Aquila ATO1, Руководство по обслуживанию

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MAINTENANCE MANUAL
AQUILA AT01
Aviation by Excellence AG
RECORDERS – MAINTENANCE PRACTICES
1.
A. This section covers miscellaneous avionic equipment. This includes the KAPI Air Control FDR 07
Data Logger System. The scope of maintenance is limited to the removal and installation of
components. The installation instructions provided herein pertains only to the replacement of
components already installed in the aircraft and is not considered to be an installation instruction
for the implementation as a modification. For this, refer to the applicable Service Bulletin or
contact the manufacturer of the aircraft. For further information on the equipment, refer to the
appropriate publications of the equipment manufacturer. For overhaul and repair, the
manufacturer of the equipment has to be consulted.
B. KAPI Air Control FDR 07 Data Logger System
The KAPI Air control FDR 07 is derived from KAPI Flight Data Recorder (FDR) and is designed to
provide a system for the recording, storing, processing, evaluation and transmission of technical,
operational and flight data. The KAPI Air control FDR 07 is based on a one circuit board system
which is controlled by a microprocessor produced at VDO. For the acquisition of the data to be
stored or transmitted to the ground station, the processing unit of the KAPI system uses both, the
access to data signals of already existing sensors in the aircraft (engine parameters) as well as its
own sensors that have to be additionally installed together with the KAPI system (airspeed and
g-sensor). Furthermore, the KAPI system processes data derived from GPS-signals that are
received with an external GPS-antenna which is a combined GPS receiving and GSM transmitting
antenna for the data transfer to the ground station.
The GPS/GSM antenna is mounted on a support bracket attached to the LH side support plate of
the Instrument Panel. Directly on the other side of the LH side support of the Instrument Panel,
the KAPI unit is installed which is the main item of the whole KAPI Data Logger System. The
KAPI system includes also two additional sensor units, the airspeed and g-sensor, which are both
mounted with attachment angles on the base plate of the instrument panel behind the gyros. The
power supply of both sensors is directly provided by the main KAPI unit and is integrated into its
connection cable. The airspeed sensor is additionally connected to the pitot pressure system of
the aircraft.
Both electrical supply circuits of the KAPI system are protected by properly labelled fuses that are
located in the engine compartment.
For more information on the KAPI Air Control FDR 07 Data Logger System, refer to the
documentation and manuals of the manufacturer of the KAPI System.
C. Specifications
(1) Physical Unit Size: H/W/L - 30 mm (1.18 in.) / 105 mm (4.13 in.)/
105 mm (4.13 in.)
Unit Weight: 0.29 kg (0.64 lbs), main unit only
(2) Power Input: 6 to 32 VDC
Consumption: max. 100 mA at 14 VDC (logged in GSM and
GPS activated).
(3) Environmental Temperature: -25°C to +65°C (operating range)
General
31-30-00
Page 201
Indicating / Recording
EFFECTIVITY
Aircraft equipped with KAPI Data Logger System
30.04.08