background image

                   

 

POH / AFM 

AQUILA  AT01-100A 

Section 1 

GENERAL 

 

Document Nr.: 

Issue: 

Supersedes Issue: 

Date: 

Page: 

FM-AT01-1010-101 

A.06 

A.02 (15.10.2013) 

01.06.2018 

1 - 8

 

 

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 

coolant. 

Description 

Ethylenglycol 

Water 

Mixture 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: 

 

2.54 US quarts  

(2.4 l) 

 

 

 

 

 

Maximum: 

 

2.64 US quarts  

(2.5 l) 

 
 

 

Overflow Bottle:

  Minimum: 

 

0.106 US quarts  

(0.1 l) 

 

 

 

 

 

Maximum: 

 

0.21 US quarts  

(0.2 l) 

1.10  WEIGHTS 

 

 

Maximum Takeoff Weight (MTOW): 

 

1653 lb. 

(750 kg) 

 

 

Maximum Landing Weight (MLW): 

 

1653 lb. 

(750 kg) 

 

 

Empty Weight (MZFW): 

 

 

 

Refer to section 6 

 

 

Max. Weight in Baggage Compartment:  

88.2 lb. 

(40 kg) 

 

 

(All baggage must be adequately strapped and secured) 

 

 

Max. Wing Loading:  

 

 

 

14.6 lb./ft² 

(71.4 kg/m²) 

 

 

Min. Wing Loading:  

 

 

ca. 

10.77 lb./ft²   (52.6 kg/m²)) 

 

Summary of Contents for AT01-100A

Page 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...

Page 2: ...6 2017 01 06 2018 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...

Page 3: ...Section Issue Approved Page Date 0 A 06 0 1 to 0 6 01 06 2018 1 A 06 1 1 to 1 12 01 06 2018 2 A 05 X 2 1 to 2 10 26 06 2017 3 A 05 X 3 1 to 3 16 26 06 2017 4 A 04 X 4 1 to 4 18 19 10 2015 5 A 05 X 5 1...

Page 4: ...e revised pages If revisions are distributed the applicable sections are to be exchanged with the updated version Generally only complete sections of the POH will be exchanged and not individual pages...

Page 5: ...AT01 100A Section 0 Document Nr Issue Supersedes Issue Date Page FM AT01 1010 101 A 06 A 05 26 06 2017 01 06 2018 0 5 Revision A 06 of AFM ref FM AT01 1010 101 is approved under the authority of DOA r...

Page 6: ...d below a AQUILA AT01 100B 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...

Page 7: ...TES 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 4...

Page 8: ...00 is provided in Section 6 of this manual and in the approved equipment overview list in the Maintenance Manual Document Number MM AT01 1020 110 This handbook includes the material required to be fur...

Page 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 damage...

Page 10: ...Height 7 87 ft 2 4 m 1 4 2 Wings Airfoil HQ XX mod Area 113 02 sq ft 10 5 m Aspect Ratio 10 1 Mean Aerodynamic Chord MAC 3 51 ft 1 07 m 1 4 3 Horizontal Stabilizer Elevator Area 21 52 sq ft 2 0 m Span...

Page 11: ...LA AT01 100A Section 1 GENERAL Document Nr Issue Supersedes Issue Date Page FM AT01 1010 101 A 06 A 02 15 10 2013 01 06 2018 1 5 1 5 AQUILA AT01 100 THREE VIEW DRAWING 2 4 m 7 87 ft 7 4 m 24 28 ft 10...

Page 12: ...0 05 Diameter 66 9 in 170 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 Righ...

Page 13: ...nt issue of the ROTAX Service Instruction SI 912 016 The following chart shows the recommended oil viscosity as a function of the climatic conditions The use of multi grade oils is recommended Figure...

Page 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...

Page 15: ...a 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 airc...

Page 16: ...keoff 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 a...

Page 17: ...No P N Part Number GFRP 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 Atti...

Page 18: ...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...

Page 19: ...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...

Page 20: ...AT01 100C AS 07 Garmin SL 40 AS 08 Garmin GTX 330 328 AS 09 Garmin GTN 650 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...

Reviews: