
or alterations not considered heavy maintenance that is approved
by the manufacturer and is specified in the manufacturer’s
maintenance manual. Level 2 authorisation as per the table in
chapter 2 is required to accomplish line maintenance.
LSA (light sport aircraft)
Aircraft designed in accordance with ASTM standards under the
jurisdiction of Committee F37 Light Sport Aircraft (for example
Specification F2244 for powered parachutes, Specification F2245
for airplanes, and Specification F2352 for Gyroplanes.) or
equivalent in other countries.
LSA Repairman Inspection
U.S. FAA-certificated repairman (light sport aircraft) with an
inspection rating as defined by 14 CFR Part 65, authorized to
perform the annual condition inspection/ 100 hour inspection on
experimental light sport aircraft, or an equivalent rating issued by
other civil aviation authorities. *
LSA Repairman Maintenance
U.S. FAA-certificated repairman (light sport aircraft) with a
maintenance rating as defined by 14 CFR Part 65, authorized to
perform line maintenance on aircraft certificated as special LSA
aircraft. Authorized to perform the annual condition/100-h
inspection on an LSA, or an equivalent rating issued by other civil
aviation authorities. *
Maintenance Manual(s)
Manual provided by an LSA manufacturer or supplier that specifies
all maintenance, repairs, and alterations authorized by the
manufacturer in accordance with the Chapter 2.
Major Repair, Alteration, or
Maintenance
Any repair, alteration, or maintenance for which instructions to
complete the task excluded from the maintenance manual(s)
supplied to the consumer are considered major. **
Manufacturer
Any entity engaged in the production of an LSA or component used
on an LSA.
Minor Repair, Alteration, or
Maintenance
Any repair, alteration, or maintenance for which instructions
provided for in the maintenance manual(s) supplied to the
consumer of the product are considered minor.
Overhaul
Maintenance, inspection, repair, or alterations that are only to be
accomplished by the original manufacturer or a facility approved by
the original manufacturer of the product. **

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Overhaul Facility
Facility specifically authorized by the aircraft or component
manufacturer to overhaul the product originally produced by that
manufacturer.
Repair Facility
Facility specifically authorized by the aircraft or component
manufacturer to repair the product originally produced by that
manufacturer.
100-h inspection
Same as an annual condition inspection, except the interval of
inspection is 100 h of operation instead of 12 calendar months.
* Experimental LSA do not require the individual performing maintenance to hold any FAA airman
certificate in the U.S.
**Alterations to the aircraft cannot be authorized without the approval of the aircraft manufacturer.

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CHAPTER 2. AUTHORISATIONS
This section details the personnel permitted to accomplish each task as detailed in section 6.
It should be noted that modifications to the airframe or engine are not permitted
without written approval from the manufacturer.
Level of
Authorization
Classification of tasks to be performed
Qualification required to perform the tasks.
Level 1
Minor maintenance, repairs and alterations
The owner / operator who holds at least a
sport pilot certificate may perform these
items.
Level 2
Line maintenance, repairs and alterations
An LSA Maintenance Repairman (or country
specific equivalent), Aeroplane A&P or an
FAA (or similarly approved) Repair Station
may perform these items.
Level 3
Heavy maintenance, repairs and alterations
An LSA Maintenance Repairman (or country
specific equivalent) with task specific
training, A&P or FAA (or similarly approved)
Repair Station may perform these items.
Level 4
Major repair, alterations and overhauls
Only the manufacturer of the LSA or
component on the LSA may perform or
authorise other entities (including, but not
limited to, contracted agents in other
countries) to perform these items.
A separate overhaul manual, in addition to
the manufacturer’s maintenance manual, is
frequently required to perform these items.
For additional information or explanations,
please contact the factory or distributer
using the contact details supplied on page 5.
WARNING

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CHAPTER 3. GENERAL SPECIFICATIONS
This section details general aircraft specifications, capacities and basic instructions for handling the
aircraft on the ground. For more detailed specifications, please refer to the accompanying BushCat
“Pilot’s Operating Handbook”.
3.1. DIMENSIONS
Dimensions of the BushCat nose-wheel and tail-dragger variants are shown on the followings pages.



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3.2. BAGGAGE SPACE
The aircraft is fitted with two storage areas as standard:
Upper baggage area behind seats:
Capacity:
59 litres
(2 ft3)
Maximum load:
23.2 kg
(51 lbs)
Lower luggage area behind seats:
Capacity:
150 litres
(5.3 ft3)
Maximum load:
6.8 kg
(15 lbs)
This combination results in a maximum baggage weight of 30kg (66lbs).
3.3. CABIN AND ENTRY DIMENSIONS
Door width:
900 mm
(35.4 inches)
Door height:
800 mm
(31.5 inches)
3.4. SPECIFIC LOADINGS
Minimum*
Maximum
Wing loading
23.56 kg/m2
(4.83 lbs/ft2)
560 kg
(1230 lbs)
MTOW
41.24 kg/m2
(8.45 lbs/ft2)
600 kg
(1320 lbs)
MTOW
44.18 kg/m2
(9.05 lbs/ft2)
Power loading
Rotax 912 UL
4.0 kg/HP
(8.81 lbs/HP)
560 kg
(1230 lbs)
MTOW
7.0 kg/HP
(15.40 lbs/HP)
600 kg
(1320 lbs)
MTOW
7.5 kg/HP
(16.52 lbs/HP)
Rotax 912 ULS
3.2 kg/HP
(7.05 lbs/HP)
560 kg
(1230 lbs)
MTOW
5.6 kg/HP
(12.33 lbs/HP)
600 kg
(1320 lbs)
MTOW
6.0 kg/HP
(13.22 lbs/HP)
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