CHECKLIST OF EMERGENCY, ABNORMAL AND NORMAL PROCEDURES
L 410 UVP
- E20
LET Kunovice 686 04 Kynovice
Czech Republic
CHECKLIST OF EMERGENCY, ABNORMAL AND NORMAL PROCEDURES
L 410 UVP
- E20
LET Kunovice 686 04 Kunovice
Czech Republic
L 410 UVP-E20 CHECKLIST OF EMERGENCY PROCEDURES
CHECKLIST OF EMERGENCY PROCEDURES
LIST OF EFFECTIVE PAGES
TABLE OF CONTENTS Using of Check lists of emergency procedures
.......
E-1 Dates of original issue and changed pages are:
Engine fire . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
E-2
Cockpit or cabin fire . . . . . . . . . . . . . . . . . . . . . . .
E-2
ORIGINAL
-0-
Front baggage compartment fire . . . . . . . . . . . . . . . .
E-3
CHANGE 1
(1)
Rear baggage compartment fire . . . . . . . . . . . . . . . .
E-3
Engine failure during take-off (wing flaps 18')
. . . . . . . .
E-3
. . . . . . . . .
E-5
Page
Engine failure during missed approach . . . . . . . . . . . .
E-6
E-l thru E-ll . . . . . . . . . . . . . . . . . . . . . . . . . 1
Both generators inoperative . . . . . . . . . . . . . . . . . . .
E-8
E-1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0
Engine failure during take-off (wing flaps 0')
Should information herein conflict with that in the Approved Flight Manual, the AFM should take precedence.
--
-
Mar 1/96 Sep 25/98
Change No.
E-2thru E-6 . . . . . . . . . . . . . . . . . . . . . . . .
1
E-7 . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
0
E-8
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
-
Sep 25/98 (1)
E-l
E-ll
(1) Sep 25/98
CHECKLIST OF EMERGENCY PROCEDURES
CHECKLIST OF EMERGENCY PROCEDURES
USING OF CHECK LISTS OF EMERGENCY PROCEDURES 1.
2.
The Check Lists of Emergency Procedures contain the abbreviated n a m e s o f n e c e s s a r y p r o c e d u r e s . F o r m o r e d e t a i l s refer t o t h e corresponding part of Flight Manual. The sequence of procedures is mandatory for both crew members. The crew activity in emergency situation is directed by instructions of pilot-in-command. Items marked ( It ) are of t o p importance and, in an emergency case must be executed at the prescribed sequence without waste of time. If there is enough time, the pilot-in-command shall instruct, the copilot to read corresponding Check List t o recheck the procedures executed.
ENGINE FlRE x 1 . Engine on fire
DETERMINE
The following items are valid for engine on fire:
x 2. Fuel fire cock
SHUT
3. Heating lever
SHUT (DOWN)
#
x 4. EXTINGUISH. - PRIM push-button
PUSH
l DLE
5. TCL 6. MANUAL FEATHER push-button
A dotted line (....) means that respective data or condition are t o be reported.
PUSH
7. PCL
I I
FEATHER
8. DC GENERATOR and AC GENERATOR
OFF
If the fire continues: 9. EXTINGUISH.- SEC. push-button
PUSH
10. Fuel stop cock / Emergency throttle lever
I
SHUT
11. ENGINE STARTING,
OFF
IELU, FUEL PUMP circuit breakers 12. Land on the nearest suitable airport
COCKPIT OR CABIN FlRE 1. Oxygen masks (goggles protecting against smoke) 2. FASTEN SEAT BELTS circuit breaker
3. Descent
PUT ON ON
INITIATED AS REQUIRED
4. Source of fire
DETERMINE
5. Portable extinguisher
FIRED (cont.)
--
-
Mar 1/96
E-2
(1) Sep 25/98
L 410 UVP-E20 CHECKLIST OF EMERGENCY PROCEDURES
CHECKLIST OF EMERGENCY PROCEDURES 6. Cockpit windows
I
OPEN
If you have not succeeded in extinguishing the fire: 7. Perform either landing on the nearest aerodrome or forced landing.
#
2. Failed engine
DETERMINE
#
3. Landing gear after take-off
+
4. Feathering propeller of inoperative engine
UP
CHECK
(a) If the automatic feathering cycle has not been accomplished:
FRONT BAGGAGE COMPARTMENT FIRE #
1. BAGGAGE COMPARTMENT EXTINGUISHING handle
3. Descent
IELU LH -r- RH circuit breakers
PULL and HOLD
2. FASTEN SEAT BELTS circuit breaker
INITIATED AS REQUIRED
FEATHER
PCL of the inoperative engine
I
OPEN
min. V2
5. Airspeed
(it is valid only for rear baggage compartment accessible from outside) 1. FIRE EXT. BAG. COMP. push-button
PUSH
2. FASTEN SEAT BELTS circuit breaker
ON
I
OFF
8. Airspeed at height of 6 minutes point for use
of max. contingency power
I
OPEN
4. Cockpit windows
KlAS (155 kmlhr IAS)
7. AUTO BANK CONTROL switch
INITIATED AS REQUIRED
3. Descent
= 84
MAXIMUM CONTINGENCY POWER
6. At height of 35 ft (10.7 m) set
REAR BAGGAGE COMPARTMENT FIRE #
OFF
(b) If the automatic feathering cycle has not been feathered even after above measures had taken then:
ON
4. Cockpit windows
PUSH
MANUAL FEATHER of inoperative engine
97 KlAS (1 80 kmlhr IAS)
9. Flaps at height of 6 minutes point for use
of max. contingency power
ENGINE FAILURE DURING TAKE-OFF (wing flaps 18')
RETRACT 100 KlAS (1 85 km/hr IAS)
10. Airspeed
Below V1 speed:
11. Inoperative engine
Abort the take-off.
FIND OUT PARAMETERS ..........
The following items are valid for inoperative engine: Above #
V I speed:
12. TCL
1 . TCL of both engines
Maximum take-off power
13. Fuel stop cock
(cont.)
