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POH / AFM

AQUILA AT01-100A

Section 4

NORMAL PROCEDURES

Document Nr.:

Issue:

Supersedes Issue:

Date:

Page:

FM-AT01-1010-101

A.09

A.08 (25.05.2020)

03.03.2021

4 - 12

4.5.2

Engine Start-up

Fuel Pump

switch

FUEL

warning light

OFF

Throttle

- Cold Engine

IDLE

- Hot Engine

0.8 in. (2 cm) OPENED

Choke

- Cold Engine

PULL, and keep pulled

- Hot Engine

RELEASE (automatic reset)

Brakes

PRESS both pedals

Propeller area

CLEAR

Ignition switch

START, then BOTH

Oil Pressure

CHECK, if oil pressure rises

CAUTION

The oil pressure has to show rising values within 10 seconds after engine start, otherwise shut

down the engine immediately!

NOTE

The starter may not be operated for more than 10 seconds at a time. Allow the starter to cool

off for at least 2 minutes between attempts.

ALT 1

warning light

OFF

10.

Fuel Pump

switch

OFF

Содержание AT01-100A 2021

Страница 1: ...EASA FAA 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 lo...

Страница 2: ...5 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 appro...

Страница 3: ...mented the list of resulting effective chapters can be found in chapter 9 Section Issue Approved Page Date 0 A 09 0 1 to 0 6 03 03 2021 1 A 08 1 1 to 1 12 25 05 2020 2 A 09 X 2 1 to 2 10 03 03 2021 3...

Страница 4: ...th the updated version 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 carri...

Страница 5: ...T01 100A Section 0 Document Nr Issue Supersedes Issue Date Page FM AT01 1010 101 A 09 A 08 25 05 2020 03 03 2021 0 5 The technical content of this document is approved under the authority of the DOA r...

Страница 6: ...ed below a AQUILA AT01 100 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...

Страница 7: ...TOR MARKINGS 2 3 2 4 POWER PLANT LIMITATIONS 2 3 2 4 1 2 4 2 Engine Propeller 2 3 2 4 2 5 POWER PLANT INSTRUMENT MARKINGS 2 5 2 6 OTHER INSTRUMENT MARKINGS 2 5 2 7 WEIGHT LIMITS 2 6 2 8 CENTER OF GRAV...

Страница 8: ...ng limitations 2 2 AIRSPEED LIMITATIONS The airspeeds given below are expressed in Indicated Airspeeds IAS the airspeed shown on the airspeed indicator Indicated Airspeed IAS kts Remarks VA Maneuverin...

Страница 9: ...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 912 S3 NOTE The engine is equipped with a hydraulic propel...

Страница 10: ...f Oil Temperature Maximum 266 F 130 C Minimum 122 F 50 C g Cylinder Head Temperature CHT Maximum 248 264 F 120 129 C h Minimum temperature to start the engine Minimum 13 F 25 C At an OAT below 13 F 2...

Страница 11: ...ting 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 248 264 120 129 Oil Pressure psi b...

Страница 12: ...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 16 8 in 0 427m aft of Datum Rearward Limit 20 6 i...

Страница 13: ...ight 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 in damage to the aircraft structure CAUTION Mane...

Страница 14: ...Amperemeter Tachometer Voltmeter Warning Light ALT 1 Other Equipment Seat belts for each occupied seat Emergency Hammer The minimum equipment listed in Table 1 is valid for Germany Other countries may...

Страница 15: ...US gal 5 2 l For approved fuel grades please refer to paragraph 1 8 CAUTION To ensure both fuel tanks are emptied evenly switch to the other tank at least every 60 minutes NOTE The amount of unusable...

Страница 16: ...l 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 including spins are prohibited For...

Страница 17: ...INSPECTION 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 T...

Страница 18: ...ection 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...

Страница 19: ...ower 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...

Страница 20: ...left right wing drain and visually inspect for contamination 2 Electrical fuel pump drain drain and visually inspect for contamination A CABIN 1 Aircraft Documentation CHECK on board 2 Ignition key RE...

