5.2 Environmental Legislation,
Standards and Guidelines
5.3 Description of the
Environment
5.4 Identification of Noise
Sensitive Receivers
5.5 Construction
Noise Impact Assessment
5.6 Operational Noise Impact
Assessment
5.7 Environmental Monitoring
and Audit
TABLES
Table 5.1 Noise Standards for Daytime
Construction Activities (Non-restricted Hours)
Table 5.2 Helicopter Noise Standards for
Planning Purposes
Table 5.3 Representative
Noise Sensitive Receivers
Table 5.4 Powered Mechanical Equipment for
Construction of the Proposed Helipad
Table 5.5 Predicted Construction Noise Levels
Table 5.6 Predicted
Cumulative Construction Noise
Level
Table 5.7 Emergency
Helicopter Landing at PYNEH (2015 ¡V 2019)
Table 5.8 Noise Data of Airbus H175 ¡V Lateral
Movements
Table 5.9 Noise
Measurement Results of Airbus H175 ¡V Non-lateral Movements
Table 5.10 Minimum
Buffer Distance Required for Airbus H175
Table 5.11 Predicted
Unmitigated Helicopter Noise Levels
Table 5.12 Summary of
Proposed Noise Barrier and Noise Reducers
Table 5.13 Predicted
Mitigated Helicopter Noise Levels
Table 5.14 Statistics of
Helicopter Noise Complaint of TMH and PYNEH
FIGURES
Figure 5.1 Representative
Noise Sensitive Receivers
Figure 5.2 Helicopter
Flight Path
Figure
5.3 Schematic
for Typical Helicopter Operation
Figure 5.4a Noise
Buffer Zone for Flight
Path
Figure 5.4b Noise
Buffer Zone for FATO of
Helipad
Figure
5.5 Proposed
Noise Barrier and Noise Reducers
Figure 5.6a Helicopter
Noise Contour (Non-lateral Movement) at +118.2 mPD
Figure 5.6b Helicopter
Noise Contour (Non-lateral Movement) at +98.2 mPD
Figure 5.6c Helicopter
Noise Contour (Non-lateral Movement) at +38.2 mPD
Figure 5.6d Helicopter
Noise Contour (Non-lateral Movement) at +5.7 mPD
Figure 5.7a Helicopter
Noise Contour (Lateral Movement) at +118.2 mPD
Figure 5.7b Helicopter
Noise Contour (Lateral Movement) at +98.2 mPD
Figure 5.7c Helicopter
Noise Contour (Lateral Movement) at +38.2 mPD
Figure 5.7d Helicopter
Noise Contour (Lateral Movement) at +5.7 mPD
APPENDICES
Appendix
5B Details of Representative Noise Sensitive
Receivers
Appendix
5C Calculation of Construction Noise Levels
Appendix
5D Airbus H175 Noise Certificate
Appendix
5E Helicopter Noise Survey Report
Appendix
5F Calculation of Helicopter Noise Levels
5.1.1.2
During the construction phase, Powered Mechanical
Equipment (PME) to be used for the construction works will be the primary noise
source. The major noise generating
activities will include the Construction of the helipad and associated
structures including covered safety walkway, staircase, noise barrier, etc.
5.1.1.3
During the operational phase, the proposed helipad will only be used for
medical emergencies, such as CASEVACs and Search and Rescue (SAR) by the Government
Flying Service (GFS). The helipad
will not be used for commercial operations, transportation of guests, training
flights or other non-emergency uses, except trial flights. The major noise source due to the Project
in the operational phase will be from helicopter maneuvering as indicated
below:
¡P
Lateral movements of the
helicopter including approach towards and departure from the proposed helipad along
its flight path; and
¡P
Non-lateral movements of
helicopter including landing on and hovering directly over the proposed helipad.
5.1.1.4
The noise impact
assessment for the Project has been conducted in accordance with the Annexes 5
and 13 of the Technical Memorandum on Environmental Impact Assessment Process
(TM-EIAO).
5.2.1
Background
5.2.1.2
Reference to the EIAO and the relevant technical
memoranda has been made for the assessment of noise impacts. Annexes 5 and 13 of the TM-EIAO set out
the criteria and guidelines for evaluating noise impacts. Assessment procedures and standards are
set out in the following technical memoranda and Guidance Note:
¡P
Technical Memorandum on Environmental Impact
Assessment Process (TM-EIAO);
¡P
Technical Memorandum on Noise from Construction Work
other than Percussive Piling (TM-GW);
¡P
Technical Memorandum for the Assessment of Noise
from Places other than Domestic Premises, Public Places or Construction Sites
(IND-TM); and
¡P
EIAO Guidance Note ¡V Preparation of Construction
Noise Impact Assessment under the Environmental Impact Assessment Ordinance
(GN9/2010).
5.2.2
Construction Phase
Construction Noise during Non-restricted Hours
5.2.2.1
Daytime construction noise, excluding percussive
piling, between the hours 0700 ¡V 1900 on weekdays, that is non-restricted hours,
should be assessed in accordance with TM-EIAO. Annex 5 of the TM-EIAO sets out the noise
standards for daytime construction activities, which are Leq(30 min)
75dB(A) for domestic premises and hotels, and Leq(30 min) 70dB(A)
during normal hours for education institutions including kindergartens (65dB(A)
during examination periods), nurseries and all other places where unaided voice
communication is required. Noise standards for daytime construction
activities are summarised in Table 5.1.
Table
5.1 Noise Standards for Daytime
Construction Activities (Non-restricted Hours)
Uses |
Construction Noise, Leq (30 mins), dB(A) |
All domestic premises
including temporary housing accommodation |
75 |
Hotels and hostels |
75 |
Educational institutions including kindergartens,
nurseries and all others where unaided voice communication is required |
70 65
(During examinations) |
Note:
1.
The above standards apply to uses which rely
on opened window for ventilation.
2.
The above standards shall be viewed as the
maximum permissible noise levels assessed at 1m from the external facade.
Helicopter Noise (Daytime Period)
Table 5.2 Helicopter Noise
Standards for Planning Purposes
Common Uses |
Helicopter Noise, Lmax, dB(A) |
All domestic premises
including temporary housing accommodation |
85 |
Hotel and hostels |
85 |
Offices |
90 |
Educational institutions including kindergartens,
nurseries and all others where unaided voice communication is required |
85 |
Places of public worship and courts of law |
85 |
Hospitals, clinics, convalescences and homes for
the aged, diagnostic rooms, wards |
85 |
Note:
1.
The above standards apply to uses which rely
on opened window for ventilation.
2.
The above standards should be viewed as the
maximum permissible noise levels assessed at 1m from the external facade.
Helicopter Noise (Evening and Night-time Period)
5.2.3.2 In accordance with the TM-EIAO, there are no specific noise standards
for helicopter noise during the evening (1900-2300) and night-time (2300-0700) periods
between the hours of 1900 and 0700 on the next day.
5.2.3.3 Criteria for evaluating such helicopter noise impacts shall be established
on a case-by-case basis so as to assess whether the proposed methodology are
consistent with the methodologies adopted for Hong Kong projects having similar
issues or with methodologies accepted by recognised national / international
organisations.
5.2.3.4 Therefore, considering the nature of this Project, reference has been
made to the approved EIA report for ¡§A Rooftop Helipad at the Proposed New
Block of Queen Mary Hospital¡¨ (Register No. AEIAR-208/2017) (QMH Helipad EIA). The QMH Helipad EIA, which was approved
in March 2017, is considered as the latest and the most relevant EIA in similar
nature for reference. The proposed rooftop
helipad at Queen Mary Hospital is considered to be comparable to this Project
as both are rooftop helipads on a trauma hospital proposed for emergency
helicopter operations only.
5.2.3.5 A review of the local and overseas/ international practices was conducted
and presented in the QMH Helipad EIA to investigate suitable assessment
approaches for the noise impact arising from emergency helicopter operations
during the evening and night-time periods.
