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Aero AT-3R100 2004 Flight Manual

Very light aeroplane
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AEROPLANE FLIGHT MANUAL
Aeroplane registration (Call sign): .......................................
Aeroplane Serial No.:
Registered under No:
Approved:
This aeroplane must be operated in accordance with information
Doc. No. ATL3.04
WARSAW
„AERO" Sp. z o. o.
„
03-942 WARSAW, POLAND
UL. WAŁ MIEDZESZYŃSKI 844
for the AT-3R100
VERY LIGHT AEROPLANE
CIVIL AVIATION OFFICE
President of the CAO
( Originally signed for President of the CAO by Mr. Z. Mazan)
and limitations contained in this Manual.
This Manual must be carried in the aeroplane at all times
.......................................
.......................................
Date: 2004-09-23
SEPTEMBER, 2004

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  • Page 1 „AERO” Sp. z o. o. „ 03-942 WARSAW, POLAND UL. WAŁ MIEDZESZYŃSKI 844 AEROPLANE FLIGHT MANUAL for the AT-3R100 VERY LIGHT AEROPLANE Aeroplane registration (Call sign): ........Aeroplane Serial No.: ........Registered under No: ........Approved: CIVIL AVIATION OFFICE President of the CAO ( Originally signed for President of the CAO by Mr.
  • Page 2 „AERO” Sp. z o.o. AT-3 R100 GENERAL INFORMATION Editor: “AERO” Sp. z o.o. O3-942 WARSAW, POLAND UL. WAŁ MIEDZESZYŃSKI 844 Approval of translation has been done to the best knowledge and judgment. In any case, the original Polish language version is authoritive.

  • Page 3: Table Of Contents

    „AERO” Sp. z o.o. GENERAL INFORMATION AT-3 R100 CONTENTS SECTION GENERAL LIMITATIONS EMERGENCY PROCEDURES NORMAL PROCEDURES PERFORMANCE WEIGHT AND BALANCE DESCRIPTION OF THE AEROPLANE AND ITS EQUIPMENT 7 SERVICING SUPPLEMENTS SEPTEMBER, 2004 Page 0-3 AEROPLANE FLIGHT MANUAL...
  • Page 4 „AERO” Sp. z o.o. AT-3 R100 GENERAL INFORMATION GENERAL INFORMATION RECORDING OF REVISIONS RECORDING OF REVISIONS All revisions to this manual, with the exception of actual changes of All revisions to this manual, with the exception of actual changes of All revisions to this manual, with the exception of actual changes of weighing data must be recorded in the table below.
  • Page 5 „AERO” Sp. z o.o. GENERAL INFORMATION AT-3 R100 List of Effective Pages Section Page Date of issue SEPTEMBER, 2004 SEPTEMBER, 2004 SEPTEMBER, 2004 OCTOBER, 2018 MARCH, 2020 NOVEMBER, 2012 NOVEMBER, 2018 JULY, 2010 NOVEMBER, 2018 0-10 JANUARY, 2012 0-11 MARCH, 2020...
  • Page 6 „AERO” Sp. z o.o. AT-3 R100 GENERAL INFORMATION List of Effective Pages (continued Section Page Date of issue Appvd. 2-12 NOVEMBER, 2012 Appvd. 2-13 AUGUST, 2008 Appvd. 2-14 NOVEMBER, 2012 Appvd. 3-1 SEPTEMBER, 2004 Appvd. 3-2 OCTOBER, 2009 Appvd. 3-3 SEPTEMBER, 2004 Appvd.
  • Page 7 „AERO” Sp. z o.o. GENERAL INFORMATION AT-3 R100 List of Effective Pages (continued) Section Page Date of issue Appvd 5-7 SEPTEMBER, 2004 Appvd 5-8 SEPTEMBER, 2004 Appvd 5-9 SEPTEMBER, 2004 Appvd 5-10 SEPTEMBER, 2004 5-11 NOVEMBER, 2012 5-12 NOVEMBER, 2012...
  • Page 8 „AERO” Sp. z o.o. AT-3 R100 GENERAL INFORMATION List of Effective Pages (continued Section Page Date of issue 7-12 SEPTEMBER, 2004 7-13 SEPTEMBER, 2004 7-14 SEPTEMBER, 2004 7-15 JULY, 2010 7-16 JULY, 2010 7-17 JULY, 2010 7-18 JULY, 2010 7-19...
  • Page 9 „AERO” Sp. z o.o. AT-3 R100 GENERAL INFORMATION List of Effective Pages (continued Section Page Date of issue SEPTEMBER, 2004 AUGUST, 2008 JULY, 2009 OCTOBER, 2017 OCTOBER, 2017 SEPTEMBER, 2017 OCTOBER, 2018 NOVEMBER, 2018 9-10 MARCH, 2018 NOVEMBER, 2018 Page 0-9...
  • Page 10 „AERO” Sp. z o.o. AT-3 R100 GENERAL INFORMATION LOG OF REVISIONS No. of Description Revised Date Revision of Revision Pages Introduction of the Supplement 0-5, 0-7 to 0-9, 30.06.2005 No. 21 6-11, 9-4 Introduction of the Supplements 0-5, 0-7 to 0-9, 15.07.2005...
  • Page 11 „AERO” Sp. z o.o. AT-3 R100 GENERAL INFORMATION No. of Description Revised Date Revision of Revision Pages Changing the amount of consumable fuel. 0-5 do 0-7, 0-9, 0-11, Introduction of the Supplements 0-12, 2-12, 2-14, 5-11, 22.11.2012 No. 53 to 55 5-12, 6-12, 7-7, 9-7, 9-8 Changed pages 9.21-9, 9.21-10...
  • Page 12 „AERO” Sp. z o.o. AT-3 R100 GENERAL INFORMATION PAGE INTENTIONALLY LEFT BLANK Page 0-12│ NOVEMBER, 2012 AEROPLANE FLIGHT MANUAL...

  • Page 13: General

    „AERO” Sp. z o.o. SECTION 1 AT-3 R100 GENERAL Section 1 GENERAL Page Introduction.................. 1-2 Basis of certification..............1-3 Warnings, cautions and remarks ..........1-3 Descriptive data................1-4 1.4.1 Airframe..................1-4 1.4.2 Engine ..................1-5 1.4.3 Propeller................... 1-5 View of the aeroplane (three projections) ........1-6 List of definitions and abbreviations..........

  • Page 14: Introduction

    Civil Aircraft Inspection Board is to be notified immediately, and if outside Poland, the local civil aviation authority. Anybody who finds this manual is requested to deliver it promptly to the manufacturer: AERO AT Sp. z o. o. , ul. COP-u 2, 39-300 Mielec, Poland tel.

  • Page 15: Basis Of Certification

    „AERO” Sp. z o. o. SECTION 1 AT-3 R100 NORMAL PROCEDURES 1.2 Basis of certification This aircraft type has been approved by European Aviation Safety Agency in accordance with JAR-VLA regulations, amended through to amendment VLA/92/1 and holds a Type Certificate No. A.021.

