SusiAir L410 UVP-E20 Standard Operating Procedures Download

Page: 254 / 280

Standard Operating Procedures

L410 UVP-E20

Document No.:

SOP-L410-0

Page EE - 68

Rev: 1

Date:JAN 18

Prepared by: LA

Checked by : CLS

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

CM2

Charging of both batteries

CHECK

CM2

BATTERY switch for battery which
is not charged

OFF

CM2

Summary of Contents for L410 UVP-E20

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

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Page 3: ...ASIPudjiastuti Aviation Susi Air DOCUMENT CONTROL Applicability All Operations of PT ASI Pudjiastuti Aviation Prepared by Luca Amante LA Checked by Colin Lindsay Smith CLS Document Control This docum...

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Page 6: ...Standard Operating Procedures L410 UVP E20 Document No SOP L410 1 Prelim Page vi Rev 1 Date Jan 18 Prepared by LA Checked by CLS This page left blank intentionally...

Page 7: ...g Procedures L410 UVP E20 Document No SOP L410 1 Prelim Page vii Rev 1 Date Jan 18 Prepared by LA Checked by CLS RECORD OF REVISIONS Rev No Revision Date Date Inserted By Signature 0 July 2017 Initial...

Page 8: ...evisions insert pages adjacent to the pages affected in accordance with filling instructions 3 Insert temporary revision number issue date date inserted name and sign 4 When a normal revision or anoth...

Page 9: ...ge Prelim Page vi 0 July 2017 RECORD OF REVISIONS Prelim Page vii 1 January 2018 RECORD OF TEMPORARY REVISIONS Prelim Page viii 0 July 2017 LIST OF EFFECTIVE PAGES Prelim Pages ix and x 1 January 2018...

Page 10: ...REV DATE CHAPTER 5 DEPARTURES Pages 5 1 thru 5 30 1 January 2018 CHAPTER 6 CRUISE Pages 6 1 thru 6 4 0 July 2017 CHAPTER 7 ARRIVAL Pages 7 1 thru 7 37 0 July 2017 CHAPTER 8 AFTER FLIGHT Pages 8 1 thr...

Page 11: ...Standard Operating Procedures L410 UVP E20 Document No SOP L410 1 Prelim Page xi Rev 1 Date Jan 18 Prepared by LA Checked by CLS...

Page 12: ...ENT CONTROL Prelim Page iii CONTROL PAGE Prelim Page v RECORD OF REVISIONS Prelim Page vii RECORD OF TEMPORARY REVISIONS Prelim Page viii LIST OF EFFECTIVE PAGES Prelim Pages ix thru x TABLE OF CONTEN...

Page 13: ...ther Checks Page 3 2 3 2 2 Propeller Pitch Lock Test Page 3 3 3 3 Crew Conduct and Sterile Environment Page 3 4 3 4 Division of Workload Page 3 5 3 4 1 Taxi Page 3 5 3 4 2 Take off Climb Page 3 5 3 4...

Page 14: ...Cockpit Cabin Preparation Page 4 7 4 5 Fuelling Page 4 7 4 5 1 Fuel Type Page 4 8 4 5 2 Fuel Specific Gravity Page 4 8 4 5 3 Requests For Fuel Page 4 8 4 5 4 Fuel Draining Page 4 8 4 6 Aircraft Doors...

Page 15: ...11 2 Radio Nav Setup Page 5 16 5 12 Receiving an ATC Departure or Arrival Clearance Page 5 16 5 13 Bluesky Satellite Tracking Page 5 17 5 14 Definitions Page 5 18 5 15 Line up Flow items Page 5 19 5 1...

Page 16: ...f Descent Page 7 2 7 3 Holding Page 7 2 7 4 Flap Gear Selection Page 7 3 7 4 1 Speed for Configuration changes Page 7 3 7 5 Approach Category Page 7 4 7 6 Navigation Setup for Approaches Page 7 4 7 7...

Page 17: ...g VS Page 7 20 7 18 6 Minimum Descent Altitude MDA H Page 7 21 7 19 CANPA Callout Table Page 7 22 7 20 Missed Approach Page 7 25 7 20 1 Missed Approach Callout Table Page 7 25 7 21 Circling Approach P...

Page 18: ...ABNORMAL AND EMERGENCY PROCEDURES 9 1 Types of Checks Page 9 1 9 1 1 Immediate Action Page 9 1 9 1 2 Checklist Items Page 9 1 9 2 PF and PM Duties During an Emergency Situation Page 9 1 9 3 Emergency...

Page 19: ...ting Procedures L410 UVP E20 Document No SOP L410 1 Prelim Page xix Rev 1 Date Jan 18 Prepared by LA Checked by CLS APPENDICES E Emergency And Abnormal Procedures Page EE 1 to EE 93 F Propeller Pitch...

Page 20: ...Standard Operating Procedures L410 UVP E20 Document No SOP L410 1 Prelim Page xx Rev 1 Date Jan 18 Prepared by LA Checked by CLS This page left blank intentionally...

Page 21: ...ce over any other regulations and CASRs provided the manual is approved by the DGCA For operations outside of Indonesia the laws of the body having legislative authority over aviation matters where th...

Page 22: ...operating procedure technique or maintenance practice which may result in damage to equipment if not carefully followed WARNING An operating procedure technique or maintenance practice which may resul...

Page 23: ...ual The holder of each copy of this manual is responsible for ensuring that any approved revisions are included in the manual The Operations Manager will be responsible for raising suitable revisions...

Page 24: ...n Number A new List of Effective Pages which shows the status of each page of the Manual Revisions to the text of the SOP Manual shall have a revision marker set in the right margin adjacent to the re...

Page 25: ...Precision Approach also referred to as CDFA Constant Descent Final Approach CAS Crew Alerting System CASRs Civil Aviation Safety Regulations Cat Aircraft Approach Category CB s Circuit breakers CFIT C...

Page 26: ...on Display MORA Minimum Off Route Altitude MSA Minimum Safe Altitude MSL Mean Sea Level NAV1 Navigation Radio number 1 NAV2 Navigation Radio number 2 NDB Non Directional Beacon Ng Compressor RPM in pe...

Page 27: ...ing System TCL Throttle Control Lever or Throttle Lever TFC Traffic Selector TKE Track Angle Error TOPO Topographic Display map mode TRK Track VDP Visual Descent Point VCALC Vertical Calculator VOR Om...

Page 28: ...flight descent OPERATING MANEUVERING SPEED Vo 147 KIAS Full application of rudder and aileron controls including maneuvers that involve angles of attack near the stall should be not be performed above...

Page 29: ...PS OPERATING SPEED 135 KIAS MAXIMUM PERMISSIBLE SPOILER EXTENSION SPEED VSPOIL 111 KIAS MINIMUM CONTROL SPEED for take off run VMCG 66 KIAS is same for flaps 0 and 18 MINIMUM CONTROL SPEED for take of...

Page 30: ...EED VALUES VERSUS TAKE OFF WEIGHT wing flaps 18 Max take off weight Measurement method Flaps position Level of noise dB A 6 600 kg CS 36 Am 2 18 83 1 ICAO Annex 16 Chapter 10 WEIGHTS Maximum ramp weig...

Page 31: ...GHT 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 WITH THE LIMITATION GIVEN IN SECTION 2...

Page 32: ...NDING 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 1 The dimensions ar...

Page 33: ...18 Prepared by LA Checked by CLS FLOOR LOADING LIMITATIONS FOR PASSENGER VERSION Maximum load on baggage compartments Rear 150Kg Front 100Kg Maximum specific load on the floors of Baggagecompartments...

Page 34: ...Maximum weight of the cargo in thecontainer 1 000 kg Maximum weight of the cargo without the separator installed 500 kg Maximum weight of the cargo in one section with the separator installed 500 kg...

