Aquila AT01 Flight Manual
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Aquila AT01 Flight Manual

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AIRPLANE FLIGHT MANUAL
LBA Approved in Normal Category based on JAR-VLA.
This Airplane Flight Manual must be carried on board the aircraft at all times and be kept within
the reach of the pilot during all flight operations. The amendment history and revision status of
each section of the Airplane Flight Manual are provided in the list of effective pages and in the
list of revisions.
This aircraft must be operated in compliance with the procedures and operating limits specified
herein.
SERIAL NO.:
REGIST. NO.:
Revision A.01 was approved by the Luftfahrt-Bundesamt (LBA) on 30/08/2002 within the scope
of the type-certification. All revisions of section 2, 3, 4 and 5 beyond the scope of documentary
changes are subject to EASA-approval.
Doc. No.
First Issued:
Cover Page Issue No.:
Aviation GmbH
AQUILA AT01
AQUILA AT01-
FM-AT01-1010-100E
05/06/2002
B.04

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  • Page 1 Aviation GmbH AIRPLANE FLIGHT MANUAL AQUILA AT01 LBA Approved in Normal Category based on JAR-VLA. This Airplane Flight Manual must be carried on board the aircraft at all times and be kept within the reach of the pilot during all flight operations. The amendment history and revision status of each section of the Airplane Flight Manual are provided in the list of effective pages and in the list of revisions.
  • Page 2 Section 0 AQUILA AT01 INTRODUCTION With the AQUILA AT01 you have acquired a very efficient training and utility aircraft, which can be operated very easily and which exhibits excellent handling qualities. Reliable operation, handling and maintenance guarantee trouble-free flights and continued airworthiness.

  • Page 3: Table Of Contents

    AIRPLANE FLIGHT MANUAL Aviation Section 0 AQUILA AT01 TABLE OF CONTENTS SECTION GENERAL OPERATING LIMITATIONS (approved section) EMERGENCY PROCEDURES (approved section) NORMAL PROCEDURES (approved section) PERFORMANCE (partly approved section) WEIGHT AND BALANCE DESCRIPTION OF THE AIRCRAFT AND ITS SYSTEMS HANDLING, SERVICE AND MAINTENANCE SUPPLEMENTS Dokument No.:...
  • Page 4 AIRPLANE FLIGHT MANUAL Aviation Section 0 AQUILA AT01 LIST OF EFFECTIVE PAGES Section approved Issue Page Date B.04 0-1 to 0-8 13/04/2015 B.01 1-1 to 1-12 12/07/2012 B.01 2-1 to 2-20 12/07/2012 B.01 3-1 to 3-16 12/07/2012 B.04 4-1 to 4-20...
  • Page 5 A new issue code appears in the footer of the pages of the revised section. The operation of the AQUILA AT01 is only permitted with an Airplane Flight Manual in the current effective status on board the aircraft.
  • Page 6 04/03/2014 supplement winter kit, supplements Garrecht TRX 1500 and 2000 B.04 Documentary changes 0, 4, 7, 9 13/04/2015 Revision B.04 of AFM ref. FM-AT01-1010-100E is approved under the authority of DOA ref. EASA.21J.025. Dokument No.: Issue: Supersedes Issue: Date: Page: FM-AT01-1010-100E B.04...
  • Page 7 AIRPLANE FLIGHT MANUAL Aviation Section 0 AQUILA AT01 RECORD OF REVISIONS When a new revision to the Airplane Flight Manual is issued, the corresponding sections have to be removed and replaced by the pages of the revised sections. Only entire sections will be changed and have to be replaced. Each time, when the incorporation of a revision is accomplished, an endorsement has to be made in the record of revisions shown below.

  • Page 8: Aviation Airplane Flight Manual

    AQUILA AT01 Purchase of Technical Publications To guarantee safe operation and correct maintenance of the aircraft AQUILA AT01, all manuals and technical publications must be kept in the current effective status. All manuals and technical publications relating to the aircraft AQUILA AT01 are available...
  • Page 9 AIRPLANE FLIGHT MANUAL Aviation Section 0 AQUILA AT01 [Intentionally left blank] Dokument No.: Issue: Supersedes Issue: Date: Page: FM-AT01-1010-100E B.04 B.03 (04/03/2014) 13/04/2015 0 - 8...
  • Page 10 Section 4 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 NORMAL PROCEDURES SECTION 4 NORMAL PROCEDURES Page INTRODUCTION AIRSPEEDS FOR NORMAL OPERATION RESERVED PRE-FLIGHT INSPECTION 4.4.1 Daily Pre-flight Check 4.4.2 Check Before Every Flight 4-11 CHECKLISTS FOR NORMAL PROCEDURES 4-13 4.5.1 Before Engine Start-up 4-13 4.5.2...

