AMC2 ORA.ATO.125 Training programme
ED
Decision 2020/005/R
TYPE
RATING COURSES – AEROPLANES
(a) Introduction
(1) When developing the training programme for
a type rating course, in addition to complying with the standards included in
the operational suitability data (OSD), as established in accordance with
Regulation (EC) 1702/2003[31]
for the applicable type, the ATO should also follow any further
recommendations contained therein.
(2) The type rating course should, as far as
possible, provide for a continual process of ground, FSTD and flight training
to enable the student to assimilate the knowledge and skills required to
operate a specific aircraft type safely and efficiently. The student’s ability
to do this should be determined by the demonstration of a satisfactory level
of theoretical knowledge of the aircraft determined by progressive checking of
knowledge and examination, progressive assessment by the ATO during flight
training and the successful completion of a practical skill test with an
examiner.
(3) The type rating course should normally be
conducted as a single, fulltime course of study and training. However, in the
situation where the course is intended to enable a pilot to fly a further
aircraft type while continuing to fly a current type, such as to enable mixed
fleet flying with the same operator, some elements of the theoretical
knowledge course conducted by self-study may be undertaken while the student
continues to fly the current type.
(b) Variants
(1) Familiarisation training: Where an
aeroplane type rating also includes variants of the same aircraft type
requiring familiarisation training, the additional familiarisation training
may be included in the theoretical knowledge training of the initial type
rating course. Flight training should be conducted on a single variant within
the type.
(2) Differences training: Where an aeroplane
type rating also includes variants of the same aircraft type for which
difference training is required, the initial training course should be
directed towards a single variant. Additional training to operate other
variants within the same type rating should be completed after successful
completion of the initial type rating course. However, elements of this
differences training may be undertaken at appropriate stages of the initial
course, with the agreement of the competent authority.
(c) Programme of theoretical knowledge and
flight training
(1) The training programme should specify the
time allocated to theoretical knowledge training, FSTD training and, if not
approved for zero flighttime training (ZFTT), the aeroplane. The initial type
rating course should be programmed on the basis that the student has the
minimum licensing and experience requirements for entry to the course. For a
first type rating on a multi-pilot aeroplane (MPA), the course should also
provide for consolidation and type-specific training in those elements of
basic multi-crew cooperation (MCC) training relevant to the type or variant.
(2) If the ATO wishes to provide a training
course that includes credit for previous experience on similar types of
aircraft, such as those with common systems or operating procedures with the
new type, the entry requirements to such courses should be specified by the
ATO and should define the minimum level of experience and qualification
required of the flight crew member.
(3) The ATO is permitted to contract elements
of training to a third party training provider. In such cases the contracted
organisation should normally be approved to conduct such training. When the
contracted organisation is not an ATO, the competent authority should, within
the approval process of the ATO, include the contracted organisation and be
satisfied that the standard of training intended to be given meets the
requirements. The other obligations of the ATO, such as student progress
monitoring and an adequate management system, can be exercised by the ATO
seeking approval and which retains responsibility for the whole course.
GROUND
TRAINING
(d) Syllabus
The ground
training syllabus should provide for the student to gain a thorough
understanding of the operation, function and, if appropriate, abnormal and
emergency operation of all aircraft systems. This training should also include
those systems essential to the operation of the aircraft, such as
‘fly-by-wire’ flight control systems, even if the flight crew have little or
no control of their normal or abnormal operation.
(e) Theoretical knowledge instruction
The
theoretical knowledge instruction training should meet the general objectives
of (but not be limited to) giving the student:
(1) a thorough knowledge of the aircraft
structure, powerplant and systems, and their associated limitations, including
mass and balance, aircraft performance and flight planning considerations;
(2) a knowledge of the positioning and
operation of the cockpit controls and indicators for the aircraft and its
systems;
(3) an understanding of system malfunctions,
their effect on aircraft operations and interaction with other systems; and
(4) the understanding of normal, abnormal and
emergency procedures.
(f) Facilities and training aids
The ATO
should provide adequate facilities for classroom instruction and have
available appropriately qualified and experienced instructors. Training aids
should enable students to gain practical experience of the operation of
systems covered by the theoretical knowledge syllabus and, in the case of
multi-pilot aeroplanes, enable such practical application of the knowledge to
be carried out in a multi-crew environment. Facilities should be made
available for student self-study outside the formal training programme.
