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SusiAir L410 UVP-E20 Standard Operating Procedures

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Document No.:
Standard Operating Procedures
SOP-L410-1
L410 UVP-E20
Prelim. Page i
STANDARD OPERATING
PROCEDURES
(SOP)
L410 UVP-E20
REVISION 1 – JANUARY 2018
Rev: 1
Date: Jan 18
Prepared by: LA
Checked by : CLS

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  • Page 1 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Prelim. Page i STANDARD OPERATING PROCEDURES (SOP) L410 UVP-E20 REVISION 1 – JANUARY 2018 Rev: 1 Date: Jan 18 Prepared by: LA Checked by : CLS...
  • Page 2 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Prelim. Page ii This page left blank intentionally Rev: 1 Date: Jan 18 Prepared by: LA Checked by : CLS...
  • Page 3 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Prelim. Page iii STANDARD OPERATING PROCEDURES LET 410 UVP E-20 REVISION 1 PT.ASIPudjiastuti Aviation (Susi Air) DOCUMENT CONTROL Applicability: All Operations of PT. ASI Pudjiastuti Aviation Prepared by: Luca Amante (LA) Checked by:...
  • Page 4 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Prelim. Page iv This page left blank intentionally Rev: 1 Date: Jan 18 Prepared by: LA Checked by : CLS...
  • Page 6 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Prelim. Page vi This page left blank intentionally Rev: 1 Date: Jan 18 Prepared by: LA Checked by : CLS...
  • Page 7 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Prelim. Page vii RECORD OF REVISIONS Rev. Revision Date Date Inserted Signature July 2017 Initial Issue Jan 2018 Rev: 1 Date: Jan 18 Prepared by: LA Checked by : CLS...
  • Page 8 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Prelim. Page viii RECORD OF TEMPORARY REVISIONS Incorporated / Date Temp Date Superseded Rev No. Removed By Rev Issue Issue Inserted INSTRUCTIONS: 1. Retain this record in the front of the document.
  • Page 9 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Prelim. Page ix LIST OF EFFECTIVE PAGES CHAPTER PAGE DATE DOCUMENT TITLE PAGE Prelim. Page i January 2018 Blank Page Prelim. Page ii July 2017 DOCUMENT CONTROL Prelim. Page iii January 2018 Blank Page Prelim.
  • Page 10 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Prelim. Page x LIST OF EFFECTIVE PAGES (continued) CHAPTER PAGE DATE Pages 5-1 thru CHAPTER 5 DEPARTURES January 2018 5-30 Pages 6-1 thru CHAPTER 6 CRUISE July 2017 Pages 7-1 thru CHAPTER 7...
  • Page 11 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Prelim. Page xi Rev: 1 Date: Jan 18 Prepared by: LA Checked by : CLS...
  • Page 12 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Prelim. Page xii TABLE OF CONTENTS CHAPTER SUBJECT PAGE PRELIMINARY PAGES Prelim. DOCUMENT TITLE PAGE Page i Prelim. DOCUMENT CONTROL Page iii Prelim. CONTROL PAGE Page v Prelim RECORD OF REVISIONS Page vii Prelim.
  • Page 13 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Prelim. Page xiii CHAPTER SUBJECT PAGE Engine Power Limitation Page 2-13 Automatic Pilot KFC 325 Page 2-14 Flap System Page 2-17 Fuel Planning Page 2-18 Icing Conditions Page 2-19 CHAPTER 3 INTRODUCTION & GENERAL...

  • Page 14: Table Of Contents

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Prelim. Page xiv CHAPTER SUBJECT PAGE 3.15 Normal Procedure Checklist Page 3-21 CHAPTER 4 PREFLIGHT Crew Daily and Pre-flight Briefing Page 4-1 4.1.1 Emergency Briefing (CAPT/PF) Page 4-1 Operational Flight Plan Page 4-4...
  • Page 15 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Prelim. Page xv CHAPTER SUBJECT PAGE Passenger Briefing Page 5-7 Departure and Arrival Brief Page 5-9 5.8.1 Briefing Cards Page 5-10 5.8.2 Expanded Briefing Information Page 5-11 5.8.3 Example Briefings Page 5-13...
  • Page 16 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Prelim. Page xvi CHAPTER SUBJECT PAGE CHAPTER 6 CRUISE Cruise Power Setting Page 6-1 Use of Navaids for Enroute Navigation Page 6-1 Engine Trend Monitoring Page 6-2 Turbulent Air Prevention Page 6-2...
  • Page 17 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Prelim. Page xvii CHAPTER SUBJECT PAGE 7.17.1 Callouts Page 7-14 7.17.2 AP/FD use on ILS Approaches Page 7-16 7.17.3 Altitude Selector Use on ILS a Approaches Page 7-17 7.18 Non-Precision Instruments Approaches Page 7-17 7.18.1...

