Pilot Operating Handbook C42 Serie - Fliegerclub Stadtlohn
Pilot Operating HandbookC42 SeriePOH C42 Series Issue-4 Rev.307.02.2017Page 1 of 92
C42 Pilot Operating HandbookPILOT OPERATING HANDBOOKfor the aircraft IKARUS C 42 SeriesModell Nr.C42 / C42B / C42C / C42E / C42CSLTZ-Nr.61141 / 61141.1 / 61141.5 / 61141.6 / 61141.7TypeIKARUS C42 SeriesAirplane Registration No.Airplane Serial-No.Reference: POH C42 SeriesIssue 4 - Rev.307.02.2017This handbook is to be kept in the aircraft at all times.The described options of the C42 Series use are certified for Germany andhave been tested in Germany.Please note that for using the C42 Series as a towplane for towing gliders,towing aerial signs or decanting sky divers, different regulations may apply indifferent countries. Please contact your local authorities for furtherclarification.POH C42 Series Issue-4 Rev.324.01.2013Page 2 of 92
RECORD OF MANUAL REVISIONSNo.IssueNo.142Description of ChangesDateSignatureModel C42CS added02.11.2015A.Kurz4Cooling system added02.11.2015A.Kurz34 Rev.1Empty weight center ofgravity deleted20.11.2015A.Kurz44 Rev.1Weight and Balance modify20.01.2016A.Kurz54 Rev.2Circuit diagramm updated02.12.2016R. Neie64 Rev.3Page 7607.02.2017A.KurzPOH C42 Series Issue-4 Rev.307.02.2017Page 3 of 92
C42 Series Pilot Operating HandbookManufacturer Contact InformationCOMCO IKARUS GmbHAm Flugplatz 1188367 Hohentengen / SwabiaGermanyTel: 49 7572 600 80Fax: 49 7572 3309Email: post@comco – ikarus.deOwnerThis Pilot Operating Handbook belongs to the aircraft:and is to be kept in the aircraft at all times.POH C42 Series Issue-4 Rev.307.02.2017Page 4 of 92
C42 Series Pilot Operating HandbookIntroductionC42 series aircraft are built in compliance with the airworthinessrequirements of various countries and are certified as Microlight,Ultralight, Advanced Ultralight and Light Sport Aircraft.To operate the aircraft the pilot must hold a license or certificateappropriate to this category of aircraft. The aircraft is not to be flownunless it is registered, carries registration markings in accordancewith the requirements of the country in which the aircraft is to be flown,and has a Permit to Fly or certificate of Airworthiness valid in thecountry of operation.The aircraft is to be flown under daytime VFR conditions. Flight inconditions other than daytime VFR without the correct aircraftequipment and pilot ratings is extremely dangerous and can result inserious injury or death.Pilots holding licences for other categories, even higher ones, arerequired to be checked out by an appropriately qualified instructor priorto flying this aircraft as it possesses characteristics that are unique tolight sport type aircraft. These characteristics include low inertia,susceptibility to turbulence and wind gradient and special engineconsiderations.The safety of all occupants, the aircraft and persons on the ground arethe sole responsibility of the Pilot in command. Do not operate thisaircraft in a manner that would endanger the occupants, the aircraft orpersons on the ground.POH C42 Series Issue-4 Rev.307.02.2017Page 5 of 92