Practices in overseas regions where the urban settings are similar to
Hong Kong where made reference to, including the United States of America (California),
Australia (Victoria), Japan and Singapore. According to the findings in the QMH
Helipad EIA, there is no statutory noise criterion for emergency services, including
air ambulance, SAR, supporting law enforcement agencies, firefighting etc., during
the evening and night-time periods with such emergency services being generally
exempted from the flight restrictions.
Noise criteria were not proposed for emergency helicopter operation
during evening and night-time periods based on the similar situation to these
reviewed cities/countries. These
review findings have been checked and considered valid as summarized in Appendix
5A.
5.2.3.6 The use of this proposed helipad during evening and night-time period
has similar situations to those reviewed cities/countries, and the QMH Helipad.
Therefore, in view of emergency
nature and without scheduled flight, noise criteria were not proposed for
emergency helicopter operation during evening and night-time period for the
Project.
5.3.1.1
As described in Section 2.2, there are three sites earmarked for hospital development
in the former south apron area of Kai Tak Development Area (KTDA), which are
Site 3C1(A), Site 3C1(B) and Site 3C1(C) (hereinafter described as ¡§Sites A, B
and C¡¨ respectively). Site A and
Site B have been allocated for development of the NAH, while Site C is occupied
by the Hong Kong Children¡¦s Hospital (HKCH), which commenced operation in
2018. Site A abuts Kwun Tong Bypass,
Cheung Yip Street and Shing Cheong Road, while Site B abuts the planned Roads
L10, L18 and D4. The construction
works for the foundations for the proposed NAH in both Site A and Site B commenced
in 2018. The Acute Block of NAH
will be located at the south-east part of Site A, and the Project site for the
helipad is proposed to be located on the roof of the Acute Block. The location of the Project site
is shown in Figure 1.1. The land use of the Project Site and its
environs are shown in Figure 2.1.
5.3.1.2 Adjacent to the eastern corner of Site A at Cheung Yip Street, there is
the existing Kai Tak Fire Station.
Two sites for Transport Department vehicle examination centres are
located beyond the Kwun Tong Bypass, which are to the north of Site A.
5.3.1.3 To the south-east of Site A, and opposite to the Acute Block, a planned
residential zone is located with a separation distance of approximately
50m. The planned residential zone
is zoned ¡§Residential (Group B)¡¨ (¡§R(B)2¡¨) according to the approved Kai Tak OZP
No. S/K22/6. This R(B)2 zone consists of two
adjacent sites, one located next to waterfront area, which has a building
height restriction of +80mPD and is currently the Public Works Central
Laboratory Building, while the other one at Lam Chak Street has a building
height restriction of +100mPD and is currently the Kowloon Bay Parking site.
5.3.1.4 Further to the east of Site A, two areas zoned ¡§Commercial (2)¡¨ are
found along both sides of Kai Hing Road. The existing Pacific Trade Centre
bounded by Lam Chak Street and Cheung Yip Street is located at about 50m from
Site A while the existing Kowloon Godown, Kerry Dangerous Goods Warehouse
(Kowloon Bay) and open storage are located at about 140m from Site A. Planning status of the Kerry Dangerous
Goods Warehouse (Kowloon Bay) site is detailed in Section 5.4.1.5.
5.3.1.5 In the ex-Kai Tak Runway in KTDA, there are planned residential zones,
currently zoned ¡§Residential (Group B)¡¨ (¡§R(B)4), ¡§R(B)5¡¨ and ¡§R(B)7¡¨) and with
building height restrictions ranging from +95mPD to +120mPD, are found. These zones are located along Shing Fung
Road (i.e. Road D3A) across the Kai Tak Approach Channel. The nearest
residential zone is about 450m to the southwest of the Project site.
5.3.1.6 Site visits were conducted in August 2019. Based on the site observation, the
existing noise environment in the vicinity of the proposed helipad was
dominated by the construction activities in Site A and Site B of NAH and traffic
noise from the nearby Kwun Tong Bypass.
5.4.1.1 Noise Sensitive Receivers (NSRs) have been identified. Relevant Outline Zoning Plans (OZP)
(i.e. Approved Kai Tak OZP No. S/K22/6, Draft Ngau Tau Kok and Kowloon Bay OZP
No. S/K13/29 and Approved Kwun Tong (South) OZP No. S/K14S/22), development
applications approved by the Town Planning Board (TPB), survey maps,
topographic maps and aerial photos etc., have been referenced in identifying
the existing and planned NSRs. Site
surveys have been carried out to confirm the status of existing representative
NSRs. Noise sensitive uses relying
on opened windows for ventilation have been selected.
5.4.1.2 In accordance with the EIA Study Brief No. ESB-311/2019, the assessment
area for noise impact assessment shall generally include areas within 300m from
the boundary of the Project site.
The assessment area shall be expanded to include NSRs at a distance over
300m from the Project, associated works and along the flight paths of the
helicopter where appropriate, if those NSRs could be affected by the
construction and operation of the Project.
NSRs which are potentially affected by the helicopter operations, but
located over 300m from the Project, are also included in the assessment.
5.4.1.3 It is noted that the Acute Block and other four blocks of the NAH will
be provided with central air-conditioning system and well-gasketted windows and
do not rely on opened window for ventilation, which are similar to the existing
HKCH. Therefore, the NAH and HKCH would not be considered in the noise impact assessment. It is also confirmed that no noise
sensitive uses which rely on opened windows for ventilation is inside the Kai
Tak Fire Station. Therefore, the
Kai Tak Fire Station would not be considered in the noise impact
assessment. Relevant advice form FSD
is shown in Appendix
5H-4.
5.4.1.4 In accordance with TPB Paper No. 10236, the earliest design year for
those proposed residential developments on Kai Tak Development (KTD) Sites 3E1,
3E2, 4E1, 4A1, 4B1, 4B2, 4B3 and 4B4 is 2026, which is later than year 2024,
the completion year of the construction works of this Project as advised by the
Project team. It is noted that some
of these sites in the ex-Kai Tak Runway have been sold according to land sale
records, such as Sites 4A1, 4B1, 4B2, 4B3, 4B4, etc., however, they are all
located over 300m from the Project. Hence, it is anticipated that these
planned residential sites will not be affected by any potential construction
noise during the entire construction period (i.e. Q4 2023 to Q4 2024) of the
Project.
5.4.1.5 According to the Section 16 planning application Case No. A/K22/13-1
approved under the Town Planning Ordinance, permission for residential
developments proposed on 7 Kai Hing Road (NKIL 5813) has been granted and valid
until 30 March 2020.
Therefore, the permission is considered as expired. Nonetheless, according to
the Section 16 planning application Case No. A/K22/27, a proposed redevelopment
on the site to a commercial building has been applied for, and is under review
at the time of preparation of this EIA report. Although NKIL 5813 is a commercial zone
currently occupied by the Kerry Dangerous Goods Warehouse
(Kowloon Bay), and the information or population intake
programme for the proposed residential development is not available at
the time of preparing this EIA report, it would be considered as a
representative planned NSR for conservative assessment in both construction and
operational phases.
5.4.1.6 No existing NSR would be affected within the 300m study area. However, the nearest existing NSR,
namely the Construction Industry Council Kowloon Bay Training Centre (CIC
Kowloon Bay), which would likely be affected, is located approximately 461m
from the Project site and has been included in the operational helicopter noise
impact assessment.
5.4.1.7 Descriptions and locations of the identified representative NSRs are
summarised in Table 5.3 and
indicated in Figure 5.1. The height information assumed for the
NSRs and photos of the existing NSR are shown in Appendix
5B.
