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AEROPRAKT-32 Pilot Operating Handbook

A32-iS-129-POH

55

9.7 Actual empty weight and CG position data

This subsection contains information about the actual empty weight and respective CG
position of the airplane. After final assembly, major repair/overhaul, replacement and/or
additional installation of any equipment the aircraft must be weighed and respective weight
and balance data recorded in the table below:

Empty weight CG position Weighed by

Date

Signature

Remarks

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Содержание A32-iS-129-POH

Страница 1: ...Handbook A32 iS 129 POH Airplane Model AEROPRAKT 32 A 32 Airplane Registration Number Airplane Serial Number 129 Date of issue 27 04 2020 Approved by Yuriy Yakovlyev Position Chief designer Date of ap...

Страница 2: ...he present manual except actual weighing data must be recorded in the following table according to information from the Manufacturer New or amended text in the revised pages will be indicated by a bla...

Страница 3: ...ures 11 3 1 General 11 3 2 Emergency checklists 11 4 Normal Procedures 16 4 1 General 16 4 2 Preflight check 16 4 3 Fuel levels fuel valve settings and respective actions 18 4 4 Engine starting 18 4 5...

Страница 4: ...6 7 13 Baggage compartment 46 7 14 Recovery system 46 8 Aircraft Ground Handling and Servicing 48 8 1 Introduction 48 8 2 Towing parking and tie down instructions 48 8 3 Servicing fuel oil and coolant...

Страница 5: ...Standard Specification for Light Sport Aircraft Manufacturer s Continued Operational Safety COS Program F2339 17 Standard Practice for Design and Manufacture of Reciprocating Spark Ignition Engines f...

Страница 6: ...1 75 m Gross weight Maximum Take Off Weight MTOW 1320 lb 600 kg Top speed at sea level ISA conditions 116 kts 215 km h Cruising speed IAS at 1000 ft ISA conditions engine RPM 3500 54 kts 100 km h 3800...

Страница 7: ...t 50 27 VS0 stalling speed at maximum takeoff weight with full flaps Green arc start 60 32 VS stalling speed at maximum takeoff weight with flaps up White arc 50 147 27 79 VS0 to VFE flap extended spe...

Страница 8: ...its G limits Approved maneuvers include turns with bank angles up to 60 side slipping with angles up to 15 level and accelerated stalls without spinning diving at a speed below VNE of 240 km h 130 kts...

Страница 9: ...speed 5800 rpm max 5 minutes Max continuous speed 5500 rpm Idle speed min 1400 rpm Oil pressure maximum minimum normal 7 bar 102 psi for a short period at cold start 0 8 bar 12 psi below 3500 RPM 2 0...

Страница 10: ...meteorological conditions Flight into icing conditions is prohibited 2 8 Crosswind limitation Maximum crosswind component for A 32 airplane is 7 m s 14 kts It is highly recommended to choose upwind d...

Страница 11: ...sh the fire 3 2 2 Engine failure during takeoff 3 2 2 1 during takeoff roll 1 Throttle IDLE 2 Lane A and B OFF 3 Fuel pumps 1 and 2 OFF 4 Brakes APPLY as necessary 3 2 2 2 immediately after takeoff 1...

Страница 12: ...warning lights is not permanently ON 11 EMS lamps A and B ON perform PRECAUTIONARY LANDING see section 3 2 6 3 2 5 Emergency landing without engine power 1 Airspeed 110 km h 59 kts best glide 2 Flaps...

Страница 13: ...Flashing Land at the nearest airfield see section 4 12 Flashing OFF OFF ON Flashing Flashing Flashing ON ON OFF ON Flashing ON ON Perform precautionary landing see section 3 2 6 3 2 9 Loss of oil pre...

Страница 14: ...ped FOLLOW PRECAUTIONARY LANDING procedure see section 3 2 6 3 2 15 Loss of primary instruments 3 2 15 1 ASI failure due to full pressure line blockage Signs of the blockage airspeed indicator reading...

Страница 15: ...achometer oil water and exhaust temperature indicators fuel quantity indicator 1 IGNORE powerplant instruments readings 2 Engine rpm CONTROL by engine noise 3 Follow PRECAUTIONARY LANDING procedure se...

Страница 16: ...rainwater snow frost ice and dirt 3 Rigging CHECK visually 4 External damage NONE 4 2 2 Power plant 1 Propeller and spinner CLEAN INTACT and SECURE 2 Top cowling REMOVE for engine inspection 3 Oil co...

