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Aquila A211 GX Operating Handbook

Aquila a211 gx pilot's operating handbook and faa approved airplane flight manual
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PILOT'S OPERATING HANDBOOK
FAA APPROVED AIRPLANE FLIGHT MANUAL
Model:
Serial Number:
Registration:
Document Number:
First Issue:
Certified according to:
This Pilot's Operating Handbook (POH) must be carried on board the aircraft at all times.
The amendment history and revision status are provided in the list of effective pages and in
the list of revisions.
The aircraft must be operated in compliance with the procedures and operating limits
stated herein.
This manual constitutes the FAA Approved Airplane Flight Manual (AFM) for operation in
the U.S. in accordance with FAR 21.29.
and
AQUILA A211 GX
AQUILA AT01-100
AT01-100C-
FM-AT01-1010-103
28.05.2013
JAR-VLA

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  • Page 1 PILOT’S OPERATING HANDBOOK FAA APPROVED AIRPLANE FLIGHT MANUAL AQUILA A211 GX Model: AQUILA AT01-100 Serial Number: AT01-100C- Registration: Document Number: FM-AT01-1010-103 First Issue: 28.05.2013 Certified according to: JAR-VLA This Pilot's Operating Handbook (POH) must be carried on board the aircraft at all times.
  • Page 2 AQUILA AT01-100C INTRODUCTION With the AQUILA AT01 you have acquired a very efficient training and utility aircraft, which is easy to operate and exhibits excellent handling qualities. To ensure reliable operation and trouble free flight, we recommend that you read this Pilot's Operating Handbook thoroughly and adhere to the operating instructions and recommendations given herein.
  • Page 3 POH / AFM Section 0 AQUILA AT01-100C TABLE OF CONTENTS SECTION GENERAL OPERATING LIMITATIONS (approved section) EMERGENCY PROCEDURES (approved section) NORMAL PROCEDURES (approved section) PERFORMANCE (partly approved section) WEIGHT AND BALANCE AIRCRAFT DESCRIPTION HANDLING AND MAINTENANCE SUPPLEMENTS Document Nr.: Issue:...
  • Page 4 POH / AFM Section 0 AQUILA AT01-100C LIST OF EFFECTIVE PAGES Section Issue Approved Page Date A.03 0-1 to 0-6 08.04.2014 A.02 1-1 to 1-12 15.10.2013 A.02 2-1 to 2-10 15.10.2013 A.02 3-1 to 3-18 15.10.2013 A.02 4-1 to 4-20 15.10.2013...
  • Page 5 Generally only complete sections of the POH will be exchanged and not individual pages. The operation of the AQUILA AT01 is only permitted with a current and up to date POH carried on board. Please refer to the following web page whenever the revision status of your POH is in question.
  • Page 6 POH / AFM Section 0 AQUILA AT01-100C Revision A.03 of AFM ref. FM-AT01-1010-103 is approved under the authority of DOA ref. EASA.21J.025. Document Nr.: Issue: Supersedes Issue: Date: Page: FM-AT01-1010-103 A.03 A.02 (15.10.2013) 08.04.2014 0 – 5...
  • Page 7 AQUILA AT01-100C PURCHASE OF TECHNICAL PUBLICATIONS To guarantee safe operation and correct maintenance of the AQUILA AT01-100 aircraft, all manuals and technical publications must be kept in the current effective status. All manuals and technical publications relating to the aircraft AQUILA AT01-100 are available...

  • Page 8: General

    1.4.1 Overall Dimensions 1.4.2 Wings 1.4.3 Horizontal Stabilizer / Elevator 1.4.4 Fuselage and Vertical Stabilizer / Rudder 1.4.5 Landing Gear AQUILA AT01-100 – THREE VIEW DRAWING ENGINE PROPELLER FUEL OIL AND COOLANT 1.9.1 Engine Oil 1.9.2 Engine Coolant 1.10 WEIGHTS 1.11...
  • Page 9 AIRCRAFT TYPE CERTIFICATION The aircraft AQUILA AT01 is type-certified in accordance with the certification specifications of the Joint Aviation Requirements for Very Light Aeroplanes (JAR-VLA, including the revision VLA/92/1) by the Luftfahrt-Bundesamt, the National Aviation Authority of Germany.
  • Page 10 Section 1 POH / AFM GENERAL AQUILA AT01-100C WARNING, CAUTIONS AND NOTES Throughout the text, special text boxes marked WARNING, CAUTION and NOTE are used. These terms are defined as follows: WARNING Procedures, practices, etc. which may result in personal injury or loss of life if not strictly adhered to.
  • Page 11 Section 1 POH / AFM GENERAL AQUILA AT01-100C PRINCIPLE AIRCRAFT DIMENSIONS 1.4.1 Overall Dimensions Wing Span: 33.79 ft (10.3 m) Length: 24.28 ft (7.4 m) Height: 7.87 ft (2.4 m) 1.4.2 Wings Airfoil: HQ-XX mod. Area: 113.02 sq. ft (10.5 m²) Aspect Ratio: 10.1...
  • Page 12 Section 1 POH / AFM GENERAL AQUILA AT01-100C AQUILA AT01-100 – THREE VIEW DRAWING 2,4 m / 7,87 ft 7,4 m / 24,28 ft 10,3 m / 33,79 ft Document Nr.: Issue: Supersedes Issue: Date: Page: FM-AT01-1010-103 A.02 28.05.2013 15.10.2013...
  • Page 13 Section 1 POH / AFM GENERAL AQUILA AT01-100C ENGINE The ROTAX 912 S3 is a 4-cylinder 4-stroke engine with air cooled cylinders and liquid cooled ® cylinder heads. The Propeller is driven via an internal reduction gearbox with an integrated overload clutch and a hydraulic constant speed propeller governor.
  • Page 14 POH / AFM Section 1 GENERAL AQUILA AT01-100C ENGINE OIL AND COOLANT 1.9.1 Engine Oil Use only oil with an API classification of “SG” or higher. Heavy duty 4-stroke motor oils tend to meet these requirements. For more information regarding engine oil selection, please refer to the Operator’s Manual for all versions of the 912 engine series, section 10.2.3, and to the...
  • Page 15 Section 1 POH / AFM GENERAL AQUILA AT01-100C 1.9.2 Engine Coolant A conventional, ethylene glycol and water based coolant is used. Please refer to the Operator’s Manual for the 912 engine series, section 10.2.3, and to the current issue of the ROTAX Service Instructions SI-912-016 when choosing an engine ®...
  • Page 16 Section 1 POH / AFM GENERAL AQUILA AT01-100C 1.11 TERMINOLOGY AND ABBREVIATIONS 1.11.1 Speeds IAS: (Indicated Airspeed) - the speed shown on the airspeed indicator KIAS: IAS expressed in knots CAS: (Calibrated Airspeed) - the indicated airspeed, corrected for position and instrument error.
  • Page 17 Section 1 POH / AFM GENERAL AQUILA AT01-100C 1.11.2 Weight and Balance Reference Datum: imaginary vertical plane from which horizontal distances are measured for balance purposes Reference Line: fixed horizontal reference line Lever Arm: The horizontal distance from the reference datum to the center of gravity (C.G.) of an item...
  • Page 18 Section 1 POH / AFM GENERAL AQUILA AT01-100C 1.11.4 Engine and Performance TOP: (Take-off Power) - maximum power permissible for takeoff MCP: (Max. Continuous Power) - maximum power permitted for continuous operation 1.11.5 Various Serial No. (S/N): Serial Number of the Aircraft Part No.
  • Page 19 Section 1 POH / AFM GENERAL AQUILA AT01-100C 1.12 CONVERSION FACTORS 1.12.1 Length 1 ft 0.304 1 in 25.4 1.12.2 Speed 1 kt 1.852 km/h 1 mph 1.609 km/h 1.12.3 Pressure 1 hPa N/m² 1 mbar 1 in. Hg 33.865 1 psi 68.97...
  • Page 20 Section 2 POH / AFM LIMITATIONS AQUILA AT01-100C SECTION 2 LIMITATIONS Page INTRODUCTION AIRSPEED LIMITATIONS AIRSPEED INDICATOR MARKINGS POWER PLANT LIMITATIONS 2.4.1 Engine 2.4.2 Propeller MARKINGS ON THE GLASS PANEL ENGINE MONITOR MVP-50P-AQ WEIGHT LIMITS CENTER OF GRAVITY LIMITS MANEUVER LIMITS 2.10...