  • Page 11: Normal Procedures

    Section 4 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 NORMAL PROCEDURES INTRODUCTION This section provides normal operating procedure checklists for the aircraft as well as recommended airspeeds. Additional information is provided in the Operators Manual for ROTAX engine Type 912 series and in the Operation and Installation Manual of mt-Propeller, latest revision.

  • Page 12: Airspeeds For Normal Operation

    Section 4 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 NORMAL PROCEDURES AIRSPEEDS FOR NORMAL OPERATION The following airspeeds are based on the maximum take-off weight of 750 kg. They may be also used for any lower operational weight. TAKE-OFF Airspeed (IAS)
  • Page 13 Section 4 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 NORMAL PROCEDURES CRUISE Airspeed (KIAS) KIAS Maneuvering speed Maximum turbulent air operating speed Maximum flap extended speed Document No.: Issue: supersedes Issue: Date: Page: FM-AT01-1010-100E B.04 B.01 (12/07/2012) 13/04/2015 4 - 4...

  • Page 14: Reserved

    Section 4 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 NORMAL PROCEDURES RESERVED [Intentionally left blank] Document No.: Issue: supersedes Issue: Date: Page: FM-AT01-1010-100E B.04 B.01 (12/07/2012) 13/04/2015 4 - 5...

  • Page 15: Pre-Flight Inspection

    Section 4 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 NORMAL PROCEDURES PRE-FLIGHT INSPECTION 4.4.1 Daily Pre-flight Check CABIN Papers CHECK on board Ignition key REMOVED BAT Switch Warning lights (alternator, ALIGHT fuel pressure) Engine instruments CHECK Fuel quantity CHECK External lights...
  • Page 16 Section 4 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 NORMAL PROCEDURES EXTERIOR CHECK, Visual Inspection CAUTION In this manual, visual inspection means the following: Inspection for mechanical damage, dirt, cracks, delamination, excessive play, looseness, leakages, incorrect attachment, foreign objects and general condition.
  • Page 17 Section 4 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 NORMAL PROCEDURES c) Tire pressure CHECK d) Tire slip marking CHECK e) Tire, wheel, brake Visual inspection f) Brake chocks REMOVE Tail boom a) Tail boom shell Visual inspection b) Skid plate...
  • Page 18 Section 4 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 NORMAL PROCEDURES Nose section, cowling WARNING Before cranking the propeller: Switch OFF the battery and ignition circuits, activate parking brake. WARNING Risk of burning and scalding Carry out pre-flight checks on the cold engine only !
  • Page 19 Section 4 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 NORMAL PROCEDURES c) Air intakes (4 NACA intakes) CHECK if clear d) Radiator / oil cooler intake CHECK if free from obstructions e) Cowling Visual Inspection CHECK Camloc fasteners f) Propeller Visual inspection...

  • Page 20: Check Before Every Flight

    Section 4 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 NORMAL PROCEDURES 4.4.2 Check Before Every Flight NOTE The fuel level dipstick for checking the fuel tank level is stored on the inner side of the baggage compartment door. Daily pre-flight inspection...
  • Page 21 Section 4 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 NORMAL PROCEDURES NOTE The oil specification in paragraph 1.9.1 has to be observed ! 5. Check coolant level Verify coolant level in the overflow bottle, replenish as required. The coolant level must be between the min. and max.

  • Page 22: Checklists For Normal Procedures

    Section 4 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 NORMAL PROCEDURES CHECKLISTS FOR NORMAL PROCEDURES 4.5.1 Before Engine Start-up Daily pre-flight check COMPLETED Passenger briefing COMPLETED Seats ADJUST as required Seat belts and harnesses FASTENED and TIGHTENED Canopy CLOSED and LOCKED...

  • Page 23: Before Taxiing

    Section 4 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 NORMAL PROCEDURES NOTE The oil pressure may rise into the YELLOW ARC RANGE as long as the oil temperature is below the normal operating temperature. NOTE If the engine does not start within 10 seconds, disengage the starter and try again after a cooling down phase of at least 2 minutes.

