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Diamond Aircraft HK 36 TC, Flight Manual

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Diamond Aircraft HK 36 TC Flight Manual Download Page 121

HK 36 TC with Rotax 912 S3

Flight Manual

Powered Sailplane

Description

Doc. No. 3.01.12-E

Rev. 1

06 Oct 2003

Page 7 - 20

79 l (20.9 US gal)

AVGAS 100 LL,
Auto Super min. 95 RON
leaded or unleaded
usable: 77 l (20.3 US gal)

SAE 15W-40

or according to

Flight Manual

Oil 3.0 l

CAUTION!

DO NOT USE AVIATION

GRADE ENGINE OIL!

Coolant

Coolant

Level

usable

77 l (20.3 gal)

Oil

Temp.

CHT

7.14.4  MISCELLANEOUS PLACARDS

Placard

Place

Remark

next to tank filler
cap

oil filler cap

oil inspection
door in upper
cowling, inside

colored red

coolant dis-
patcher vessel;
equalizing
reservoir

2 pieces

next to caution
light for coolant
level

%

on fuel quantity
indicator

oil and cylinder
head tempera-
ture indicators

Summary of Contents for HK 36 TC

Page 1: ......

Page 2: ...u can expect many hours of incident free flight operation from your powered sailplane Translation of this Flight Manual has been done by best knowledge and judgement In any case the original document...

Page 3: ......

Page 4: ...K 36 TC with Rotax 912 S3 Flight Manual Introduction Rev No Reason Chap ter Page s Date of Revision EASA Approval No ACG verification Date Inserted Signature Doc No 3 01 12 E Rev 1 06 Oct 2003 Page 0...

Page 5: ...6 Oct 2003 06 Oct 2003 06 Oct 2003 06 Oct 2003 06 Oct 2003 Ch Page Date 3 3 1 EASA appr 3 2 EASA appr 3 3 EASA appr 3 4 EASA appr 3 5 EASA appr 3 6 EASA appr 3 7 EASA appr 3 8 EASA appr 3 9 EASA appr...

Page 6: ...06 Oct 2003 06 Oct 2003 06 Oct 2003 06 Oct 2003 06 Oct 2003 06 Oct 2003 6 6 1 6 2 6 3 6 4 6 5 6 6 6 7 6 8 6 9 6 10 6 11 6 12 06 Oct 2003 06 Oct 2003 06 Oct 2003 06 Oct 2003 06 Oct 2003 06 Oct 2003 06...

Page 7: ...IONS an approved chapter 2 EMERGENCY PROCEDURES an approved chapter 3 NORMAL PROCEDURES an approved chapter 4 PERFORMANCE a partly approved chapter 5 MASS WEIGHT AND BALANCE a non approved chapter 6 P...

Page 8: ...12 E Rev 1 06 Oct 2003 Page 1 1 CHAPTER 1 GENERAL Page 1 1 INTRODUCTION 1 2 1 2 CERTIFICATION BASIS 1 2 1 3 WARNINGS CAUTIONS AND NOTES 1 3 1 4 EXPLANATIONS AND ABBREVIATIONS 1 4 1 5 UNITS OF MEASUREM...

Page 9: ...ailplane manufacturer This Flight Manual conforms to the current version of the customer s powered sail plane However any optional equipment COM NAV etc is not considered For their operation the opera...

Page 10: ...ight Manual WARNING Means that the non observation of the corresponding procedure leads to an immediate or important degradation in flight safety CAUTION Means that the non observation of the correspo...

Page 11: ...e relative to the air TAS is CAS corrected for errors due to altitude and tem perature b Meteorological terms Pressure altitude Altitude indicated by the altimeter when the subscale is set to 1013 25...

Page 12: ...d Useful load Occupants baggage and fuel d Miscellaneous ACL Anti Collision Light Strobe Light AGL Above Ground Level CG Center of Gravity ELT Emergency Locator Transmitter GFRP Glass fiber reinforced...