  • Page 21: Airspeed Limitations

    Section 2 POH / AFM LIMITATIONS AQUILA AT01-100C INTRODUCTION This section includes all operating limitations, instrument markings and basic placards necessary for the safe operation of the aircraft, its engine, standard systems and standard equipment. WARNING The aircraft must be operated in compliance with the operating limitations.

  • Page 22: Airspeed Indicator Markings

    Section 2 POH / AFM LIMITATIONS AQUILA AT01-100C AIRSPEED INDICATOR MARKINGS The airspeeds given below are expressed in Indicated Airspeeds (IAS): Marking (IAS) [kts] Remarks White arc 39-90 Full flap operating range Green arc 49-130 Normal operating range Operations in this region must be conducted with...
  • Page 23 Section 2 POH / AFM LIMITATIONS AQUILA AT01-100C Oil Pressure Minimum: 11.6 psi (0.8 bar) below 590 RPM 29 –72.5 psi (2.0-5.0 bar) above 590 RPM Normal: Maximum during a cold start: 101.5 psi (7.0 bar) (only for a short time)
  • Page 24 Section 2 POH / AFM LIMITATIONS AQUILA AT01-100C 2.5 MARKINGS ON THE ENGINE MONITOR MVP-50P-AQ The following table shows the instrument markings shown on the MVP-50P-AQ and their meaning. Green Arc Red Line Yellow Arc Red Line (normal MVP-50P-AQ (minimum)

  • Page 25: Weight Limits

    Section 2 POH / AFM LIMITATIONS AQUILA AT01-100C WEIGHT LIMITS Maximum Takeoff Weight 1653 lb (750 kg) Maximum Landing Weight 1653 lb (750 kg) Max. Weight in Baggage Compartment 88.2 lb ( 40 kg) WARNING Exceeding the weight limits can overload the aircraft and is prohibited. In addition, aircraft performance and handling characteristics may be detrimentally affected.
  • Page 26 Section 2 POH / AFM LIMITATIONS AQUILA AT01-100C FLIGHT LOAD FACTORS The following flight load factors may not be exceeded while performing any approved maneuvers. Flight Load Factor at V at V With Flaps Extended Positive -2.0 -2.0 Negative WARNING Exceeding the flight load factors limits may result in damage to the aircraft structure.
  • Page 27 Section 2 POH / AFM LIMITATIONS AQUILA AT01-100C 2.11 KINDS OF OPERATION LIMITS / MINIMUM EQUIPMENT Certified for: visual flights by Day Table 1 For VFR by Day*  Garmin G-500 Flight and navigational instruments  Magnetic Compass  Working timepiece with a seconds hand** ...

  • Page 28: Fuel Limitations

    For approved fuel grades, please refer to paragraph 1.8. 2.13 TEMPERATURE LIMITATIONS Parts of the aircraft structure that are exposed to direct vertical sunlight must be painted WHITE. 2.14 OPERATING ALTITUDE The Aquila AT01-100 has a maximum operating altitude of 14,500 ft. Document Nr.: Issue: Supersedes Issue: Date:...
  • Page 29 Section 2 POH / AFM LIMITATIONS AQUILA AT01-100C 2.15 PLACARDS 1) On the instrument panel, in the lower middle section of the panel: This aircraft is certified according to JAR-VLA for day VFR operations under non-icing conditions. All aerobatic maneuvers,...

  • Page 30: Table Of Contents

    POH / AFM SECTION 3 AQUILA AT01-100C EMERGENCY PROCEDURES SECTION 3 EMERGENCY PROCEDURES Page INTRODUCTION 3.1.1 Resetting circuit-breakers AIRSPEEDS FOR EMERGENCY OPERATION ENGINE FAILURES – CHECKLISTS 3.3.1 Engine Failure During the Take-off Run 3.3.2 Engine Failure Immediately After Take-off 3.3.3...
  • Page 31 POH / AFM SECTION 3 AQUILA AT01-100C EMERGENCY PROCEDURES 3.12 TRIM CONTROL SYSTEM FAILURES 3-14 3.12.1 Trim System Inoperative 3-14 3.12.2 Trim Actuator Runaway 3-15 3.13 AVIONICS MALFUNCTIONS 3-15 3.13.1 Complete Avionics Failure 3-15 3.13.2 Receive Mode Failure of COM-Equipment 3-15 3.13.3...