Page 35: ...ARGO COMPARTMENT Maximum load of the extended baggage cargo compartment 230 kg 507 lb Maximum load of the small extended baggage cargo compartment 230 kg 507 lb Maximum specific load on the floor 400...

Page 36: ...upants including the crew is 19 The maximum permissible number of occupants including the crew for cargo version is 3 FOR 19 PASSENGERS VERSION The maximum permissible number of occupants including th...

Page 37: ...with fuel pumps inoperative is 13 120 ft The maximum permissible pressure airport altitude for take off and landing is 13 120 ft AIR TEMPERATURE LIMITATION The airplane is admitted for operation at a...

Page 38: ...e steady component of cross wind from dry and wet take off and landing pawed runways 25 kts from unpaved grass strips 20 kts from paved take off and landing runways with a layer of water 10 kts TAIL W...

Page 39: ...onstrated 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...

Page 40: ...limb speed with the aircraft in clean configuration torque shall not exceed 100 ITT not exceeding 720 C Cruise Cruise propeller RPM setting is 1700 RPM and Ng not exceeding 98 4 Maximum cruise ITT sha...

Page 41: ...eed to use VS for a smooth level off as the ALT capture logic allows for high rates of climb and descent Flap Extension Flaps can be extended and retracted while the AP is engaged and maximum flap ext...

Page 42: ...r LOC signals The NAV annunciators located above this button will annunciate NAV ARM until the automatic capture sequence is initiated then NAV will be annunciated The sequence of the PFD display annu...

Page 43: ...l annunciator lights tests the roll and pitch rate monitors tests the auto trim fault monitor checks the manual trim drive voltage and tests all autopilot valid and dump logic If the preflight test is...

Page 44: ...hich will provide up or down pitch command changes While in Pitch Attitude Hold mode will adjust the pitch attitude at a rate of 0 7 deg sec While in Altitude Hold mode will adjust the altitude at a r...

Page 45: ...o divert i e weather below non precision minima or no weather forecast available fuel should be loaded to land with no less than 225Kg at the alternate 2 The above are minimum fuel requirements and mu...

Page 46: ...NDITIONS MINIMUM AIRSPEEDS Flaps retracted position 0 VREF 7 KIAS Flaps extended position18 VREF 7 KIAS For VREF airspeed see section 5 of the AFM WARNING MAXIMUM FLAP DEFLECTION IN ICING CONDITION IS...

Page 47: ...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 If there is still no response INCAPACITATION must...

Page 48: ...y the FO as appropriate On completion of a checklist the FO willverbally confirm that the checks are complete E G TAXI CHECKLIST COMPLETE 3 2 Operating the Checklist At the appropriate time the PF sha...

Page 49: ...that the item has been carried out and give theprescribed response Where the checklist response is nominated as Set or As Required theresponse shall be appropriate to the situation Responding As Requi...

Page 50: ...y way with the conduct of those duties Activities such as eating meals paperwork and engaging in non essential conversations during critical phases of flight are not permitted Both pilots shouldmainta...

Page 51: ...e controlled by the PF when the autopilot is engaged and by the PM when the Autopilot is disengaged During take off the throttle control levers are the responsibility of the captain regardless of who...

Page 52: ...truments must continuously be monitored by both pilots 3 5 Crew Responsibilities Refer to the Operations Manual Section 9 3 6 Checklist Format Preflight internal and external checks are designed to be...

Page 53: ...ATURE CELSIUS FUEL AND FUEL FLOW KILOGRAMS WEIGHT KILOGRAMS POSITION HDDD MM MM HDDD MM SS S BARO TRANSITION ALERT OFF AIRSPACE ALERTS ALTITUDE 200 default ALL OTHERS OFF AUDIO ALERT FEMALE MFD DATA B...

Page 54: ...FFIC TOPO TERRAIN and AIRWY ON MAP ORIENTATION HDG UP AUTO ZOOM OFF MAX LOOK FWD 30 min MIN LOOK FWD 5 min TIME OUT 0 min LAND DATA ON TRACK VECTOR ON WIND VECTOR ON 2 MIN NAV RANGE RING ON TOPO DATA...

Page 55: ...LS AVIATION ACTIVE FPL 2000NM ACTIVE FPL WPT MED 2000NM LARGE APT LRG 500NM MEDIUM APT MED 300NM SMALL APT MED 100NM SAFE TAXI NA 3NM RWY EXTENSION 30NM INT WAYPOINT LRG 30NM NDB WAYPOINT MED 30NM VOR...

Page 56: ...AILROAD 30NM LARGE CITY SMALL 800NM MEDIUM CITY MED 100NM SMALL CITY MED 50NM STATE PROV MED 1500NM RIVER LAKE SMALL 200NM USER WAYPOINT LRG 150NM NOTE The DCLTR can be used to remove unnecessary data...

Page 57: ...hts shall always be used when taxiing and remain on until aminimum of 2 000 feet AGL has been reached Theyshall be extinguished when above 2 000 feet or clear of traffic for nightoperations On descent...

Page 58: ...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 CLOUD...

Page 59: ...avigators and Garmin approved GPS SBAS antennas The GTN navigation system is installed in accordance with AC 20 138D The GTN system and associated navigation interface in this airplane have the follow...

Page 60: ...n the home page The GTN 650 750 unit displays only the traffic advisory information The traffic altitude filter is possible to display on PFD and GTN 650 750 independently to each other To choose alti...

Page 61: ...awareness in flight The electronic map is an aid to navigation and it is designed to facilitate the use of authorized government charts not replaced them Land and water data is provided only as gener...

Page 62: ...A Checked by CLS 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...

Page 63: ...A push button and BARO SET MINIMUMS knob on the display control panel The radar altimeter shall be set at 2 500 feet before departure and remain set throughout the flight except as required for arriva...

Page 64: ...idance TAWS isintended only to enhance situational awareness TAWS provides the following alerts 1 Forward Looking Terrain Avoidance FLTA Reduced Required Terrain Clearance RTC Reduced Required Obstacl...

Page 65: ...ltitude feet Flight Phase Level Flight Descending En Route 700 500 Terminal 350 300 Approach 150 100 Departure 100 100 NOTE The TAWS uses Geometric Altitude as its reference altitude GPS calculatedalt...

Page 66: ...ht Into Terrain FIT System issues an alert when the airplane is too low with respect to terrain based on landing gear status flaps position and groundspeed When flaps extension is not expected Flap ov...

Page 67: ...1 Date JAN 18 Prepared by LA Checked by CLS 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 al...

Page 68: ...Standard Operating Procedures L 410 UVP E20 Document No SOP L410 0 Page 3 22 Rev 1 Date JAN 18 Prepared by LA Checked by CLS This page is left intentionally in blank...

Page 69: ...ould decide and define if they willautomatically take immediate control as PF in an emergency situation The pre flight briefing should cover a discussion of Flight plan departure route takeoff weight...

Page 70: ...nd theCaptain will call MY CONTROLS and immediately move the throttle levers TCL to idle and apply brakes as required Reverse thrust and spoilers can be used at Captain discretion 1 The Captain will a...

Page 71: ...identify and confirm the engine failedand ensure that the auto Feather has engaged In the event that the Auto Feather does not activate crew will ensure that the propeller is manually feathered After...

Page 72: ...wer setting charts MSA Minimum IFR altitude from previous waypoint to that waypoint Can be a Grid MORA MSA Airway MEA etc TAS Defaults are 145 for CLB 200 below 10000 196 above 10000 Wind kts Enter av...

Page 73: ...lternate Doc No ASI OFP 2012 08 g Reg Continge ncy Cruise Wind Dir Mag Speed Type L410 Holding PIC Signature 000 0 VFR IFR Dispatch Fuel Fuel On Board DEP Sched Off POB OUT TO WT OFF TO CG ARR ON LDG...

Page 74: ...e Captain does the walkaround The FO conduct the emergency exits equipement inspection and the prepares the paperworks aircraft logbook flight plan weight balance etc After each sector of the day a br...