  • Page 24: Before Take-Off (At The Taxi Holding Position)

    Section 4 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 NORMAL PROCEDURES CAUTION Do not operate the engine at high RPM when taxiing to prevent stone chipping or other damage by foreign objects or splashed water. 4.5.5 Before Take-off (at the Taxi Holding Position)

  • Page 25: Climb

    Section 4 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 NORMAL PROCEDURES 4.5.6 Take-off CAUTION To increase throttle raise RPM first then increase manifold pressure second. To decrease throttle lower manifold pressure first then decrease RPM second. Throttle FULL OPEN Tachometer CHECK if within 2200-2260 RPM...

  • Page 26: Cruise

    Section 4 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 NORMAL PROCEDURES 4.5.8 Cruise Throttle AS REQUIRED (Ref. to Section 5) Propeller control lever SET between 1650 and 2260 RPM NOTE Continuous operation at maximum manifold pressure with propeller speed below 2140 RPM should be avoided to minimize engine wear, especially at pressure altitudes below 3000ft and at high CHT.

  • Page 27: Landing

    Section 4 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 NORMAL PROCEDURES 4.5.10 Landing Seat belts and harnesses CHECK if TIGHT Electrical fuel pump Carburetor heat Throttle AS REQUIRED Airspeed 90 KIAS Flaps TAKE-OFF or LANDING position Trim AS REQUIRED Flaps LANDING position...

  • Page 28: Performance (Partly Approved Section)

    Section 4 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 NORMAL PROCEDURES 4.5.13 Engine Shut-down Throttle IDLE Parking brake Flaps LANDING position CHECK on frequency 121.5 MHz AVIONICS switch Ignition switch Electrical equipment Instrument light BAT switch Brake chocks and tie-downs AS REQUIRED 4.5.14 Flight in Heavy Rain and/or with Very Dirty Wings...

  • Page 29: Intentionally Left Blank

    Section 4 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 NORMAL PROCEDURES [Intentionally left blank] Document No.: Issue: supersedes Issue: Date: Page: FM-AT01-1010-100E B.04 B.01 (12/07/2012) 13/04/2015 4 - 20...

  • Page 30: Description Of The Aircraft And Its Systems

    Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION SECTION 7 DESCRIPTION OF THE AIRCRAFT AND ITS SYSTEMS Page INTRODUCTION AIRFRAME 7.2.1 Fuselage 7.2.2 Wing 7.2.3 Empennage FLIGHT CONTROLS 7.3.1 Aileron Control 7.3.2 Elevator Control and Trim System 7.3.3 Rudder Control 7.3.4...
  • Page 31 Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION SEATS, SEATBELTS AND HARNESSES 7-12 7.6.1 Seat Adjustment 7-13 BAGGAGE COMPARTMENT 7-13 CANOPY 7-14 POWER PLANT 7-15 7.9.1 Engine 7-16 7.9.2 Throttle and Choke 7-17 7.9.3 Propeller and Propeller Control 7-18 7.9.4...
  • Page 32 Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION 7.12 PITOT-STATIC SYSTEM 7-29 7.13 STALL WARNING SYSTEM 7-30 7.14 AVIONICS 7-31 7.15 RESERVED (Intentionally left blank) 7-32 Document No.: Issue: Supersedes Issue: Date: Page: FM-AT01-1010-100E B.04 B.01 (12/07/2012) 13/04/2015...

  • Page 33: Introduction

    Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION INTRODUCTION Section 7 of the Airplane Flight Manual contains a general description of and operating instructions for the aircraft and its systems. Refer to Section 9 for the description of and operating instructions for the optional equipment and systems.

  • Page 34: Airframe

    Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION AIRFRAME The majority of the aircraft structure is constructed in composite design. Glass fibre (GFRP) as well as carbon fibre materials (CFRP) are used that are bedded into an epoxy resin matrix. The aircraft structure consists of both, monolithic GFRP or CFRP shells / structural components and sandwich shells with a structural foam core based on PVC.

  • Page 35: Empennage

    Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION The outboard end of each wing half is shaped into a winglet, which contains the NAV- Lights, Anti-Collision Lights as well as the outlets of the fuel tank vents, to reduce the induced drag of the airplane.

