Experience the world of Rotax aircraft engines
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POWERING YOUR ULTIMATE FLIGHT Experience the world of Rotax aircraft engines Issoire Aviation / APM Simba / Rotax 915 iS, 915 iSc
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Transcript of Experience the world of Rotax aircraft engines
Powering yourultimate flightexperience the world of Rotax aircraft engines
issoire Aviation / APM Simba / rotax 915 iS, 915 iSc
BRP iS A world leAder in the deSign, MAnufActuring, diS-tribution, And MArketing of Motorized recreAtionAl vehicleS And PowerSPortS engineS.
BRP-Rotax iS A MArket leAder in the develoPing And MAnufActuring of innovAtive PowertrAinS for PowerSPort ProductS.
nAMe:BRP-Rotax GmbH & Co KG
locAtionS:Gunskirchen, Austria (Europe)
MAnufActuring SiteS:Austria, Mexico
eMPloyeeS:1,150
ProcureMent office:Hong Kong
ownerShiP:100% subsidiary of BRP
Our high-tech premium engines for maximum performance, light weight, fuel efficiency, longevity and reliability, form the hearts of le-gendary BRP products as well as of motorcycles, karts and light and ultralight aircraft. We have developed more than 350 Rotax engine models and produced over 7 million engines.
nAMe:Bombardier Recreational Products Inc. (BRP)
heAdquArterS: Valcourt, Québec (Canada)
MAnufActuring SiteS:Canada, USA, Mexico, Finland, Austria
eMPloyeeS:8,700 worldwide
ownerShiP:Shares are traded on the Toronto Stock Exchange under the symbol „DOO“
With our high-performance engines that power the world of mo-tor sports we set the pace for the industry with legendary products such as Ski-Doo and Lynx snowmobiles, Sea-Doo watercraft, Can-Am all-terrain and side-by-side vehicles, and Can-Am Spyder roadsters.
AS the lArgeSt Producer of SMAll gASoline AircrAft engineS in the world, our AircrAft engineS Are the firSt choice of More thAn 250 AircrAft MAnufActurerS Around the globe. Join uS.
benefit froM iMProved fuel efficiency, low-oPerAting coStS, clASS leAding Power to weight rAtio, beSt in-clASS uSeful loAd And flight rAnge, And the well known reliAbility.
unleash the PoweR, enjoy the lightness, exceed youR exPectations.
rotAx AircrAft engineS, the coMPAny And itS ownerShiP
180,000+ rotAx AircrAft engineS Produced
50,000+ engineS of the 912/914 engine SerieS Produced
50.000+ rotAx AircrAft engineS in oPerAtion
rotAx AircrAft engineS, the coMPAny And itS ownerShiP
SPreAd your wingS
fActS & figureS 60+ Million flying hourS
of the rotAx 912/914/915 engineS fleet
APProx. 5 Million flying hourS of the rotAx 912/914/915 engineS fleet Per yeAr
the sky is the limit
icon / A5 / rotax 912 iS Sport
our wArrAntieS And Service network
Service Center
Repair Center
Distributor* only applies to the Rotax 912 and 914 engine series
wherever you Are, we Are with youWe are committed to highest customer satisfaction by offering you outstanding service and support. The sales and service of our aircraft engines and genuine replacement parts are provided by authorized distributors and their network on all 5 continents in more than 100 countries.
Our distributor network has factory trained mechanics and provides professional service for your engine throughout its life. Our service partners have a well-stocked inventory to enable you to spend even more time in the air. Rotax genuine spare parts are covered by the manufacturer’s warranty. Parts availability for Rotax aircraft engines is guaranteed for at least ten years.
RegulaR waRRanty foR 4-stRoke engines24 months or 400 hours (whatever comes first) of regular warranty for certified 4-stroke engines
18 months or 200 hours (whatever comes first) of regular warranty for non-certified 4-stroke engines
Rotax extended seRvice teRms (R.e.s.t.)*Beside the regular manufacturer warranty, the high quality standards enable BRP-Rotax to offer you a special program called the Rotax Ex-tended Service Terms (R.E.S.T.) with two different types of extended warranty for Rotax 4-stroke aircraft engines (this offer only applies if allowed under applicable law).
one yeaR Plus coveRageR.E.S.T. Rotax Extended Service Terms +1 additional year or up to 200 hours, whatever comes first
full tBo coveRageR.E.S.T. Rotax Extended Service Terms+3 additional years or up to TBO of 2,000 hours, whatever comes first
engine RegistRation Easy paperless engine
registration process Increase of service quality Security feature: no way of
re-registration of stolen engines
attendees from engine operators to maintenance personnel. To offer you our full support, manuals, catalogues and all useful documentation are downloadable free of charge at www.flyrotax.com
In the scope of providing highest quality, our globally standardized training program called ”iRMT“ (independent Rotax Maintenance Trai-ning) provides the relevant knowledge and technical education to all
woRldwide on site
our wArrAntieS And Service network
At your Service
Service Center
Repair Center
Distributor
duRaBility & ReliaBility redundAnt ignition SySteM
liquid And Air cooled
teSting ProcedureS exceeding certificAtion StAndArdS
oPen youRself to new PossiBilities
the technicAl detAilS of our excePtionAl AircrAft engineS
Air-fuel MixtureThe iS technology offers optimized air-fuel mixture at all operatingconditions as well as easy starts under cold weather conditionscompared to carburetor engines.
PerforMAnce*Due to a turbocharger system which is capable for high pressure ratiosand to the new designed gearbox with improved gear ratio, sufficient performance at low propeller rpm is provided to power even 4-seater aircraft consistently up to 15,000 ft with full power.
PoweR & PeRfoRmance reduction geAr box
eASe of uSe
AdditionAl AlternAtor
low oPeRating & oPeRational costs
uSAge of different fuel tyPeS
overloAd clutch
iS inJection technology
* Rotax 915 iS/iSc
oPen youRself to new PossiBilities
the technicAl detAilS of our excePtionAl AircrAft engineS
redundAnt inJectorSFuel injection is controlled individually by the ECU via two redundant injectors per cylinder. This gives you a more fuel-efficient flight thanks to an optimized calibration of the fuel-air mixture. The outcome: longer flight distances.
eco ModeThe engines automatically improve its fuel efficiency by switching to a lean ECO mode once the throttle is pulled back to a throttle setting below 97% after start and climb phases.
budSThe BRP Utility and Diagnostic Software for Rotax aircraft engines (BUDS Aircraft) is designed to give you insight into the engine manage-ment system and enables mechanics to make fast engine checks.
eASe of uSeVarious features such as knock control or engine management system (EMS) in combination with other advantages such as no carburator icing and transient engine behaviour lead to an improved and easy operation.
eMSThe Engine Management System (EMS) controls ignition, fuel- and air mixture electronically and is implemented redundantly to ensure a higher level of safety. The system is designed to be single fault redundant.
ecuThe Electronic Control Unit (ECU) controls the fuel and air mixtureelectronically and is implemented redundantly into the EMS to ensurea higher level of safety.
