Standard Operating Procedures
L410 UVP-E20
Document No.:
SOP-L410-1
Page 2- 3
Rev: 1
Date: JAN 18
Prepared by: LA
Checked by: CLS
MINIMUM TAKE
−
OFF SAFETY SPEED V
2
V
2 18
AND V
R 18
AIRSPEED VALUES VERSUS TAKE-OFF WEIGHT (wing flaps 18°)
Max. take-off
weight
Measurement method
Flaps position
Level of noise
dB(A)
6,600 kg
CS-36, Am.2,
18°
83.1
(ICAO
−
Annex 16,
Chapter 10)
WEIGHTS
Maximum ramp weight is 6,620 kg.
Maximum take-off weight is 6,600 kg.
Maximum landing weight is 6,400 kg.
Maximum zero fuel weight:
−
without wing tip tanks is 6,000 kg
−
with wing tip tanks is 6,060 kg.
Summary of Contents for L410 UVP-E20
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