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HELIDECK OPERATIONS
AND PROCEDURES
MANUAL
Document Control Sheet
Control Information
Title Document (NL)
Title Document (UK) Helideck Operations and Procedures Manual
Type Document (NL/UK) Industrie Leidraad/Industry Guideline
Control Number: 14
Control Status: Controlled / Uncontrolled when Printed.
Issue Status This document has been published electronically on the NOGEPA Website. In order to maintain this document as a “controlled copy" any formal revisions will be published via this Website and should replace all previously issued revisions.
Document Review Timeframe for document review – C3
C1 - 12 Months C2 - 24 Months C3 – 36 Months
Approved by:
Health & Safety Committee
Name:
S. Floore
Date: 12 October 2011
Operations Committee Name:
R. Happé
Date: 12 October 2011
Executive Committee Name:
G. v.d. Brink
Date: 12 October 2011
Revision History
Rev Date Description Author Reviewed. Reviewed Approved
0 First Issue M.Meskes
1 30-09-2009 Revision 1 J. Klootsema S.Floore R. Happé C. Guéritte
2 12-10-2011 Update regulations & inspection J. Klootsema S. Floore R. Happé G.v.d. Brink
This document will be controlled by the NOGEPA Secretary. This document will be sent to the NOGEPA Executive Committee for approval if: - A new NOGEPA Guideline is issued. - Significant changes are made to the content of a particular NOGEPA Guideline All other changes and revisions will be approved by the Health and Safety Committee.
Introduction
Purpose
To provide information on the management and operation of offshore helidecks on mining installations and vessels, and the provision of suitable arrangements to assure their availability under both normal and emergency situations.
General Information Since oil and gas exploration began on the Dutch Continental Shelf, the Offshore Industry has been dependent on the efficient use of helicopters for logistics and emergency support. The primary role is moving people to and from their workplaces on the offshore facilities. Other roles include freight movement, emergency evacuation and search and rescue. The helicopter‟s evolution, over the years since the late 60‟s, into a routine “workhorse” has inevitably brought its operational support activities into sharper focus. The harsh operating environment, some serious and fatal incidents and the emergence of goal setting offshore safety requirements, have all contributed to a greater awareness concerning the problems associated with operating helicopters in a maritime environment. The greater awareness of operating is generally not matched by a clear understanding of the technical requirements associated with the interface between aeronautical / oil and gas / marine operations. Guidelines are intended to contribute to the level of technical understanding in the offshore oil and gas industry and work in connection with it. They focus on the various elements of offshore helideck operations and the achievement of higher standards of safety and operability. They are:
• Regulatory requirements and auditing. • Helideck inspection. • Helideck operations. • Maintenance. • Competence and training. • Comments are welcome to [email protected] . After 2 years we will review comments received and
consider preparing a revision.
Copyright Statement
All rights reserved. No part of this publication may be reproduced in a retrieval system or transmitted
in any form or by any means including, but not limited to: electronic, mechanical or photocopying without the permission of:
NOGEPA
Koningin Julianaplein 30-05B
Postbus 11729
2502 AS „s-Gravenhage
The Netherlands
Chapter 1
Table of contents
: Relevant Legislation
Chapter 2
Chapter 3
Chapter 4
Chapter 5
Chapter 6
Chapter 7
Chapter 8
Chapter 9
Chapter 10
Chapter 11
:
:
:
:
:
:
:
:
:
:
Helideck Regulations
Operating Procedures
Special Procedures
Communication
Helicopter Loading
Transportation of special loads
Refuel Facilities
Helicopters frequently used
Company Specific Requirements
Appendices
GLOSSARY OF TERMS AND ABBREVIATIONS
Most of the terms below are used in this document, however the list also includes other terms in common
use in Logistics and Air Logistics.
µ
150° sector
180° sector
210° sector
ADELT
AFFF
(Pronounced “mu”) measurement of friction.
Obstructed Sector of a helideck / Limited obstacle sector. (= LOS)
Vertical Obstacle free Sector of a helideck.
Obstacle free Sector of a helideck. (= OFS)
Automatically Deployable Emergency Locator Transmitter.
Aqueous Film Forming Foam.
Aircraft Operator Company operating helicopters.
CO2
CPI
“D”
“D” circle
dB(A)
DSV
ERP
ERT
ETA
HDA
HLO
HSE
IATA
IFR
IMC
Inbound Flight
Installation
LOS NDB
NAI
NUI
OIM OFS
Platform
Rig
RO
R/T
SAR
SLA
VFR
VHF
VMC
Z
Carbon Dioxide.
Crash Position Indicator.
The largest overall dimensions of the helicopter when rotors are turning. This
dimension will normally be measured from the most forward position of the main rotor
tip path plane to the most rearward position of the tail tip path plane.
A circle, usually imaginary unless the helideck itself is circular, the diameter of which
is the “D” value of the largest helicopter the helideck is intended to serve.
Decibels – a measure of noise level.
Diving Support Vessel.
Emergency Response Plan.
Emergency Response Team.