C42 Series Pilot Operating HandbookBear in mind that the engines used in C42 aircraft are not certifiedaviation engines and thus may not offer the same safety standardsfound in other classes of aircraft. Prepare your flight so that you canalways reach an emergency landing area should you experienceengine failure. On cross country flights, ALWAYS keep an emergencylanding field in sight.Changes to the control system, structure,wings and engine are prohibited.These changes would invalidate any certificate of airworthiness orpermit to fly and as such would result in an insurance becoming nulland void.All operating difficulties and equipment failures should be reported toyour dealer or the manufacturer.For fire safety reasons, smoking is prohibited on board of the aircraft.POH C42 Series Issue-4 Rev.307.02.2017Page 6 of 92
C42 Series Pilot Operating HandbookThree side view: IKARUS C42 SeriesIKARUS C42POH C42 Series Issue-4 Rev.307.02.2017Page 7 of 92
C42 Series Pilot Operating HandbookIKARUS C42B / C42E (C42B LSA)POH C42 Series Issue-4 Rev.307.02.2017Page 8 of 92
C42 Series Pilot Operating HandbookIKARUS C42CPOH C42 Series Issue-4 Rev.307.02.2017Page 9 of 92
C42 SERIES Flight And Operators ManualTable of ContentsC42CSPOH C42 Series Issue-4 Rev.307.02.2017Page 10 of 92
C42 SERIES Flight And Operators ManualTable of ContentsTitle pageRecord of Manual RevisionsManufacturer Contact InformationIntroductory remarksThree-side viewTable of contents234581 Operating limitations . 141.11.21.31.41.51.61.71.81.91.101.11Airspeeds: . 14Weights . 14Structural limitations: . 15Center of gravity limits: . 15Airspeed markings: . 15Engine rpm limitations . 16Rpm indicator markings . 16Flap settings . 16Propellers for Rotax 912 UL: . 17Propellers for Rotax 912 UL S . 19Engine limitations according to the Rotax operating manual . 202 Kinds of operation limitations . 213 Operation of the Engine . 214 Flight Operations . 234.14.24.34.44.54.64.74.84.94.10Taxiing: . 23Take-off and climb: . 23Cruising flight . 25Turning flight . 25Stalls . 26Descent and landing . 27Shutting down the engine: . 27Sudden loss of engine power: . 28Using the optional cowl flap on the aircraft C42 . 30Emergency procedures . 31POH C42 Series Issue-4 Rev.307.02.2017Page 11 of 92
C42 SERIES Flight And Operators ManualTable of Contents5 Ground Handling . 335.15.25.35.4Towing . 33Hoisting . 33Parking. 34Tie-Down . 346 Minimum equipment . 367 Dimensions . 368 Weight and balance . 378.1Loading plan: . 389 Data placard and checklist: . 3910 “Before take-off” checklist . 4011 Approved equipment . 4112 Flight performance: . 4312.112.212.312.4Take-off distance . 43Rate of climb Rotax 912 UL Rotax 912 UL S . 43Cruising speed (solo) . 44Engine off performance (solo) . 4413 Attaching the wings. 4513.1 Attaching the wings to the fuselage . 4513.2 Folding the wings for hangaring . 4714 Pre-flight inspection . 4814.114.214.314.414.514.614.714.814.914.10Engine. 48Landing gear . 48Left wing . 49Left side of fuselage . 49Empennage . 50Right side of fuselage . 50Right wing . 50Cabin, inside and outside . 50Instruments . 51Drainage . 51POH C42 Series Issue-4 Rev.307.02.2017Page 12 of 92
C42 SERIES Flight And Operators ManualTable of Contents15 Care and maintenance . 5216 Rigging data . 5417 Information for ultralights with towing gear . 5817.117.217.317.417.5Equipment of the towing aircraft . 58Operating limitations . 59Flight characteristics and performance . 61Placards . 62Emergency procedures during towing . 6318 Inspection and maintenance intervals . 6519 Special features of the aircraft equipped for handicapped pilots7220 Flying with the IKARUS C42 Series with the doors removed . 7421 Additional instructions for dropping parachutists . 7522 Instructions for the use of the LiFe-Battery . 7723 COMCO IKARUS Manufacturer Warranty. 7824 Appendix: . 8224.124.224.324.424.524.624.7Placards . 82Data placard . 83Service Problem Report Form -Aircraft . 84Inspections performed . 85Location of the parachute rescue system . 86Banner towing . 89Wiring diagram . 92POH C42 Series Issue-4 Rev.307.02.2017Page 13 of 92
