Aeroprakt Ltd. A-32 Pilot Operating Handbook Download Page 1

 

Aeroprakt Ltd. 

24, Polevaya str., Kiev, Ukraine 

Tel: 0038 044 496-77-21 

Fax: 0038 044 496-77-31 

e-mail: 

[email protected]

 

www.aeroprakt.kiev.ua

 

 

AEROPRAKT

-

32

 

Pilot Operating Handbook

 

A32

-

048

-

POH

 

 

Airplane Model: 

AEROPRAKT-32 (A-32) 

Airplane Registration Number: 

 

Airplane Serial Number: 

048 

Date of issue: 

12.01.2018 

Approved by:    

Yuriy Yakovlyev 

Position: 

Chief designer 

Date of approval: 

12.01.2018 

This manual must be carried in the airplane at all times. 

This airplane is to be operated in compliance with information and limitations contained herein. 

Summary of Contents for A-32

Page 1: ...g Handbook A32 048 POH Airplane Model AEROPRAKT 32 A 32 Airplane Registration Number Airplane Serial Number 048 Date of issue 12 01 2018 Approved by Yuriy Yakovlyev Position Chief designer Date of app...

Page 2: ...e 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 blac...

Page 3: ...rgency procedures 10 3 1 General 10 3 2 Emergency checklists 10 4 Normal Procedures 15 4 1 General 15 4 2 Preflight check 15 4 3 Engine starting 17 4 4 Taxiing 18 4 5 Before takeoff 18 4 6 Normal take...

Page 4: ...mpartment 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 48 8 4 Approved...

Page 5: ...n and Manufacture of Reciprocating Spark Ignition Engines for Light Sport Aircraft F2506 13 Standard Specification for Design and Testing of Light Sport Aircraft Propellers F2745 15 Standard Specifica...

Page 6: ...2 22 m Wheel base 4 ft 2 in 1 27 m Wheel track 5 ft 9 in 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 10...

Page 7: ...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 spee...

Page 8: ...ctor limits 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...

Page 9: ...normal maximum 0 15 0 4 bar 2 2 5 8 psi 0 5 bar 7 26 psi Fuel antiknock properties min RON 95 min AKI 911 European standard EN 228 super EN 228 super plus Aviation standard AVGAS 100 LL ASTM D910 Oil...

Page 10: ...bandon cockpit 5 Take measures to extinguish the fire 3 2 2 Engine failure during takeoff 3 2 2 1 during takeoff roll 1 Throttle IDLE 2 Ignition OFF 3 Brakes APPLY as necessary 3 2 2 2 immediately aft...

Page 11: ...valves CLOSE 5 Landing area SELECT consider altitude and wind No place suitable for landing use recovery system 6 Emergency call TRANSMIT 121 5 MHz or nearest airfield frequency 7 Flaps EXTEND FULLY o...

Page 12: ...h 59 kts best glide 3 Oil pressure CONTROL 4 Oil pressure normal follow PRECAUTIONARY LANDING procedure see section 3 2 6 5 Oil pressure high follow EMERGENCY LANDING procedure see section 3 2 5 3 2 1...

Page 13: ...the blockage airspeed indicator reading either does not change with changing airspeed in level flight or reduces during a steady descent or increases during a steady climb 1 Airspeed indicator reading...

Page 14: ...l quantity indicator 1 IGNORE powerplant instruments readings 2 Engine rpm CONTROL by engine noise 3 Follow PRECAUTIONARY LANDING procedure see section 3 2 6 3 2 16 Loss of flight controls 1 Elevator...

Page 15: ...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 coo...

Page 16: ...rface 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 hin...

Page 17: ...AVAILABLE 7 Baggage container BAGGAGE SECURED CONTAINER CLOSED 8 Starter key REMOVED 9 All electrical switches OFF 10 Flight instruments INTACT CHECK READINGS 11 Movements of controls check FREE and F...

Page 18: ...NGAGE BRAKES 4 5 Before takeoff 1 Hold position OCCUPY 2 Brakes ENGAGE 3 Coolant temperature CHECK minimum 140 F 60 C 4 Oil temperature CHECK minimum 120 F 50 C 5 Fuel level CHECK 6 Fuel valves CHECK...

Page 19: ...temperature max 130 C 266 F 4 9 Cruise 1 Flight altitude OCCUPY and monitor in strong turbulence at least 100 m 300 ft 2 Cruise speed SET in strong turbulence min 100 km h 54 kts max 151 km h 81 kts 3...

Page 20: ...al 90 km h 49 kts 10 km h 5 kts in rain or strong turbulence 4 Direction ALIGN the airplane WITH THE RUNWAY using rudder pedals 5 Side drift ELIMINATE by banking against the drift crosswind if any 6 F...

Page 21: ...fied 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 5 5 m s 1080 fpm Maximum rate of climb at VY 6 m s 1180 fpm 5 4 Cruise s...

