MARO HS16
MARO HS16
MARO HS16
If a mechanic is using a Torquemeter, what he must check first?
That the torquemeter is labelled and that the due date for next calibration has not expired
A commercial transport aircraft is equipped with a set of service points for system servicing and refilling of system fluids (liquid or gaseous). Mention 5 examples of such service points.
- Portable water filling
- IDG Oil filling
- APU Oil filling
- Engine Oil filling
- Hydraulic Oil filling (Bremsflüssigkeit)
- Oxygen System
- Toilet Servicing (leeren)
The basic structure of a commercial transport aircraft is mainly made of Aluminium alloys. On which structural components no Aluminium alloy is used and what instead?
- Tital alloy (engine)
- Engine Pylon, engine disks
Composite materials are also extensively used in aircraft structures. Mention 3 examples of aircraft parts, which are most commonly produced with composite materials.
- flaps, flap track fairings, spoiler, belly fairing
- radome, stabilizer, L/G doors, naccelle rowlings
A line maintenance engineer shall exchange one of several identical components on an aircraft. He will be able to identify the component’s location by means of the
- Major zone, zone and sub zone numbers
- FIN number (Functional Identification Number)
Aircraft systems and structures are identified by means of a specific classification system. Name it.
ATA chapters (Air Transport Assocciation System)
For maintenance purposes, mainly related to the landing gear, four jacking points are provided. Where have they located?
- one below each wing
- one in front of the nose landing gear bay
- one safety point under the rear fuselage point
The air conditioning system basically ensures
- temperatur regulation
- ventilation and pressurisation
Which are the controllers related to the pressurization system?
CPC 1 & CPC 2
Correct cabin pressurization is obtained by controlling the conditioned air discharge through
two outflow valves
Which and how many valves do prevent excessive positive or negative differential pressure?
- Two Safety Valves (installed on aft pressure dome)
- One Negative Pressure Relieve Valve (installed on FWD Fuselage)
Mention 5 communication systems installed on A330 Aircraft.
- 2 HF / 3VHF Systems
- SELCAL (selective calling)
- ACARS (Aicraft Communication Addressing and Reporting System)
- SATCOM System
- Passenger Address System
- CIDS (Cabin Intercommunication Data System)
- IFE
- Interphone communication System
- Cockpit Voice Recorder
- CPDLC
For what reason interphones are used – mention 3
- Cabin interphone (Cabin - Cockpit)
- Flight interphone (Ground engineer)
- Service interphone (com. between verious interphones)
Mention the possible supply sources for the aircraft’s electrical systems
AC electrical power supplied to the aircraft systems has following voltage/frequency characteristics:
115V / 400Hz
How many Batteries are installed (name it)?
3 Batteries (2 Main Batteries BAT 1+2; 1 APU Battery)
How are the main electrical systems feeded if during flight both IDG and the APU Generator fails?
With the Emergency Generator (Constant Speed Motor / Generator) driven by the green hydraulic system & RAT activation
What are the aircraft equipment and furnishings?
- the cockpit
- the passenger compartment
- the cargo compartments
- the avionics compartment
- the emergency equipment
What is the Nacelle and what is the purpose of it?
- Nacelle is the aerodynamic structure around the basic engine (Nose Cowl or Intake Cowl, Fan Cowls, Thrus Reverser, Exhaust Nozzle and Exhaust Plug)
- The purpose is to prevent damage to the basic engine, to smoothout the Fan Air Flow, give additional strenght to the engine structure.
Write in full text the following acronyms:
- DFDR:
- THS:
- RAT:
- CVR:
- FCPC:
- SFCC:
- ACARS:
DFDR: Digital Flight Data Recorder
THS: Trimmable Horizont Stabilizer
RAT: Ram Air Turbine
CVR: Cockpit Voice Recorder
FCPC: Flight Control Primary Computer
SFCC: Slat/Flap Control Computer
ACARS: Aicraft Communication Addressing and Reporting System
Which compartments are given to load freight?
FWD, AFT and BULK Cargo compartments
The fire protection system consists of
The flight controls are driven by which hydraulic system?
