Maintenance Manual XA41/XA42
AMM-XA42-0040-001 C.00
Page
8
Page date:
Chapter 12
25.09.2018
12-10-07 Tire Inflation
The specified tire pressure of the main landing gear wheels is 3.5 (bar) / 50 (psi). The
tailwheel is made of solid rubber. You cannot inflate it.
12-10-08 Overview of Fluids for Replenishing
FUEL
Use AvGas 100 or 100LL only.
The fuel capacities of the main tank and wing tanks are as follows:
Total fuel capacity:
277 (L) / 73.2 (US gal)
• Wing tanks:
2x 105 (L) / 2x 27.7 (US gal)
• Main tank:
67 (L) / 17.7 (US gal)
Usable fuel capacity (Total):
266 (L) / 70.3 (US gal)
Usable fuel capacity (Acro):
57 (L) / 15.1 (US gal)
OIL
The oil quantity of the Lycoming AEIO-580-B1A engine is:
Maximum sump capacity:
15.15 (L) / 16 (USqt)
Minimum sump capacity:
8.52 (L) / 9 (USqt)
The engine oil must have the specifications as given in the table below, refer to the
Lycoming AEIO-580-B1A Operation and Installation Manual:
Table: Recommended oil grades*
Average Ambient
Air
MIL-J-6082B or
SAE J1966 Spec.
Mineral Grades
MIL-L-22851 or
SAE J1899 Spec.
Ashless Dispersant Grades
All Temperatures
---
SAE15W50 or SAE20W50
More than 27 (°C) / 80
(°F)
SAE 60
SAE 60
More than 16 (°C) / 60
(°F)
SAE 50
SAE 40 or SAE 50
-1 (°C) / 30 (°F) thru 32 (°C) /
90 (°F)
SAE 40
SAE 40
-18 (°C) / 0 (°F) thru 21
(°C) / 70 (°F)
SAE 30
SAE 30, SAE 40 or SAE20W40
Less than -12 (°C) / 10
(°F)
SAE 20
SAE 30 or SAE20W30
* Use only mineral oil during the first 50 hours of operation for these engines:
New engines
Newly overhauled engines
Rebuilt engines
Engines with one or more replaced cylinders.
Summary of Contents for XA41
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