  • Page 16: Descriptive Data

    SECTION 1 „AERO” Sp. z o o. GENERAL AT-3 R100 1.4 Descriptive data This AT-3 R100 Very Light Aeroplane is a two-seat, single engine, low wing, all metal aeroplane, with a three-wheel fixed landing gear with a nose wheel. 1.4.1. Airframe: 1.

  • Page 17: Engine

    „AERO” Sp. z o. o. SECTION 1 AT-3R100 GENERAL - Ailerons (angles related to the wing chord) 20 2 - Up 15 2 - Down - Rudder (angles related to the chord of the fin) 30 2 - Each side - Wing flaps (angles related to the wing chord) 0...

  • Page 18: View Of The Aeroplane (Three Projections)

    SECTION 1 „AERO” Sp. z o o. GENERAL AT-3 R100 1.5 View of the aeroplane (three projections) Page 1-6 SEPTEMBER, 2004 AEROPLANE FLIGHT MANUAL...

  • Page 19: List Of Definitions And Abbreviations

    „AERO” Sp. z o.o. SECTION 1 AT-3 R100 GENERAL 1.6 List of definitions and abbreviations The following words or expressions have been used or may be helpful in particular Sections of this manual. Basic speeds and their denotations: IAS – “INDICATED AIRSPEED” means the speed of an air vessel...
  • Page 20 SECTION 1 „AERO” Sp. z o o. GENERAL AT-3 R100 – Maximum never exceed airspeed. This is a limit speed, which cannot be exceeded in any conditions. – Maximum structural cruising speed. This is a limit speed which cannot be exceeded except in non-turbulent conditions, and then, only with care.
  • Page 21 „AERO” Sp. z o.o. SECTION 1 AT-3 R100 GENERAL Meteorological denotations ISA – International Standard Atmosphere. ISA assumptions: - The air is a dry perfect gas - The temperature at sea level is 15 °C / 59° F, - The pressure at sea level is 1013.25 hPa, - The drop in the temperature is 3.25 °C per each 500 m of altitude...
  • Page 22 SECTION 1 „AERO” Sp. z o o. GENERAL AT-3 R100 Terminology used for weights and definition of the centre of gravity of the aeroplane. Maximum takeoff weight – it is the maximum aeroplane weight at the moment of beginning the takeoff Maximum landing weight –...
  • Page 23 „AERO” Sp. z o.o. SECTION 1 AT-3 R100 GENERAL Operational denotations Take-off run – the distance from the location where the aeroplane begins to move, to the location where the aeroplane lifts-off from the takeoff surface. Take-off distance – the distance from the location where the aeroplane begins to move, to the location where the aeroplane reaches the altitude of 15 m / 50 ft.
  • Page 24 SECTION 1 „AERO” Sp. z o o. GENERAL AT-3 R100 THIS PAGE IS LEFT INTENTIONALLY BLANK Page 1-12 SEPTEMBER, 2004 AEROPLANE FLIGHT MANUAL...

  • Page 25: Limitations

    „AERO” Sp. z o. o. SECTION 2 AT-3 R100 LIMITATIONS Section 2 LIMITATIONS Page 2.1. Introduction ................2-2 2.2. Airspeeds.................. 2-2 2.3. Marking of the airspeed indicator..........2-3 2.4. Power plant................2-4 2.5. Marking of the engine monitoring instruments ......2-6 2.6.

  • Page 26: Introduction

    SECTION 2 „AERO” Sp. z o. o. LIMITATIONS AT-3 R100 2.1. Introduction This Section contains the limitations on the operation of this aeroplane, the marking of the instruments and the basic informative placards required for safe operation of the aeroplane, engine, the standard systems and the standard equipment.

  • Page 27: Marking Of The Airspeed Indicator

    „AERO” Sp. z o. o. SECTION 2 AT-3 R100 LIMITATIONS 2.3. Marking of the airspeed indicator The table below shows the markings of the airspeed indicator and the meaning of the colour coding. White sector Range for safe deployment of wing flaps.

  • Page 28: Power Plant

    SECTION 2 „AERO” Sp. z o. o. LIMITATIONS AT-3 R100 2.4. Power plant ENGINE Manufacturer BOMBARDIER-ROTAX Engine model 912S2 OR 912S4 Maximum takeoff power 73.5 kW / 98.5 HP Maximum continuous power 69 kW / 92.5 HP Engine maximum RPM - take-off (5 MIN.)
  • Page 29 „AERO” Sp. z o. o. SECTION 2 AT-3 R100 LIMITATIONS Fuel: Automotive gasoline, unleaded, minimum RON 95 EN228 Premium, EN228 Premium Plus, AVGAS 100LL. Refer to the Rotax 912S Series Engine Operating Manual for limitations and recommendations relating to fuel grades used Oils: The oils, to be marked “SF”...

  • Page 30: Marking Of The Engine Monitoring Instruments

    SECTION 2 „AERO” Sp. z o. o. LIMITATIONS AT-3 R100 2.5. Marking of the engine monitoring instruments Stated below, are the ways in which the engine monitoring instruments are marked, as well as the meanings of the coloured markings. Coloured...

  • Page 31: Weight

    „AERO” Sp. z o. o. SECTION 2 AT-3 R100 LIMITATIONS 2.6. Weight Maximum take-off weight 582 kg / 1283 lb Maximum landing weight 582 kg / 1283 lb Empty, equipped aeroplane weight 350 kg / 772 lb Maximum load in the luggage compartment:...
  • Page 32 SECTION 2 „AERO” Sp. z o. o. LIMITATIONS AT-3 R100 2.7. Limitation of C.G position Distance of the extreme C.G. positions from the leading edge of the Mean Aerodynamic Chord (MAC). WEIGHT 9 9 9 9 [%] MAC Page 2-8...

  • Page 33: Approved Manoeuvres

    „AERO” Sp. z o. o. SECTION 2 AT-3 R100 LIMITATIONS 2.8. Approved manoeuvres The aeroplane is approved to perform the following manoeuvres: - All normal flight manoeuvres - Stall (except tail slide) - Lazy eight - Chandelle - Steep turn not exceeding 60° of bank...

  • Page 34: Controlled Load Factors

    SECTION 2 „AERO” Sp. z o. o. LIMITATIONS AT-3 R100 2.9. Controlled Load Factors The limits of maximum permissible load factors: With wing flaps retracted: -1.5 to +3.8 With wing flaps extended: 0 to +2 2.10. Crew of the aircraft The minimum crew of this aeroplane is 1 pilot 2.11.
  • Page 35 „AERO” Sp. z o. o. SECTION 2 AT-3 R100 LIMITATIONS LIST OF MINIMUM EQUIPMENT SYSTEMS OR DEVICES, VFR DAY* ELECTRIC POWER SYSTEM AND DEVICES 1. Battery 2. Alternator 3. Voltammeter 4. Generator warning light FLIGHT AND NAVIGATION INSTRUMENTS 1. Airspeed indicator 2.