Green, Blue and Yellow Hydraulic Systems
The roll movement is achieved by which surfaces?
2 Ailerons and 5 spoilers on each wing
A computer arrangement permanently controls and monitors the flight control surfaces. Name the involved computers
3 FCPC, 2 FCSC, 2 SFCC, 2 FCDC
All the flight controll surfaces are electrically controlled and hydraulically operated. Which flight Controlls (actuators) are backed-up with mechanical cables?
- THS (Pitch axis) -> Trimmable horizontal stabilizer
- Rudder (Yaw Axis)
The 3 principal flight control modes are
The purpose of the Manoeuvre Load Alleviation (MLA) function is to reduce the loads applied to the outer wing structure during high g manoeuvre. Explain the function's principle.
The function is achieved by 2 ailerons & 3 external spoilers on each wing. These surfaces are deflected upwards on both wings.
Fill in the missing word within the below shown "fly by wire" philosophy.
Auto Pilot or Pilot command/order - Computed order - ...
Feedback / Aircraft response
What are the main advantages of the "fly by wire" philosophy?
Improvement in redundancy, in handling qualities and thus in performances.
Name the three Flight Laws.
- Normal Law
- Alternate Law
- Direct Law
Name all available Fuel Tanks.
- Center Tank
- LH & RH Inner Wing Tanks
- LH & RH Outer Wing Tanks
- LH & RH Wing surge vent Tanks
- Trim Tank
- Ventilisation Tank / Vent Box
From which Fuel Tank the engine are feeded?
LH & RH Inner Wing Tanks (Collector Cell)
Are the Fuel Tank Pumps interchangeable?
The purpose of the Trim Transfer System is to
control the center of gravity position
There are a number of Magnetic Lever Indicators installed. For what reason?
To determine the physical Aircraft fuel volume in the tanks, if the indication system is inoperative or showing a wrong value.
The aircraft is equipped with three hydraulic systems which are connected to each other. True or False?
False! Green, Blue and Yellow System are fully independent
In normal operation the Hydraulic Systems are powered by Engine Driven Pumps (EDPs). What is the nominal pressure?
3000 psi
Engines are not running and the yellow electrical pump for cargo door opening is not functioning. What can be done?
Cargo door opening with the mechanical hand pump (located at the yellow ground service panel)
Which is the main Hydraulic System?
Green Hydraulic System
-
- 1 / 144
-
Lernkarten
Which of the following sentences is wrong?
During a quality audit an aircraft affected Level 1 finding was opended. The finding must be actioned
Before next flight
How and by whom an aircraft is released between two letter checks?
CRS signature by B1 or B2 certifying staff on technical log after maintenance action
Mention 5 items which are mandatory to be listed on the CRS after a maintenance letter check.
- Aircraft Type
- Aircraft Registration and MSN
- Operator Name
- Type of Maintenance Check
- Location of the Check
- Date of check completed
- Aircraft FH / FC
- Reference to Bill of Work
- Contract Reference
- Deferred items
- Part-145 approval reference
- Name & Signature of authorized person
Write in full text the following acronym ARC
Airworhiness Review Certificate
The periodical airworthiness review which shall be carried out on all aircraft in an operator’s fleet consists of
- Full documented review
- Physical survey
An ARC is valid for
The Subpart-I approval including assessed Review Staff must be in place for each approved CAMO.
What is the meaning of «controlled environment»?
An aircraft in a controlled environment is an aircraft continuously managed by an approved continuing airworthiness management organisation, which has not changed organisations in the previous 12 months, and which is maintained by approved maintenance organisations
An Aircraft will enter the fleet from a third country (outside EU). Which ARC must be issued and by whom?
ARC 15a, by the competent authority
In which case the CAMO shall send a documented recommendation to the competent authority?
- if an aircraft will enter the fleet from thirs country
- if the CAMO is not Subpart-I approved
- it the aircraft is not within the controled environment
When Subpart-I approved, is it allowed to subcontract Subpart-I realted tasks to another Subport-I approved organisation?
