GM1 to Appendix 9 Training, skill
test and proficiency check for MPL, ATPL, type and class ratings, and
proficiency check for IRs
ED Decision 2019/005/R
TYPE SPECIFIC UPRT AND GO-AROUND TRAINING IN FSTD
(a) General
(1) The
upset recovery training exercises should be mainly manoeuvre-based but may
include some scenario-based training elements. The manoeuvre-based training
enables type rating applicants to apply their handling skills and recovery
strategy whilst leveraging CRM principles to return the aeroplane from an
upset condition to a stabilised flight path.
(2) If
training is conducted in an FSTD, it is important that applicants understand
the limitations of the FSTD in replicating the physiological and psychological
aspects of upset recovery exercises.
Note: In
order to avoid negative training and negative transfer of training, the ATO
should ensure that the selected upset recovery exercises take into consideration
the limitations of the FFS.
(b) Stall event recovery in
FSTD (Appendix 9, Section B(5) exercise 7.2.1; Section B(6) exercise 3.7.1)
(1) It is of
utmost importance that stall event recovery training takes into account the
capabilities of the FFS used. To deliver stall event recovery training, the
FFS should be qualified against the relevant UPRT elements of CS-FSTD Issue 2.
Stall event recovery training should include training up to the stall
(approach-to-stall). Post-stall training may be delivered provided the device
has been qualified against the relevant optional elements of CS-FSTD Issue 2
and the operator demonstrates that negative training or negative transfer of
training is avoided. A ‘stall event’ is defined as an occurrence whereby the
aeroplane experiences one or more conditions associated with an
approach-to-stall or a post stall.
(2) Stall
event recovery training should emphasise the requirement to reduce the AoA
whilst accepting the resulting altitude loss. High-altitude stall event
training should be included so that flight crew experience the aeroplane
control response, the significant altitude loss during the recovery, and the
increased time required to recover. The training should also emphasise the
risk of triggering a secondary stall event during the recovery.
(3) Recovery
from a stall event should always be conducted in accordance with the stall
event recovery procedures of the OEMs.
Note: If an
OEM-approved recovery procedure does not exist, ATOs should develop and train
the aeroplane-specific stall recovery procedure based on the template in Table
1 below. Refer to Revision 3 of the Airplane Upset Prevention and Recovery
Training Aid (AUPRTA) for a detailed explanation and rationale of the stall
event recovery template as recommended by the OEMs.
Table 1: Recommended stall
event recovery template
|
Stall event
recovery template |
||
|
Pilot Flying (PF) Immediately do the following at first indication of a stall (aerodynamic buffeting, reduced roll stability and aileron effectiveness, visual or aural cues and warnings, reduced elevator (pitch) authority, inability to maintain altitude or arrest rate of descent, stick shaker activation (if installed)) during any flight phases except at lift-off. |
Pilot Monitoring (PM) |
|
|
1. |
AUTOPILOT — DISCONNECT (A large out-of-trim condition could be encountered when the autopilot is disconnected) |
MONITOR airspeed and attitude throughout the recovery and ANNOUNCE any continued divergence |
|
2. |
AUTOTHRUST/AUTOTHROTTLE — OFF |
|
|
3. |
(a) NOSE-DOWN PITCH CONTROL apply until stall warning is eliminated (b) NOSE-DOWN PITCH TRIM (as needed) (Reduce the AoA whilst accepting the resulting altitude loss.) |
|
|
4. |
BANK — WINGS LEVEL |
|
|
5. |
THRUST — ADJUST (as needed) (Thrust reduction for aeroplanes with underwing-mounted engines may be needed) |
|
|
6. |
SPEEDBRAKES/SPOILERS — RETRACT |
|
|
7. |
When airspeed is sufficiently increasing — RECOVER to level flight (Avoid the secondary stall due to premature recovery or excessive G-loading) |
|
(c) Nose-high
and nose-low recovery exercises (Appendix 9, Section B(5) exercise 7.2.2; B(6)
exercise 3.7.2)
Nose-high and nose-low recovery exercises should be conducted in
accordance with the strategies recommended by the OEMs contained in Tables 2
and 3 below.
