Rotax 912-UL User Manual

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page 12 - 5
Jan. 01/2007
Effectivity: 912 Serie
OM Edition 1 / Rev. 0
BRP-Rotax
05478
CUSTOMER
SERVICE INFORMATION REPORT
OPER. Control No. ATA Code
A/C Reg. No.
Enter pertinent data
MANUFACTURER MODEL/SERIES SERIAL NUMBER
AIRCRAFT POWERPLANT PROPELLER 5. SPECIFIC PART
(of component)
CAUSING TROUBLE
Part Name MFG. Model or Part No. Serial No. Part/Defect Location
4. 3. 2. 6. ENGINE COMPONENT
(Assembly that includes part)
Engine
/
Comp. Name Manufacturer Model or Part No. Serial Number
Engine TSN Engine TSO Engine Condition 7. Date Sub.
8. Comments
(Describe the malfunction or defect and the circumstances under which
it occurred. State probable cause and recommendations to prevent recurrence.)
Optional Information: Check a box below, if this report is related to an aircraft
Accident; Date Incident; Date
TELEPHONE NUMBER: ( ) ———
REP. STA
SUBMITTED BY:
1.
Muster
0
ROTAX
A-Z L1.V R
DISTRICT
OFFICE
OPER
MECH AIR TAXI MFG ACG COMMUTER OTHER
OPERATOR
DESIGNATOR
AIRCRAFT ENGINES

Rotax 912-UL Specifications

General

Displacement	1211 cc
Bore x Stroke	79.5 mm x 61 mm
Compression Ratio	9.0:1
TBO (Time Between Overhaul)	2000 hours
Engine Type	4-cylinder, 4-stroke
Power Output	80 hp
Cooling System	Liquid/air-cooled
Fuel Type	Avgas 100LL or unleaded automotive gasoline
Oil Capacity	3 liters
Fuel System	2 carburetors
Oil System	Dry sump forced lubrication with separate oil tank
Reduction Gear Ratio	2.43:1
Max Continuous Power	75 hp (56 kW)