  • Page 18: L410 Uvp-E20

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Prelim. Page xviii CHAPTER SUBJECT PAGE CHAPTER 8 AFTER FLIGHT Shutdown Flow Items Page 8-1 Shutdown Checklist Page 8-2 Post Flight Page 8-2 Event Requiring Special Inspection Page 8-3 Event Requiring a Mandatory Safety Report...
  • Page 19 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Prelim. Page xix APPENDICES Emergency And Abnormal Procedures Page EE-1 to EE-93 Propeller Pitch Lock Page FF-1 Rev: 1 Date: Jan 18 Prepared by: LA Checked by : CLS...
  • Page 20 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Prelim. Page xx This page left blank intentionally Rev: 1 Date: Jan 18 Prepared by: LA Checked by : CLS...
  • Page 21 This Standard Operating Procedures Manual for the L410 UVP-E20 has been compiled to provide information and instruction to all flight crew on the manner in which their duties are executed when flying the L410 UVP-E20. All flight and ground operations personnel shall follow the procedures contained in this manual in the performance of their duties in accordance with Civil Aviation Safety Regulations.
  • Page 22 To highlight areas where mountain procedures may differ from normal procedures. Important notice To simplify matters, the official term: L410 UVP-E20 Aircraft may be changed to LET or L410 within the text of this manual. Rev: 1 Date: JAN 18...
  • Page 23 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 1 - 3 1.2. Manual Authority The Operations Manager is the authority responsible for the provision of this SOP Manual and all subsequent editions and revisions to it. The Operations Manager...
  • Page 24 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 1 - 4 All Revisions to the SOP Manual shall be approved by the DGCA. Revised copies of the SOP Manual shall be sent to all manual holders, who shall replace the outdated pages (or the complete Manual), with the revised pages.
  • Page 25 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 1 - 5 Definition and Abbreviation Above Aerodrome Elevation Air Data Computer Automatic Direction Finder AFCS Autopilot Flight Control System Aircraft Flight Manual Above Ground Level Attitude Heading Reference System Altitude Management System...
  • Page 26 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 1 - 6 Feet per Minute (climb- and descent rate) Glideslope angle (Jeppesen charts) Ground Power Unit Generator Control Unit Global Positioning System Ground Speed Intermediate Approach Fix Indicated Air Speed...
  • Page 27 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 1 - 7 STAR Standard Terminal Arrival Traffic Awareness System TAWS Terrain Awareness Warning System Throttle Control Lever or Throttle Lever. Traffic Selector Track Angle Error TOPO Topographic Display (map mode)
  • Page 28 Page 2- 1 LIMITATIONS 2.1 Aircraft Limitations Unless specifically mentioned in these SOPs the aircraft limitations apply as per the AFM L410 UVP-E20. AIRSPEEDS 182 KIAS MAXIMUM OPERATING LIMIT SPEED, V This operating limitation must not be deliberately exceeded in any regime of flight (climb, level flight, descent).
  • Page 29 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 2- 2 MAXIMUM FLAPS OPERATING SPEED 135 KIAS MAXIMUM PERMISSIBLE SPOILER EXTENSION SPEED, V 111 KIAS SPOIL MINIMUM CONTROL SPEED − for take−off run V 66 KIAS (is same for flaps 0°and 18°) MINIMUM CONTROL SPEED −...
  • Page 30 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 2- 3 MINIMUM TAKE−OFF SAFETY SPEED V AND V AIRSPEED VALUES VERSUS TAKE-OFF WEIGHT (wing flaps 18°) 2 18 R 18 Max. take-off Level of noise weight Measurement method Flaps position dB(A) CS-36, Am.2,...
  • Page 31 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 2- 4 CAUTION THE ACTUAL MAXIMUM PERMISSIBLE TAKE-OFF WEIGHT IS THE LOWEST ONE OF THE WEIGHTS DETERMINED BY FLIGHT MANUAL, PARA: TAKE-OFF WAT CURVES, TAKE-OFF FIELD LENGTHS AND NET TAKE-OFF FLIGHT PATH DATA, EN-ROUTE DATA.
  • Page 32 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 2- 5 CENTRE OF GRAVITY (LANDING GEAR EXTENDED) The centre of gravity limits must be always inside the envelope given by the curve shown in Fig. 2 − 1. The position of the Mean Aerodynamic Chord is shown in Fig. 2 −...
  • Page 33 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 2- 6 FLOOR LOADING LIMITATIONS FOR PASSENGER VERSION Maximum load on baggage compartments: Rear .................150Kg Front .................100Kg Maximum specific load on the floors of Baggagecompartments (front and rear) ..........400 kg/m Maximum specific load on the floor of passenger cabin.....
  • Page 34 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 2- 7 LIMITATIONS FOR CARGO VERSION Maximum load in baggage compartments: − Rear ..................150 kg − Front ..................100 kg Maximum weight of the cargo in thecontainer 1,000 kg Maximum weight of the cargo without the separator 500 kg installed....
  • Page 35 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 2- 8 LIMITATIONS FOR BAGGAGE / CARGO COMPARTMENT Maximum load of the extended baggage/cargo compartment........ 230 kg (507 lb) Maximum specific load on the floor 400 kg/m2 (82 ............lb/sq.ft) Maximum number of occupants including the crew is 19.
  • Page 36 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 2- 9 MAXIMUM NUMBER OF OCCUPANTS FOR 17 PASSENGERS VERSION The maximum permissible number of occupants including the crew is 19. The maximum permissible number of occupants including the crew for cargo version is 3.
  • Page 37 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 2- 10 PERFORMANCE LIMITATIONS MAXIMUM ALTITUDE The maximum permissible operating altitude is 14,000 ft. The maximum permissible operating altitude with fuel pumps inoperative is 13,120 The maximum permissible pressure airport altitude for take-off and landing is 13,120...
  • Page 38 Document No.: Standard Operating Procedures SOP-LET410 LET 410 UVPE-20 Page 2- 11 CROSSWIND SPEED LIMITATION Maximum permissible gust component of cross wind: −from dry and wet take-off and landing pawed runways ......29 Maximum permissible steady component of cross wind: −from dry and wet take-off and landing pawed runways ......
  • Page 39 Document No.: Standard Operating Procedures SOP-LET410 LET 410 UVPE-20 Page 2- 12 RUNWAY CONDITIONS (DEMONSTRATED VALUES) The take-off and the landing are demonstrated from and on paved and unpaved runways which comply with the following requirements: Paved take-off and landing runways: The friction coefficient of the take-off and landing runway is at least 0.2;...
  • Page 40 Document No.: Standard Operating Procedures SOP-LET410 LET 410 UVPE-20 Page 2- 13 2.2 Engine Power Limitations WARNING The following numbers are not to be used are limitations and shall not standard setttings. Take-off Climb Cruise Descent Continuous (max 5 min) Engine inop Torque...
  • Page 41 Document No.: Standard Operating Procedures SOP-LET410 LET 410 UVPE-20 Page 2- 14 2.3 Automatic Pilot KFC 325 Climb: Autopilot is not to be used in VS mode during climb. The only acceptable modes are pitch and indicated airspeed hold (IAS) mode. IAS is the preferred mode once the flaps have been retracted.
  • Page 42 Document No.: Standard Operating Procedures SOP-LET410 LET 410 UVPE-20 Page 2- 15 KMC 321 AUTOPILOT MODE CONTROLLER - This mode controller consists of nine Flight Director mode select buttons (Push on - Push off), mode annunciators, the vertical trim control, the yaw damper engage(disengage button, the autopilot engage) disengage button and the preflight test button.
  • Page 43 Document No.: Standard Operating Procedures SOP-LET410 LET 410 UVPE-20 Page 2- 16 MODE ANNUNCIATORS - The mode symbol located above each mode button will illuminate when the mode is engaged except for the NAV and APR modes. When either the NAV, APR or BC mode button is pressed the appropriate ARM annunciator above either the NAV or APR mode button will illuminate until the...
  • Page 44 Document No.: Standard Operating Procedures SOP-LET410 LET 410 UVPE-20 Page 2- 17 changing air conditions, power changes and/or aircraft configuration changes. 14. ALTITUDE HOLD (ALT) MODE - When pushed will select the Altitude Hold mode, which commands the airplane to maintain the pressure altitude existing at the moment of selection.
  • Page 45 Document No.: Standard Operating Procedures SOP-LET410 LET 410 UVPE-20 Page 2- 18 2.5 Fuel Planning VFR .......... Fuel to destination + 255Kgs (45Min) IFR with alternate ....Fuel to destination + fuel to alternate+ 255Kgs* IFR with no alternate ....Fuel to destination + 680Kg Notes: 1.
  • Page 46 Document No.: Standard Operating Procedures SOP-LET410 LET 410 UVPE-20 Page 2- 19 2.6 Icing Conditions: AIRSPEEDS IN ICING CONDITIONS MINIMUM AIRSPEEDS − Flaps retracted (position 0°) VREF+7 KIAS − Flaps extended (position18°) VREF+7 KIAS For V airspeed see section 5 of the AFM. WARNING MAXIMUM FLAP DEFLECTION IN ICING CONDITION IS LIMITED TO 18°.
  • Page 47 Document No.: Standard Operating Procedures SOP-L410-0 L 410 UVP-E20 Page 3 - 1 3 INTRODUCTION & GENERAL The purpose of this document is to integrate Susi Air procedures with the AFM in a practical way. This document must be consulted in conjunction with the AFM. Where a discrepancy exists, the manufacturer’s documents shall prevail.
  • Page 48 Document No.: Standard Operating Procedures SOP-L410-0 L 410 UVP-E20 Page 3 - 2 3.1 Method and Use of Checklists At all times the PM shall read the checklist on request from the PF hence the prescribed aircraft checklists are to be used at all times. It is, however, not a DO list, but a CHALLENGE RESPONSE checklist.
  • Page 49 Document No.: Standard Operating Procedures SOP-L410-0 L 410 UVP-E20 Page 3 - 3 3.2.2 Propeller Pitch Lock Test Refer toAppendix E or AFMSection IV Normal Procedures. All other checklists shall then becarried out as follows: The challenge shall be called aloud by the PM. The PF / PM shall check that the item has been carried out and give theprescribed response.
  • Page 50 Document No.: Standard Operating Procedures SOP-L410-0 L 410 UVP-E20 Page 3 - 4 3.3 Crew Conduct and Sterile Environment No flight crewmember may engage in any activity which would distract any other flightcrewmember from the performance of their duties or which could interfere inany way with the conduct of those duties.
  • Page 51 Document No.: Standard Operating Procedures SOP-L410-0 L 410 UVP-E20 Page 3 - 5 3.4 Division of Workload Any particular item in the cockpit shall generally be operated by the same crew member throughout the flight as laid out in the division of workload diagrams. Exceptions to this are: 3.4.1 Taxi During taxi, the throttle control levers are always the responsibility of the Captain.
  • Page 52 Document No.: Standard Operating Procedures SOP-L410-0 L 410 UVP-E20 Page 3 - 6 3.4.3 Cruise, Descent & Approach In Fight the throttle control levers are the responsibility of the PF. Only when the PF requests power changes, the PM adjust the throttle control levers. If the PM notices that the engine parameters are out of limits during critical stages of flight, he must adjust the throttle control levers to normal parameters, but this has to be communicated to the PF.
  • Page 53 Document No.: Standard Operating Procedures SOP-L410-0 L 410 UVP-E20 Page 3 - 7 GPS UNIT SETUP(AUX page) DATE/ TIME UTC DISPLAY UNITS NAV ANGLE MAGNETIC DISTANCE AND SPEED NAUTICAL ALTITUDE AND VERTICAL SPEED FEET BAROMETRIC PRESSURE HECTOPASCALS TEMPERATURE CELSIUS FUEL AND FUEL FLOW KILOGRAMS WEIGHT KILOGRAMS...
  • Page 54 Document No.: Standard Operating Procedures SOP-L410-0 L 410 UVP-E20 Page 3 - 8 MAP SETUP Navigation map page – MENU OVERLAYS - TRAFFIC, TOPO,TERRAIN and AIRWY MAP ORIENTATION HDG UP AUTO ZOOM MAX LOOK FWD 30 min MIN LOOK FWD 5 min TIME OUT 0 min...
  • Page 55 Document No.: Standard Operating Procedures SOP-L410-0 L 410 UVP-E20 Page 3 - 9 AVIATION ACTIVE FPL 2000NM ACTIVE FPL WPT 2000NM LARGE APT 500NM MEDIUM APT 300NM SMALL APT 100NM SAFE TAXI RWY EXTENSION 30NM INT WAYPOINT 30NM NDB WAYPOINT 30NM VOR WAYPOINT 150NM...
  • Page 56 Document No.: Standard Operating Procedures SOP-L410-0 L 410 UVP-E20 Page 3 - 10 AIRWAY AIRWAYS LOW ALT AIRWAY 200NM HI ALT AIRWAY 300NM LAND LAT / LON SMALL FREEWAY 300NM NATIONAL HWY 80NM LOCAL HWY 30NM LOCAL ROAD 15NM RAILROAD 30NM LARGE CITY SMALL...
  • Page 57 Document No.: Standard Operating Procedures SOP-L410-0 L 410 UVP-E20 Page 3 - 11 NOTE: Using wind vector option (X/Y) during the finals checks will allow for a directreading of the headwind/ x wind component 3.8 Lights Anticollision Beacon and Position lights shall remain on at all times when the betteries are switched ON.
  • Page 58 Document No.: Standard Operating Procedures SOP-L410-0 L 410 UVP-E20 Page 3 - 12 WARNING IF A NIGHT FLIGHT IS PLANNED, CHECK OPERATION OF ALL LIGHTS AND MAKE SURE A FLASHLIGHT IS AVAILABLE FOR BOTH CREW MEMBERS AND PROPERLYSTOWED. WARNING ANTICOLLISION BEACON MAY CAUSE DISORIENTATION ORVERTIGO WHEN IN CLOUDS.
  • Page 59 Document No.: Standard Operating Procedures SOP-L410-0 L 410 UVP-E20 Page 3 - 13 3.9 GARMIN GTN 750 The Garmin GTN navigation system is a GPS system with a Satellite Based Augmentation System (SBAS), comprised of Garmin TSO-C146c GTN 650 and GTN 750 navigators and Garmin approved GPS/SBAS antennas.
  • Page 60 Document No.: Standard Operating Procedures SOP-L410-0 L 410 UVP-E20 Page 3 - 14 The device is connected to the external Garmin GTS 8000 TCAS II unit and it is possible to display the output from this unit on the GTN 650/750 screen. To display the Traffic information, touch the Traffic key on the home page.
  • Page 61 Document No.: Standard Operating Procedures SOP-L410-0 L 410 UVP-E20 Page 3 - 15 The WX radar shall be selected to standby before commencing taxi. The WXradar shall be turned to standby whenever not required (VMC). When using the weather radar, enable WATCH® and Weather Alerts and may be overlaid on the map display.
  • Page 62 Document No.: Standard Operating Procedures SOP-L410-0 L 410 UVP-E20 Page 3 - 16 3.10GARMIN GTN 650 GTN 650 Control and Display Layout – typical When flying in busy airspace or when a large number of aircrafts are operating in the vicinity, the traffic page should be set on the GTN 650 to improve situational awareness in flight.
  • Page 63 Document No.: Standard Operating Procedures SOP-L410-0 L 410 UVP-E20 Page 3 - 17 3.11 Radar Altimeter KRA 405B (with EFIS EFI 890R system). THE RADAR ALTIMETER IS AN AWARENESS TOOL ONLY AND IS NOT TO BE USED TO DETERMINE MINIMUMS. THE BAROMETRIC MINIMUM (ALTIMETER) REMAINS THE PRIMARY SOURCE.
  • Page 64 Document No.: Standard Operating Procedures SOP-L410-0 L 410 UVP-E20 Page 3 - 18 3.12 Terrain Awareness Although all Susi Air L410UVP-E20 Aircraft are equipped withTAWS, it is essential crews are aware that this is a tool to increase situational awareness and NOT tobe used for primary terrain avoidance.
  • Page 65 Document No.: Standard Operating Procedures SOP-L410-0 L 410 UVP-E20 Page 3 - 19 FLTA and PDA alerts can be inhibited by pressing the Menu key on the Terrain page and then TAWS Inhibit key. Tab. 1 Minimum Clearance Altitude (feet) Flight Phase Level Flight Descending...
  • Page 66 Document No.: Standard Operating Procedures SOP-L410-0 L 410 UVP-E20 Page 3 - 20 3.13 Ground Proximity Warning System (GPWS) It provides the followings alerts: 1. Excessive Closure Rate (ECR): System issues an alert when the airplane is determined to be closing upon terrain at an excessive speed for a given gear and flaps configuration.
  • Page 67 Document No.: Standard Operating Procedures SOP-L410-0 L 410 UVP-E20 Page 3 - 21 3.14 Weight and Balance The pilot in command is responsible for ensuring that the aircraft is operated within the published weight and balance limits at all times. Refer to Appendix B.
  • Page 68 Document No.: Standard Operating Procedures SOP-L410-0 L 410 UVP-E20 Page 3 - 22 This page is left intentionally in blank Rev: 1 Date: JAN 18 Prepared by: LA Checked by: CLS...