Page 75: ...ling procedures can be found in the Operations Manual The following is a supplement to those existing policies andprocedures for the L410UVP E20 If the crew is present when fuelling is taking place th...

Page 76: ...ible 4 5 4 Fuel Draining Fuel must be drained from ALL drain points before the first flight of the day if contaminants are found EVERY drain pointmust be drained until there is no evidence of contamin...

Page 77: ...ere there are no critical items and therefore the FO does the flow and then reads the checklist after Captain instruction 4 8 Before Start Call and Response Before engine start both crew will make sur...

Page 78: ...nce Starter ON Monitor atillumination of limiter active cell Announce Limiter Active Monitor At first indication of oil pressure on selected engines oil pressure gauge Announce Oil pressure rising Mon...

Page 79: ...normal Voltage atillumination of engine starting cell Announce Starter ON Monitor atillumination of limiter active cell Announce Limiter Active Monitor At first indication of oil pressure on selected...

Page 80: ...APT Limiter Active Whenvoltsdrop FO Voltdrop v At first indication of oil pressure on selected engines oil pressure gauge CAPT Oil pressure rising At first indication of Ng CAPT Ng rising At first ind...

Page 81: ...Prop 920 60 RPM Torque At least 8 Oil Temp Min 20 C Oil pressure 1 2 Kp cm2 After the start procedures of both engine has been succesfully accomplished both pilots carry out separate flows for the se...

Page 82: ...ti Skid FLAPS WX radar Departure Emerg Briefing GND staff ext power Trims Reverse Latch Spoiler ABC Autofeather Steering windshield heat Autopilot transfer 4 10 1 AFTER START ITEMS CM 1 CM 2 DC GEN LH...

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Page 84: ...BETA RANGE cell coming on when TCL is moved from idle power to reverse power position PCL is set to fine pitch During taxing check turn and bank indicator function on attitude indicator on the PFD To...

Page 85: ...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 performancecons...

Page 86: ...eriod 35 to 50 sec the ATT and HDG flags will be in view but will clear after a successful initialization Prior to takeoff if the two headings disagree but are not slewing away from the airplane headi...

Page 87: ...oring engine parameters instruments and checking the controls The Captain will call for the appropriate items and the FO will carry out the actions as explained below Captain First Officer ITEM ACTION...

Page 88: ...l frequency Once Taxi Clearance has been obtained the Captain will switch the taxi light on and askfor the parking brakes to be released Prior commencing taxi both crew shall keep good lookout on both...

Page 89: ...he 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 All other times it sh...

Page 90: ...cards o Brief details of flight duration level weather enroute etc Normally this briefing shall be in Indonesian language If both English speakingand Indonesian speaking passengers are on board the b...

Page 91: ...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 Kami moh...

Page 92: ...oyed toovercome them It is recommended you transfer control of the aircraft before beginningthe brief Briefing structure PF must display Flight Plan page on the GPS Briefing commences with PF reading...

Page 93: ...Standard Operating Procedures L410 UVP E20 Document No SOP L410 1 Page 5 10 Rev 1 Date JAN 18 Prepared by LA Checked by CLS 5 8 1 Briefing Cards...

Page 94: ...possibility of windshear in the event we encounter windshear we will review crew coordination for windshear Turbulence Wind X wind Rain runway contamination Use of separator vane Reduced visibility Lo...

Page 95: ...lity of a missed approach Non ILS approaches Vertical profile monitoring Offset approaches Runway characteristics People and animal incursions on runways Night Crew Airport familiarity Experience leve...

Page 96: ...20 set on the CDI with GPS selected Initial Altitude isset to 9500 ft Terrain Grid MORA 12 300 Weather Rain we will keep the windscreens on until clear of rain Operational shortfield takeoff technique...

Page 97: ...recommended configuration for flying operations GPS is the primary method of navigation however all applicable navaids shall be tuned and identified on GTN 750 650 It is recommended to have the approp...

Page 98: ...hat the planned cruising altitude Once the aircraf is airborne Flight Director can be selected by pressing CWS or by selecting the appropriate mode The flight director modes of operation are the same...

Page 99: ...rried out prior to receiving an ATC clearance asclearances are generally not given until taxiing for departure or whenapproaching the airport for arrival This is to allow for a more thorough brief ina...

Page 100: ...rk which guarantees worldwide availability ofsignal with no blank spots All Bluesky installations consist of a modem unit installed in the remote avionicscompartment as well as a control head and ACH1...

Page 101: ...BRG 1 NAV 1 2 GPS None and frequency if app BRG 2 NAV 1 2 GPS None and frequency if app Initial Alt eg 9 500 feet as read on AMS Squawk Assigned or in absence select 1200 VFR Eg CDI GPS intial course...

Page 102: ...cond step is done once the aircraft is lined up with the runway centreline LINE UP C R Crew shall carry out the lineup checklist at the holding point beforeenetering the active runway NOTE Be aware of...

Page 103: ...minate PM Auto featherarmed Airspeedindication PM Airspeedalive Airspeed 60 KIAS PM 60 knots PF Checked At V1 Captain removes hand from the throttle levers PM V1 At Vr PM Rotate At first indication of...

Page 104: ...speed above 15 to 20 KIAS use rudder nose wheel and upwind ailerons deflection as required to keep runway centerline Rudder deflection decreases with increasing speed Required ailerons deflection can...

Page 105: ...Above 400 feet AGL and 100 KIAS raise the flaps PF Flapsup PM Flaps up selected When the flaps are indicating up PM Flaps up indicated Once the flaps are up while accelerating to 120 KIAS engage the Y...

Page 106: ...climbing towards rising terrain and a steeper climb rate is required crew shall use Vx 104 KIAS best angle of climb airspeed NOTE To conserve the airframe life it is recommended to apply TCL setting o...

Page 107: ...w shall set the missed approach altitude 5 Where no FAF exists crew shall set minimums upon leaving the last level segment When within 1 000 feet of the selected altitude the altitude alerter will giv...

Page 108: ...pe captured Any subsequent selections in the form of mode annunciations must beannounced by the PF Eg VS down 500 to which the PM should respond check Prior to disengagement the PF shall call disconne...

Page 109: ...pilot Engagement The airplane must be trimmed before in flight autopilot engagement AP Button PRESS Check AP and YD annunciation on PFD I II If no mode is selected at the time of autopilot engagement...

Page 110: ...ll be used with the corresponding annunciations in theAFCS status box Available LateralModes Annunciator Callout Armed FDMode GPS GPS NAV GPSAPPR GPS Approach APPR LOC Localizer APPR VOR VOR NAV APPR...

Page 111: ...eedModes Annunciator Callout ArmedFD Mode ASEL CAP or ALT SEL Altitude preselected captured Capturing altitude ASEL ALTHOLD Altitude Hold mode captured Altitude Hold ALT hold GA GoAround mode GA GS Gl...

Page 112: ...Monitoring Select Heading mode Heading mode selected Select Indicated Air Speed Indicated Air Speed Selected Arm Nav Mode Nav Mode Armed Select Flight Director Flight Director Selected Select Alt hol...

Page 113: ...en to be outside tolerances The following system of cross checking altimeters during flight is mandatory Once an altimeter setting is received the PM shall initiate the call out For eg altimeter 1012...

Page 114: ...RANSFER The following procedure must be used to transfer the Autopilot to the alternate steering source RH or LH PFD a Disconnect the autopilot and yaw damper switch on the flight director b Depress t...

Page 115: ...hould be avoided The autopilot should be disengaged during inadvertent severe turbulence penetration or it is recommended to use basic pitch attitude hold mode When turbulence is anticipated or encoun...

Page 116: ...icates the severity of a thunderstorm A lightning strike can puncture the skin of an aircraft and can damage communication andnavigation equipment In addition it can damage engine components and has b...