C42 SERIES Pilot Operating Handbook1Operating limitations1.1 Airspeeds:Never-exceed speed:C42C42B / C42E / C42CC42CSVNE 97 ktsVNE 116 ktsVNE 121 kts(180 km/h)(216 km/h)(225 km/h)Speed in turbulent airC42 / C42B / C42E / C42CC42CSVBVB 97 kts 101 kts(180 km/h)(187 km/h)Maximum manoeuver speed:C42 / C42B / C42E / C42C / C42CSVA (148 km/h)Speed with landing flap set. Vfeuntil 2009since 2009Stall speed:80 kts57 kts63 ktsflap position 0:flap position 1:flap position 2:VS1 VS2 VS3 VFE 105 km/hVFE 117 km/h40 kts38 kts35 kts(75 km/h)(70 km/h)(65 km/h)If VA speed is exceeded, only little rudder movement are allowed.1.2 WeightsMaximum take-off weight:Maximum take-off weight withinstalled rescue system992 lbs (450,0 kg)1041 lbs (472.5 kg)Empty weight (see last Weight and Balance plan)kgMinimum payload: (see last Weight and Balance plan) 144 lbs (65 kg)POH C42 Series Issue-4 Rev.307.02.2017Page 14 of 92
C42 SERIES Pilot Operating Handbook1.3 Structural limitations:Positive limit load factor:Negative limit load factor: 4 g-2 g1.4 Center of gravity limits:Reference datum:Forward center of gravity:Rearward center of gravity:Wing leading edge at a rib station11.8 inches aft of datum (300 mm)22.0 inches aft of datum (560 mm)1.5 Airspeed markings:38 - 57 kts38 – 63 kts(71 – 105 km/h)(71 – 117 km/h)Green arc:C42 / C42B / C42E / C42CC42CS43 - 97 kts43 – 101 kts(79 - 180 km/h)(79 - 187 km/h)Yellow arc:C42B / C42E / C42CC42CS97 – 116 kts97 – 121 kts(180 - 216 km/h)(187 - 225 km/h)Yellow triangle:VX 54 kts(100 km/h)Yellow line:VA 75 kts(148 km/h)VNE 97 ktsVNE 116 ktsVNE 121 kts(180 km/h)(216 km/h)(225 km/h)until 2009 / whitesince 2009 / whiteRed line:C42AC42B / C42E / C42CC42CSATTENTION : C42 A- No yellow area ! - VB VNEPOH C42 Series Issue-4 Rev.307.02.2017Page 15 of 92
C42 SERIES Pilot Operating HandbookThe deviation curve for the airspeed indicator can be interpolated from thefollowing tableIASkm/hEASkm/h1.660708090 100 110 120 130 140 150 160 170 180 190 20065748391 100 109 117 125 134 142 151 160 168 177 185Engine rpm limitationsMaximum engine rpm:Maximum continuous rpm:1.7n 5800 rpm, 5 min. maxn 5500 rpmRpm indicator markingsYellow arc:Red line:n 5500 - 5800 rpmn 5800 rpm1.8 Flap settingsPosition 0:Position 1:Position 2:POH C42 Series Issue-4 Rev.3cruisingtake-off / landinglanding07.02.2017Page 16 of 92
C42 SERIES Pilot Operating Handbook1.9Propellers for Rotax 912 UL:With propeller WARP DRIVE 2-blade 68” (1.72 m Ø) constant speed,pitch 23.5 at 15.75 inches (0.40 m) from hub,full throttle rpm on the groundmax. 5200 1/minPropeller rpmapprox. n 2300 1/minWith propeller WARP DRIVE 3-blade 68” (1.72 m Ø)pitch 21.0 at 15.75 inches (0.40 m) from hub,full throttle rpm on the groundmax. 5200Propeller rpmapprox. n 23001/min1/minWith propeller Sport-Prop 3-blade 68” (1.72 m Ø)pitch 19.5 at 15.75 inches (0.40 m) from hub,full throttle rpm on the groundmax. 4900Propeller rpmapprox. n 21501/min1/minWith propeller GSC 3-blade 68” (1,72 m Ø)pitch 21.0 at 15.75 inches (0.40 m) from hub,full throttle rpm on the groundPropeller rpm1/min1/minPOH C42 Series Issue-4 Rev.3max. 4900approx. n 215007.02.2017Page 17 of 92