  • Page 32: Emergency Procedures

    POH / AFM SECTION 3 AQUILA AT01-100C EMERGENCY PROCEDURES INTRODUCTION This section provides checklists with the recommended procedures for coping with various emergency situations. Emergencies caused by aircraft or engine malfunctions are extremely rare if all pre-flight inspections and required maintenance is properly conducted.

  • Page 33: Engine Failures - Checklists

    POH / AFM SECTION 3 AQUILA AT01-100C EMERGENCY PROCEDURES ENGINE FAILURES – CHECKLISTS 3.3.1 Engine Failure before Take-off Throttle IDLE Brakes APPLY as required 3.3.2 Engine Failure Immediately After Take-off and during Climb Airspeed (IAS) 70 KIAS WARNING Depending on the own speed and altitude, the wind condition and the remaining engine power a forced landing must be initiated under consideration of the local conditions.

  • Page 34: In-Flight Engine Failure

    POH / AFM SECTION 3 AQUILA AT01-100C EMERGENCY PROCEDURES 3.3.3 In-flight Engine Failures ENGINE ROUGHNESS 1. Carburetor heat PULL (ON) 2. Fuel Pump switch 3. Ignition switch SWITCH through the positions L-BOTH, then R-BOTH 4. Throttle Maintain setting If roughness continues: 5.
  • Page 35 POH / AFM SECTION 3 AQUILA AT01-100C EMERGENCY PROCEDURES ENGINE RESTART PROCEDURE WITH STOPPED PROPELLER Non-essential electrical equipment ALT1 / BAT switch Propeller control lever START position Fuel selector valve SWITCH to fullest tank Fuel Pump switch Throttle warm engine...

  • Page 36: Forced Landings

    POH / AFM SECTION 3 AQUILA AT01-100C EMERGENCY PROCEDURES When power is restored: Oil pressure CHECK Choke PUSHED (OFF) Electrical equipment SWITCH ON (as required) Oil temperature CHECK FORCED LANDINGS Generally the flight path should always be chosen such that, in the event of an emergency, a suitable landing field can be reached.

  • Page 37: Emergency Landing

    POH / AFM SECTION 3 AQUILA AT01-100C EMERGENCY PROCEDURES Touch down with lowest possible airspeed. After touchdown: Brakes APPLY as required Fuel selector valve Ignition switch ALT1 / BAT switch 3.4.2 Emergency Landing NOTE An emergency landing occurs in a state of distress, such as an engine failure, fuel starvation or mechanical problems with the aircraft.

  • Page 38: Engine Fire In Flight

    POH / AFM SECTION 3 AQUILA AT01-100C EMERGENCY PROCEDURES 3.5.2 Engine Fire In-flight Throttle WIDE OPEN Fuel selector valve Cabin heat PUSHED (OFF) Canopy slide-window OPEN Perform a precautionary landing without engine power as described in Section 3.5.3 Electrical Fire with Smoke on the Ground...

  • Page 39: Inadvertent Flight Into Icing Conditions

    POH / AFM SECTION 3 AQUILA AT01-100C EMERGENCY PROCEDURES INADVERTENT FLIGHT IN ICING CONDITIONS WARNING Intentional flight in icing conditions is prohibited. During unintentional flight in icing conditions proceed as follows: Carburetor heat PULL (ON) Leave icing conditions immediately by flying a reciprocal heading and/or changing...

  • Page 40: Power-Off Glide

    POH / AFM SECTION 3 AQUILA AT01-100C EMERGENCY PROCEDURES POWER-OFF GLIDE Achievable gliding distances vary depending on altitude and current wind conditions. This is very important when choosing a landing site or reaching a near-by airfield. To achieve maximum gliding distance:...

  • Page 41: Electrical System Malfunctions

    POH / AFM SECTION 3 AQUILA AT01-100C EMERGENCY PROCEDURES 3.10 ELECTRICAL SYSTEM MALFUNCTIONS 3.10.1 Complete Electrical System Failure 1. ALT1 / BAT switch CHECK if ON 2. BAT1 circuit breaker (see 3.1.1) RESET if tripped 3. ALT1 circuit breaker (see 3.1.1)

  • Page 42: Low Voltage Indication

    POH / AFM SECTION 3 AQUILA AT01-100C EMERGENCY PROCEDURES 3.10.3 Low Voltage Indication A) On the ground (voltmeter values YELLOW or RED) Engine speed Increase RPM until value turns GREEN (RPM should be below 1350) All non-essential equipment OFF, until value turns GREEN.

  • Page 43: Flap Control System Malfunctions

    POH / AFM SECTION 3 AQUILA AT01-100C EMERGENCY PROCEDURES 3.11 FLAP CONTROL SYSTEM MALFUNCTIONS FLAP POSITION INDICATOR or FLAP ACTUATOR MALFUNCTION Flap Actuator circuit breaker (see 3.1.1) RESET, if tripped Flap Control circuit breaker (see 3.1.1) RESET, if tripped Flap position...

  • Page 44: Trim Actuator Runaway

    POH / AFM SECTION 3 AQUILA AT01-100C EMERGENCY PROCEDURES 3.12.2 Trim Actuator Runaway Control Column HOLD in position Trim Actuator circuit breaker PULL Trim switch CHECK if pressed or jammed If the problem is obvious, and can be solved: Trim Actuator circuit breaker (see 3.1.1) RESET NOTE Approx.

  • Page 45: Primary Flight Display Failure

    POH / AFM SECTION 3 AQUILA AT01-100C EMERGENCY PROCEDURES 3.13.4 Primary Flight Display Failure 1. PFD circuit breaker (see 3.1.1) RESET, if tripped 2. AHRS circuit breaker (see 3.1.1) RESET, if tripped 3. ADC circuit breaker (see 3.1.1) RESET, if tripped It is possible to safely continue flight, even if the PFD failure cannot be corrected in flight, by referencing the remaining instruments.

  • Page 46: Ahrs Failure

    POH / AFM SECTION 3 AQUILA AT01-100C EMERGENCY PROCEDURES 3.13.7 AHRS Failure 1. AHRS circuit breaker (see 3.1.1) RESET, if tripped NOTE In the event of an AHRS Failure, the horizon is no longer displayed on the PFD. Additionally a red “X”...