582 UL65 HP 912 UL/A/F80 HP 912 ULS/S100 HP 912 iS/iSc100 HP SPOR
T
914 UL/F115 HP 915 iS/iSc141 HP
4-cylinder 4-stroke liquid-/air-cooled engine
with opposed cylinders Dry sump forced lubrication
with separate oil tank, automatic adjustment by hydraulic valve tappets Redundant electronic fuel injection Engine management system
Electric starter Propeller speed reduction gearbox Air intake system TBO 2,000 hrs
2-cylinder 2-stroke liquid-cooled engine
with rotary valve intake Dual electronic ignition Integrated water pump and thermostat Exhaust system Carburetors
4-cylinder 4-stroke liquid-/air-cooled engine
with opposed cylinders Dry sump forced lubrication
with separate oil tank, automatic adjustment by hydraulic valve tappet 2 carburetors Mechanical fuel pump
Dual electronic ignition Electric starter Propeller speed reduction gearbox TBO 2,000 hrs
The Rotax 912 iS Sport engine offers all well known advantages of the Rotax 4-stroke engine series complemented by additional features, for example, the engine management system.
This engine series is available as non-certified (Rotax 912 iS) as well as certified version (Rotax 912 iSc) according to CS-E.
4-cylinder 4-stroke liquid-/air-cooled engine
with opposed cylinders Dry sump forced lubrication
with separate oil tank, automatic adjustment by hydraulic valve tappet 2 carburetors Mechanical fuel pump
Dual-electronic ignition Electric starter Propeller speed reduction gearbox Air intake system TBO 2,000 hrs
4-cylinder 4-stroke liquid-/air-cooled engine
with opposed cylinders With turbo charger With automatic waste gate control Dry sump forced lubrication
with separate oil tank Automatic adjustment
by hydraulic valve tappet
2 carburetors Dual electronic ignition Electric starter Propeller speed reduction gearbox Engine mount assembly Air intake system Exhaust system TBO 2,000 hrs
In comparison to the 80 hp version of the Rotax 912 series the 100 hp product line offers more power while keeping the same weight.
This engine series offers the best power to weight ratio in its class and is available as non-certified (Rotax 912 ULS) and certified engine (Rotax 912 S) according to FAR33.
The Rotax 912 series is well regarded for its reliability and efficiencyand is primarily targeted as the entry level motor in the light aviationindustry. The 80 hp version of the Rotax 912 series is available asnon-certified (Rotax 912 UL) as well as certified version according to FAR 33 (Rotax 912 F) and JAR 22 (Rotax 912 A).
Over 30,000 units of this popular Rotax 2-stroke engine have been sold. This engine type is well regarded for its easy maintenance and robustness.
Based on the proven concept of the Rotax 912 / 914 engine series, the Rotax 915 iS engine offers more power, the best power-to-weight ratio in its class, full take-off power up to 15,000 feet (4,570 m) and a service ceiling of 23,000 feet (7,010 m). Available as ASTM compliant version (Rotax 915 iS)as well as EASA CS-E certified (Rotax 915 iSc).
The turbo charged Rotax 914 series offers more performance at high altitudes while delivering lower weight engines.
This series is available as non-certified version (Rotax 914 UL)and certified version (Rotax 914 F) according to FAR 33 andJAR-E.
Engine with propeller speed reduction gearbox i = 2.43
Exhaust system
Overload clutch
Engine suspension frame
External alternator
Air guide hood
Airbox
128 Nm
WEIghT
PERfORMANCE
TORquE
MA x RPM*
BORE STROkE
DISPl ACEMENT fuElmin. MON 85 RON 95*
min. AkI 91*1352 cm3 82.6 cu in
61.0 mm84.0 mm 3.31 in 2.4 in
5800 1/min.
94 ft. lb. 5100 1/min.
73.5 kW 100 hp 5800 1/min.
56.6
4.0
1.7
2.0
3.0
0.8
1.3
124.5
8.8
3.7
4.4
6.6
1.8
2.8
kg lbEngine with propeller speed reduction gearbox i = 2.43 with overload clutch
Exhaust system
Engine mount
External alternator
Air guide hood
fuel pumps assy
WEIghT
PERfORMANCE
TORquE
MA x RPM limited for max. 5 minutes
BORE STROkE
DISPl ACEMENT fuElmin. MON 85 RON 95*
min. AkI 91*1352 cm3 82.6 cu in
61.0 mm84.0 mm 3.31 in 2.4 in
5800 1/min.
73.5 kW 72.0 kW** 68.0 kW
100 hp98 hp
92.5 hp
5800 1/min5500 1/min5000 1/min
63.6
4.8
2.0
3.0
0.4
1.6
140.2
10.5
4.4
6.6
0.8
3.5
kg lbEngine with gearbox, turbocharger, intercooler, cooling air baffle, wi-ring harness, sensors, flange with overboost valve, air hoses, clamps, magneto valve block with hoses, ECu, fusebox with regulators, oil tank, exhaust system.
Without fuel pumps assembly, radiator and oil cooler
99 kW
WEIghT
MA x. TAkE-Off PERfORMANCE
MA x. CONTINuOuS PERfORMANCE
BORE STROkE
DISPl ACEMENT fuElmin. MON 85 RON 95
min. AkI 911352 cm3 82.5 cu in
61.0 mm84.0 mm 3.31 in 2.4 in
135 hp 5500 1/min.
104 kW 141 hp 5800 1/min.
84.6 186.4
kg lbEngine with propeller speed reduction gearbox i = 2.43
Exhaust system
Overload clutch
Engine suspension frame
External alternator
Air guide hood
144 Nm
WEIghT
PERfORMANCE
TORquE
MA x RPM*
BORE STROkE
DISPl ACEMENT fuElmin. MON 85 RON 95*
min. AkI 91*1211.2 cm3 73.91 cu in
61.0 mm79.5 mm 3.13 in 2.4 in
5800 1/min.
106 ft. lb. 4900 1/min.
84.5 kW 115 hp 5800 1/min.
64.0
4.0
1.7
2.0
3.0
0.8
140.8
8.8
3.7
3.7
6.6
1.8
kg lbEngine
Exhaust system
2 carburetors
Electric starter
PSRg* “B“ / i = 2.58
PSRg* “C“ / i = 2.62 / 3.0 / 3.47 / 4.0
PSRg* “E“ / i = 2.62 / 3.0 / 3.47 / 4.0*Propeller speed reduction gearbox
75 Nm
WEIghT
PERfORMANCE
TORquE
MA x RPM
BORE STROkE
DISPl ACEMENT fuElmin. MON 83 RON 91**
min. AkI 87**580 cm3 35.4 cu in
64.0 mm76.0 mm 2.99 in 2.52 in
6800 1/min.
55.3 ft. lb. 6000 1/min.
48.0 kW 65 hp 6500 1/min.