C42 SERIES Pilot Operating HandbookWith propeller Neuform CR2-75 2-blade 69” (1,75 m Ø)pitch 27.0 at r 14.37 inches (0.365 m),full throttle rpm on the groundmax. 5100Propeller rpmapprox. n 22501/min1/minWith propeller Neuform CR3-75 3-blade 69” (1,75 m Ø)pitch 24.0 at r 14.37 inches (0.365 m),full throttle rpm on the groundmax. 4800Propeller rpmapprox. n 21001/min1/minWith propeller Kiev Prop BB 263/1700 3-blade (1,71 m Ø)Pitch 22,0 at r 0,4 m from hub,full throttle rpm on the groundmax. 4800propeller rpmapprox. n 21001/min1/minWith propeller Helix H50F-1,75m-R-SI-12-3 3-blade (1,75 m Ø),Pitch. 16.0 at r 656 mmfull throttle rpm on the groundmax. 4880propeller rpmapprox. n 21501/min1/minPOH C42 Series Issue-4 Rev.307.02.2017Page 18 of 92
C42 SERIES Pilot Operating Handbook1.10 Propellers for Rotax 912 UL SWith propeller WARP DRIVE 3-blade 68” (1,72 m Ø)pitch 25.0 at 15.75 inches (0.40 m) from hub,full throttle rpm on the groundmax. 5200Propeller rpmapprox. n 21501/min1/minWith propeller GSC 3-blade 68” (1,72 m Ø)pitch 25.0 at 15.75 inches (0.40 m) from hub,full throttle rpm on the groundmax. 4900Propeller rpmapprox. n 20001/min1/minWith propeller Neuform CR3-75 3-blade 69” (1,75 m Ø)pitch 27.0 at r 14.37 inches (0.365 m),full throttle rpm on the groundmax. 4900Propeller rpmapprox. n 20001/min1/minWith propeller Neuform CR3-V-R2H 3-blade 69” (1,80 m Ø), adjustablepitch 16 - 30 at r 29.53 inches (0.75 m),full throttle rpm on the groundmax. 4200 - 56001/minPropeller rpmapprox. n 1700 - 23001/minWith propeller Kiev Prop BB 283/1800 3-blade (1,80 m Ø)Pitch 24,0 at r 0,4 m from hub,full throttle rpm on the groundmax. 4900Propeller rpmapprox. n 20001/min1/minWith propeller Helix H50F-1,75m-R-S-14-3 3-blade (1,75 m Ø),Pitch 17.0 bei r 656 mmfull throttle rpm on the groundapprox ca. 4800Propeller rpmapprox ca. n 19751/min1/minWith propeller DUC-Flash-1,75m-3-blade (1,75 m Ø),Pitch 23,5 bei r 0,66 mmfull throttle rpm on the groundapprox ca. 5250Propeller rpmapprox ca. n 21601/min1/minPOH C42 Series Issue-4 Rev.307.02.2017Page 19 of 92
C42 SERIES Pilot Operating Handbook1.11 Engine limitations according to the Rotax operatingmanualTake-off (5 min)Continuous75%65%55%ROTAX 91281 hp / 5800 rpm79 hp / 5500 rpm59 hp / 5000 rpm51 hp / 4800 rpm43 hp / 4300 rpmROTAX 912S100 hp / 5800 rpm95 hp / 5500 rpm69 hp / 5000 rpm61 hp / 4800 rpm51 hp / 4300 rpmType of oilAERO Shell Sport Plus 4(bzw. siehe Rotax Handbuch)Amount of oilmin 0.57 imp. gallons (2.6 l)max 0.67 imp. gallons (3.05 l)Oil temperaturemin 122 F (50 C)min 122 F (50 C)max 284 F (140 C)max 266 F (130 C)optimum 194 -230 F (90 -110 C)Oil pressure:normal operating pressure 29 - 72 psi (2 - 5 bar)(cold start 101.45 psi/7 bar)Fuel: Euro-Super ROZ 95 unleaded (DIN EN 228 with max. 5% ethanol)Super Plus ROZ 98 unleaded (DIN EN 228 with max. 5% ethanol)AVGAS 100 LLAVGAS UL91Fuel pressure2.17 - 5.80 psi (0.15 - 0.4 bar)Cylinder head temp.max. 302 F (150 C)max. 275 F (135 C)optimum 230 F (110 C) optimum 230 F (110 C)Coolant temperature:max.248 F (120 C)Magneto checkrpm dropPOH C42 Series Issue-4 Rev.3optimal 212 F (100 C)at 4000 rpmmax. 300 rpm07.02.2017Page 20 of 92
