Rotax 915 i A series Maintenance Manual page 393

REMOVAL
Preparation
Before the wiring harness is removed, the work and
checks described below must be carried out to identi-
fy any further malfunctions in the cylinder head and
rectify them as part of repair work.
General visual inspection.
See Maintenance Manual Line for the en-
gine type 915 i A SeriesChapter 05-00-00
and 12-00-00.
Carry out an engine test run.
See Maintenance Manual Line for the en-
gine type 915 i A Series Chapter 12–20–
00.
• Disconnect the wiring harness from the aircraft
frame.
• Disconnect all detachable connections (all cable
ties, cable holders, clamps etc.).
NOTE
All connectors must be provided with a protec-
tive covering after being removed or detached.
STARTER RELAY — DISCONNECTION
Step Procedure
1 Loosen hex. nut M6 and remove it along
with the washer 6.4. Remove starter ca-
bles from terminals. Pull off faston con-
nector. Press the lock to pull off the faston
connector.
2 Remove the grounding bolt/ screw. Ob-
serve the instructions of the aircraft
manufacturer.
Effectivity: 915 i A Series
Edition 0/Rev. 0
BRP-Rotax
MAINTENANCE MANUAL HEAVY
Figure 17.3
Starter relay
1
3 Washer 6.4
5 Ground
AMBIENT AIR PRESSURE AND
TEMPERATURE SENSOR —
DISCONNECTION
Wiring harness designation:
• AAPTS
Step Procedure
1 Push in the tab on the top of the connec-
tor and at the same time pull the connec-
tor out of the connection socket.
2
Hex. nut M6
4
Faston connector
6
Bolt/ screw
76–50–00
Page 9
August 01 2018