Page 117: ...Standard Operating Procedures L410 UVP E20 Document No SOP L410 1 Page 6 4 Rev 1 Date JAN 18 Prepared by LA Checked by CLS This page has intentionally left blank...

Page 118: ...not hesitate to revert to conventional means of profilemanagement WARNING Check the MORA MSA and terrain clearance before initiating descent Garmin GTN750 Vertical Calculator VCALC The Vertical Calcul...

Page 119: ...nfiguration Holding is to be conducted in the clean configuration Speed Minimum of 135KIAS maximum147KIAS Vb Each hold shall be briefed using the TSAFE format T Type of hold entry direction of initial...

Page 120: ...be described as either Up 18 or 42 PF PM Flap Up Speed checked flaps up selected Flaps up Flap 18 Speed checked flaps 18selected Flaps 18 Flap 42 Speed checked flaps 42selected Flaps 42 Gear Up Speed...

Page 121: ...as long as raw data is monitored Aside from NDBapproaches the Final approach course must be flown with the CDI selectedto NAV 1 or NAV 2 and the appropriate navaid NDB approaches may beflown using ei...

Page 122: ...MDA 50 feet For visual approaches in reduced visibility set 500 feet AGL 7 7Arrival Approach Briefing The most important factor of the approach briefing is that it is carried out in a lowworkload envi...

Page 123: ...nd contact approach Terrain MSA from the south 6900 which is also the highest Weather Low ceiling expecting to break out at minimums light crosswind Operational Expecting radar vectors planning on usi...

Page 124: ...Weather Cloud base 1500 ft Crosswind from the right Operational Radar vectored approach I will hand fly from top of descent Lotsof traffic so I will keep my speed up on the approach and configure at 1...

Page 125: ...rule can be applied and to provide a fixed reference format that makes flight operations and communications on the flight deck with different crew easier The call outs also ensure that there are no m...

Page 126: ...0fpmof briefedROD from theFAF CANPA PM Descent Rate PFtakes corrective action PF Correcting Aircraftmore than 5 knotsfrom briefedspeed once established onfinal PM Speed PFtakes corrective action PF Co...

Page 127: ...called PF Descentchecklist Thedescentchecklististhencompleted PM Descentchecklistcomplete When released to a lower altitude the PM sets the new assigned altitude in the AMS PM feet set PF Check 1000 f...

Page 128: ...5 KIAS If a complete arrival procedure has been selected via the GPS the initialapproach phase may be completed using the GPS for guidance if the approachis in the database Raw data must be monitored...

Page 129: ...greater than 1000 ft min isrequired a special briefing shall be included in the approach briefing 6 Power setting is appropriate for the aircraft configuration and idle power shall not be used 7 All b...

Page 130: ...ach and the course shows full deflection On an NDB approach and the aircraft is beyond 5 degrees of the finalapproach course On a precision approach radar PAR usually limited to military aerodromes ap...

Page 131: ...Atlocalizerintercept PF LOCALIZERCAPTURED PM CHECK Call madeby PFwhenAPPR Annunciatorturnsgreen Established on the LOC PF SETGOAROUNDHDG PM GO AROUND HDG SET PF requeststherunway Headingtobeset NOTE H...

Page 132: ...t flap 42 PM selects flap as requested Landing Checklist at 1 500 feet AGL PF LANDING CHECKLIST PM LANDING CHECKLIST PM LANDING CHECKLIST COMPLETE PF request the checklist PM reads the checklist and t...

Page 133: ...d approach and calls PF GOING AROUND SETPOWER FLAPS 18 PM POWER SET FLAPS 18 PFcalls for go around power PMsets power and flaps as required for the go around procedure Set the flap and check instrumen...

Page 134: ...eet AGL however if not stable by 300 feet AGL the approach must be discontinued Reducing speed to minimum approach speed will help increase the descentangle The PM must crosscheck the next crossing al...

Page 135: ...for flying constant angle nonprecision approaches CANPA These methods provide a constant angleapproach which reduces exposure to crew error and CFIT accidents Thesemethods also make it much easier for...

Page 136: ...feet Threshold ELV 20feet Note 3 degrees slope equals 320 feet per nautical mile GSin KIAS 90 100 110 120 Slope 3 00 Deg RODft min 450 550 600 650 7 18 3 AP FD Use on CANPA Approaches Automatic flight...

Page 137: ...d to 90 KIAS At or after the FAF or once established inbound on an approach with noFAF commence descent and complete the final checklist Select VS mode anddescend at appropriate vertical speed to arri...

Page 138: ...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 Upon arrival at MDA H or any time therea...

Page 139: ...PTURED PM CHECK Call made by PF when APPR Annunciator turns green Established on the final approach course PF SET GO AROUND HDG PM GO AROUND HDG SET PF requests the runway Heading to be set NOTE HDG b...

Page 140: ...AP YD must me disconnected PF FLAP 42 PM SPEED CHECK ED FLAP 42 SELECTED PM FLAPS 42 PF CHECK IF REQUIRED PF request flap 42 PM selects flap as requested Landing Checklist at 1 500 feet AGL PF LANDIN...

Page 141: ...e Eg lights straight ahead Call by PF at minima PM shall state if visual reference has been acquired or not If visual PF LANDING AP YD DISCONNECT PM CHECK AP YD DISCONNECTED Call made by PF PF manuall...

Page 142: ...und The Captain may elect to call for the go around prior to reaching the decision altitude MAP if the quality of the approach is below the required standards 7 20 1 Missed Approach Callout Table If n...

Page 143: ...circuit altitude according to your aircraft category This will make any manoeuvrings safer and brings your view of the landing runway into a more normal perspective With weather conditions close to th...

Page 144: ...tude is captured the PFD will display ALT HOLD Once within thecircling area PF shall use HDG modeto maneuver within the circling area NOTE Use the RWY waypoint on the FPL if available it will provide...

Page 145: ...dditionally the intended Category shall beincluded in the approach brief Categories are based on PANS OPS criteriaas indicated on the bottom left corner of the approach chart Category A MAX IAS 100 Ra...

Page 146: ...re beginning the turn to base This should ensure the aircraft stays within the protected area Before turningbase or when initiating the turn to base leg select flaps as required and begindecelerating...

Page 147: ...to intercept the missed approach course Continue theturn until established on an intercept heading to the missed approach coursecorresponding to the instrument approach procedure just flown Maintain t...

Page 148: ...spected An altitude of 1 000 feet above aerodrome elevation is used for the downwind leg On selection of flaps 18 or 42 the landing checklist shall be completed Tocompensate for gusts pilotsshall add...

Page 149: ...learance OBTAINED LandingLights AS REQUIRED LandingLights AS REQUIRED Radar STANDBY 7 24Landing Checklist WARNING Failure to ensure the Yaw Damper is disengaged prior to landing can result in loss of...

Page 150: ...l move the power lever out of reverse at45KIASto minimize debris damage to thepropeller Once the aircraft is slowed to 30KIASthe Captain will retract spoilers take control and request manual steering...

Page 151: ...ED GEAR UP lights out Call made by PM PFcrosschecks positive rate of climb and call for gear up Above 400 feet and 100 KIAS raise the flaps PF Flaps up PM Flaps up selected Flap retraction at PF comma...

Page 152: ...clear of the runway at a safe taxi speed Captain First Officer ITEM ACTION ITEM ACTION Landing lights OFF RIGHT AFT Wind shield heating OFF Pitot Static heat OFF Anti ice OFF Flaps UP Auto feather DI...

Page 153: ...rts with no ramp Crews must ensure that all items are completed by using the appropriate checklist NOTE In a busy enviroment crew shall complete the checklist after selecting Park Brake ON Crew shall...

Page 154: ...ev 1 Date JAN 18 Prepared by LA Checked by CLS 7 29 Engine Cooldown Shutdownis after 5 minutes This is the time needed for the engine cool downand it may include taxiing time During taxiing the gasgen...