  • Page 36: Elevator Control And Trim System

    Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION 7.3.2 Elevator Control and Trim System The elevator is operated by forward and rearward deflections of either control stick of the dual flight control system. The control input is transferred to the control surfaces solely by push rods. The deflections of the elevator control surfaces are effectively limited by adjustable stops that confine the travel of the control stick.

  • Page 37: Flap Control And Flap Position Indication

    Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION CAUTION Check the proper seat position before every engine start-up to ensure the availability ot the full operating range of the nose wheel steering and the toe brakes. 7.3.4 Flap Control and Flap Position Indication The flaps are operated and fixed in the selected position by an electrical flap actuator.

  • Page 38: Instrument Panel (Standard Equipment)

    AIRPLANE FLIGHT MANUAL Section 7 Aviation AQUILA AT01 SYSTEM DESCRIPTION INSTRUMENT PANEL (Standard Equipment) NOTE: Note: Items 13, 14 and 15 may be arranged The Engine Hour Meter is either installed interchanged among each other with on position 23 as a circular instrument or regard to their installation position.

  • Page 39: Flight Instruments

    Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION 7.4.1 Flight Instruments The flight instruments are located in the instrument panel in front of the pilot’s seat. 7.4.2 Switches and Other Controls The switches for all electrical systems are arranged in a row below the flight instruments on the right side adjacent to the ignition switch.

  • Page 40: Cabin Heat

    Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION 7.4.3 Cabin Heat For the cabin heating, ram air is heated in a shrouded chamber at the exhaust muffler and flows through a duct into the cabin if the heat control valve is opened. Behind the firewall, the heated air is subdivided for windshield defrosting and cabin heating.

  • Page 41: Seats, Seatbelts And Harnesses

    To release the parking brake, push down the control knob up to its end stop. SEATS, SEATBELTS AND HARNESSES The seats of the AQUILA AT01 are fabricated from composite materials and are equipped with integrated safety head rests and removable hard-wearing seat cushions.

  • Page 42: Seat Adjustment

    The seats are locked in place by releasing the push knob. BAGGAGE COMPARTMENT The AQUILA AT01 incorporates a large baggage compartment behind the seats which can be loaded through a lockable baggage door. The baggage compartment is also accessible through the cabin.

  • Page 43: Canopy

    CANOPY The big canopy of the AQUILA AT01 offers an excellent all around view. It consists of a rear portion with a window which is bonded into the fuselage structure and a large one- piece acrylic glass dome bonded into a composite frame that can be swivelled forward to open for a comfortable cabin entry.

  • Page 44: Power Plant

    POWER PLANT The AQUILA AT01 is powered by a ROTAX 912 S engine which is a four-stroke cycle engine with four cylinders horizontally opposed. The normal aspirated engine is in standard configuration equipped with a dual breakerless capacitor discharge ignition system and a reduction gearbox with integrated shock absorbers and overload clutch.

  • Page 45: Engine

    Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION 7.9.1 Engine The ROTAX 912 S engine is equipped with liquid cooled cylinder heads, ram-air cooled cylinders and a dry sump forced lubrication system. The engine has two carburettors, one for the right cylinders and one for the left cylinders of the engine. For oil and engine coolant cooling, a combined oil cooler/radiator is installed in the front part of the lower engine cowling behind the main cooling air intake.

  • Page 46: Throttle And Choke

    Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION CAUTION The specifications for operating fluids issued by ROTAX® Aircraft Engines Inc. for the 912S engine must be adhered to. CAUTION Before every takeoff, a functional check of both ignition circuits must be performed.

  • Page 47: Propeller And Propeller Control

    SYSTEM DESCRIPTION 7.9.3 Propeller and Propeller Control The AQUILA AT01 is equipped with a two-blade hydraulically controlled variable pitch propeller (constant speed propeller) in wood-composite-hybrid design for thrust generation. The propeller blades are constructed with a wooden core covered by glass...

  • Page 48: Fuel System

    The activated Carburettor Heat reduces the engine power. 7.10 FUEL SYSTEM The AQUILA AT01 is equipped with a drainable integral fuel tank in each wing. The fuel capacity of each tank is approximately 60 Litres, the unusable fuel portion is 5.2 Litres per tank.
  • Page 49 Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION CAUTION The electrical fuel pump must be switch on during all take-offs and landings as well as in those cases where too low fuel pressure is indicated by the fuel pressure warning light.

