check list

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 41 0 UVP-E20 CHECKLIST OF EMERGENCY PROCEDURES

TABLE OF CONTENTS

Using of Check lists of emergency procedures . . . . . . . E-1

Engine fire . . . . . . . . . . . . . . . . . . . . . . . . . . . . . E-2

Cockpit or cabin fire . . . . . . . . . . . . . . . . . . . . . . . E-2

. . . . . . . . . . . . . . . . Front baggage compartment fire E-3

. . . . . . . . . . . . . . . . Rear baggage compartment fire E-3

Engine failure during take-off (wing flaps 18') . . . . . . . . E-3

Engine failure during take-off (wing flaps 0') . . . . . . . . . E-5

Engine failure during missed approach . . . . . . . . . . . . E-6

Both generators inoperative . . . . . . . . . . . . . . . . . . . E-8

Should information herein conflict with that in the Approved Flight Manual, the AFM should take precedence.

-- - -

Sep 25/98 (1) E-l

CHECKLIST OF EMERGENCY PROCEDURES

LIST OF EFFECTIVE PAGES

Dates of original issue and changed pages are:

ORIGINAL - 0 - Mar 1/96

CHANGE 1 (1) Sep 25/98

Page Change No.

. . . . . . . . . . . . . . . . . . . . . . . . . E-l thru E-ll 1

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . E-1 0

. . . . . . . . . . . . . . . . . . . . . . . . E-2thru E-6 1

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . E-7 0

E-8 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

E-ll (1) Sep 25/98


USING OF CHECK LISTS OF EMERGENCY PROCEDURES

1. The Check Lists of Emergency Procedures contain the abbreviated names o f necessary p rocedures .For more deta i ls refer t o the corresponding part of Flight Manual. The sequence of procedures is mandatory for both crew members.

2. The crew activity in emergency situation is directed by instructions of pilot-in-command.

Items marked ( It ) are of top 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 to recheck the procedures executed.

A dotted line (....) means that respective data or condition are to be reported.


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 I 5. TCL l DLE

6. MANUAL FEATHER push-button PUSH I 7. PCL FEATHER

8. DC GENERATOR and AC GENERATOR OFF

If the fire continues: 9. EXTINGUISH.- SEC. push-button

10. Fuel stop cock / Emergency throttle lever

11. ENGINE STARTING, IELU, FUEL PUMP circuit breakers

PUSH I SHUT

OFF

12. Land on the nearest suitable airport

COCKPIT OR CABIN FlRE

1. Oxygen masks (goggles protecting against smoke) PUT ON

2. FASTEN SEAT BELTS circuit breaker ON

3. Descent INITIATED AS REQUIRED

4. Source of fire DETERMINE

5. Portable extinguisher FIRED

(cont.) -- -

Mar 1/96 E-2 (1) Sep 25/98

L 41 0 UVP-E20 CHECKLIST OF EMERGENCY PROCEDURES

6. Cockpit windows OPEN

If you have not succeeded in extinguishing the fire: I

7. Perform either landing on the nearest aerodrome or forced landing.

FRONT BAGGAGE COMPARTMENT FIRE

# 1. BAGGAGE COMPARTMENT EXTINGUISHING handle PULL and HOLD

2. FASTEN SEAT BELTS circuit breaker ON


4. Cockpit windows OPEN I REAR BAGGAGE COMPARTMENT FIRE

(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


4. Cockpit windows OPEN I ENGINE FAILURE DURING TAKE-OFF (wing flaps 18')

Below V1 speed:

Abort the take-off.

Above VI speed:

# 1 . TCL of both engines Maximum take-off power

(cont.)

Sep 25/98 (1) E-3


# 2. Failed engine DETERMINE

# 3. Landing gear after take-off UP

+ 4. Feathering propeller of inoperative engine CHECK

(a) If the automatic feathering cycle has not been accomplished:

MANUAL FEATHER of inoperative engine PUSH

IELU LH -r- RH circuit breakers OFF

(b) If the automatic feathering cycle has not been feathered even after above measures had taken then:

PCL of the inoperative engine FEATHER

5. Airspeed min. V2 = 84 KlAS (155 kmlhr IAS)

6. At height of 35 ft (10.7 m) set MAXIMUM CONTINGENCY POWER

7. AUTO BANK CONTROL switch OFF

8. Airspeed at height of 6 minutes point for use of max. contingency power

9. Flaps at height of 6 minutes point for use of max. contingency power

97 KlAS (1 80 kmlhr IAS)

RETRACT

10. Airspeed 100 KlAS (1 85 km/hr IAS)

11. Inoperative engine FIND OUT PARAMETERS ..........

The following items are valid for inoperative engine:

12. TCL IDLE

13. Fuel stop cock / Emergency throttle lever SHUT

(cont.)

E-4 (1) Sep 25/98


14. DC GENERATOR and AC GENERATOR switches

15. ENGINE STARTING,IELU, FUEL PUMP circuit breakers

OFF

OFF

ENGINE FAILURE DURING TAKE-OFF (wing flaps 0')

Below V1 speed:

Abort the take-off.

Above V1 speed:

1. TCL of both engines Maximum take-off power

x 2. Failed engine DETERMINE

x 3. Landing gear after take-off UP

+ 4. Feathering propeller of inoperative engine CHECK

(a) If the automatic feathering cycle has not been accomplished

MANUAL FEATHER of inoperative engine PUSH I IELU LH + RH circuit breakers OFF



5. Airspeed rnin. V2 = 97 KlAS (180 krnfhr IAS)

6. At height of 35 ft (10.7 m) set MAXIMUM CONTINGENCY POWER


(cont.)