29.1
5.1
1.8
3.5
4.5
8.0
11.2
64.0
11.2
4.0
7.7
9.9
17.6
24.7
kg lbEngine with propeller speed reduction gearbox i = 2.27 (opt. i = 2.43)
Exhaust system
Overload clutch
Engine suspension frame
External alternator
Air guide hood
Airbox
103 Nm
WEIghT
PERfORMANCE
TORquE
MA x RPM*
BORE STROkE
DISPl ACEMENT fuElmin. MON 83 RON 91*
min. AkI 87*1211.2 cm3 73.9 cu in
61.0 mm79.5 mm 3.13 in 2.4 in
5800 1/min.
75.9 ft. lb. 4800 1/min.
59.6 kW 80 hp 5800 1/min.
55.4
4.0
1.7
2.0
3.0
0.8
1.3
122.0
8.8
3.7
4.4
6.6
1.8
2.8
kg lb
POWERINg yOuRULTimATe FLigHT
ROTAx engineS
** leaded, unleaded, AVgAS 100ll Ethanol 10 * leaded, unleaded, AVgAS 100ll Ethanol 10 * leaded, unleaded, AVgAS 100ll Ethanol 10 * leaded, unleaded, AVgAS 100ll Ethanol 10 * leaded, unleaded, AVgAS 100ll Ethanol 10
4-cylinder 4-stroke liquid-/air-cooled engine
with horizontally opposed cylinders Dry sump forced lubrication
with separate oil tank, automatic adjustment by hydraulic valve tappet Redundant electronic fuel injection
and ignition Engine management system (EMS)
Electric starter (12 or 24 volt) Propeller speed reduction gearbox Air intake system with intercooler Turbocharger with stainless steel
exhaust Service ceiling of 23,000 feet TBO 1,200 hrs
121 Nm 125 Nm 132 Nm***
89 ft. lb.92 ft. lb.97 ft. lb.
5800 1/min5500 1/min5000 1/min
** max. continuous power at 5500 1/min *** MOgAS, no hydraulic governor
Picture: Rotax 912 ulS - DCDI with options Picture: Rotax 914 ul - DCDI with options Engine performance may vary depending on, among other things, general conditions, ambient temperature and altitude.
AlTITuDE PERfORMANCE - ISA CONDITIONS
Engi
ne P
ower
[%] o
f Max
imum
Cob
ntin
uous
Pow
er
80
60
40
20
100
0 5000 10000 15000 23000 30000912 ulS/S 912 iS 914 915 iSAltitude [ft]
1) Information on the back side of the brochure
fuel
Con
sum
ptio
n [l
iter]
per f
light
hou
r
fuel Costs [Euro] per 100 flight hoursvs. 912 iS Sport
fuel type
fuEl CONSuMPTION AND fuEl COSTS VS. 912 iS SPORT1)30
25
20
15
582 UL65 HP 912 UL/A/F80 HP 912 ULS/S100 HP 912 iS/iSc100 HP SPOR
T
914 UL/F115 HP 915 iS/iSc141 HP
4-cylinder 4-stroke liquid-/air-cooled engine
with opposed cylinders Dry sump forced lubrication
with separate oil tank, automatic adjustment by hydraulic valve tappets Redundant electronic fuel injection Engine management system
Electric starter Propeller speed reduction gearbox Air intake system TBO 2,000 hrs
2-cylinder 2-stroke liquid-cooled engine
with rotary valve intake Dual electronic ignition Integrated water pump and thermostat Exhaust system Carburetors
4-cylinder 4-stroke liquid-/air-cooled engine
with opposed cylinders Dry sump forced lubrication
with separate oil tank, automatic adjustment by hydraulic valve tappet 2 carburetors Mechanical fuel pump
Dual electronic ignition Electric starter Propeller speed reduction gearbox TBO 2,000 hrs
The Rotax 912 iS Sport engine offers all well known advantages of the Rotax 4-stroke engine series complemented by additional features, for example, the engine management system.
This engine series is available as non-certified (Rotax 912 iS) as well as certified version (Rotax 912 iSc) according to CS-E.
4-cylinder 4-stroke liquid-/air-cooled engine
with opposed cylinders Dry sump forced lubrication
with separate oil tank, automatic adjustment by hydraulic valve tappet 2 carburetors Mechanical fuel pump
Dual-electronic ignition Electric starter Propeller speed reduction gearbox Air intake system TBO 2,000 hrs
4-cylinder 4-stroke liquid-/air-cooled engine
with opposed cylinders With turbo charger With automatic waste gate control Dry sump forced lubrication
with separate oil tank Automatic adjustment
by hydraulic valve tappet
2 carburetors Dual electronic ignition Electric starter Propeller speed reduction gearbox Engine mount assembly Air intake system Exhaust system TBO 2,000 hrs
In comparison to the 80 hp version of the Rotax 912 series the 100 hp product line offers more power while keeping the same weight.
This engine series offers the best power to weight ratio in its class and is available as non-certified (Rotax 912 ULS) and certified engine (Rotax 912 S) according to FAR33.
The Rotax 912 series is well regarded for its reliability and efficiencyand is primarily targeted as the entry level motor in the light aviationindustry. The 80 hp version of the Rotax 912 series is available asnon-certified (Rotax 912 UL) as well as certified version according to FAR 33 (Rotax 912 F) and JAR 22 (Rotax 912 A).
Over 30,000 units of this popular Rotax 2-stroke engine have been sold. This engine type is well regarded for its easy maintenance and robustness.
Based on the proven concept of the Rotax 912 / 914 engine series, the Rotax 915 iS engine offers more power, the best power-to-weight ratio in its class, full take-off power up to 15,000 feet (4,570 m) and a service ceiling of 23,000 feet (7,010 m). Available as ASTM compliant version (Rotax 915 iS)as well as EASA CS-E certified (Rotax 915 iSc).
The turbo charged Rotax 914 series offers more performance at high altitudes while delivering lower weight engines.
This series is available as non-certified version (Rotax 914 UL)and certified version (Rotax 914 F) according to FAR 33 andJAR-E.
Engine with propeller speed reduction gearbox i = 2.43
Exhaust system
Overload clutch
Engine suspension frame
External alternator
Air guide hood
Airbox
128 Nm
WEIghT
PERfORMANCE
TORquE
MA x RPM*
BORE STROkE
DISPl ACEMENT fuElmin. MON 85 RON 95*
min. AkI 91*1352 cm3 82.6 cu in
61.0 mm84.0 mm 3.31 in 2.4 in
5800 1/min.
94 ft. lb. 5100 1/min.
73.5 kW 100 hp 5800 1/min.
56.6
4.0
1.7
2.0
3.0
0.8
1.3
124.5
8.8
3.7
4.4
6.6
1.8
2.8
kg lbEngine with propeller speed reduction gearbox i = 2.43 with overload clutch
Exhaust system
Engine mount
External alternator
Air guide hood
fuel pumps assy
WEIghT
PERfORMANCE
TORquE
MA x RPM limited for max. 5 minutes
BORE STROkE
DISPl ACEMENT fuElmin. MON 85 RON 95*
min. AkI 91*1352 cm3 82.6 cu in
61.0 mm84.0 mm 3.31 in 2.4 in
5800 1/min.