(g) Computer-based training (CBT)
CBT provides
a valuable source of theoretical instruction, enabling the students to
progress at their own pace within specified time limits. Many such systems
ensure that syllabus subjects are fully covered and progress can be denied
until a satisfactory assimilation of knowledge has been demonstrated. Such
systems may allow self-study or distance learning, if they incorporate
adequate knowledge testing procedures. When CBT is used as part of the
theoretical knowledge instruction phase, the student should also have access
to a suitably qualified instructor able to assist with areas of difficulty for
the student.
(h) Self-study and distance learning
Elements of
the theoretical knowledge syllabus may be adequately addressed by distance
learning, if approved, or self-study, particularly when utilising CBT.
Progress testing, either by self-assessed or instructor-evaluated means should
be included in any self-study programme. If self-study or distance learning is
included in the theoretical knowledge training, the course should also provide
for an adequate period of supervised consolidation and knowledge testing.
(i) Progress tests and final theoretical
knowledge examination
(1) The theoretical knowledge training
programme should provide for progressive testing of the assimilation of the
required knowledge. This testing process should also provide for retesting of
syllabus items so that a thorough understanding of the required knowledge is
assured. This should be achieved by intervention by a qualified instructor or,
if using CBT with a self-testing facility, and by further testing during the
supervised consolidation phase of the ground course.
(2) The final theoretical knowledge
examination should cover all areas of the theoretical knowledge syllabus. The
final examination should be conducted as a supervised written (including
computer-based) knowledge test without reference to course material. The pass
mark of 75% assumes the achievement of satisfactory levels of knowledge during
the progressive phase tests of the course. The student should be advised of
any areas of lack of knowledge displayed during the examination and, if
necessary, given remedial instruction. A successful pass of the theoretical
knowledge course and final examination should be a pre-requisite for
progression to the flight training phase of the type rating course, unless
otherwise determined in the OSD established in accordance with Regulation (EC)
1702/2003.
FLIGHT
TRAINING
(j) Flight simulation training devices
(FSTDs)
A type
rating course for a multi-pilot aeroplane should include FSTD training.
The amount
of training required when using FSTDs will depend on the complexity of the
aeroplane concerned, and to some extent on the previous experience of the
pilot. Except for those courses giving credit for previous experience (c.2.),
a minimum of 32 hours of FSTD training should be programmed for a crew of a
multipilot aeroplane, of which at least 16 hours should be in an FFS operating
as a crew. FFS time may be reduced if other qualified FSTDs used during the
flight training programme accurately replicate the cockpit environment,
operation and aeroplane response. Such FSTDs may typically include flight
management computer (FMC) training devices using hardware and computer
programmes identical to those of the aeroplane.
(k) Aeroplane training with FFS
(1) with the exception of courses approved for
ZFTT, certain training exercises normally involving take-off and landing in
various configurations should be completed in the aeroplane rather than in an
FFS. Unless otherwise specified in the OSD established in accordance with
Regulation (EU) No 748/2012 this take-off and landing training should include:
(A) at least four landings in the case of MPAs
(or single-pilot high performance complex aeroplanes (SP HPAs)) where the
student pilot has more than 500 hours of MPA experience (or SPA experience) in
aeroplanes of similar size and performance or, in all other cases, at least
six landings;
(B) at least one full-stop landing; and
(C) one go-around with all engines operating.
This
aeroplane training may be completed after the student pilot has completed the
FSTD training and has successfully undertaken the type rating skill test,
provided it does not exceed 2 hours of the flight training course.
(2) courses approved for ZFTT
(i) During the specific simulator session
before line flying under supervision (LIFUS), consideration should be given to
varying conditions, for example:
(A) runway surface conditions;
(B) runway length;
(C) flap setting;
(D) power setting;
(E) crosswind and turbulence conditions; and
(F) maximum take-off mass (MTOM) and maximum
landing mass (MLM).
(ii) At least one landing should be conducted
as full-stop landing. The session should be flown in normal operation. Special
attention should be given to the taxiing technique.
(iii) A training methodology should be agreed
with the competent authority that ensures the trainee is fully competent with
the exterior inspection of the aeroplane before conducting such an inspection
un-supervised.
(iv) The LIFUS should be performed as soon as
possible after the specific FFS session.
(v) The licence endorsement should be entered
on the licence after the skill test, but before the first four take-offs and
landings in the aeroplane. At the discretion of the competent authority,
provisional or temporary endorsement and any restriction should be entered on
the licence.
