Aero AT-3 R100 Operating Handbook
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Aero AT-3 R100 Operating Handbook

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AVIATION TRAINING
Pilot's Operating Handbook
Aero AT3 R100
HA-VOA

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  • Page 1 AVIATION TRAINING Pilot’s Operating Handbook Aero AT3 R100 HA-VOA...
  • Page 2 „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 3 „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 4: 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 5 „AERO” Sp. z o.o. AT-3 R100 GENERAL INFORMATION RECORDING OF REVISIONS All revisions to this manual, with the exception of actual changes of weighing data must be recorded in the table below. The new or corrected text in the corrected pages, is to be marked at the margin with a vertical line and the number of the revision and the date of the revision is to be printed at the bottom of the page.
  • Page 6 „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 AUGUST, 2008 JUNE, 2011 MARCH, 2011 JUNE, 2011 JULY, 2010 JUNE, 2011 0-10 JUNE, 2011 SEPTEMBER, 2004...
  • Page 7 „AERO” Sp. z o.o. AT-3 R100 GENERAL INFORMATION List of Effective Pages (continued Section Page Date of issue Appvd. 2-12 MARCH, 2011 Appvd. 2-13 AUGUST, 2008 Appvd. 2-14 MARCH, 2011 Appvd. 3-1 SEPTEMBER, 2004 Appvd. 3-2 OCTOBER, 2009 Appvd. 3-3 SEPTEMBER, 2004 Appvd.
  • Page 8 „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 MARCH, 2011 5-12 MARCH, 2011...
  • Page 9 „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 10 „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, 2010 JUNE, 2011 JUNE, 2011 Page 0-9 AEROPLANE FLIGHT MANUAL...
  • Page 11 „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 12: 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 13: Introduction

    Aero Sp. Z o. o. 03-942 Warszawa, Miedzeszyński 844, Poland, email aero@post.pl, tel 0048 22 616 20 87 , fax 00 48 22 617 85 28 and if outside Poland, to the local civil aviation authority. Page 1-2 SEPTEMBER, 2004 AEROPLANE FLIGHT MANUAL...

  • Page 14: 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 15: Descriptive Data

    „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. Dimensions: - Span 7.550 m / 24’...

  • Page 16: Engine

    „AERO” Sp. z o.o. SECTION 1 AT-3 R100 GENERAL - Ailerons (angles related to the wing chord) 20° ±2° - Up 15° ±2° - Down - Rudder (angles related to the chord of the fin) 25° ±2° - Each side - Wing flaps (angles related to the wing chord) 0°...

  • Page 17: 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 18: 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 19 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 20 „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 21 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 22 „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 23 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 24: 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 25: 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 26: 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 27: 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 28 „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 29: 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 30: 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 31 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 32: 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 33: 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 34 „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 35: Fuel

    The dual control system enables the aeroplane to be controlled from both the port and starboard seats. 2.14. Limitation placards Placards on the instrument panel: AT-3 R100 AIRPLANE, APPROVED IN ACCORDANCE WITH JAR-VLA FOR VFR-DAY OPERATIONS. FLIGHTS IN KNOWN ICING CONDITIONS PROHIBITED. AEROBATIC MANOEUVRES INCLUDING SPINS PROHIBITED.
  • Page 36 „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 37 SECTION 2 „AERO” Sp. z o. o. LIMITATIONS AT-3 R100 On the fuel tank filler airplane to AT3-054: FUEL 70 LITRES UNLEADED MIN RON 95 EN228 Premium/Premium Plus AVGAS 100LL airplane from AT3-055: FUEL 65 LITRES UNLEADED MIN RON 95...

  • Page 38: 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 39: 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 40: Engine Re-Starting In Flight

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

  • Page 41: 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 42: Gliding

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

  • Page 43: Landing After Engine Failure

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

  • Page 44: 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 45: 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 46: 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 47: Introduction

    Section 9. 4.2. Rigging and de-rigging the aeroplane If de-rigging the aeroplane and preparation for transportation is necessary, refer to Aeroplane Maintenance Manual of AT-3 R100 Aeroplane, Section 2.6 – Transport of the de-rigged Aeroplane 4.3. Daily pre-flight and post-flight inspection...
  • Page 48 „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 49: 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 50: 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 51 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 52 „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 53: 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 54: 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 55 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 56 „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 57: 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 58: 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 59: 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 60: 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 61: 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 62 „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 63 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 64: 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 65: 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 66 “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 67 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 68 “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 15 ° - Wing flap position (for takeoff) - Lift-off speed IAS = 77 km/h / 49 mph / 42 kts...

  • Page 69: 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 70 “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 71: 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 72 “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 73 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 74: 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 – airplane from AT3-055 or “glass cockpit”...
  • Page 75 Pressure altitude Airspeed Consumable fuel Consumable fuel Engine Fuel Endur Endur speed consumption Range Range ance ance Pressure altitude Airspeed Consumable fuel Consumable fuel Engine Fuel Endur Endur speed consumption Range Range ance ance...

  • Page 76: 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 77 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 78: 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 79: Noise

    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 5-16...