Sep 25/98 (1)
IDLE
/ Emergency throttle lever
SHUT
(cont.) E-3
E-4
(1) Sep 25/98
CHECKLIST OF EMERGENCY PROCEDURES
CHECKLIST OF EMERGENCY PROCEDURES 14. DC GENERATOR and AC GENERATOR switches
8. Airspeed at height of 6 minutes point for use
OFF
15. ENGINE STARTING,IELU, FUEL PUMP circuit breakers
of max. contingency power
OFF
100 KlAS (1 85 kmlhr IAS) FIND OUT PARAMETERS..........
9. Inoperative engine
The following items are valid for i~ ?operative engine:
ENGINE FAILURE DURING TAKE-OFF (wing flaps 0')
IDLE
10. TCL Below V1 speed:
11. Fuel stop cock / Emergency throttle lever
Abort the take-off. Above V1 speed: Maximum take-off power
1. TCL of both engines
x 2. Failed engine
12. DC GENERATOR and AC GENERATOR switches
OFF
13. ENGINE STARTING,IELU, FUEL PUMP circuit breakers
OFF
DETERMINE
x
3. Landing gear after take-off
+
4. Feathering propeller of inoperative engine
ENGINE FAILURE DURING MISSED APPROACH
UP CHECK
x 1. TCL of both engines
Maximum contingency power or intermediate contingency power
+
2. Airspeed
rnin. 84 KlAS (155 km/hr IAS)
~c
3. Wing flaps
18'
+
4. Landing gear
UP
(a) If the automatic feathering cycle has not been accomplished MANUAL FEATHER of inoperative engine IELU LH
+ RH circuit breakers
I
PUSH OFF
(b) If the automatic feathering cycle has not been feathered even after above measures had taken then:
rnin. V2
6. At height of 35 ft (10.7 m) set 7. AUTO BANK CONTROL switch
x 5. Feathering propeller of inoperative engine
FEATHER
PCL of the inoperative engine
5. Airspeed
SHUT
=
CHECK
(a) If the automatic feathering cycle has not been accomplished:
97 KlAS (180 krnfhr IAS)
MANUAL FEATHER of inoperative engine
MAXIMUM CONTINGENCY POWER
IELU LH
OFF
+ RH circuit breakers
PUSH OFF
(cont.)
(cont.) Sep 25/98 (1)
E-5
E-6
( 1 ) Sep 25/98
L 410 UVP-E20
L 410 UVP-E20
CHECKLIST OF EMERGENCY PROCEDURES
CHECKLIST OF EMERGENCY PROCEDURES
BOTH GENERATORS INOPERATIVE
(b) If the automatic feathering cycle has not been feathered even after above measures had taken then:
6. Airspeed
min.V;? = 84 KlAS (155 kmlkr IAS)
3. Discharging current of batteries
11. Inoperative engine
OFF FIND OUT AMPERES .......
5. Place for landing
400 ft (122 m) above runway
I
GIVEN IN Fig. 1 see below
4. Time to battery discharge
97 KlAS (1 80 kmlhr IAS)
9. Wing flaps at height of
10. Airspeed
CHECK SWITCHING-ON, SWITCH OFF and then back ON
2. Equipment not marked b y yellow strip
OFF
7. AUTO BANK CONTROL switch
8. Airspeed at height of 400 ft (122 m) above runway:
1 . DC GENERATOR L.H.,R.H.
FEATHER
PCL of the inoperative engine
DETERMINE
RETRACT 100 KlAS (185 kmlhr IAS) FIND OUT PARAMETERS..........
The following items are valid for inoperative engine: 12. TCL 13. Fuel stop cock 1 Emergency throttle lever
IDLE SHUT
14. DC GENERATOR and AC GENERATOR switches
OFF
15. ENGINE STARTING,IELU, FUEL PUMP circuit breakers
OFF
Operation Time [min]
Discharging current [A] Fig. 1
Mar 1/96
E-7
( 1 ) Sep 25/98
L 410 UVP-E20 CHECKLIST OF ABNORMAL PROCEDURES
CHECKLIST OF ABNORMAL PROCEDURES
TABLE OF CONTENTS
. . . . . . . . . . . . . . . . . . . . . . AB-1 Missed approach with one engine inoperative . . . . . . . . . . AB-1 Spontaneuous IELU intervention . . . . . . . . . . . . . . . . . . AB-2 Minimum oil pressure . . . . . . . . . . . . . . . . . . . . . . . . .AB-2 Metal chips in the oil . . . . . . . . . . . . . . . . . . . . . . . . . AB-3 Use of emergency fuel control circuit . . . . . . . . . . . . . . . AB-3
TABLE OF CONTENTS (CONT.)
. . . . . AB-9 Total failure of pneumatic airframe deicing . . . . . . . . . . . AB-9 Failure of one section of pneumatic airframe deicing
Engine shutdown in flight
............ Failure of electric windshield heating . . . . . . . . . . . . . . Propeller deicing failure . . . . . . . . . . . . . . . . . . . . . . Blocking of static pressure head . . . . . . . . . . . . . . . . Blocking of pitot pressure head . . . . . . . . . . . . . . . . . Failure of pneumatic deicing timer relay
1
Failure of automatic switch of fuel transfer from wing tip tanks AB-4
. . . . . . . . . . . . . . . . . . . . . . . . AB-4 Failure of one D.C. Generator . . . . . . . . . . . . . . . . . . . .AB-5 Failure of one A.C. Generator . . . . . . . . . . . . . . . . . . . .AB-5 Failure of one 36V AC Inverter . . . . . . . . . . . . . . . . . . . AB-5
Minimum fuel pressure
Failure of the 115V AC/400 Hz Inverter 1 .
1
AB-10 AB-1 1 AB-11
LIST OF EFFECTIVE PAGES Dates of original issue and changed pages are:
. . . . . . . . . . . . . . . . . . . . . AB-6 . . . . . . . . . . . . . . . . . . . . . . . . . . AB-6
. . . . . . . . . . . . . . AB-7 Wing flaps retracting failure . . . . . . . . . . . . . . . . . . . . . AB-7 Extension of one ABC tab during take-off . . . . . . . . . . . . .AB-7 Emergency extension of landing gear . . . . . . . . . . . . . . . AB-7
AB-10
Should information herein conflict with that in the Approved Flight Manual. the AFM should take precedence.
. . . . . . . . . . . . . AB-6
Failure in the battery circuit Battery overheating
AB-10
Emergency extension of wing flaps 18'
1
ORIGINAL
-0-
Mar 1/96
CHANGE 1
(1)
Sep 25/98
Page
Change No.
....................... AB-1 thru AB-11 . . . . . . . . . . . . . . . . . . . . . . AB-l thru AB-II
1 1
. . . . . . . . . . . . . . . . . . . . . . AB-8 . . . . . . . . . . . . . . . . . . . . . . . . . . AB-9
Deflated tire o n one wheel Emergency braking
(cont.) AB-lI
(1) Sep 25/98
CHECKLIST OF ABNORMAL PROCEDURES
CHECKLIST OF ABNORMAL PROCEDURES Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . 97 KlAS (180 kmlhr IAS)
ENGINE SHUTDOWN I N FLIGHT
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACTED
Operating engine . . . . . . . . . . . . . . . . . . . INTERMEDIATE CONTINGENCY POWER OR AS REQUIRED
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . 100 kt (185 kmlhr) IAS
Failed engine: TCL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE MANUAL FEATHERING push-button (unless automatic feathering has already taken place) . . . . . . . . . . . . . . . . . . . . PUSH Fuel stop cock / Emergency throttle lever . . . . . . . . . . . . . . . . SHUT DC GENERATOR and AC GENERATOR switches . . . . . . . . . . . . . OFF
SPONTANEUOUS IELU INTERVENTION
I
a) At altitudes up t o 2,300 ft (700 m) AGL (level I) TCL . . . . . . match with the TCL position of the correctly working engine IELU circuit breaker (appropriate engine) . . . . . . . . . . . . . . . . . . OFF TCL . . . . . . . . . . . . . . . . . . . . . .
