Maintenance Manual XA41/XA42
AMM-XA42-0040-001 C.00
Page
2
Page date:
Chapter 71
25.09.2018
71-00-00 GENERAL
The XA41 and the XA42 have a Lycoming AEIO-580-B1A aircraft engine.
For information on the engine, refer to the manufacturer’s manual.
71-01-00 MANIFOLD
The engine has six custom manifold pipes. For the installation of the manifolds on the
engine, refer to Figure 71-1.
No. Quantity
Component
P/N
1
1
Intake manifold 1
XA42-7100-111
2
1
Intake manifold 2
XA42-7100-112
3
1
Intake manifold 3
XA42-7100-113
4
1
Intake manifold 4
XA42-7100-114
5
1
Intake manifold 5
XA42-7100-115
6
1
Intake manifold 6
XA42-7100-116
7
6
Manifold flange
74360 Lycoming
8
6
Gasket
71973 Lycoming
9
11
Bolt
LW-25-1.25 Lycoming
10
11
Locking washer
STD-160 Lycoming
11
11
Washer
STD-8 Lycoming
12
6
O-ring
72711 Lycoming
Figure 71-1: Manifold installation
Summary of Contents for XA41
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