  • Page 47: Starter Malfunction

    POH / AFM SECTION 3 AQUILA AT01-100C EMERGENCY PROCEDURES 3.14 STARTER MALFUNCTION If, during engine start, the starter does not decouple from the engine (a continuous and excessive howling tone is audible). Throttle IDLE Ignition switch Repair damage before conducting planned flight.
  • Page 48 Section 4 POH / AFM NORMAL PROCEDURES AQUILA AT01-100C SECTION 4 NORMAL PROCEDURES Page INTRODUCTION AIRSPEEDS FOR NORMAL OPERATION DAILY INSPECTION PRE-FLIGHT INSPECTION CHECKLISTS FOR NORMAL PROCEDURES 4-11 4.5.1 Before Engine Start-up 4-11 4.5.2 Engine Start-up 4-12 4.5.3 Before Taxiing 4-13 4.5.4...

  • Page 49: Normal Procedures

    Section 4 POH / AFM NORMAL PROCEDURES AQUILA AT01-100C INTRODUCTION This section provides normal operating procedures and checklists for the aircraft as well as recommended airspeeds. Additional information is provided in the current issues of the Operators Manual for ROTAX...

  • Page 50: Airspeeds For Normal Operation

    Section 4 POH / AFM NORMAL PROCEDURES AQUILA AT01-100C AIRSPEEDS FOR NORMAL OPERATION The following airspeeds are based on the maximum take-off weight of 1653 lbs (750 kg). They may also be used for any lower operational weight. TAKE-OFF Airspeed (IAS)

  • Page 51: Daily Inspection

    Section 4 POH / AFM NORMAL PROCEDURES AQUILA AT01-100C DAILY INSPECTION CAUTION The daily inspection is begun by checking all 3 fuel sumps for water and contamination. This must be done before the aircraft is moved. Otherwise the fuel in the sump may mix.
  • Page 52 Section 4 POH / AFM NORMAL PROCEDURES AQUILA AT01-100C B) EXTERIOR CHECK, Visual Inspection CAUTION In this manual, visual inspection means the following: Inspect for mechanical damage, dirt, cracks, delamination, excessive play, looseness, leaks, incorrect attachment, foreign objects and general condition.
  • Page 53 Section 4 POH / AFM NORMAL PROCEDURES AQUILA AT01-100C Left main landing gear a) Landing gear strut Visual inspection b) Wheel fairing Visual inspection (refer to 7.11.4) c) Tire pressure and slip marking CHECK d) Tire, wheel, brake Visual inspection...
  • Page 54 Section 4 POH / AFM NORMAL PROCEDURES AQUILA AT01-100C Nose section, cowling WARNING Before cranking the propeller: Ignition and ALT1/BAT switch: OFF Set the parking brake. WARNING RISK OF BURNS ! Only check the oil and coolant levels when the engine is cool.
  • Page 55 Section 4 POH / AFM NORMAL PROCEDURES AQUILA AT01-100C Nose landing gear a) Nose gear strut Visual inspection b) Wheel fairing Visual inspection CAUTION Both parts of the 2 piece nose wheel fairing must always be installed on the aircraft...

  • Page 56: Pre-Flight Inspection

    Section 4 POH / AFM NORMAL PROCEDURES AQUILA AT01-100C PRE-FLIGHT INSPECTION (Walk Around) Daily Inspection Confirm has been carried out. Tow bar Remove Fuel level CHECK with dipstick and verify with the indicated fuel level on the fuel gauge WARNING...
  • Page 57 Section 4 POH / AFM NORMAL PROCEDURES AQUILA AT01-100C 6. Tie-down straps remove 7. Baggage door CHECK if closed and locked 8. Pitot cover remove 9. Control locks remove 10. Seating position adjust and lock, check that nose wheel steering and brakes can be operated 11.

  • Page 58: Checklists For Normal Procedures

    Section 4 POH / AFM NORMAL PROCEDURES AQUILA AT01-100C CHECKLISTS FOR NORMAL PROCEDURES 4.5.1 Before Engine Start-up Daily and Pre-Flight Inspection COMPLETED Passenger Briefing COMPLETED Seats ADJUSTED Seat Belts and Harnesses FASTENED Canopy CLOSED and LOCKED Check locking mechanism Parking Brake...

  • Page 59: Engine Start-Up

    Section 4 POH / AFM NORMAL PROCEDURES AQUILA AT01-100C 4.5.2 Engine Start-up Fuel Pump switch Fuel Pressure within GREEN range Throttle - Cold Engine IDLE - Hot Engine 0.8 in. (2 cm) OPENED Choke - Cold Engine PULL, and keep pulled...

  • Page 60: Before Taxiing

    Section 4 POH / AFM NORMAL PROCEDURES AQUILA AT01-100C 4.5.3 Before Taxiing CAUTION Warm up the engine for approx. 2 min at 800 RPM and then at 1000 RPM until the Oil Temperature reaches a temperature of at least 122°F (50°C)

  • Page 61: Before Take-Off (At The Taxi Holding Position)

    Section 4 POH / AFM NORMAL PROCEDURES AQUILA AT01-100C 4.5.5 Before Take-off (at the Taxi Holding Position) Brakes APPLY Parking Brake Compass and gyro Instruments CHECK setting Fuel Selector Valve LEFT or RIGHT, switch to the fuller tank Fuel Pressure...

  • Page 62: Take-Off

    Section 4 POH / AFM NORMAL PROCEDURES AQUILA AT01-100C 4.5.6 Take-off (up to 50 ft) Throttle WIDE OPEN Tachometer CHECK if within 2300 - 2385 RPM Elevator, control column NEUTRAL during initial ground roll Rudder pedals Maintain direction Rotate speed...

  • Page 63: Cruise

    Section 4 POH / AFM NORMAL PROCEDURES AQUILA AT01-100C 4.5.8 Cruise Throttle AS REQUIRED (Ref. to Section 5, Page 5-11) Propeller control lever SET 1650 to 2260 RPM NOTE For best manifold pressure/propeller speed combinations: Refer to Section 5, page 5-11...

  • Page 64: Landing

    Section 4 POH / AFM NORMAL PROCEDURES AQUILA AT01-100C 4.5.10 Landing Lap belt CHECK SECURE Fuel Pump switch Carburetor heat PULL (ON) Throttle AS REQUIRED Airspeed 90 KIAS Flaps switch T/O or LDG Trim switch AS REQUIRED Flaps switch Approach speed...