  • Page 80: Weight And Balance

    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 6-1 AEROPLANE FLIGHT MANUAL...
  • Page 81 The procedure for weighing aeroplane is contained in the Maintenance Manual of the AT-3 R100 aeroplane. Any change in the weight of the empty aeroplane, e.g. after new equipment is fitted, repairs or re- painting, will necessitate re-calculation of the table 6.3 “Weight and Balance Schedule”...
  • Page 82 “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 83 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 84 Warning When calculating the total moment, values for fuel are negative, so must be deducted from the totals for pilot, passenger and luggage Pilot and passenger fuel luggage Chart: 1 Values of the moments...
  • Page 85 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 86 “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 87 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 88 SERIAL NUMBER CALL SIGN WEIGHT AND MOMENT OF THE EMPTY AEROPLANE (LAST TWO COLUMNS) CHANGE OF WEIGHT DESCRIPTION OF THE DATE SIGNATURE ADDED (+) REMOVED (-) MODIFICARTION MOM. ARM. MOM. [kg] [kgm] [kg] [kgm] [kg] [kgm] New factory built aeroplane with the equipment installed according to the equipment list Chronology of the construction and equipment modifications effecting changes of weight and moment of the aeroplane...
  • Page 89 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 90 “AERO” Sp. z o.o. SECTION 6 AT-3 R100 WEIGHT AND BALANCE OPTIONAL EQUIPMENT Type of equipment Model Installed Turn coordinator 1394T100-7Z Artificial horizon GH-112 Artificial horizon R.C. Allen RCA-26AK-2 Directional Gyro Indicator R.C. Allen RCA15AK-1 Clock M877 Clock ACzS-1 Clock Mitchell...
  • Page 91 SECTION 6 “AERO” Sp. z o.o. WEIGHT AND BALANCE AT-3 R100 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 „Fuel pump on” light AT3.61.630.0...

  • Page 92: 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 93: Introduction

    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 94: 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 95: 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 96: 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 97: 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 98: Control Of The Wing Flaps

    “AERO” Sp. z o.o. SECTION 7 AT-3 R100 DESCRIPTION OF THE AEROPLANE AND ITS EQUIPMENT 1. 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 99: 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 100: 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 101 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 102: 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 103 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 104 “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 105 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 106: 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 107 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 108: 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 109 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 110 “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 111 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 112: 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 113: 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 114: 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 115: 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 116 “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 117: 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 118: 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 119 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 120: 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. The operational instructions for the optional equipment are given in the section 9 – Supplements.
  • Page 121 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 122: 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 123 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 124: 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 125: 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 126: Aeroplane Repair Or Modification

    “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 127: 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 128: 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 129 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 130: 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 131: 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 132: 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 133: 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 134: 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 135: 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 136 AERO Sp. z o.o. SECTION 9 AT-3R100 SUPPLEMENT No. 44 Section 9 SUPPLEMENT No. 44 VFR-NIGHT (analog instruments) OCTOBER, 2010 Page 9.44-1 AEROPLANE FLIGHT MANUAL...
  • Page 137 SECTION 9 AERO Sp. z o.o. SUPPLEMENT No. 44 AT-3R100 Section 1. General The same as for the standard airplane Section 2. Limitations 2.11. Types of operation This aeroplane is approved for flights by day and night in Visual Meteorological Conditions (VMC-Day/Night)
  • Page 138 AERO Sp. z o.o. SECTION 9 AT-3R100 SUPPLEMENT No. 44 LIST OF MINIMUM EQUIPMENT SYSTEMS OR DEVICES VFR Night ELECTRIC POWER SYSTEM AND DEVICES 1. Battery 2. Generator 3. Alternator 4. Generator warning light 5. Alternator warning light LIGHTING 1. Position lights 2.
  • Page 139 SECTION 9 AERO Sp. z o.o. SUPPLEMENT No. 44 AT-3R100 2.14. Limitation placards AT-3 R100 AIRPLANE, APPROVED IN ACCORDANCE WITH JAR-VLA FOR VFR-DAY/NIGHT OPERATIONS. FLIGHTS IN KNOWN ICING CONDITIONS PROHIBITED. AEROBATIC MANOEUVRES INCLUDING SPINS PROHIBITED. OTHER LIMITATIONS ACC. TO AIRPLANE FLIGHT...
  • Page 140 AERO Sp. z o.o. SECTION 9 AT-3R100 SUPPLEMENT No. 44 In purpose to reduce light flesh on the canopy plexi it is recommended to use instrument panel shade assembled per Supplement No 44 „VFR-Night (analog instruments)” to Maintenance Manual. 4.4.2. Pre-flight inspection of the aeroplane Cabin •...
  • Page 141 SECTION 9 AERO Sp. z o.o. SUPPLEMENT No. 44 AT-3R100 4.5.12. Before landing • Landing light 4.5.15. After landing • Landing light • Taxiing light (if necessary) The rest of the section is the same as for the standard aeroplane.
  • Page 142 AERO Sp. z o.o. SECTION 9 AT-3R100 SUPPLEMENT No. 44 7.4. Instrument panel Fig. 1. Instrument panel lighting 1. Dimmer „FLIGHT INSTRUMENTS” 2. Dimmer „ENGINE INSTRUMENTS” 3. Dimmer „COCKPIT LIGHTING” 4. Dimmer „RADIO” 5. Lighting of switches and circuit breakers (light posts) 6.
  • Page 143 SECTION 9 AERO Sp. z o.o. SUPPLEMENT No. 44 AT-3R100 The cabin and instrument lighting consists of four independent circuits: flight and navigation instruments engine monitoring instruments and lighting of switches and circuit breakers. radio equipment cockpit lighting Rotating the knob to the left, to the point detectable switch function causes deactivation of selected circuit of lighting.

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