Note: As the
OEM procedures always take precedence over the recommendations, ATOs should
consult the OEM on whether any approved type-specific recovery procedures are
available prior to using the templates.
Refer to Revision 3 of the Airplane Upset Prevention and Recovery Training Aid (AUPRTA) for a detailed explanation and rationale of nose-high and nose-low recovery strategies as recommended by the OEMs.
Table 2: Recommended
nose-high recovery strategy template
|
Nose-high recovery
strategy template |
||
|
Either pilot —
Recognise and confirm the developing situation by announcing ‘nose high’ |
||
|
PF |
PM |
|
|
1. |
AUTOPILOT — DISCONNECT (A large out-of-trim
condition could be encountered when the autopilot is disconnected) |
MONITOR airspeed
and attitude throughout the recovery and ANNOUNCE any continued divergence |
|
2. |
AUTOTHRUST/AUTOTHROTTLE — OFF |
|
|
3. |
APPLY as much nose-down
control input as required to obtain a nose-down pitch rate |
|
|
4. |
THRUST — ADJUST
(if required) (Thrust reduction for
aeroplanes with underwing-mounted engines may be needed) |
|
|
5. |
ROLL — ADJUST
(if required) (Avoid exceeding
60-degree bank) |
|
|
6. |
When airspeed is
sufficiently increasing — RECOVER to level flight (Avoid the secondary
stall due to premature recovery or excessive G-loading) |
|
|
NOTE: (1)
Recovery to level flight may require use of pitch trim. (2)
If necessary, consider reducing thrust in aeroplanes with
underwing-mounted engines to aid in achieving nose-down pitch rate. (3)
WARNING: Excessive use of pitch trim or rudder
may aggravate the upset situation or may result in high structural loads. |
||
Table 3:
Recommended nose-low recovery strategy template
|
Nose-low recovery
strategy template |
||
|
Either pilot —
Recognise and confirm the developing situation by announcing ‘nose low’ (If the autopilot or
autothrust/autothrottle is responding correctly, it may not be appropriate
to decrease the level of automation while assessing if the divergence is
being stopped) |
||
|
PF |
PM |
|
|
1. |
AUTOPILOT — DISCONNECT (A large out-of-trim
condition could be encountered when the autopilot is disconnected) |
MONITOR airspeed
and attitude throughout the recovery and ANNOUNCE any continued divergence |
|
2. |
AUTOTHRUST/AUTOTHROTTLE — OFF |
|
|
3. |
RECOVERY
from stall if required |
|
|
4. |
ROLL
in the shortest direction to wings level (It may be necessary to
reduce the G-loading by applying forward control pressure to improve roll
effectiveness) |
|
|
5. |
THRUST
and DRAG — ADJUST (if required) |
|
|
6. |
RECOVER
to level flight (Avoid the secondary
stall due to premature recovery or excessive G-loading.) |
|
|
NOTE: (1)
Recovery to level flight may require use of pitch trim. (2)
WARNING: Excessive use of pitch trim or rudder
may aggravate the upset situation or may result in high structural loads. |
||
(d) Go-around
with all engines operating from various stages during an instrument approach
(Appendix 9, Section B(5) exercise 7.3; B(6) exercise 4.1.)
(1) The
objective of the go-around exercises is to expose the student pilot to the
physiological effects caused by a go-around. The instructor should ensure that
student pilots understand the objective of the exercises and provide students
with appropriate coping strategies, including TEM. Due consideration
should be given to environmental conditions when evaluating the demonstration
of task proficiency and related criteria.
(2) A
go-around may be commenced at any time during an approach, including before
the aeroplane is in the landing configuration. Historically, most go-around
training has been conducted when the aeroplane is in the landing configuration
prior to commencing the go-around. Students must be prepared to adapt the
go-around manoeuvre if the go-around is commenced prior to the point where the
aeroplane is fully configured for landing. Situation awareness in relation to
flap and gear configuration, aeroplane speed and missed approach altitude is
important.