Estimated Time of Arrival.
Helideck Assistant.
Helicopter Landing Officer.
Health and Safety Executive.
International Air Transport Association.
Instrument Flight Rules.
Instrument Meteorological Conditions.
Flight from offshore to onshore.
Oil production platform or rig.
Limited Obstacle Sector, the 150° sector within which obstacles may be permitted.
Non-Directional Beacon.
Normally Attended Installation.
Normally Unattended Installation.
Offshore Installation Manager.
Obstacle Free Sector.
Production platform.
Drilling Rig.
Radio Operator.
Radio Telephony.
Search and Rescue.
Safe Landing Area.
Visual Flight Rules.
Very High Frequency.
Visual Meteorological Conditions.
ZULU (Time Scale).
Chapter 1
Relevant Legislation
Chapter 1 – Relevant Legislation
1.1 Roles and Responsibilities as
defined by law
This chapter is intended to provide the HLO
with a brief overview of the regulations on the Dutch North Sea. Emphasis is placed on the responsibilities of the HLO/HDA
1.2 International regulations
There are a number of organizations,
internationally, that have established regulations,
rules or guidelines that are used for the basis by individual countries for the establishment of their own regulations.
1.2.1 Joint Aviation Authority
The Joint Aviation Authority (JAA) is an
organization in which more than 20 countries in
Europe cooperate to establish requirements for the safe operation of aircraft. The national aviation authorities of the countries bordering the North Sea offshore are all represented in the JAA.
1.2.2 ICAO
The International Civil Aviation Organization
(ICAO) is a worldwide organization, which has
established standards of practice, which are
accepted as being normal for the aviation industry. The JAA and its member countries operate to the ICAO standards as a minimum.
1.2.3 EASA The European Aviation Safety Agency is the Centerpiece of the European Union‟s strategy for aviation safety. It monitors the implementation of standards through inspections in the Member States and provides the necessary technical expertise, training and research. Their mission is to promote the highest common standards of safety and environmental protection in civil aviation.
2
Chapter 1 – Relevant Legislation
1.6 The Netherlands
Which legislation and regulations do apply?
Legislation covering the duties of a Helicopter Landing Officer employed in areas under the control of the Netherlands are to be found in the following publications
Dutch Aviation Act
Dutch Mining Decree, article 51
Arbo Decree, art 2.14, section 3
Regulations safe use of airports and
other terrains (Nov 2009)
International regulations:
JAR Ops. 3
ICAO annex 14/18 CAP 437
1.6.1 Related duties.
There are a number of duties that may be
carried out by a person or persons working in support of the helicopter activities. All
personnel when carrying out such duties
shall be under the direct control of the Helicopter Landing Officer (HLO).
1.6.2 Nogepa training courses
1.1 A/B HLO
1.3 A/B HDA 2.6 A/B Fire team member 2.8 A/B Fire team leader 2.9 A/B Fire team (NUI)
3
Chapter 2
Helideck Regulations
Chapter 2 – Helideck Regulations
2. Helideck
This section describes the regulations, guidelines and mandatory instructions for the management,
operation and equipping of helidecks on offshore installations and vessels operating in
the Dutch sector of the North Sea.
Obstacles with respect to the landing
area.
2.1 Obstacle free area above the
helideck level.
The upper side of the landing area and the
horizontal area leading to it is bordered by an
imaginary circle with a radius of up to 500 meters. The center of this circle is situated on
the arc of the inscribed circle "D".
That imaginary circle is divided into two sectors: Obstacle Free Sector (OFS) with an angle of 210°.
Limited Obstacle Sector (LOS) with an angle of 150°.
In the OFS, outside the white perimeter line,
there may be no obstacles penetrating the plane of the circle "D" that are higher
than 0.25 meters. Inside de white perimeter line there may be no obstacles higher than 2,5 cm.
In LOS out to a distance of 0.62 "D" measured from the center of the helideck,
objects shall not exceed a height of 1/20 "D" with a maximum height of 1.1 meters above
the plane of the helideck.
Obstacle free area below the helideck
level.
This area must extend over an arc of at least
180° with the origin at the center of the Touch down and Lift Off area (TLOF), with a descending gradient at a ratio of one unit
horizontally to five units vertically (5:1) from
the edge of the TLOF within that 180° sector.
2
Chapter 2 – Helideck Regulations
2.2 Illumination of the helideck and the
surrounding area.
During the hours of darkness, and if the visibility is
1500 m or less, helideck and obstruction lighting must be switched on not less than 5 minutes before
any expected helicopter operation.
2.2.1 Surface lighting (floodlighting)
The landing area must have non-dazzling surface
lighting (Flood Lights). They must allow the pilot to see the deck markings, not blind him.
2.2.2 Perimeter lighting
The regulations state that the landing area must be
delineated by green omni directional lights, spaced at intervals of not more than three (3) meters around the perimeter of that landing area.
2.2.3 Obstruction lighting
Red omni-directional obstruction lighting of at least
10 candelas, must be fitted to all high structures
including the jibs of cranes. High obstructions should where possible be illuminated by floodlights, shining upwards along the obstruction.