73.5 kW 72.0 kW** 68.0 kW
100 hp98 hp
92.5 hp
5800 1/min5500 1/min5000 1/min
63.6
4.8
2.0
3.0
0.4
1.6
140.2
10.5
4.4
6.6
0.8
3.5
kg lbEngine with gearbox, turbocharger, intercooler, cooling air baffle, wi-ring harness, sensors, flange with overboost valve, air hoses, clamps, magneto valve block with hoses, ECu, fusebox with regulators, oil tank, exhaust system.
Without fuel pumps assembly, radiator and oil cooler
99 kW
WEIghT
MA x. TAkE-Off PERfORMANCE
MA x. CONTINuOuS PERfORMANCE
BORE STROkE
DISPl ACEMENT fuElmin. MON 85 RON 95
min. AkI 911352 cm3 82.5 cu in
61.0 mm84.0 mm 3.31 in 2.4 in
135 hp 5500 1/min.
104 kW 141 hp 5800 1/min.
84.6 186.4
kg lbEngine with propeller speed reduction gearbox i = 2.43
Exhaust system
Overload clutch
Engine suspension frame
External alternator
Air guide hood
144 Nm
WEIghT
PERfORMANCE
TORquE
MA x RPM*
BORE STROkE
DISPl ACEMENT fuElmin. MON 85 RON 95*
min. AkI 91*1211.2 cm3 73.91 cu in
61.0 mm79.5 mm 3.13 in 2.4 in
5800 1/min.
106 ft. lb. 4900 1/min.
84.5 kW 115 hp 5800 1/min.
64.0
4.0
1.7
2.0
3.0
0.8
140.8
8.8
3.7
3.7
6.6
1.8
kg lbEngine
Exhaust system
2 carburetors
Electric starter
PSRg* “B“ / i = 2.58
PSRg* “C“ / i = 2.62 / 3.0 / 3.47 / 4.0
PSRg* “E“ / i = 2.62 / 3.0 / 3.47 / 4.0*Propeller speed reduction gearbox
75 Nm
WEIghT
PERfORMANCE
TORquE
MA x RPM
BORE STROkE
DISPl ACEMENT fuElmin. MON 83 RON 91**
min. AkI 87**580 cm3 35.4 cu in
64.0 mm76.0 mm 2.99 in 2.52 in
6800 1/min.
55.3 ft. lb. 6000 1/min.
48.0 kW 65 hp 6500 1/min.
29.1
5.1
1.8
3.5
4.5
8.0
11.2
64.0
11.2
4.0
7.7
9.9
17.6
24.7
kg lbEngine with propeller speed reduction gearbox i = 2.27 (opt. i = 2.43)
Exhaust system
Overload clutch
Engine suspension frame
External alternator
Air guide hood
Airbox
103 Nm
WEIghT
PERfORMANCE
TORquE
MA x RPM*
BORE STROkE
DISPl ACEMENT fuElmin. MON 83 RON 91*
min. AkI 87*1211.2 cm3 73.9 cu in
61.0 mm79.5 mm 3.13 in 2.4 in
5800 1/min.
75.9 ft. lb. 4800 1/min.
59.6 kW 80 hp 5800 1/min.
55.4
4.0
1.7
2.0
3.0
0.8
1.3
122.0
8.8
3.7
4.4
6.6
1.8
2.8
kg lb
POWERINg yOuRULTimATe FLigHT
ROTAx engineS
** leaded, unleaded, AVgAS 100ll Ethanol 10 * leaded, unleaded, AVgAS 100ll Ethanol 10 * leaded, unleaded, AVgAS 100ll Ethanol 10 * leaded, unleaded, AVgAS 100ll Ethanol 10 * leaded, unleaded, AVgAS 100ll Ethanol 10
4-cylinder 4-stroke liquid-/air-cooled engine
with horizontally opposed cylinders Dry sump forced lubrication
with separate oil tank, automatic adjustment by hydraulic valve tappet Redundant electronic fuel injection
and ignition Engine management system (EMS)
Electric starter (12 or 24 volt) Propeller speed reduction gearbox Air intake system with intercooler Turbocharger with stainless steel
exhaust Service ceiling of 23,000 feet TBO 1,200 hrs
121 Nm 125 Nm 132 Nm***
89 ft. lb.92 ft. lb.97 ft. lb.
5800 1/min5500 1/min5000 1/min
** max. continuous power at 5500 1/min *** MOgAS, no hydraulic governor
Picture: Rotax 912 ulS - DCDI with options Picture: Rotax 914 ul - DCDI with options Engine performance may vary depending on, among other things, general conditions, ambient temperature and altitude.
AlTITuDE PERfORMANCE - ISA CONDITIONS
Engi
ne P
ower
[%] o
f Max
imum
Cob
ntin
uous
Pow
er
80
60
40
20
100
0 5000 10000 15000 23000 30000912 ulS/S 912 iS 914 915 iSAltitude [ft]
1) Information on the back side of the brochure
fuel
Con
sum
ptio
n [l
iter]
per f
light
hou
r
fuel Costs [Euro] per 100 flight hoursvs. 912 iS Sport
fuel type
fuEl CONSuMPTION AND fuEl COSTS VS. 912 iS SPORT1)30
25
20
15
582 UL65 HP 912 UL/A/F80 HP 912 ULS/S100 HP 912 iS/iSc100 HP SPOR
T
914 UL/F115 HP 915 iS/iSc141 HP
4-cylinder 4-stroke liquid-/air-cooled engine
with opposed cylinders Dry sump forced lubrication
with separate oil tank, automatic adjustment by hydraulic valve tappets Redundant electronic fuel injection Engine management system
Electric starter Propeller speed reduction gearbox Air intake system TBO 2,000 hrs
2-cylinder 2-stroke liquid-cooled engine
with rotary valve intake Dual electronic ignition Integrated water pump and thermostat Exhaust system Carburetors
4-cylinder 4-stroke liquid-/air-cooled engine
with opposed cylinders Dry sump forced lubrication
with separate oil tank, automatic adjustment by hydraulic valve tappet 2 carburetors Mechanical fuel pump
Dual electronic ignition Electric starter Propeller speed reduction gearbox TBO 2,000 hrs
The Rotax 912 iS Sport engine offers all well known advantages of the Rotax 4-stroke engine series complemented by additional features, for example, the engine management system.
This engine series is available as non-certified (Rotax 912 iS) as well as certified version (Rotax 912 iSc) according to CS-E.
4-cylinder 4-stroke liquid-/air-cooled engine
with opposed cylinders Dry sump forced lubrication
with separate oil tank, automatic adjustment by hydraulic valve tappet 2 carburetors Mechanical fuel pump
Dual-electronic ignition Electric starter Propeller speed reduction gearbox Air intake system TBO 2,000 hrs
4-cylinder 4-stroke liquid-/air-cooled engine
with opposed cylinders With turbo charger With automatic waste gate control Dry sump forced lubrication
with separate oil tank Automatic adjustment
by hydraulic valve tappet
2 carburetors Dual electronic ignition Electric starter Propeller speed reduction gearbox Engine mount assembly Air intake system Exhaust system TBO 2,000 hrs
In comparison to the 80 hp version of the Rotax 912 series the 100 hp product line offers more power while keeping the same weight.
This engine series offers the best power to weight ratio in its class and is available as non-certified (Rotax 912 ULS) and certified engine (Rotax 912 S) according to FAR33.
The Rotax 912 series is well regarded for its reliability and efficiencyand is primarily targeted as the entry level motor in the light aviationindustry. The 80 hp version of the Rotax 912 series is available asnon-certified (Rotax 912 UL) as well as certified version according to FAR 33 (Rotax 912 F) and JAR 22 (Rotax 912 A).
Over 30,000 units of this popular Rotax 2-stroke engine have been sold. This engine type is well regarded for its easy maintenance and robustness.
Based on the proven concept of the Rotax 912 / 914 engine series, the Rotax 915 iS engine offers more power, the best power-to-weight ratio in its class, full take-off power up to 15,000 feet (4,570 m) and a service ceiling of 23,000 feet (7,010 m). Available as ASTM compliant version (Rotax 915 iS)as well as EASA CS-E certified (Rotax 915 iSc).
The turbo charged Rotax 914 series offers more performance at high altitudes while delivering lower weight engines.
This series is available as non-certified version (Rotax 914 UL)and certified version (Rotax 914 F) according to FAR 33 andJAR-E.
Engine with propeller speed reduction gearbox i = 2.43
Exhaust system
Overload clutch
Engine suspension frame
External alternator
Air guide hood
Airbox
128 Nm
WEIghT
PERfORMANCE
TORquE
MA x RPM*
BORE STROkE
DISPl ACEMENT fuElmin. MON 85 RON 95*
min. AkI 91*1352 cm3 82.6 cu in
61.0 mm84.0 mm 3.31 in 2.4 in
5800 1/min.
94 ft. lb. 5100 1/min.
73.5 kW 100 hp 5800 1/min.
56.6
4.0
1.7
2.0
3.0
0.8
1.3
124.5
8.8
3.7
4.4
6.6
1.8
2.8
kg lbEngine with propeller speed reduction gearbox i = 2.43 with overload clutch
Exhaust system
Engine mount
External alternator
Air guide hood
fuel pumps assy
WEIghT
PERfORMANCE
TORquE
MA x RPM limited for max. 5 minutes
BORE STROkE
DISPl ACEMENT fuElmin. MON 85 RON 95*
min. AkI 91*1352 cm3 82.6 cu in
61.0 mm84.0 mm 3.31 in 2.4 in
5800 1/min.
73.5 kW 72.0 kW** 68.0 kW
100 hp98 hp
92.5 hp
5800 1/min5500 1/min5000 1/min
63.6
4.8
2.0
3.0
0.4
1.6
140.2
10.5
4.4
6.6
0.8
3.5
kg lbEngine with gearbox, turbocharger, intercooler, cooling air baffle, wi-ring harness, sensors, flange with overboost valve, air hoses, clamps, magneto valve block with hoses, ECu, fusebox with regulators, oil tank, exhaust system.
Without fuel pumps assembly, radiator and oil cooler
99 kW
WEIghT
MA x. TAkE-Off PERfORMANCE
MA x. CONTINuOuS PERfORMANCE
BORE STROkE
DISPl ACEMENT fuElmin. MON 85 RON 95
min. AkI 911352 cm3 82.5 cu in
61.0 mm84.0 mm 3.31 in 2.4 in
135 hp 5500 1/min.
104 kW 141 hp 5800 1/min.
84.6 186.4
kg lbEngine with propeller speed reduction gearbox i = 2.43
Exhaust system
Overload clutch
Engine suspension frame
External alternator
Air guide hood
144 Nm
WEIghT
PERfORMANCE
TORquE
MA x RPM*
BORE STROkE
DISPl ACEMENT fuElmin. MON 85 RON 95*
min. AkI 91*1211.2 cm3 73.91 cu in
61.0 mm79.5 mm 3.13 in 2.4 in
5800 1/min.
106 ft. lb. 4900 1/min.
84.5 kW 115 hp 5800 1/min.
64.0
4.0
1.7
2.0
3.0
0.8
140.8
8.8
3.7
3.7
6.6
1.8
kg lbEngine
Exhaust system
2 carburetors
Electric starter
PSRg* “B“ / i = 2.58
PSRg* “C“ / i = 2.62 / 3.0 / 3.47 / 4.0
PSRg* “E“ / i = 2.62 / 3.0 / 3.47 / 4.0*Propeller speed reduction gearbox
75 Nm
WEIghT
PERfORMANCE
TORquE
MA x RPM
BORE STROkE
DISPl ACEMENT fuElmin. MON 83 RON 91**
min. AkI 87**580 cm3 35.4 cu in
64.0 mm76.0 mm 2.99 in 2.52 in
6800 1/min.
55.3 ft. lb. 6000 1/min.
48.0 kW 65 hp 6500 1/min.
29.1
5.1
1.8
3.5
4.5
8.0
11.2
64.0
11.2
4.0
7.7
9.9
17.6
24.7
kg lbEngine with propeller speed reduction gearbox i = 2.27 (opt. i = 2.43)
Exhaust system
Overload clutch
Engine suspension frame
External alternator
Air guide hood
Airbox
103 Nm
WEIghT
PERfORMANCE
TORquE
MA x RPM*
BORE STROkE
DISPl ACEMENT fuElmin. MON 83 RON 91*
min. AkI 87*1211.2 cm3 73.9 cu in
61.0 mm79.5 mm 3.13 in 2.4 in
5800 1/min.
75.9 ft. lb. 4800 1/min.
59.6 kW 80 hp 5800 1/min.
55.4
4.0
1.7
2.0
3.0
0.8
1.3
122.0
8.8
3.7
4.4
6.6
1.8
2.8
kg lb
POWERINg yOuRULTimATe FLigHT
ROTAx engineS
** leaded, unleaded, AVgAS 100ll Ethanol 10 * leaded, unleaded, AVgAS 100ll Ethanol 10 * leaded, unleaded, AVgAS 100ll Ethanol 10 * leaded, unleaded, AVgAS 100ll Ethanol 10 * leaded, unleaded, AVgAS 100ll Ethanol 10
4-cylinder 4-stroke liquid-/air-cooled engine
with horizontally opposed cylinders Dry sump forced lubrication
with separate oil tank, automatic adjustment by hydraulic valve tappet Redundant electronic fuel injection
and ignition Engine management system (EMS)
Electric starter (12 or 24 volt) Propeller speed reduction gearbox Air intake system with intercooler Turbocharger with stainless steel
exhaust Service ceiling of 23,000 feet TBO 1,200 hrs
121 Nm 125 Nm 132 Nm***
89 ft. lb.92 ft. lb.97 ft. lb.
5800 1/min5500 1/min5000 1/min
** max. continuous power at 5500 1/min *** MOgAS, no hydraulic governor
Picture: Rotax 912 ulS - DCDI with options Picture: Rotax 914 ul - DCDI with options Engine performance may vary depending on, among other things, general conditions, ambient temperature and altitude.