  • Page 69: Chapter 4 Preflight

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 4 - 1 PREFLIGHT 4.1 Crew Daily and Pre-flight Briefing The intention of these briefings is to ensure that all crew members are aware of all pertinent factors which may affect the conduct of the flights. By discussingthese factors early in the duty period and before flights, there is ample time torevise plans and straighten out misconceptions.
  • Page 70 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 4 - 2 The following standard briefing should be as follows: It will be my departure using flap 18° (or non-Standard flaps 0°). Kts, Vr___Kts, Kts. 1___ 2___ Emergencies before V1 ·...
  • Page 71 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 4 - 3 Emergencies after V1 · This part of the briefing is conducted by the PF. In the event of emergencies after V1, we will continue the take off by applying maximum power, and establish a positive rate of climb, retract the gear and accelerate to V2.

  • Page 72: Operational Flight Plan

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 4 - 4 4.2 Operational Flight Plan Every flight conducted in accordance with Part 135 of the DGCA is required tohave an operational flight plan. Refer to the following pages for a copy of anddescription of the OFP. An Excel OFP shall be made available to crews at allstations.
  • Page 73 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 4 - 5 Fuel YYYY-MM-DD Date I certify the accuracy of and accept Requirments this Operational Flight Plan IAW CASR 135.601. Captai Taxi PT ASI Pudjiastuti Trip Aviation Flight Operational Flight...

  • Page 74: Aircraft Preparation

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 4 - 6 4.3 Aircraft Preparation The aircraft is prepared by both pilots simultaneously as per normal procedures checklist. The Captain does the walkaround. The FO conduct the emergency exits equipement inspection and the prepares the paperworks (aircraft logbook, flight plan, weight&balance etc..

  • Page 75: Cockpit/Cabin Preparation

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 4 - 7 4.4 Cockpit/ Cabin Preparation Once the Preflight Checklisthas been completed,the Captain completes the systems checks. The FO completes a general inspection of the cabin, ensuring that seats are correctlypositioned and secured, life vests and briefing cards are present, the seat belt/no smoking signs are working and the aircraft is presentable to passengers.

  • Page 76: Fuel Type

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 4 - 8 4.5.1 Fuel type JET & JETA1 are the only permissible fuel type to be used. 4.5.2 Fuel Specific Gravity Conversion from Liters to Kilograms shall be made using the Specific Gravity (SG) of 0.8.

  • Page 77: Concept Of Ground And Air Checklist

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 4 - 9 4.7Concept of Ground and Air checklist L410 UVP-E20 NORMAL CHECKLIST G R O UN D A IR The L410 on the ground can only be controlled by the Captain, therefore all checklist prior take- off and after landing are carried out by the FO.

  • Page 78: Engine Starting

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 4 - 10 4.9 Engine Starting BATTERY ENGINE START Condition Check prop area clear Check prop area clear Before start checklist complete, ook out and check prop clear After engine start approval, Selecting Announce: Starting N°1/2 Start timing, check voltage Push starter and hold for 3 (min 14 V for 4 sec.) – VA...
  • Page 79 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 4 - 11 GPU ENGINE START Condition Check voltage Verify External Power on VA selector set to CWD is on. emergency bus, check voltage Voltage of the GPU (unloaded) between 27-29V / minimum 20 V Before start checklist complete, ook out Check prop area clear Check prop area clear and check prop clear After engine start approval, Selecting Announce:Starting N°1/2...
  • Page 80 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 4 - 12 General start callouts StartCallouts Lookoutandcheckpropclear CAPT:“Clear(No1/2)” “Clear(No1/2)” Selectingengineswitch CAPT:“Starting(No1/2)” atillumination of engine starting cell CAPT:“Engine Starting” atillumination of limiter active cell CAPT:“Limiter Active” Whenvoltsdrop “Voltdrop….v” At first indication of oil pressure on selected engines oil CAPT:“Oil pressure rising”...
  • Page 81 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 4 - 13 4.10. After Start The following values are for reference only and based on standard ISA and sealevel. For the correct values, crew shall refer to the aircraft AFM.

  • Page 82: After Start

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 4 - 14 4.10.1 AFTER START ITEMS CM 1 CM 2 • DC GEN LH/RH • INVERTER 36 V II • AC GEN LH/RH • ADC I + II • VENTILATION/AC •...
  • Page 83 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 4 - 15 Page intentionally left blank Rev: 1 Date: JAN 18 Prepared by: LA Checked by: CLS...

  • Page 84: Chapter 5 Departures

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 1 5 DEPARTURES 5.1 Taxiing Taxi can only be carried out from the left seat. During the taxi to the holding point, the FO will obtain the departure clearance.Taxiing is normally initiated by cycling the PCL’s to feather and return to the full forward position, cycle is limited to 30 seconds (see AFM 4-12).
  • Page 85 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 2 5.2 Operations on Unsealed Surfaces Parkingthe aircraft with the nose wheel straight also minimizes power required. The aircraft should be kept moving unless it isabsolutely necessary to stop. Rolling takeoff’s are to be used unless necessary for performanceconsiderations.
  • Page 86 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 3 5.3 Instrument Check After AHS1-2 alignment is complete, verify no messages* are present, altimeters crosscheckedand headings set and cross-checked.Instrument checks are done during the turns, when safe and practical.

  • Page 87: Taxi Flow Items

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 4 5.4 Taxi Flow Items During the taxi, the FO must hold the control yoke in the neutral position while the Captain taxies the aircraft. While taxiing the aircraft, the Captain calls for each of the various “TAXI ITEMS”, and the FO completes them as per the sequence below.

  • Page 88: Taxi Checklist

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 5 5.5 Taxi Checklist Once the After Start Checklist has been completed, and all red Xsand comparator messages are extinguished, the Captain will instruct the FO torequest Taxi Clearance; if operating from uncotrolled aerdromes, the FO will make a general broadcast on the local frequency.
  • Page 89 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 6 5.6 Use of Radios Radio calls and PA‘s shall be made by the PM. Com 1 shall be used for all normal communications. Com 2 shall be used for gathering ATIS information, talking to company, andwhen talking to two ATC facilities simultaneously.

  • Page 90: Passenger Briefing

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 7 5.7 Passenger Briefing To activate the PA, press both MUTE and SPR buttons on the audio panel, the associated led lights will start flashing, then press the TX button on the control column.
  • Page 91 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 8 10 MINUTES BEFORE LANDING Para Penumpang yang terhormat, Kita akan segera mendarat di bandara..(destination’s airport) Kami mohon untuk mengencangkan sabuk pengaman anda. Terima kasih. AFTER LANDING Para penumpang yang terhormat, Kita telah mendarat di bandara ..(destination’s airport)

  • Page 92: Departure And Arrival Brief

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 9 5.8 Departure and Arrival Briefing Briefing Philosophy The departure and arrival briefings should generaterelevant, thought provoking discussion. Every departure and arrival must be viewed in the context of the specificthreats posed by the operation and the strategies that will be employed toovercome them.

  • Page 93: Briefing Cards

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 10 5.8.1 Briefing Cards Rev: 1 Date: JAN 18 Prepared by: LA Checked by: CLS...

  • Page 94: Expanded Briefing Information

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 11 5.8.2 Expanded Briefing Information TERRAIN · Relevant terrain/ obstacles near the airport - departure/ arrival path Relevant MSA If an MSA is unavailable; obtainterrain info from the following ·...
  • Page 95 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 12 THREATS · · Comm’s · Tracking · Procedural Control · Traffic Density · Missed approach vital actions if there is a high probability of a missed · approach ·...

  • Page 96: Example Briefings

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 13 5.8.3 Example Briefings Example #1: Departure Brief Departure RWY 24 Halim, weather CAVOK. “Runway 24 Departure Initial Turn expected to the Left Initial course to BND is 134 set on the CDI with GPS selected Initial Altitude is set to 9500 ft Terrain –...

  • Page 97: Navigation Set Up For Takeoff

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 14 5.9 Navigation Set Up for Takeoff Composite COMP 360 HSI – HSI display The standard configuration for PFD 1 and PFD 2 is COMP 360 HIS. Composite COMP ARC MAP can be used prior take-off to check GPS flight plan and its...

