Standard Operating Procedures
L410 UVP-E20
Document No.:
SOP-L410-0
Page EE - 52
Rev: 1
Date:JAN 18
Prepared by: LA
Checked by : CLS
ABNORMAL CHECKLISTS
1.
POWERPLANT
1.1
ENGINE SHUTDOWN IN FLIGHT
AB 4
1.2
MISSED APP WITH ONE ENGINE INOPERATIVE
AB 5
1.3
LANDING WITH ONE ENGINE INOPERATIVE
AB 6
1.4
IN FLIGHT ENGINE STARTING
AB 7
1.5
COMPRESSOR SURGING
AB 8
1.6
MINIMUM OIL PRESSURE
AB 9
1.7
METAL CHIPS IN THE OIL
AB 10
1.8
USE OF EMERGENCY FUEL CONTROL CIRCUIT
AB 11
1.9
BETA RANGE AND PROPELLER PITCH LOCK SIGNALLING
AB 12
2.
FUEL
2.1
FAILURE OF AUTOMATIC SWITCHING-ON FUEL TRANSFER
AB 13
2.2
MINIMUM FUEL PRESSURE
AB 14
2.3
FUEL LOW LEVEL
AB 15
2.4
FUEL LEAK
AB 16
3.
ELECTRICAL SYSTEM
3.1 FAILURE OF ONE DC GENERATOR
AB 17
3.2 FAILURE OF ONE AC GENERATOR
AB 18
3.3 FAILURE OF ONE 36 V AC INVERTER
AB 19
3.4 FAILURE OF ONE 115V AC INVERTER
AB 20
3.5 FAILURE OF BATTERY CIRCUIT
AB 21
3.6 BATTERY OVERHEATING
AB 22
4.
HYDRAULIC SYSTEM
4.1 EMERGENCY EXTENTION OF WING FLAPS 18
⁰
AB 23
4.2 WING FLAPS RECTRACT FAILURE
AB 24
4.3 SPONTANEOUS EXTENSION OF ONE ABC TAB DURING T/O
AB 25
4.4 EMERGENCY BRAKING
AB 26
Summary of Contents for L410 UVP-E20
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