8. Airspeed at height of 6 minutes point for use of max. contingency power 100 KlAS (1 85 kmlhr IAS)

9. Inoperative engine FIND OUT PARAMETERS ...... ... .

?operative engine:

IDLE

lever SHUT

The following items are valid for i~

10. TCL

11. Fuel stop cock / Emergency throttle



OFF

OFF

ENGINE FAILURE DURING MISSED APPROACH

x 1. TCL of - both engines Maximum contingency power or intermediate contingency

power

+ 2. Airspeed rnin. 84 KlAS (1 55 km/hr IAS)

~c 3. Wing flaps 18'

+ 4. Landing gear UP

x 5. Feathering propeller of inoperative engine CHECK

(a) If the automatic feathering cycle has not been accomplished:

MANUAL FEATHER of inoperative engine PUSH

IELU LH + RH circuit breakers OFF

(cont.)

Sep 25/98 (1) E-5 E-6 ( 1 ) Sep 25/98

L 410 UVP-E20 CHECKLIST OF EMERGENCY PROCEDURES



6. Airspeed min.V;? = 84 KlAS (1 55 kmlkr IAS)


8. Airspeed at height of 400 ft (122 m) above runway: 97 KlAS (1 80 kmlhr IAS)

9. Wing flaps at height of 400 ft (1 22 m) above runway RETRACT

10. Airspeed 100 KlAS (1 85 kmlhr IAS)

11. Inoperative engine FIND OUT PARAMETERS ..........

The fol lowing items are valid for inoperative engine:

12. TCL

13. Fuel stop cock 1 Emergency throttle lever



IDLE

SHUT

OFF

OFF

Mar 1/96 E-7

L 410 UVP-E20 CHECKLIST OF EMERGENCY PROCEDURES

BOTH GENERATORS INOPERATIVE

1 . DC GENERATOR L.H.,R.H. CHECK SWITCHING-ON, I SWITCH OFF and then back ON

2. Equipment not marked by yellow strip OFF

3. Discharging current of batteries FIND OUT AMPERES .......

4. Time to battery discharge GIVEN IN Fig. 1 see below

5. Place for landing DETERMINE

Operation Time [min]

Discharging current [A]

Fig. 1

( 1 ) Sep 25/98

CHECKLIST OF ABNORMAL PROCEDURES

TABLE OF CONTENTS

. . . . . . . . . . . . . . . . . . . . . . Engine shutdown in flight 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 1

. . . . . . . . . . . . . . . . . . . . . . . . .

. . . . . . . . . . . . . . . Use of emergency fuel control circuit AB-3

Failure of automatic switch of fuel transfer from wing tip tanks AB-4

. . . . . . . . . . . . . . . . . . . . . . . . Minimum fuel pressure AB-4

Failure of one D.C. Generator AB-5 1

. . . . . . . . . . . . . . . . . . . .

. . . . . . . . . . . . . . . . . . . . Failure of one A.C. Generator AB-5

. . . . . . . . . . . . . . . . . . . Failure of one 36V AC Inverter AB-5

. . . . . . . . . . . . . . Failure of the 11 5V AC/400 Hz Inverter 1 AB-6

. . . . . . . . . . . . . . . . . . . . . Failure in the battery circuit AB-6

. . . . . . . . . . . . . . . . . . . . . . . . . . Battery overheating AB-6

. . . . . . . . . . . . . . Emergency extension of wing flaps 18' AB-7

. . . . . . . . . . . . . . . . . . . . . Wing flaps retracting failure AB-7

Extension of one ABC tab during take-off AB-7 1

. . . . . . . . . . . . . . . . . . . . . . . . . . . . Emergency extension of landing gear AB-7

. . . . . . . . . . . . . . . . . . . . . . Deflated tire on one wheel AB-8

. . . . . . . . . . . . . . . . . . . . . . . . . . Emergency braking AB-9

(cont.)

L 410 UVP-E20 CHECKLIST OF ABNORMAL PROCEDURES

TABLE OF CONTENTS (CONT.)

Failure of one section of pneumatic airframe deicing . . . . . AB-9

. . . . . . . . . . . Total failure of pneumatic airframe deicing AB-9

. . . . . . . . . . . . Failure of pneumatic deicing timer relay AB-10

. . . . . . . . . . . . . . Failure of electric windshield heating AB-10

. . . . . . . . . . . . . . . . . . . . . . Propeller deicing failure AB-10

. . . . . . . . . . . . . . . . Blocking of static pressure head AB-1 1

. . . . . . . . . . . . . . . . . Blocking of pitot pressure head AB-11

Should information herein conflict with that in the Approved Flight Manual. the AFM should take precedence .



ORIGINAL -0- Mar 1/96

CHANGE 1 (1) Sep 25/98

Page Change No . AB-l thru AB-II . . . . . . . . . . . . . . . . . . . . . . . 1

AB-1 thru AB-11 . . . . . . . . . . . . . . . . . . . . . . 1

AB-lI (1) Sep 25/98


ENGINE SHUTDOWN IN FLIGHT

. . . . . . . . . . . . . . . . . . . Operating engine INTERMEDIATE CONTINGENCY POWER OR AS REQUIRED

Failed engine:

TCL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE

MANUAL FEATHERING push-button (unless automatic feathering has already taken place) . . . . . . . . . . . . . . . . . . . . PUSH I Fuel stop cock / Emergency throttle lever . . . . . . . . . . . . . . . . SHUT

DC GENERATOR and AC GENERATOR switches . . . . . . . . . . . . . OFF

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

MISSED APPROACH WITH ONE ENGINE INOPERATIVE

. . . . . . . . . . . . . . . . . . . . . . Operating engine Maximum contingency power or intermediate contingency power

. . . . . . . . . . . . . . . . . . . . Propeller of inoperative engine FEATHER

. . . . . . . . . . . . . . . . . . . . Climb at airspeed 84 KlAS (1 55 kmlhr IAS)

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Flaps 18'

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Landing gear UP

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Search lights OFF

At a height of 400 ft (122 m) above the runway:

(cont.)