  • Page 98: Flight Director Usage On Takeoff

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 15 5.10 Flight Director Usage on Takeoff Use of the Flight Director for takeoff is recommended in low visibility, low ceiling takeoffs, however it can only be engaged after take-off. Before entering the runway, the heading bug shall be set to the heading of the runway to be used.

  • Page 99: Departure Procedure

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 16 5.11 Departure Procedure 5.11.1 GPS Nav Setup The required flight plan must be loaded into the GTN750/650. Tracks, waypoints and altitude restrictions shall be checked against OFP and published procedures.

  • Page 100: Bluesky Satellite Tracking

    Page 5 - 17 5.13 Bluesky Satellite Tracking All L410 UVP-E20 aircraft operated by the company are equipped with theBluesky Satellite Tracking system. This system enables company flight followingto track all aircraft with high precision, maintain two-way contact the crews bydata and voice channels, and provides emergency response with high speedand precision.

  • Page 101: Definitions

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 18 5.14 Definitions: Terrain Switch: Must always be in NORMAL except in airports which are not in the database and would thus cause an immediate TERRAIN warning after liftoff.

  • Page 102: Lineup Flow Items

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 19 5.15 Lineup Flow Items Captain FirstOfficer ITEM ACTION ITEM ACTION Steering PEDAL Instruments ALIGNED/NO RED X’S Instruments ALIGNED/NO RED X’s Windows SHUT Windows SHUT Stall/Pitot/Static Heat Transponder TA/RA/ RANGE20nm...
  • Page 103 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 20 Rolling takeoffs are preferred for passenger comfort and to minimize propellerchips if ample runway is available. Advance the power levers smoothly ensuringthat the oil temperatures and pressures are rising normally, the propeller rpmstabilizes at 2020 RPM, and that the Torque, ITT and the Ng remain withinlimits.

  • Page 104: Take Off Procedure

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 21 TAKE-OFF WITH CROSSWIND Use standard AFM procedures for take-off with flaps 18° and 0° for crosswind gusts up to 20 kts. When cross wind component exceeds 20 kts apply in addition the following procedures : •...

  • Page 105: Climb Procedures

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 22 5.19 Climb Procedure Initial climb to 400 feet AGL, no aircraft configuration changes shall be made unless required due terrain,weather or ATC considerations. Initial climb speed is V2+5 KIAS as briefed by the crew.

  • Page 106: Climb Airspeed

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 23 5.20 Climb Airspeed Normal cruise climb airspeeds are 135 to 145 KIAS. The speed may be varied for reasons of terrain, weather, ATC, or passenger comfort (unpressurized aircraft).

  • Page 107: Use Of Altitude Selector

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 24 5.22 Use of Altitude Selector Setting theALTITUDE SELECTOR shall follow the procedure below: When receiving a clearance, the PF/ PM shall set the altitude on theindicator and then call for eg.
  • Page 108 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 25 5.23 Autopilot Operation Use of the autopilot is encouraged to reduce workload and improve passengercomfort.The autopilot is a tool to be used to enhance situational awareness but shouldnot be overly relied upon.

  • Page 109: Autopilot Operation

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 26 5.23.1 AUTOPILOT OPERATION Refer to AFMSECTION IX, SUPPLEMENT No. 118, Autopilot KFC 325 1. Before take off A/P DISC/TRIM INTER (A/P DISC) Switch PRESS. 2. In-flight Autopilot Engagement The airplane must be trimmed before in-flight autopilot engagement.

  • Page 110: Afcs Callout Table

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 27 5.24 AFCS Callout Table The following callouts shall be used with the corresponding annunciations in theAFCS status box. Available LateralModes Annunciator Callout Armed FDMode GPSAPPR GPS Approach APPR...
  • Page 111 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 28 AvailableVerticalorSpeedModes ArmedFD Annunciator Callout Mode ASEL CAP or Altitude preselected captured ASEL ALT SEL “Capturing altitude” ALTHOLD Altitude Hold mode captured ALT(hold) “Altitude Hold” GoAround mode Glideslope captured...
  • Page 112 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 29 5.24.1 Flight Director/ Autopilot Management Systems Selection Call Outs Pilot Flying Pilot Monitoring “Select Heading mode” “Heading mode selected” “Select Indicated Air Speed” “Indicated Air Speed Selected” “Arm Nav Mode”...
  • Page 113 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 5 - 30 5.25 Standard Altimetry Calls When altimeters are set, both pilots must repeat the number that they are settingand cross check the altimeters. The Captains altimeter shall be considered asthe master during instrument checks unless proven to be outside tolerances.

  • Page 114: Chapter 6 Cruise

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 6 - 1 6. CRUISE 6.1 Cruise Power Setting 1. Refer To Table 2-10 in AFM for Limits ITT & Torque. 2. Refer to AFM Section V pg 5-150 Fig 5-82 3.

  • Page 115: Engine Trend Monitoring

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 6 - 2 6.3 Engine Trend Monitoring Regular trend monitoring during stabilized flight is an essential part of the company’s maintenance program. The early detection of changes in engine parameters can prevent more costly repairs being necessary at a later time.

  • Page 116: Avoidance Of Thunderstorms And Associated Hazards

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 6 - 3 6.5 Avoidance of Thunderstorms and Associated Hazards Company policy is that Captains will try to avoid severe turbulence; particularly that associated with cumulonimbus activity whenever possible. Take off and landings should not be attempted when cumulonimbus activity is present within 5 nm of an airfield.
  • Page 117 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 6 - 4 This page has intentionally left blank Rev: 1 Date: JAN 18 Prepared by: LA Checked by: CLS...
  • Page 118 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 1 7. ARRIVAL It is recommended theuse of VCALC function to ensure tocross the IAF at the prescribed altitude, allowing for time to decelerate if required for instrument approaches and from the airport 6 nautical miles at2000 feet AGL for visual conditions.

  • Page 119: Descent Power Setting

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 2 7.1 Descent Power Setting Throughout descent the TCLs shall be reduced to maintain a recommended airspeed of 170 KIAS. Asthe aircraft descends the torque increases and the airspeed mayexceed the maximum permissible speed at lower altitudes.

  • Page 120: Flap& Gear Selection

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 3 7.4 Flap& Gear Selection The PF shall request configuration changes. The PM must confirm that the speed/altitude criteria are met and then action the desired configuration change. The PM must only respond once the configuration change is complete.The challenge and response for flap selection is as follows:...

  • Page 121: Approach Category

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 4 7.5 Approach Category Approaches for the LET 410are eitherCat A or Cat Bdepending on the landing weight. Refer to AFM or Chapter 7.21.4 Figure 7.5 . 7.6 Navigation Setup for Approaches Garmin GTN 750: Whenever approaches are in the database they shall be loaded to aid insituational awareness.

  • Page 122: Arrival/Approach Briefing

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 5 MINIMUMS: For every instrument approach the barometric minimums must be set.Select on DCP-5031 Display Control Panel: • For ILS approaches set DA. • For Non precision approaches set MDA + 50 feet.

  • Page 123: Example Arrival Briefing

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 6 7.7.1 Example Arrival Briefings Example #1 Complex IFR Arrival Brief: Arrival Halim from Nusawiru ATIS: Halim information Bravo, weather at one six three five five Zulu. Wind twozero zero at 15, visibility 3 km in rain.
  • Page 124 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 7 ATIS: Polonia information Delta, weather at zero six zero five Zulu. Wind one fourzero 15 gusting 20, visibility 5 km. Fifteen hundred broken, Three thousandovercast temperature two niner, dew- point two three.

  • Page 125: Approach Deviation Callouts

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 8 7.8 Approach Deviation Callouts The use of the “two communication” rule is essential to a well-structured multi-crew operation. At any stage of flight, where a challenge is made and no response is forthcoming, a second challenge should be made.
  • Page 126 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 9 GSmorethan halfscale “Glideslope” PFtakes “Correcting” deflection after corrective established action ROD different bymore “Descent PFtakes “Correcting” than 200fpmof Rate” corrective briefedROD from theFAF action (CANPA) Aircraftmore than+/-5 “Speed” PFtakes “Correcting”...

  • Page 127: Descent Callout

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 10 7.9 Descent Callouts Descent Callouts 15minsbeforedescent,thePMwillobtain PF: “Ready for briefing?” theweather/ATIS(asapplicable) PM: “Ready” Before briefing the approach, the required data must be configured and set. (ApproachspeedandDA/MDA) Thedescentchecklististhencalled PF:“Descentchecklist” Thedescentchecklististhencompleted PM:“Descentchecklistcomplete”...

  • Page 128: Approach Checklist

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 11 7.11 Approach Checklist Carried out approximately 15nm before the airport Approach Callouts PF calls for approach checklist, PM will action the PF: “Approach Checklist” checklist. APPROACH call out Fuel Transfer / X-feed COMPLETED...

  • Page 129: Stable Approach Concept

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 12 7.13 Stable Approach Concept A stabilized approach is one of the key features of safe approaches andlandings in air transportation operations. It is intended to decrease workload,minimize crew distraction, and reduce the hazards associated with configurationchanges at a critical phase of flight;...

  • Page 130: Mandatory Missed Approach

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 13 NOTE No Go-Around performed by Susi Air crew will ever be investigated or followedup in a punitive way. Reasons for a Go-Around may be required for analysis butno crew will be “blamed” for doing it.

  • Page 131: Ils Approach

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 14 ILS Approach 7.17 7.17.1 Callouts NOTE: The following table depicts an ILS with the AP in use. Phase ofFlight Call-out Remarks On interecet heading and PF: “ARM APPROACH MODE”...

  • Page 132: L410 Uvp-E20

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 15 At glideslope intercept Call made by PM when glide PF: “GLIDE SLOPE CAPTURED Slope annunciator turns green. PM: “CHECK” Response made by PF Selecting missed approach altitude on AMS PF request altitude as per plate PF: “SET MISSED APPROACH...

  • Page 133: Ap/Fd Use On Ils Approaches

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 16 At DA/H PF: “minimum” Call by PFat minima, PM shall state if visual reference has PM: “NOT VISUAL” or landing been acquired or not. reference” Eg. “lights straight-ahead” If visual PF: “LANDING, AP-YD...