Page 13: ...meters per second kts knots mph miles per hour fpm feet per minute km h 1 852 kts km h 1 609 mph m s x 196 85 fpm Speed of rotation RPM revolutions per minute Mass kg kilograms lb pounds kg x 2 2046 l...

Page 14: ...d Schempp Hirth type air brakes in the upper surface of the wings In order to enable a fast disassembly and a space saving storage the powered sail plane can be furnished with a wing folding mechanism...

Page 15: ...HK 36 TC with Rotax 912 S3 Flight Manual General Doc No 3 01 12 E Rev 1 06 Oct 2003 Page 1 8 1 7 THREE VIEW DRAWINGS...

Page 16: ...HK 36 TC with Rotax 912 S3 Flight Manual General Doc No 3 01 12 E Rev 1 06 Oct 2003 Page 1 9...

Page 17: ...ATOR MARKINGS 2 6 2 4 POWER PLANT FUEL AND OIL 2 7 2 4 1 ENGINE 2 7 2 4 2 ENGINE OIL 2 8 2 4 3 FUEL 2 10 2 4 4 PROPELLER 2 10 2 5 POWER PLANT INSTRUMENT MARKINGS 2 11 2 6 MASS WEIGHT 2 12 2 7 CENTER O...

Page 18: ...limitations instrument markings and basic placards necessary for the safe operation of the powered sailplane its engine standard sys tems and standard equipment The limitations included in this chapte...

Page 19: ...ntrol deflection vRA Rough air speed 210 113 130 Do not exceed this speed except in smooth air and then only with caution Examples of rough air are lee wave rotors thunderclouds etc vA Maneuvering spe...

Page 20: ...heavy gusts lee wave rotors thunderclouds whirlwinds and turbulence at close range to mountain ridges WARNING The maneuvering speed stated on the previous page ap plies to the maximum T O mass of 770...

Page 21: ...climb This airspeed is marked on the air speed indicator with a blue radial line vx Best angle of climb speed 95 51 59 At this airspeed the powered sailplane climbs with the maximum possible an gle of...

Page 22: ...210 46 113 53 130 Normal operating range Lower limit is 1 1 vS1 at max flight mass and most forward CG Upper limit is rough air speed vRA yellow arc 210 261 113 141 130 162 Caution range rough air sp...

Page 23: ...eller through a speed reducing gear with a gear ratio of 2 43 1 The RPM indicator of the powered sailplane indicates the propeller RPM Conse quently all RPM s given in this manual are propeller RPM s...

Page 24: ...imum oil pressure 7 bar 102 psi short term in the event of cold start Normal oil pressure range 2 to 5 bar 29 to 73 psi Oil quantity Minimum oil quantity 2 0 liters 2 1 US qts Maximum oil quantity 3 0...

Page 25: ...HK 36 TC with Rotax 912 S3 Flight Manual Operating Limitations Doc No 3 01 12 E Rev 1 06 Oct 2003 Page 2 9...

Page 26: ...100LL b Automotive fuel min RON 95 EN 228 Super EN 228 Super Plus NOTE Due to its high lead concentration AVGAS causes in creased wear of the valve seats and produces more resi due in the combustion c...

Page 27: ...nstrument Red Line Minimum Limit Green Arc Normal Operating Range Yellow Arc Caution Range Red Line Maximum Limit RPM indicator 600 2260 RPM 2260 2385 RPM 2385 RPM Oil temperature indicator 50 C 122 F...

Page 28: ...f all non lifting parts 610 kg 1345 lb Maximum mass in baggage compartment 12 kg 26 lb Maximum useful load including fuel see Mass Balance Form page 6 5 f Maximum useful load on right seat 110 kg 243...

Page 29: ...ignment and empty mass CG specifications can be found in the Airplane Maintenance Manual Doc No 3 02 21 Section 4 The permissible flight CG range is Maximum forward CG 318 mm 12 52 in aft of datum pla...