-

Sep 25/98 (1) AB-1


. . . . . . . . . . . . . . . . . . . . . . . . . Airspeed 97 KlAS (1 80 kmlhr IAS)

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Flaps RETRACTED

. . . . . . . . . . . . . . . . . . . . . . . . . . Airspeed 100 kt (1 85 kmlhr) IAS

SPONTANEUOUS IELU INTERVENTION

a) At altitudes up to 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 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

As soon as the propeller starts to unfeather:

TCL . . . . . . . . . . move slowly forward to set the desired engine power

Moreover the gas generator speed must be checked against the ambient air temperature - see AFM.

MINIMUM OIL PRESSURE

(OIL PRESSURE signal light)

. . . . . . . . . . . . . . . . . Oil pressure on the 3-pointer indicator CHECK

If the oil pressure is not within the operating range . . . . . . . . . . . PERFORM Engine shutdown in flight

AB-2 (1) Sep 25/98


METAL CHIPS IN THE OIL

(CHIP signal light)

IN FLIGHT WITH BOTH ENGINES RUNNING

. . . . . . . . . . . . . . . . . . . . . . Parameters of affected engine CHECK

Continue the flight while paiyng particular attention to the parameters of affected engine.

If the oil temperature is above the maximum limit:

. . . . . . . . . . . . . . . Power of affected engine REDUCE AS REQUIRED

If the parameters of affected engine continue to fluctuate:

Carry out procedure Engine shutdown in flight.

UNDER UNFAVOURABLE FLIGHT CONDITION SUCH AS ICING CONDI- TIONS, THUNDERSTORMS, MOUNTAINS, ETC., OR WHEN FLYING ON ONE ENGINE

Set the power of affected engine to a level at which the main parametrs of the engine will remain within the permissible limits.

If i t proves impossible to set the power to such a level:

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.

USE OF EMERGENCY FUEL CONTROL CIRCUIT

TCL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE

. . . . . . . . . . . . . . . . . . . . . . . . . . ISOL. VALVE circuit breaker ON

(cont.)

Sep 25/98 (1) AB-3

ISOL


4 VALVE amber cell on the CWD . . . . . . . . . . . . . CHECK ON

. . . . . . . . . Fuel stop cock/Emergency throttle lever Move slowly forward to the emergency circuit area

FAILURE OF AUTOMATIC SWITCHING ON FUEL TRANSFER FROM WlNG -TIP TANKS

(ACTUATE TRANSFER signal light)

. . . . . . . . . . . . . . . . . . . WING TIP TANK switch for affected side ON I

. . . . . . . . . . . . . . . . . . . . . Green light FUEL TRANSFER CHECK ON

MINIMUM FUEL PRESSURE

(FUEL PRESSURE signal light)

FUEL PUMP LH (RH) circuit breaker . . . . . . . . . . . . . . . . CHECK ON

. . . . . . . . . . . . . . . . . . . . . . . . . . . MINIMUM FUEL signal CHECK

. . . . . . . . . . . . . . . . Fuel quantity in the group of tanks in use CHECK

. . . . . . . . . . . . . . . . . . . . . . . . . . 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

AB-4 (1) Sep 25/98


FAILURE OF ONE D.C. GENERATOR

(DC GENERATOR (LH or RH) signal light)

. . . . . . . . Switches on the overhead panel CHECK if it is not false alarm

DC GENERATOR switch of failed unit . . . . . . . . . . . . OFF and back ON

If the signal light remains on:

. . . . . . . . . . . . . . . . . . . . . . . . . . . . Failed DC GENERATOR OFF

. . . . . . . VA METER selector switch SWITCH first to BATTERY I VA and then to BATTERY II VA position

. . . . . . . . . . . . . . . . . . . . Right VA meter CHECK the charging rate

FAILURE OF ONE A.C. GENERATOR

(AC GENERATOR (LH or RH) signal lights)

. . . . . . . . Switches on the overhead panel CHECK if it is not false alarm

AC GENERATOR switch of failed unit . . . . . . . . OFF and then back ON


. . . . . . . . . . . . . . . . . . . . . . . . . . . Failed AC GENERATOR OFF

FAILURE OF ONE 36V AC INVERTER

(INVERTER 36 V AC signal light)

. . . . . . . . . . . . . . . . . . . . . 36V AC INVERTER switches CHECK ON

(cont.)

--

Sep 25/98 (1) AB-5


INVERTER switch . . . . . . . . . . . . . . . OFF and then back ON


. . . . . . . . . . . . . . . . . . . . . . . . . . . 36 V AC INVERTER switch OFF

FAILURE OF THE 115V AC/400 Hz INVERTER I

(INVERTER I 115V AC signal light)

. . . . . . . . . . . . . . . . . . . . . AC INVERTER 1 115 V switch CHECK ON

. . . . . . . . . . . . . AC INVERTER I 115 V switch OFF and then back ON


. . . . . . . . . . . . . . . . . . . . . . . . . AC INVERTER 1 115 V switch OFF

FAILURE OF BATTERY CIRCUIT

(BATTERY signal light)

Switches on the overhead panel . . . . . . . . CHECK if it is not false alarm

VA METER selector switch . . . . . . . . . . . . on the inverter selection panel SET successively to

BATTERY I VA and II VA

. . . . . . . . . . . . . . . . . . . . . . . . . Charging of both batteries CHECK

BATTERY switch for the battery which is not charged . . . . . . . . . . OFF

BATTERY OVERHEATING

If the amber caution light comes on, continue the flight

If the red warning light comes on:

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . BATTERY l (11) switch. OFF

AB-6 (1) Sep 25/98


EMERGENCY EXTENSION OF WlNG FLAPS 18'

. . . . . . . . . . . . . . . . . . . . WING FLAPS control lever POSITION 18'

WING FLAPS EMERGENCY EXTENSION lever . . . . . . . . . . . . DOWN

Pump with emergency hydraulic pump until appropriate indication on

I wing flaps position indicator comes on.