(vi) Where a specific arrangement exists
between the ATO and the commercial air transport operator, the operator
proficiency check (OPC) and the ZFTT specific details should be conducted
using the operator's standard operating procedures (SOPs).
(3) All training exercises should be designed
to remain within the training envelope as determined by the ATO (Note: Further
guidance regarding the training envelope can be found in GM1 ORA.ATO.125 point (f)).
(l) Aeroplane without FFS
(1) Flight training conducted solely in an
aeroplane without the use of FSTDs cannot cover the crew resource management
(CRM) and multicrew cockpit (MCC) aspects of MPA flight training, and for
safety reasons cannot cover all emergency and abnormal aircraft operation
required for the training and skill test. In such cases, the ATO should
demonstrate to the competent authority that adequate training in these aspects
can be achieved by other means. For training conducted solely on an MPA where
two pilots are trained together without the use of an FSTD, a minimum of 8
hours of flight training as pilot flying (PF) for each pilot should normally
be required. For training on a single-pilot aeroplane, 10 hours of flight
training should normally be required. It is accepted that for some relatively
simple single or multi-engine aircraft without systems such as pressurisation,
flight management system (FMS) or electronic cockpit displays, this minimum
may be reduced.
(2) Aeroplane training normally involves an
inherent delay in achieving an acceptable flight situation and configuration
for training to be carried out in accordance with the agreed syllabus. These
could include ATC or other traffic delay on the ground prior to take-off, the
necessity to climb to height or transit to suitable training areas and the
unavoidable need to physically reposition the aircraft for subsequent or
repeat manoeuvres or instrument approaches. In such cases it should be ensured
that the training syllabus provides adequate flexibility to enable the minimum
amount of required flight training to be carried out.
(la) Additional UPRT training as per point
FCL.725.A(c) UPRT as per point FCL.725.A(c) should include the elements and
components in table 1.
Table
1: Elements and respective components of upset prevention training
|
Elements and components |
TK instruction |
FSTD/ Aeroplane training |
|
|
A. |
Aerodynamics |
||
|
1. |
General aerodynamic
characteristics |
• |
|
|
2. |
Aeroplane certification
and limitations |
• |
|
|
3. |
Aerodynamics (high and
low altitudes) |
• |
• |
|
4. |
Aeroplane performance
(high and low altitudes) |
• |
• |
|
5. |
AoA and stall awareness |
• |
• |
|
6. |
Stick shaker or other stall-warning
device activation (as applicable) |
• |
• |
|
7. |
Stick pusher (as
applicable) |
• |
• |
|
8. |
Mach effects (if
applicable to the aeroplane type) |
• |
• |
|
9. |
Aeroplane stability |
• |
• |
|
10. |
Control surface
fundamentals |
• |
• |
|
11. |
Use of trims |
• |
• |
|
12. |
Icing and contamination
effects |
• |
• |
|
13. |
Propeller slipstream (as
applicable) |
• |
• |
|
B. |
Causes of and
contributing factors to upsets |
||
|
1. |
Environmental |
• |
|
|
2. |
Pilot-induced |
• |
|
|
3. |
Mechanical (aeroplane
systems) |
• |
|
|
C. |
Safety review of
accidents and incidents relating to aeroplane upsets |
||
|
1. |
Safety review of
accidents and incidents relating to aeroplane upsets |
• |
|
|
D. |
G-load awareness and
management |
||
|
1. |
Positive/negative/increasing/decreasing
G-loads |
• |
• |
|
2. |
Lateral G awareness
(sideslip) |
• |
• |
|
3. |
G-load management |
• |
• |
|
E. |
Energy management |
||
|
1. |
Kinetic energy vs
potential energy vs effect of thrust-drag ratio on the total energy |
• |
• |
|
F. |
Flight path management |
||
|
1. |
Relationship between
pitch, power and performance |
• |
• |
|
2. |
Performance and effects
of differing power plants (if applicable) |
• |
• |
|
3. |
Manual and automation
inputs for guidance and control |
• |
• |
|
4. |
Type-specific
characteristics |
• |
• |
|
5. |
Management of go-arounds
from various stages during the approach |
• |
• |
|
6. |
Automation management |
• |
• |
|
7. |
Proper use of rudder |
• |
• |
|
G. |
Recognition |
||
|
1. |
Type-specific examples
of physiological, visual and instrument clues during developing and
developed upsets |
• |
• |
|
2. |
Pitch/power/roll/yaw |
• |
• |
|
3. |
Effective scanning (effective
monitoring) |
• |
• |
|
4. |
Type-specific stall
protection systems and cues |
• |
• |
|
5. |
Criteria for identifying
stalls and upsets |
• |
• |
|
H. |