  • Page 65: Engine Shutdown

    Section 4 POH / AFM NORMAL PROCEDURES AQUILA AT01-100C 4.5.13 Engine Shutdown Throttle IDLE Parking Brake Flaps switch CHECK (frequency 121.5 MHz) Avionics switch Ignition Switch Electrical equipment ALT1 / BAT switch NOTE The GARMIN G500 and the MVP-50P-AQ are turned off with the ALT1/BAT switch.
  • Page 66 Section 4 POH / AFM NORMAL PROCEDURES AQUILA AT01-100C 4.5.15 Flight in Heavy Rain and/or with Wing Contamination CAUTION When flying with wet and/or contaminated wings and control surfaces, performance and handling qualities may be reduced. This applies in particular to take-off distance, climb performance, cruising speed and stall characteristics.
  • Page 67 Section 4 POH / AFM NORMAL PROCEDURES AQUILA AT01-100C [intentionally left blank] Document Nr.: Issue: Supersedes Issue: Date: Page: FM-AT01-1010-103 A.02 28.05.2013 15.10.2013 4 - 20...

  • Page 68: Performance (Partly Approved Section)

    Section 5 POH / AFM PERFORMANCE AQUILA AT01-100C SECTION 5 PERFORMANCE Page INTRODUCTION PERFORMANCE CHARTS 5.2.1 Airspeed Calibration 5.2.2 Stall Speeds 5.2.3 Crosswind Component 5.2.4 Flight Planning 5.2.5 Take-off Distance 5.2.6 Climb Performance / Cruise Altitude 5.2.7 Climb: Fuel Consumption, Time and Distance Cruise Performance (TAS –...
  • Page 69 INTRODUCTION The performance data in the following charts give an overview on the performance and capabilities of the AQUILA AT01. This information provides the basis for flight planning prior to every flight. All data in the charts haves been acquired during flight testing conducted with an aircraft and engine in a good operating condition.
  • Page 70 Section 5 POH / AFM PERFORMANCE AQUILA AT01-100C PERFORMANCE CHARTS 5.2.1 Airspeed Calibration Airspeed calibration accounts for the position error of the pitot-static pressure system, but not for the instrument error. Assumption: zero instrument error Example: 120 KIAS (indicated airspeed) corresponds to 118 KCAS (calibrated airspeed) Fig.: 5.2.1 Airspeed Calibration...
  • Page 71 Section 5 POH / AFM PERFORMANCE AQUILA AT01-100C 5.2.2 Stall Speeds Stall speeds were determined in the following configuration: Forward center of gravity (CG) limit: 16.8 in (427 mm) behind the Ref. Datum Takeoff weight 1653 lb. (750 kg) Engine idle...
  • Page 72 Section 5 POH / AFM PERFORMANCE AQUILA AT01-100C 5.2.3 Demonstrated Crosswind Component, Crosswind Diagram Maximum demonstrated crosswind component: 15 knots (27 km/h) WARNING Stronger crosswind components may render the aircraft uncontrollable! 0° 10° 20° 30° 40° 50° 60° 70° 80°...
  • Page 73 Section 5 POH / AFM PERFORMANCE AQUILA AT01-100C 5.2.4 Flight Planning The performance tables and diagrams on the following pages contain all information required for flight planning from take-off at your point of departure to the landing at your destination.
  • Page 74 POH / AFM Section 5 AQUILA AT01-100C PEFORMANCE 5.2.5 Take-off Distance 1000 3280 Notes: Airspeed [KIAS] Take-off Weight [lbs]([kg]) Lift-Off 50 ft - For operations on dry, grass runway, increase ground roll 1653 (750) distance by 25%, on soft grass runway up to 40%.
  • Page 75 POH / AFM Section 5 AQUILA AT01-100C Performance 5.2.6 Rate of Climb / Cruise Altitude Take-off Weight Service Ceiling (ISA) Best Rate-of-Climb Speed [KIAS] [lbs]([kg]) MSL-5000 ft 10 000 ft 13 000 ft 1500 1653 (750) 14 500 ft 1323 (600)
  • Page 76 POH / AFM Section 5 PERFORMANCE AQUILA AT01-100C 5.2.7 Climb: Fuel, time and Distance Conditions: Vy= 65 KIAS, to 5000 ft 2260 rpm, MCP, Vy= 63 KIAS, to 10.000 ft Flaps : UP For each 8°C above ISA, increase Vy= 61 KIAS, to 13.000 ft m = 750 kg (1653 lb) time, distance and fuel by 10%.
  • Page 77 POH / AFM Section 5 AQUILA AT01-100C FLUGLEISTUNGEN 5.2.8 Cruising Speed (TAS - True airspeed) Conditions: Notice: Flying without any wheel fairings or with mud guards reduces performance up to Performance: Settings after schedule on page 5-11 10%. Flight weight: 750 kg (1653 lb)
  • Page 78 Section 5 POH / AFM PERFORMANCE AQUILA AT01-100C 5.2.9 Cruise Power Settings Engine performance in % of MCP Pressure Standard altitude Head temperature [°C] [°F] [ft] [U/min] [in Hg] [l/h] [gal/h] [U/min] [in Hg] [l/h] [gal/h] [U/min] [in Hg] [l/h]...
  • Page 79 POH / AFM Section 5 PERFORMANCE AQUILA AT01-100C 5.2.10 Maximum Endurance Condition: NOTE: Fuel quantity: usable fuel 28.9 US gal (109.6 l) Power setting: according to the table on page 5-10 A not properly maintained engine The calculation of the endurance includes:...
  • Page 80 POH / AFM Section 5 PERFORMANCE AQUILA AT01-100C 5.2.11 Maximum Range Condition: NOTE: Fuel quantity: usable fuel 28.9 US gal (109.6 l) Power setting: according to the table on page 5-10 A not properly maintained engine The calculation of the range includes:...
  • Page 81 POH / AFM Section 5 AQUILA AT01-100C PERFORMANCE 5.2.12 Descent: Fuel, Time and Distance Process: Conditions: In descent follow a speed of 121 KIAS. Manifold Pressure: as required. Approx. 15 in Hg Set performance for a descent rate of 750 ft / min.
  • Page 82 Section 5 POH / AFM PERFORMANCE AQUILA AT01-100C 5.2.13 Landing Distance Airspeed [KIAS] NOTES: Ldg Weight - When landing on a dry, grass runway, increase the required landing distances by 15%. [lbs]([kg]) in 50 ft Touchdown - Increase ground roll appropriately for wet grass/ground, ice, snow and slush.
  • Page 83 POH / AFM Section 5 PERFORMANCE AQUILA AT01-100C 5.2.14 Climb Performance after Balked Landing Conditions: 1000 Performance: full throttle Rotation spees: 2385 rpm Flaps: LDG Speed: 55 KIAS Pressure Head (-22) (-4) (14) (32) (50) (68) (86) (1650) (1550) (1500)
  • Page 84 Section 5 POH / AFM PERFORMANCE AQUILA AT01-100C 5.2.15 Flight Planning Example The following contains a flight-planning example to demonstrate the use of the tables, charts and data presented in this section of the POH. The flight planning is based upon...
  • Page 85 Section 5 POH / AFM PERFORMANCE AQUILA AT01-100C We now have all the necessary data to determine the required take-off distances from chart 5.2.5: Take-off ground roll.........202 m Lift-off speed...........50 KIAS Take-off distance over a 50 ft obstacle...375 m Airspeed in 50 ft..........57 KIAS The required take-off distance is less than the available runway length (TODA) of 620m.
  • Page 86 Section 5 POH / AFM PERFORMANCE AQUILA AT01-100C CRUISE Cruise altitude is chosen under consideration of flight distance, en-route winds and aircraft performance. In this flight-planning example, a typical cruise altitude and en- route wind condition has been chosen. The range diagram 5.2.11 on page 5-13 shows the relationship between the engine power setting and the maximum achievable range.
  • Page 87 Section 5 POH / AFM PERFORMANCE AQUILA AT01-100C CALCULATION OF FUEL REQUIRED Fuel required for engine start-up and taxiing 0.53 US gal (2.0 ltr) (General Value, see remark “Fuel Quantity” on pg. 5-12 and 5-13) Fuel required for climb (page 5-18) +0.92 US gal (3.5 ltr)
  • Page 88 Section 5 POH / AFM PERFORMANCE AQUILA AT01-100C The total amount of fuel required is calculated as follows: Engine start-up, taxiing and climb 1.45 US gal (5.5 ltr) Cruise 20.26 US gal (76.7 ltr) Descent 0.23 US gal (0.9 ltr) Total fuel required 21.94 US gal (83.1 ltr)
  • Page 89 Section 5 POH / AFM PERFORMANCE AQUILA AT01-100C Sample Calculation: Cruise altitude: 2000 ft ISA temperature: 52°F (11°C) Temperature in cruise altitude: 70°F (21°C) (ISA + 10°C) Power setting: RPM: 2000 RPM Manifold pressure for ISA (see chart): 24.7 in Hg Manifold pressure calculated for ISA + 10°C:...