After the gas generator has stopped: FUEL PUMP and WING TIP TANKS circuit breaker . . . . . . . . . . . . OFF STARTING ENGINE, IELU circuit breaker switches . . . . . . . . . . . . OFF P C L . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FEATHER
if necessary adjust engine power
b) At altitudes above 2,300 ft (700 m) AGL (level II) TCL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . I D L E IELU circuit breaker (appropriate engine) . . . . . . . . . . . . . . . . . . OFF AUTO FEATHERING switch . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
MISSED APPROACH WITH ONE ENGINE INOPERATIVE Operating engine . . . . . . . . . . . . . . . . . . . . . . Maximum contingency power or intermediate contingency power Propeller of inoperative engine
. . . . . . . . . . . . . . . . . . . . FEATHER
Climb at airspeed . . . . . . . . . . . . . . . . . . . .
As soon as the propeller starts to unfeather: TCL . . . . . . . . . . move slowly forward t o set the desired engine power Moreover the gas generator speed must be checked against the ambient air temperature - see AFM.
84 KlAS (1 55 kmlhr IAS)
MINIMUM OIL PRESSURE
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18'
(OIL PRESSURE signal light)
Landing gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP Search lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
OFF
At a height of 400 ft (122 m) above the runway:
Oil pressure on the 3-pointer indicator . . . . . . . . . . . . . . . . . CHECK If the oil pressure is not within the operating range . . . . . . . . . . . PERFORM Engine shutdown in flight
(cont.) -
Sep 25/98 (1)
AB-1
AB-2
(1) Sep 25/98
L 410 UVP-E20 CHECKLIST OF ABNORMAL PROCEDURES
CHECKLIST OF ABNORMAL PROCEDURES ISOL
METAL CHIPS I N THE OIL
4 VALVE amber cell on the CWD . . . . . . . . . . . . . CHECK ON
Fuel stop cock/Emergency throttle lever . . . . . . . . . Move slowly forward to the emergency circuit area
(CHIP signal light) IN FLIGHT WITH BOTH ENGINES RUNNING
FAILURE OF AUTOMATIC SWITCHING ON FUEL TRANSFER FROM WlNG -TIP TANKS
Parameters of affected engine . . . . . . . . . . . . . . . . . . . . . . CHECK Continue the flight while paiyng particular attention to the parameters of affected engine.
(ACTUATE TRANSFER signal light)
If the oil temperature is above the maximum limit: Power of affected engine . . . . . . . . . . . . . . . REDUCE AS REQUIRED If the parameters of affected engine continue t o fluctuate:
WING TIP TANK switch for affected side
. . . . . . . . . . . . . . . . . . .
ON Green light FUEL TRANSFER . . . . . . . . . . . . . . . . . . . . . CHECK ON
Carry out procedure Engine shutdown in flight.
MINIMUM FUEL PRESSURE
UNDER UNFAVOURABLE FLIGHT CONDITION SUCH AS ICING CONDITIONS, THUNDERSTORMS, MOUNTAINS, ETC., OR WHEN FLYING ON ONE ENGINE
(FUEL PRESSURE signal light) FUEL PUMP LH (RH) circuit breaker
. . . . . . . . . . . . . . . . CHECK ON
Set the power of affected engine t o a level at which the main parametrs of the engine will remain within the permissible limits.
MINIMUM FUEL signal . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
If it proves impossible t o set the power t o such a level:
Fuel quantity in the group of tanks in use . . . . . . . . . . . . . . . . CHECK
If flying on both engines, stop the malfunctioning engine and land at the nearest airfield. If flying on one engine only, do not stop the engine but carry out a procedure Forced landing.
Crossfeed . . . . . . . . . . . . . . . . . . . . . . . . . . USE IF NECESSARY Fuel pressure on the three-pointer indicator . . . . . . . . . . . . . . CHECK If the engine operates irregularly: TCL of the faulty engine . . . . . . . . . . . . . . . . . . . . . . . . . . .
IDLE
USE PROCEDURE - ENGINE SHUTDOWN IN FLIGHT
USE OF EMERGENCY FUEL CONTROL CIRCUIT TCL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE ISOL. VALVE circuit breaker . . . . . . . . . . . . . . . . . . . . . . . . . . ON (cont.) Sep 25/98 (1)
AB-3
AB-4
(1) Sep 25/98
I
L 410 UVP-E20
L 410 UVP-E20
CHECKLIST OF ABNORMAL PROCEDURES
CHECKLIST OF ABNORMAL PROCEDURES
INVERTER switch . . . . . . . . . . . . . . . OFF and then back ON
FAILURE OF ONE D.C. GENERATOR
If the signal light remains on:
(DC GENERATOR (LH or RH) signal light) Switches on the overhead panel . . . . . . . . CHECK if it is not false alarm
36 V AC INVERTER switch . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
DC GENERATOR switch of failed unit . . . . . . . . . . . . OFF and back ON
FAILURE OF THE 115V AC/400 Hz INVERTER I
If the signal light remains on:
(INVERTER I 115V AC signal light)
Failed DC GENERATOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF VA METER selector switch . . . . . . . SWITCH first t o BATTERY I VA and then t o BATTERY II VA position Right VA meter . . . . . . . . . . . . . . . . . . . . CHECK the charging rate
AC INVERTER 1 115 V switch . . . . . . . . . . . . . . . . . . . . . CHECK ON AC INVERTER I 115 V switch . . . . . . . . . . . . . OFF and then back ON
If the signal light remains on: AC INVERTER 1 115 V switch . . . . . . . . . . . . . . . . . . . . . . . . . OFF
FAILURE OF ONE A.C. GENERATOR (AC GENERATOR (LH or RH) signal lights)
FAILURE OF BATTERY CIRCUIT
Switches o n the overhead panel . . . . . . . . CHECK if it is not false alarm
(BATTERY signal light)
AC GENERATOR switch of failed unit . . . . . . . . OFF and then back ON
Switches on the overhead panel . . . . . . . . CHECK if it is not false alarm
If the signal light remains on:
VA METER selector switch on the inverter selection panel . . . . . . . . . . . . SET successively to BATTERY I VA and II VA
Failed AC GENERATOR
. . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
Charging of both batteries . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
FAILURE OF ONE 36V AC INVERTER
BATTERY switch for the battery which is not charged
. . . . . . . . . . OFF
(INVERTER 36 V AC signal light) BATTERY OVERHEATING
36V AC INVERTER switches . . . . . . . . . . . . . . . . . . . . . CHECK ON
If the amber caution light comes on, continue the flight
(cont.)
If the red warning light comes on: BATTERY l (11) s w i t c h . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF -
Sep 25/98 (1)
AB-5
AB-6
(1) Sep 25/98
L 410 UVP-E20 CHECKLIST OF ABNORMAL PROCEDURES
CHECKLIST OF ABNORMAL PROCEDURES
AR EMERGENCY EXTENSION lever . . . . . . . . . . . . down
EMERGENCY EXTENSION OF WlNG FLAPS 18'
Pump with emergency hydraulic pump until the 3 green lights on landing gear position indicator come on and until resistance on pump handle increases.