System malfunction (including immediate
handling and subsequent operational considerations, as applicable) |
||
|
1. |
Flight control defects |
• |
• |
|
2. |
Engine failure (partial
or full) |
• |
• |
|
3. |
Instrument failures |
• |
• |
|
4. |
Loss of reliable
airspeed (see also point (lb) of this AMC) |
• |
• |
|
5. |
Automation failures |
• |
• |
|
6. |
Fly-by-wire (FBW)
protection degradations |
• |
• |
|
7. |
Stall protection system
failures including icing alerting systems |
• |
• |
(lb) Flight path management (manual or
automatic, as appropriate) during unreliable airspeed indication and other
failures at high altitude in aeroplanes with a maximum cruising altitude above
FL300
The
following training elements should be integrated into type rating training
courses for aeroplanes with a maximum cruising altitude above FL300:
|
Element |
TK
instruction |
FSTD
/ Aeroplane training |
|
Basic flight physics principles concerning flight
at high altitude, with a particular emphasis on the relative proximity of
the critical Mach number and the stall, pitch behaviour, and an
understanding of the reduced stall angle of attack when compared with low
altitude flight. |
• |
• |
|
Interaction of the automation (autopilot, flight
director, auto-throttle/auto-thrust) and the consequences of failures
inducing disconnection of the automation. |
• |
• |
|
Consequences of an unreliable airspeed and other
failures indication at high altitude and the need for the flight crew to
promptly identify the failure and react with appropriate (minimal) control
inputs to keep the aircraft in a safe envelope. |
• |
• |
|
Degradation of FBW flight control laws/modes and
its consequence on aircraft stability and flight envelope protections,
including stall warnings. |
• |
• |
|
Practical training, using appropriate simulators,
on manual handling at high altitude in normal and in non-normal flight
control laws/modes, with particular emphasis on pre-stall buffet, the
reduced stall angle of attack when compared with low altitude flight, and
the effect of pitch inputs on the aircraft trajectory and energy state. |
|
• |
|
The requirement to promptly and accurately apply
the stall recovery procedure, as provided by the aircraft manufacturer, at
the first indication of an impending stall. Differences between
high-altitude and low-altitude stalls must be addressed. |
• |
• |
|
Procedures for taking over and transferring manual
control of the aircraft, especially for FBW aeroplanes with independent
side-sticks. |
• |
• |
|
Task sharing and crew coordination in high
workload/stress conditions with appropriate call-out and acknowledgement to
confirm changes to the aircraft flight control law/mode. |
• |
• |
SKILL
TEST
(m) Upon completion of the flight training, the
pilot will be required to undergo a skill test with an examiner to demonstrate
adequate competency of aircraft operation for issue of the type rating. The
skill test should be separate from the flight training syllabus, and provision
for it cannot be included in the minimum requirements or training hours of the
agreed flight training programme. The skill test may be conducted in an FFS,
the aeroplane or, in exceptional circumstances, a combination of both.
COURSE
COMPLETION CERTIFICATE
(n) The HT, or a nominated representative,
should certify that all training has been carried out before an applicant
undertakes a skill test for the type rating to be included in the pilot’s
licence. If an ATO is unable to provide certain elements of the training that
is required to be carried out on an aircraft the ATO may issue such a
certificate confirming the completion of the ground training or the training
in an FSTD.
[31] Commission Regulation (EC) No 1702/2003 of 24 September 2003 laying down implementing rules for the airworthiness and environmental certification of aircraft and related products, parts and appliances, as well as for the certification of design and production organisations (Part 21) (OJ L 243, 27.9.2003, p. 6). Regulation as last amended by Regulation (EC) No 1194/2009 (OJ L 321, 8.12.2009, p. 5).
EASA aviation regulations mandate comprehensive type rating courses for pilots, blending theoretical knowledge, simulator, and flight training. Courses must address aircraft systems, malfunctions, and emergency procedures. Training should include upset prevention and high-altitude flight. Skill tests validate pilot competency before license endorsement.
* Summary by Aviation.Bot - Always consult the original document for the most accurate information.
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