  • Page 134: Altitude Selector Use On Ils A Approaches

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 17 If cleared to intercept the localizer only The crew must select NAV mode. Selecting APR arms the GS. Capturing the Glideslope from above Capturing the glideslope from above should be avoided, however due to radar vectors, wind, late approach clearance etc.

  • Page 135: Non-Precision Instrument Approaches General

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 18 7.18.1 Non-Precision Instrument Approaches General Over the past several decades there have been a number of CFIT andunstabilised approach incidents and accidents associated with non-ILSapproaches and landings. Many of these could have been prevented by the use of constant angleapproach methods.

  • Page 136: Ap/Fd Use On Canpa Approaches

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 19 Table 1 CANPA Calculation: Target Ht. Distance Out Manual Calc. (Nm) Target Ht 6 NM 1940 feet 5 NM 1620 feet 4NM 1300 feet 3 NM 980 feet 2 NM 660 feet 1 NM 340 feet Threshold ELV feet Note: 3 degrees slope equals 320 feet per nautical mile.

  • Page 137: Altitude Selector Use On Canpa Approaches

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 20 APR mode should not be selected until: • The VOR is tuned and identified • CDI Green with correct Nav source selected. • The aircraft is on an inbound intercept heading •...

  • Page 138: Minimum Descent Altitude Mda(H)

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 21 7.18.6 Minimum Descent Altitude MDA(H) Approaches should be flown to a published MDA(H) used as a decisionaltitude. should expand instrument scan include outside visual cueswhen approachingMDA(H). Do not continue the approach below MDA(H)unless the aircraft is in a position from which a normal approach to therunway of intended landing can be made and a suitable visual reference can bemaintained.

  • Page 139: Canpa Callout Table

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 22 7.19 CANPA Callout Table The following table shows a VOR CANPA approach. Phase of Flight Call-out Remarks On interecet heading and cleared for the PF: “ARM APPROACH MODE” Call made by PF requesting approach.
  • Page 140 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 23 At FAF (if applicable) Call made by PM when at FAF. PM: “FINAL APPROACH FIX, ” PFsets the MDA and calls the altitude. PF: “MDA _____ FEET SET” PM checks and sets theMDA.
  • Page 141 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 24 100 ft above MDA/H PF: “100 ABOVE, Call made by PF, PM shall look out for required visual PM: “LOOKING UP” refernces. At MDA/H + 50 feet PF: “minimum”...

  • Page 142: Missed Approach

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 25 7.20 Missed Approach Once reaching minimum, the PF calls “ minimum and state the action: Landing/Go around, however if the PF doesn’t make the call out, the PM must immediately call out: minimum and if not visual, PM must call “Go Around”.

  • Page 143: Circling Approach

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 26 7.21 Circling Approach A circling approach is a instrument flight manoeuvre with visual references. Each circling situation is different, because of the variables such as runway layout, final approach track, wind velocity terrain and meteorological conditions.

  • Page 144: Ap/Fd Use On A Circking Approach

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 27 If visual reference is lost while circling to land from IMC approach, PF issues command “GO AROUND“ and the missed approach specified for that particular instrument procedure must be followed.

  • Page 145: Circling Category

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 28 Figure 7-4 Circling speeds and circling restrictions 7.21.4 Circling Category Circling approaches can be either Cat A or B for Susi Aircraft. If Cat B is used,ensure the Cat B minimums are used (which may be more restrictive.
  • Page 146 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 29 Figure 7-5 Circling radius (Cat A shown) 1.68 nm Cat A PAN OPS Figure 7-6 PANS-OPS shown on bottom left corner of approach chart along with categories Adjust airplane heading and timing so that the airplane ground track does notexceed the obstruction clearance distance from the runway at any time duringthe circling approach.

  • Page 147: Missed Approach - Circling

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 30 “original PF“(the pilot whowas PF during the initial phase of the approach) has the runway in sight, he/she may take control and continue the approach and land (Captain discretion).

  • Page 148: Visual Approach

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 31 7.22 Visual Approach Whenever a visual approach and landing is to be initiated or accepted the pilotmust have the required visual meteorological conditions prior to descendingbelow the MSA such that a visual circuit may be flown at all times with the airportrunway in full unobstructed view of the (PF).

  • Page 149: Landing Flow Items

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 32 7.23Landing Flow Items PilotFlying PilotMonitoring ITEM ACTION ITEM ACTION CabinLights Heating CLOSED IceProtection OFF(Asrequired) Gear DOWN Gear DOWN,LOCKED, 3GREENS Brakes CHEKCED Brakes CHECKED Steering PEDAL Steering PEDAL/INDICATED Flaps 18°...

  • Page 150: Landing

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 33 7.25 Landing As the threshold is crossed the power lever should slowly be reduced towardidle and the spoilers deployed. If FO is conductingthe landing,a call to the Captain to deploy the spoilers shall be made.

  • Page 151: Rejected Landing

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 34 7.26 Rejected Landing No visual cues/references at MAP PF/PM: “GO AROUND” PF call sfor go-around power, max continuous power, and orApproach not stabilized rotates the aircraft 8° to 10°...

  • Page 152: After Landing Flow Items

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 35 After a Go Around, all checklists shall be completed (After Take-Off, Climb,Approach and Fina). The Captain may elect to fly the circuit with Gear Down and flaps set at 18 degrees.