C42 SERIES Pilot Operating Handbook2Kinds of operation limitations-Aerobatics and manoeuvres with more than 60 bank are prohibited-Daylight, VFR conditions only.-No flight in icing conditions-Do not attempt flight in turbulent conditions or inwinds exceeding 22 kts (40 km/h), and less when it is gusty.-Always follow the appropriate regulations for this category of aircraft.3Operation of the EngineThe Rotax 912 is a 4-cylinder, four stroke, horizontally opposed,water-cooled engine.Never move the prop with theignition (MAG) switches on!Fuel type for four-stroke 912 UL and 912 ULS engine:Super leaded or unleaded (according to DIN EN 228 with max. 5%ethanol), AVGAS 100 LL or AVGAS UL91To start the engine:Main fuel valveElectrical fuel pumpThrottleChokeCarburettor heatIgnition (both magnetos)Propeller blade areaBrakesAfter engine starts, chokeOPENONIDLEOPENOFFONCLEARONCLOSEDIf the engine does not start, repeat the starting procedure.POH C42 Series Issue-4 Rev.307.02.2017Page 21 of 92
C42 SERIES Pilot Operating HandbookIf the engine has been flooded, close main fuel valve, open the throttle to ahalf and start the engine. When the engine starts, quickly reduce the throttleto idle.A four-stroke engine requires a fairly long warm up period. Run
C42 Series Pilot Operating Handbook POH C42 Series Issue-4 Rev.3 07.02.2017 Page 5 of 92 Introduction C42 series aircraft are built in compliance with the airworthiness requirements of various countries and are certified as Microlight,
C42 Series Pilot Operating Handbook POH C42 Series Issue-3_Rev_1 28.01.2014 Page 4 of 91 Introduction C42 series aircraft are built in compliance with the airworthiness requirements of various countries and are certified as Microlight,
Pilot’s Operating Handbook And FAA Approved Airplane Flight Manual (abridged for KCN Aero Club) N49696 For complete information, consult Pilot’s operating Manual This abbreviated pilot’s handbook contains excerpts of the Cessna 152 Pilot’s Operating Handbook. Standard Temperature Chart added January 2, 2003 Performance - Specifications .
C42 Owner’s Manual (Microlight) Page 5 IKARUS C-42 FLIGHT AND OPERATOR’S MANUAL Preamble A record of all amendments is to be found in the front of this manual. The C42 aircraft is a Microlight, conforming to the definition within BCAR Section S, 1999. To operate the aircraft th
Forecast Pilot Supply & Demand. 26 UND U.S. Airline Pilot Supply Forecast (2016) predicts cumulative pilot shortage of 14,000 by 2026. Boeing Pilot Outlook (2017) projects worldwide growth in pilot demand, with 117,000 pilots needed in North America by 2036. CAE Airline Pilot Demand Outlook (2017) indicates 85,000 new
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o Après MODEL NO./ NO. DE MODELO/ N o DE MODÈLE Le numéro de série est localisé : 'Sur la fiche d informations techniques (2) o Après SERIAL NO. / NUMERO DE SERIE/ NUMÉRO DE SÉRIE : o Saisissez tous les chiffres et le / après SERIAL NO. / NUMERO DE SERIE/ NUMÉRO DE SÉRIE : N'incluez pas les espaces
ACCOUNTING 0452/22 Paper 2 October/November 2017 1 hour 45 minutes Candidates answer on the Question Paper. No Additional Materials are required. READ THESE INSTRUCTIONS FIRST Write your Centre number, candidate number and name on all the work you hand in. Write in dark blue or black pen. You may use an HB pencil for any diagrams or graphs. Do not use staples, paper clips, glue or correction .