  • Page 90: Weight And Balance

    Section 6 POH / AFM WEIGHT AND BALANCE AQUILA AT01-100C SECTION 6 WEIGHT AND BALANCE / EQUIPMENT LIST Page INTRODUCTION AIRCRAFT WEIGHING WEIGHT AND BALANCE DATA 6.3.1 Weight and Balance Record DETERMINING WEIGHT AND BALANCE FOR FLIGHT 6.4.1 Load moment determination (loading graph) 6.4.2...
  • Page 91 Section 6 POH / AFM WEIGHT AND BALANCE AQUILA AT01-100C INTRODUCTION Before delivery, the manufacturer determines the basic empty weight and moment as well as the empty C.G. location for each aircraft. This data is documented in the Weight and Balance Record in section 6.3.1 of this section.
  • Page 92 Section 6 POH / AFM WEIGHT AND BALANCE AQUILA AT01-100C AIRCRAFT WEIGHING Reference Datum (BE): Leading edge of wing root rib Horizontal reference line: Place a wedge (800 : 77) 63 in (1600 mm) ahead of the leading edge of the horizontal stabilizer. Place a level on the wedge and level the aircraft.
  • Page 93 Section 6 POH / AFM WEIGHT AND BALANCE AQUILA AT01-100C Aircraft Weighing: Example in [lb, in] Position Weight [lb] Lever [in] Moment [in*lb] Nose Wheel = 234 = - 33 = - 7722 Left Main Wheel = 441 = + 31...
  • Page 94 Section 6 POH / AFM WEIGHT AND BALANCE AQUILA AT01-100C Replace with current Aircraft Weighing Report Document Nr.: Issue: Supersedes Issue: Date: Page: FM-AT01-1010-103 A.02 28.05.2013 15.10.2013 6 - 5...
  • Page 95 Section 6 POH / AFM WEIGHT AND BALANCE AQUILA AT01-100C 6.3.1 Weight and Balance Record Document Nr.: Issue: Supersedes Issue: Date: Page: FM-AT01-1010-103 A.02 28.05.2013 15.10.2013 6 - 6...
  • Page 96 Section 6 POH / AFM WEIGHT AND BALANCE AQUILA AT01-100C DETERMINING WEIGHT AND BALANCE FOR FLIGHT In order to operate the aircraft within the approved weight and C.G. limits, the take-off weight and the flight C.G. position must be determined, taking into consideration the loading for the planned flight.
  • Page 97 Section 6 POH / AFM WEIGHT AND BALANCE AQUILA AT01-100C 6.4.1 Load moment determination (loading graph) Loading Graph Seat most Seat most forward rearward Kraftstoff fuel baggage Gepäck 940 1010 Moment of loading [kg m] ([lb ft]) NOTE When determining the C.G. position, the fact that the seat is adjustable must be taken in to consideration.
  • Page 98 Section 6 POH / AFM WEIGHT AND BALANCE AQUILA AT01-100C 6.4.2 Weight and Moment Determination Registration No.: Aquila AT01 Lever from leading Example Calculating edge of wing root Loading Weight Moment Weight Moment rib (BE) Condition [lb] [in lb] [lb]...

  • Page 99: Poh / Afm Aquila At01-100C

    Section 6 POH / AFM WEIGHT AND BALANCE AQUILA AT01-100C 6.4.3 Approved Center of Gravity Range and Moment Limits xS =16.8 in 17.1 17.9 18.7 19.5 20.3 xS = 20.6 in xS = 427mm xS = 523 mm 1675 1650...
  • Page 100 Section 6 POH / AFM WEIGHT AND BALANCE AQUILA AT01-100C 6.4.4 Estimating Center of Gravity Position using MVP-50P-AQ The "Weight and Balance" function of the MVP-50P-AQ offers a comfortable and simple way of estimating the current C.G. position. The weights of the pilot, passenger, baggage and fuel are entered into the "Weight and Balance"...