AlTITuDE PERfORMANCE - ISA CONDITIONS
Engi
ne P
ower
[%] o
f Max
imum
Cob
ntin
uous
Pow
er
80
60
40
20
100
0 5000 10000 15000 23000 30000912 ulS/S 912 iS 914 915 iSAltitude [ft]
1) Information on the back side of the brochure
fuel
Con
sum
ptio
n [l
iter]
per f
light
hou
r
fuel Costs [Euro] per 100 flight hoursvs. 912 iS Sport
fuel type
fuEl CONSuMPTION AND fuEl COSTS VS. 912 iS SPORT1)30
25
20
15
582 UL65 HP 912 UL/A/F80 HP 912 ULS/S100 HP 912 iS/iSc100 HP SPOR
T
914 UL/F115 HP 915 iS/iSc141 HP
4-cylinder 4-stroke liquid-/air-cooled engine
with opposed cylinders Dry sump forced lubrication
with separate oil tank, automatic adjustment by hydraulic valve tappets Redundant electronic fuel injection Engine management system
Electric starter Propeller speed reduction gearbox Air intake system TBO 2,000 hrs
2-cylinder 2-stroke liquid-cooled engine
with rotary valve intake Dual electronic ignition Integrated water pump and thermostat Exhaust system Carburetors
4-cylinder 4-stroke liquid-/air-cooled engine
with opposed cylinders Dry sump forced lubrication
with separate oil tank, automatic adjustment by hydraulic valve tappet 2 carburetors Mechanical fuel pump
Dual electronic ignition Electric starter Propeller speed reduction gearbox TBO 2,000 hrs
The Rotax 912 iS Sport engine offers all well known advantages of the Rotax 4-stroke engine series complemented by additional features, for example, the engine management system.
This engine series is available as non-certified (Rotax 912 iS) as well as certified version (Rotax 912 iSc) according to CS-E.
4-cylinder 4-stroke liquid-/air-cooled engine
with opposed cylinders Dry sump forced lubrication
with separate oil tank, automatic adjustment by hydraulic valve tappet 2 carburetors Mechanical fuel pump
Dual-electronic ignition Electric starter Propeller speed reduction gearbox Air intake system TBO 2,000 hrs
4-cylinder 4-stroke liquid-/air-cooled engine
with opposed cylinders With turbo charger With automatic waste gate control Dry sump forced lubrication
with separate oil tank Automatic adjustment
by hydraulic valve tappet
2 carburetors Dual electronic ignition Electric starter Propeller speed reduction gearbox Engine mount assembly Air intake system Exhaust system TBO 2,000 hrs
In comparison to the 80 hp version of the Rotax 912 series the 100 hp product line offers more power while keeping the same weight.
This engine series offers the best power to weight ratio in its class and is available as non-certified (Rotax 912 ULS) and certified engine (Rotax 912 S) according to FAR33.
The Rotax 912 series is well regarded for its reliability and efficiencyand is primarily targeted as the entry level motor in the light aviationindustry. The 80 hp version of the Rotax 912 series is available asnon-certified (Rotax 912 UL) as well as certified version according to FAR 33 (Rotax 912 F) and JAR 22 (Rotax 912 A).
Over 30,000 units of this popular Rotax 2-stroke engine have been sold. This engine type is well regarded for its easy maintenance and robustness.
Based on the proven concept of the Rotax 912 / 914 engine series, the Rotax 915 iS engine offers more power, the best power-to-weight ratio in its class, full take-off power up to 15,000 feet (4,570 m) and a service ceiling of 23,000 feet (7,010 m). Available as ASTM compliant version (Rotax 915 iS)as well as EASA CS-E certified (Rotax 915 iSc).
The turbo charged Rotax 914 series offers more performance at high altitudes while delivering lower weight engines.
This series is available as non-certified version (Rotax 914 UL)and certified version (Rotax 914 F) according to FAR 33 andJAR-E.
Engine with propeller speed reduction gearbox i = 2.43
Exhaust system
Overload clutch
Engine suspension frame
External alternator
Air guide hood
Airbox
128 Nm
WEIghT
PERfORMANCE
TORquE
MA x RPM*
BORE STROkE
DISPl ACEMENT fuElmin. MON 85 RON 95*
min. AkI 91*1352 cm3 82.6 cu in
61.0 mm84.0 mm 3.31 in 2.4 in
5800 1/min.
94 ft. lb. 5100 1/min.
73.5 kW 100 hp 5800 1/min.
56.6
4.0
1.7
2.0
3.0
0.8
1.3
124.5
8.8
3.7
4.4
6.6
1.8
2.8
kg lbEngine with propeller speed reduction gearbox i = 2.43 with overload clutch
Exhaust system
Engine mount
External alternator
Air guide hood
fuel pumps assy
WEIghT
PERfORMANCE
TORquE
MA x RPM limited for max. 5 minutes
BORE STROkE
DISPl ACEMENT fuElmin. MON 85 RON 95*
min. AkI 91*1352 cm3 82.6 cu in
61.0 mm84.0 mm 3.31 in 2.4 in
5800 1/min.
73.5 kW 72.0 kW** 68.0 kW
100 hp98 hp
92.5 hp
5800 1/min5500 1/min5000 1/min
63.6
4.8
2.0
3.0
0.4
1.6
140.2
10.5
4.4
6.6
0.8
3.5
kg lbEngine with gearbox, turbocharger, intercooler, cooling air baffle, wi-ring harness, sensors, flange with overboost valve, air hoses, clamps, magneto valve block with hoses, ECu, fusebox with regulators, oil tank, exhaust system.
Without fuel pumps assembly, radiator and oil cooler
99 kW
WEIghT
MA x. TAkE-Off PERfORMANCE
MA x. CONTINuOuS PERfORMANCE
BORE STROkE
DISPl ACEMENT fuElmin. MON 85 RON 95
min. AkI 911352 cm3 82.5 cu in
61.0 mm84.0 mm 3.31 in 2.4 in
135 hp 5500 1/min.
104 kW 141 hp 5800 1/min.
84.6 186.4
kg lbEngine with propeller speed reduction gearbox i = 2.43
Exhaust system
Overload clutch
Engine suspension frame
External alternator
Air guide hood
144 Nm
WEIghT
PERfORMANCE
TORquE
MA x RPM*
BORE STROkE
DISPl ACEMENT fuElmin. MON 85 RON 95*
min. AkI 91*1211.2 cm3 73.91 cu in
61.0 mm79.5 mm 3.13 in 2.4 in
5800 1/min.
106 ft. lb. 4900 1/min.
84.5 kW 115 hp 5800 1/min.
64.0
4.0
1.7
2.0
3.0
0.8
140.8
8.8
3.7
3.7
6.6
1.8
kg lbEngine
Exhaust system
2 carburetors
Electric starter
PSRg* “B“ / i = 2.58
PSRg* “C“ / i = 2.62 / 3.0 / 3.47 / 4.0
PSRg* “E“ / i = 2.62 / 3.0 / 3.47 / 4.0*Propeller speed reduction gearbox
75 Nm
WEIghT
PERfORMANCE
TORquE
MA x RPM
BORE STROkE
DISPl ACEMENT fuElmin. MON 83 RON 91**
min. AkI 87**580 cm3 35.4 cu in
64.0 mm76.0 mm 2.99 in 2.52 in
6800 1/min.
