The document provides information on the maintenance levels, documentation, and technical specifications of the Airbus H-145 D2 helicopter. It discusses three maintenance levels - organizational level which includes daily maintenance, inspections, and simple repairs; intermediate level which includes repairs and inspections; and depot level which includes major overhauls. The document also lists the various technical manuals and documents provided for maintenance technicians, pilots, and manufacturers of components. It specifies that the H-145 D2 is a multi-purpose twin-engine helicopter that seats 8 people and is powered by two Turbomeca Arriel 2E engines.

1. Generalidades y Características Técnicas del
Helicóptero Airbus H-145 D2
AUTOR: CBOS. GONZALEZ BRYAN

2. BK145 D--2
 Since July 2010 flight tests were carried out with a new Fenestron
tail unit. Besides are new Arriel 2E engines with FADEC control
installed, they provide about 25 % more power. A four axis
autopilot system is standard configuration. The cockpit is equipped
with the new HELIONIX avionics system comprising three big
color screens. Its commercial name is H145. The number of
delivered helicopters at the end of the year 2017 is around 160.

3. General Description
of the BK117 D-2
Main Rotor System
Fuselage
Engines
Tail Rotor System
Flight Controls
Electrical System
Landing Gear
Fuel System
General The BK117 D-2 is a
multi purpose twin engine
helicopter in the 4 t class with
eight seats in the basic version

4. Main Rotor System
The main rotor
blades are
manufactured from
fiber-reinforced
plastic and are
directly connected to
the rigid titanium
rotor head.
Fuselage
The primary structure
mainly consists of
sheet metal. Cabin
frame, bottom shell,
doors, engine cowlings
and access panels are
made of composite
material.
Tail Rotor System
The helicopter is
equipped with a fan
in shroud type of tail
rotor (Fenestron)
with 10 blades and a
carbon fiber tail
boom.
Flight Controls
The main rotor is
controlled by a so
called “Flexball”
type cable, routed
from the control
elements via the
cabin nose to the
cabin roof mounted
hydraulic system.
Landing Gear
The BK117 D-2 has
two cross tubes and
two skids. The cross
tubes are designed to
absorb forces during
touch down of the
helicopter, by
bending.
Fuel System
The fuel system
comprises three fuel
tanks, a fuel supply
system, are fueling
and ventilation
system and a
monitoring system.
Engines
The BK117 D-2 is
powered by two
Turbomeca Arriel 2E
engines with a power
output of 445 kW
each.
Electrical System
The fully redundant
28.5 VDC electrical
system is supplied by
two generators and
the battery.

5. Structural Groups of the BK117 D-2
Helicopter Dimensions
Cabin Dimensions

6. Maintenance Concept
GENERAL
Maintenance” covers all scheduled and
unscheduled maintenance activities. It also
applies to the on condition maintenance. It is
based on condition monitoring by visual
checks/inspections and diagnostic features such
as chip detectors, filter bypass indicators,
boroscope access, failure code indications,
built-in tests, warning lights etc.
ORGANIZATIONAL
LEVEL
DEPOT LEVEL (D)
INTERMEDIAT
E LEVEL
The organizational level covers tasks of
the daily servicing,
maintenance checks, inspections for
condition, exchange of
components (e.g. LRU) and quick, simple
repairs as specified in the
aircraft maintenance manual (AMM)
The intermediate level covers repairs on/off
helicopter, extended
periodical inspections as specified in the
aircraft maintenance manual.
To fulfill these tasks, maintenance facility,
qualified personal, test
equipment and special tools are required.
Depot level covers major repair or
overhaul at the manufacturer or at
authorized service stations under
industrial premises.
More extensive tools/test equipment and
specialized personnel are
necessary.
 NOTE The maintenance manual covers
all tasks of organizational level and intermediate
level.
NOTE Documentation and spares for depot
level tasks will be delivered to authorized customers only.

7. BK117 D-2 HELICOPTER
DOCUMENTATION
TECHNICIAN’S
DOCUMENTATION
TECHNICAL
CONTROL
DOCUMENTATION
Structural Repair
Manual (SRM)
Standard Practice
Manual (MTC)
Avionic Manual
(AVM)
Electronic Component
Maintenance Manual (ECMM)
(only on USB stick available)
Wiring Diagram
Manual (WDM)
Illustrated Parts Catalog
inclusive Tools Catalog
(IPC)
- Corrosion and Erosion
Control Guide (CECG)
Airworthiness
Limitations Section
(ALS)
Aircraft Maintenance
Manual (AMM)
System Description
Section (SDS)
Master Servicing
Manual (MSM)
Historical Record
- LOAP (List of
Applicable Publications,
hard copy)
Service Bulletins / Alert
Service Bulletins,
Emergency Alert
Service Bulletins (hard
copy)
Information Notice/ Safety
Information Notice (hard
copy)

8. PILOT’S DOCUMENTATION
The pilot has four documents available
(hardcopy):
NOTE The Flight Manual, the Pilot’s Checklist, the Log
Book and the Minimum Equipment List are hard copies
and must always be present in the helicopter.
OTHER MANUFACTURER’S DOCUMENTATION
The manufacturers of engines, avionics and optional equipment
deliver their own documentation.
Information about these documentation is to be found in the LOAP
Part III.

9. 1.The System Description Section (SDS) belongs to?
a) Technical Control Documentation
b) Technician’s Documentation
c) Maintenance Levels
d) General Description
2. The Historical Register belongs to?
a) Technical Control Documentation
b) Technician’s Documentation
c) Maintenance Levels
d) General Description
3. The concept of organizational level covers the tasks of the daily service, Maintenance controls, status inspections,
belongs to?
a) Depot Level (D)
b) Organizational Level
c) Intermediate Level
d) Maintenance Levels
4. Mention BK117 D-2 maintenance levels
 Organizational Level (O)
 Intermediate Level (I)
 Depot Level (D)
5. Complete the sentence
 The BK145 D-2 is a multi purpose twin engine helicopter in the 4 t class with eight seats in the basic version.
Questions

10. https://www.youtube.com/watch?v=fNsy4fFnxTo