  • Page 153: When Clear Of Runway Checklist

    Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 36 7.28 When Clear of Runway Checklist This checklist is to be completed when the aircraft is clear of the runway or hasreached taxi speed at airports with no ramp. Crews must ensure that all items are completed by using the appropriate checklist.
  • Page 154 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 7- 37 7.29 Engine Cooldown Shutdown is after 5 minutes. This is the time needed for the engine cool downand it may include taxiing time. During taxiing the gasgenerator speed may rise to maximum 70% Ng for a period not exceeding 15 seconds.
  • Page 155 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 8 - 1 8. AFTER FLIGHT 8.1 Shutdown Flow Items Once the aircraft is parked, the Captain will set the TCLs to idle (5 min cooling), and feather the propellers (min 40, seconds to remove oil from the reduction gearbox), and announce “Set Park Brake”.
  • Page 156 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 8 - 2 8.2 Shut Down Checklist SHUTDOWN call out FEATHER PCL Capt. OFF AC/DC GEN Capt. SHUT ETL Capt. OFF Engine Start CB's / ELU's Capt. OFF (NG < 5%) Fuel Pumps Capt. OFF Lighting, Avionic I/II Capt. OFF BATTERIES / 36V Inverter Capt. OFF Circuit Breakers Capt.
  • Page 157 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 8 - 3 8.4 Events Requiring Special Inspection The following events require a special inspection before the next flight: • Hard Landing. • Lightning Strike. • Prop Strike or sudden engine stoppage.
  • Page 158 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 8 - 4 8.5 Events requiring a mandatory safety report Any time the Captain or FO deem it necessary, they shall without hesitation file a safety report. Here are some mandatory events requiring a safety report: •...
  • Page 159 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 9 - 1 9. ABNORMAL AND EMERGENCY PROCEDURES 9.1 Types of Checks 9.1.1 Immediate Action Procedures found on the emergency checklist which are BOLD FACED type are immediate action items which should be committed to memory.
  • Page 160 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 9 - 2 NOTE CWD messages can give you incorrect information due to sensor faults etc. Before actioning any checklist; investigation (time permitting) is essential. Ie. ENGINE FIRE MESSAGE. Call for the appropriate memory items/ checklist time permitting...
  • Page 161 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 9 - 3 2) Find a landing site a) Engine Failure • Are there any airports nearby? • Any emergency landing sites? • Any terrain between us and the landing site? •...
  • Page 162 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 9 - 4 3) Company a) Bluesky – Emergency button required? i) Make a call or send a message time permitting? b) Call on company frequency 4) Passengers a) The PM shall brief the passengers on any emergency situation.
  • Page 163 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 9 - 5 This course of action is to enhance our CRM procedure’s and make our decision making process clear and concise during critical phases of flight. After such an event, a mandatory safety report is required, even if the Captain followed the advice and no control takeover was required.
  • Page 164 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 9 - 6 9.5 WINDSHEAR To prevent a windshear accident from occurring, obey the following windshear rules. Avoidance • Visual Identification of severe weather • LLWAS (Low Level Windshear Alert System) •...
  • Page 165 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 9 - 7 9.6 TCAS Traffic Warnings For specific crew procedures, refer to APPENDIX E. EMERGENCY AND ABNORMAL PROCEDURES Rev: 1 Date: Jan 18 Prepared by : LA Checked by : CLS...
  • Page 166 Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 9 - 8 9.7 Abnormal Checklist Refer AFM L410 UVP-E20 SECTION IIIA ABNORMAL PROCEDURES. For specific crew procedures, refer to APPENDIX E. EMERGENCY AND ABNORMAL PROCEDURES 9.8 Emergency Checklist Refer AFM L410 UVP-E20 SECTION III EMERGENCY PROCEDURES.
  • Page 167 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 9 - 9 Rev: 1 Date: Jan 18 Prepared by : LA Checked by : CLS...
  • Page 168 Document No.: Standard Operating Procedures SOP-L410-1 L410 UVP-E20 Page 9 - 10 This page is left intentionally in blank Rev: 1 Date: Jan 18 Prepared by : LA Checked by : CLS...
  • Page 169 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page AA -1 APPENDIX A- BLUESKY SATELLITE TRACKING Control Head The control head is the primary interface with the modem unit installed in theaircraft. By looking at the LED indicators on this unit the pilots can instantly seethe status of the entire system.
  • Page 170 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page AA -2 Blinking: The unit is attempting to transmit or receive via the Iridium satellitenetwork. The following routine transmit intervals are set in the aircraftand should be observable by the crew: 1.
  • Page 171 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page AA -3 Ethernet Port Software on the D1000 unit is accessed through the Ethernet port on the frontpanel. A standard Ethernet cable is required. LED indicators: • LNK – The LNK LED indicates that a connection between the unitEthernet port and an attached device has been made.
  • Page 172 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page AA -4 be conducted and authorized by company management personnel incoordination with all parties involved. NOTE Ensure you press the quick position button BEFORE actioning checklists itemswhich call for all electric power to be removed from the aircraft to ensure thesignal is sent.
  • Page 173 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page AA -5 The main screen normal display has the following information: With the Menu Navigation Button all menus and sub-menus can be selected(see Menu Quick Reference table on the right). The following is a description ofall menu functions available with the ACH 1000.
  • Page 174 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page AA -6 Phone Number Entry: All calls from the Bluesky system are handled asinternational calls and require a country code. Sincethe ‘+’ symbol represents “00”, simply enter thecountry code and the phone number.
  • Page 175 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page AA -7 INCOMING MESSAGES Incoming messages are signaled by a blue message light on the Bluesky controlhead. The crew should monitor this indicator regularly during flight. Retrieving and Reading Messages: Highlight “MESSAGES” in the main menuand press the Right Menu Navigation button.
  • Page 176 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page AA -8 Delete Messages: After you have been prompted to send an acknowledgementreceipt you will be prompted with a delete option. Todelete the message you have just viewed, press the ‘1’ button. To save the message press the ‘2’ button.
  • Page 177 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page AA -9 Destination: The same code system as for Origin is used for Destinations. ETE: Estimated time En-route, this field will accept data in the format of hoursand minutes. This information will be used to calculatethe ETA displayed for flight tracking.
  • Page 178 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page AA -10 This page is left intentionally in blank Rev: 0 Date: Jul 17 Prepared by: TRI Checked by: TM...
  • Page 179 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page BB -1 APPENDIX B. WEIGHT AND BALANCE ReferSection VI in the AFM_L410UVP-E20. (6-2). Loading rules: • Crews must not solely rely on ground crew to ensure correct loading ofthe aircraft. •...
  • Page 180 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page BB -2 WEIGHT AND BALANCE LOADING FOR 19 PASSENGER CONFIGURATION Payload (kg) Arm (m) Moment (kg.m) -1.333 F.S. Forward baggage (max.100 kg) 0.103 F.S. CREW seats 1.235 F.S. Seat Row 1 1.995...
  • Page 181 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page BB -3 Rev: 0 Date: Jul 17 Prepared by: TRI Checked by: TM...
  • Page 182 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page BB -4 PAYLOAD AND FUEL MOMENT FOR 19 PASSENGER CONFIGURATION Moments listed are kg.m for weights located as shown Payload weight (kg) F.S. 0.103 m Crew seats 10.3 12.4 14.4 16.5 18.5...
  • Page 183 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 PageCC -1 APPENDIX C.NORMAL CHECKLIST ReferSection IV Normal Procedures in the AFM_L410UVP-E20. L410 UVP-E20 AFTER START call out NORMAL Capt. Overhead CB's CHECKLIST Ventilation Capt. GROUND ON / aligned Capt. STBY attitude indicator...
  • Page 184 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 PageCC -2 PAGE 2 AFTER TAKE-OFF LANDING call out call out Gear UP / Lights off Landing gear DOWN / Locked Flaps UP / Indicated Flaps SET / Indicated YAW Damper Yaw Damper...
  • Page 185 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 PageDD -1 APPENDIX D.AUTO-FEATHER CHECKS ReferSection IV Normal Procedures in the AFM_L410UVP-E20. Perform it before the first flight of the day. PROP FEATHERING circuit breaker........... AUT. BANK CONTROL circuit breaker ..........PCL ......................
  • Page 186 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 PageDD -2 TCL of the other engine ...............back to IDLE On the test panel of the left control panel: PROP FEATHERING AUTObutton ............ release On the overhead panel PROP FEATHERING circuit breaker......... switch OFF and back ON AUT.
  • Page 187 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 1 APPENDIXE.EMERGENCY AND ABNORMAL PROCEDURES General This Appendix is designed to provide pilots with standardized procedures based on AFM Emergency and Abnormal checklists. To streamline the transition from the type rating, to line training and the daily line operations, the procedures in this appendix follow the philosophy laid out on the Flight Crew Training Manual utilized by the crew during initial type rating course.
  • Page 188 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 2 be left open for the rest of the flight, unless further reset attempts are allowed according to the checklists. If the failure alert disappears, continue normal operation and record the event into the maintenance log.
  • Page 189 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 3 ***** PAGE INTENTIONALLY LEFT BLANK ***** Rev: 1 Date:JAN 18 Prepared by: LA Checked by : CLS...
  • Page 190 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 4 Cockpit Management In the event of an emergency or abnormality, checklists must be completed in the following order, if relevant: • Memory items; • Emergency/Abnormal checklist; • Normal checklist; and •...
  • Page 191 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 5 If emergency procedure requires memory items Command “MEMORY ITEMS“ Puts his hand or finger on appropriate control element or switch and reports his intention e.g. “LEFT POWER LEVER IDLE“...
  • Page 192 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 6 FIRE AND SMOKE DRILLS 2.1.1 Following items should be done without waste of time COCKPIT OR CABIN FIRE EC 20 Item Action > Oxygen Masks, Goggles PUT ON...
  • Page 193 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 7 FRONT BAGGAGE COMPARTMENT FIRE EC 20 Item Action > BAGGAGE COMPARTMENT PULL OUT FASTEN SEAT BELTS SWITCH ON DESCENT INITIATE AS REQUIRED COCKPIT WINDOWS OPEN AS REQUIRED BOTH Note: In case of fire or smoke in the cockpit proceed to a nearest suitable airport.