Table 5.3 Representative
Noise Sensitive Receivers
NSR ID |
Description |
Zoning |
Noise Sensitive Use |
Distance from Project (m) |
CNIA(1) |
HNIA(2) |
Existing NSR |
||||||
E01 |
Construction Industry
Council Kowloon Bay Training Centre (CIC Kowloon Bay) |
Government,
Institution or Community |
Education
Institution |
465 |
- |
Yes |
Planned NSRs |
||||||
P01a |
Kai Tak Development Site
3E1 (KTD Site 3E1) |
Residential
(Group B) |
Domestic
Premises |
154 |
- |
Yes |
P01b |
155 |
- |
Yes |
|||
P01c |
164 |
- |
Yes |
|||
P02a |
Kai Tak Development Site
3E2 (KTD Site 3E2) |
Residential
(Group B) |
Domestic
Premises |
163 |
- |
Yes |
P02b |
214 |
- |
Yes |
|||
P03 |
Proposed Residential
Development at Kerry Dangerous Goods Warehouse (Kowloon Bay)
(NKIL 5813) |
Commercial |
Domestic
Premises |
249 |
Yes |
Yes |
P04 |
Kai Tak Development Site
4E1 (KTD Site 4E1) |
Residential
(Group B) |
Domestic
Premises |
633 |
- |
Yes |
P05 |
Kai Tak Development Site
4A1 (KTD Site 4A1) |
Residential
(Group B) |
Domestic
Premises |
442 |
- |
Yes |
P06 |
Kai Tak Development Site
4B1 (KTD Site 4B1) |
Residential
(Group B) |
Domestic
Premises |
402 |
- |
Yes |
P07 |
Kai Tak Development Site
4B2 (KTD Site 4B2) |
Residential
(Group B) |
Domestic
Premises |
401 |
- |
Yes |
P08 |
Kai Tak Development Site
4B3 (KTD Site 4B3) |
Residential
(Group B) |
Domestic
Premises |
420 |
- |
Yes |
P09 |
Kai Tak Development Site
4B4 (KTD Site 4B4) |
Residential
(Group B) |
Domestic
Premises |
497 |
- |
Yes |
Note:
(1). CNIA ¡V
Construction Noise Impact Assessment
(2). HNIA ¡V Helicopter Noise Impact Assessment
5.5.1
Identification of Noise Impact
5.5.1.1 As mentioned in Section 2,
the Project will be constructed after the completion of superstructure work for
the Acute Block of the New Acute Hospital (NAH). The proposed helipad will be built on
the rooftop of the newly constructed Acute Block of the NAH and, therefore, demolition
works, site formation and superstructure works are not required for the
Project. The potential construction
noise source will be from the PME to be used during construction activities for
the steel framework, helipad structure, safety walkway, access ramp and noise
barrier.
5.5.2
Assessment Methodology
5.5.2.1 The assessment of noise impacts from the construction (excluding
percussive piling) of the Project has been based on the methodology given in
Annex 13 of the TM-EIAO. The
typical approach is summarised as follows:
¡P
Formulate construction programme and work sequences;
¡P
Identify representative NSR that may be affected by
the construction of the Project;
¡P
Establish the construction plant inventory;
¡P
Assign Sound Power Level (SWL) for each piece of
PME based on the TM-GW and the list of Sound power level of other commonly used
PME;
¡P
Calculate the correction factors based on the
distance between the NSR and the notional noise source positions at different
works areas;
¡P
Apply noise corrections in the calculations for
distance, operation time, screening and façade correction, if any;
¡P
Predict the construction noise levels at NSR and
compare against the noise standards (Table
5.1); and
¡P
Determine mitigation measures, as necessary, and
assess any residual impacts.
5.5.2.2 The predicted construction noise level (CNL) at the NSR is calculated
based on the equation defined below:
CNL
= SWLTotal +CD +Cs +CT +CF
Where,
SWLTotal - Total sound power level, dB(A);
CD - Distance correction, dB(A);
CB - Screening correction, dB(A);
CT - Percentage on time correction, dB(A)
CF - Façade correction, dB(A).
5.5.3
Noise Emission Inventory
5.5.3.1 The construction works of the helipad and the associated structures will
be constructed after the completion of superstructure work for the Acute Block
of NAH. The construction works of
the helipad and the associated structures will be conducted in one phase for
worst-case assessment. The construction programme, construction plant inventory and percentage
on time of each piece of PME have been provided and confirmed reasonable,
feasible and practicable by the Engineer/ HA based on the best available
information at the moment, including the proposed construction method as
presented in Section 2.5. The inventory will be subject to change
by the Contractor in future. The
construction schedule provided by the Engineer has been prepared based upon an
assumption that all works will be undertaken during non-restricted hours
only. As refer to the
implementation programme of the Project in Section
2.6, the construction will be tentatively commenced in Q4 2023, and
completed in Q4 2024. The PME to be
used for the helipad construction and their SWLs are listed in Table 5.4 and Appendix 5C.
Table 5.4 Powered
Mechanical Equipment for Construction of the Proposed Helipad
PME Adopted |
ID code in TM-GW |
SWL, dB(A) |
No. of PME |
Air Compressor, air flow < 10m3/min |
CNP 001 |
100 |
1 |
Crane, tower (electric) |
CNP 049 |
95 |
1 |
Breaker, hand-held, mass > 35kg |
CNP 026 |
114 |
1 |
Welding Set |
Note (1) |
78 |
2 |
Note:
(1). SWL of Welding Plant was referenced from
the approved EIA Report of West Kowloon Cultural District (Register No.
AEIAR-178/2013).
5.5.4
Prediction and Evaluation of Construction Noise Impact
5.5.4.1 The construction noise impact assessment has been conducted based on the
construction plant inventory for the helipad construction.
5.5.4.2 All pieces of the PME for general construction works have been assumed
to be placed at a single notional source at a position mid-way between the
approximate geographical centre of the construction site and the boundary
nearest to the NSR. This position is referred to as the notional source
position according to the TM-GW. However, considering the size of helipad, with
a diameter of 30m, is relatively small when compared to general construction
sites, the notional source position will be assumed as the point of the helipad
nearest to the NSR for conservative assessment. A 3dB(A) has been added to the predicted
noise levels as a façade correction.
5.5.4.3 The maximum predicted noise level at the NSR during construction phase
is summarized in Table 5.5. Detailed calculation is given in Appendix 5C.
5.5.4.4 According to the assessment result in Table 5.5, the predicted maximum construction noise levels at the
NSR would not exceed the noise criterion of 75dB(A).
Table 5.5 Predicted Construction Noise Level
NSR ID |
NSR |
CNL (Leq(30
mins)), dB(A) |
Assessment
Criterion, dB(A) |
P03 |
Proposed
Residential Development at Kerry Dangerous Goods Warehouse (Kowloon Bay)
(NKIL 5813) |
61 |
75 |
5.5.4.5 In addition, the structural works for the proposed helipad would take
approximately one year only.
5.5.4.6 Considering the above, no adverse construction noise impacts are anticipated.
5.5.5
Cumulative Impacts with Concurrent Project
Concurrent Projects
5.5.5.1 Key concurrent projects in the vicinity of the proposed helipad are
identified in Section 2.7. Those projects that would have potential
construction works undertaken concurrently with the helipad construction (i.e.
2023 to 2024) are detailed below. The
construction activities of the projects taking place concurrently within 300m
of a given NSR would be considered to contribute to the cumulative impacts at
those NSRs.
New Acute Hospital at Kai Tak Development by Hospital Authority
5.5.5.2 The proposed helipad will be constructed after the completion of
superstructure for the NAH. However,
there will be concurrent construction of the proposed helipad and the finishing
works for both Site A and Site B of NAH between 2023 and 2024. The type, operation time and quantities
of the PME likely to be used for the finishing works of the NAH and their SWLs
are presented in Appendix 5C. The construction programme
and construction plant inventory adopted for the assessment is confirmed and
provided by the Project Engineer who is responsible for the design of
construction works of NAH.