WING FLAPS control lever . . . . . . . . . . . . . . . . . . . . POSITION 18' WING FLAPS EMERGENCY EXTENSION lever . . . . . . . . . . . .
DOWN
Pump with emergency hydraulic pump until appropriate indication on wing flaps position indicator comes on.
I
Increase airspeed t o . . . . . . . . . . . . . . . . . 135 KlAS (250 kmlhr IAS) Climb . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . t o safe altitude
WlNG FLAPS RETRACTING FAILURE Real position of the flaps . . . . . . . . . . . . . . . . . . . . . .
If after t h e use of t h e emergency hydraulic p u m p some of the landing gear legs are stuck i n t h e intermediate position:
Wait . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6 0 seconds
. . CHECK
If the flaps have remained in the take-off position (1) ' 8
Sideslip. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PERFORM
Maintain climb with speed of 124 KlAS (230 kmlhr IAS)
If locking of t h e landing gear leg does not take place: Sideslip . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Decide continue flight with airspeed not exceeding 135 KlAS (250 kmlhr IAS).
Repeat 3 times
After repeating t h e sideslip 3 times without result: Airplane swinging with bank of 30' t o 45'. . . . . . . . . . . . . . . . . . . . . . . . . . . . PERFORM
EXTENSION OF ONE ABC TAB DURING TAKE-OFF
Perform this manoeuvre max. 8 times.
Level aircraft by means of the ailerons. AUT. BANK CONTROL switch on the central control panel . . . . . . . . . . . . . . . . . . . . . . . . . OFF
DEFLATED TIRE ON ONE WHEEL
If the ABC tab retracted . . . . . . . . . . . . . . . . CONTINUE THE FLIGHT
DURING TAKE-OFF
If the ABC tab does not retract, trim the aircraft using the aileron trim and do not exceed 111 KlAS (205 kmlhr IAS). Decide whether t o continue the flight or to land on the airfield of departure.
Below or equal VI speed . . . . . . . . . . . . . . . .
INTERRUPT TAKE-OFF
Relieve load on the wheel with faulty tire and use maximum reverse power. Above VI speed . . . . . . . . . . . . . . . . . . . CONTINUE THE TAKE-OFF
EMERGENCY EXTENSION OF LANDING GEAR LANDING GEAR lever . . . . . . . . . . . . . . . . . . . . . . (cont.)
DOWN position
(cont.)
I AB-8
(1) Sep 25/98
f1
I
L 410 UVP-E20
L 410 WP-E20
CHECKLIST OF ABNORMAL PROCEDURES
CHECKLIST OF ABNORMAL PROCEDURES
DO NOT RETRACT LANDING GEAR
URE OF PNEUMATIC DEICING TIMER RELA
Retract flaps at altitude 400 ft (122 m)
TEST A, B, C push-button . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH
Accelerate t o 135 KlAS (250 km/hr IAS) DO NOT EXCEED THIS AIRSPEED DURING FURTHER CLIMB.
If only one of the light does not come on when tested, this means a burnt out bulb filament. Replace the bulb. If failure is not due to a bulb:
DURING LANDING Relieve load on the wheel with faulty tire and use maximum reverse power.
Function selector of pneumatic deicing . . . . . . . . . . . . . . . . MANUAL Selector switch next to lights . . . . . . . . . . . Set to A, then B, then t o C
EMERGENCY BRAKING PARKING BRAKE lever
FAILURE OF ELECTRIC WINDSHIELD HEATING
. . . . . . . . . . . . . . . . . Move to STOP position
If the outer panes of the windshield crack, or if sparking is observed in the heater element or the heater element bus bar:
Pump with emergency hydraulic pump t o build up necessary braking pressure (max. pressure 45 + 3 kp/cm2 [640 43 psi])
+
WINDSHIELD HEATING LH or RH circuit breaker . . . . . . . . . . . . . OFF
FAILURE OF ONE SECTION OF PNEUMATIC AIRFRAME DEICING Check whether engagement of the faulty section is accompanied by a rise of the ITT, either above the permissible maximum ITT or by more than 3 0 ' ~above the previous value. I F YES, switch the function selector to MANUAL and DO NOT USE THE FAULTY SECTION ANY MORE. As soon as possible, LEAVE THE POTENTIAL ICING AREA.
LEAVE THE ICING AREA and avoid any potential icing area.
PROPELLER DEICING FAILURE Simultaneous coming o n of b o t h PROPELLER DEICING cells o n the central warning display means m a i n circuit failure of propeller d e i c i n g cycling switch. PROP DEICING switch on the right instrument panel . . . . . . . . . . . . . . . STDBY I or STDBY II If this does not rectify the trouble:
TOTAL FAILURE OF PNEUMATIC AIRFRAME DEICING
LEAVE THE ICING AREA (cont.)
Main switch of pneumatic deicing system . . . . . . . . . . . . . . . . . OFF Take steps t o LEAVE THE ICING AREA immediately.
Sep 25/98 (1)
AB-9
AB-lo
(1) Sep 25/98
I
L 410 UVP-E20
L 410 UVP-E20
CHECKLIST OF ABNORMAL PROCEDURES
CHECKLIST OF ABNORMAL PROCEDURES
Coming o n of one of the PROPELLER DEICING cells on the CWD o r the alternate flashing of the PROPELLER DEICING cells o n the LH and RH sides of the CWD mens blades heating failure.
I
If engine vibrations become noticeable: Reduce engine power output, or stop the engine.
STATIC PRESSURE HEAD FAILURE STATIC PRESSURE I and II heater buttons
. . . . . . . Check switching-on
The green lights in these push-buttons must stay on.
If the left hand instruments are affected: EMERGENCY STATIC PRESSURE cock
. . . . . . . . . . . . . . . . . OPEN Intentionally left blank
If the right hand instruments are affected: AUTOPILOT (if installed)
. . . . . . . . . . . . . . . . . . . . . DISCONNECT
Continue the flight without any special measures, but disregard readings of the vertical speed indicator, altimeter and air speed indicator on the right instrument panel.
PlTOT PRESSURE HEAD FAILURE If the left hand instruments are affected: PlTOT PRESSURE cock . . . . . . . . . . . . . . . . . . . . . . . .
Position II
If the r i g h t hand instruments are affected: AUTOPILOT (if installed) . . . . . . . . . . . . . . . . . . . . . DISCONNECT
I
Continue the flight without any special measures, but disregard readings of the airspeed indicator on the right instrument panel.
Sep 25/98 (1)
AB-11
AB-12
Mar 1/96
L 410 UVP-E20 CHECKLIST OF NORMAL PROCEDURES
CHECKLIST OF NORMAL PROCEDURES
TABLE OF CONTENTS
TABLE OF CONTENS (CONT.)
