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POH

AQUILA AT01-200C

Section 4

NORMAL PROCEDURES

Document Nr.:

Issue:

Supersedes Issue:

Date:

Page:

FM-AT01-1010-106

A.02

A.01 (02.03.2020)

03.03.2021

4 - 7

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

c) Tire pressure and slip marking

CHECK

d) Tire, wheel

Visual inspection

e) Shock absorber

uni

Visual inspection

f) Chocks and tow bar

REMOVE

Nose section, cowling

WARNING

Before cranking the propeller:

Ignition, ALT1/BAT switch and ALT2/BAT2 switch: OFF

Set the parking brake.

WARNING

RISK OF BURNS !

Only check the oil and coolant levels when the engine is cool.

a) Check oil level

Turn the propeller several times in the

direction of

engine rotation

to pump oil from the engine back into

the oil tank.

CAUTION

NEVER turn the propeller against the direction of engine rotation.

Stop turning the propeller when air begins to return to the oil tank. This is indicated by the
sound of air rushing from the open oil tank.

Use the oil dip stick to check that the oil level is between the -min./max.- markings. The
difference between -min./max.- is approximately 0.48 US Quarts (0.45 l).

CAUTION

The oil specification in Section 1.9.1 must be adhered to!

Содержание AT01-200

Страница 1: ...EASA approved and mandatory Failing to follow the procedures and limits set forth in this handbook can lead to a loss of liability by the manufacturer THE HANDBOOK The handbook is presented in loose...

Страница 2: ...02 03 2020 03 03 2021 0 2 TABLE OF CONTENTS SECTION GENERAL 1 OPERATING LIMITATIONS approved section 2 EMERGENCY PROCEDURES approved section 3 NORMAL PROCEDURES approved section 4 PERFORMANCE partly a...

Страница 3: ...nted the list of resulting effective chapters can be found in chapter 9 Section Issue Approved Page Date 0 A 02 0 1 to 0 6 03 03 2021 1 A 02 1 1 to 1 12 03 03 2021 2 A 02 X 2 1 to 2 10 03 03 2021 3 A...

Страница 4: ...d by a vertical black line adjacent to the applicable revised area A new issue code appears in the footer of the revised pages If revisions are distributed the applicable sections are to be exchanged...

Страница 5: ...1 200C Section 0 Document Nr Issue Supersedes Issue Date Page FM AT01 1010 106 A 02 A 01 02 03 2020 03 03 2021 0 5 The technical content of this document is approved under the authority of the DOA ref...

Страница 6: ...1 200 related Manuals and Publications AQUILA Aviation International GmbH OT Sch nhagen Flugplatz D 14959 Trebbin Tel 49 0 33731 707 0 Fax 49 0 33731 707 11 E Mail kontakt aquila aviation de Internet...

Страница 7: ...OTES 1 3 1 4 PRINCIPLE AIRCRAFT DIMENSIONS 1 4 1 4 1 1 4 2 1 4 3 1 4 4 1 4 5 Overall Dimensions Wings Horizontal Stabilizer Elevator Fuselage and Vertical Stabilizer Rudder Landing Gear 1 4 1 4 1 4 1...

Страница 8: ...egarding equipment approved for installation in the AQUILA AT01 200 is provided in Section 6 of this manual and in the approved equipment overview list in the Maintenance Manual Document Number MM AT0...

Страница 9: ...not strictly adhered to The issues addressed under these text boxes directly affect the airworthiness and the safe operation of the aircraft CAUTION Procedures practices etc which may result in damag...

Страница 10: ...eight 7 87 ft 2 40 m 1 4 2 Wings Airfoil HQ XX mod Area 113 02 sq ft 10 50 m Aspect Ratio 10 10 Mean Aerodynamic Chord MAC 3 51 ft 1 07 m 1 4 3 Horizontal Stabilizer Elevator Area 21 52 sq ft 2 00 m S...

Страница 11: ...POH AQUILA AT01 200C N VFR Section 1 GENERAL Document Nr Issue Supersedes Issue Date Page FM AT01 1010 281 A 02 A 01 02 03 2020 03 03 2021 1 5 1 5 AQUILA AT01 200 THREE VIEW DRAWING...

Страница 12: ...75 05 Diameter 68 9 in 175 cm 1 8 FUEL The following fuel grades are approved for use min RON 95 EN228 Super ASTM D4814 EN228 Super plus AVGAS 100LL ASTM D910 AVGAS UL 91 ASTM D7547 Left Fuel Tank Rig...

Страница 13: ...e of the ROTAX Service Instruction SI 914 019 The following chart shows the recommended oil viscosity as a function of the climatic conditions The use of multi grade oils is recommended Figure 1 2 CAU...