Central Kowloon Route - Slip Road S5 by HyD
5.5.5.3 The construction of the Slip Road S5 project will tentatively commence
in 2023 and be completed in 2024. The
300m boundary of the project does not cover the NSR P03. Therefore, the potential cumulative noise
impact arising from the construction of Slip Road S5 has not been included in
this noise assessment.
Kai Tak Development - Trunk Road T2 and Infrastructure at South Apron by
CEDD
5.5.5.4 According to the approved EIA report for the Trunk Road T2 (Register No.
AEIAR-174/2013), the Trunk Road T2 is planned to be a dual 2-lane highway of
about 3.0 km connecting the Central Kowloon Route (CKR) and Tseung Kwan O ¡V Lam
Tin Tunnel (TKO-LTT). Construction
of the Trunk Road T2 will commence in 2020, and it is targeted to be completed
in 2026. Hence, there will be
concurrent construction with the proposed helipad. In addition, it is noted that NSR P03 is located within the
300m assessment area of the Trunk Road T2 project. Therefore,
Trunk Road T2 has been identified as a concurrent project which may contribute
potential cumulative impacts at NSR P03.
With reference to the approved EIA report for Trunk Road T2 (Register
No. AEIAR-174/2013), the maximum predicted mitigated construction noise level
at NSR P03, referred to as NSR KER1 in AEIAR-174/2013, is 75dB(A).
Kai Tak Development ¡V Remaining infrastructure works for Developments at
the Former Runway and South Apron, Road L10 & 18 by CEDD
5.5.5.5 The construction of the Road L10 & 18 project was commenced in 2019
and will be tentatively completed in 2026.
However, this project is located more than 300 from the NSR P03. Therefore, the potential cumulative
noise impact arising from the construction of Road L10 & 18 has not been
included in this noise assessment.
Cumulative Impacts
5.5.5.6 The cumulative noise impacts at the NSR have been assessed and
summarised in Table 5.6. Detailed
calculation is given in Appendix 5C.
Table 5.6 Predicted
Cumulative Construction Noise Level
Concurrent Projects |
CNL (Leq(30
mins)), dB(A) |
Cumulative CNL (Leq(30
mins)), dB(A) |
Assessment Criterion, dB(A) |
The Project |
61 |
75 |
75 |
Site A of NAH |
58 |
||
Site B of NAH |
46 |
||
Trunk Road T2 |
75 |
5.5.5.7 The predicted cumulative construction noise level at the representative
NSR, the proposed Residential
Development at Kerry Dangerous Goods Warehouse (Kowloon
Bay), does not
exceed the noise criterion of 75dB(A).
Hence, adverse cumulative construction noise impacts are not
anticipated.
5.5.6
Mitigation of Construction Noise Impact
5.5.6.1 The assessment results show that there would be no adverse noise impact
at the identified NSR and no mitigation measures would be required. However, good site practices and use of
quieter construction plant are still recommended to minimise the noise impact
during the construction of the proposed helipad. The following site practices are
recommended:
¡P
Quiet powered mechanical
equipment (QPME) shall be used, and PME shall also be serviced regularly during
the construction programme;
¡P
Only well maintained
plants shall be used in the construction of the Project; and
¡P
Machines and plant that
may be in intermittent use should be shut down between works periods or
throttled down to a minimum between work periods.
5.5.6.2 Besides, the ¡§Recommended Pollution Control Clauses for Construction
Contracts¡¨ published by the EPD should be adopted in the Contract Specification
for the Contractors to follow and implement relevant measures and good site
practices in minimising noise impact.
5.5.7
Residual Impacts
5.5.7.1 Cumulative construction noise impacts on the representative NSR are
assessed and comply with the daytime construction noise standard. No adverse residual impact is
anticipated during the construction phase of the Project.
5.6.1
Identification of Potential Noise Impacts
Background
5.6.1.1 During the operational phase, the key noise issue would be from the helicopter
operations associated with the proposed Helipad. There are no other noise sources
associated with the Project in the operational phase. Other potential noise sources proposed
for the NAH, such as outdoor building services equipment, shall be assessed
under a separate environmental study and designed to fulfill the relevant environmental
requirements.
Helicopter Operational Mode
5.6.1.2 Noise will be generated by helicopters during manoeuvring over the
helipad within the Final Approach and Take-Off (FATO) area, lateral (approaching
/ departure) flight movements and flyover. The different operational modes that may generate noise are summarised
as follows:
Non-lateral Movements
¡P
Hovering: Helicopter
turns on the spot over the helipad to achieve the desirable orientation for
touchdown / lift-off;
¡P
Touchdown: Helicopter
descends on the helipad surface;
¡P
Idling: Helicopter
remains on the helipad surface with its rotary blades kept running; and
¡P
Lift-off: Helicopter
ascends vertically from the helipad surface to achieve a hover before departure.
Lateral Movements
¡P
Approach: Helicopter
approaches the helipad while it is descending at an angle to the helipad
surface;
¡P
Take-off: Helicopter
leaves the helipad while it is climbing up at an angle to the helipad surface;
and
¡P
Flyover: Helicopter
cruises before approach or after take-off.
Flight Sectors
5.6.1.3 The selection of flight sectors for the helicopter flights to and from
the proposed helipad has been based on the following considerations. The
flight sectors in the north-west and south-east, and south have been recommended
by the GFS for the proposed helipad. The extent of the flight sectors and the
locations of the representative NSRs are presented in Figure 5.2. The GFS has emphasised
that the proposed flight sectors are the best compromise with all factors and
have been kept to a minimum in size so as to minimise the potential for noise
impact on the surroundings. The
flight paths to and from the proposed helipad have been carefully defined for
helicopters to fly over the Kai Tak Approach Channel or Kwun Tong Typhoon
Shelter and away from densely populated areas such as the ex-Kai Tak Runway to
the south-west, Kowloon Bay to the north and Kwun Tong to the east. Meanwhile, a minimum horizontal buffer
distance of 116m from NSRs could be maintained by the chosen flight paths as
illustrated in Figure 5.4a (Refer
to Section 5.6.4.1). Relevant
advice from GFS is given in Appendix 5H-2. As advised by the GFS, the chosen flight paths during the operation of
the helipad may be altered slightly subject to the actual weather conditions
and the obstacles clearance to the surroundings, such as movement of birds or
unexpected localised turbulence. Furthermore,
subject to flight condition, helicopter operations are expected to be in one-way-direction within the selected
flight sectors, that is, the arrival flight and departure flight shall be from
east to west or east to south-west and vice versa. Using the same flight path for
approaching and departure of each operation is not preferred to minimise the
overall exposure from helicopter noise at the NSRs.
Flight Profile
5.6.1.4 Based on details from the GFS, in preparing for departure, the
helicopter will descend with a gentle slope until it reaches a flight height of
300ft above the helipad. Within
300ft above the helipad, the flight path shall be projected at a gradient of 8%
(about 4.6 degrees) for both approaching and departure. The schematic for typical helicopter
operation is illustrated in Figure 5.3. Relevant advice from GFS
is given in Appendix 5H-3. The summary of the typical
flight profiles is as follows:
1. Cruise / Flyover: Typical flight height of 1500ft above mean sea level
with flight speed of 140kts, descending 500ft/min with flight speed of 100kts
until 300ft above the helipad;
2. Approach: From 300ft above the helipad, flight speed would reduce from
60kts to 0kts with an approach angle of 4.6 degrees within 60 seconds;
3. Hovering (Approach): The desirable orientation for touchdown would be
achieved within 5 seconds at around 2.5m above the helipad;
4. Touchdown: Descends on to the helipad within 3 seconds;
5. Idling: 5 minutes for casualty handover under normal circumstances;
6. Lift-off: Ascends from helipad to achieve a hover before departure
within 3 seconds;
7. Hovering (Departure): Achieve desirable orientation for take-off within
5 seconds, at around 2.5m above helipad;
8. Take-off: Flight speed increases from 0kts to 60kts with a departure
angle of 4.6 degrees within 60 seconds up to 300ft above the helipad; and
9. Cruise / Flyover: Ascends at 500ft/min with a flight speed of 100kts
until achieve a typical flight height of 1500ft above mean sea level, at
typical flight height, the flight speed increases to 140kts.