  • Page 36: Fuel

    SECTION 2 „AERO” Sp. z o. o. LIMITATIONS AT-3 R100 2.12. Fuel Fuel tank: capacity: - Total capacity 68.5 litres / 18.09 US gal - Consumable fuel 65.0 litres / 17.7 US gal - Unusable fuel 3.5 litres / 0.92 US gal Approved fuel: - Automotive unleaded gasoline of minimum RON 95.
  • Page 37 „AERO” Sp. z o. o. SECTION 2 AT-3 R100 LIMITATIONS On the instrument panel below of the airspeed indicator MAX MANOEUVRING SPEED = 208 km/h IAS MAX MANOEUVRING SPEED = 112 KTS IAS MAX MANOEUVRING SPEED = 129 MPH IAS...
  • Page 38 SECTION 2 „AERO” Sp. z o. o. LIMITATIONS AT-3 R100 On the fuel tank filler FUEL 65 LITRES UNLEADED MIN RON 95 EN228 Premium/Premium Plus AVGAS 100LL On the oil filler, one from below labels: OIL 3,5 L OIL 3.6 US QTS...

  • Page 39: Emergency Procedures

    „AERO” ,Sp. z o.o. SECTION 3 AT-3 R100 EMERGENCY PROCEDURES Section 3 EMERGENCY PROCEDURES Page 3.1. Introduction ................3-2 3.2. Engine failure................3-2 3.2.1. Engine failure during takeoff ..........3-2 3.2.2. Engine failures in flight ............3-2 3.3. Engine re-starting in flight ............3-3 3.4.

  • Page 40: Introduction

    SECTION 3 „AERO” Sp. z 0.0. EMERGENCY PROCEDURES AT-3 R100 3.1. Introduction Section 3 contains information concerning controlling and procedures, which are to be utilised in emergency situations, and which may occur during aeroplane operation. To prevent danger in emergency situations, the basic indications contained in this section are to be considered and applied as required.

  • Page 41: Engine Re-Starting In Flight

    „AERO” ,Sp. z o.o. SECTION 3 AT-3 R100 EMERGENCY PROCEDURES 3.3. Engine re-starting in flight IAS = 120 km/h / 75 mph / 65 kts • Maintain airspeed To be CHECKED • Fuel quantity in the tank OPEN • Fuel valve Switch ON •...

  • Page 42: Smoke And Fire

    SECTION 3 „AERO” Sp. z 0.0. EMERGENCY PROCEDURES AT-3 R100 3.4. Smoke and fire 3.4.1. Engine fire on ground In case of engine fire on ground take the following steps below: SHUT • Fuel valve FULL OPEN • Throttle •...

  • Page 43: Gliding

    „AERO” ,Sp. z o.o. SECTION 3 AT-3 R100 EMERGENCY PROCEDURES In case of fire in the electrical system IAS = 120 km/h / 75 mph / 65 kts • Maintain airspeed • Electrical equipment TO BE USED • Fire extinguisher (if fire is in the cabin) KEEP OPEN •...

  • Page 44: Landing After Engine Failure

    SECTION 3 „AERO” Sp. z 0.0. EMERGENCY PROCEDURES AT-3 R100 3.6.2. Landing after engine failure EXTEND • Wing flaps to 40º IAS = 100 km/h / 62 mph / 54 kts • Maintain approach airspeed FASTEN FIRMLY • Safety belts UNLOCK •...

  • Page 45: Other Emergency Procedures

    „AERO” ,Sp. z o.o. SECTION 3 AT-3 R100 EMERGENCY PROCEDURES 3.8. Other emergency procedures 3.8.1. Icing • The aeroplane is not equipped with a de-icing system. Therefore the area, where icing conditions exist is to be left as soon as possible.

  • Page 46: Failure Of The Static Or Pitot Pressure Systems

    SECTION 3 „AERO” Sp. z 0.0. EMERGENCY PROCEDURES AT-3 R100 3.8.4. Failure of the static and pitot pressure systems The failure of the flight and navigation instruments might be caused by leakage or constriction of the pipes of the static or pitot pressure systems.

  • Page 47: Normal Procedures

    „AERO” Sp. z o. o. SECTION 4 AT-3 R100 NORMAL PROCEDURES Section 4 NORMAL PROCEDURES Page 4.1. Introduction ................. 4-2 4.2. Rigging and de-rigging the aeroplane ......... 4-2 4.3. Daily pre-flight and post-flight inspection ......4-2 4.4. Preparation for flight............4-4 4.4.1.

  • Page 48: Introduction

    SECTION 4 „AERO” Sp. z o. o. NORMAL PROCEDURES AT-3 R100 4.1. Introduction Section 4 contains the list of inspection tasks and detailed procedures for normal aeroplane operation with standard equipment installed. Normal procedures concerning the optional equipment or systems are contained in Section 9.
  • Page 49 „AERO” Sp. z o. o. SECTION 4 AT-3 R100 NORMAL PROCEDURES - Check the sensor of pitot and static pressure is clean - Check the sediment tanks of the pitot and static pressure systems in the following way: - Unscrew the caps.

  • Page 50: Preparation For Flight

    SECTION 4 „AERO” Sp. z o. o. NORMAL PROCEDURES AT-3 R100 Recommended daily post-flight inspection - Check the fuel, oil and cooling systems for leaks. - Check fixing and general condition of the radio antennas - Check the general condition of the aeroplane and its landing gear.

  • Page 51: Pre-Flight Inspection Of The Aeroplane

    „AERO” Sp. z o. o. SECTION 4 AT-3 R100 NORMAL PROCEDURES 4.4.2. Pre-flight inspection of the aeroplane It is the duty of the pilot to perform a pre-flight inspection prior to the flight or after a break in flights, when he has left the cabin. The inspection is to be made, starting with the cabin and walking clockwise around the aeroplane.
  • Page 52 SECTION 4 „AERO” Sp. z o. o. NORMAL PROCEDURES AT-3 R100 - Ignition – to be set OFF CHECK - Fuel level – to be checked with the gauge CHECK - Battery and generator – to be switched OFF CHECK - All electrical equipment–...
  • Page 53 „AERO” Sp. z o. o. SECTION 4 AT-3 R100 NORMAL PROCEDURES (6.). Starboard landing gear and front part of fuselage Tyre – Check the tyre pressure (visually) CHECK - Brake system CHECK - Oil level and presence of the dipstick...

  • Page 54: Normal Procedures And List Of Inspection Tasks

    SECTION 4 „AERO” Sp. z o. o. NORMAL PROCEDURES AT-3 R100 4.5. Normal procedures and list of inspection tasks 4.5.1. Airspeeds for safe operation Airspeed Flaps km/h Take off: – lift-off 15º – at altitude 15 m Maximum angle of climb (VX) 0º...