Page 30: ...00 WARNING Exceeding the maximum permissible load factors can over stress the powered sailplane 2 10 FLIGHT CREW Solo flights must be conducted from the left seat 2 11 KINDS OF OPERATION The powered...

Page 31: ...g time meter 1 Manifold pressure indicator 1 Oil pressure indicator 1 Oil temperature indicator 1 Cylinder head temperature indicator 1 Fuel quantity indicator 1 Ammeter 1 Fuel pressure warning light...

Page 32: ...when using a battery with a capacity of 18 amp re hours The capacity of the lead accumulator is highly dependent on the temperature There fore the duration of continuous soaring at low ambient tempera...

Page 33: ...t into known icing conditions prohibited This powered sailplane is certified for the following flight operations as of date of original airworthiness certificate DAY VFR Altitude vNE IAS m ft km h kts...

Page 34: ...A DISCHARGED BATTERY DURING FLIGHT 3 6 3 7 3 PROPELLER REMAINS IN FEATHERED POSITION 3 7 3 7 4 ENGINE FAILURE DURING CRUISE 3 9 3 7 5 CARBURETOR ICING 3 10 3 8 FIRE 3 11 3 8 1 ENGINE FIRE DURING STAR...

Page 35: ...der them in the Flight Manual it is absolutely necessary for the pilot to know the powered sailplane and to have knowledge and experience in solving problems that may occur 3 2 CANOPY JETTISON 1 Red c...

Page 36: ...53 mph Behavior with power on See behavior with power off Exception at 50 to 100 power straight and level flight and maximum rearward center of gravity the powered sailplane may perform a stall dive...

Page 37: ...ol stick forward Ailerons neutral After spin movement has terminated 2 Bring rudder in neutral position pull powered sailplane out smoothly 3 6 SPIRAL DIVE RECOVERY There is no tendency to a spiral di...

Page 38: ...el valve check OPEN 2 Electric fuel pump check ON 3 Propeller speed control TAKE OFF 4 Ignition switch BOTH 5 Choke OFF WARNING If the symptoms cannot be eliminated immediately and the engine refuses...

Page 39: ...12 mph 9 Propeller speed control slowly move from FEATHER to TAKE OFF 10 Oil pressure must be available within 10 seconds 11 Choke as required 12 RPM and throttle as required CAUTION After prolonged s...

Page 40: ...s started with the propeller in feathered pitch and the throttle control in IDLE position 1 Electrical equipment OFF 2 Fuel valve OPEN 3 Master switch ON 4 Mode select switch POWER FLIGHT 5 Caution li...

Page 41: ...the feathered position this however increases engine wear 12 Oil pressure must be available within 10 seconds 13 Choke as required 14 RPM and throttle as required 15 Electric fuel pump OFF 16 Electri...

Page 42: ...side temperatures below 10 C 50 F 5 Ignition switch check BOTH 6 Fuel quantity indicator check NOTE If the symptoms cannot be eliminated and the engine re fuses to deliver enough power proceed as foll...

Page 43: ...n the engine RPM and or loss of manifold pressure and or irregular run ning of the engine without a change in the throttle control position the choke position the propeller setting the air speed or th...

Page 44: ...TAKE OFF a If take off can still be aborted 1 Throttle control IDLE 2 Cabin heat switch off 3 Brakes apply bring powered sailplane to a stop 4 Evacuate powered sailplane immediately b If take off cann...

Page 45: ...n heat switch off 6 Master switch OFF 7 Sliding knockout windows open if required 8 Carry out landing without engine power see Paragraph 4 5 5 3 8 3 ENGINE FIRE DURING FLIGHT 1 Airspeed 105 km h 57 kt...