  • Page 101: Equipment List

    Service Bulletin. When in doubt, the type certificate holder or the production organization of AQUILA Aviation should be contacted. After every change to the aircraft that could cause the empty weight or moment to change (for example, the installation or removal of equipment), the empty weight and C.G.
  • Page 102 Section 6 POH / AFM WEIGHT AND BALANCE AQUILA AT01-100C 6.5.1 Current Equipment List of the Aircraft AQUILA AT01-100 Registration: S/N: AT01-100C- Installation Designation / Description Manufacturer Model / P/N Location **) Mark where applicable Describe installation location or enter lever arm from reference datum in [in] (keep algebraic sign of lever arm in mind) Document Nr.:...
  • Page 103 Section 6 POH / AFM WEIGHT AND BALANCE AQUILA AT01-100C AQUILA AT01-100 Registration: S/N: AT01-100C- Installation Designation / Description Manufacturer Model / P/N Location **) Mark where applicable Describe installation location or enter lever arm from reference datum in [in] (keep algebraic sign of lever arm in mind) Document Nr.:...
  • Page 104 Section 7 POH / AFM AIRCRAFT DESCRIPTION AQUILA AT01-100C SECTION 7 DESCRIPTION OF THE AIRCRAFT AND ITS SYSTEMS Page INTRODUCTION 7.1.1 Garmin G-500 (Primary Flight Display) 7.1.2 Glass Panel Engine Monitor MVP-50P-AQ AIRFRAME FUSELAGE WING EMPENNAGE FLIGHT CONTROLS 7.6.1 Ailerons 7.6.2...
  • Page 105 Section 7 POH / AFM AIRCRAFT DESCRIPTION AQUILA AT01-100C 7.12 POWER PLANT 7-13 7.12.1 Engine 7-13 7.12.2 Propeller 7-13 7.12.3 Throttle and Propeller Control 7-14 7.12.4 Choke 7-15 7.12.5 Carburetor Heat 7-15 7.13 FUEL SYSTEM 7-16 7.13.1 Overview 7-16 7.13.2...

  • Page 106: Introduction

    Section 7 POH / AFM AIRCRAFT DESCRIPTION AQUILA AT01-100C INTRODUCTION Section 7 of the Pilot's Operating Handbook contains a description of the entire aircraft and its systems, including the integration of the GARMIN G500 system and the Glass Panel Engine Monitor MVP-50P-AQ as well as information related to their use.

  • Page 107: Glass Panel Engine Monitor Mvp-50P-Aq

    Section 7 POH / AFM AIRCRAFT DESCRIPTION AQUILA AT01-100C 7.1.2 Glass Panel Engine Monitor MVP-50P-AQ The MVP-50P-AQ consists of an indication / actuation interface (MVP-50), an engine data converter (ECD-33) and the attached probes. When engine limits are exceeded, the warning light ENG in the annunciator panel of the MVP- 50P-AQ will illuminate YELLOW (caution) or RED (operating limit).

  • Page 108: Airframe

    The Aquila AT01-100 is a modern single engine two seater in a side-by-side configuration. Due to its high useful load, roomy cockpit, large baggage compartment, good cruise performance and light yet incredibly sturdy airframe, the Aquila is not only a great aircraft for longer tours but also an ideal training platform.

  • Page 109: Empennage

    The horizontal stabilizer assembly is bonded directly to the fuselage and cannot be removed. FLIGHT CONTROLS The flight controls of the Aquila AT01-100 are of conventional design using a control column and non-adjustable rudder pedals. The elevator and ailerons are controlled via push-pull-rods, the rudder via cables.

  • Page 110: Rudder

    Section 7 POH / AFM AIRCRAFT DESCRIPTION AQUILA AT01-100C 7.6.3 Rudder The rudder is controlled by the rudder pedals by way of cables running in special guides. The control surface travel is limited by stops at the lower rudder attachment fitting.
  • Page 111 Pilot’s Operating Handbook Abschnitt 7 AQUILA AT01-100C AIRCRAFT DESCRIPTION NOTE: INSTRUMENT PANEL AT01-100C (sample) actual installation differ depending certified changes complementary equipment. 12 13 For minimum instrument requirements, refer to Section 2.12 of this manual Description Description Description Description Description...

  • Page 112: Overview Control Panel

    Pilot’s Operating Handbook Section 7 AIRCRAFT DESCRIPTION AQUILA AT01-100C 7.7.1 Overview Control Panel Controls and displays located on the control panel which is located below the midsection of the instrument panel, are placed so as to be easily viewed and operated from both seats.

  • Page 113: Seats, Seatbelts And Harnesses

    7.10 CANOPY The large canopy of the AQUILA AT01-100 offers an excellent all around view and allows unrestricted access to the cabin. Small sliding windows on both sides of the canopy serve as emergency view windows and can be used for additional cabin ventilation.

  • Page 114: Landing Gear

    Because of the robust landing gear and the 5.00 x 5 wheels on the nose and main wheels the AQUILA AT01-100 can be easily operated from a grass surface. The aircraft can be operated with full size wheel pants or, for soft field operation, mud guards.

  • Page 115: Wheel Fairings

    It is important that no dirt or snow accumulate underneath the wheel pants. For this reason the Aquila AT01-100 can be operated with either full wheel pants (high-speed), with mud guards (soft-field), or without any wheel fairings. The aircraft can also be flown with a combination of wheel fairings, as long as the left and right main wheels have the same fairing.

  • Page 116: Power Plant

    Pilot’s Operating Handbook Section 7 AIRCRAFT DESCRIPTION AQUILA AT01-100C 7.12 POWER PLANT 7.12.1 Engine The ROTAX 912S is a 4 cylinder, 4 stroke horizontally opposed engine with liquid- cooled cylinder heads and air-cooled cylinder barrels. It has brushless magnetos, 2 carburetors, a mechanical fuel pump, a reduction drive, an integrated alternator (ALT2), an alternator (ALT1) and an attachment for a hydraulic constant speed propeller.

  • Page 117: Throttle And Propeller Control

    Pilot’s Operating Handbook Section 7 AIRCRAFT DESCRIPTION AQUILA AT01-100C 7.12.3 Throttle and Propeller Control The black throttle lever and the blue propeller control lever are located on the central control panel. The throttle controls the manifold pressure (MP): Throttle forward:...