55.3 ft. lb. 6000 1/min.
48.0 kW 65 hp 6500 1/min.
29.1
5.1
1.8
3.5
4.5
8.0
11.2
64.0
11.2
4.0
7.7
9.9
17.6
24.7
kg lbEngine with propeller speed reduction gearbox i = 2.27 (opt. i = 2.43)
Exhaust system
Overload clutch
Engine suspension frame
External alternator
Air guide hood
Airbox
103 Nm
WEIghT
PERfORMANCE
TORquE
MA x RPM*
BORE STROkE
DISPl ACEMENT fuElmin. MON 83 RON 91*
min. AkI 87*1211.2 cm3 73.9 cu in
61.0 mm79.5 mm 3.13 in 2.4 in
5800 1/min.
75.9 ft. lb. 4800 1/min.
59.6 kW 80 hp 5800 1/min.
55.4
4.0
1.7
2.0
3.0
0.8
1.3
122.0
8.8
3.7
4.4
6.6
1.8
2.8
kg lb
POWERINg yOuRULTimATe FLigHT
ROTAx engineS
** leaded, unleaded, AVgAS 100ll Ethanol 10 * leaded, unleaded, AVgAS 100ll Ethanol 10 * leaded, unleaded, AVgAS 100ll Ethanol 10 * leaded, unleaded, AVgAS 100ll Ethanol 10 * leaded, unleaded, AVgAS 100ll Ethanol 10
4-cylinder 4-stroke liquid-/air-cooled engine
with horizontally opposed cylinders Dry sump forced lubrication
with separate oil tank, automatic adjustment by hydraulic valve tappet Redundant electronic fuel injection
and ignition Engine management system (EMS)
Electric starter (12 or 24 volt) Propeller speed reduction gearbox Air intake system with intercooler Turbocharger with stainless steel
exhaust Service ceiling of 23,000 feet TBO 1,200 hrs
121 Nm 125 Nm 132 Nm***
89 ft. lb.92 ft. lb.97 ft. lb.
5800 1/min5500 1/min5000 1/min
** max. continuous power at 5500 1/min *** MOgAS, no hydraulic governor
Picture: Rotax 912 ulS - DCDI with options Picture: Rotax 914 ul - DCDI with options Engine performance may vary depending on, among other things, general conditions, ambient temperature and altitude.
AlTITuDE PERfORMANCE - ISA CONDITIONS
Engi
ne P
ower
[%] o
f Max
imum
Cob
ntin
uous
Pow
er
80
60
40
20
100
0 5000 10000 15000 23000 30000912 ulS/S 912 iS 914 915 iSAltitude [ft]
1) Information on the back side of the brochure
fuel
Con
sum
ptio
n [l
iter]
per f
light
hou
r
fuel Costs [Euro] per 100 flight hoursvs. 912 iS Sport
fuel type
fuEl CONSuMPTION AND fuEl COSTS VS. 912 iS SPORT1)30
25
20
15
firSt in the worldDTA has been working with ROTAX for more than 20 years now, and we have been the first trike manufacturer in the world to install a Rotax 912 engine for trike aircrafts that flew round the world, back in 1995, so the relationship that we have with Rotax has been more than profitable for us.
DTA always had a reputation for quality and reliability, so we do not even think of changing our engine provider since we always talk to people that share the same passion for flying. Rotax has always been receptive to our needs, so it is really a win-win business between us.
George MonierDTA sas
outStAndingIn one word: outstanding! This is one of the greatest developments in aviation piston engines since decades. The 912 series and the 915 iS are all bringing the best from everything Rotax has built over the last 30 years: weight/power ratio, fuel economy, power, performances, high altitude be-nefits, excellent cost of ownership value...
Paolo PascaleCEO, Costruzioni Aeronautiche TECNAM S.r.l.
the Perfect fitThe high power to weight ratio provided by the 9 series Rotax is critical to the overall twin engine design of the AirCam. Add to that excellent re-liability, quite operation and very good fuel efficiency and you have the perfect fit.
Phillip LockwoodAirCam & Lockwood Aviation Supply
hAndS down the winnerWhen it came to ICON choosing a powerplant for the A5 Aircraft based on power-to-weight, reliability, availability, and price ... the Rotax 912 iS was hands down the winner.
Kirk HawkinsCEO, ICON Aircraft Inc.
StAte of the ArtRotax aircraft engines represent the state of the art in design, reliability and customer service. Our relationship with Rotax dates back to the mid 1980’s, we sell our aircraft worldwide with Rotax and with confidence.
We have sold our aircraft to over 30 countries and can always rely on the exceptional reliability and worldwide customer service that Rotax delivers.
Russell Duncan Director, Airborne
oPtiMized coStRotax engines have the perfect power-to-weight balance and and an effi-cient power production to optimize cost of ownership for private pilots as well as for flight schools and other commercial usage. The company offers a global network to support customers with technical advise, spares, ser-vices and AOG support everywhere to keep them flying.
Ivo BoscarolCEO, Pipistrel d.o.o. Ajdovscina
beSt Product on the MArketWe choose Rotax because we have known it for decades, even before aircraft engines, we knew Rotax for motorcycle engines. We believe it is currently the best product on the market in terms of reliability.
Our company rejects the installation of handmade products or derivatives, Rotax has the technical and technological skills to meet our reliability and safety standards.
And last but not least, we have a great feeling with the Italian distributor Luciano Sorlini S.p.A., they give us an excellent support, they are always ready to respond with courtesy, professionalism and friendliness to our requests.
Razzano TancrediCEO, I.C.P. srl
our collAborAtionS with internAtionAl AircrAft MAnufActurerS
oem statementsbenefitS down to eArth
brM Aero/bristell ng 5/rotax 912 iS Sport, 912 ulS, 914 ul, 915 iS
Aerospool / wt9 dynamics / rotax 912 ulS2 Air creation / Skypper / rotax 912 ulS Autogyro / Mto Sport 2017 / rotax 912 ulS, 914 ul, 915 iS
Pipistrel / virus Sw / rotax 912 iS Sport
Progressive Aerodyne / Searey / rotax 915 iS
Phot
o ©
deo
n M
itton
tl ultralights / Sting S4 / rotax 912 iS Sport, 912 ulS, 914 ul van‘s Aircraft / rv 12i / 912 iS Sport, 912 ulS
Magni gyro / M24 orion / rotax 914 ul
i.c.P. / Savannah S / rotax 912 ulS, 912 iS Sport
issoire Aviation / APM 41 Simba / rotax 915 iS, 915 iSc
the Airplane factory / Sling 4 / rotax 914 ul, 915 iS tecnam / P2006t / rotax 912 S
tecnam / P2008Jc / rotax 912 S
our collAborAtionS with internAtionAl AircrAft MAnufActurerS
diamond / dA-20 katana / 912 S, 912 iSc Sport
internAtionAl AwArdS And our coMPAny hiStory
awaRds &ceRtificatesour AwArdS Are cornerStoneS of truSt, our certificAteS Are iMPortAnt MileStoneS in the coMMerciAlizAtion of new AircrAft engineS.