Page 46: ...OTHER EMERGENCIES 3 9 1 MALFUNCTION OR FAILURE OF PROPELLER SPEED CONTROL 1 Throttle control keep RPM in admissible range 2 Airspeed reduce 3 9 2 ICING 1 Leave icing area 2 Constantly move the contro...

Page 47: ...ne reason for illumination if the light does not extinguish Lack of fuel pressure may result in engine failure See NOTE in 3 7 4 ENGINE FAILURE DURING CRUISE page 3 9 3 9 4 CAUTION LIGHT FOR COOLANT L...

Page 48: ...submerge immediately after touching the water and then surface again 1 Parachute harness open 2 Seat harness tighten 3 Approach speed normal 4 Touchdown with minimum speed and air brakes retracted NO...

Page 49: ...REFLIGHT INSPECTION 4 14 4 5 NORMAL PROCEDURES AND RECOMMENDED SPEEDS 4 15 4 5 1 STARTING ENGINE RUN UP TAXIING PROCEDURES 4 15 4 5 2 TAKE OFF AND CLIMB 4 19 4 5 3 FLIGHT INCLUDING IN FLIGHT ENGINE ST...

Page 50: ...placed over the bolt handles to secure the bolts The A and B bolts are fixed to the fuselage at the wing root The A bolt is placed in front of the spar tunnel and the B bolt lies near the trailing ed...

Page 51: ...reach the wires 3 Insert main bolt while moving the wing tip in small circles The aileron and air brake control systems are automatically connected Do not release the wing before the main bolt has be...

Page 52: ...ep wing in its correct position 4 Introduce spar stump into spar tunnel while ensuring the smooth insertion of A and B bolts Connect position lights optional and ACL strobe light optional when the gap...

Page 53: ...dure NOTE When installing or removing the wings ensure that the powered sailplane will not drop onto its nose wheel or tail skid as the center of gravity shifts Winglet installation 1 Clean the bolts...

Page 54: ...NING The elevator control system is not connected automatically 5 Slip the horizontal stabilizer onto both rearward bolts 6 Screw in the fastening bolt to the stop with an 8 mm hexagon key applying mo...

Page 55: ...om dispersing the powered sailplane should not be agitated prior to the drain check 2 Ensure completeness of the onboard documents and ensure that the remaining operating time before the next schedule...

Page 56: ...cure mounting excessive play damage and cracks Check aileron control system for improper connection lack of load transmis sion and interference Check air brakes for incomplete retraction ensure flushn...

Page 57: ...3 full Check engine compartment for obvious defects Check coolers for obstruction 12 Inspection of left main landing gear Check landing gear strut for damage and cracks Check wheel fairing for damage...

Page 58: ...evel check illuminates for approx 3 seconds and extinguishes CAUTION If the caution light for the coolant level does not extinguish coolant must replenished dispatcher vessel located cen trally on the...

Page 59: ...k of propeller FEATHER position Rudder pedals adjust Canopy closed locked Fuel valve OPEN Parking brake set Electrical equipment OFF Master switch ON Mode select switch POWER FLIGHT Caution light for...

Page 60: ...seconds CAUTION If oil pressure is too low turn off engine immediately NOTE When the powered sailplane has been parked for long periods or the hydraulic pressure accumulator is emptied for any other r...

Page 61: ...E Unless the propeller speed control is actuated simulta neously with the ignition switch the propeller will remain in the take off position Propeller feathering is only possible at 500 RPM or above s...

Page 62: ...valve OPEN 4 Fuel quantity checked 5 Canopy locked 6 Seat harness on secure 7 Propeller check 8 Magneto check 9 Carburetor heat OFF 10 Controls free 11 Trim checked 12 Parking brake released 13 Air b...

Page 63: ...PEN 5 Controls free 6 Air brakes check operation lock 7 Parking brake set 8 Electrical equipment OFF 9 Master switch ON 10 Mode select switch POWER FLIGHT 11 Caution light for coolant level illuminate...