Flight Frequency
5.6.1.5 As mentioned in Section 5.1.1.3,
the proposed helipad at the NAH will be solely used for emergency use and not
for scheduled helicopter operations except trial flights. Table
5.7 presents the record of the GFS¡¦s emergency helicopter operations at the
PYNEH, the current most utilised hospital helipad, between 2015 and 2019. Relevant advice from GFS is given in Appendix 5H-3.
Table 5.7 Emergency Helicopter Landing at PYNEH
(2015 ¡V 2019)
PYNEH Helipad |
2015 |
2016 |
2017 |
2018 |
2019 |
||||||||||
D |
E |
N |
D |
E |
N |
D |
E |
N |
D |
E |
N |
D |
E |
N |
|
No. of flight |
152 |
17 |
32 |
153 |
31 |
31 |
218 |
32 |
45 |
164 |
35 |
42 |
175 |
33 |
42 |
Average no. of day(s) per
flight |
2.4 |
21.5 |
11.4 |
2.4 |
11.8 |
11.8 |
1.7 |
11.4 |
8.1 |
2.2 |
10.4 |
8.7 |
2.1 |
11.1 |
8.7 |
Total in the year: |
201 |
215 |
295 |
241 |
250 |
Source:
1. Data are advised by Government Flying Service
Note:
1. D ¡V Daytime (07:00 ¡V 19:00); E ¡V Evening Time
(19:00 ¡V 23:00); N ¡V Night-time (23:00 ¡V 07:00).
2. All emergency flights including all type CASEVACs and
SAR are presented as reference for the assessment.
5.6.1.6 According to Table 5.7, the
highest annual emergency helicopter landing at PYNEH was found in 2017. The flight records reflected that the
average number of daily emergency helicopter landing was less than one, with emergency
helicopter landings in the daytime period being about once every one to two days
on average. Also, the evening and
night-time emergency helicopter landings at the PYNEH were one flight about more
than every ten days and eight days respectively on average.
5.6.1.7 The proposed helipad at the NAH, together with the planned helipad at
QMH upon its completion, shall share the existing number of helicopter landings
and, thus, the flight frequency at the PYNEH would be reduced in future. Also, since the existing flight
frequency at PYNEH shall be shared by the proposed helipad at NAH, it is
expected that the flight frequency at NAH would not be higher than the existing
flight frequency at the PYNEH conservatively.
5.6.1.8 In preparation for the provision of 24-hour emergency services, trial
flights will be conducted by the GFS at least two months (or earlier if the
helipad facilities are available) prior to the commissioning of the proposed
helipad for the NAH operations. Around
2- 3 trial flights will be arranged per week during the daytime and evening
time. The purpose of the trial
flights is to confirm the flight perimeters of the flight sectors and for the
GFS¡¦s aircrew to familiarise themselves with the operational procedures and
operating environment. Before the
helipad commissioning, the GFS will conduct trial flights mainly during the daytime
to begin with, followed by some evening trials between 19:00 to 23:00. It is noted that the GFS will minimise
the evening trials and will not conduct trial flights during the night-time between
23:00 to 07:00 of the next day to reduce the possible noise impacts to the
surroundings. When the helipad is
fully operational, trial flights will only be arranged on a need basis, that is
for pilots away from office during the familiarisation phase, for new GFS
pilots or if some major new developments are implemented in the vicinity of the
proposed helipad that may cause concerns to flight safety.
5.6.2
Assessment Methodology
5.6.2.1 According to Table 1A, Annex 5 of the TM-EIAO, helicopter noise impacts at
an NSR shall be assessed in terms of A-weighted maximum sound pressure level Lmax.
The helicopter noise level (Lmax)
at an NSR can be calculated using the following formula:
Lmax
= Lmax(ref) + CD +CB +CF
Where,
Lmax ¡V Helicopter noise level at 1m from the external façade
of NSR, dB(A);
Lmax (ref) ¡V Sound Pressure Level at reference distance,
dB(A);
CD ¡V Distance correction, dB(A);
CB ¡V Barrier correction, dB(A);
CF ¡V Façade correction, dB(A).
5.6.2.2
Since all the identified NSRs are located at some distance,
over 150m, from the FATO of the proposed helipad and the helicopter flight paths,
the helicopter can be considered as a ¡¥point¡¦ source for noise assessment. Therefore, the sound pressure level at
NSRs has been evaluated based on standard acoustic principles of a ¡¥point¡¦
source, that is,the sound pressure received at NSRs will be inversely
proportional to the square of the distance between the noise source and the
NSR. The distance correction CD can be calculated using the following formula:
CD = ¡V20log10(R / R(ref))
Where,
R ¡V Shortest distance from a noise source to NSR, m;
R(ref) ¡V Reference distance from a noise source to a measurement point,
m.
5.6.2.3 A barrier correction of ¡V5dB(A) has been applied where the
representative NSRs are screened with no direct line of sight by a substantial
barrier. A façade correction of
+3dB(A) has, also, been assumed at the representative NSRs in order to account
for the reflection effect due to building façades.
5.6.2.4 Wind speed and direction can influence sound propagation especially over
long distances. However, the wind
speed and wind direction are unpredictable as they are not steady and can vary
from time to time. As detailed in Sections 5.6.1.4 and 5.6.1.6, the
emergency helicopter operations are expected to be less than once a day on
average and the duration of different operational modes range from 2-3 seconds
to 5 minutes. According to the QMH
Helipad EIA, the co-existence of wind, which will enhance the sound perceived,
that is, wind bending down after blowing above a ridge line, and the GFS¡¦s
helicopter operations should be rare.
The ¡§Transportation Noise Reference Book¡¨ (P. M. Nelson, 1987, England:
Butterworths) mentions that the prediction of aircraft noise traditionally and
consciously avoids the wind effect by stating noise levels for a ¡§still air¡¨
situation. Reference to overseas
practices, including Japan and Australia, have been made in the QMH Helipad EIA
and states that helicopter noise standards and assessments do not take account of
the effects of wind. In addition, according
to the practices detailed in the Technical Memorandum for the Assessment of
Noise from Places other than Domestic Premises, Public Places or Construction
Sites (IND-TM) issued under the NCO, noise measurements should not be carried
out at a time and location which is affected by wind as it would generate
noise/affect the measurement results.
Therefore, it is considered inappropriate to include the wind effect in
the helicopter noise impact assessment for the reasonable worst case scenarios
and the adoption of the correction for wind effect is not considered in the assessment.
5.6.3
Helicopter Noise Levels
5.6.3.1 As mentioned in Section 2.2.3.1,
the three Super Puma AS332 L2 helicopters and four Dauphin EC155 B1 helicopters
previously utilised for emergency evacuations have been replaced by seven
medium-sized single-model helicopters Airbus H175 by the GFS, and these Airbus
H175 helicopters will be used at the new helipad at the NAH. Also, the three Super Puma AS332 L2
helicopters were entered into retirement starting from 7th April
2020. Relevant confirmation from
GFS is given in Appendix 5H-1.
5.6.3.2 The new Airbus H175 helicopters will be equipped with more advanced
engines resulting in quieter flight noise compared with the Super Puma AS332 L2
and Dauphin EC155 B1. The Airbus
H175 will comply with the latest standards on noise for helicopters as
stipulated by the International Civil Aviation Organization (ICAO). The ICAO has stipulated noise standards
for lateral movements of helicopters, including approach, take-off and
flyover. The maximum Effective
Perceived Noise Levels (EPNLs) for helicopters¡¦ lateral movements operating at full
load conditions is used as the noise certification standard adopted by the ICAO
Council. The relevant noise
certificate for the Airbus H175 with advice from GFS are presented in Appendix 5D and the EPNLs data are summarised in Table 5.8.
