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1. Loss of communications 7700 Emergency pee Zour A Aviation AIRPLANE FLIGHT MANUAL AFM SUPPLEMENT seamen ak AQUILA ATO1 AVE 22 KEYS FOR OTHER VT 02 FUNCTIONS 1 0 To switch on the system press key I O shortly After the start the unit performs the built in test and shows the operating mode For switching off press key I O for at least 3 seconds Release the key when the LCD becomes blank IDENT key pressed activates the Special Position Identification SPI Pulse for 18 seconds identifying your transponder return from others on the air traffic controller s screen The word IDENT will appear in the upper left corner of the display while the IDENT mode is active Pressing the flight ID key invokes the menu to setup the flight ID The Flight ID is transmitted with every Mode S interrogation NOTE The flight id may be changed if required Usually the FID is the callsign of your aircraft unless field 7 of the flight plan contains other data Before each flight check always your flight id has been set correctly VFR To simplify operation the VT 02 provides a pre programmable VFR code which can be invoked by pressing the inner knob of the rotary encoder longer than 2sec The previous active reply code will then be moved to the bottom line inactive area and overwrites the existing active value there If the pre programmed reply code is identical with the reply code in the botto2. 700 operating code Spe A YUILA Aviation AIRPLANE FLIGHT MANUAL AFM SUPPLEMENT tea Ol AQUILA ATO1 AVE 22 4 NORMAL PROCEDURES NOTE The expected coverage of the VT 02 is limited to the line of sight Low altitude or aircraft antenna shielding by the aircraft itself may result in reduced range Range can be improved by climbing to a higher altitude 4 5 3 BEFORE TAXIING 1 Avionic Master Switch ON The transponder will switch into the standby SBY mode The transponder is activated but will not respond to any interrogations from the ATC Secondary Surveillance Radar 5 5 BEFORE TAKE OFF Transponder Mode Selection Key ALT In this mode the transponder will respond in Mode A Mode C and Mode S operation identification and altitude to interrogations from ATC and TCAS equipped aircrafts NOTE Pressing the Mode Selection Key ON activates only Mode A operation of the Transponder The Transponder will respond to interrogations with the identification code only The replies do not include altitude information 4 5 12 AFTER LANDING 1 Transponder Mode Selection Key 5 PERFORMANCE No change to the basic Airplane Flight Manual 6 WEIGHT AND BALANCE The change of the empty weight and corresponding centre of gravity after the installation or removal of the Garrecht VT 02 Mode S Transponder has to be Spe determined and recorded in accordance with section 6 of th
3. AVE 22 1 GENERAL This Supplement provides the information necessary for the efficient operation of the AQUILA AT0O1 when the Mode S Transponder GARRECHT VT 02 is installed It contains a general description of the Transponder its basic operation and its integration into the AQUILA AT01 For a detailed description of the Mode S Transponder GARRECHT VT 02 and full operating instructions refer to the effective issue of the VT 02 User Manual 02 0200 10E The information contained within this Supplement is to be used in conjunction with the complete Airplane Flight Manual Furthermore the VT 02 User Manual should always be carried on board of the aircraft during flight 2 OPERATING LIMITATIONS A connection of the VT 02 with a TCAS collision avoidance system is currently not intended for the AQUILA ATO1 The operating limitations of the basic Airplane Flight Manual apply without any changes or restrictions 3 EMERGENCY PROCEDURES 3 13 3 _ TO TRANSMIT A SIGNAL REPRESENTING LOSS OF ALL COMMUNICATION IN CONTROLLED AIRSPACE Mode Key Press until Mode ALT active Double shaft rotary encoder outer knob Select 7600 operating code Inner knob of the double shaft rotary encoder Push activate 7600 operating code TO TRANSMIT AN EMERGENCY SIGNAL Mode Key Press until Mode ALT active Double shaft rotary encoder outer knob Select 7700 operating code Inner knob of the double shaft rotary encoder Activate 7
4. Aou Aviation AIRPLANE FLIGHT MANUAL AFM SUPPLEMENT ie Aviation AQUILA ATO1 AVE 22 SECTION 9 Airplane Flight Manual Supplement Mode S Transponder GARRECHT VT 02 This AFM Supplement is applicable and must be inserted into Section 9 of the Airplane Flight Manual if the Garrecht VT 02 Mode S Transponder is installed in the AQUILA AT01 The information of this AFM Supplement adds or replaces information of the basic Airplane Flight Manual FID IDENT The technical content of this Airplane Flight Manual Supplement is approved under the authority of DOA No EASA 21J 025 Sch nhagen 19 03 2009 Document No Supersedes Issue FM AT01 1010 322 o oaa oo o 19 03 2009 AVE22 1 A UILA Aviation AIRPLANE FLIGHT MANUAL AFM SUPPLEMENT NA viation AQUILA ATO1 AVE 22 0 1 LIST OF REVISIONS AND AMENDMENTS AN Affected Date of Revision Reason for Amendment Revision Initial Issue minor change MB AT01 00297 2009 19 March 0 2 LIST OF EFFECTIVE PAGES eines e AVE22 1 to A 01 19 03 2009 AVE20 9 0 3 TABLE OF CONTENTS Section 1 GENERAL AVE22 3 Section 2 OPERATING LIMITATIONS AVE22 3 Section 3 EMERGENCY PROCEDURES AVE22 3 Section 4 NORMAL PROCEDURES AVE22 4 Section 5 PERFORMANCE AVE22 4 Section 6 WEIGHT AND BALANCE AVE22 4 Section 7 SYSTEMS DESCRIPTION AVE22 5 Section 8 HANDLING SERVICE AND MAINTENANCE AVE22 9 pee A UILA Aviati AIRPLANE FLIGHT MANUAL AFM SUPPLEMENT viaton AQUILA ATO1