Page 64: ...is too low turn off engine immediately NOTE When the powered sailplane has been parked for long periods or the hydraulic pressure accumulator is emptied for any other reason a loss of oil pressure may...

Page 65: ...loading the engine allow the oil temperature to rise to 50 C with the cowl flap open at 1000 to 1500 RPM also possible during taxiing 25 Choke OFF 26 Check ignition circuits at 1700 RPM RPM drop 50 to...

Page 66: ...f the SOARING posi tion wait until propeller speed drops to approximately 1800 RPM Reset to TAKE OFF position Carry out this procedure at least three times CAUTION Unless this procedure is carried out...

Page 67: ...ered sailplane will lift off by itself at approximately 90 km h 49 kts 56 mph 8 Perform climb with at least 95 km h 51 kts 59 mph Monitor oil pressure oil temperature and cylinder head temperature whi...

Page 68: ...FUEL CONSUMPTION CRUISING SPEED ENDUR ANCE RANGE In flight engine stop 1 Throttle control IDLE 2 Electrical equipment OFF WARNING Starting the engine with the electric starter can become impossible a...

Page 69: ...thering will occur with the propeller rotating 6 Cowl flap CLOSE In flight engine start NOTE Starting the engine is possible up to a density altitude of at least 5000 meters 16400 ft 1 Electrical equi...

Page 70: ...essure accumulator The oil pressure indicator may drop to zero for a maximum of 15 seconds 12 Choke push forward as required 13 Electrical equipment as required 14 Oil temperature check 15 Propeller c...

Page 71: ...2 Electric fuel pump ON 3 Power reduce 4 Carburetor heat ON 5 Cowl flap OPEN 6 Trim as required 7 Air brakes as required NOTE The air brake lever is arrested when the air brakes are extended half way...

Page 72: ...s Usually the upper limit is approximately 150 km h 81 kts 93 mph A control force reversal can occur when the rudder is fully deflected and the ailerons are deflected opposite to the rudder To recover...

Page 73: ...Doc No 3 01 12 E Rev 1 06 Oct 2003 Page 4 25 10 Touchdown on main landing gear 11 Wheel brakes apply as required using toe brakes CAUTION The wheels have a differential braking system Apply toe brakes...

Page 74: ...the throttle control first select full throttle and then re tract the air brakes NOTE Climbing is possible with the air brakes fixed in the half extended position 3 Perform climb with at least 95 km...

Page 75: ...the engine takes too much time during final approach 1 Trim as required 2 Air brakes as required NOTE The air brake lever is arrested when the air brakes are extended half way With slightly increased...

Page 76: ...5 6 omitted 4 5 7 HIGH ALTITUDE FLIGHT The never exceed speed vNE is reduced at pressure altitudes above 2000 meters 6500 ft as shown in the following table Pressure altitude Never exceed speed vNE me...

Page 77: ...avy rain should be avoided because of the reduced visibility CAUTION The powered sailplane has no lightning protection system 4 5 9 AEROBATICS CAUTION Aerobatics and spinning are not permitted 4 5 10...

Page 78: ...ed parking or in unpredictable wind conditions the powered sailplane should be moored or stored in a hangar It is also advisable to cover the Pitot tube CAUTION Avoid outdoor parking for prolonged per...

Page 79: ...IRSPEED INDICATOR SYSTEM CALIBRATION 5 3 5 2 2 STALLING SPEEDS 5 4 5 2 3 TAKE OFF PERFORMANCE 5 5 5 3 ADDITIONAL INFORMATION 5 6 5 3 1 DEMONSTRATED CROSSWIND PERFORMANCE 5 6 5 3 2 GLIDE PERFORMANCE AN...

Page 80: ...has been determined on the basis of flight tests with the pow ered sailplane and power plant in good condition with the wheel fairings installed and using average piloting techniques The specified air...

