Diamond Aircraft DA 40 NG User manual

DA 40 NG AFM
Supplement S10 Flight Data Logging
Device
SUPPLEMENT S10
TO THE AIRPLANE FLIGHT MANUAL
DA 40 NG
FLIGHT DATA LOGGING DEVICE
Doc. No. : 6.01.15-E
Date of Issue : 29 Jan 2016
Design Change Advisory : OÄM 40-337/b
This Supplement to the Airplane Flight Manual has been approved under the authority
of DOA No. EASA.21J.052.
DIAMOND AIRCRAFT INDUSTRIES GMBH
N.A. OTTO-STR. 5
A-2700 WIENER NEUSTADT
AUSTRIA Page 9-S10-1, Rev. 0

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0.2 RECORD OF REVISIONS
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0.4 TABLE OF CONTENTS
Page
1. GENERAL ...............................................9-S07-6
2. OPERATINGLIMITATIONS..................................9-S07-7
3. EMERGENCY PROCEDURES ...............................9-S07-7
4A. NORMAL OPERATING PROCEDURES ........................9-S07-7
4B. ABNORMAL OPERATING PROCEDURES ......................9-S07-7
5. PERFORMANCE ..........................................9-S07-7
6. MASS AND BALANCE / EQUIPMENT LIST .....................9-S07-8
7. DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS ...........9-S07-9
8. AIRPLANEHANDLING,CARE ANDMAINTENANCE ............9-S07-12

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Supplement S10 Flight Data Logging
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1. GENERAL
This Supplement describes the function of the Flight Data Logging Device and supplies
all information for the safe and efficient operation of the system. The Flight Data
Logging Device is NOT covered by a TSO, but it has proven fire and crash resistance.
The Flight Data Logging Device is able to record audio signals and flight data. The
recordings can be stored on a SD card and processed with an analysis software on a
personal computer. The recordings are also stored in a hardened and fire proof unit.
The main applications of the Flight Data Logging Device are:
- Flight Data Monitoring
- Training Support
- Troubleshooting Assistance
- Incident/Accident Analysis
This Supplement is a permanent part of the AFM and must remain in the AFM at all
times when the Flight Data Logging Device is installed. For specific information refer to
the documentation of the Flight Data Logging Device manufacturer.

DA 40 NG AFM
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Device
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2. OPERATING LIMITATIONS
No change.
3. EMERGENCY PROCEDURES
No change.
4A. NORMAL OPERATING PROCEDURES
No change.
4B. ABNORMAL OPERATING PROCEDURES
No change.
5. PERFORMANCE
No change.

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Device
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6. MASS AND BALANCE / EQUIPMENT LIST
6.5 Equipment List and Equipment Inventory
Airplane Serial No.: Registration: Date:
Description Type Part No.: Manufacturer S/N in-
stalled
INDICATING / REC. SYSTEM
Sensor Interface Unit APICAP-003 iaero
Power Supply Unit APIPWR-001 iaero
Data Retrieval Unit APISD-001 iaero
Memory and Data Processing Unit APIV2-002-HARDEN iaero
CAN / ARINC Interface Unit i2060-002 iaero
EMI Filter D44-2463-50-00 Diamond Aircraft

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7. DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS
7.13 FLIGHT DATA LOGGING DEVICE
GENERAL DESCRIPTION
The Flight Data Logging Device (APIBOX) is a solid state digital Flight Data
Monitoring System designed for General Aviation use, allowing the recording of a
very large number of aircraft and flight parameters as well as audio signals and to
perform their analysis on the ground on a dedicated and user friendly software. Data
is easily downloaded from the system after each flight using a standard SD card and
can be reviewed on a personal computer through the use of an Analysis Software
provided with the system.
Refer also to the iaero, APIBOX System, Diamond DA 40 NG User Manual.
SYSTEM OVERVIEW
The APIBOX SYSTEM consists of five main components:
• The Memory and Data Processing Unit (APIV2-002-HARDEN) receives
digital raw data from the Sensor Interface Unit, converts them into directly
readable parameters and stores them into the hardened and fire proof
memory. Recorded capacity of the MDPU is very large, both in terms of
audio signals and recorded parameters.
• The Power Supply Unit (APIPWR-001) is connected to the aircraft´s
Battery Bus and Hot Bus and supplies 28V DC to the Memory and Data
Processor Unit.
• The Sensor Interface Unit (APICAP-003) receives the aircraft analog and
digital inputs as well as the pilot and copilot audio intercom unit signals
and processes them into required formats before transmitting them to the
Memory and Data Processing Unit.

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• The CAN/ARINC Interface Unit (i2060-002) receives data from the engine
CAN busses and from the Garmin G1000 via ARINC 429 busses.
• The Data Retrieval Unit (APISD-001), receives all data from the Memory
and Data Processing Unit and stores the data on a removable SD card.
All components of the APIBOX SYSTEM are installed in the aft baggage
compartment under the floor panel, just behind the left passenger seat.
WORKING PRINCIPALS
Data recording
The APIBOX SYSTEM is automatically switched ON when the aircraft Electric Master
switch is selected to the ON position.
The shutdown of the APIBOX SYSTEM is not commanded directly by the pilot but by
a set of conditions that must be met before the system turns itself off:
• Ground speed less than 5 kt
• No engine power
• Accelerometers "still" (no detection of movement)
• Airspeed less than 40 kt
Data are recorded and stored simultaneously and in real time in the crash and fire
resistant memory of the Memory and Data Processing Unit and on the SD card
inserted in the Data Retrieval Unit. All data are recorded at 1 Hz frequency except for
load factors that are recorded at 8 Hz. Total recording capacity of FDR data is about
100 hours and the recording capacity of audio signals is about 50 hours. If one elects
to conserve for example only the last 2 hours of audio recording, then system
memory will store close to 1000 hours of airplane parameters.

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Following parameters are recorded with the installed system:
• Accelerometers (1-4)
• Absolute pressure
• Differential pressure
• Engine type
• Engine number
•RPM
• Coolant temperature
• Power load
• Fuel pressure
• Battery voltage
• Oil temperature
• Oil pressure
• Gearbox temperature
• Fuel Flow
• Autopilot engage status (Optional)
• Flaps (Optional)
• Audio data
Minimum and maximum values of each parameter for each individual flight of the
airplane are recorded and are stored for the whole life of the airplane/system. These
stored data cannot be erased.
Data Downloading
Data can be downloaded manually using a removable SD card. Manual data
download on the ground is done very simply by removing the SD card from the Data
Retrieval Unit and then uploading them into almost any personal computer equipped
with iaero’s Analysis Software.

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Device
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Data Analysis
Each APIBOX SYSTEM is provided with iaero’s Analysis Software that can be
installed on almost any personal computer. When data are uploaded from an SD card
into a Personal Computer, the recorded data are analyzed by the program and
displayed on a synthetic and user-friendly display.
Refer also to iaero, APIBOX SYSTEM documentation.
8. AIRPLANE HANDLING, CARE AND MAINTENANCE
No change.
Other manuals for DA 40 NG
2
Table of contents