Standard Operating Procedures
L410 UVP-E20
Document No.:
SOP-L410-0
Page EE - 53
Rev: 1
Date:JAN 18
Prepared by: LA
Checked by : CLS
5.
LANDING GEAR
5.1 EMERGENCY EXTENSION OF LANDING GEAR
AB 27
5.2 FAILURE OF LANDING GEAR RECTRACTION
AB 28
5.3 DEFLATED TIRE ON WHEEL
AB 29
6.
ANTIICING/DEICING
6.1 ONE SECTION OF PNEUMATIC AIRFRAME DEICING FAILURE
AB 30
6.2 TOTAL FAILURE OF PNEUMATIC AIRFRAME DEICING
AB 31
6.3 FAILURE OF PNEUMATIC DEICING TIME RELAY
AB 32
6.4 ELECTRIC WIND SHIELD HEATING FAILURE
AB 33
6.5 PROPELLER DEICING FAILURE
AB 34
6.6 STATIC HEAD FAILURE
AB 35
6.7 PITOT HEAD FAILURE
AB 36
7.
AUTOPILOT
7.1
AMS FAILURE
AB 37
7.2
ONE ENGINE FAILURE OPERATION
AB 38
Summary of Contents for L410 UVP-E20
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