WlNG FLAPS RETRACTING FAILURE

Real position of the flaps . . . . . . . . . . . . . . . . . . . . . .

If the flaps have remained in the take-off position (1 8')

Maintain climb with speed of 124 KlAS (230 kmlhr IAS)

Decide continue flight with airspeed not exceeding 135 KlAS (250 kmlhr IAS).

. . CHECK

EXTENSION OF ONE ABC TAB DURING TAKE-OFF

Level aircraft by means of the ailerons.

AUT. BANK CONTROL switch . . . . . . . . . . . . . . . . . . . . . . . . . on the central control panel OFF

. . . . . . . . . . . . . . . . If the ABC tab retracted CONTINUE THE FLIGHT

If the ABC tab does not retract, trim the aircraft using the aileron trim and do not exceed 11 1 KlAS (205 kmlhr IAS). Decide whether to continue the flight or to land on the airfield of departure.

EMERGENCY EXTENSION OF LANDING GEAR

. . . . . . . . . . . . . . . . . . . . . . LANDING GEAR lever DOWN position I (cont.)


AR EMERGENCY EXTENSION lever . . . . . . . . . . . . down f 1

Pump with emergency hydraulic pump until the 3 green lights on landing gear position indicator come on and until resistance on pump handle increases. I If after the use of the emergency hydraulic pump some of the landing gear legs are stuck i n the intermediate position:

. . . . . . . . . . . . . . . . . Increase airspeed to 135 KlAS (250 kmlhr IAS)

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Climb to safe altitude

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Wait . 60 seconds

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Sideslip. PERFORM

If locking of the landing gear leg does not take place:

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Sideslip Repeat 3 times

After repeating the sideslip 3 times without result:

Airplane swinging with . . . . . . . . . . . . . . . . . . . . . . . . . . . bank of 30' to 45'. PERFORM

Perform this manoeuvre max. 8 times.

DEFLATED TIRE ON ONE WHEEL

DURING TAKE-OFF

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

(cont.)

AB-8 (1) Sep 25/98


DO NOT RETRACT LANDING GEAR

Retract flaps at altitude 400 ft (1 22 m)

Accelerate to 135 KlAS (250 km/hr IAS) DO NOT EXCEED THIS AIRSPEED DURING FURTHER CLIMB.

DURING LANDING

Relieve load on the wheel with faulty tire and use maximum reverse power.

EMERGENCY BRAKING

. . . . . . . . . . . . . . . . . PARKING BRAKE lever Move to STOP position

Pump with emergency hydraulic pump to build up necessary braking pressure (max. pressure 45 + 3 kp/cm2 [640 + 43 psi])

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.

IF 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.

TOTAL FAILURE OF PNEUMATIC AIRFRAME DEICING

Main switch of pneumatic deicing system . . . . . . . . . . . . . . . . . OFF

Take steps to LEAVE THE ICING AREA immediately.

L 410 WP-E20 CHECKLIST OF ABNORMAL PROCEDURES

URE OF PNEUMATIC DEICING TIMER RELA

TEST A, B, C push-button . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH

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:

Function selector of pneumatic deicing . . . . . . . . . . . . . . . . MANUAL

Selector switch next to lights . . . . . . . . . . . Set to A, then B, then to C

FAILURE OF ELECTRIC WINDSHIELD HEATING

If the outer panes of the windshield crack, or if sparking is observed in the heater element or the heater element bus bar:

WINDSHIELD HEATING LH or RH circuit breaker . . . . . . . . . . . . . OFF

LEAVE THE ICING AREA and avoid any potential icing area.

PROPELLER DEICING FAILURE

Simultaneous coming on of both PROPELLER DEICING cells on the central warning display means main circuit failure of propeller deicing cycling switch.

I PROP DEICING switch on the right instrument panel . . . . . . . . . . . . . . . STDBY I or STDBY II

If this does not rectify the trouble:

LEAVE THE ICING AREA

(cont.)

Sep 25/98 (1) AB-9 AB- lo (1) Sep 25/98


Coming on of one of the PROPELLER DEICING cells on the CWD or the alternate flashing of the PROPELLER DEICING cells on 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

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

I f the r ight 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.

L 41 0 UVP-E20 CHECKLIST OF ABNORMAL PROCEDURES

Intentionally left blank

Sep 25/98 (1) AB-11 AB-12 Mar 1/96

CHECKLIST OF NORMAL PROCEDURES

TABLE OF CONTENTS

External inspection . . . . . . . . . . . . . . . . . . . . . . . . . . N-1

Internal inspection . . . . . . . . . . . . . . . . . . . . . . . . . . N-5

Pilot's compartment preparation . co-pilot . . . . . . . . . . . . N - 6

Pilot's compartment preparation . pilot in comand . . . . . . . N-7 1

Preliminary procedures . . . . . . . . . . . . . . . . . . . . . . . N - 7

Before engine starting . . . . . . . . . . . . . . . . . . . . . . . . N-8

Engine starting . . . . . . . . . . . . . . . . . . . . . . . . . . . . N - 8

Failed starting attempt . . . . . . . . . . . . . . . . . . . . . . . . N - 9

Before taxiing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . N - 9

Taxiing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . N-11

Before line up . . . . . . . . . . . . . . . . . . . . . . . . . . . . . N-11

Before take -off . . . . . . . . . . . . . . . . . . . . . . . . . . . . N - 1 2

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

. . . . . . . . . . . . . . . . . . . . . . . . Passing transition level N - 1 5

(cont.)