Страница 14: ...ture ratio anti freeze water 50 15 50 15 CAUTION Low quality or contaminated coolant may lead to deposits in the cooling system which may result in insufficient engine cooling Coolant Quantity Minimum...

Страница 15: ...ea level KCAS CAS expressed in knots TAS True Airspeed the airspeed relative to undisturbed air which is the CAS corrected for altitude temperature and compressibility GS Ground speed speed of the air...

Страница 16: ...akeoff weight and basic empty weight Usable Fuel Fuel available for flight planning Unusable fuel Fuel remaining in the fuel tanks that cannot be safely used in flight Center of Gravity C G The point...

Страница 17: ...Glass Fiber Reinforced Plastic CFRP Carbon Fiber Reinforced Plastic ACL Anti Collision light VFR Visual Flight Rules PFD Primary Flight Display ADC Air Data Computer AHRS Attitude and Heading Referenc...

Страница 18: ...2 CONVERSION FACTORS 1 12 1 Length 1 ft 0 304 m 1 in 25 4 mm 1 12 2 Speed 1 kt 1 852 km h 1 mph 1 609 km h 1 12 3 Pressure 1 hPa 100 N m 1 mbar 1 in Hg 33 865 hPa 1 psi 68 97 mbar 1 12 4 Mass Weight 1...

Страница 19: ...D INDICATOR MARKINGS 2 3 2 4 POWER PLANT LIMITATIONS 2 3 2 4 1 2 4 2 Engine Propeller 2 3 2 4 2 5 MARKINGS ON THE GLASS PANEL ENGINE MONITOR MVP 50P AQ 2 5 2 6 WEIGHT LIMITS 2 6 2 7 CENTER OF GRAVITY...

Страница 20: ...ss Panel Engine Monitor MVP 50P AQ must be carried on board the aircraft and be accessible to the crew during flight 2 2 AIRSPEED LIMITATIONS The airspeeds given below are expressed in Indicated Airsp...

Страница 21: ...165 Maximum speed for all operations 2 4 POWER PLANT LIMITATIONS 2 4 1 Engine a Manufacturer BRP ROTAX GmbH Co KG Gunskirchen Austria b Model 914 F3 NOTE The engine is equipped with a hydraulic propel...

Страница 22: ...Pressure Maximum MCP 35 inHg Maximum TOP 5 min 40 inHg g Oil Temperature Maximum 266 F 130 C Minimum 122 F 50 C h Cylinder Head Temperature CHT Maximum 248 F 120 C i Minimum temperature to start the e...

Страница 23: ...inimum Green Arc normal operating range Yellow Arc caution Red Line maximum Tachometer RPM 535 2260 2260 2385 2385 Oil Temperature F C 122 50 122 266 50 130 266 130 Cylinder Head Temperature F C 248 1...

Страница 24: ...wing leading edge at the fuselage wing junction With the aircraft leveled the reference datum and the vertical fall in a plane The center of gravity must be within the following limits Forward Limit...

Страница 25: ...ceeded while performing any approved maneuvers Flight Load Factor g at VA at VNE With Flaps Extended Positive 4 0 4 0 2 0 Negative 2 0 2 0 0 WARNING Exceeding the flight load factors limits may result...

Страница 26: ...nstruments MVP 50P AQ Annunciator panel AP7DAQ BAT2 TCU Lighting Position lights Anti Collision Lights Landing Lights Instrument lighting Cabin lighting Flashlight Other Equipment Seat belts for each...

Страница 27: ...0 minutes NOTE The amount of unusable fuel was determined with flap on LDG and VFE 90 kts It is the worst case fuel supply configuration within section 4 NORMAL PROCEDURES NOTE The fuel quantity fuel...

Страница 28: ...M AT01 1010 281 A 02 A 01 02 03 2020 03 03 2021 2 10 2 15 PLACARDS 1 On the instrument panel in the lower middle section of the panel 2 On the instrument panel below the Airspeed Indicator 3 On the in...

Страница 29: ...SPECTION 4 9 4 5 CHECKLISTS FOR NORMAL PROCEDURES 4 11 4 5 1 4 5 2 4 5 3 4 5 4 4 5 5 4 5 6 4 5 7 4 5 8 4 5 9 4 5 10 4 5 11 4 5 12 4 5 13 4 5 14 4 5 15 Before Engine Start up Engine Start up Before Tax...

Страница 30: ...tion 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 en...

Страница 31: ...er operational weight TAKE OFF Airspeed IAS kts Normal climb speed to 50 Feet Flaps T O 57 Best rate of climb speed at sea level Flaps UP VY 65 Best angle of climb speed at sea level Flaps T O VX 52 L...