External inspection . . . . . . . . . . . . . . . . . . . . . . . . . . N-1
On final approach . . . . . . . . . . . . . . . . . . . . . . . . . . N - 1 5
Internal inspection . . . . . . . . . . . . . . . . . . . . . . . . . . N-5
Missed approach with both engines operating . . . . . . . . . N - 1 6
Pilot's compartment preparation .co-pilot . . . . . . . . . . . . N - 6 Pilot's compartment preparation .pilot in comand . . . . . . . N-7 Preliminary procedures
After landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . N - 1 7 Shutting down the engine on ground . . . . . . . . . . . . . . . N - 1 9
. . . . . . . . . . . . . . . . . . . . . . . N-7
Before engine starting . . . . . . . . . . . . . . . . . . . . . . . . Engine starting
1
N-8
Should information herein conflict with that i n the Approved Flight Manual. the AFM should take precedence.
. . . . . . . . . . . . . . . . . . . . . . . . . . . . N-8
Failed starting attempt . . . . . . . . . . . . . . . . . . . . . . . . N - 9
LIST OF EFFECTIVE PAGES
Before taxiing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . N - 9 Taxiing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . N-11
Dates of original issue and changed pages are: ORIGINAL
Before line up . . . . . . . . . . . . . . . . . . . . . . . . . . . . . N-11 Before take -off . . . . . . . . . . . . . . . . . . . . . . . . . . . . N - 1 2
CHANGE
-0 .
Mar 1 / 9 6 Sep 25/98
After take-off . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . N - 1 2 Climb . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . N - 1 3 Flight in severe turbulence
. . . . . . . . . . . . . . . . . . . . .N - 1 3
Flight under icing conditions . . . . . . . . . . . . . . . . . . . . N - 1 3 Inadvertent flight into freezing rain or freezing drizzle . . . . . N - 1 4 After leaving the posible icing area . . . . . . . . . . . . . . . . . N - 1 4 Before descent
. . . . . . . . . . . . . . . . . . . . . . . . . . . .N - 1 5
Descent . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .N - 1 5
Page
Change No .
N-l thru N-ll . . . . . . . . . . . . . . . . . . . . . . . . 1 N-1 thru N - 2 . . . . . . . . . . . . . . . . . . . . . . . . 1 N-3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0
N - 4 thru N - 1 9 . . . . . . . . . . . . . . . . . . . . . . . 1 N-20 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0
Passing transition level . . . . . . . . . . . . . . . . . . . . . . . . N - 1 5 (cont.) N-ll
(1) Sep 25/98
L 410 UVP-E20 CHECKLIST OF NORMAL PROCEDURES
CHECKLIST OF NORMAL PROCEDURES
RIGHT MAIN LANDING GEAR
EXTERNAL INSPECTION
Tie rods
FRONT FUSELAGE PART INSPECTION
. . . . . . . . . . . . . . . . . . . . . . . . . . . . Check for damage
Nose cover locks . . . . . . . . . . . . . . . . . . . . . . . . . . Check if closed
Tire . . . . . . . . . . . . . Check for damage, deformation or underinflation
. . . . . . . . . . . . . . . . . . Check for damage
Water pump . . . . . . . . . Check if the proper quantity supply is adjusted
Skin, searchlights glazing Rotary ice detector
Water tank . . . . . . . . . . . . . . . . . . . . . . . . Check for water quantity
. . . . . . . . . . . . . . . . . . . . . . Check for damage
Air ventilation intake . . . . . . . . . . . . . . . . . . . . . . No foreign objects
RIGHT POWER UNIT
Holes of static pressure heads covers . . . . . . . . . . . Check if removed
Cover . . . . . . . . . . . . . . . . . . . . . . . . . . Check for proper closing
Holes of static pressure heads, L.H., R.H. . . . . . . . . . . Check for soiling Cockpit window Windshield vipers
Propeller blades cover . . . . . . . . . . . . . . . . . . . . . Check if removed
. . . . . . . . . . . . . . . . . Check for damage and soiling
Propeller blades and blocking
. . . . . . . . . . . . . . . . . . . . . . . Check for damage
Rubber strip on the fuselage . . . . . . . . . . Check for damage or unstick Emergency exit . . . . . . . . . . . . . . . . . . . . . . . . . . . Check if closed
I
I
Check if removed
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check if up
Drainage fuel sample (if performed by pilot see AFM, Section 8) . . . . . . . . . . . . . . . . . . . Check for water in fuel
Servo control tie rods . . . . . . . . . . . . . . . . . . . . . Check for damage Tire . . . . . . . . . . . . . Check for damage, deformation or underinflation
RIGHT WING Wing deicing system . . . . . . . . . . . . . . . . . . . . . Check for damage
RIGHT PlTOT PRESSURE HEAD (RH)
Wingtip (if installed)
. . . . . . . . . . . . . . . . . . Check if removed
(cont.)
Engine inlet cover . . . . . . . . . . . . . . . . . . . . . . .
Separator vane
NOSE LANDING GEAR
Inlet and drainage holes of pitot pressure head . . . . . . . . . . Check for damage or foreign objects
. . . . . . . . . . . . . . . . . . . . . . . . Check for oil leakage
Air inlet . . . . . . . . . . . . . . . . . . . . . . . . . Check for foreign objects
Antenna on the lower part of the fusselage . . . . . . . . Check for damage
Pitot pressure head cover
Propeller hub
. . . . . . . . . . . . . . . Check for damage
I
. . . . . . . . . . . . . . . . . . . . . Check for damage
I
Wingtip tank . . . . . . . . . . . . . . Check for damage, deformation and fuel leakage and filler neck closed Navigation lights
. . . . . . . . . . . . . . . . . . . . . . . Check for damage (cont.)
N-2
(1) Sep 25/98
L 410 UVP-E20 CHECKLIST OF NORMAL PROCEDURES Aileron trailing edge and flaps . . . . . . . . . . . . . . .