  • Page 55: Using An Electric Ground Power Source

    „AERO” Sp. z o. o. SECTION 4 AT-3 R100 NORMAL PROCEDURES 4.5.3. Using an electric ground power source The aeroplane is equipped to use electric power from external sources. A typical power receptacle (of 11041 – type) is installed at the port side of the fuselage, in front of the wing.
  • Page 56 SECTION 4 „AERO” Sp. z o. o. NORMAL PROCEDURES AT-3 R100 Cool engine procedure - Fuel valve – set to OPEN - Starting device (Choke) - Battery and generator - “GENERATOR FAILURE” light - illumination CHECK - Fuel pump - Throttle lever – to be set to...
  • Page 57 „AERO” Sp. z o. o. SECTION 4 AT-3 R100 NORMAL PROCEDURES Hot engine procedure The same as for cool engine start, but without turning the propeller and the starting device (choke) is to be set to OFF. Procedure for low temperature The procedure is the same as for cool engine, but the throttle lever may be set to idle only.

  • Page 58: Before Taxiing

    SECTION 4 „AERO” Sp. z o. o. NORMAL PROCEDURES AT-3 R100 Ignition switch in position “1” Ignition switch in position “2” Ignition switch in position “1 +2” Throttle – full open Maximum engine speed CHECK NOTE Maximum engine speed on ground is 5050 RPM.

  • Page 59: Before Takeoff

    „AERO” Sp. z o. o. SECTION 4 AT-3 R100 NORMAL PROCEDURES 4.5.7. Before take-off - Fastening of the seat belts CHECK - Fuel valve – to be opened CHECK - Fuel pump T T T T - Trim and balancing tab – to be set for take-off...

  • Page 60: Cruise

    SECTION 4 „AERO” Sp. z o. o. NORMAL PROCEDURES AT-3 R100 4.5.10. Cruise - Throttle – as required - Trim and balancing tab – as for cruise - Engine operational parameters – to be MONITORED 4.5.11. Descent - Throttle – as required...

  • Page 61: Engine Shutdown

    „AERO” Sp. z o. o. SECTION 4 AT-3 R100 NORMAL PROCEDURES - Artificial horizon OFF and LOCK -Turn indicator - Transponder 4.5.16. Engine shutdown - Radio transmitter SWITCH OFF - Electrical equipment SWITCH OFF - Throttle – to be set to...

  • Page 62: Flight Manoeuvres

    SECTION 4 „AERO” Sp. z o. o. NORMAL PROCEDURES AT-3 R100 CAUTION! NEVER TRY TO STALL AT LOW ALTITUDE For stall speed – refer to Section 5. NOTE At engine ratings higher than idle, the stalling speed is lower than that given in the table, by 2 to 15 km/h / 1.2 to 9.3 mph / 1 to 8 kts depending on wing flap position and aeroplane weight.

  • Page 63: Operational Speed During Takeoff And Landing

    „AERO” Sp. z o. o. SECTION 4 AT-3 R100 NORMAL PROCEDURES strong crosswind, also turn the aeroplane axis from the landing direction towards the crosswind. Turn back to the landing direction immediately before touchdown. Lowering the nose wheel earlier after touchdown helps to maintain direction.
  • Page 64 SECTION 4 „AERO” Sp. z o. o. NORMAL PROCEDURES AT-3 R100 THIS PAGE IS LEFT INTENTIONALLY BLANK Page 4-18 SEPTEMBER, 2004 AEROPLANE FLIGHT MANUAL...

  • Page 65: Performance

    “AERO” Sp. z o.o. SECTION 5 AT-3 R100 PERFORMANCE Section 5 PERFORMANCE Page 5.1. Introduction ................5-2 5.2. Approved data ................5-3 5.2.1. Calibration of the airspeed indicator system ...... 5-3 5.2.2. Stalling speed..............5-4 5.2.3. Take-off performance............5-5 5.2.4. Landing distance ..............5-6 5.2.5.

  • Page 66: Introduction

    SECTION 5 “AERO” Sp. z o.o. PERFORMANCE AT-3 R100 5.1. Introduction This Section contains approved data concerning the following issues: - Calibration of the airspeed indicator system. - Stalling speeds - Take-off performance. - Supplementary information from the manufacturer. The diagrams have been computed on the basis of actual flight test data, for correct engine and aircraft operation and applying average piloting techniques.

  • Page 67: Approved Data

    “AERO” Sp. z o.o. SECTION 5 AT-3 R100 PERFORMANCE 5.2. Approved data 5.2.1. Calibration of the airspeed indicator system The diagram is based on test flight data. CAS = IAS + δ δ δ δ V δV – aerodynamic correction...

  • Page 68: Stalling Speed

    SECTION 5 “AERO” Sp. z o.o. PERFORMANCE AT-3 R100 5.2.2. Stalling speed Aeroplane maximum weight 582 [kg] Throttle idle Stalling speed km/h km/h 0° 0° 15° 40° 0° 30° 15° 40° 0° 60° 15° 40° Page 5-4 SEPTEMBER, 2004 AEROPLANE FLIGHT MANUAL...

  • Page 69: Take-Off Performance

    “AERO” Sp. z o.o. SECTION 5 AT-3 R100 PERFORMANCE 5.2.3. Take-off performance Conditions: - Maximum weight 582 kg - Airstrip surface concrete - Rating Takeoff power - Wing flap position (for takeoff) 15 ° - Lift-off speed IAS = 77 km/h / 49 mph / 42 kts...

  • Page 70: Landing Distance

    SECTION 5 “AERO” Sp. z o.o. PERFORMANCE AT-3 R100 TAKE-OFF RUN AND TAKE-OFF DISTANCES (continuation) Pressure altitude 1000 [m] (3281 ft) ºC Ambient temperature ºF -5.8 12.2 30.2 48.2 66.2 84.2 Take-off run Take-off distance to H=15m (50 ft) 1450...
  • Page 71 “AERO” Sp. z o.o. SECTION 5 AT-3 R100 PERFORMANCE LANDING DISTANCES Pressure altitude 0 [m] STD ºC Ambient temperature. ºF Landing distance from 15m (50 ft) 1322 1375 1424 1476 1529 1578 Landing run Pressure altitude 500 m (1460 ft) STD ºC...

  • Page 72: Climb Performance

    SECTION 5 “AERO” Sp. z o.o. PERFORMANCE AT-3 R100 5.2.5. Climb performance Wing flaps retracted (0º) Conditions: - Maximum weight 582 kg (1283 lb) - Rating (Power setting) (full) nominal power - Airspeed V =120 km/h / 75 mph / 65 kts IAS This airspeed is to be reduced by 3 km/h for each 1000 m of altitude (0.57 mph / 0.5 kts for each 1000 ft of altitude).
  • Page 73 “AERO” Sp. z o.o. SECTION 5 AT-3 R100 PERFORMANCE CLIMB PERFORMANCE (FLAPS 0° ) Pressure altitude 0 m STD Ambient ºC ºF temperature OAT m/s 4,40 4,30 4,20 4,10 3,96 3,83 Rate of climb ft/m 866 Pressure altitude 500 m (1460 ft) STD Ambient ºC...
  • Page 74 SECTION 5 “AERO” Sp. z o.o. PERFORMANCE AT-3 R100 CLIMB PERFORMANCE (FLAPS 15° ) Pressure altitude 0 m STD Ambient temperature ºC ºF m/s 3,86 3,78 3,69 3,60 3,48 3,37 Rate of climb ft/m Pressure altitude 500 m (1460 ft) STD Ambient temperature ºC...