Table 5.8 Noise
Data of Airbus H175 ¡V Lateral Movements
Operation Mode |
Reference Distance, m |
Noise Level |
|
EPNL, EPNdB [1] |
Lmax, dB(A) [2] |
||
Approach |
120 |
95.1 |
82.1 |
Take-off |
150 |
89.8 |
76.8 |
Flyover |
150 |
91.0 |
78.0 |
Note:
1. The EPNLs are determined under conditions prescribed in Chapter 8 and
Appendix 4 of Annex 16 of ICAO, and prescribed in 14 CFR 36 Appendix.
2. Lmax = ENPL ¡V 13 dB(A) with reference to the ¡§Transportation
Noise Reference Book¡¨ (P. M. Nelson, 1987, England: Butterworths).
5.6.3.3 However, the noise data for non-lateral movements are not available in
the Noise Certificate for the Airbus H175.
In order to obtain representative noise data for non-lateral movements of
the Airbus H175 for assessment purposes, a helicopter noise survey was carried
out on 22 May 2019 at Lo Wu Shooting Range. The detailed helicopter noise survey
report is presented in Appendix 5E, and the measurement results are summarised in Table 5.9.
Table 5.9 Noise
Measurement Results of Airbus H175 ¡V Non-lateral Movements
Operation Mode |
Reference Distance,
m |
Measured Highest
Noise Level Lmax of Airbus H175, dB(A) |
Highest Noise Level
Lmax of Replaced
Helicopters, dB(A) [1] |
Idling |
150 |
75.4 |
82.0 |
Lift-off |
150 |
82.4 |
89.0 |
Hovering |
150 |
83.5 |
90.6 |
Touchdown |
150 |
78.9 |
89.0 |
Note:
1. As mentioned in Section 5.6.3.1,
replaced helicopters include Super Puma AS332 L2 and Dauphin EC155 B1. The highest
noise levels among the replaced helicopters are represented by Super Puma AS332
L2 as extracted from the Table 4.10 of QMH Helipad EIA (Register No.
AEIAR-208/2017).
5.6.3.4 Based on the noise measurement results for non-lateral movements of
Airbus H175, it is found that its highest noise levels are around 7dB(A) ¡V
10dB(A) lower than that of the replaced helicopters.
5.6.4
Noise Impacts in Daytime ¡V Unmitigated Scenario
Helicopter and Helipad Buffer Distances
5.6.4.1 In order to keep the noise impact not higher than the daytime criterion
Lmax 85dB(A), the minimum buffer distances required between
identified residential NSRs and the Airbus H175 helicopter in different
operation modes have been estimated.
Assuming no barrier correction, backward calculation of the equations in
Section 5.6.2 and the noise data presented
in Table 5.8 and Table 5.9 have been adopted. NSRs outside the minimum buffer
distances would not be subject to adverse helicopter noise impacts in the daytime. The estimated buffer distances are
presented in Table 5.10.
Table 5.10 Minimum
Buffer Distance Required for Airbus H175
Operation Mode |
Estimated Buffer
Distance, m |
Buffer Distance
Required, m |
|
Non-Lateral Movements
at FATO of Helipad |
Hovering |
170 |
170 |
Lift-off |
150 |
||
Touchdown |
100 |
||
Idling |
67 |
||
Lateral Movements along Flight Path |
Approach |
116 |
116 |
Take-off |
79 |
||
Flyover |
90 |
Lateral Movements of Airbus H175 along Flight Path
5.6.4.2 Based on the 116m buffer distance required from the flight path for
lateral movements of the Airbus H175, a horizontal buffer zone of flight path has
been determined. The buffer zone of
the flight path and the locations of the NSRs are shown in Figure 5.4a.
5.6.4.3 It is found that all representative NSRs are located outside the buffer zone. Therefore, adverse helicopter noise
impacts on all representative NSRs are not anticipated during lateral
movements.
Non-Lateral Movements of Airbus H175 at FATO of Helipad
5.6.4.4 Based on the 170m buffer distance from FATO of the helipad for
non-lateral movements of the Airbus H175, a horizontal buffer zone of FATO has
been determined. The buffer zone of
the FATO and the locations of NSRs are shown in Figure 5.4b.
5.6.4.5 It is found that three NSR, namely P01a and P01b for KTD Site 3E1 and
P02a for KTD Site 3E2, fall within the horizontal FATO buffer zone. Therefore, adverse helicopter noise
impacts on these NSRs may be anticipated during non-lateral movements of the
helicopter, subject to actual slant distances and presence of screening
structures, if any. All other
representative NSRs are located outside the FATO buffer zone.
Predicted Noise Levels
5.6.4.6 The noise levels at NSRs due to helicopter operations have been
predicted. The highest predicted noise
levels and the corresponding operation mode are summarised in Table 5.11 and detailed calculations
are presented in Appendix 5F.
Table 5.11 Predicted
Unmitigated Helicopter Noise Levels
NSR ID |
Description |
Highest Predicted Noise Level Lmax (1), dB(A) |
Operation Mode |
Compliance (Y/N) |
Existing NSR |
||||
E01 |
Construction Industry
Council Kowloon Bay Training Centre (CIC Kowloon Bay) |
78 |
Approach |
Y |
Planned NSRs |
||||
P01a |
Kai Tak Development
Site 3E1 (KTD Site 3E1) |
85 |
Approach |
Y |
P01b |
86 |
Hovering |
N |
|
P01c |
85 |
Approach / Hovering |
Y |
|
P02a |
Kai Tak Development
Site 3E2 (KTD Site 3E2) |
85 |
Hovering |
Y |
P02b |
84 |
Approach |
Y |
|
P03 |
Proposed
Residential Development at Kerry Dangerous Goods Warehouse (Kowloon Bay)
(NKIL 5813) |
85 |
Approach |
Y |
P04 |
Kai Tak Development
Site 4E1 (KTD Site 4E1) |
83 |
Approach |
Y |
P05 |
Kai Tak Development
Site 4A1 (KTD Site 4A1) |
82 |
Approach |
Y |
P06 |
Kai Tak Development
Site 4B1 (KTD Site 4B1) |
85 |
Approach |
Y |
P07 |
Kai Tak Development
Site 4B2 (KTD Site 4B2) |
85 |
Approach |
Y |
P08 |
Kai Tak Development
Site 4B3 (KTD Site 4B3) |
84 |
Approach |
Y |
P09 |
Kai Tak Development
Site 4B4 (KTD Site 4B4) |
84 |
Approach |
Y |
Note:
1. Bold noise levels indicate exceedance of the daytime noise criterion of
Lmax 85 dB(A)
5.6.4.7 Based on the assessment results, the predicted highest helicopter noise levels
range from Lmax 78 dB(A) to 86 dB(A) at the NSRs. Daytime noise exceedances of 1dB(A) are
predicted at NSR P01b during helicopter hovering at the proposed helipad. It is predicted that approximate the top
12 floors of NSR P01b would be subjected to these noise exceedances.
5.6.5
Noise Mitigation Measures
5.6.5.1 In order to mitigate helicopter noise impact at the NSR, noise
mitigation measures, including setback of helipad and installation of noise
barrier and noise reducers on the top edge of the noise screening
structure/barrier, have been considered, and proposed as far as practicable for
the proposed helipad. GFS has
advised on the practicality of the mitigation measures in terms of helicopter
operations, as documented in Appendix 5H-3.
Setback of Helipad
5.6.5.2 As mentioned in Section 2.4.2,
the proposed helipad has been intentionally located on the western side of the
rooftop of Acute Block of the NAH in order to reduce the noise impacts and
direct lines of sight at nearby NSRs. Setback has, therefore, been provided for
the nearest NSRs, i.e. P01a and P01b of KTD Site 3E1. The separation distances between the
helipad and these NSRs have been maximised.