Страница 17: ...surface CLEAN and INTACT 2 Clamps stops REMOVED 3 Horizontal stabilizer attachment fittings and bolts INTACT and SECURE 4 Rudder elevator and trim tab CLEAN and INTACT 5 Rudder elevator and trim tab h...

Страница 18: ...T CHECK READINGS 11 Movements of controls check FREE and FULL 12 Yokes Stick rudder pedals elevator trim tab lever NEUTRAL 13 Flaps RETRACTED 14 Parking brake ON 4 3 Fuel levels fuel valve settings an...

Страница 19: ...ED Cold engine Warm engine a Throttle 2000 RPM 2 minutes b CHECK Oil pressure above 3 bar c Throttle 2500 2600 RPM d Battery charge check ON e Throttle 2500 RPM till oil temp 50 C f Throttle IDLE a Th...

Страница 20: ...5 Fuel level CHECK see 4 3 6 Fuel valves CHECK see 4 3 7 Flaps EXTEND position 1 4 7 Normal takeoff 1 Rudder pedals NEUTRAL 2 Brakes RELEASE 3 Throttle gradually FULL POWER 4 Yoke Stick elevator NEUTR...

Страница 21: ...00 km h 54 kts 2 Flaps EXTEND position 1 Wind stronger 8 m s 16 kts FLAPS UP 3 Elevator trim tab ADJUST as required 4 Approach speed on final 100 km h 54 kts 10 km h 5 kts in rain or strong turbulence...

Страница 22: ...l off at approximately 0 3 m 1 ft Gradually reduce bank and side drift while flaring and leveling off 7 Throttle IDLE 8 Touchdown at minimum speed at the beginning of the runway Avoid touching ground...

Страница 23: ...e specified below Best angle of climb speed VX 100 km h 54 kts Best rate of climb speed VY 120 km h 65 kts Maximum rate of climb at VX 2 8 m s 551 fpm Maximum rate of climb at VY 4 2 m s 827 fpm 5 4 C...

Страница 24: ...ration 6 1 Weight and Balance Chart This subsection contains weighing and CG location data of the aircraft in configuration as built Any permanent modification of the aircraft configuration such as re...

Страница 25: ...11 026 Total 599 6 1 322 1 1019 5 88 503 XCG Total moment Total weight 1 700 66 9 Note XCG must be between 1 529 m and 1 780 m 19 and 37 MAC as shown in Fig 2 6 2 Installed equipment list This subsect...

Страница 26: ...AEROPRAKT 32 Pilot Operating Handbook A32 iS 129 POH 26 No Equipment description and Part No Weight kg CG arm m...

Страница 27: ...he frames are made of 6061T6 aluminum alloy sheets of 0 063 to 0 080 thickness The fuselage skin is made of 2024T3 aluminum alloy sheets of 0 02 to 0 04 thickness Engine cowling is made of composites...

Страница 28: ...ator through the fuel line 12 coarse filter 13 and then through the fuel line 14 the fuel is fed to inlet of the 1st main fuel pump 15 and then to the inlet of the 2nd auxiliary fuel pump 17 The 1st a...

Страница 29: ...ll fill that tank completely and will start escaping it via the vent tube For that reason it is not recommended to operate the engine with both fuel valves open CAUTION If air gets to the fuel lines t...

Страница 30: ...ig 4 is combined it consists of two 4 0 mm 5 32 cables passing through a block of pulleys and a fairlead rocker and pushrod Push and pull forces are applied by the pilot to the control stick 1 is pass...

Страница 31: ...e cables are running through the flexible sheaths 6 in the central console and a fairlead 7 located near frame No 9 The antiservo trim tab is hinged at the trailing edge of the AMHT Tension of the cab...

Страница 32: ...wo pulleys 9 near the frame No 9 Adjustment of the nose landing gear position is achieved with pedals set to neutral position using pushrods 4 and 5 The cable tension and adjustment of the rudder posi...

Страница 33: ...o the outer left and right 7 bellcranks Then the control force is passed from the outer bellcranks to the flaperons via the outer pushrods 8 The inner bellcranks hinged on the flap extension mechanism...

Страница 34: ...r 2 having three holes for the pin 3 on the lever Unfixing is achieved by bending the spring like lever to the right After the pin comes out of the fixer hole the lever can be set to the selected posi...

Страница 35: ...the friction force adjusting lever back increases the throttle lever friction pushing it forward reduces 7 7 6 Brake control system The main wheel brakes Fig 10 are actuated hydraulically using the br...