  • Page 50: Fuel Storage And Ventilation

    Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION 7.10.1 Fuel Storage and Ventilation The inner surfaces of the composite integral tanks are coated with a special fuel tank sealant to protect the fibre composite structure against decomposition. To dampen,...

  • Page 51: Electrical Fuel Pump And Fuel Strainer

    Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION In both normal operating positions (LEFT/RIGHT), the fuel supply and corresponding return line of the selected fuel tank are opened, whereas the fuel supply and return line of the other fuel tank are closed. The valve-handle points towards the direction of the fuel tank being selected.

  • Page 52: Fuel Tank Drainage System

    Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION seated on the upper surface of the wing. After pulling the dipstick out of the fuel tank, the fuel level can be determined by the “wetted” area of the dipstick in comparison with the respective engraved markings and may be compared with the electrical fuel level indication on the instrument in the cockpit.

  • Page 53: Electrical System

    7.11 ELECTRICAL SYSTEM The AT01 is equipped with a 12 V direct current (DC) electrical system that is powered by an engine driven alternator and a battery. The electrical equipment is operated and controlled by rocker switches which are located on the lower left section of the instrument panel provided that the red “ALT/BAT”-Master Switch is engaged.

  • Page 54: Ignition System And Starter

    Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION 7.11.2 Ignition System and Starter The engine is equipped with an electronically controlled ignition system of a breakerless capacitor discharge design that has two separate ignition circuits which are independent of each other.
  • Page 55 Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION Fig.: Electrical System Schematic Document No.: Issue: Supersedes Issue: Date: Page: FM-AT01-1010-100E B.04 B.01 (12/07/2012) 13/04/2015 7 - 26...

  • Page 56: Electrical Equipment And Circuit Breakers

    Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION 7.11.3 Electrical Equipment and Circuit Breakers All electrical equipment may be separately turned on or off by circuit breakers of push- pull type or by rocker switches with built-in circuit breaker function.

  • Page 57: Fuel Pressure Warning Light

    Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION 7.11.6 Fuel Pressure Warning Light If the fuel pressure at the fuel distributor in the fuel supply line to the carburettors drops below 0.15 bar, a pressure-controlled switch activates the red fuel pressure warning light located in the upper mid-section of the instrument panel.
  • Page 58 Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION 7.12 PITOT-STATIC SYSTEM Total and Static Pressure are taken from a pitot-static tube installed on the lower surface of the left wing and are transferred through the interior of the wing to the wing- body intersection by total and static pressure lines.
  • Page 59 Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION The pitot-static system error may be ignored for the altitude measurement. An airspeed calibration chart is provided in Section 5 of this manual. While the aircraft is parked on the ground, the pitot-static tube cover delivered with the aircraft and labelled with the tag “Remove Before Flight”...
  • Page 60 Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION 7.14 AVIONICS Depending on the installed optional avionic equipment, a NAV/COM Transceiver, a Transponder or a Multi-functional Display might be located in the centre section of the instrument panel. Detailed information on the operation of this equipment and descriptions of its systems are provided in the associated Airplane Flight Manual Supplements in Section 9.
  • Page 61 Section 7 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SYSTEM DESCRIPTION 7.15 RESERVED [Intentionally left blank] Document No.: Issue: Supersedes Issue: Date: Page: FM-AT01-1010-100E B.04 B.01 (12/07/2012) 13/04/2015 7 - 32...

  • Page 62: Supplements

    9.2. Paragraph 9.2 “Index of Supplements” lists all existing approved AFM supplements for the AQUILA AT01. This table may be also used as a directory for this section, appropriately adapted to your aircraft.
  • Page 63 Section 9 AIRPLANE FLIGHT MANUAL Aviation AQUILA AT01 SUPPLEMENTS INDEX OF SUPPLEMENTS Registration: S/N: AT01- Supplement Title Pages Issue Installed AVE1 Bendix King NAV/COM KX 125 AVE1-1 to 8 A.01 AVE2 Bendix King Transponder KT 76A AVE2-1 to 6 A.01...
  • Page 64 Day-VFR and Night-VFR-Operation AVE23-1 to 18 A.02 ASPEN EFD 1000 – PFD AVE24 AVE24-1 to 8 A.02 ( only SNs listed in SB-AT01-021) AVE25 ASPEN EFD 1000 – MFD AVE25-1 to 8 A.02 GARMIN G500 PFD/MFD System AVE26 AVE26-1 to 10 A.03...

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