CHECKLIST OF NORMAL PROCEDURES Check for damage
Static wicks, aileron, wing tip tank . . . . . . . . . . . . . Check for damage, one static wick may be missing Aileron control tie rods . . . . . . . . . . . . . . . . . . . . Check for damage Flaps controls tie rods
. . . . . . . . . . . . . . . . . . . . Check for damage
Beacon . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check for damage Antenna
. . . . . . . . . . . . . . . . . . . . . . . . . . . . Check for damage
REAR PART OF FUSELAGE Static wick . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check for damage, it may be missing
ABC tabs, spoiler . . . . . . . . . . . . . . . . . . . . . . . . . Check if closed
Lower fin . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check for damage
Control locks (see AFM, Section 8)
. . . . . . . . . . . . . . . . . . . . . Check if removed
LEFT LANDING GEAR
Fuel tank filling neck
. . . . . . . . . . . . . . . . . . . . . . . Check if closed
Tie rods . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check for damage
I
Tire . . . . . . . . . . . . . Check for damage, deformation or underinflation RIGHT SlDE OF FUSELAGE Emergency exit . . . . . . . . . . . . . . . . . . . . . . . . . . .Check if closed Emergency lights
LEFT POWER UNIT
. . . . . . . . . . . . . . . . . . . . . . . Check for damage
Lavatory door (if installed) . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check if secured
LEFT WING
. . . . . . . . . . . . . . . . . Same inspection as right
. . . . . . . . . . . . . . . . . . . . . . Same inspection as right
LEFT SlDE OF FUSELAGE Emergency exit . . . . . . . . . . . . . . . . . . . . . . . . . . Check if closed
TAIL UNlT Tail deicing system
. . . . . . . . . . . . . . . . . . . . . . Check for damage
Emergency lights . . . . . . . . . . . . . . . . . . . . . . . Check for damage
. . . . . . . . . . . . . Check for damage
Static ice detector and lights . . . . . . . . . . . . . . . . Check for damage
Elevator and rudder trailing edges
. . . . . . . . . . Check for damage orpunstick
Elevator and rudder control tie rods . . . . . . . . . . . . Check for damage
Rubber strip on the fuselage
Control locks (see AFM, Section 8)
LEFT PlTOT PRESSURE HEAD . . . . . . . . . . Same inspection as right
. . . . . . . . . . . . . . . . . . . . . Check if removed
Static wicks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check for damage, one may be missing on the elevator (conf.)
Mar 1/96
N-3
FRONT PART OF THE FUSELAGE Beggage compartment doors (after loading the baggage) . N-4
. . . . . . . . . . . . . . . . . . Check if closed (1) Sep 25/98
L 410 UVP-E20 CHECKLIST OF NORMAL PROCEDURES
CHECKLIST OF NORMAL PROCEDURES
INTERNAL INSPECTION
PILOT'S COMPARTMENT PREPARATION
- CO-PILOT
Pressure in oxygen bottle and mask with microphone . . . . . . CHECKED
1. Check ceiling panels, carpets, upholstery passenger's seats and faste-
ning items for intactness and cleannes, check the first-aid box.Check the location of life jackets (if installed). The number of life jackets shall correspond with number of persons on the aircraft. 2. Check load distribution and fastening, fastening of the protective net
Parking brake . . . . . . . . . . . . . . . . . . . . . . . . STOP, pressure ...... Landing gear . . . . . . . . . . . . . . . . . . . . . . . . DOWN, Lever Locked TCL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
in the rear baggage compartment accessible from inside.
PCL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FEATHER
3. Check the pressure in oxygen bottles (for passengers) and the total of masks.
Fuel fire cocks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN
4. Check state of the passenger cabin lights.
Fuel stop cock I Emergency throttle levers . . . . . . . . . . . . . . . CLOSE
5. DOOR
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CLOSE
Circuit breakers under the cover (except LOGO - if installed and WATER INJECTION - if you don't decide t o use water injection ) . . . . . . . . . . . . . . . . . ON
6. Check if the movable pins are in position LOCKED. 7. Remove the lock pins of all emergency exits and insert them into bag on the back side of the pilot's seat.
BATTERY I, 11
8. Check by moving if the emergency door's control handle is locked in the
position CLOSED and check the emergency door sealing.
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
INVERTER 36 V I . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON INTERCOM I, II; VHF I . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
I
9. Set the pilot seats t o the required position.
ON
Battery, External power supply voltage . . . . . . . . . . . . . 20 V minimum Selector of converters . . . . . . . . . . . . . . . . . . . . . . . . AUTOMATIC Pneumatic de-icing system . . . . . . . . . . . . . . . . . . . . . . . . . . OFF Propeller de-icing . . . . . . . . . . . . . . . . . . . . . . . . . . . . ZERO (off) Windshield heating . . . . . . . . . . . . . . . . . . . . . . . . . . .ZERO (off) Fuel quantity . . . . . . . . . . . . . . . . L.H. ....... kg (Ib), R.H. ....... k g (Ib) Flight recorder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED VHF I (left) . . . . . . . . . . . . . . . . . . . . . CHECKED, frequency .......... (cont.)
Sep 25/98 (1)
N-5
N-6
(1) Sep 25/98
I
L 410 UVP-E20 CHECKLIST OF NORMAL PROCEDURES
CHECKLIST OF NORMAL PROCEDURES Clock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET UP, time .........
RECORDER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON REC FAlL light on the flight recorder control box comes on.
Report . . . . . . . . . . . . . . . . . . . . . . . PREPARATION COMPLETED
FIRE EXTIN. push-button cover on central control panel . . . CHECK SEALING
PILOT'S COMPARTMENT PREPARATION COMMAND
ENGINE STARTING LH, RH . . . . . . . . . . . . . . . . . . . . . . . . . . ON
- PILOT I N
Pressure in oxygen bottle and mask with microphone . . . . . . . . CHECK
FUEL PUMP LH, RH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Free motion of controls . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
FUEL PRESSURE signal cells . . . . . . . . . . . . . . . . . . . . . . . . . OFF
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED
Area around propellers and removing of the blocking . . . . . . . . . . . . . . . . FREE I CHECKED
Heating
Signalling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
ON
Decrease hydraulic fluid pressure in main hydraulic circuit.
Fire signalling system . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
ANTICOLL. BEACON, VOICE RECORDER (if installed) . . . . . . . . . .
ON
External inspection . . . . . . . . . . . . . . . . . . . . . . . . . PERFORMED
Voice recorder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
Internal inspection . . . . . . . . . . . . . . . . . . . . . . . . .
Engine starting
PERFORMED
Fuel stop cock / Emergency throttle lever
. Centre of gravity position . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . %
ENGINE STARTING push-button . . . . . . . . . . . . . . . . . . . . . . PUSH
VHFl
I
. . . . . . . . . . . . . . . OPEN
STOP WATCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . START During the starting cycle, check the engine parameters (ITT, nG, oil pressure, pressure rise in hydraulic system, ENGINE STARTING cell goes off after 20 seconds)
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
When the engines have stabilized at their idling speed:
PRU on the Flight recorder . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
DC GENERATOR and AC GENERATOR switches . . . . . . . . . . . . . ON
(cont.)
(cont.)
Sep 25/98 (1)
N-7
I
I
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . READY
Passengers . . . . . . . . . . . . . . . . . . . . . . . . . ............, ON BOARD
BEFORE ENGINE STARTING
I
ENGINE STARTING
CHECKED, ON BOARD
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET
(
PRU on the Flight recorder . . . . . . . . . . . . . . . . . . . . . . . . . . .ON REC FAlL light on the flight recorder control box must go off. I
PRELIMINARY PROCEDURES
Operational, technical and personal documents . . . . . . . . . . . . . . .
I1
N-8
(1) Sep 25/98
I
L 410 UVP-E20
L 410 UVP-E20
CHECKLIST OF NORMAL PROCEDURES
CHECKLIST OF NORMAL PROCEDURES
Ground power source . . . . . . . . . . . . . . . . . . . . . . . DISCONNECT
SPEC. EQUIPMENT. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
EXT POWER SUPPLY cell . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
AUTOPILOT, ELECTRIC TRIM (if installed) . . . . . . . . . . . . . . . . .