  • Page 194 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 8 EXCEEDING STRUCTURAL LIMITS AS OVERWEIGHT LANDING 2.1.2 In exceptional cases it is permitted to land with mass more than 6.400 kg or with fuel in wing tip tanks. Each this case must be recorded in the Airplane Log book and Technical Log Book.
  • Page 195 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 9 DISTRESS COMMUNICATIONS AND ALERTING ATC TO EMERGENCIES 2.1.4 When a pilots or crew encounters an emergency or distress situation they can simply call for assistance by contacting ATC on frequency in use or on Guard frequency...
  • Page 196 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 10 Transponder setting At the same time the aircraft transponder should be set accordingly: Mode A/C/S and codes 7700 for emergency – 7600 for loss of two-way radio communication –...
  • Page 197 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 11 INTENTIONALLY LEFT BLANK Rev: 1 Date:JAN 18 Prepared by: LA Checked by : CLS...
  • Page 198 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 12 EMERGENCY CHECKLISTS USING OF CHECK LISTS OF EMERGENCY PROCEDURES EC 2 AIRSPEEDS FOR SAFE OPERATION EC 2 POWERPLANT ENGINE FIRE ON GROUND EC 3 ENGINE FIRE EC 4 ENGINE FAILURE DURING TAKE-OFF (AT SPEED ≤V1) FLAPS 18°/0°...
  • Page 199 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 13 SMOKE COCKPIT OR CABIN FIRE EC 19 FIRE IN FRONT OR REAR BAGGAGE COMPARTMENT EC 20 Rev: 1 Date:JAN 18 Prepared by: LA Checked by : CLS...
  • Page 200 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 14 EC 2 USING OF CHECKLISTS OF EMERGENCY PROCEDURES USING OF CHECK LISTS OF EMERGENCY PROCEDURES The Check Lists of Emergency Procedures contain the abbreviated names of necessary procedures. For more details, refer to the corresponding part of Airplane Flight Manual.
  • Page 201 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 15 AIRSPEEDS FOR SAFE OPERATION EC 2 1. Rotation airspeedwith wing flaps in 18° or 0° position VR 18 or VR 0 - variable see section 5 of this AFM 2.
  • Page 202 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 16 EC 3 ENGINE FIRE ON GROUND Item Action The following items are valid for engine on fire before V1: > TCL´s IDLE > SPOILERS DEPLOY CM 1 >...
  • Page 203 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 17 If fire remains: > EXTINGUISHER SECONDARY push-butt. PUSH SEC. ADVISE CM 2 AIRCRAFT EVACUATION AS REQUIRED CM 1 BATTERY CM 1 Rev: 1 Date:JAN 18 Prepared by: LA...
  • Page 204 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 18 EC 4 ENGINE FIRE Item Action > ENGINE on fire DETERMINE BOTH The following items are valid for engine on fire: > FUEL STOP COCK/ EMERGENCY SHUT THROTTLE LEVER >...
  • Page 205 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 19 EC 5 ENGINE FAILURE DURING TAKE-OFF (AT SPEED ≤ V1) FLAPS 18°/ 0° Item Action ABORT THE TAKE-OFF ENGINE FAILURE DURING TAKE-OFF (AT SPEED > V1) FLAPS 18°...
  • Page 206 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 20 (b) If the inoperative engine propeller has not been feathered even after above measures had been taken then: > PCL of the inoperative engine FEATHER AIRSPEED min. V2, FLAPS 18 AUT.
  • Page 207 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 21 (b) If the engine operates at idle and other parameters correspond to idle power then: PROPELLER UNFEATHER USE of emergency fuel control circuit Rev: 1 Date:JAN 18 Prepared by: LA...
  • Page 208 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 22 ENGINE FAILURE DURING TAKE-OFF (AT SPEED > V1) FLAPS 0° EC 6 Item Action > TCL of both engines check TAKE OFF RATING > FAILED ENGINE DETERMINE BOTH...
  • Page 209 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 23 AIRSPEED V2 0 up to 1,500 ft (457 m) above runway INOPERATIVE ENGINE CHECK PARAMETERS (a) If the engine is fully stopped The following items are valid for inoperative engine:...
  • Page 210 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 24 EC 7 ENGINE FAILURE DURING MISSED APPROACH Item Action > TCL of both engines set TAKE OFF RATING > AIRSPEED min. V2, FLAPS 18 WING FLAPS > LANDING GEAR >...
  • Page 211 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 25 TCL of operating engine set continuous OEI rating AIRSPEED V2 0 up to 1,500 ft (457 m) above runway Accomplish the following procedures for inoperative engine: IDLE FUEL STOP COCK...
  • Page 212 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 26 EC 8 TWO ENGINES OFF Item Action *If possible IN FLIGHT ENGINE STARTING CHECK LIST (AB 7) * If unsuccessful FASTEN SEAT BELTS circuit breaker SWITCH ON PCL’S...
  • Page 213 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 27 EC 9 BOTH GENERATORS INOPERATIVE Item Action LH GENERATOR and RH GEN. CHECK SWITCHING ON switches on the overhead panel ALL CIRCUIT BREAKERS NOT SWITCH OFF MARKED WITH YELLOW STRIP BATTERIES DISCHARGING CURRENT FIND OUT AMPERES ..
  • Page 214 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 28 AUTOPILOT MALFUNCTION EC 10 Item Action > AIRPLANE CONTROL WHEEL GRASP FIRMLY > A/P DISC/TRIM INTER (A/P DISC) PRESS to disengage > AIRPLANE MANUAL FLIGHT OPERATIONS ELECTRIC TRIM MALFUNCTION...
  • Page 215 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 29 FDR FAULT EC 11 Item Action On the ground: RECORDER circuit breaker CHECK IN FLIGHT EXECUTION MMEL or MEL CM 1 In the air: FLIGHT* CONTINUE * After landing, report ground personnel...
  • Page 216 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 30 EC 12 AIR DATA SOURCE FAILURE Item Action As indicated by red X on airspeed, altitude or vertical speed field: > WRONG SIDE IDENTIFIED > ADC REVERT* DEPRESS *at wrong side >...
  • Page 217 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 31 EC 12 RADAR ALTIMETER FAILED Item Action Indicated by red RA FAIL on PFD: RADAR ALTIMETER CIRCUIT CHECK BREAKER IF OPEN RESET ONE TIME Rev: 1 Date:JAN 18...
  • Page 218 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 32 EC 13 FORCED LANDING Item Action Preparation: PLACE FOR LANDING SELECTED APPROACH SPEED MIN.V2 NOTIFY XPDR 7700 SAFETY HARNESS CONTR.LEVER FRONT(locked) POSITION EGPWS CIRCUIT BRAKER FUEL FROM THE WING TIP TANK TO THE MAIN...
  • Page 219 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 33 After impact , when aircraft stopped: EXTINGUSHER BOTH PUSH BOTH EVACUATION* INITIATE CM 1 *ON GROUN EMERGENCY EVACUATION CHECK LIST (EC 19) DC + AC GENERATORS Battery I. + II.
  • Page 220 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 34 EC 14 LANDING ON WATER Item Action LANDING GEAR FLAPS PASSENGERS PREPARE FUEL BURNOFF TO MIN. FORCED LANDING CHECKLIST (EC13) Rev: 1 Date:JAN 18 Prepared by: LA Checked by : CLS...
  • Page 221 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 35 LANDINGS WITH FAULTY LANDING GEAR EC 14 Item Action SOFT SURFACE FOR LANDING SELECTED MINIMUM LANDING TOUCH DOWN SPEED SPEED FORCED LANDING CHECKLIST (EC13) CAUTION IF POSSIBLE DO NOT LAND ON A HARD -SURFACED RUNWAY.
  • Page 222 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 36 *LANDING ON NOSE WHEEL AND ONE MAIN WHEEL NOTE BEFORE TOUCH DOWN, BANK THE AIRPLANE TOWARD THE EXTENDED MAIN WHEEL, AND KEEP THE BANK FOR AS LONG AS POSSIBLE BY MEANS OFF THE AILERONS AND PEDAL - OPERATING STEERING.
  • Page 223 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 37 RECOMMENDED PROCEDURES FOR EGPWS ALERTS IN FLIGHT EC 15 Item Action ACTIVATION OF THE VOICE WARNING " PULL UP , TERRAIN TERRAIN,PULL UP" or "OBSTACLE , OBSTACLE,PULL UP".
  • Page 224 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 38 If GLIDESLOPE alert > GLIDESLOPE path RESTORE. on back course app. EGPWS P/CANCEL PRESS Other emergencies( ditching or other off airport landings) TERR INHIBIT ON switch. Press. EGPWS CB.
  • Page 225 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 39 EGPWS CAUTION ANY OF THE FOLLOWING CONDITIONS IS REGARDED AS AN EGPWS CAUTIONARY ALERT: • ACTIVATION OF THE EGPWS “CAUTION TERRAIN”, “CAUTION OBSTACLE”, “TOO LOW TERRAIN”, “SINKRATE”, “DONT SINK”, “GLIDESLOPE”, “TOO LOW FLAPS” OR “TOO LOW GEAR”...
  • Page 226 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 40 OF THE TERRAIN AWARENESS AND ALERTING DISPLAY (TAD). *** CONTINUE AT NEX PAGE *** Rev: 1 Date:JAN 18 Prepared by: LA Checked by : CLS...
  • Page 227 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 41 PROCEDURE FOR GLIDESLOPE ALERTS: BELOW GLIDESLOPE ALERTS CONSIST OF “SOFT” AND “HARD” ALERTS BASED ON THE DEGREE OF GLIDESLOPE DEVIATION AND ALTITUDE. RESPOND TO THESE ALERTS AS NECESSARY TO CORRECT THE AIRCRAFT FLIGHT PATH BACK TO THE GLIDESLOPE CENTERLINE OR PERFORM A MISSED APPROACH.
  • Page 228 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 42 EC 16 TCAS WARNING Item Action TRAFIC ADVISORY: „TRAFIC,TRAFIC“ > LANDING LIGHTS > FASTEN SEAT BELTS > PCLs 1900 RPM > CHECK SAVE ALTITUDE RESOLUTION ADVISORY: „CLIMB,CLIMB or DESCENT,DESCENT“...
  • Page 229 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 43 *** CONTINUE AT NEX PAGE *** Rev: 1 Date:JAN 18 Prepared by: LA Checked by : CLS...
  • Page 230 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 44 The following Resolution Advisories require 2.5 seconds response time and up to 0.35 G. Aural Visual Crew response “INCREASE DESCENT, Follows “DESCEND” Indicates the vertical speed INCREASE DESCENT”...
  • Page 231 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 45 WINDSHEAR/MICROBURST EC 17 Item Action > TCL of both engines SET AS REQUIRED > PCL‘S MAX PRM > AIRSPEED MIN. V stall > A/C CONFIGURATION NO CHANGE >...
  • Page 232 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 46 STALL RECOVERY EC 17 Item Action (CLEAN CONFIGURATION) AP/FD DISENGAGE > > AIRPLANE CONTROL WHEEL GRASP FIRMLY > ATTITUDE LOWER NOSE > TCL’S AS REQUIRED > AFTER STALL RECOVERY...
  • Page 233 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 47 EC 18 BOMB ON BOARD Item Action LOAD FACTOR AVOID LANDING GEAR DOWN FLAPS HANDLE BOMB CAREFULY AVOID SHOCKS Place bomb near cargo door preferably in a bag attached to the door handle, surround it with damping material.
  • Page 234 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 48 EC 19 EMERGENCY DESCENT Item Action > FASTEN SEAT BELTS SIGN > TCL’S IDLE > TRANSPONDER SET 7700 > ATC / PAX NOTIFY DESCENT (CHECK MSA) ROD as REQUIRED >...
  • Page 235 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 49 EC 20 COCKPIT OR CABIN FIRE Item Action > Oxygen Masks, Goggles PUT ON BOTH FASTEN SEAT BELTS circuit breaker DESCENT INITIATE AS REQUIRED SOURCE OF FIRE DETERMINE...
  • Page 236 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 50 INTENTIONALLY LEFT BLANK Rev: 1 Date:JAN 18 Prepared by: LA Checked by : CLS...
  • Page 237 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 51 ABNORMAL PROCEDURES MISSED APPROACH ONE ENGINE INOPERATIVE Note: configuration for GA - feathered inop engine and flaps in position 18°. Command „GO AROUND, MAX POWER“. Sets MAX T/O POWER on operative engine and transits aircraft into climbing.
  • Page 238 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 52 ABNORMAL CHECKLISTS POWERPLANT ENGINE SHUTDOWN IN FLIGHT AB 4 MISSED APP WITH ONE ENGINE INOPERATIVE AB 5 LANDING WITH ONE ENGINE INOPERATIVE AB 6 IN FLIGHT ENGINE STARTING...