  • Page 75: Supplementary Information

    “AERO” Sp. z o.o. SECTION 5 AT-3 R100 PERFORMANCE 5.3. Supplementary information 5.3.1. Cruise Airspeed, range and endurance Conditions: - Maximum weight 582 kg (1283 lb) - Wing flaps retracted - Automotive gasoline, unleaded RON 95 - Consumable fuel: 65 litres / 17.17 US GAL...
  • Page 76 SECTION 5 “AERO” Sp. z o.o. PERFORMANCE AT-3 R100 Page 5-12 NOVEMBER, 2012 AEROPLANE FLIGHT MANUAL...

  • Page 77: Climb After Balked Landing

    “AERO” Sp. z o.o. SECTION 5 AT-3 R100 PERFORMANCE 5.3.2. Climb after balked landing It is possible to retract the flaps by hand in not more than 2 sec., without loss of altitude, or abrupt change in angle of attack, or special piloting skill.

  • Page 78: Demonstrated Crosswind On Take-Off And Landing

    SECTION 5 “AERO” Sp. z o.o. PERFORMANCE AT-3 R100 5.3.6. Demonstrated crosswind at take-off and landing Correct aeroplane handling characteristics have been demonstrated during takeoff and landing with the crosswind velocity up to 6 m/sec. (21.6 km/h / 13.4 mph / 11.7 knots).

  • Page 79: Combined Diagram Of Aeroplane Characteristics

    “AERO” Sp. z o.o. SECTION 5 AT-3 R100 PERFORMANCE 5.3.7. Combined diagram of aeroplane characteristics GT-2/173/VRR-FW101SRTC Propeller Maximum aeroplane weight 582 kg Maximum power. wing flaps retracted absolute ceiling static ceiling engine RPM when climbing maximum airspeed rate of climb...

  • Page 80: Noise

    SECTION 5 “AERO” Sp. z o.o. PERFORMANCE AT-3 R100 5.3.8. Noise The outside noise level of the AT-3 R100 aeroplane, determined in accordance with the procedure in Chapter 10 Annex 16 ICAO is: 66.6 +0.35 dB (A), while the permissible level is 70.32 dB (A).

  • Page 81: Weight And Balance

    “AERO” Sp. z o.o. SECTION 6 AT-3 R100 WEIGHT AND BALANCE Section 6 WEIGHT AND BALANCE Page 6.1. Introduction ................6-2 6.2. Weight and Balance Calculation..........6-2 6.3. Weight and Balance Schedule ………………………………..6-9 6.4. AT-3 R100 Equipment List…………………………………….6-10 SEPTEMBER, 2004...

  • Page 82: Introduction

    SECTION 6 “AERO” Sp. z o.o. WEIGHT AND BALANCE AT-3 R100 6.1. Introduction This Section contains the limitations of the useful load, within which the aeroplane may be operated safely. The procedure for weighing aeroplane is contained in the Maintenance Manual of the AT-3 R100 aeroplane.
  • Page 83 “AERO” Sp. z o.o. SECTION 6 AT-3 R100 WEIGHT AND BALANCE Graphical method From the table 6.3:” Weight and Balance schedule” the actual weight and moment of the empty aeroplane should be read off. If on the rear wall of...
  • Page 84 SECTION 6 “AERO” Sp. z o.o. WEIGHT AND BALANCE AT-3 R100 WARNING The total weight of the aeroplane must not be less than 409 kg or greater than 582 kg Using Chart: 2 -”Aircraft loading” it can be verified whether the Centre of Gravity is inside the acceptable marked range (envelope) for the specific maximum weight and moment.
  • Page 85 “AERO” Sp. z o.o. SECTION 6 AT-3 R100 WEIGHT AND BALANCE Weight (kg) SEPTEMBER, 2004 Page 6-5 AEROPLANE FLIGHT MANUAL...
  • Page 86 SECTION 6 “AERO” Sp. z o.o. WEIGHT AND BALANCE AT-3 R100 Weight of the loaded aeroplane (kg) Page 6-6 JULY, 2010 AEROPLANE FLIGHT MANUAL...
  • Page 87 “AERO” Sp. z o.o. SECTION 6 AT-3 R100 WEIGHT AND BALANCE Calculation Method From the table 6.3: “Weight and Balance Schedule” the actual weight and moment of the empty aeroplane should be read off. If on the rear wall of the cockpit is installed the collapsible tow bar to the weight of empty aeroplane +1,5 kg should be added and moment +2,6 kgm should be increased.
  • Page 88 SECTION 6 “AERO” Sp. z o.o. WEIGHT AND BALANCE AT-3 R100 Calculate the arm of the Centre of Gravity of the aeroplane (X Where: M – total moment of the aeroplane Q – total weight of the aeroplane WARNING The Arm of the Centre of Gravity (X ) is measured rearwards from the leading edge of the wing.

  • Page 89: Weight And Balance Schedule

    “AERO” Sp. z o.o. SECTION 6 AT-3 R100 WEIGHT AND BALANCE 6.3 Weight and Balance schedule SEPTEMBER, 2004 Page 6-9 AEROPLANE FLIGHT MANUAL...

  • Page 90: R100 Equipment List

    SECTION 6 “AERO” Sp. z o.o. WEIGHT AND BALANCE AT-3 R100 6.4 AT-3 R100 Equipment list STANDARD EQUIPMENT Name: Airspeed indicator Altimeter Vertical speed indicator Compass Fuel level indicator Variant ..Electronic tachometer Engine monitoring Oil temp. indicator instruments Oil pressure indicator Fuel pressure ind.
  • Page 91 “AERO” Sp. z o.o. SECTION 6 AT-3 R100 WEIGHT AND BALANCE WEIGHT AND BALANCE OPTIONAL EQUIPMENT Type of equipment Type of equipment Model Installed Turn coordinator Turn coordinator 1394T100-7Z Artificial horizon Artificial horizon GH-112 Artificial horizon Artificial horizon R.C. Allen RCA-26AK-2 Directional Gyro Indicator R.C.
  • Page 92 SECTION 6 “AERO” Sp. z o.o. WEIGHT AND BALANCE AT-3 R100 OPTIONAL EQUIPMENT Type of equipment Model Installed Anti-collision strobe WHELEN 70509 Position lights AT3.61.440.0 GPS-VHF Antena AT3.62.400.0 Rotated propeller axis AT3.52.500.0 ELT KANNAD 406 AF-COMPACT Fuel system with additional fuel tank AT3.53.500.0...
  • Page 93 “AERO” Sp. z o.o. SECTION 6 AT-3 R100 WEIGHT AND BALANCE WEIGHT AND BALANCE OPTIONAL EQUIPMENT Type of equipment Type of equipment Model Installed Radio- -transceiver GTR 225A Radio- -transceiver GTN 650 Inertial seat belts Inertial seat belts AT3.76.050.0 Control of the flap on the Control of the flap on the AT3.54.450.0...
  • Page 94 SECTION 6 “AERO” Sp. z o.o. “AERO” Sp. z o.o. WEIGHT AND BALANCE WEIGHT AND BALANCE AT-3 R100 THIS PAGE IS LEFT INTENTIONALLY BLANK THIS PAGE IS LEFT INTENTIONALLY BLANK THIS PAGE IS LEFT INTENTIONALLY BLANK Page 6-14 DECEMBER, 2015...