Page 155: ...es the Captain completes their flows and requests SHUTDOWN CHECKLIST The checklist is challenge response with the FO reading the checklist and the Captain responding accordingly Captain First Officer...

Page 156: ...ll open the passenger door and supervise the unloading of passengers and offer assistance where required The Captain must remain seated until after the last passenger has disembarked to assist with un...

Page 157: ...n before the next flight Hard Landing Lightning Strike Prop Strike or sudden engine stoppage Bird Animal Strike Severe Turbulence Exceeding Operational Limits The Amber OVER TEMP Light is on As displa...

Page 158: ...uel Communication problem between A C and ATC ATS Any traffic conflict with less than 3nm horizontal and or 700 ft vertical clearance Aborted takeoff or landings due to obstacles animals or persons on...

Page 159: ...ures and crew coordination for selected emergencies The Captain however has the overall authority as to how non normal situations are handled NOTE The most important thing to remember is to Aviate Nav...

Page 160: ...appropriate Memory Items as set out in the appropriate checklist If there are no memory items he she shall call for the checklist EXAMPLE Engine Failure in Flight ITEM ACTION PM PF Both TCLs REQUIRED...

Page 161: ...are the nearest airports Do I have enough Fuel to divert to selected airfield What is the terrain like on my diversion route What is the weather like enroute and at my diversion airport Does the failu...

Page 162: ...rew member the Captain must discontinue his present course of action and follow the Desired Course of Action unless the Captain determines that to do so would jeopardize the aircraft and the safety of...

Page 163: ...terrain warning sounds in VMC conditions the crew shall determine the cause for the warning and visually avoid any terrain or obstacles If applicable the terrain warning may be inhibited if continued...

Page 164: ...WX Radar o Before takeoff o On approach GS monitoring Brief windshear escape maneuver as part of Threats Recognition Aural Warning from EGWPS and EFI 890R system Indicated airspeed variations in exces...

Page 165: ...ng Procedures L410 UVP E20 Document No SOP L410 1 Page 9 7 Rev 1 Date Jan 18 Prepared by LA Checked by CLS 9 6 TCAS Traffic Warnings For specific crew procedures refer to APPENDIX E EMERGENCY AND ABNO...

Page 166: ...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...

Page 167: ...Standard Operating Procedures L410 UVP E20 Document No SOP L410 1 Page 9 9 Rev 1 Date Jan 18 Prepared by LA Checked by CLS...

Page 168: ...Standard Operating Procedures L410 UVP E20 Document No SOP L410 1 Page 9 10 Rev 1 Date Jan 18 Prepared by LA Checked by CLS This page is left intentionally in blank...

Page 169: ...teady The Message LED Indicator will be a steady blue when there is amessage in the unit s Inbox The indicator goes off when ANYmessage in the Inbox is read See in chapter 1 19 2 for messagereading in...

Page 170: ...he Bluesky system turn OFF then ON again If that does not correct the problem contactoperations as soon as possible in another way to give an ALL CLEAR message If the unit loses the Iridium signal the...

Page 171: ...ible If the crew wants to place a voice call time permittingduring an emergency the emergency button has to be de activated first In mostcases the following procedure is the most suitable for emergenc...

Page 172: ...c power to be removed from the aircraft to ensure thesignal is sent ACH 1000 The ACH 1000 enhances the cockpit interface of the Blue Sky equipmentinstalled and has the following main functions Satelli...

Page 173: ...CH 1000 SPEED DIALING Quick Keys for Speed Dialing When PHONE ishighlighted on the menu screen press thecorresponding key on the numerical keypad thatreferences the preconfigured speed dial party Menu...

Page 174: ...ssed by the pilots Menu Navigation Highlight MESSAGES by using the Up or Down MenuNavigation Button and press the Right MenuNavigation Button Next highlight SHORT CODE and press the Right Menu Navigat...

Page 175: ...p and Down Menu Navigation button until the Messagenumber you wish to read is displayed Press the OK button and your messagewill be displayed Use the Up or Down Menu Navigation button to view the enti...

Page 176: ...e captain is starting the engine Sending a Flight Plan Highlight Flight Plan from the Main Menu Then pressthe Right Menu Navigation Button When inputting the information for theconfigured fields you m...

Page 177: ...s opposed topassengers on board and infants Fuel on Board This field will accept the hours of fuel remaining on the aircraftin hours and minutes format Ex 3 15 3 hours and15 minutes of fuel remaining...

Page 178: ...Standard Operating Procedures L410 UVP E20 Document No SOP L410 0 Page AA 10 Rev 0 Date Jul 17 Prepared by TRI Checked by TM This page is left intentionally in blank...

Page 179: ...and the aisle are to remain clear if passengers are carried General balance guidelines Passenger loading should be from the center row 3 of the aircraft andmove both forward and aft equally The cargo...

Page 180: ...F S Seat Row 4 3 515 F S Seat Row 5 4 275 F S Seat Row 6 5 035 F S Seat Row 7 5 785 F S AFT baggage max 100 kg 6 650 TOTAL PAYLOAD AND MOMENT EMPTY WEIGHT AND MOMENT ZERO FUEL WEIGHT AND MOMENT MAX AL...

Page 181: ...Standard Operating Procedures L410 UVP E20 Document No SOP L410 0 Page BB 3 Rev 0 Date Jul 17 Prepared by TRI Checked by TM...

Page 182: ...0 773 3 843 6 913 9 984 2 1 054 5 F S 4 275 m seat Row 5 85 5 171 0 256 5 342 0 427 5 513 0 598 5 684 0 769 5 855 0 940 5 1 026 0 1 111 5 1 197 0 1 282 5 F S 5 035 m seat Row 6 100 7 201 4 302 1 402 8...

Page 183: ...ls CHECKED Capt ON Capt TA RA FO ON Capt Ice Protection AS REQUIRED FO Beacon Position lights ON Capt call out ON Capt PEDAL PF OFF Capt MAX PF OFF Capt OFF Capt AS REQUIRED PF ASIPA SOP L410 E20 NLCL...

Page 184: ...OFF Capt CHECKED Both Down Unlocked PM COMPLETED PM REVISION 1 Altimeters Approach Briefing AFTER TAKE OFF LANDING Gear Steering Ice Protection Heater Airconditioning AFTER LANDING Spoiler ABC Autofea...

Page 185: ...ition On the central control panel AUTO FEATHER switch ON On the test panel of the left control panel PROP FEATHERINGAUTObutton press and hold The AUTO FEATHER signals of both engines must light up wi...

Page 186: ...the left control panel PROP FEATHERING AUTObutton release On the overhead panel PROP FEATHERING circuit breaker switch OFF and back ON AUT BANK CONTROL circuit breaker switch OFF and back ON On the ce...

Page 187: ...further expected to have thorough understanding of what is executed by performing a certain item in the checklist It is not possible to cover all combinations of Malfunctions events in checklists and...

Page 188: ...r reset attempts are allowed according to the checklists If the failure alert disappears continue normal operation and record the event into the maintenance log CAUTION ALL EMERGENCY OR ABNORMALITY MU...

Page 189: ...Standard Operating Procedures L410 UVP E20 Document No SOP L410 0 Page EE 3 Rev 1 Date JAN 18 Prepared by LA Checked by CLS PAGE INTENTIONALLY LEFT BLANK...

Page 190: ...rmal checklist a Task Sharing PF is responsible for Flight path and speed control Power lever Aircraft configuration Navigation PM is responsible for Checklist reading Execution of required action Pro...

Page 191: ...ency procedure PF Issues command to perform CHECKLIST according to failure e g BATTERY OVERHEATING ABNORMAL CHECKLIST PM Takes appropriate CHECKLIST and reads its name thus confirming correctness of t...

