AMC4Β SPA.LVO.100(c)Β Low-visibility operations and
operations with operational credits
ED
Decision 2022/012/R
OPERATIONS
WITH OPERATIONAL CREDITS β HELICOPTER SPECIAL AUTHORISATION CATEGORYΒ I (HELIΒ SAΒ CATΒ I) OPERATIONS
For HELI
SA CAT I operations, the following should apply:
(a)Β Β Β Β HELI SA CAT I operations should only be
conducted to a runway with an approach lighting system. The following visual
aids should be available:
(1)Β Β Β Β standard runway day markings, approach
lights, runway edge lights, threshold lights, and runway end lights;
(2)Β Β Β Β for operations with an RVR below 450Β m,
runway centre line markings.
(b)Β Β Β Β An ILS/MLS that supports a HELI SA CAT I
operation should be an unrestricted facility.
(c)Β Β Β Β Β The helicopter should be:
(1)Β Β Β Β equipped with a 3-axis autopilot capable
of flying the approach to the minima;
(2)Β Β Β Β able to maintain Vy in IMC on a coupled
Type B approach;
(3)Β Β Β Β equipped with a radio altimeter or other
device capable of providing equivalent performance; and
(4)Β Β Β Β equipped with two independent navigation
aids capable of Type B CAT I approaches and certified for CAT I.
(d)Β Β Β Β The DH of a HELI SA CAT I operation should
not be lower than the highest of:
(1)Β Β Β Β the minimum DH specified in the AFM, if
stated;
(2)Β Β Β Β the minimum height to which the PA aid can
be used without the specified visual reference;
(3)Β Β Β Β the applicable OCH for Category A
aeroplanes or the OCH for Category H if available;
(4)Β Β Β Β the DH to which the flight crew is
qualified to operate;
(5)Β Β Β Β 130Β ft on a CAT II landing system;
(6)Β Β Β Β 150Β ft on a CAT I ILS certified to Class
I/C/1 or MLS certified to 100Β ft/E/1; or
(7)Β Β Β Β 200Β ft on other landing systems;
(8)Β Β Β Β 200Β ft unless the autopilot is a
4-axis autopilot with automatic level-off capability.
(e)Β Β Β Β The lowest RVR minima to be used are
specified in TableΒ 11.
TableΒ 11
HELI SA CAT
I operation minima
|
RVR versus approach lighting system |
||||
|
DH (ft) |
Class of light facility |
|||
|
|
FALS |
IALS |
BALS |
NALS |
|
201β250 |
450 |
650 |
750 |
1Β 000 |
|
181β200 |
300 |
450 |
650 |
900 |
|
151β180 |
300 |
350 |
550 |
750 |
|
130β150 |
300 |
300 |
400 |
600 |
(f)Β Β Β Β Β Operations
(1)Β Β Β Β The minimum crew should be two pilots or
one pilot and a technical crew member. The technical crew member should be
seated in the front seat and be allocated no other task than assisting the
pilot, from the initial approach fix (IAF) onwards.
(2)Β Β Β Β On a CATΒ II landing system, the
flight crew should use the radio altimeter or other equivalent device for the
determination of the DH.
(3)Β Β Β Β On a CATΒ I ILS, the flight crew
should use the altimeter for the determination of the DH. The crew should
cross-check the altitude with the radio altimeter or equivalent device,
considering the local geography.
(4)Β Β Β Β The AFCS and radio altimeter should be
serviceable prior to commencing the approach.
(5)Β Β Β Β The approach should be flown in coupled
4-axis mode down to minima or below.
(6)Β Β Β Β The flight crew should promptly initiate a
go-around if any of the following conditions are met below a 1Β 000-ft
height:
(i)Β Β Β Β Β discrepancy in altitude/radio altitude
information;
(ii)Β Β Β Β discrepancy in navigation information;
(iii)Β Β Β Β partial or total failure of an AFCS system
or navigation system;
(iv)Β Β Β Β deviation of ΒΌ scale or more on the
landing system navigation display.
(7)Β Β Β Β The planning minima at the alternate where
a HELI SA CAT I approach is envisaged should be as defined in TableΒ 12.
TableΒ 12
Planning
minima at the alternate with HELI SA CAT I operations
|
Type of approach |
Aerodrome ceiling |
Weather minima |
|
Two or more usable Type B instrument approach
operations*** |
DA/H*
+Β 100Β ft |
RVR**
+Β 300Β m |
|
One usable Type B instrument approach operation |
DA/H
+Β 150Β ft |
RVR
+Β 450Β m |
*Β Β Β Β Β Β Β The
higher of the usable DA/H or MDA/H.
**Β Β Β Β Β The
higher of the usable RVR or VIS.
***Β Β Β Compliance
with CAT.OP.MPA.192(d) should be ensured.