Страница 36: ...AEROPRAKT 32 Pilot Operating Handbook A32 iS 129 POH 36 Fig 10 Brake control system...

Страница 37: ...AEROPRAKT 32 Pilot Operating Handbook A32 iS 129 POH 37 7 8 Instrument panel This airplane has the following flight instruments set and instrument panel arrangement Fig 11 Instrument panel...

Страница 38: ...marking 6 Cockpit heating control knob and marking 7 Left tank fuel level indicator and marking 8 Right tank fuel level indicator and marking 9 Left tank Fuel Low warning light and marking 10 Right ta...

Страница 39: ...e joints 5 used to disconnect the lines when the left wing is removed during aircraft disassembly The full 2 and static 3 pressure lines are connected to the airspeed indicator The altimeter and verti...

Страница 40: ...tem and consumers from short circuit and must be of appropriate type and size When battery is supplying power to the consumers while alternator is not generating and supplying power to the battery e g...

Страница 41: ...AEROPRAKT 32 Pilot Operating Handbook A32 iS 129 POH 41 Fig 13 Wiring diagram of A 32 electrical system main...

Страница 42: ...AEROPRAKT 32 Pilot Operating Handbook A32 iS 129 POH 42 Fig 14 Wiring diagram of installation of the SV EMS 221 engine instrument...

Страница 43: ...AEROPRAKT 32 Pilot Operating Handbook A32 iS 129 POH 43 Fig 15 Wiring diagram of installation of the SV D1000 flight instrument...

Страница 44: ...AEROPRAKT 32 Pilot Operating Handbook A32 iS 129 POH 44 Fig 16 Wiring diagram of installation of the servo autopilot...

Страница 45: ...AEROPRAKT 32 Pilot Operating Handbook A32 iS 129 POH 45 Fig 17 Wiring diagram for installation of the SV COM 425 radio Fig 18 Wiring diagram for installation of PTT buttons...

Страница 46: ...n the closed position with a lock Both left and right doors have air scoops for ventilation de misting of the glass and providing pilot view for landing in poor visibility conditions snow rain etc 7 1...

Страница 47: ...AEROPRAKT 32 Pilot Operating Handbook A32 iS 129 POH 47 Fig 19 Recovery system...

Страница 48: ...tie down shall be done with its nose into the wind preferably or at least across the wind but never tail to the wind to avoid damaging the control surfaces For tying the airplane down use the wing str...

Страница 49: ...aked in water with addition of mild washing agents Never use gasoline solvents or other aggressive liquids for washing the airplane and especially the cockpit glass Cockpit glass must be finally washe...

Страница 50: ...nnecting the wings it is recommended to insert all the fasteners back and lock them with safety wire or pins not to loose them Also secure with safety wire the spherical bearings in the forward and re...

Страница 51: ...as follows 1 Remove the tail fairing of fuselage 2 Disconnect the control rod from the antiservo trim tab arm 3 Disconnect the control rod from the AFHT arm 4 Unfasten the bolts of the AFHT attachment...

Страница 52: ...in the oil and close all drain openings with plugs remove the oil cooler disconnect electrical system cables connector is installed on the firewall disconnect the throttle and choke control cables dis...

Страница 53: ...with the manuals for that kind of equipment or special instruments Airplane owner pilot must follow the instructions of those manuals and respective subsections of this manual to ensure safe and effi...

Страница 54: ...ipment All equipment installed or replaced in this airplane must be listed in the table below The equipment affecting weight and balance of the airplane must be also listed in the table of the section...

Страница 55: ...ion about the actual empty weight and respective CG position of the airplane After final assembly major repair overhaul replacement and or additional installation of any equipment the aircraft must be...

Страница 56: ...following a Level flight at various airspeeds and engine power settings Elevator trim tab shall be used for trimming the airplane in pitch b Climb at various airspeeds and full power of the engine El...

Страница 57: ...h 54 kts and engine speed adjusted so that in the beginning of the final turn the airplane is at approximately 500 ft 9 It is recommended to make the final turn with a bank angle below 20 While makin...

Страница 58: ...due to that During high speed flight the engine parameters must be monitored and exceeding its operational limits must be prevented To recover from a steep spiral the engine RPM must be reduced first...

Страница 59: ...ropeller thrust Special attention shall be paid to maintaining the airspeed The imitated engine failures shall be done at every leg of the airfield circuit Total time of imitated engine failure traini...

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