Page 22: ...e 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 replacement removal installati...

Page 23: ...1 026 Total 599 0 1 320 8 1013 1 87 949 XCG Total moment Total weight 1 691 66 6 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 subsecti...

Page 24: ...AEROPRAKT 32 Pilot Operating Handbook A32 048 POH 24 No Equipment description and Part No Weight kg CG arm m...

Page 25: ...c The fuselage is an all metal semimonocoque structure The 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...

Page 26: ...tax GmbH Co KG Austria The engine is has the flat four layout dry sump lubrication system with a separate oil tank of 3 l 0 8 US gal capacity automatic valve clearance adjustment two carburetors mecha...

Page 27: ...landing gear beam The drain valve allows draining fuel through the hole in the bottom rear panel of fuselage The drain valve itself is located under the protecting cover separating it from the cables...

Page 28: ...AEROPRAKT 32 Pilot Operating Handbook A32 048 POH 28 Fig 3 Fuel system schematic...

Page 29: ...ol system see Fig 4 is combined it consists of two 4 0 mm 5 32 cables passing through a block of pulleys and a fairlead bellcrank and pushrod Push and pull forces are applied by the pilot to the yoke...

Page 30: ...seats and is accessible for both pilots The trim tab control lever is connected with cables 2 to the trim tab control bellcrank 3 The cables are running through the flexible sheaths 6 in the central...

Page 31: ...ttached to the nose landing gear strut is connected to the pedals with the right 4 and left 5 pushrods The right 6 and left 7 cables connect the pedals to the rudder arms The cable routing is ensured...

Page 32: ...and left 10 bellcranks Then the control force is passed from the outer bellcranks to the flaperons via the outer pushrods 11 The inner bellcranks hinged on the flap extension mechanism beam 12 are co...

Page 33: ...AEROPRAKT 32 Pilot Operating Handbook A32 048 POH 33 Fig 8 Flap extension mechanism Aileron drooping flap extension angles 1st position 10 1 2nd position 20 1...

Page 34: ...Rearmost throttle lever position corresponds to MIN engine RPM the foremost position to MAX engine RPM Pulling the friction force adjusting lever back increases the throttle lever friction pushing it...

Page 35: ...AEROPRAKT 32 Pilot Operating Handbook A32 048 POH 35 Fig 10 Engine pre start mixture control Fig 1 Carburettor heating control...

Page 36: ...b 3 forward the shutter is set to its lower open position and ambient cold air comes through the air intake on top of the engine cowling To set the carburettor heating to ON PULL the control knob back...

Page 37: ...The master cylinder 1 is connected with a hose 8 to the extension tank 7 installed on the firewall in the engine compartment When the brake lever is pulled the brake pads squeeze the brake disc creat...

Page 38: ...AEROPRAKT 32 Pilot Operating Handbook A32 048 POH 38 7 8 Instrument panel This airplane has the following flight instruments set and instrument panel arrangement Fig 12 Instrument panel...

Page 39: ...M MAX TAKEOFF MASS 600 KG 1320 LB LIMIT LOAD FACTOR 4 0 2 0 4 Carburetor heating control knob and marking 5 Cockpit heating control knob and marking 6 Left tank fuel level indicator and marking 7 Righ...

Page 40: ...ircraft disassembly The full and static pressure lines are connected to the airspeed indicator s Static pressure for altimeter and vertical speed indicator is supplied from the cockpit Good condition...

Page 41: ...em 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...

Page 42: ...AEROPRAKT 32 Pilot Operating Handbook A32 048 POH 42 Fig 14 Wiring diagram of A 32 electrical system main...

Page 43: ...AEROPRAKT 32 Pilot Operating Handbook A32 048 POH 43 Fig 15 Wiring diagram for installation of the autopilot servo...

Page 44: ...AEROPRAKT 32 Pilot Operating Handbook A32 048 POH 44 Fig 16 Wiring diagram for installation of the Dynon D 10A flight instrument Fig 17 Wiring diagram for installation of the TRIG TY91 radio...

Page 45: ...AEROPRAKT 32 Pilot Operating Handbook A32 048 POH 45 Fig 18 Wiring diagram for installation of the TRIG TT21 transponder Fig 19 Wiring diagram for installation of PTT and disengage autopilot buttons...

Page 46: ...he 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 13Ba...

Page 47: ...AEROPRAKT 32 Pilot Operating Handbook A32 048 POH 47 Fig 20 Recovery system...

Page 48: ...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 struts near...

Page 49: ...oaked 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 wash...

Page 50: ...ecting 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 rear...

Page 51: ...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 t...

Page 52: ...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 disco...

Page 53: ...ith 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 effici...

Page 54: ...pment 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...

Page 55: ...n 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 w...

Page 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 Ele...

Page 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 making...

Page 58: ...limit loads 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 re...

Page 59: ...g propeller 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 tra...

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