Page 192: ...items should be done without waste of time COCKPIT OR CABIN FIRE EC 20 Item Action CM Oxygen Masks Goggles PUT ON BOTH FASTEN SEAT BELTS circuit breaker ON PM DESCENT INITIATE AS REQUIRED PF SOURCE OF...

Page 193: ...epared by LA Checked by CLS FRONT BAGGAGE COMPARTMENT FIRE EC 20 Item Action CM BAGGAGE COMPARTMENT PULL OUT CM2 FASTEN SEAT BELTS SWITCH ON PM DESCENT INITIATE AS REQUIRED PF COCKPIT WINDOWS OPEN AS...

Page 194: ...fuel in wing tip tanks Each this case must be recorded in the Airplane Log book and Technical Log Book 2 1 3 LIGHTNING STRIKES In case of Lightning strikes check all electronic equipment and radios C...

Page 195: ...ress MAYDAY preferably three times is a serious and for imminent danger and require immediate assistance in flight fire mechanical failures structural damage This phrase commands radio silence on the...

Page 196: ...0 Page EE 10 Rev 1 Date JAN 18 Prepared by LA Checked by CLS c Transponder setting At the same time the aircraft transponder should be set accordingly Mode A C S and codes 7700 for emergency 7600 for...

Page 197: ...Standard Operating Procedures L410 UVP E20 Document No SOP L410 0 Page EE 11 Rev 1 Date JAN 18 Prepared by LA Checked by CLS INTENTIONALLY LEFT BLANK...

Page 198: ...WO ENGINES OFF EC 8 4 ELECTRICAL SYSTEM BOTH GENERATORS INOPERATIVE EC 9 5 AP FD AUTOPILOT MALFUNCTION EC 10 AP FD ELECTRICAL TRIM MALFUNCTION EC 10 FDR FAULT EC 11 6 EFIS COMPLETE LOSS OF EFIS PRESEN...

Page 199: ...dard Operating Procedures L410 UVP E20 Document No SOP L410 0 Page EE 13 Rev 1 Date JAN 18 Prepared by LA Checked by CLS 9 SMOKE COCKPIT OR CABIN FIRE EC 19 FIRE IN FRONT OR REAR BAGGAGE COMPARTMENT E...

Page 200: ...the corresponding part of Airplane 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 comman...

Page 201: ...VR 0 variable see section 5 of this AFM 2 Minimum safe take off airspeed with wing flaps in 18 or 0 position V2 18 or V2 0 variable see section 5 of this AFM 3 One engine inoperative best angle of cl...

Page 202: ...tion CM The following items are valid for engine on fire before V1 TCL s IDLE PF SPOILERS DEPLOY CM 1 BRAKES AS REQUIRED CM 1 ATC ADVISE CM 2 When the aircraft stopped PARKING BRAKE SET CM 2 PAX ADVIS...

Page 203: ...s L410 UVP E20 Document No SOP L410 0 Page EE 17 Rev 1 Date JAN 18 Prepared by LA Checked by CLS If fire remains EXTINGUISHER SECONDARY push butt PUSH SEC PM ATC ADVISE CM 2 AIRCRAFT EVACUATION AS REQ...

Page 204: ...are valid for engine on fire FUEL STOP COCK EMERGENCY THROTTLE LEVER SHUT PM MANUAL FEATHER push button PUSH PM FUEL FIRE COCK SHUT PM HEATING lever SHUT DOWN CM 1 EXTINGUISHER PRIMARY push butt PUSH...

Page 205: ...ABORT THE TAKE OFF ENGINE FAILURE DURING TAKE OFF AT SPEED V1 FLAPS 18 EC 5 Item Action CM TCL of both engines check TAKE OFF RATING PM FAILED ENGINE DETERMINE BOTH After lift off LANDING GEAR UP PM F...

Page 206: ...itch OFF PM At height of 400 ft 120m above RWY check TAKE OFF RATING PM INCREASE THE AIRSPEED V2 FLAPS 0 3 kts PF WING FLAPS RETRACT FLAPS 0 PM TCL of operating engine set continuous OEI rating PM AIR...

Page 207: ...VP E20 Document No SOP L410 0 Page EE 21 Rev 1 Date JAN 18 Prepared by LA Checked by CLS b If the engine operates at idle and other parameters correspond to idle power then PROPELLER UNFEATHER PM USE...

Page 208: ...FEATHERING CHECK PM a If the automatic feathering cycle has not been accomplished MANUAL FEATHER push button of the inoperative engine PUSH PM ELU LH RH circuit breakers OFF PM b If the inoperative e...

Page 209: ...ECK PARAMETERS PM a If the engine is fully stopped The following items are valid for inoperative engine TCL IDLE PM FUEL STOP COCK EMERGENCY THROTTLE LEVER SHUT PM GENERATOR DC AC switches OFF PM ENGI...

Page 210: ...ATHERING CHECK PM a If the automatic feathering cycle has not been accomplished MANUAL FEATHERING push button of the inoperative engine PUSH PM ELU LH RH circuit breakers OFF PM b If the inoperative e...

Page 211: ...y LA Checked by CLS TCL of operating engine set continuous OEI rating PM AIRSPEED V2 0 up to 1 500 ft 457 m above runway PM Accomplish the following procedures for inoperative engine TCL IDLE PM FUEL...

Page 212: ...ASTEN SEAT BELTS circuit breaker SWITCH ON PM PCL S FEATHER PM IF propellers aren t feathered MANUAL FEATHER push button PUSH PM PCL s FEATHER PM FUEL STOP COCK EMERGENCY THROTTLE LEVER SHUT PM ALL UN...

Page 213: ...INOPERATIVE EC 9 Item Action CM LH GENERATOR and RH GEN switches on the overhead panel CHECK SWITCHING ON PM ALL CIRCUIT BREAKERS NOT MARKED WITH YELLOW STRIP SWITCH OFF PM BATTERIES DISCHARGING CURR...

Page 214: ...C PRESS and HOLD throughout recovery PF TRIM Circuit Breaker PULL PM AIRPLANE RETRIM manually PF CAUTION WHEN DISCONNECTING THE AUTOPILOT AFTER A TRIM MALFUNCTION HOLD THE CONTROL WHEEL FIRMLY UP TO 5...

Page 215: ...ground RECORDER circuit breaker CHECK IN PM FLIGHT EXECUTION MMEL or MEL CM 1 In the air FLIGHT CONTINUE PF After landing report ground personnel COMPLETE LOSS OF EFIS PRESENTATION EC 11 Item Action...

Page 216: ...on CM As indicated by red X on airspeed altitude or vertical speed field WRONG SIDE IDENTIFIED PM ADC REVERT DEPRESS at wrong side IF BOTH ADC S HAVE FAILED USE STANDBY INSTRUMENTS PF AHRS FAILURE EC...

Page 217: ...UVP E20 Document No SOP L410 0 Page EE 31 Rev 1 Date JAN 18 Prepared by LA Checked by CLS RADAR ALTIMETER FAILED EC 12 Item Action CM Indicated by red RA FAIL on PFD RADAR ALTIMETER CIRCUIT BREAKER C...

Page 218: ...SELECTED PF APPROACH SPEED MIN V2 PF ATC NOTIFY PM XPDR 7700 PM SAFETY HARNESS CONTR LEVER FRONT locked POSITION EGPWS CIRCUIT BRAKER OFF PM FUEL FROM THE WING TIP TANK TO THE MAIN WING TANK TRANSFER...

Page 219: ...GHT MAKE APP WITH THE EMERG EXTERNAL LIGHT SWITCHED ON AT ALT FROM 500 FT TO 350 FT SWITCH ON THE LANDING LIGHTS I II IT IS RECOMMENDED THAT FOR ALL EMERG LANDINGS ON LAND THE WING FLAPS SHOULD BE EXT...

Page 220: ...VP E20 Document No SOP L410 0 Page EE 34 Rev 1 Date JAN 18 Prepared by LA Checked by CLS LANDING ON WATER EC 14 Item Action CM LANDING GEAR UP PM FLAPS 42 PM PASSENGERS PREPARE PM FUEL BURNOFF TO MIN...