(3) Unanticipated
go-arounds may startle the students (e.g. unexpected ATC constraints,
automation malfunction, adverse weather, etc.). Students may find themselves
faced with a situation where they have to perform a large number of critical
actions under a high workload (e.g. setting thrust, landing gear retraction,
flight path management). The instructor should explain that there is also a
possibility of disorientation during a go-around because of the somatogravic
effect produced by large longitudinal acceleration felt by the inner-ear as
the aeroplane speed increases. This effect cannot be reproduced in an FSTD.
(4) It is
vital that the correct pitch attitude is selected and maintained, while the
aeroplane is kept in trim as it accelerates (depending on the aeroplane type).
On some aeroplane types with under-slung engines the pitch response with all
engines functioning may be amplified due to the relatively low gross weight
towards the end of a flight and the high thrust available from modern
aeroplane engines. It is particularly important that trim changes are
anticipated on such aeroplanes.
(5) ATOs
should develop scenarios for go-around training containing different take-off
and approach stall situations that also involve surprise and startle effects
and include:
(i) a
go-around from the non-landing configuration;
(ii) a
go-around at low gross weight using maximum go-around thrust;
(iii) a
go-around from the outer marker or equivalent point;
(iv) a
go-around below 500 ft using, as applicable/permitted, reduced go-around
thrust;
(v) a
go-around initiated above the published missed approach altitude; and
(vi) a
normal go-around from the landing configuration using reduced go-around thrust
(if available / type-specific).
(6) Training
should also incorporate topics such as flight path management (manual and
automatic), application of procedures, startle factors, communication,
workload management and situation awareness. The objective of this training is
to highlight:
(i) differences
to procedures when the aircraft is in the non-landing configuration;
(ii) differences
in handling characteristics at low gross weights and high thrust settings;
(iii) the
threat associated with go-arounds close to the published missed approach
altitudes;
(iv) startle
and surprise associated with an unplanned go-around (ATC, blocked runway,
etc.);
(v) the
importance of effective communication between flight crew;
(vi) the
requirement to be aware of the aircraft energy state during a go-around; and
(vii) the
importance of engaging the autopilot or flight director in the correct modes
during a go-around.
(7) Go-around
training should not be limited to addressing the somatogravic effects caused
by a go-around. Training should also cover topics such as flight path
management (manual and automatic), application of procedures, startle factor,
communication, workload management and situation awareness. Flight path
management training should address:
(i) the
handling differences of a lighter than normal aircraft which may differ to
handling experienced during take-off when the aircraft is much heavier;
(ii) the
different reaction of the aeroplane (pitch and vertical speed) comparing a
go-around performed with reduced G/A thrust (if the function is available) and
a go-around performed with full G/A thrust (a different weight).
(8) The
importance of correct selection of TO/GA modes by the PF should also be
emphasised (pushing TO/GA, selected the correct thrust lever detent, etc.)
(9) The
importance of the PM role in the go-around manoeuvre should also be
highlighted. The PM usually has higher workload as they need to reconfigure
the aircraft, engage FMA modes, communicate with ATC and monitor the actions
of the PF. This excessive workload for the PM may lead him or her to
prioritise actions to the detriment of monitoring activities. The phenomenon
of attentional tunnelling may also need to be addressed. This happens when one
pilot, or both, focus exclusively on a problem at the expense of general
monitoring of the flight parameters.
EASA regulations mandate specific upset prevention and recovery training (UPRT) in flight simulation training devices (FSTD), focusing on stall recovery and unusual attitude scenarios. Training emphasizes understanding FSTD limitations, OEM procedures, and avoiding negative training. Go-around training addresses physiological effects, flight path management, and crew coordination during various approach stages.
* Summary by Aviation.Bot - Always consult the original document for the most accurate information.
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