Engine parametres
. . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
Radar screen (if installed) . . . . . . . . . . . . . . . . . . . . . . . . . . STBY GPS (if installed)
In case of starting engines without ground power supply
NAV 11 NAV 2 change-over switch (if installed)
DC GENERATOR of running engine . . . . . . . . . . . . . . . . . . . . . . ON
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .65% (max. 70%)
Hydraulic pressure
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
Graphic unit (if installed) . . . . . . . . . . . . . . . . . . . . . . . . . . . STBY
Before starting up the second engine:
n~
ON
. . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
. . . CHECK position NAV
1
Brakes . . . . . . . . . . . . . . . . . DEPRESS and check accum. pressure
I
R.H. horizon and turn indicator . . . . . . . . . . . . . . . . . . . . . . . . ON L.H. horizon and turn indicator . . . . . . . . . . . . . . . . . . . . . . . . ON SPOILERS switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
FAILED STARTING ATTEMPT Fuel stop cock 1 Emergency throttle lever . . . . . . . . . . . . . . . . SHUT ENGINE STARTING circuit breaker . . . . . . . . . . . . . . . . . . . . . OFF
AUT. BANK CONTROL switch . . . . . . . . . . . . . . . . . . . . . . . . . ON AUTO FEATHER switch Nosewheel steering
. . . . . . . . . . . . . . . . . . . . . . . . . . . . 014 '
. . . . . . . . . . . . . . . . . . . . . . . . . . . MANUAL
Brake antiskid . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
BEFORE TAXIING POWERSUPPLY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON RADIONAVIGATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON PROP. FEATHERING / AUT. BANK CONTROL . . . . . . . . . . . . . . . . ON VHF I, II, HF (if installed) . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON FASTEN SEAT BELTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON ROTARY ICE DETECTOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON PA, RADAR (if installed) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON (cont.)
Central warning display . . . . . . . . .
ON
FLAPS 18', MANUAL STEERING and AUT.BANK CONTROL stay on
Gyromagnetic compasses . . . . . . . . . . . . . . . . . . . . . . . CHECKED GPS (if installed)
...........................
SET MODE
DME change-over switch. . . . . . . . . . . . . . . . . . . . . . . . . NAV I (11) Radio-altimeter
. . . . . . .
CHECKED, SET TO DH (MDH) ............. ft ( 4
Electric system . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK Electric trim function . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK Elevator trim . . . . . . . . . . . . . . . . . set according to centre of gravity (cont.)
Sep 25/98 (1)
I
N-9
N-10
(1) Sep 25/98
I I
L 410 UVP-E20
L 410 UVP-E20
CHECKLIST OF NORMAL PROCEDURES
CHECKLIST OF NORMAL PROCEDURES
Aileron trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . Neutral position
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18' or 0"
Rudder trim . . . . . . . . . . . . . . . . . . . . . . . One division t o the right
I SSR II swich (if installed) . . . . . . . . . . . . . . . . . . . . . . . . . . SET I
Navigation systems . . . . . . . . . . . . . . CHECKED, frequencies ...........
Transponder . . . . . . . . . . . . . . . . . . . . . . . . . . Code .........., STBY
Transponders . . . . . . . . . . . . . . . . . . . . . .
Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FREE
CHECKED, standby I, II
Autopilot (if installed) . . . . . . . . . . . . . . . . . . . . . . . TEST, CHECK PCL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
BEFORE TAKE-OFF
FINE PITCH
Reverse thrust latch . . . . . . . . . . . . . . . . . . . . . . . . . . . Removed
Nosewheel steering change-over switch . . . . . . . . . . . . . . . . PEDAL
For taxiing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Ready
Instruments
SEARCHLIGHTS TAXIING I, II . . . . . . . . . . . . . . . . . . . . . . . . . ON
Gyromagnetic compasses . . . . . . . . . . . . . . . CHECK runway heading
Parking brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASED
Graphic unit (if installed) . . . . . . . . . . . . . . . . . . . . .
I
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OK
AS REQUIRED
I
After clearance for take-off received
TAXIING
Transponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
ON
Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
Pitot heating . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
ON
Propeller hydraulic system . . . . . . . . . . . . . . . . . . . . . . . . . .VENT
Stop watch
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STARTED
Turn and bank indicator . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
AFTER TAKE-OFF Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET1
BEFORE LINE UP Cockpit windows . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SHUT Horizons . . . . . . . . . . . . . . . . . . . . . . . . . . UNCAGE AND CHECK Engine parameters
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OK
1
Landing gear lever lock . . . . . . . . . . . . . . . . . . . . . . . . . REMOVE Landing gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
UP oo
Windshield heating, PROP. DEICING . . . . . . . . . . . . . . . ON, STAGE I
TCL . . . . . . . . . . . . . . . . . . . . . . . . . Maximum continuous power
Heating . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Taxi lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
(cont.)
CLOSED
SPOILERS, ABC system, AUTO FEATHER . . . . . . . . . . . . . . . . . OFF N-12
(1) Sep 25/98
1
L 410 UVP-E20
L 410 UVP-E20
CHECKLIST OF NORMAL PROCEDURES
CHECKLIST OF NORMAL PROCEDURES
CLIMB TCL . . . . . . . . . . . . . . . . . . . . . . . . . . Maximum continuous power
ICE DETECTOR LIGHTING push-button . . . . . . . . . . PUSH (as required)
PCL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1,900 RPM
Function selector of pneumatic deicing . . . . . . . . . . . . . . . AUTOMAT
Two engine climbing airspeed . . . . . . . .
Cycle rate selector switch . . . . . . . . . . . . . . . . . . . . FAST or SLOW
At trans. altitude ALTIMETERS
min. 135 KlAS (250 kmlhr IAS)
. . . . . . . . . . . . . . . .
set STANDARD
INADVERTENT FLIGHT INTO FREEZING RAIN
Recommended vertical speed (with passengers) . . . . . . . . . . . . . . . . . . . . . max. 590 fpm (3 mls)
Autopilot (if installed) . . . . . . . . . . . . . . . . . . . . . . . . DISCONNECT
FASTEN SAFETY BELTS circuit breaker . . . . . . . . . . . . AS REQUIRED
Airspeed . . . . . . . . . . . . . . . . . . . . . max. 150 KlAS (278 km/h lASj
FLIGHT IN SEVERE TURBULENCE Reduce airspeed t o
change t o leave these Altitude or heading . . . . . . . . . . . . . . . . meteorological conditions
. . . . . . . . . . . . . . max. 143 KlAS (265 kmlhr IAS)
I
FASTEN SEAT BELTS circuit breaker . . . . . . . . . . . . . . . SWITCH ON
FLIGHT UNDER ICING CONDITIONS
WINDSHIELD HEATING change-over switch . . . . . . . . . . . . . . . . . .