Page 221: ...ND ON A HARD SURFACED RUNWAY NOSE WHEEL LANDINGS with main wheels retracted NOTE IF IT IS POSSIBLE TO RETRACT THE NOSE WHEEL RETRACT IT AND PERFORM THE WHEELS UP LANDING IF IT IS IMPOSSIBLE TO RETRACT...

Page 222: ...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 CAUTION TO SHORTEN THE LANDING RUN THE EXTENDED MAIN WHEEL...

Page 223: ...RRAIN PULL UP or OBSTACLE OBSTACLE PULL UP A P DISCONNECT PF ENGINE POWER SET MCT PF PROPPELERS SET MAX RPM PM PITCH APROX 10 SET PF A C CONFIG MAINTAIN EXIST PF AIRSPEED Vx 100 KIAS MAINTAIN PF If WA...

Page 224: ...0 0 Page EE 38 Rev 1 Date JAN 18 Prepared by LA Checked by CLS If GLIDESLOPE alert GLIDESLOPE path RESTORE PF on back course app EGPWS G S P CANCEL PRESS PM Other emergencies ditching or other off air...

Page 225: ...TERRAIN TERRAIN PULL UP OR OBSTACLE OBSTACLE PULL UP ACTIVATION OF THE RED PULL UP ANNUNCIATOR PROCEDURE FOR WARNING ALERTS APPLY MAXIMUM CONTINUOUS POWER AS DETERMINED BY EMERGENCY NEED IF ENGAGED DI...

Page 226: ...Standard Operating Procedures L410 UVP E20 Document No SOP L410 0 Page EE 40 Rev 1 Date JAN 18 Prepared by LA Checked by CLS OF THE TERRAIN AWARENESS AND ALERTING DISPLAY TAD CONTINUE AT NEX PAGE...

Page 227: ...TS AS NECESSARY TO CORRECT THE AIRCRAFT FLIGHT PATH BACK TO THE GLIDESLOPE CENTERLINE OR PERFORM A MISSED APPROACH TO INHIBIT NUISANCE MESSAGES E G ON BACKCOURSE APPROACHES THE GPWS G S P CANCEL SWITC...

Page 228: ...Item Action CM TRAFIC ADVISORY TRAFIC TRAFIC LANDING LIGHTS ON PM FASTEN SEAT BELTS ON PM PCLs 1900 RPM PM CHECK SAVE ALTITUDE PM RESOLUTION ADVISORY CLIMB CLIMB or DESCENT DESCENT AUTOPILOT DISCONNEC...

Page 229: ...Standard Operating Procedures L410 UVP E20 Document No SOP L410 0 Page EE 43 Rev 1 Date JAN 18 Prepared by LA Checked by CLS CONTINUE AT NEX PAGE...

Page 230: ...ADJUST VERTICAL SPEED ADJUST VSI indicated prohibited vertical speed in RED Goal is vertical speed in GREEN Promptly and smoothly reduce vertical speed to that shown in the GREEN arc as indicated on...

Page 231: ...10 0 Page EE 45 Rev 1 Date JAN 18 Prepared by LA Checked by CLS WINDSHEAR MICROBURST EC 17 Item Action CM TCL of both engines SET AS REQUIRED PF PCL S MAX PRM PM AIRSPEED MIN V stall PF A C CONFIGURAT...

Page 232: ...N AP FD DISENGAGE PF AIRPLANE CONTROL WHEEL GRASP FIRMLY PF ATTITUDE LOWER NOSE PF TCL S AS REQUIRED PF AFTER STALL RECOVERY RESUME NORMAL FLIGHT PF LANDING CONFIGURATION AP FD DISENGAGE PF AIRPLANE C...

Page 233: ...CLS BOMB ON BOARD EC 18 Item Action CM LOAD FACTOR AVOID PF LANDING GEAR DOWN PM FLAPS 18 PM HANDLE BOMB CAREFULY AVOID SHOCKS PM Place bomb near cargo door preferably in a bag attached to the door ha...

Page 234: ...SIGN ON PM TCL S IDLE PF TRANSPONDER SET 7700 PM ATC PAX NOTIFY PM DESCENT CHECK MSA ROD as REQUIRED PF ON GROUND EMERGENCY EVACUATION EC 19 Item Action CM ATC NOTIFY PM AIRCRAFT STOPPED CM 1 PARKING...

Page 235: ...breaker ON PM DESCENT INITIATE AS REQUIRED PF SOURCE OF FIRE DETERMINE PM PORTABLE EXTINGUSHER USE PM COCKPIT WINDOWS OPEN BOTH If you have not succeeded in extinguishing the fire LAND ASAP OR PERFOM...

Page 236: ...Standard Operating Procedures L410 UVP E20 Document No SOP L410 0 Page EE 50 Rev 1 Date JAN 18 Prepared by LA Checked by CLS INTENTIONALLY LEFT BLANK...

Page 237: ...OSITIVE RATE PF Checks climbing and commands GEAR UP In case of GA flaps 42 configuration retract flaps to 18 before gear up and PF command FLAPS 18 PM Moves landing gear control handle to retracted p...

Page 238: ...RCUIT AB 11 1 9 BETA RANGE AND PROPELLER PITCH LOCK SIGNALLING AB 12 2 FUEL 2 1 FAILURE OF AUTOMATIC SWITCHING ON FUEL TRANSFER AB 13 2 2 MINIMUM FUEL PRESSURE AB 14 2 3 FUEL LOW LEVEL AB 15 2 4 FUEL...

Page 239: ...5 3 DEFLATED TIRE ON WHEEL AB 29 6 ANTIICING DEICING 6 1 ONE SECTION OF PNEUMATIC AIRFRAME DEICING FAILURE AB 30 6 2 TOTAL FAILURE OF PNEUMATIC AIRFRAME DEICING AB 31 6 3 FAILURE OF PNEUMATIC DEICING...

Page 240: ...ON AB 41 XBUS COMPARATION AB 42 BUS I II 26V AC FAULIRE AB 43 9 NAV GPS 9 1 LOSS OF GPS SBAS NAV DATA AB 44 9 2 GPS APP DOWNGRADE AB 45 9 3 LOSS OF COM RAD TUNING FUNCTIONS AB 46 9 4 DATA SOURCE HDG F...

Page 241: ...TCL of operating engine set continuous OEI rating or lower as required PM Procedure on the controls of the opposite engine to be shutdown TCL IDLE PM MANUAL FEATHER push button PUSH PM FUEL STOP COCK...

Page 242: ...op Engine feathered IAS at or above 84 KIAS TCL of operating engine TAKE OFF RATING PM PCL of inoperating engine FEATHER PM Perform transition to climb at airspeed V2 FLAPS 18 PF WING FLAPS FLAPS 18 P...

Page 243: ...m above runway AIRSPEED VREF FLAPS 42 PF TCL IDLE PF At a height of 10 ft 3 m above runway AIRPLANE VERTICAL SPEED FLARE PF VERTICAL SPEED 200 TO 100 FPM PF Immediately after touch down according to c...

Page 244: ...the most essential electric equipment MAXIMUM ALTITUDE 13 000 ft 4 000 m PF ELU circuit breaker of the stopped engine OFF PM RECOMMENDED AIRSPEED 108 119 KIAS PF MAXIMUM AIRSPEED 162 KIAS PF If flyin...

Page 245: ...rise continues FUEL STOP COCK EMERGENCY THROTTLE SHUT PM NOTE AFTER THE ENGINE HAS STOPPED TAKE THE ACTION SPECIFIED IN ENGINE SHUTDOWN IN FLIGHT CHECK LIST AB 4 MINIMUM OIL PRESSURE AB 9 Item Action...