L 410 UVP-E20 CHECKLIST OF NORMAL PROCEDURES

TABLE OF CONTENS (CONT.)

On final approach . . . . . . . . . . . . . . . . . . . . . . . . . . N - 1 5

. . . . . . . . . Missed approach with both engines operating N - 1 6

After landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . N - 1 7

Shutting down the engine on ground . . . . . . . . . . . . . . . N - 1 9

Should information herein conflict with that in the Approved Flight Manual. the AFM should take precedence .



-0 . Mar 1 / 9 6 ORIGINAL

CHANGE Sep 25/98

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 - 2 0 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0

N-ll (1) Sep 25/98


EXTERNAL INSPECTION

FRONT FUSELAGE PART INSPECTION

. . . . . . . . . . . . . . . . . . . . . . . . . . Nose cover locks Check if closed

. . . . . . . . . . . . . . . . . . Skin, searchlights glazing Check for damage

. . . . . . . . . . . . . . . . . . . . . . Rotary ice detector Check for damage

. . . . . . . . . . . . . . . . . . . . . . Air ventilation intake No foreign objects

. . . . . . . . . . . Holes of static pressure heads covers Check if removed

. . . . . . . . . . Holes of static pressure heads, L.H., R.H. Check for soiling

. . . . . . . . . . . . . . . . . Cockpit window Check for damage and soiling

. . . . . . . . . . . . . . . . . . . . . . . Windshield vipers Check for damage

. . . . . . . . . . Rubber strip on the fuselage Check for damage or unstick

Emergency exit Check if closed I

. . . . . . . . . . . . . . . . . . . . . . . . . . .

. . . . . . . . Antenna on the lower part of the fusselage Check for damage

NOSE LANDING GEAR

. . . . . . . . . . . . . . . . . . . . . Servo control tie rods Check for damage

. . . . . . . . . . . . . Tire Check for damage, deformation or underinflation

RIGHT PlTOT PRESSURE HEAD (RH)

. . . . . . . . . . . . . . . . . . Pitot pressure head cover Check if removed

Inlet and drainage holes of . . . . . . . . . . pitot pressure head Check for damage or foreign objects

(cont.) I


RIGHT MAIN LANDING GEAR

. . . . . . . . . . . . . . . . . . . . . . . . . . . . Tie rods Check for damage


. . . . . . . . . Water pump Check if the proper quantity supply is adjusted

. . . . . . . . . . . . . . . . . . . . . . . . Water tank Check for water quantity

RIGHT POWER UNIT

. . . . . . . . . . . . . . . . . . . . . . . . . . Cover Check for proper closing

. . . . . . . . . . . . . . . . . . . . . Propeller blades cover Check if removed

. . . . . . . . . . . . . . . Propeller blades and blocking Check for damage

Propeller hub Check for oil leakage I

. . . . . . . . . . . . . . . . . . . . . . . .

. . . . . . . . . . . . . . . . . . . . . . . Engine inlet cover Check if removed

. . . . . . . . . . . . . . . . . . . . . . . . . Air inlet Check for foreign objects

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . Separator vane Check if up

Drainage fuel sample (if performed by pilot

. . . . . . . . . . . . . . . . . . . see AFM, Section 8) Check for water in fuel

RIGHT WING

. . . . . . . . . . . . . . . . . . . . . Wing deicing system Check for damage

Wingtip (if installed) 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


. . . . . . . . . . . . . . . Aileron trailing edge and flaps 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

. . . . . . . . . . . . . . . . . . . . . . . . . ABC tabs, spoiler Check if closed

Control locks . . . . . . . . . . . . . . . . . . . . . (see AFM, Section 8) Check if removed

. . . . . . . . . . . . . . . . . . . . . . . Fuel tank filling neck Check if closed

RIGHT SlDE OF FUSELAGE

. . . . . . . . . . . . . . . . . . . . . . . . . . . Emergency exit Check if closed

. . . . . . . . . . . . . . . . . . . . . . . Emergency lights Check for damage

Lavatory door . . . . . . . . . . . . . . . . . . . . . . . . . . . . (if installed) Check if secured

TAIL UNlT

. . . . . . . . . . . . . . . . . . . . . . Tail deicing system Check for damage

. . . . . . . . . . . . . Elevator and rudder trailing edges Check for damage

. . . . . . . . . . . . Elevator and rudder control tie rods Check for damage

Control locks . . . . . . . . . . . . . . . . . . . . . (see AFM, Section 8) Check if removed

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Static wicks Check for damage, one may be missing on the elevator

(conf.)

Mar 1/96 N-3


. . . . . . . . . . . . . . . . . . . . . . . . . . . . . Beacon Check for damage

. . . . . . . . . . . . . . . . . . . . . . . . . . . . Antenna Check for damage

REAR PART OF FUSELAGE

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Static wick Check for damage, it may be missing I

. . . . . . . . . . . . . . . . . . . . . . . . . . . . Lower fin Check for damage

LEFT LANDING GEAR

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . Tie rods Check for damage


. . . . . . . . . . . . . . . . . LEFT POWER UNIT Same inspection as right

. . . . . . . . . . . . . . . . . . . . . . LEFT WING Same inspection as right

LEFT SlDE OF FUSELAGE

. . . . . . . . . . . . . . . . . . . . . . . . . . Emergency exit Check if closed

. . . . . . . . . . . . . . . . . . . . . . . Emergency lights Check for damage

. . . . . . . . . . . . . . . . Static ice detector and lights Check for damage

. . . . . . . . . . Rubber strip on the fuselage Check for damage orpunstick

. . . . . . . . . . LEFT PlTOT PRESSURE HEAD Same inspection as right

FRONT PART OF THE FUSELAGE

Beggage compartment doors . . . . . . . . . . . . . . . . . . . (after loading the baggage) Check if closed

N-4 (1) Sep 25/98


INTERNAL INSPECTION

1. Check ceiling panels, carpets, upholstery passenger's seats and fastening 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 in the rear baggage compartment accessible from inside.