Страница 32: ...right wing drain and visually inspect for contamination 2 Gascolator drain drain and visually inspect for contamination A CABIN 1 Aircraft Documentation CHECK on board 2 Ignition key REMOVED 3 ALT1 BA...

Страница 33: ...020 03 03 2021 4 5 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...

Страница 34: ...n CHECK fitting and bolt connection proper control cable connection and safe tied d Vertical stabilizer Visual inspection 4 Right main landing gear a Landing gear strut Visual inspection b Wheel Fairi...

Страница 35: ...er Ignition ALT1 BAT switch and ALT2 BAT2 switch OFF Set the parking brake WARNING RISK OF BURNS Only check the oil and coolant levels when the engine is cool a Check oil level Turn the propeller seve...

Страница 36: ...r d Cooler intake oil water intercooler CHECK if free from obstructions e Cowling Visual Inspection CHECK Camloc fasteners f Propeller and Spinner Visual inspection g Propeller blades CHECK for cracks...

Страница 37: ...ne is cool 4 Check oil level Turn the propeller several times in the direction of engine rotation to pump oil from the engine back into the oil tank Stop turning the propeller when air begins to retur...

Страница 38: ...Seating position adjust and lock check that nose wheel steering and brakes can be operated 11 Carburetor heat CHECK for free movement then PUSH OFF 12 Cabin heat CHECK for free movement then PUSH OFF...

Страница 39: ...ottle IDLE 11 Propeller Control Lever HIGH RPM position 12 Avionics Switch OFF 13 P S Heat if installed OFF 14 Circuit Breakers CHECK all set NOTE Cage the Attitude Indicator if installed before switc...

Страница 40: ...how rising values within 10 seconds after engine start otherwise shut down the engine immediately NOTE The starter may not be operated for more then 10 seconds at a time Allow the starter to cool off...

Страница 41: ...nd P S HEAT YELLOW warning lights illuminate 4 Engine instruments CHECK NOTE Oil can be brought up to temperature during taxiing 5 Voltmeter CHECK if GREEN 6 ALT1 switch OFF ammeter ALT2 5A ALT2 OK 7...

Страница 42: ...RPM drop must be noticeable then BOTH position 9 Carburetor heat PULL ON no RPM drop if TCU OK 10 Carburetor temperature indicator slight rise in temperature 11 Carburetor heat PUSH OFF 12 Propeller...

Страница 43: ...ION For the shortest take off distance over a 50 feet obstacle at sea level 7 Rotate speed 50 KIAS 8 Climb speed VX 52 KIAS 4 5 7 Climb 1 Throttle max 5 minutes WIDE OPEN 40 inHg afterwards 100 MCP 35...

Страница 44: ...11 3 Flaps switch UP 4 Trim switch SET as required 5 P S Heat switch if installed AS REQUIRED OFF AT OAT 59 F 15 C 6 Engine instruments CHECK if in GREEN range 7 Carburetor temperature indicator MONIT...

Страница 45: ...required CAUTION In strong headwinds or crosswinds in turbulent air or in wind shear it may be desirable to approach using less flaps and at a higher airspeed 4 5 11 Go Around Balked Landing 1 Propell...

Страница 46: ...ion Switch OFF 8 ALT2 BAT2 switch OFF 9 Electrical equipment OFF 10 ALT1 BAT switch OFF NOTE The GARMIN G500 TXi and the MVP 50P AQ are turned off with the ALT1 BAT switch 11 Chocks and tie downs AS R...

Страница 47: ...ng 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 per...

Страница 48: ...POH AQUILA AT01 200C Section 4 NORMAL PROCEDURES Document Nr Issue Supersedes Issue Date Page FM AT01 1010 106 A 02 A 01 02 03 2020 03 03 2021 4 20 intentionally left blank...

Страница 49: ...ce of installed equipment Only the supplements that apply to the configuration of your aircraft must be contained in this section Section 9 2 Index of Supplements lists all existing approved supplemen...

Страница 50: ...t VFR AT01 200C AS 09 Garmin GTN 650 Xi AS 10 Garmin GMA 350 c AS 11 ELT Kannad 406 AS 14 Trig TT22 AS 17 Garmin GTR 225 225A 225B AS 18 Garmin GNC 255A 255B AS 19 Garmin GMA 340 AS 21 Garmin GTX 335...

Страница 51: ...0P AQ This POH supplement is applicable and must be inserted into Section 9 of the Pilot s Operating Handbook when the AQUILA AT01 200C is equipped for Day and Night VFR Section 1 2 and 3 of the basic...

Страница 52: ...Change Effected Pages Date of Issue A 01 Initial Issue EASA 10072382 All 02 03 2020 A 02 editorial changes chapt 1 2 03 03 2021 0 2 LIST OF CURRENT PAGES Page Issue Date Page Issue Date 1 1 to 1 12 A...

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