Rotax 914 series User Manual

Effectivity: 914 Serie BRP-Powertrain page 9-3
OM Edition 2 / Rev. 0 April 01/2010
d05038.fm
9.1) Form
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 914 series Specifications

General

Bore	79.5 mm
Stroke	61 mm
Compression Ratio	9.0:1
Cooling System	Liquid-cooled cylinder heads, air-cooled cylinders
Redline	5800 rpm
Engine Type	4-cylinder, 4-stroke
Fuel Type	Avgas 100LL
Oil System	Dry sump
Fuel System	fuel injection
TBO (Time Between Overhauls)	2000 hours
Displacement	1.211 liters (1211 cc)
Power Output	84.6 kW (115 hp) at 5, 800 rpm