3. Check the pressure in oxygen bottles (for passengers) and the total of masks.

4. Check state of the passenger cabin lights.

5. DOOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSE

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.

8. Check by moving if the emergency door's control handle is locked in the position CLOSED and check the emergency door sealing.

9. Set the pilot seats to the required position. I

Sep 25/98 (1) N-5


PILOT'S COMPARTMENT PREPARATION - CO-PILOT

Pressure in oxygen bottle and mask with microphone CHECKED I

. . . . . .

. . . . . . . . . . . . . . . . . . . . . . . . Parking brake STOP, pressure ......

. . . . . . . . . . . . . . . . . . . . . . . . Landing gear DOWN, Lever Locked

TCL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PCL FEATHER

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Fuel fire cocks OPEN

Fuel stop cock I Emergency throttle levers . . . . . . . . . . . . . . . CLOSE

Circuit breakers under the cover (except LOGO - if installed and WATER INJECTION

. . . . . . . . . . . . . . . . . - if you don't decide to use water injection ) ON

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BATTERY I, 1 1 ON

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INVERTER 36 V I ON

INTERCOM I, II; VHF I . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 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.)

N-6 (1) Sep 25/98


. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Clock SET UP, time .........

. . . . . . . . . . . . . . . . . . . . . . . Report PREPARATION COMPLETED

PILOT'S COMPARTMENT PREPARATION - PILOT IN COMMAND

Pressure in oxygen bottle and mask with microphone . . . . . . . . CHECK

. . . . . . . . . . . . . . . . . . . . . . . . . . Free motion of controls CHECK

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Heating CLOSED

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Signalling CHECK

. . . . . . . . . . . . . . . . . . . . . . . . . . . Fire signalling system CHECK

PRELIMINARY PROCEDURES

. . . . . . . . . . . . . . . . . . . . . . . . . External inspection PERFORMED

. . . . . . . . . . . . . . . . . . . . . . . . . Internal inspection PERFORMED

Operational, technical . . . . . . . . . . . . . . . and personal documents CHECKED, ON BOARD

. . . . . . . . . . . . . . . . . . . . . . . . . Passengers ............, ON BOARD

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Centre of gravity position %

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Altimeters SET I BEFORE ENGINE STARTING

VHFl . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

. . . . . . . . . . . . . . . . . . . . . . . . . . PRU on the Flight recorder OFF

(cont.)

Sep 25/98 (1) N-7


RECORDER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON REC FAlL light on the flight recorder control box comes on. I

. . . FIRE EXTIN. push-button cover on central control panel CHECK SEALING 1 . . . . . . . . . . . . . . . . . . . . . . . . . . ENGINE STARTING LH, RH ON

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FUEL PUMP LH, RH ON

. . . . . . . . . . . . . . . . . . . . . . . . . FUEL PRESSURE signal cells OFF ( Area around propellers and removing of the blocking . . . . . . . . . . . . . . . . FREE I CHECKED I Decrease hydraulic fluid pressure in main hydraulic circuit.

. . . . . . . . . . . . . . . . . . . . . . . . . . . PRU on the Flight recorder ON REC FAlL light on the flight recorder control box must go off. I ANTICOLL. BEACON, VOICE RECORDER (if installed) . . . . . . . . . .

ON I . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Voice recorder CHECK I

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Engine starting READY

ENGINE STARTING

Fuel stop cock / Emergency throttle lever . . . . . . . . . . . . . . . OPEN

ENGINE STARTING push-button . . . . . . . . . . . . . . . . . . . . . . PUSH I . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 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)

When the engines have stabilized at their idling speed:

DC GENERATOR and AC GENERATOR switches . . . . . . . . . . . . . ON

(cont.)

N-8 (1) Sep 25/98

L 41 0 UVP-E20 CHECKLIST OF NORMAL PROCEDURES

. . . . . . . . . . . . . . . . . . . . . . . Ground power source DISCONNECT

. . . . . . . . . . . . . . . . . . . . . . . . . . . EXT POWER SUPPLY cell OFF

. . . . . . . . . . . . . . . . . . . . . . . . . . . . Engine parametres CHECK

In case of starting engines without ground power supply

Before starting up the second engine:

. . . . . . . . . . . . . . . . . . . . . . DC GENERATOR of running engine ON

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . n~ .65% (max. 70%)

. . . . . . . . . . . . . . . . . . . . . . . . . . . . Hydraulic pressure CHECK I FAILED STARTING ATTEMPT

. . . . . . . . . . . . . . . . Fuel stop cock 1 Emergency throttle lever SHUT

. . . . . . . . . . . . . . . . . . . . . ENGINE STARTING circuit breaker OFF

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.)


. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SPEC. EQUIPMENT. ON

AUTOPILOT, ELECTRIC TRIM (if installed) . . . . . . . . . . . . . . . . . ON

. . . . . . . . . . . . . . . . . . . . . . . . . . Radar screen (if installed) STBY

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . GPS (if installed) ON

. . . . . . . . . . . . . . . . . . . . . . . . . . . Graphic unit (if installed) STBY

NAV 11 NAV 2 change-over switch (if installed) . . . 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

. . . . . . . . . . . . . . . . . . . . . . . . . AUT. BANK CONTROL switch ON

. . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO FEATHER switch 01'4

. . . . . . . . . . . . . . . . . . . . . . . . . . . Nosewheel steering MANUAL

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Brake antiskid ON

Central warning display . . . . . . . . . FLAPS 18', MANUAL STEERING and AUT.BANK CONTROL stay on

Gyromagnetic compasses CHECKED I

. . . . . . . . . . . . . . . . . . . . . . .