  • Page 239 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 53 LANDING GEAR EMERGENCY EXTENSION OF LANDING GEAR AB 27 FAILURE OF LANDING GEAR RECTRACTION AB 28 DEFLATED TIRE ON WHEEL AB 29 ANTIICING/DEICING ONE SECTION OF PNEUMATIC AIRFRAME DEICING FAILURE...
  • Page 240 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 54 EFIS DCU FAILURE AB 39 ATT/PITCH/ROLL MISCOMPARE AB 40 ASPD/ALT COMPARATION AB 41 XBUS COMPARATION AB 42 BUS I(II) 26V AC FAULIRE AB 43 NAV/GPS LOSS OF GPS/SBAS NAV DATA...
  • Page 241 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 55 ENGINE SHUTDOWN IN FLIGHT AB 4 Item Action TCL of operating engine set continuous OEI rating or lower, as required Procedure on the controls of the opposite engine to be shutdown: IDLE MANUAL FEATHER.
  • Page 242 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 56 MISSED APPROACH WITH ONE ENG. INOPERATIVE AB 5 Item Action CONDITION - Flaps 18° or 42° Inop. Engine - feathered IAS at or above 84 KIAS TCL of operating engine...
  • Page 243 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 57 LANDING WITH ONE ENGINE INOPERATIVE AB 6 Item Action At a height of 50 ft (15 m) above runway: AIRSPEED VREF, FLAPS 42 IDLE At a height of 10 ft (3 m) above runway:...
  • Page 244 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 58 IN FLIGHT ENGINE STARTING AB 7 Item Action The sequence is the same as in ground starting. During the starting cycle, switch off all except the most essential electric equipment.
  • Page 245 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 59 COMPRESSOR SURGING AB 8 Item Action IDLE If the ITT rise continues: FUEL STOP COCK/EMERGENCY SHUT THROTTLE* NOTE AFTER THE ENGINE HAS STOPPED, TAKE THE ACTION SPECIFIED IN...
  • Page 246 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 60 METAL CHIPS IN THE OIL AB 10 Item Action (CHIP signal is illuminated) Parameters of affected engine CHECK ● Continue the flight while paying particular attention to the parameters of affected engine.
  • Page 247 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 61 USE OF EMERGENCY FUEL CONTROL CIRCUIT AB 11 Item Action IDLE ISOLATION VALVE AMBER ISOLATION VALVE CHECKED ON BOTH LIGHT FUEL STOP COCK/ EMERGENCY move slowly THROTTLE LEVER...
  • Page 248 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 62 BETA RANGE AND PROPELLER PITCH LOCK SIGNALLING AB 12 Item Action a) On final approach, When the amber BETA RANGE cell (in the Engine section of the CWD) comes on...
  • Page 249 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 63 BETA RANGE AND PROPELLER PITCH LOCK SIGNALLING AB 12 c) During other phases of the flight, When the amber BETA RANGE cell (in the Engine section of the CWD) comes on but amber PROPELLER PITCH LOCK cell does not come on, it is false signaling.
  • Page 250 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 64 FAILURE OF AUTOMATIC SWITCHING ON FUEL TRANFER FROM WING-TIP- AB 12 TANKS Item Action WING TIP TANK FUEL TRANS. switch for the affected side GREEN LIGHT FUEL TRANFER...
  • Page 251 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 65 AB 13 LOW FUEL LEVEL Item Action AVOID EXCESSIVE A/C ATTITUDES LAND AS SOON AS POSSIBLE FUEL LEAK AB 14 Item Action (a) If fuel leakage is observed soon after take-off: Return to airport of departure.
  • Page 252 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 66 AB 15 FAILURE OF ONE DC - GENERATOR Item Action DC GENERATOR switches CHECK ON DC GENERATOR OFF than ON switch of failed unit If DC GENERATOR is fault:...
  • Page 253 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 67 FAILURE OF ONE AC - GENERATOR AB 16 Item Action AC GENERATOR LH or RH switches CHECK ON AC GENERATOR OFF than ON switch of failed unit If AC GENERATOR is fault:...
  • Page 254 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 68 FAILURE OF BATTERY CIRCUIT AB 18 Item Action BATTERY switches CHECK ON VA METER selector switch Set first to BAT I VA and BAT II VA position Charging of both batteries...
  • Page 255 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 69 BATTERY OVERHEATING AB 19 Item Action BATTERY I (II) switch EMERGENCY EXTENSION OF WING FLAPS 18° AB 20 Item Action WING FLAPS control lever FLAPS 18° CM 2...
  • Page 256 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 70 WING FLAPS RETRACTING AB 21 Item Action Real position of the flaps CHECK If the flaps have remained in the take-off position (18°): Maintain climb with airspeed 124 KIAS...
  • Page 257 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 71 SPONTANEOUS EXTENSION OF ONE ABC-TAB AB 22 during TAKE-OFF Item Action AILERONS LEVEL THE AIRPLANE AUTO-BANK CONTROL switch If the ABC tab retracts: FURTHER FLIGHT CONTINUE FLIGHT If the ABC tab does NOT retract:...
  • Page 258 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 72 EMERGENCY EXTENSION OF LANDING GEAR AB 24 Item Action LANDING GEAR lever DOWN LANDING GEAR EMERGENCY EXTENSION lever DOWN CM 2 EMERGENCY HYDRAULIC PUMP Pump until the 3 green lights...
  • Page 259 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 73 FAILURE OF THE LANDING GEAR TO RETRACT AFTER TAKE - OFF AB 25 Item Action If the landing gear fails to retract either all green lights or all red lights do not go off...
  • Page 260 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 74 DEFLATED TIRE ON ONE WHEEL AB 26 Item Action During take-off: AIR SPEED BELOW OR EQUAL V1 ABORT TAKE-OFF Relieve the load on the wheel with faulty tire and use reverse power as required.
  • Page 261 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 75 ONE SECTION OF PNEUMATIC AIRFRAME DEICING FAILURE AB 27 Item Action 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 30°C ABOVE...
  • Page 262 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 76 FAILURE OF PNEUMATIC DEICING RELAY AB 29 Item Action TEST A; B; C SECTION PUSH BUTTON CM 2 If only one of the lights does not come on when it is tested, this means a burnt out bulb filament.
  • Page 263 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 77 PROPELLER DEICING FAILURE AB 31 Item Action Simultaneous coming on of both propeller deicing cells on the cwd means main circuit failure of propeller deicing cycling switch: PROP DEICING switch...
  • Page 264 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 78 STATIC HEAD FAILURE AB 32 Item Action STATIC PRESSURE I AND II CHECK ON CM 2 (the green lights in these push buttons must stay on) If the LH INSTRUMENTS are affected:...
  • Page 265 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 79 PITOT HEAD FAILURE AB 33 Item Action If the LH INSTRUMENTS are affected: PITOT PRESSURE black cock POSITION II CM 1 If the RH INSTRUMENTS are affected: AUTOPILOT...
  • Page 266 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 80 ENGINE FAILURE (AUTOPILOT COUPLED) AB 35 Item Action DISENGAGE AIRPLANE RUDDER AND TRIM MANUALLY AILERON AXES Follow the basic Airplane Flight Manual engine inoperative procedures. CAUTION IF RUDDER TRIM CANNOT BE MAINTAINED WHEN POWER IS CHANGED DURING AN ENGINE INOPERATIVE COUPLED APPROACH, DISENGAGE AUTOPILOT AND CONTINUE APPROACH MANUALLY.
  • Page 267 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 81 DCU FAILURE AB 36 Item Action DCU CIRCUIT BREAKER RESET* NOTE In the event of a total failure of the DCU the TAWS, TCAS and Flight Director information will not be displayed on either of the pilot's PFD’s.
  • Page 268 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 82 DCU FAILURE AB 37 *** CONTINUE BELOW *** * If amber “XBUS” message is displayed: PFD I, II CIRCUIT BREAKER CHECK* *IF OPEN, RESET * If Amber BUS I (II) 26V AC signal cell lights on the central warning display–...
  • Page 269 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 83 LOSS OF GPS/SBAS NAVIGATION DATA AB 38 Item Action NAVIGATION USE ALTERNATE SOURCES** **If no alternate navigation USE GTN sources DEAD RECKONING (DR) MODE NOTE All information normally derived from GPS will become less accurate over time.
  • Page 270 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 84 LOSS OF COM RADIO TUNING FUNCTIONS AB 40 Item Action IF ALTERNATE COM IS USE ALTERNATE COM AVAILABLE DATA SOURCE - HEADING SOURCE INOPERATIVE OR CONNECTION TO AB 41...
  • Page 271 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 85 AUDIO PANELS FAILURE AB 43 Item Action NOTE The audio will only be heard in the left ear of a stereo headset in the emergency mode. In case of both audio panels are in emergency mode do not attempt to transmit at the same time because both crewmembers are connected to the COM 1 and modulation may be compromised.
  • Page 272 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 86 FAILURE OF AIRCONDITIONING SYSTEM AB 45 Item Action FANS circuit breaker SWITCH - ON VENTILATION control lever FULLY OPEN AIRCONDITION triple-throw switch FANS position In case of abnormal function of Airconditioning system...
  • Page 273 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 87 TCAS ADVISORY AB 46 Item Action RECOMMENDED PROCEDURES FOR RESOLUTION ADVISORIES IN FLIGHT CAUTION ALWAYS ATTEMPT TO VISUALLY CLEAR AIRSPACE BEFORE MANEUVERING YOUR AIRCRAFT IN RESPONSE TO A TCAS ADVISORY. DO NOT OVERREACT TO A RESOLUTION ADVISORY. FLY ONLY THE VERTICAL SPEED COMMANDED.
  • Page 274 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 88 EGPWS Caution „SINK RATE“ – descent rate must be decreased, until caution of GPWS is finished Caution „TERRAIN,TERRAIN or TERRAIN AHEAD.TERRAIN AHEAD“ – flight crew must check its position and distance from terrain –...
  • Page 275 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 89 – sets PCLs to MAX according to PF command, adjusts engine power to Maximum according to engine parameters and reports „POWER SET“ – in case of command „FLAPS 18“, sets the flap handle to 18 and after this position is reached (according to flap position indicator) reports „FLAPS 18 SET“...
  • Page 276 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 90 Caution „DONT SINK“ – flight crew interrupts descend and increases engine power – if the caution lasts transits into climbing Caution „TOO LOW TERRAIN“ – In day and in VMC conditions with sufficient visual reference must not take in to account such caution –...
  • Page 277 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 91 ACAS / TCAS The following Resolution Advisories require 2.5 seconds response time and up to 0.35 G. Aural Visual Crew response “INCREASE Follows a “DESCEND” advisory. Indicates the vertical speed which MUST...
  • Page 278 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 92 CAUTION ALWAYS ATTEMPT TO VISUALLY CLEAR AIRSPACE BEFORE MANEUVERING YOUR AIRCRAFT IN RESPONSE TO A TCAS ADVISORY. DO NOT OVERREACT TO A RESOLUTION ADVISORY. FLY ONLY THE VERTICAL SPEED COMMANDED. USING HIGHER VERTICAL SPEED THAN THAT COMMANDED ON THE RA/VSI IS NOT BETTER.
  • Page 279 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 Page EE - 93 WINDSHEAR I the event of reported windshear, increase the APP speed to compensate for loss of speed that is common for a low –level windshear. It is recommended to use Flaps 18° for landing. In case of several windshear or non-stabilized flight attitude be prepared to adopt GO-AROUND procedure.
  • Page 280 Document No.: Standard Operating Procedures SOP-L410-0 L410 UVP-E20 PageFF -1 APPENDIX F.PROPELLER PITCH LOCK ReferSection IV Normal Procedures in the AFM_L410UVP-E20. Perform it before the first flight of the day, test must be performed during propeller unfeathering. TCL ..................IDLE PCL ..................

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