Page 81: ...HK 36 TC with Rotax 912 S3 Flight Manual Performance Doc No 3 01 12 E Rev 1 06 Oct 2003 Page 5 3 5 2 ACG APPROVED DATA 5 2 1 AIRSPEED INDICATOR SYSTEM CALIBRATION...

Page 82: ...vS1 81 km h 87 km h 96 km h 115 km h Stall speeds at different bank angles in kts Air brakes Bank angle 0 30 45 60 retracted vSO 42 kts 45 kts 50 kts 60 kts extended vS1 44 kts 47 kts 52 kts 62 kts St...

Page 83: ...s 56 mph Climb out speed appr 95 km h 51 kts 59 mph Runway level asphalt surface Take off roll 193 m 633 ft Take off distance to clear a 15 m 50 ft obstacle 308 m 1010 ft NOTE For take off distances u...

Page 84: ...f 30 km h 16 kts Landing 30 km h 16 kts 5 3 2 GLIDE PERFORMANCE AND FLIGHT POLAR Minimum rate of descent 1 18 m s 232 fpm at 97 km h 52 kts 60 mph Maximum lift drag ratio 27 at 105 km h 57 kts 65 mph...

Page 85: ...roll s2 Take off distance to clear a 15 m 50 ft obstacle Head wind comp kts OAT C Pressure altitude above MSL QFE 0 m 0 ft 1013 hPa 400 m 1310 ft 966 hPa 800 m 2620 ft 921 hPa 1200 m 3940 ft 877 hPa...

Page 86: ...t s2 ft s1 ft s2 ft s1 ft s2 ft s1 ft s2 ft 0 32 535 860 614 965 712 1089 823 1240 59 623 981 719 1204 837 1257 978 1434 86 728 1112 843 1263 988 1444 1161 1634 5 32 420 709 482 797 558 902 653 1024 5...

Page 87: ...x 16 According to Chapter 10 61 8 dB A According to Chapter 6 for Austria only 62 3 dB A for basic training and towing flight Austrian Federal Law Gazette 29 Oct 1993 738th Decree 5 3 5 CLIMB PERFORMA...

Page 88: ...with a well maintained and correctly adjusted powered sailplane Conditions Pressure altitude 1800 m 5900 ft Prop speed Manif press Fuel flow Cruising speed Endur ance Range Fuel tank capacity RPM inH...

Page 89: ...least 0 7 inHg under the maximum obtainable This reduces the fuel consumption considerably whilst hardly affecting the cruising speed For an economical cruise it is recommended to set the propeller sp...

Page 90: ...RODUCTION 6 2 6 2 WEIGHING PROCEDURE 6 2 6 3 WEIGHING REPORT 6 3 6 4 BASIC EMPTY MASS AND MOMENT 6 4 6 5 MASS OF ALL NON LIFTING PARTS 6 4 6 6 MASS AND BALANCE FORM 6 5 6 7 USEFUL LOAD 6 7 6 7 1 MAXIM...

Page 91: ...in the Airplane Maintenance Manual Doc No 3 02 21 Section 4 WARNING Exceeding the maximum flight mass maximum gross weight can lead to overstressing of the powered sailplane Falling short of the minim...

Page 92: ...ition The Weighing Report is filed in the Airplane Maintenance Log NOTE After equipment changes repair work repainting etc the new empty mass empty weight and the corresponding CG position must be det...

Page 93: ...k and no baggage The CG will not exceed the maximum forward position if not more than 220 kg 485 lb of useful load on the seats and 10 kg 22 lb of fuel for a half hour flight are aboard 6 5 MASS OF AL...

Page 94: ...a record of all weighings The Mass and Balance Form must be updated by an authorized person using the data recorded in the currently effective Weighing Report The corresponding instructions can be fou...

Page 95: ...BALANCE FORM SERIAL NO ________________ CALL SIGN _______________ Date of weighing Empty mass weight Empty mass CG pos aft of datum Max useful load Minimum useful load on seats with full fuel tank Si...

