Standard Operating Procedures
L410 UVP-E20
Document No.:
SOP-L410-1
Page 2- 4
Rev: 1
Date: JAN 18
Prepared by: LA
Checked by: CLS
CAUTION
THE ACTUAL MAXIMUM PERMISSIBLE TAKE-OFF WEIGHT IS
THE LOWEST ONE OF THE WEIGHTS DETERMINED BY FLIGHT
MANUAL, PARA: TAKE-OFF WAT CURVES, TAKE-OFF FIELD
LENGTHS AND NET TAKE-OFF FLIGHT PATH DATA, EN-ROUTE
DATA. WITH THE LIMITATION GIVEN IN SECTION 2 IN MIND.
NOTE
In exceptional cases it is permitted to land with
weight of 6,600 kg, or with fuel in the wing tip tanks.
Each this case must be recorded in the Airplane
Log Book
Summary of Contents for L410 UVP-E20
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