5.6.5.3 Besides, screening could be provided by the top edge of south-east roof
structure of Acute Block for NSR P01a due to this setback. Illustration of the screening is shown in
Appendix 5G. This setback has already been
taken account of in the unmitigated scenario of the helicopter noise impact
assessment.
Screening by Noise Barrier and Noise Reducers
5.6.5.4 Installation of noise barrier at the rooftop of the Acute Block of the NAH
can provide noise screening from the proposed helipad for nearby NSR, where the
roof edge of Acute Block is not sufficient. The noise barrier can reduce the direct
lines of sight between the NSR and the helicopter during non-lateral movements on
the helipad, achieving a minimum 5dB(A) noise reduction. In order to further improve the noise
shielding effect, noise reducers are proposed along the top edge of the noise screening
structures, including the proposed noise barrier and the south-east roof
structure of the Acute Block. Noise
reducers can improve the noise reducing performance of the noise screening
structure by modifying the upper sound diffracting edge. Specification of the proposed noise
barrier and noise reducers are given below:
Noise Barrier
¡P
The noise barrier shall be made of materials having
a surface mass density of at least 15kg/m2; and
¡P
The noise barrier shall be free of gaps or
openings.
Noise Reducers
¡P
Insertion loss performance of the Noise Reducers
shall be tested in accordance with ISO 10847 to achieve not less than 2dB(A);
and
¡P
Sound absorption performance of the Noise Reducers
shall be tested in accordance with ISO 354 to achieve not less than 0.7 at 400
Hz.
5.6.5.5 Nevertheless, the practicality on the proposed location of noise barrier
and reducers on the roof of Acute Block have been considered. The proposed noise barrier and noise
reducers should not affect approaching and departure operations of helicopters. Maximum height of the noise barrier and
noise reducers is also subject to building height restriction under the current
OZP. Therefore, proposed horizontal
and vertical extent of the noise barrier and noise reducers have been maximized
under the above constraints.
5.6.5.6 The extent of the proposed noise barrier and noise reducers are summarised
in Table 5.12 and shown in Figure 5.5. Illustration of screening
by the noise barrier with noise reducer on top for NSR P01b is shown in Appendix 5G. PlanD¡¦s advice on the
acceptability of noise barrier proposed at the rooftop of the Acute Block is
given in Appendix 2A.
Table 5.12 Summary
of Proposed Noise Barrier and Noise Reducers
Location |
Noise Mitigation
Measure |
Approx. Length (m) |
Top Level (mPD) |
Approx. 10m from Helipad to the Southeast |
Noise Barrier with
Noise Reducer on Top |
21.6 |
+123.9[1] |
Top Edge of Southeast Roof Structure of Acute Block |
Noise Reducer |
89.5 |
Min. +110.0[2] |
Note:
1. Around 4.75m above the proposed helipad surface at +119.15 mPD.
2. Based on the latest information provided by the Architectural Consultant
for the design of the NAH, the level of the south-east roof of Acute Block is
+110.0mPD. However, an additional solid
structure, such as a solid wall, might be proposed on and along the south-east
roof edge, and its height is not confirmed at the time of preparing this EIA report
and subject to further design of Acute Block. Nonetheless, it is agreed that the noise
reducer should be mounted on the top of the highest solid structure on the roof
at the south-east side. Therefore,
it is conservatively assumed that the minimum level of this noise reducer is
+110.0mPD. In case the additional
solid structure is proposed, the noise reducer will be proposed on top of it,
subject to the height constraints as mentioned in Section 5.6.5.5.
5.6.6
Noise Impacts in Daytime ¡V Mitigated Scenario
5.6.6.1 With the implementation of the above mitigation measures, the mitigated
noise levels at the NSRs due to helicopter operations associated with the
proposed helipad have been predicted.
The highest predicted noise levels and the corresponding operation mode are
summarised in Table 5.13 and detailed
calculations are presented in Appendix 5F.
Table 5.13 Predicted
Mitigated Helicopter Noise Levels
NSR ID |
Description |
Highest Predicted Noise Level Lmax, dB(A) |
Operation Mode |
Compliance (Y/N) |
Existing NSR |
||||
E01 |
Construction
Industry Council Kowloon Bay Training Centre (CIC Kowloon Bay) |
78 |
Approach |
Y |
Planned NSRs |
||||
P01a |
Kai Tak Development
Site 3E1 (KTD Site 3E1) |
85 |
Approach |
Y |
P01b |
85 |
Approach |
Y |
|
P01c |
85 |
Approach / Hovering |
Y |
|
P02a |
Kai Tak Development
Site 3E2 (KTD Site 3E2) |
85 |
Hovering |
Y |
P02b |
84 |
Approach |
Y |
|
P03 |
Proposed
Residential Development at Kerry Dangerous Goods Warehouse (Kowloon Bay)
(NKIL 5813) |
85 |
Approach |
Y |
P04 |
Kai Tak Development
Site 4E1 (KTD Site 4E1) |
83 |
Approach |
Y |
P05 |
Kai Tak Development
Site 4A1 (KTD Site 4A1) |
82 |
Approach |
Y |
P06 |
Kai Tak Development
Site 4B1 (KTD Site 4B1) |
85 |
Approach |
Y |
P07 |
Kai Tak Development
Site 4B2 (KTD Site 4B2) |
85 |
Approach |
Y |
P08 |
Kai Tak Development
Site 4B3 (KTD Site 4B3) |
84 |
Approach |
Y |
P09 |
Kai Tak Development
Site 4B4 (KTD Site 4B4) |
84 |
Approach |
Y |
5.6.6.2 With the implementation of the mitigation measures, the predicted
highest helicopter noise levels range from Lmax 78 dB(A) to 85 dB(A)
at the NSRs. All NSRs predicted with
exceedance of daytime helicopter noise criteria in the unmitigated scenario,
i.e. approximate the top 12 floors of NSR P01b, could be protected by the
direct noise mitigation measures. Thus,
adverse helicopter noise impacts at the NSRs during the daytime period are not
anticipated.
5.6.6.3 Noise contours, in terms of Lmax at four different mPD levels
including the general ground level, and the levels of lowest, middle and the
highest representative NSRs, are presented in Figure 5.6a to Figure 5.6d to show the distribution of the highest predicted helicopter noise
levels among all non-lateral operation modes under mitigated scenario. While noise contours for highest
predicted helicopter noise levels among all lateral operation modes are
presented in Figure 5.7a to Figure 5.7d.
5.6.7
Noise Impacts in Evening and Night-time
5.6.7.1 Since there are no relevant noise criteria in the TM-EIAO, nor in any overseas/
international guidelines applicable to emergency helicopter operations in the evening
and night-time periods, the helicopter noise impact during such time periods has
not been quantitatively assessed.
As mentioned in Section 5.2.3.5,
the emergency helicopter operations during the evening and night-time periods are
generally exempted from flight restrictions based on international practices.
5.6.7.2 Nonetheless, all practicable noise mitigation measures have been
exhausted and adopted at the proposed helipad to minimise the helicopter
noise. The new Airbus H175 helicopters
with lower noise levels have been adopted by the GFS. The design and selection of flight paths
have been optimised to avoid flying over the noise sensitive areas. The setback of the helipad and
installation of noise barrier and noise reducers have, also, been utilised to
provide screening and noise attenuation.
The proposed helipad has been designed and its operation has been
planned in a practicable manner to avoid adverse helicopter noise impact.