  • Page 118: Choke

    Pilot’s Operating Handbook Section 7 AIRCRAFT DESCRIPTION AQUILA AT01-100C 7.12.4 Choke The choke control knob is located on the control panel to the right of the carburetor heat and cabin heat controls. The choke may only be used for a short time when starting the engine in cold conditions.

  • Page 119: Fuel System

    Pilot’s Operating Handbook Section 7 AIRCRAFT DESCRIPTION AQUILA AT01-100C 7.13 FUEL SYSTEM 7.13.1 Overview right wing tank right wing tank left wing tank left wing tank Fuel supply line Fuel supply line Fuel return line Fuel return line Fuel Vent...

  • Page 120: Fuel Tank

    Pilot’s Operating Handbook Section 7 AIRCRAFT DESCRIPTION AQUILA AT01-100C 7.13.2 Fuel Tank Each wing is equipped with an integral fuel tank. The fuel line of each tank is equipped with a removable coarse fuel filter. The fuel filler caps can be locked.

  • Page 121: Fuel Level Indication

    Pilot’s Operating Handbook Section 7 AIRCRAFT DESCRIPTION AQUILA AT01-100C 7.13.4 Fuel Level Indication A floating sensor which is easy to maintain supplied information concerning fuel levels which are then displayed on the MVP-50P-AQ. The floating gauge is located above the fuel supply;...

  • Page 122: Electrical System

    Pilot’s Operating Handbook Section 7 AIRCRAFT DESCRIPTION AQUILA AT01-100C 7.14 ELECTRICAL SYSTEM The AT01-100 is equipped with a 12 V direct current (DC) electrical system that is powered by an engine-driven alternator and a battery. When the ALT1 / BAT switch is engaged, the electrical equipment can be operated and controlled by rocker switches located on the lower left section of the instrument panel.
  • Page 123 Pilot’s Operating Handbook Section 7 AIRCRAFT DESCRIPTION AQUILA AT01-100C ALT1 - Excitation ALT1 Chronometer (opt.) Excitation ALT1 ALT1 ALT1 Pitot Heat Warning Lights opt. Battery Relay ALT2 ALT2 ALT2 NVFR (optional) Regulator Shunt Starter Position of Ignition Switch Starter Relay External Power (opt.)

  • Page 124: Electrical Equipment And Circuit Breakers

    Pilot’s Operating Handbook Section 7 AIRCRAFT DESCRIPTION AQUILA AT01-100C 7.14.3 Electrical Equipment and Circuit Breakers All electrical equipment can be turned on or off by push-pull type circuit breakers or by rocker switches with built-in circuit breaker function. COM/NAV-equipment along with other avionic equipment is supplied with electrical power through the Avionics switch.

  • Page 125: Voltmeter And Amperemeter

    Pilot’s Operating Handbook Section 7 AIRCRAFT DESCRIPTION AQUILA AT01-100C If a yellow or red range is reached, the affected data or value will blink in the appropriate color. In addition, the yellow or red ENG warning light in the annunciator panel will illuminate.

  • Page 126: External Power Unit

    Pilot’s Operating Handbook Section 7 AIRCRAFT DESCRIPTION AQUILA AT01-100C 7.17 EXTERNAL POWER UNIT (optional) It is recommended to use an External Power Unit (EPU) for engine start-up at outside air temperatures below –10° C. The EPU receptacle is optional and is mounted on the right fuselage side below the battery.

  • Page 127: Pitot Heat

    Pilot’s Operating Handbook Section 7 AIRCRAFT DESCRIPTION AQUILA AT01-100C 7.18.1 Pitot Heat (optional) On request, a heated pitot-static tube can be installed. The heater is turned on using the P/S Heat switch. The size and location of the heated pitot static tube are identical to the unheated version.
  • Page 128 POH / AFM Section 8 AQUILA AT01-100C HANDLING & MAINTENANCE SECTION 8 HANDLING, SERVICE & MAINTENANCE Page INTRODUCTION AIRCRAFT INSPECTION PERIODS MODIFICATIONS AND REPAIRS GROUND HANDLING 8.4.1 Towing 8.4.2 Parking 8.4.3 Tie-Down 8.4.4 Jacking CLEANING AND CARE 8.5.1 Painted Surfaces 8.5.2...
  • Page 129 AIRCRAFT INSPECTION PERIODS The required inspection items are listed and described in the AQUILA AT01 Maintenance Manual (Document number MM-AT01-1020-110), the Operation Manual of the ROTAX type ®...

  • Page 130: Ground Handling

    POH / AFM Section 8 AQUILA AT01-100C HANDLING & MAINTENANCE GROUND HANDLING 8.4.1 Towing 8.4.1.1 Moving forwards The aircraft can be safely moved and controlled by one person on a smooth and level surface with the tow bar attached to the nose wheel.
  • Page 131 POH / AFM Section 8 AQUILA AT01-100C HANDLING & MAINTENANCE 8.4.3 Tie-Down The aircraft has three tie-down points; two are located on the lower surface of the wings in the outboard section (fitted with M 8 threads) and the third is located on the lower fin. The tie-down points are marked by red circles.

  • Page 132: Cleaning And Care

    Care should be taken when washing the wings near the stall warning. 8.5.1 Painted Surfaces To maintain the excellent flight performance and handling qualities of the AQUILA AT01 the aircraft must be kept clean and free of damage. Therefore it is recommended to regularly clean the aircraft, paying close attention to the leading edges of the wings and stabilizers.
  • Page 133 POH / AFM Section 8 AQUILA AT01-100C HANDLING & MAINTENANCE 8.5.2 Canopy Since acrylic glass can be easily scratched, the same principles apply as for cleaning painted surfaces. The canopy should be cleaned using plenty of water, a soft clean sponge and chamois leather.
  • Page 134 If modifications requiring an STC have been conducted on your aircraft at a Maintenance Organization other than AQUILA Aviation, it is the owner’s responsibility to ensure that the appropriate supplements are included in this manual and properly recorded in the index of supplements in section 9.2.
  • Page 135 Garmin GNS 430W AS-20* NOTE For the devices listed above and marked with an *, it is possible to perform a software update. These will be released on our website (www.aquila-aviation.de) by an appropriate SI (Service Information). Document Nr.: Issue:...

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