Page 246: ...of affected engine REDUCE AS REQUIRED If the parameters of affected engine continue to fluctuate PERFORM ENGINE Shut Down in flight UNTER UNFAVOURABLE FLIGHT CONDITION SUCH AS ICING THUNDERSTORM MOUT...

Page 247: ...Date JAN 18 Prepared by LA Checked by CLS USE OF EMERGENCY FUEL CONTROL CIRCUIT AB 11 Item Action CM TCL IDLE PM ISOLATION VALVE ON PM AMBER ISOLATION VALVE LIGHT CHECKED ON BOTH FUEL STOP COCK EMERG...

Page 248: ...E cell in the Engine section of the CWD comes on perform the following TCL IDLE PM MANUAL FEATHER push button under cover PUSH PM After manual feathering and also if propeller has not been feathered F...

Page 249: ...ER PITCH LOCK cell does not come on it is false signaling ELU LH RH SWITCH OFF PM When the amber BETA RANGE cell in the Engine section of the CWD and amber PROPELLERLOCK cell come on ELU LH RH SWITCH...

Page 250: ...TIP TANK FUEL TRANS switch for the affected side ON PM GREEN LIGHT FUEL TRANFER CHECK ON PM MINIMUM FUEL PRESSURE AB 13 Item Action CM FUEL PUMP LH RH CHECK ON PM MINIMUM FUEL signal CHECK PM FUEL QUA...

Page 251: ...tion CM a If fuel leakage is observed soon after take off Return to airport of departure Do not utilize fuel transfer system CM 1 b If leakage is observed on route FUEL LEVEL CHECK PM Continue to the...

Page 252: ...hecked by CLS FAILURE OF ONE DC GENERATOR AB 15 Item Action CM DC GENERATOR switches CHECK ON PM DC GENERATOR switch of failed unit OFF than ON PM If DC GENERATOR is fault DC GENERATOR switch off fail...

Page 253: ...ENERATOR LH or RH switches CHECK ON PM AC GENERATOR switch of failed unit OFF than ON PM If AC GENERATOR is fault AC GENERATOR switch of failed unit OFF PM FAILURE OF ONE OF 36 V AC INVERTER AB 17 Ite...

Page 254: ...ate JAN 18 Prepared by LA Checked by CLS FAILURE OF BATTERY CIRCUIT AB 18 Item Action CM BATTERY switches CHECK ON PM VA METER selector switch Set first to BAT I VA and BAT II VA position CM2 Charging...

Page 255: ...by CLS BATTERY OVERHEATING AB 19 Item Action CM BATTERY I II switch OFF PM EMERGENCY EXTENSION OF WING FLAPS 18 AB 20 Item Action CM WING FLAPS control lever FLAPS 18 CM 2 WING EMERGENCY lever DOWN OP...

Page 256: ...WING FLAPS RETRACTING AB 21 Item Action CM Real position of the flaps CHECK PM If the flaps have remained in the take off position 18 Maintain climb with airspeed 124 KIAS PF After climbing Airspeed...

Page 257: ...f the ABC tab retracts FURTHER FLIGHT CONTINUE FLIGHT PF If the ABC tab does NOT retract Trim the airplane Using the aileron trim and do NOT exceed 111 KIAS PF Decide whether to continue the flight or...

Page 258: ...3 green lights on landing gear position indicator come on and until resistance on pump handle increases CM 2 If after the use of the emergency hydraulic pump some of the landing gear legs are stuck in...

Page 259: ...R lever has been moved into UP position LANDING GEAR LEVER DOWN AND THEN UP AGAIN PM If the green or red signal light has not gone off LANDING GEAR lever DOWN PM EXTENSION OF THE LANDING GEAR ACCORDIN...

Page 260: ...During take off AIR SPEED BELOW OR EQUAL V1 ABORT TAKE OFF PF Relieve the load on the wheel with faulty tire and use reverse power as required AIR SPEED ABOVE V1 CONTINUE TAKE OFF PF LANDING GEAR DO...

Page 261: ...ION IS ACCOMPANIED BY A RISE OF THE ITT EITHER ABOVE THE PERMISSIBLE MAXIMUM ITT OR BY MORE THAN 30 C ABOVE THE PREVIOUS VALVE PM IF YES SWITCH THE FUNCTION SELECTOR TO MANUAL AND DO NOT USE THE FAULT...

Page 262: ...tested this means a burnt out bulb filament Replace the bulb IF FAILURE IS NOT DUE TO BULB SELECTOR OF PNEUMATIC DE ICING MANUAL CM 2 Selector switch next to lights SECTION A THEN B THEN C CM 2 FAILUR...

Page 263: ...ming on of both propeller deicing cells on the cwd means main circuit failure of propeller deicing cycling switch PROP DEICING switch STDBY I OR STDBY II CM 2 Coming on of one of the amber PROPELLER D...

Page 264: ...CM 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 EMERGENCY STATIC PRESSURE red cock OPEN CM 1 If the RH INSTRUMENTS are...

Page 265: ...ion CM If the LH INSTRUMENTS are affected PITOT PRESSURE black cock POSITION II CM 1 If the RH INSTRUMENTS are affected AUTOPILOT DISCONNECT PF Continue the flight without any special measures but dis...

Page 266: ...AUTOPILOT COUPLED AB 35 Item Action CM AP DISENGAGE PF AIRPLANE RUDDER AND AILERON AXES TRIM MANUALLY PF Follow the basic Airplane Flight Manual engine inoperative procedures CAUTION IF RUDDER TRIM C...

Page 267: ...ROLL COMP miscompare message is displayed EFIS STBY ATT STBY COMPASS AND GPS CROSSCHECK PM FAULTY AHRS UNIT IDENTIFY PM ATT HDG REVERT ON EFECTIVE SIDE SELECT PM XXXX COMP COMP RESET PRESS PM If ambe...

Page 268: ...AB 37 CONTINUE BELOW If amber XBUS message is displayed PFD I II CIRCUIT BREAKER CHECK PM IF OPEN RESET If Amber BUS I II 26V AC signal cell lights on the central warning display electro INV I I II II...

Page 269: ...ction CM NAVIGATION USE ALTERNATE SOURCES PM If no alternate navigation USE GTN sources DEAD RECKONING DR MODE PM NOTE All information normally derived from GPS will become less accurate over time IF...

Page 270: ...IO TUNING FUNCTIONS AB 40 Item Action CM IF ALTERNATE COM IS AVAILABLE USE ALTERNATE COM PM DATA SOURCE HEADING SOURCE INOPERATIVE OR CONNECTION TO GTN LOST MESSAGE AB 41 Item Action CM AP HDG mode PF...

Page 271: ...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 EGPWS SYSTEM DEACTIVATION AB 44 Item Action CM Parti...

Page 272: ...rcuit breaker SWITCH ON PM VENTILATION control lever FULLY OPEN CM1 AIRCONDITION triple throw switch FANS position CM1 In case of abnormal function of Airconditioning system for example loss of coolin...

Page 273: ...HT 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 USI...

Page 274: ...terrain configuration causes this caution flight crew is sure about its position and this situation is included in landing briefing the flight crew must not take into account this caution neither in...

Page 275: ...o 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 FL...

Page 276: ...ion TOO LOW GEAR In IMC conditions or at night perform GA procedure In VMC conditions with sufficient visual reference extend landing gear At altitudes below 500 ft AGL initiate GA procedure Caution T...

Page 277: ...CENT as indicated by the GREEN arc on the VSI display MONITOR VERTICAL SPEED Present vertical speed is outside the RED arc as shown on the VSI Keep vertical speed out of the RED unsafe area as indicat...

Page 278: ...SPACE 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...

Page 279: ...A Checked by CLS 7 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 lan...

Page 280: ...er unfeathering TCL IDLE PCL move from FEATHER to FINE PITCH position On the left control panel PROPELLER PITCH LOCK TEST button press and hold at propeller speed about 700 RPM Propeller speed must st...

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