ROTARY ICE DETECTOR . . . . . . . . . . . . . . . . . . . . . . . CHECK ON
I
WINDSHIELD HEATING change-over switch . . . . . . . . . . . . . . SET t o II PROP DEICING change-over switch. .
AFTER LEAVING THE POSSIBLE ICING AREA
MAIN I or II (depending on rate of ice accretion)
SEPARATOR VANE LH and RH switches on the overhead panel . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED ONIOFF switch of pneumatic deicing system . . . . . . . . . AS REQUIRED
I
PROP DEICING change-over switch . . . . . . . . . . . . . . . . . . ICE DETECTORISTATIC circuit breaker . . . . . . . . . . . . . . . . ON for period necessary for clearing away of all ice, then OFF SEPARATOR VANE LH and RH switches
I
on the overhead panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF Switch of pneumatic deicing system . . . . . . . . . . . . . . . . . . . . . OFF
(cont.)
Sep 25/98 (1)
N-13
I
(1) Sep 25/98
1
L 410 UVP-E20
L 410 UVP-E20
CHECKLIST OF NORMAL PROCEDURES
CHECKLIST OF NORMAL PROCEDURES Radar (if installed)
BEFORE DESCENT
Airspeed . . . . . . . . . . . . . . . . . . . . .
Approach information . . . . . . . . . . . . . . . . . . . . . . . . . RECIEVED FASTEN SEAT BELTS circuit breaker . . . . . . . . . . . . . . . . . . . . . ON
min. 89 KlAS (165 kmlhr IAS)
Heating . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SHUT
I
DESCENT
I
100 ft (30 rn) above DH (MDA):
PCL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Fine pitch Autopilot (if installed) . . . . . . . . . . . . . . . OFF or GO- AROUND at DH
Engines . . . . . . . . . . . . . . from max. cont. power to flight idle power Recommended vertical airspeed (with passengers) . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STBY
590 ftlmin (3 mls).
At decision height (if decide t o land):
I
PASSING TRANSITION LEVEL
Airspeed . . . . . . . . . . . . . . . . . . . . . . . .
84 KlAS (155 kmlhr IAS)
MISSED APPROACH WITH BOTH ENGINES OPERATING
Altimeters . . . . . . . . . . . . . . . . . . . Set to QNH ......compare altitude Brakes . . . . . . . . . . . . . . . . . . Brake accumulator pressure checked AUTO FEATHER, AUTO BANK CONTROL, SPOILERS switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON Radio altimeter . . . . . . . . . . . . . . . . . . . . . . . . . .
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 42'
SET DH.........ft
(a) ABOVE DH (MDH) TCL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Max. take-off power Climbing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Initiate Landing gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
UP
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . 84 KlAS (155 kmlhr IAS) Landing lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
O N FINAL APPROACH Airspeed . . . . . . . . . . . . . . . . . . . . . max. 135 KlAS (250 kmlhr IAS)
After reaching a height of 400 ft (122 m)
Landing gear . . . . . . . . . . . . . . . . . . . . . . . . DOWN and LOCKED
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . 94 KlAS (175 kmlhr IAS)
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
18'
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
PEDAL CONTROL cell . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
ONI
LANDING LIGHTS
Airspeed
oo
. . . . . . . . . . . . . . . . . . . . . . . . 108 KlAS (200 kmlhr IAS) (cont.)
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON (cont.)
Sep 25/98 (1)
N-15
N-16
(1) Sep 25/98
I
L 410 UVP-E20 CHECKLIST OF NORMAL PROCEDURES
CHECKLIST OF NORMAL PROCEDURES
Deicing (windshield, propeller)
(b) BELOW DH (MDH)
TCL
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Max. take-off power
GPS (if installed)
. . . . . . . . . . . . . . . . . . 84 KlAS (155 kmlhr IAS) Landing gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
....................................... Landing lights. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Spec. equipment
18'
. . . . . . . . . . . . . . . . . . . . . . . . . 94 KlAS (175 kmlhr IAS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . o O(
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . 108 KlAS (200 kmlhr IAS) After reaching a height of 1500 ft (457 m):
.........................
135 KlAS (250 kmlh IAS)
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF PROP. FEATHERINGIAUT. BANK CONTROL circuit breaker . . . . . . . OFF ADF, NAV, DME . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF HF (if installed)
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF INVERTERS except No 1 36 V . . . . . . . . . . . . . . . . . . . . . . . . . OFF Stop watch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STOP
STBY GYRO HORIZON
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON Transponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STBY. Graphic unit (if installed) . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF Nose wheel steering . . . . . . . . . . . . . . . . . . . . . . . . . . . MANUAL Taxi lights
........................................
oo
SPOILERS, AUT. BANK CONTROL, AUTOFEATHER switches . . . . . .
OFF
Heating of air pressure heads
OFF
..................... ........................
. . . . . . . . . . . . . . . . . . . . . . . OFF PA, RADAR (if installed) . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF SEPARATOR VANE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF Ice detectors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
GYROCOMPASS
AFTER LANDING
Flaps
. . . . . . . . . . . . . . . . . . . . . . . . . . . OFF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
Autopilot, elect. trim (if installed)
OFF
Airspeed
Airspeed
1
Radar screen (if installed)
After reaching a height of 400 ft (122 m)
Flaps
. . . . . . . . . . . . . . . OFF and LOCK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
Horizons, Turn and bank indicator
Transmition t o climb at an airspeed . . . .
Flaps
. . . . . . . . . . . . . . . . . . . . . . . . OFF
After stopping airplane:
. . . . . . . . . . . . . . . . . . . . OFF . . . . . . . . . . . . . . . . . . . . . . pressure 25 + 5 kp/cm2
FASTEN SEAT BELTS circuit breaker
1
Parking brake
1
(cont.)
Sep 25/98 (1)
N-17
N-18
(1)
S e p 25/98
I
L 410 UVP-E20
L 410 UVP-E20
CHECKLIST OF NORMAL PROCEDURES
CHECKLIST OF NORMAL PROCEDURES
SHUTTING DOWN THE ENGINE ON GROUND TCL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE P C L . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FEATHER Taxi lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
OFF
VHF, INTERCOM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
OFF
After 3 minutes, needed for the engine cooling: AC, DC GENERATORS
. . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
Fuel stop cock / Emergency throttle lever . . . . . . . . . . . . . . . . SHUT STOP WATCH . . . . . . . . . . . . . . . . . . .
START (to check run out gas generator speed)
After gas generator has stopped: ANTICOL. BEACON, VOICE RECORDER (if installed)
. . . . . . . . . .
IELU, ENGINE STARTING . . . . . . . . . . . . . . . . . . . . . . . . . . .
OFF
Intentionally left blank
1
OFF
FUELPUMP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF INVERTER 36V I . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . All circuit breaker under cover
OFF
. . . . . . . . . . . . . . . . . . . . . . . OFF
BATTERY I,II . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF For long term parking: PCL . . . . . . . . . . . . . . . . . . . . . . . Move out of "Feathered" position
Sep 25/98 (1)
N-19
N-20
Mar 1/96