An EASA Part 145 maintenance organisation, its structures and its processes are described in the
A Part 145 maintenance organisation shall appoint a manager who has corporate authority for ensuring that all maintenance required by the customer can be financed and carried out to the standard required by the regulations. This person is
The appointment of a Quality Assurance Manager by a Part 145 maintenance organisation depends on the workscope
An EASA Part 145 maintenance organisation shall maintain
Aircraft maintenance approvals are divided in different categories. Mention the related maintenance categories listed on an approval:
Class A: aircraft manitenance (line/base)
Class B: engine prop apu maint
Class C: component maint. (engin. apu excl.)
Class D: specialiseed services (ndt)
The holder of a category B1 licence is entitled to release an aircraft after a Base Maintenance letter check.
Any EASA Part 145 maintenance organisation shall have aircraft type rated supporting certifying staff trained according the related EASA Part. These certifying staff holding a B1 or B2 licence which corresponds to following categories:
B1 (mechanics, aircraft systems), B2 (avionics & electrical)
The minimum age for certifying staff category B1 and B2 is
21 years
The CRS after an aircraft maintenance letter check can be signed by which licence holder?
Certifying Staff with C-licence
A workshop mechanics will find work instructions for a maintenance task to be performed on a component removed from the aircraft in the following manual
Which document provides working instructions and is signed off by the mechanic once the job is completed?
Workcard / Jobcard / Taskcard
The Production planning of an EASA Part 145 maintenance organisation shall ensure
availability of personnel, tools, equipment, material, maintenance data and facilities
What are the four human factors, which might influance the individual negatively?
- Fatigue
- External Distractions
- Stress / Pressure
- Personal Issues
How long the maintenance organisation must retain maintenance records?
three years from the date the aircraft/component was released
What stands "SMS" for within the context of aviation?
Safety Management System
How long a maintenance organisation approval is valid?
unlimited duration
If a mechanic is using a Torquemeter, what he must check first?
That the torquemeter is labelled and that the due date for next calibration has not expired
A commercial transport aircraft is equipped with a set of service points for system servicing and refilling of system fluids (liquid or gaseous). Mention 5 examples of such service points.
- Portable water filling
- IDG Oil filling
- APU Oil filling
- Engine Oil filling
- Hydraulic Oil filling (Bremsflüssigkeit)
- Oxygen System
- Toilet Servicing (leeren)
The basic structure of a commercial transport aircraft is mainly made of Aluminium alloys. On which structural components no Aluminium alloy is used and what instead?
- Tital alloy (engine)
- Engine Pylon, engine disks
Composite materials are also extensively used in aircraft structures. Mention 3 examples of aircraft parts, which are most commonly produced with composite materials.
- flaps, flap track fairings, spoiler, belly fairing
- radome, stabilizer, L/G doors, naccelle rowlings
A line maintenance engineer shall exchange one of several identical components on an aircraft. He will be able to identify the component’s location by means of the
- Major zone, zone and sub zone numbers
- FIN number (Functional Identification Number)
Aircraft systems and structures are identified by means of a specific classification system. Name it.
ATA chapters (Air Transport Assocciation System)
For maintenance purposes, mainly related to the landing gear, four jacking points are provided. Where have they located?
- one below each wing
- one in front of the nose landing gear bay
- one safety point under the rear fuselage point
The air conditioning system basically ensures
- temperatur regulation
- ventilation and pressurisation
Which are the controllers related to the pressurization system?
CPC 1 & CPC 2
Correct cabin pressurization is obtained by controlling the conditioned air discharge through
two outflow valves
Which and how many valves do prevent excessive positive or negative differential pressure?
- Two Safety Valves (installed on aft pressure dome)
- One Negative Pressure Relieve Valve (installed on FWD Fuselage)
Mention 5 communication systems installed on A330 Aircraft.
- 2 HF / 3VHF Systems
- SELCAL (selective calling)
- ACARS (Aicraft Communication Addressing and Reporting System)
- SATCOM System
- Passenger Address System
- CIDS (Cabin Intercommunication Data System)
- IFE
- Interphone communication System
- Cockpit Voice Recorder
- CPDLC