5. GRATION INTO THE AQUILA AT01 The electrical circuits of the Mode S Transponder Garrecht VT 02 are connected to the Avionic Bus of the on board electrical power supply and protected by a 3 A circuit breaker which enables the complete disconnection of the Transponder unit from electric power The circuit breaker is labelled with a placard denoted Transponder and is installed in the right section of the instrument panel among the other circuit breakers Besides of the transponder unit which is installed in the avionic rack in the midsection of the instrument panel a transponder antenna and Altitude Encoder is part of the Transponder system The Altitude Encoder is connected to the on board Static Pressure System and is integrated in the VT 02 transponder The transponder antenna is installed on the lower surface of the cockpit structure below the co pilot s seat For a detailed description of the integration of the Transponder unit into the aircraft and its connection to the on board electrical system as well as its installation into the AQUILA AT01 refer to the effective revision of the Maintenance Manual of the AQUILA AT01 document no MM AT01 1020 100 pee A UILA Aviation AIRPLANE FLIGHT MANUAL AFM SUPPLEMENT viaton AQUILA ATO1 AVE 22 8 HANDLING SERVICE AND MAINTENANCE In order to increase the service life of the VT 02 Mode S Transponder it should always be deactivated during engine start up and shut d
6. e basic Airplane Flight Manual 7 SYSTEMS DESCRIPTION GENERAL The Garrecht VT 02 panel mounted Non Diversity Mode S Transponder is a radio transmitter and receiver that operates on radar frequencies receiving ground radar or TCAS interrogations at 1030 MHz and transmitting a coded response of pulses to ground based radar on a frequency of 1090 MHz The VT 02 is equipped with IDENT capability that activates the Special Position Identification SPI pulse for 18 seconds Mode S transmit receive capability also requires 1090 MHz transmitting and 1030 MHz receiving for Mode S functions In addition to displaying the selected transponder code reply symbol and mode of operation the VT 02 screen also displays pressure altitude The VT 02 transponder is powered on by pressing the I O key After power on a start up page will be displayed while the unit performs a self test To activate the Transponder the ALT BAT Master Switch as well as the Avionics Master Switch has to be in the ON position GARRECHT VT 02 FRONT VIEW FLOG 3706 MODE IDENT GAARRECHT Avioni TRANSPONDER MODE SELECTION KEYS Display SBY Selects the standby mode When in standby mode the transponder will not reply to any interrogations Spe A UILA Aviati AIRPLANE FLIGHT MANUAL AFM SUPPLEMENT re On AQUILA ATO1 AVE 22 Selects MODE A operation of the transponder In this mode the transponder replies to interrogations as indicated by the Reply Symbo
7. l R Replies do not include altitude information Selects MODE A MODE C and MODE S operation of the transponder In ALT mode the transponder replies to identification and altitude interrogations as indicated by the Reply Symbol R Replies to altitude interrogations include the standard pressure altitude received from the internal altitude source Altitude Encoder which is not adjusted for barometric pressure Any time the function ON or ALT is selected the transponder becomes an active part of the Air Traffic Control Radar Beacon System ATCRBS The transponder also responds to interrogations from TCAS equipped airplanes CODE SELECTION Code selection is done with the double shaft rotary encoder providing 4096 active identification codes Rotating the outer knob of the double shaft encoder selects the position of the code to be modified A blinking cursor is indicating the selected position Use the inner knob to modify the value at the selected position When all changes are done press the inner button to activate the modified standby code NOTE The identification code should be entered carefully irrespective if assigned by ATC or using a standard transponder code Important Codes 1200 VFR code for any altitude in the US Refer to ICAO standards 2000 VFR code commonly used in Europe Refer to ICAO standards 7000 VFR code commonly used in Europe Refer to ICAO standards 7600
8. m line active and standby reply code will just be interchanged Function FUNCTION DISPLAY In the upper left corner of the LCD screen the current pressure altitude related to 1013 25 hPa will be shown as Flight Level FL Replies are indicated by a blinking R in the lower left corner of the LCD screen The current mode is shown in the centre of the bottom line of the screen The current Transponder identification Squawk is indicated in the upper right corner of the LCD screen The standby Transponder identification is indicated below The activated mode will be shown centered in the lower row Spe Ao JILA Aviation AIRPLANE FLIGHT MANUAL AFM SUPPLEMENT R A AQUILA ATO1 AVE 22 FAILURE ANNUNCIATION In case of failure the system shows a W on the LCD screen Additionally a frequently repeated audio signal occurs Both can be terminated by pressing the I O key shortly In case of detecting a fatal failure the system will be switched into Standby SBY mode All system operating will be terminated to prevent damages to system components In this case the system screen will show FAIL instead of active and standby reply code No transponder data will be transfered VT 02 MODE S TRANSPONDER FEATURES MODE S DATA TRANSMISSION In addition to 4096 codes and pressure altitude the VT 02 is capable of transmitting airplane registration number or flight ID transponder capability and maximum speed range INTE
9. own since electrical surges during the start up may cause damage to the unit eae FM AT01 1010 322 A 01 19 03 2009 AVE22 9
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