Page 96: ...pit 6 7 2 USEFUL LOAD ON THE SEATS Minimum useful load on the seats The Mass and Balance Form and the limitations placard in the cockpit show the following data Minimum useful load on the seats for so...

Page 97: ...the seats The useful load on one seat must not exceed 110 kg 243 lb Lever arm of useful load on the seats A lever arm of 143 mm 5 63 in aft of datum plane is assumed for all CG calculations 6 7 3 USEF...

Page 98: ...e Mass and Balance Diagram is a supplement to the Mass and Balance Form It gives the pilot the information whether a loading is permissible taking maximum permissible useful load and minimum useful lo...

Page 99: ...oundary hence the loading is permissible Example B Pilot 65 kg 143 lb solo flight Long range tank full 60 kg 132 lb baggage 12 kg 26 lb total mass of fuel and baggage 72 kg 159 lb The loading overstep...

Page 100: ...HK 36 TC with Rotax 912 S3 Flight Manual Mass Balance Doc No 3 01 12 E Rev 1 06 Oct 2003 Page 6 11 Examples...

Page 101: ...HK 36 TC with Rotax 912 S3 Flight Manual Mass Balance Doc No 3 01 12 E Rev 1 06 Oct 2003 Page 6 12...

Page 102: ...KE SYSTEM 7 4 7 5 LANDING GEAR SYSTEM 7 5 7 6 SEATS AND SAFETY HARNESSES 7 6 7 7 BAGGAGE COMPARTMENT 7 6 7 8 COCKPIT 7 7 7 9 POWER PLANT 7 9 7 10 FUEL SYSTEM 7 14 7 11 ELECTRICAL SYSTEM 7 15 7 12 PITO...

Page 103: ...extended at all speeds up to vNE The air brakes have oil dampers but must be locked This is performed by pushing the lever to the forward stop overcoming the resistance occurring after the air brake...

Page 104: ...push rods and the rudder is driven by control cables Elevator control forces can be compensated by means of a spring trim system The aileron and air brake control systems are automatically connected w...

Page 105: ...grip use your feet to push the pedals forward until they lock 7 4 AIR BRAKE SYSTEM There is a blue air brake lever on either side panel By pulling the lever rearward the air brakes are unlocked and e...

Page 106: ...s Parking brake The draw button is located on the center console behind the trim lever The parking brake is released when the button is in the inserted position To set the parking brake draw the butto...

Page 107: ...o fixture for the release cord of parachutes with automatic release Therefore these parachutes cannot be used Each seat is provided with a four part harness To fasten the harness the end pieces must b...

Page 108: ...HK 36 TC with Rotax 912 S3 Flight Manual Powered Sailplane Description Doc No 3 01 12 E Rev 1 06 Oct 2003 Page 7 7 7 8 COCKPIT Optional equipment is marked with asterisks...

Page 109: ...with its deviation table is mounted to the canopy above the instrument panel Cabin heat The draw button for the cabin heat is located in the center console under the instru ment panel Button pulled ou...

Page 110: ...and push it away in an upward direction 7 9 POWER PLANT Engine Liquid cooled 4 cylinder four stroke engine Rotax 912 S3 Crankshaft speeds in parentheses Displacement 1352 cm3 82 5 in3 Max output power...

Page 111: ...r console Carburetor heat Small rectangular lever Lever fully rearward carburetor heat ON The carburetor heat is normally OFF lever fully forward Throttle control Large round lever Lever fully forward...

Page 112: ...s closed during soaring in order to reduce drag At outside temperatures below 0 C 32 F partial closing of the cowl flap avoids continuous operation with an oil temperature below 80 C NOTE Continuous o...

Page 113: ...aulic pressure is needed to reduce the blade pitch Small pitch is achieved by applying hydraulic pressure supplied by the governor A spring moves the propeller to the feathered pitch position Propelle...