AwArdSBRP-Rotax was awarded 1st place Innovation Award in the category Aero Engines by aerokurier Best Brands 2009
BRP-Rotax was awarded the Dr. August Raspet Memorial Award for Outstanding Contributions to the Advancement of Light Aircraft Design by the Experimental Aircraft Association (EAA) in 2013
Rotax 912 iS was awarded the Most Advanced Powertrain Concept by fliegermagazin 2013
Rotax 912 iS was awarded the Innovation Award in the category Powertrain of the Future by aerokurier 2014
Rotax 912 iS was awarded the Innovation Award in the category Powertrain of the Future by aerokurier 2015
Rotax 915 iS was awarded in the category Best Powertrain Concept by fliegermagazin 2016
Rotax 915 iS was awarded the Innovation Award in the category Powertrain of the Future by aerokurier 2017
certificAteS
doA / PoAImportant milestones for the Rotax aircraft engines business were to meet the Design and Production certification standards of the European Aviati-on Safety Agency (EASA). The Design Organisation Approval (DOA) and Production Organisation Approval (POA) are valid for all types of certified aircraft engines.
eASA tyPe certificAteThe EASA Type Certificate (TC) allows BRP to produce certified engines for the European market and to make changes on certified piston engines. These are important milestones in the commercialization of new aircraft engines. The European Aviation Safety Agency (EASA) promotes the hig-hest standards of safety and environmental protection in civil aviation in Europe and worldwide.
AStMASTM (American Society for Testing and Materials) is an international standard organization that develops and publishes voluntary consensus and technical standards for a wide range of materials, products, systems and services. All Rotax 4-stroke aircraft engines and the 2-stroke Ro-tax 582 UL comply with the ASTM F2339 standard published by ASTM (Standard Practice for Design and Manufacture of Reciprocating Spark Ignition Engines for Light Sport Aircraft).
Dr. Thomas Hametner Maximilian FeischlHead of Design Organisation Accountable Manager
Gunskirchen,
BRP-Rotax GmbH & Co KG I Rotaxstraße 1 I 4623 Gunskirchen I Austria
COMPLIANCE STATEMENT -DECLARATION OF COMPLIANCE
to ASTM
References:
1. ASTM
2. Serial Numbers (since ASTM has been established for ROTAX Aircraft Engines)
912 A ..................................................... from S/N 4410660 on912 F ..................................................... from S/N 4412888 on912 S .................................................... from S/N 4923163 on912 UL ................................................... from S/N 4407160 on912 ULS ................................................ from S/N 5644817 on912 ULSFR ............................................ from S/N 4430116 on912 iS / iS Sport...................................... from S/N 4417078 on912 iSc Sport........................................... from S/N 4417412 on914 F ...................................................... from S/N 4420471 on914 UL .................................................... from S/N 4419024 on915 iS A ................................................. from S/N 9132042 on
Engine Type: Engine s/n:
F2339-06
F2339-06
The product complies with the ASTM standard based on BRP’s quality system for record keeping andinstructions for continued airworthiness.
No features or characteristics are found which would make the engine unsafe provided it is installed, operated andmaintained in accordance with instructions and limitations as defined by BRP-Rotax approved documentation.
BRP-Rotax GmbH & Co KG hereby declares that the aircraft engine or part of thereof as described in the statement ofcompliance confirms to the applicable ASTM standard.F2339-06
F2339-06
22.11.2017
FB 16-012-1/M www.flyrotax.com
as time flies Bythe coMPAny hiStory of brP-rotAxSPotlight on rotAx AircrAft engineS
internAtionAl AwArdS And our coMPAny hiStory
192019471970197519781984198919941996199820032005200520062012201320142017
Founding of Rotax-Werk AG in Dresden, Germany
Relocation to Gunskirchen, Austria
Bombardier aquires Rotax-Werk AG,becoming Bombardier-Rotax GmbH
Certification of the first Rotax aircraft engine (Rotax 642)
Rotax 502 and 505 ultralight engines produced(based on snowmobile engine 503)
Start of development of Rotax 912 engine
Type Certificate for Rotax 912 A
Type Certificate for Rotax 912 F
Type Certificate for Rotax 914 F
Type Certificate for Rotax 912 S
Design Organisation Approval by EASA
Production Organisation Approval by EASA
Rotax 912/914 engine series compliant toLight Sport Aircraft Norm ASTM
Rotax 582 engine compliant to Light Sport Aircraft Norm ASTM
Launch of Rotax 912 iS aircraft engine
BRP Inc. becomes a public company
Launch of Rotax 912 iS Sport aircraft engine
Launch of Rotax 915 iS engine
For almost a century, we have dedicated ourselves to passion and innovation. It’s about what we build and the emotions we provide. Be a part of this unique heritage of ingenuity and excellence, benefit from our experience, start your own adventure.
make youR fRee timeyouR Best time
we Are dedicAted to continuAlly finding new And better wAyS to helP you enJoy your fAvourite PowerSPortS. Our desire to thrill is paired with an emphasis on rider and pilot responsibility, placing per-sonal safety above all else. So that each outing can be the most enjoyable, and memorable experience possible.
www.flyrotax.com1) Based on cruise power setting at 5,000 rpm at 5,000 ft MSL and comparable fuel consumption according to the following sources (Feb. 2012):www.tcmlink.com/EngSpecSheetDocs/O200B.pdf, www.lycoming.com/news-and-events/pdfs/233-engine.pdf, www.jabiru.net.au/images/6-cylinder/3300%20Aero%20Engi-ne%20Flyer.pdf, Costs of fuel: Mogas EUR 1.60 / liter and Avgas EUR 2.408 / liter - air-port Wels Februray 1, 2012
Note: Rotax UL aircraft engines do not comply with federal safety regulations for standard aircraft. This engine is for use in experimental and ultralight uncertified aircraft only and only in circumstances in which an engine failure will not compromise safety. Before opera-ting the engine read operator‘s manual. Information is available from your local authorized Rotax-distributor.
BRP-Rotax GmbH & Co KG reserves the right at any time to discontinue or change specifi-cations, prices, designs, features, models or equipment without incurring obligation. Engi-ne performance may vary depending on, among other things, general conditions, ambient temperature and altitude. These technical data and the information contained therein are property of BRP- Rotax GmbH & Co KG and must not be reproduced, neither entirely nor partially, and passed on to third parties without previous consent in writing by BRP-Rotax GmbH & Co KG. For information only – without commitment to subsequent modifications.
© 2018 BRP-Rotax GmbH & Co KG. All rights reserved. ®, TM and the BRP logo are trademarks of Bombardier Recreational Products Inc. (BRP) or its affiliates. All other tra-demarks are the property of their respective owners.
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