. . . . . . . . . . . . . . . . . . . . . . . . . . . GPS (if installed) SET MODE

. . . . . . . . . . . . . . . . . . . . . . . . DME change-over switch. NAV I (11) I 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) N-9 N-10 (1) Sep 25/98


. . . . . . . . . . . . . . . . . . . . . . . . . . . . Aileron trim Neutral position

. . . . . . . . . . . . . . . . . . . . . . . Rudder trim One division to the right

. . . . . . . . . . . . . . Navigation systems CHECKED, frequencies ...........

. . . . . . . . . . . . . . . . . . . . . . Transponders CHECKED, standby I, II

. . . . . . . . . . . . . . . . . . . . . . . Autopilot (if installed) TEST, CHECK

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PCL FINE PITCH

. . . . . . . . . . . . . . . . . . . . . . . . . . . Reverse thrust latch Removed

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . For taxiing Ready

. . . . . . . . . . . . . . . . . . . . . . . . . SEARCHLIGHTS TAXIING I, II ON

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Parking brake RELEASED

TAXIING

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Brakes CHECK

. . . . . . . . . . . . . . . . . . . . . . . . . . Propeller hydraulic system VENT

. . . . . . . . . . . . . . . . . . . . . . . . . . Turn and bank indicator CHECK

BEFORE LINE UP

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Cockpit windows SHUT 1 . . . . . . . . . . . . . . . . . . . . . . . . . . Horizons UNCAGE AND CHECK

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Engine parameters OK

. . . . . . . . . . . . . . . Windshield heating, PROP. DEICING ON, STAGE I

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Heating CLOSED

(cont.)


. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Flaps 18' or 0"

. . . . . . . . . . . . . . . . . . . . . . . . . . I SSR II swich (if installed) SET I

. . . . . . . . . . . . . . . . . . . . . . . . . . Transponder Code .........., STBY

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Controls FREE

BEFORE TAKE-OFF

. . . . . . . . . . . . . . . . Nosewheel steering change-over switch PEDAL I . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Instruments OK

. . . . . . . . . . . . . . . Gyromagnetic compasses CHECK runway heading

Graphic unit (if installed) AS REQUIRED I

. . . . . . . . . . . . . . . . . . . . .

After clearance for take-off received

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Transponder ON

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pitot heating ON

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Stop watch STARTED

AFTER TAKE-OFF

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Brakes SET1

. . . . . . . . . . . . . . . . . . . . . . . . . Landing gear lever lock REMOVE

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Landing gear UP

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . oo 1

. . . . . . . . . . . . . . . . . . . . . . . . . TCL Maximum continuous power

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Taxi lights OFF

. . . . . . . . . . . . . . . . . SPOILERS, ABC system, AUTO FEATHER OFF

N-12 (1) Sep 25/98


CLIMB

. . . . . . . . . . . . . . . . . . . . . . . . . . TCL Maximum continuous power

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PCL 1,900 RPM

. . . . . . . . Two engine climbing airspeed min. 135 KlAS (250 kmlhr IAS)

. . . . . . . . . . . . . . . . At trans. altitude ALTIMETERS set STANDARD

Recommended vertical speed . . . . . . . . . . . . . . . . . . . . . (with passengers) max. 590 fpm (3 mls)

. . . . . . . . . . . . FASTEN SAFETY BELTS circuit breaker AS REQUIRED

FLIGHT IN SEVERE TURBULENCE

. . . . . . . . . . . . . . Reduce airspeed to max. 143 KlAS (265 kmlhr IAS)

. . . . . . . . . . . . . . . FASTEN SEAT BELTS circuit breaker SWITCH ON I FLIGHT UNDER ICING CONDITIONS

. . . . . . . . . . . . . . . . . . . . . . . ROTARY ICE DETECTOR CHECK ON

. . . . . . . . . . . . . . WINDSHIELD HEATING change-over switch SET to II I PROP DEICING change-over switch. . MAIN I or II (depending I

on rate of ice accretion)

SEPARATOR VANE LH and RH switches . . . . . . . . . . . . . . . . . . . . . . . . on the overhead panel AS REQUIRED I

. . . . . . . . . ONIOFF switch of pneumatic deicing system AS REQUIRED

(cont.)

Sep 25/98 (1) N-13

L 41 0 UVP-E20 CHECKLIST OF NORMAL PROCEDURES

ICE DETECTOR LIGHTING push-button . . . . . . . . . . PUSH (as required)

. . . . . . . . . . . . . . . Function selector of pneumatic deicing AUTOMAT

. . . . . . . . . . . . . . . . . . . . Cycle rate selector switch FAST or SLOW

INADVERTENT FLIGHT INTO FREEZING RAIN

. . . . . . . . . . . . . . . . . . . . . . . . Autopilot (if installed) DISCONNECT

Airspeed . . . . . . . . . . . . . . . . . . . . . max. 150 KlAS (278 km/h lASj

. . . . . . . . . . . . . . . . Altitude or heading change to leave these meteorological conditions

AFTER LEAVING THE POSSIBLE ICING AREA I

WINDSHIELD HEATING change-over switch . . . . . . . . . . . . . . . . . .