(8)Β Β Β Β Under commercial air transport, if no
other alternate is selected and the weather forecast at destination is not
based on Part-MET of Regulation (EU) 2017/373, the planning minima at the
alternate where a HELI SA CAT I approach is envisaged should be as defined in
TableΒ 13.
TableΒ 13
Planning
minima at the alternate with HELI SA CAT I operations with alternative weather
source at destination
|
Type of approach |
Aerodrome ceiling |
Weather minima |
|
Two or more usable Type B instrument approach
operations *** |
DA/H * +Β 200Β ft |
RVR** +Β 600Β m |
|
One usable Type B instrument approach operation |
DA/H +Β 300Β ft |
RVR +Β 900Β m |
*Β Β Β Β Β Β Β The
higher of the usable DA/H or MDA/H.
**Β Β Β Β Β The
higher of the usable RVR or VIS.
***Β Β Β Compliance
with CAT.OP.MPA.192(d) should be ensured.
(g)Β Β Β Β Crew training and competency
(1)Β Β Β Β Under CAT, NCC and SPO, the aerodrome used
for HELI SA CAT I operations should be considered as a Category C aerodrome
under ORO.FC.105.
(2)Β Β Β Β A crew member should undergo training to
determine the eligibility of a HELI SA CAT I approach as determined under points
(a) to (c), and to determine the applicable minima under points (d) and (e).
(3)Β Β Β Β A crew member should have the relevant
knowledge to implement the operating procedures described in point (f).
(4)Β Β Β Β A crew member that is involved in HELI SA
CAT I operations should undergo initial and recurrent training to proficiency
using a suitable FSTD, including one approach and landing and one go-around
using the lowest minima defined in points (d) and (e).
(5)Β Β Β Β The recurrent training should have a
validity of 6 calendar months. The validity period should be counted from the
end of the month when the check was taken. When the training is undertaken
within the last 3Β months
of the validity period, the new validity period should be counted from the
previous expiry date.
(6)Β Β Β Β In addition to (5), a technical crew
member that is involved in HELI SA CAT I operations should be trained to
perform navigation and monitoring functions under IFR, as described under AMC3Β SPA.NVIS.130(f). The training and checking should
include all of the following on the given helicopter type:
(i)Β Β Β Β Β initial and recurrent general training;
(ii)Β Β Β Β initial and recurrent monitoring training;
(iii)Β Β Β Β initial and recurrent navigation training;
(iv)Β Β Β Β initial and recurrent aircraft/FSTD
training focusing on crew cooperation with the pilot;
(v)Β Β Β Β Β line flying under supervision (LIFUS);
(vi)Β Β Β Β initial and recurrent operator proficiency
checks, which should meet all of the following criteria:
(A)Β Β Β Β the technical crew member should complete
an operator proficiency check to demonstrate competence in carrying out
normal, abnormal and emergency procedures, covering the relevant aspects
associated with the flight operational tasks described in the operations
manual and not covered in the line check;
(B)Β Β Β Β the initial training course should include
an operator proficiency check;
(C)Β Β Β Β the operator proficiency check should be
valid for a given helicopter type. In order to consider an operator
proficiency check to be valid for several helicopter types, the operator
should demonstrate that the types are sufficiently similar from the technical
crew memberβs perspective;
(D)Β Β Β Β the validity period of the operator
proficiency check should be 12Β calendarΒ months.
The validity period should be counted from the end of the month when the check
was performed. When the operator proficiency check is undertaken within the
last 3Β months of
the validity period, the new validity period shall be counted from the
original expiry date;
(E)Β Β Β Β the operator proficiency check should be
conducted by a suitably qualified instructor nominated by the operator to
conduct flight crew operator proficiency checks;
(vii)Β Β Β initial and recurrent line checks, which
should meet all of the following criteria:
(A)Β Β Β Β the line check should be performed on the
helicopter;
(B)Β Β Β Β the technical crew member should
demonstrate competence in carrying out normal operations described in the
operatorβs operations manual;
(C)Β Β Β Β the line check should take place after the
completion of the LIFUS;
(D)Β Β Β Β the validity period of the line check
should be 12Β calendarΒ months. The validity period should
be counted from the end of the month when the check was performed. When the
line check is undertaken within the last 3Β months of the validity period, the new
validity period should be counted from the original expiry date;
(E)Β Β Β Β the line check should be conducted by a
suitably qualified commander nominated by the operator;
(F)Β Β Β Β any task-specific items may be checked by
a suitably qualified technical crew member nominated by the operator and
trained in CRM concepts and the assessment of non-technical skills.
For Helicopter Special Authorization Category I (HELI SA CAT I) operations, specific visual aids, equipment, and autopilot capabilities are required. Decision Height (DH) and Runway Visual Range (RVR) minima are defined based on lighting systems. Crew training, including simulator sessions and proficiency checks, is mandatory for pilots and technical crew members.
* Summary by Aviation.Bot - Always consult the original document for the most accurate information.
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