Page 114: ...ignition switched OFF The propeller stops rotating only when it is feathered Therefore a propeller brake is not required The propeller governor is flanged to the engine It is driven directly by the e...

Page 115: ...the fuel shut off valve the engine driven fuel pump and finally to the float chambers of the two carburetors Fuel shut off valve The fuel shut off valve is located on the left side of the center conso...

Page 116: ...button for the radio is integrated into the control stick The radio loud speaker is installed in the baggage compartment A backrest mounted connection set for two headsets is optional 7 12 PITOT AND S...

Page 117: ...Cruise Feather 7 13 MISCELLANEOUS EQUIPMENT For the operation of additional avionics refer to the manuals of the respective manu facturers 7 14 PLACARDS INSCRIPTIONS 7 14 1 LIMITATION PLACARDS Limitat...

Page 118: ...pull to close Cabin heat pull ON Cabin Air Fuel Valve OPEN CLOSED Parking Brake pull CANOPY JETTISON Pull both handles fully rearward Push canopy up and away instrument pa nel center sec tion LH and...

Page 119: ...anding IC Fuel Pr Pump Lights Light Fuel Qty Oil Temp Oil Press CHT Generator Battery Main CB Attitude Gyro Direction Gyro Turn Bank 7 14 3 PLACARDS FOR ELECTRICAL EQUIPMENT Placard Place Remark shade...

Page 120: ...d Place Remark Doc No 3 01 12 E Rev 1 06 Oct 2003 Page 7 19 COM GPS NAV ADF MKR COM NAV COM GPS XPDR QDR QDMR Vol Headset Pilot Headset Copilot instrument pa nel RH section next to circuit breakers op...

Page 121: ...light Manual Oil 3 0 l CAUTION DO NOT USE AVIATION GRADE ENGINE OIL Coolant Coolant Level usable 77 l 20 3 gal Oil Temp CHT 7 14 4 MISCELLANEOUS PLACARDS Placard Place Remark next to tank filler cap o...

Page 122: ...No 3 01 12 E Rev 1 06 Oct 2003 Page 7 21 2 3 bar 33 psi 1 8 bar 26 psi next to main wheels 2 pieces next to nose wheel The placard for the Start Check is shown in Section 4 4 PREFLIGHT INSPECTION Plac...

Page 123: ...o 3 01 12 E Rev 1 06 Oct 2003 Page 8 1 CHAPTER 8 POWERED SAILPLANE HANDLING CARE AND MAINTENANCE Page 8 1 INTRODUCTION 2 8 2 POWERED SAILPLANE INSPECTION PERIODS 2 8 3 POWERED SAILPLANE ALTERATIONS OR...

Page 124: ...countered 8 2 POWERED SAILPLANE INSPECTION PERIODS Inspections are scheduled every 100 200 and 600 hours The respective inspection checklists are prescribed in the Airplane Maintenance Manual Doc No 3...

Page 125: ...2 E Rev 1 06 Oct 2003 Page 8 3 8 5 CLEANING AND CARE It is advisable to remove insects with a wet sponge at the end of every flying day CAUTION Excessive dirt accumulation degrades flight performance...

Page 126: ...HK 36 TC with Rotax 912 S3 Flight Manual Supplements Doc No 3 01 12 E Rev 1 06 Oct 2003 Page 9 1 CHAPTER 9 SUPPLEMENTS Page 9 1 GENERAL 9 2 9 2 LIST OF SUPPLEMENTS 9 3...

Page 127: ...ptional equipment of the HK 36 TC Unless otherwise stated the procedures given in the Supplements must be applied in addition to the procedures given in the main part of the Flight Manual All approved...

Page 128: ...LEMENTS Powered sailplane S N Call Sign Date Suppl No Title Rev No Date applicable YES NO 1 Tow Plane Operation 3 06 Oct 2003 9 9 3 Electrical Power Socket for Additional Equipment 1 06 Oct 2003 9 9 5...

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