Rotax 503 UL DCDI - Page 4

d04085
page 1 - 4
Jan. 01/2007
Effectivity: 447 SCDI, 503 DCDI,
582 DCDI
OM Edition 1 / Rev. 0
BRP-Rotax
9.3.4) Gearbox lubrication ............................................................. 9 - 6
9.4) Electric system ................................................................................ 9 - 7
9.5) Propeller gearbox ............................................................................ 9 - 8
9.5.1) Type "B" gearbox ................................................................ 9 - 8
9.5.2) Type "C" gearbox ................................................................ 9 - 8
9.5.3) Type "E" gearbox ................................................................ 9 - 8
10) Operating parameters ................................................................. 10 - 1
10.1) Performance graphs for stand. conditions (ISA) ...................... 10 - 3
10.2) Operating media ............................................................................ 10 - 7
10.2.1) Coolant ............................................................................ 10 - 7
10.2.2) Fuel .................................................................................. 10 - 8
10.2.3) Lubricants ...................................................................... 10 - 10
10.3) Standard operation ..................................................................... 10 - 11
10.3.1) Before engine start ........................................................ 10 - 11
10.3.2) Daily checks .................................................................. 10 - 12
10.3.3) Pre-flight checks ............................................................ 10 - 13
10.3.4) Engine start .................................................................... 10 - 14
10.3.5) Prior to take-off .............................................................. 10 - 15
10.3.6) Checking of ignition unit (not possible for 447 UL SCDI) ...... 10 - 15
10.3.7) Operation in flight ............................................................. 10 - 15
10.3.8) Special operating conditions: ........................................... 10 - 16
10.4) Abnormal operation ..................................................................... 10 - 18
10.4.1) Engine stop - Start during flight ....................................... 10 - 18
10.4.2) Exceeding of max. admissible engine speed ................... 10 - 18
10.4.3) Exceeding of max. admissible cyl. head temperature ...... 10 - 18
10.4.4) Exceeding of max. admissible exhaust gas temperature . 10 - 18
10.4.5) Too low fuel pressure ....................................................... 10 - 18
11) Checks ........................................................................................ 11 - 1
11.1) Engine preservation ...................................................................... 11 - 1
11.1.1) After each flight .................................................................. 11 - 1
11.1.2) At engine stoppage of 1 to 4 weeks ................................... 11 - 1
11.1.3) At out of service periods or storage of engine for longer
than 4 weeks up to 1 year ................................................. 11 - 2
12) Trouble shooting ....................................................................... 12 - 1
13) ROTAX
®
authorized Distributors .............................................. 13 - 1