5.6.7.3 In accordance with the Civil Aviation (Aircraft Noise) Ordinance (Cap.
312), if the Director-General of Civil Aviation considers it appropriate, for
the purpose of avoiding, limiting or mitigating the effect of noise and
vibration connected with the taking off or landing of aircraft at an aerodrome,
to prohibit aircraft from taking off or landing, or to limit the number of
occasions on which they may take off or land, at an aerodrome during certain
periods, he may by notice in the Gazette to prohibit aircraft of descriptions
specified in the notice from taking off or landing at the aerodrome (otherwise
than in an emergency) during periods so specified; or specify the maximum
number of occasions on which aircraft of descriptions so specified may be
permitted to take off or land at the aerodrome (otherwise than in an emergency)
during periods so specified. Since
the use of the proposed helipad at NAH is for emergency service, which will be
on an as needed basis that cannot be controlled, restrictions such as limiting
the number of helicopter flights in evening and night-time periods or
restrictions on the operating hours of the helipad are not practical. The
proposed helipad at NAH will be available 24 hours a day for emergency uses
with no scheduled helicopter operation.
As mentioned in Section 5.6.1.6,
the evening and night-time emergency helicopter landings at the PYNEH were one
flight about more than every ten days and eight days respectively on average
and the frequency would be expected to be less for the NAH. The longest duration among different
operation modes of helicopter is 5 minutes. According to the QMH Helipad EIA, the
noise complaints about the helipad operation of TMH and PYNEH were rarely
received and total 7 noise complaints were received by HA and CAD in the years
between 2011 to 2015, as presented in Table
5.14. From 2016 to 2019, there
were 5 noise complaints received by CAD about the helipad operation of
PYNEH. It showed the general
understanding to such critical services and tolerance to the emergency
helicopter operation within the community.
Table 5.14 Statistics
of Helicopter Noise Complaint of TMH and PYNEH
Hospital |
Commencement Year |
No. of Noise
Complaints Received by HA |
No. of Noise
Complaints Received by CAD |
|
2011 - 2015 [1, 2] |
2011 - 2015 [1] |
2016 - 2019 |
||
TMH |
1992 |
0 |
0 |
0 |
PYNEH |
2004 |
1 |
6 |
5 |
Note:
1. Data are
extracted from the QMH Helipad EIA (Register No. AEIAR-208/2017)
2. As advised
by HA, the statistics of helicopter noise complaints received by HA in
2016-2019 are not available.
5.6.8
Cumulative Helicopter Noise Impacts
5.6.8.1 As advised by GFS, there is no other existing helipads or regular
helicopter flight routes identified in the vicinity of the proposed helipad.
5.6.8.2 However, it is noted that the GFS Kai Tak Division (GFS KTD) is planned
at the tip of the ex-Kai Tak Runway, which is about 1.5km to the south-east of
the NAH site. GFS have confirmed
that the flight paths of the proposed helipad and the GFS KTD would not overlap
with each other concurrently for flight safety reasons. Communications between helicopters and
the GFS control base will be on-going throughout all flight operations to
ensure the availability of flight paths.
Hence, cumulative helicopter noise impacts are not anticipated.
5.6.9
Evaluation of Residual Helicopter Noise Impacts
5.6.9.1 The proposed helipad has been designed and its operation has been
planned in practicable manner to minimise helicopter noise impact. A new helicopter fleet with quieter
operational noise levels has been adopted by the GFS. Flight sectors have been chosen for
helicopter movements and the flight paths have been designed to maintain buffer
distances from the NSRs. With the
implementation of the proposed practicable mitigation measures, including the
setback of helipad, noise barrier and noise reducers, helicopter noise impacts
on the representative NSRs have been mitigated as far as practicable. Also, the predicted helicopter noise
levels comply with the relevant helicopter noise standard as detailed in Table 5.2.
5.6.9.2 Typical flight height of the GFS¡¦s helicopter during flyover is 1500ft
above mean sea level and the duration of the flyover noise event is about 2-3
seconds. Under normal
circumstances, the duration of helicopter idling at the proposed helipad will
not be more than 5 minutes for casualty handover. Noise event of hovering at a height
around 2.5m above the helipad will be within 5 seconds before touchdown or
after lift-off.
5.6.9.3 The helicopter operation for emergency medical services provided by GFS
occurs randomly over the year. With
reference to the past helicopter flight records, the average number of daily
emergency helicopter operation was less than one. The operation during daytime period is
about once every one to two days on average, and the operation during evening
and night-time period are expected not more than one flight in ten days and
eight days on average respectively.
5.6.9.4 Based on the above, it is considered that all practicable noise
mitigation measures have been exhausted and adopted in the operation design of
the proposed helipad. Helicopter
noise impacts have been minimised, and thus, adverse residual noise impacts are
not anticipated during the operational phase of the Project.
5.6.10
Assessment of Side Effects and Constraints
5.6.10.1 Due to the inclusion of proposed noise barrier and noise reducers to the
Project, potential visual and air quality impacts are identified as the potential
side effects. Visual Impact
Assessment for the Project and the associated structures, including the
proposed noise barrier and noise reducers are detailed in Section 7. Air Quality
Impact Assessment in Section 3 has
also taken into account the proposed noise barrier.
5.6.10.2 As mentioned in the Section 5.6.5.1
and Appendix 5H-3, GFS has no objection on the noise mitigation measures in terms of
helicopter operation. Potential
constraint on the NAH building itself and other developments nearby due to the inclusion
of proposed noise barrier and noise reducers is not anticipated.
5.7.1.1
As no construction phase noise exceedances are anticipated,
therefore, construction phase noise monitoring is not considered as being
required. However, regular site
inspections during the construction phase, of at least once per week, are recommended
to ensure good working practices are being effectively implemented to minimise any
construction noise as far as possible.
5.7.1.2
During the operational phase, with the
implementation of mitigation measures, there would be no noise exceedances of
the relevant noise criterion at the representative NSRs. Also, the proposed helipad is solely for
emergency use only with no scheduled flights and the anticipated frequency of
usage is less than once per day. As
such, operational phase noise monitoring is not considered necessary.
5.7.1.3
The Environmental Monitoring and Audit (EM&A)
requirements and implementation of noise mitigation measures are detailed in
the stand-alone Project EM&A Manual.
5.8.1.1 The potential noise impacts associated with the Project in the construction
and operational phases have been assessed.
5.8.1.2 The noise impacts arising from daytime construction activities for the
Project have been evaluated. No
evening or nighttime construction works will be scheduled. Cumulative construction noise impacts
with concurrent project have also been considered. It is shown that the predicted noise
levels at the one representative NSR will comply with the relevant construction
noise criterion and no specific mitigation measures will be required. Nonetheless, the adoption of good site
practices and use of quieter PMEs have been recommended to minimise the construction
noise impacts. Hence, no adverse
construction noise impacts are anticipated.
5.8.1.3 In the operational phase, the noise impacts arising from GFS¡¦s helicopter
operation associated with the Project have been evaluated. The helicopter noise impact assessment
was conducted using a conservative approach under the worst-case scenario. All practicable measures, including carefully
chosen flight sectors and one-way-direction for approaching and take-off
subject to flight condition, and maintaining buffer distance for flight paths
to fly away from NSRs, have been utilized for helicopter operation. With the implementation of direct noise
mitigation measures, including setback of helipad and installation of noise
barrier and noise reducers, the helicopter noise impacts have been minimized,
and the predicted helicopter noise levels at the representative NSRs are within
the criteria in Table 5.2. Nonetheless, the emergency medical helicopter
operation occurs randomly over the year, it is anticipated that the average helipad
usage will be less than once per day, while the duration of each emergency use
will be about 7 minutes as detailed in Section
5.6.1.4.
5.8.1.4 The proposed helipad in NAH will share the landing frequency for
emergency medical services at the existing and planned helipad facilities at
public hospitals. The Project
enables point-to-point direct and speedy transfers of patients / survivors that
require special care to the NAH. It
is critical to lifesaving and significant for provision of timely treatment to
patients. It is also an essential
infrastructure development in Hong Kong to cater for the change in population
and to maintain a high quality of medical services which shall be generally
agreed by the public.