  • Page 95: Description Of The Aeroplane And Its Equipment

    “AERO” Sp. z o.o. SECTION 7 AT-3 R100 DESCRIPTION OF THE AEROPLANE AND ITS EQUIPMENT Section 7 DESCRIPTION OF THE AEROPLANE AND ITS EQUIPMENT Page 7.1. Introduction ................7-2 7.2. Airframe ..................7-2 7.2.1. Fuselage ................7-2 7.2.2. Wings ................. 7-3 7.2.3.

  • Page 96: Description Of The Aeroplane

    SECTION 7 “AERO” Sp. z o.o. DESCRIPTION OF THE AEROPLANE AT-3 R100 AND ITS EQUIPMENT 7.1. Introduction This Section contains a description of the aeroplane and of its equipment. 7.2. Airframe 7.2.1. Fuselage The fuselage, made of duralumin sheet, has a rectangular section, open in the area of the cabin.

  • Page 97: Wings

    “AERO” Sp. z o.o. SECTION 7 AT-3 R100 DESCRIPTION OF THE AEROPLANE AND ITS EQUIPMENT 7.2.2. Wings The wings are made of aluminium and are connected to the fuselage by means of the main and of the rear spars. The ailerons and the wing flaps are of similar design are connected to the wing by means of flat hinges.

  • Page 98: Slab Tail

    SECTION 7 “AERO” Sp. z o.o. DESCRIPTION OF THE AEROPLANE AT-3 R100 AND ITS EQUIPMENT 7.2.3. Slab tail The tail plane is a slab tail design with a structure similar to the wing, mass balanced, hinged at two points. The trim & balancing tab are contained within the contour of the tail plane.

  • Page 99: Fin And Rudder

    “AERO” Sp. z o.o. SECTION 7 AT-3 R100 DESCRIPTION OF THE AEROPLANE AND ITS EQUIPMENT 7. 7.2.4. Fin and rudder The vertical tail unit consists of fin and rudder. The fin is an integral part of fuselage structure. Fin and rudder 1.

  • Page 100: Flight Control

    SECTION 7 “AERO” Sp. z o.o. DESCRIPTION OF THE AEROPLANE AT-3 R100 AND ITS EQUIPMENT 7.3. Flight control This section contains a description of the control mechanisms of the wing flaps, the ailerons, the elevator, the trim & balancing tab and of the rudder.

  • Page 101: Control Of The Wing Flaps

    “AERO” Sp. z o.o. SECTION 7 AT-3 R100 DESCRIPTION OF THE AEROPLANE AND ITS EQUIPMENT 7.3.2 Control of the wing flaps The wing flaps which are of crocodile type (split flaps) are located below the trailing edge of the wing, between the fuselage and the ailerons.

  • Page 102: Control Of The Elevator

    SECTION 7 “AERO” Sp. z o.o. DESCRIPTION OF THE AEROPLANE AT-3 R100 AND ITS EQUIPMENT 7.3.3. Control of the elevator The slab tail elevator is fixed to the spar of the fin. The scheme of the elevator control is shown in the illustration below.

  • Page 103: Control Of The Trim/Balancing Tab

    “AERO” Sp. z o.o. SECTION 7 AT-3 R100 DESCRIPTION OF THE AEROPLANE AND ITS EQUIPMENT 7.3.4. Control of the trim/balancing tab The trim & balancing tab is fixed to the trailing edge of the slab tail elevator is driven by torsion shaft, self locking screw gear and assembly of levers and pushrods .
  • Page 104 SECTION 7 “AERO” Sp. z o.o. DESCRIPTION OF THE AEROPLANE AT-3 R100 AND ITS EQUIPMENT 7.3.5. Rudder Control The rudder is fixed to the fin. The illustration below shows the schematic of the rudder control. Schematic showing the set-up of the pedals controlling the rudder 1.

  • Page 105: Instrument Panel

    “AERO” Sp. z o.o. SECTION 7 AT-3 R100 DESCRIPTION OF THE AEROPLANE AND ITS EQUIPMENT 7.4. Instrument panel The equipment installed in this aeroplane is specified in the List of Equipment on page 6-4. SEPTEMBER, 2004 Page 7-11 AEROPLANE FLIGHT MANUAL...
  • Page 106 SECTION 7 “AERO” Sp. z o.o. DESCRIPTION OF THE AEROPLANE AT-3 R100 AND ITS EQUIPMENT 1- Port throttle lever 2- Clock * 3- Airspeed indicator 4- Stall warning light * 5- Artificial horizon * 6- Altimeter 7- Vertical speed indicator...
  • Page 107 “AERO” Sp. z o.o. SECTION 7 AT-3 R100 DESCRIPTION OF THE AEROPLANE AND ITS EQUIPMENT 19- Fuel quantity indicator 20- Cylinder head temperature indicator (CHT) 21- Oil pressure indicator 22- “Starter engaged” light 23- “Generator failure” light 24- Compass 25- Tachometer 26- “Fuel reserve”...
  • Page 108 SECTION 7 “AERO” Sp. z o.o. DESCRIPTION OF THE AEROPLANE AT-3 R100 AND ITS EQUIPMENT 30- Volt-Ammeter 31- Hour meter * 32- Carburettor air temperature indicator 33- Fuel pressure indicator 34- Transponder * 35- Radio-transceiver * 36- 12V- DC Supply...

  • Page 109: Landing Gear System

    “AERO” Sp. z o.o. SECTION 7 AT-3 R100 DESCRIPTION OF THE AEROPLANE AND ITS EQUIPMENT 7.5. Landing gear system The aircraft has a three-wheel, fixed landing gear, with nose wheel. The main landing gear is of a flat spring design. The nose wheel is fitted with a rubber shock absorber 7.5.1.
  • Page 110 SECTION 7 “AERO” Sp. z o.o. DESCRIPTION OF THE AEROPLANE AT-3 R100 AND ITS EQUIPMENT Diagram of the braking system Brake fluid container Feeding line Brake cylinder Insulating valve Parking brake valve (option) Brake pressure line Bleeding valve Brake calliper...