Страница 21: ...2020 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 lea...

Страница 22: ...ion 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 Fai...

Страница 23: ...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 Th...

Страница 24: ...ual inspection f Chocks and tow bar REMOVE 8 Left wing a Entire wing surface upper and under side Visual inspection b Fuel vent CHECK if clear c BAT switch ON d Stall warning press to upper detent war...

Страница 25: ...ol 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 return to the...

Страница 26: ...Control locks remove 10 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 fre...

Страница 27: ...ck locking mechanism 6 Parking Brake SET pull lever back 7 Control column CHECK for free movement and correct control surface deflections 8 Fuel Selector Valve LEFT or RIGHT 9 Carburetor Heat PRESS 10...

Страница 28: ...L and keep pulled Hot Engine RELEASE automatic reset 5 Brakes PRESS both pedals 6 Propeller area CLEAR 7 Ignition switch START then BOTH 8 Oil Pressure CHECK if oil pressure rises CAUTION The oil pres...

Страница 29: ...mperature during taxiing 4 Voltmeter CHECK if needle is within the green range 5 Trim switch and indication functional CHECK 6 Flap switch and indication functional CHECK afterwards UP 7 P S Heat swit...

Страница 30: ...drop must be noticeable then BOTH position 9 Carburetor heat PULL ON RPM drop 20 to 50 RPM 10 Carburetor temperature indicator if installed CHECK 11 Carburetor heat PUSH OFF 12 Propeller control leve...

Страница 31: ...wer RPM second CAUTION 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 WIDE OPEN 2 Propeller control leve...

Страница 32: ...SET as required 6 P S Heat switch if installed as required OFF at OAT 59 F 15 C 7 Engine instruments CHECK if in green range 8 Carburetor temperature indicator if installed MONITOR CAUTION During fli...

Страница 33: ...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 Thrott...

Страница 34: ...e aircraft must be grounded for example at the end of the exhaust pipe 3 Open fuel tank filler cap 4 Refuel both tanks equally NOTE Insert the fuel pump nozzle carefully into the tanks to avoid damage...

Страница 35: ...N 8 HANDLING SERVICE MAINTENANCE Page 8 1 INTRODUCTION 8 2 8 2 AIRCRAFT INSPECTION PERIODS 8 2 8 3 MODIFICATIONS AND REPAIRS 8 2 8 4 GROUND HANDLING 8 3 8 4 1 8 4 2 8 4 3 8 4 4 Towing Parking Tie Down...

Страница 36: ...MM AT01 1020 110 the Operation Manual of the ROTAX type 912 engine series and the mt propeller Operation and Installation Manual CAUTION If the engine is operated extensively on AVGAS 100LL more than...

Страница 37: ...raft can be pivoted around the main landing gear CAUTION 1 Never push pull or lift on the horizontal stabilizer or the spinner 2 Never push or lift the control surfaces and flaps 8 4 2 Parking For sho...

Страница 38: ...ith the aircraft and suitable tie down ropes in the aircraft The tie down points should be covered with tape while flying to keep them clean 8 4 4 Jacking Two conical jacking points are located on the...

Страница 39: ...ld be washed regularly using plenty of water a clean sponge and chamois leather Severe contamination and dirt especially insects should be washed off immediately after every flight as it is more diffi...

Страница 40: ...ilable Always follow the manufacturer s instruction to ensure the desired results The inside of the canopy may be treated in the same way 8 5 3 Propeller Refer to current issue of the Operating and In...

Страница 41: ...iece 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 supplem...

Страница 42: ...N 650 Xi AS 10 Garmin GMA 350 AS 11 ELT Kannad 406 AS 12 Garrecht TRX 1500 AS 13 Garrecht TRX 2000 AS 14 Trig TT22 AS 15 Garmin SL 30 AS 16 ADF KR 87 AS 17 Garmin GTR 225 225A 225B AS 18 Garmin GNC 25...

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