POH
AQUILA AT01-200C (N/VFR)
Section 2
LIMITATIONS
Document Nr.:
Issue:
Supersedes Issue:
Date:
Page:
FM-AT01-1010-281
A.02
A.01 (02.03.2020)
03.03.2021
2 - 3
2.3 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
Yellow arc
130-165
Operations in this region must be conducted with
caution and only in smooth air.
Red line
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 propeller governor and drives the propeller via a
reduction gearbox. The gearbox reduction ratio is 2.43 : 1.
The tachometer indicates the propeller speed. As a result, all rpm readings in this manual are
expressed as propeller speeds, unlike the data in the Engine Operator's Manual.
c)
Power Plant Limitations
Maximum Takeoff Power:
113.3 BHP (84.5 kW)
Maximum Takeoff Prop Speed (5 min.):
2385 RPM
Maximum Continuous Power:
98.6 BHP (73.5 kW)
Maximum Continuous Prop Speed:
2260 RPM