  • Page 111: Parking Brake

    “AERO” Sp. z o.o. SECTION 7 AT-3 R100 DESCRIPTION OF THE AEROPLANE AND ITS EQUIPMENT 7.5.2. Parking Brake The parking brake valve is installed in between the seats tunnel and the parking brake lever is accessible from the left seat.
  • Page 112 SECTION 7 “AERO” Sp. z o.o. DESCRIPTION OF THE AEROPLANE AT-3 R100 AND ITS EQUIPMENT Parking Brake AT3.47.100.0 Valve of parking brake AT3.47.100.0 is non-return valve. After set this valve lever “on” is possible to increase pressure inside the breaking system lines and brake the airplane.
  • Page 113 “AERO” Sp. z o.o. SECTION 7 AT-3 R100 DESCRIPTION OF THE AEROPLANE AND ITS EQUIPMENT Parking Brake AT3.47.130.0 Valve of parking brake AT3.47.130.0 is cut-off valve. After set this valve lever “on” is not possible to increase pressure inside the breaking system lines, brake cylinders are cut off from callipers.
  • Page 114 SECTION 7 “AERO” Sp. z o.o. DESCRIPTION OF THE AEROPLANE AT-3 R100 AND ITS EQUIPMENT 7.6. Seats, seat belts and harness The seat position is permanently fixed (not adjustable). The illustration below shows the installation of the seats. Each seat is fitted with adjustable safety belts.

  • Page 115: Luggage Compartment

    “AERO” Sp. z o.o. SECTION 7 AT-3 R100 DESCRIPTION OF THE AEROPLANE AND ITS EQUIPMENT 7.7. Luggage compartment The luggage compartment is located behind the seats and consists of two containers (see illustration). The containers are fitted with lids made of metal, locked by latches.

  • Page 116: Canopy

    SECTION 7 “AERO” Sp. z o.o. DESCRIPTION OF THE AEROPLANE AT-3 R100 AND ITS EQUIPMENT 7.8. Canopy The canopy consists of an epoxy fibreglass composite frame and of profiled acrylic sheet. The canopy can be moved forward, rotating around an axis located in front of the cabin. After entering the cabin...

  • Page 117: Power Unit

    “AERO” Sp. z o.o. SECTION 7 AT-3 R100 DESCRIPTION OF THE AEROPLANE AND ITS EQUIPMENT 7.9. Power unit 7.9.1. Engine Rotax 912S2 or 912S4 engine - Four-stroke, opposed, four cylinder engine - Cylinder heads cooled with fluid, cylinders cooled with air...

  • Page 118: Fuel System

    SECTION 7 “AERO” Sp. z o.o. DESCRIPTION OF THE AEROPLANE AT-3 R100 AND ITS EQUIPMENT 7.10. Fuel system The fuel is contained in the fuel tank, which is located between the instrument panel and the firewall. The fuel tank, made of composite, is contained in a sack, made of fabric resistant to smoke and to fuel.
  • Page 119 “AERO” Sp. z o.o. SECTION 7 AT-3 R100 DESCRIPTION OF THE AEROPLANE AND ITS EQUIPMENT Diagram of the fuel system Fuel tank Filler cap with the measuring stick Coarse fuel filter Fuel level sensor Reserve fuel sensor Reserve fuel signalling lamp...

  • Page 120: Pitot And Static Pressure Systems

    SECTION 7 “AERO” Sp. z o.o. DESCRIPTION OF THE AEROPLANE AT-3 R100 AND ITS EQUIPMENT 7.11. Pitot and static pressure systems The sensors [9] and [8] receive air under pitot and static pressure and transmit it to the airspeed indicator [3], altimeter [2] , vertical speed indicator [1] and altitude encoder[7](option) -see the scheme on the illustration.

  • Page 121: Electric System

    “AERO” Sp. z o.o. SECTION 7 AT-3 R100 DESCRIPTION OF THE AEROPLANE AND ITS EQUIPMENT 7.12. Electrical system The source of on board electric power is the generator and the battery. It is a 12 Volt system. Automatic circuit breakers located on the instrument panel protect the system.
  • Page 122 SECTION 7 “AERO” Sp. z o.o. DESCRIPTION OF THE AEROPLANE AT-3 R100 AND ITS EQUIPMENT Automatic circuit breaker (permanently switched on) Switch with automatic circuit breaker (switched manually) Switch (switched manually) Page 7-28 JULY, 2010 AEROPLANE FLIGHT MANUAL...

  • Page 123: Aeroplane Equipment

    “AERO” Sp. z o.o. SECTION 7 AT-3 R100 DESCRIPTION OF THE AEROPLANE AND ITS EQUIPMENT 7.13. Aeroplane equipment A detailed list of standard aeroplane equipment, as well as of the possible optional equipment is given in the Maintenance Manual of the AT-3 R100 aeroplane.
  • Page 124 SECTION 7 “AERO” Sp. z o.o. DESCRIPTION OF THE AEROPLANE AT-3 R100 AND ITS EQUIPMENT 7.13.2. Carburettor heating installation Closing of the air flow from the cold air inlet causes suction of the hot air from the engine compartment through the heat exchanger located above the muffler.

  • Page 125: Air Intake Covers

    “AERO” Sp. z o.o. SECTION 7 AT-3 R100 DESCRIPTION OF THE AEROPLANE AND ITS EQUIPMENT 7.13.3 Air intake covers In case of airplane operation in low ambient temperature it is recommended that intake air covers are used to reduce the intensity of the cooling effect.
  • Page 126 SECTION 7 “AERO” Sp. z o.o. DESCRIPTION OF THE AEROPLANE AT-3 R100 AND ITS EQUIPMENT THIS PAGE IS LEFT INTENTIONALLY BLANK Page 7-32 JULY, 2010 AEROPLANE FLIGHT MANUAL...

  • Page 127: Servicing

    “AERO” Sp. z o.o. SECTION 8 AT-3 R100 SERVICING Section 8 SERVICING Page 8.1. Introduction ................8-2 8.2. Scheduled aeroplane inspections..........8-2 8.3 Aeroplane repair or modification..........8-3 8.4. Ground servicing............... 8-3 8.4.1. Relocating the aeroplane on ground ........8-4 8.4.2.

  • Page 128: Introduction

    SECTION 8 “AERO” Sp. z o.o. SERVICING AT-3 R100 8.1. Introduction This Section contains procedures for the correct control of the aeroplane on the ground and servicing, recommended by the aeroplane manufacturer. also contains some requirements concerning inspections and basic maintenance, which are to be observed in order to maintain the performance and reliability of a new aeroplane.

  • Page 129: Ground Servicing

    “AERO” Sp. z o.o. SECTION 8 AT-3 R100 SERVICING 8.3 Aeroplane repairs or modifications Any repair or modification of the aeroplane design may only be performed by authorized personal. NOTE Prior to any modification of the aeroplane, ensure with the Civil...

  • Page 130: Relocating The Aeroplane On Ground

    SECTION 8 “AERO” Sp. z o.o. SERVICING AT-3 R100 8.4.1. Relocating the aeroplane on ground If using the towing bar on a level surface, one person is able to move the aeroplane. The towing bar is to be fixed to the nose wheel ferrules.

  • Page 131: Parking

    “AERO” Sp. z o.o. SECTION 8 AT-3 R100 SERVICING Collapsible tow bar installed on rear wall in the cockpit 1. Taw bar 3. Ferrule of tow bar handle 2. Safety pin 4. Ferrules of tow bar forks 9 9 9 9 8.4.2.
  • Page 132 SECTION 8 “AERO” Sp. z o.o. SERVICING AT-3 R100 Collapsible tow bar installed on the control stick and rudder pedals 1. Catch pawl 4. Control stick grip 2. Safety pin 5. Rudders pedals 3. Tow bar 6. Tow bar handle...

  • Page 133: Tying Down

    “AERO” Sp. z o.o. SECTION 8 AT-3 R100 SERVICING 8.4.3. Tying down There are lugs for the tie-down ropes on the aeroplane. They are located under the wingtips, at the rear of the aeroplane (tail skid) and at the front (nose landing gear ferrules).

  • Page 134: Lifting

    SECTION 8 “AERO” Sp. z o.o. SERVICING AT-3 R100 8.4.4. Lifting When jacking the aeroplane the following procedure should be followed: 1. Put a stand (under a rib) under each wing to prevent the aeroplane from tilting. NOTE. Instead of using jacks, the aeroplane may also be lifted by hand, when holding the lower fuselage edges in the area between the firewall and the wing and in front of the horizontal stabilizer.

  • Page 135: Levelling

    “AERO” Sp. z o.o. SECTION 8 AT-3 R100 SERVICING 8.4.5. Levelling After lifting, the aeroplane should be levelled, so that the cabin wall edges are horizontal (see the illustration). SPIRIT LEVEL EDGES OF CABIN WALLS JUNE, 2010 Page 8-9 AEROPLANE FLIGHT MANUAL...

  • Page 136: Cleaning And Basic Maintenance

    SECTION 8 “AERO” Sp. z o.o. SERVICING AT-3 R100 8.5. Cleaning and basic maintenance It is essential for the reliability of the aeroplane components to always keep them clean. 8.5.1. External painted surfaces Prior to cleaning, take the following steps: - Protect the wheels, especially the brake discs, covering them.

  • Page 137: Glass Panels

    “AERO” Sp. z o.o. SECTION 8 AT-3 R100 SERVICING 8.5.2. Glass panels The greatest care should be taken to avoid scratches when cleaning glass panels of Plexiglas. Never wipe the glass panels when dry. Rinse the panel with clean water or solution of mild soap and then wipe with soft clean cloth, sponge or chamois-leather.

  • Page 138: Propeller

    SECTION 8 “AERO” Sp. z o.o. SERVICING AT-3 R100 8.5.3. Propeller The propeller is to be cleaned in the same way as the painted surfaces, but with great care. 8.5.4. Engine The engine is to be cleaned as indicated in the Engine Maintenance Manual.

  • Page 139: Supplements

    “AERO” Sp. z o.o. SECTION 9 AT-3R100 SUPPLEMENTS Section 9 SUPPLEMENTS Page 9.1. Introduction ................... 9-2 9.2. List of introduced supplements ............. 9-2 SEPTEMBER, 2004 Page 9-1 AEROPLANE FLIGHT MANUAL...
  • Page 140 SECTION 9 “AERO” Sp. z o.o. SUPPLEMENTS AT-3R100 9.1. Introduction This section contains relevant supplements needed for safe operation of the aeroplane when equipped with supplementary systems, installed by the aeroplane manufacturer and specified below. 9.2. List of introduced supplements Introduced.
  • Page 141 “AERO” Sp. z o.o. SECTION 9 AT-3R100 SUPPLEMENTS Introduced. Document number Title of the supplement introduced Date, Signature Artificial horizon R.C. Allen Supplement No. 9 4 Pages RCA-26AK-2 Directional gyro R.C. Allen Supplement No. 10 4 Pages RCA15AK-1 Mitchell Clock 99500-ELT Supplement No.
  • Page 142 SECTION 9 “AERO” Sp. z o.o. SUPPLEMENTS AT-3R100 Introduced. Document number Title of the supplement introduced Date, Signature TRIM TAB Supplement No. 20 6 Pages AT3.33.070.0 Supplement No. 21 ELPROP 3-1-1P Propeller 12 Pages KX 125 Nav/Com System Supplement No. 22...
  • Page 143 “AERO” Sp. z o.o. SECTION 9 AT-3R100 SUPPLEMENTS Introduced. Document number Title of the supplement introduced Title of the supplement introduced Date, Signature Supplement No. 31 Fuel system with additional fuel tank Fuel system with additional fuel tank 26 Pages Supplement No.
  • Page 144 SECTION 9 “AERO” Sp. z o.o. “AERO” Sp. z o.o. SUPPLEMENTS AT-3R100 Introduced. Document number Title of the supplement introduced Title of the supplement introduced Date, Signature Supplement No. 42 Artificial Horizon 4200-10/11 4 Pages Supplement No. 43 VFR Night (glass cockpit) 8 Pages Supplement No.
  • Page 145 “AERO” Sp. z o.o. SECTION 9 AT-3R100 SUPPLEMENTS Introduced. Document number Title of the supplement introduced Date, Signature Supplement No. 53 Artificial Horizon RCA 2600 6 Pages Supplement No. 54 Flight Hour Meter 4 Pages WINTER QUARTZ 1510 FSZM Supplement No. 55 30°...
  • Page 146 SECTION 9 “AERO” Sp. z o.o. “AERO” Sp. z o.o. SUPPLEMENTS AT-3R100 Introduced. Document number Title of the supplement introduced Title of the supplement introduced Date, Signature Supplement No. 64 DAVTRON M800 Series Clocks 6 Pages Supplement No. 65 ROTAX 912iSc Sport engine 46 Pages Supplement No.
  • Page 147 “AERO” Sp. z o.o. SECTION 9 AT-3R100 SUPPLEMENTS Introduced. Document number Title of the supplement introduced Title of the supplement introduced Date, Signature Supplement No. 74 FLARM 8 Pages LXNAV FlarmMouse Supplement No. 75 Wing fuel tanks 26 Pages Supplement No. 76...
  • Page 148 SECTION 9 “AERO” Sp. z o.o. SUPPLEMENTS AT-3R100 PAGE INTENTIONALLY LEFT BLANK Page 9-10 MARCH, 2018 AEROPLANE FLIGHT MANUAL...

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