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 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . on the overhead panel OFF 1

. . . . . . . . . . . . . . . . . . . . . Switch of pneumatic deicing system OFF

(1) Sep 25/98


BEFORE DESCENT

Approach information . . . . . . . . . . . . . . . . . . . . . . . . . RECIEVED

FASTEN SEAT BELTS circuit breaker . . . . . . . . . . . . . . . . . . . . . ON

I DESCENT

Engines . . . . . . . . . . . . . . from max. cont. power to flight idle power

Recommended vertical airspeed . . . . . . . . . . . . . . . . . . . . . . (with passengers) 590 ftlmin (3 mls). I

PASSING TRANSITION LEVEL

Altimeters . . . . . . . . . . . . . . . . . . . Set to QNH ...... compare altitude

Brakes . . . . . . . . . . . . . . . . . . Brake accumulator pressure checked

AUTO FEATHER, AUTO BANK CONTROL, . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SPOILERS switches ON

. . . . . . . . . . . . . . . . . . . . . . . . . . Radio altimeter SET DH ......... ft

ON FINAL APPROACH

. . . . . . . . . . . . . . . . . . . . . Airspeed max. 135 KlAS (250 kmlhr IAS)

. . . . . . . . . . . . . . . . . . . . . . . . Landing gear DOWN and LOCKED

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Flaps 18'

PEDAL CONTROL cell . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONI . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LANDING LIGHTS ON

(cont.)

Sep 25/98 (1) N-15


. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Radar (if installed) STBY

. . . . . . . . . . . . . . . . . . . . . Airspeed min. 89 KlAS (165 kmlhr IAS)

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Heating SHUT I 100 f t (30 rn) above DH (MDA):

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PCL Fine pitch

Autopilot (if installed) . . . . . . . . . . . . . . . OFF or GO- AROUND at DH

At decision height (if decide t o land):

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Flaps 42'

Airspeed . . . . . . . . . . . . . . . . . . . . . . . . 84 KlAS (155 kmlhr IAS)

MISSED APPROACH WITH BOTH ENGINES OPERATING

(a) ABOVE DH (MDH)

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TCL Max. take-off power

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Climbing Initiate

Landing gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

. . . . . . . . . . . . . . . . . . . . . . . . . Airspeed 84 KlAS (155 kmlhr IAS)

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Landing lights OFF

After reaching a height of 400 ft (122 m)

. . . . . . . . . . . . . . . . . . . . . . . . . . Airspeed 94 KlAS (1 75 kmlhr IAS)

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . oo I

. . . . . . . . . . . . . . . . . . . . . . . . Airspeed 108 KlAS (200 kmlhr IAS)

(cont.)

N-16 (1) Sep 25/98


(b) BELOW DH (MDH)

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TCL Max. take-off power

Transmition to climb . . . . . . . . . . . . . . . . . at an airspeed . . . . . 84 KlAS (155 kmlhr IAS)

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Landing gear UP

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Flaps 18'

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Landing l ights. OFF

After reaching a height of 400 ft (122 m)

. . . . . . . . . . . . . . . . . . . . . . . . . Airspeed 94 KlAS (1 75 kmlhr IAS)

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Flaps . oO ( . . . . . . . . . . . . . . . . . . . . . . . . . Airspeed 108 KlAS (200 kmlhr IAS)

After reaching a height of 1500 ft (457 m):

. . . . . . . . . . . . . . . . . . . . . . . . . Airspeed 135 KlAS (250 kmlh IAS)

AFTER LANDING

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Taxi lights ON

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Transponder STBY.

. . . . . . . . . . . . . . . . . . . . . . . . . . . Graphic unit (if installed) OFF

. . . . . . . . . . . . . . . . . . . . . . . . . . . Nose wheel steering MANUAL

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SPOILERS, AUT. BANK CONTROL,

oo 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTOFEATHER switches OFF

. . . . . . . . . . . . . . . . . . . . . . . . Heating of air pressure heads OFF 1 (cont.)

Sep 25/98 (1) N-17


. . . . . . . . . . . . . . . . . . . . . . . . Deicing (windshield, propeller) OFF

. . . . . . . . . . . . . . . Horizons, Turn and bank indicator OFF and LOCK 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . GPS (if installed) OFF

. . . . . . . . . . . . . . . . . . . . . . . . . . . Radar screen (if installed) OFF

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Spec. equipment OFF

. . . . . . . . . . . . . . . . . . . . . . . Autopilot, elect. trim (if installed) OFF

. . . . . . . . . . . . . . . . . . . . . . . . . . . . PA, RADAR (if installed) OFF

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SEPARATOR VANE OFF

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Ice detectors OFF

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HF (if installed) OFF

. . . . . . . PROP. FEATHERINGIAUT. BANK CONTROL circuit breaker OFF

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADF, NAV, DME OFF

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . GYROCOMPASS OFF

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . STBY GYRO HORIZON OFF

. . . . . . . . . . . . . . . . . . . . . . . . . INVERTERS except No 1 36 V OFF

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Stop watch STOP

After stopping airplane:

FASTEN SEAT BELTS circuit breaker OFF I

. . . . . . . . . . . . . . . . . . . .

Parking brake pressure 25 + 5 kp/cm 2 . . . . . . . . . . . . . . . . . . . . . .

N-18 (1) Sep 25/98


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) OFF 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . IELU, ENGINE STARTING OFF

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FUELPUMP OFF

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INVERTER 36V I OFF

. . . . . . . . . . . . . . . . . . . . . . . All circuit breaker under cover OFF

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BATTERY I,II OFF

For long term parking:

. . . . . . . . . . . . . . . . . . . . . . . PCL Move out of "Feathered" position

Sep 25/98 (1) N-19


Intentionally left blank

N-20 Mar 1/96

check list

Documents

rec fall light

signal light

pneumatic

separator

automatic

central control

move slowly

propeller