3
Chapter 2 – Helideck Regulations
2.3 The anti slip net
There must be an adequate friction coefficient in
both wet and dry conditions to allow the helicopter to remain in one place on the deck without slipping.
It must have friction coefficient of at least μ = 0.65.
If an “anti-slip net”, or “landing net”, is used to
achieve the required levels of grip for the helicopter, it must:
• be made of a material that is not a hazard for helicopter turbines;
• have at least ø 15 mm, but not more than Ø 20 mm; • cover the aiming circle;
• have a mesh which is not less than 200
mm and not more than 250 mm and in such a way that it cannot slide or change size;
• be secured every 1.5 meters around the landing area perimeter;
• be tensioned to approximately 2225 N
(500 lbs). Where no device is available to
test the tension a simple test may be done by standing in the middle of the net (with the feet in the mesh of the net) and lifting the net. If the net does cannot be raised more than ± 25 cm and returns smartly to the deck then the tension is considered to be adequate.
An alternative to the traditional landing net is to use frictape. When frictape is used chocks must be used to secure the helicopter on deck.
2.4 Clear landing area
The helideck must be kept free of any snow or ice
during helicopter operations. Equipment for this purpose must be available on the installation at all times.
2.5 Perimeter safety net
A flame retardant, UV resistant safety net must be
Installed around the helideck, unless safety is ensured
By another construction. The net should be made of
Fire resistant flexible material that is protected
against the influences of weather, and have a mesh
not more than 80 mm.
The net should be secured in such a way that its
inboard edge is below the edge of the helideck and
with its outboard edge at least 1.5 meters away from the edge of the helideck, sloping upwards with an angle of 10° and not exceeding a height of 0.25 m above the plane of the landing area.
4
Chapter 2 – Helideck Regulations
2.6 Access to the helideck
The helideck must be accessible from at least two
points, positioned as far as practically possible from each other.
2.7 Meteorological equipment
2.7.1 Wind sock
A windsock must be installed to give an indication of
the direction and condition of the wind over the landing area. The windsock should be positioned in clear air and visible to the pilot irrespective from the wind and approach direction.
For night operations the windsock must be clearly
illuminated.
2.7.2 Weather instruments
Permanently manned offshore installations must be
equipped with calibrated instruments to measure the current weather conditions in order to be able to
inform the pilot. The instruments must include at
least: • an anemometer - to measure wind speed
and direction; • a barometer – to measure air pressure; • a thermometer – to measure air temperature.
2.8 Operational equipment
Offshore installations must have available, in the
immediate vicinity of the helideck, all the equipment
that will be needed for use in connection with helicopter operations including:
1. Rope, bonding material;
2. Chocks or sand bags (min. 4);
3. A scale for weighing the baggage;
4. An electrical power supply* for start-up
of helicopter.
Does not apply for Normally Unmanned Installations
5
Chapter 2 – Helideck Regulations
2.9 Passenger safe areas
A poster indicating the safe areas that passengers
must use when leaving or approaching the helicopter
should be placed in a prominent position on the
installation.
2.10 Emergency rescue equipment
(crash box)
The equipment which will be necessary in the event
of an accident involving a helicopter must be in the vicinity of the helideck and must be ready for use. This will include at least the following items:
1. Adjustable wrench
2. Set of assorted screwdrivers
3. Tin snip
4. Aircraft type rescue axe.
5. Hacksaw heavy duty.
6. Minimal 6 spare heavy-duty blades.
7. Grab hook.
8 Crash knife.
9. Crowbar with a length of 100 cm.
10. Large bolt cutter 24". (60 cm.)
11. Fire blanket.
12. Fire resistant gloves. (2 pairs)
13. Life line, length 15 meters and 15 mm diam.
14. Ladder. (advised length = 3 meters)
15. Inventory list
2.11 Personnel requirements.
On every installation, during helicopter operations
there must be a number of trained persons (at least 2) at or near the access points to the helideck.
Each person should be fully trained in helicopter fire
fighting and rescue procedures (NOGEPA 2.6/2.8/2.9). The Helicopter Landing Officer and the Helideck Assistant should wear a vest with respectively HLO or HDA on the front and the backside.
Firefighting personnel must wear the correct
protective clothing.
6
Chapter 2 – Helideck Regulations
2.12 Fire fighting equipment requirements
The following fire fighting and rescue equipment
must be located, for immediate use in the event of
an accident. It is advised to have a system for
testing the equipment.
2.12.1 Foam forming agent
The minimum requirement for foam production is six
(6) litres of the solution per minute, per square meter of the landing area, for a duration of not less than five (5) minutes. In case of film forming foam the quantity maybe reduced with one third.
2.12.2 Dry powder extinguishers
There must be at least two (2) dry powder fire
extinguishers having a total capacity of not less
than forty five (45) kg.
2.12.3 Other extinguishers
There must be carbon dioxide (CO2)extinguishers of a total
capacity of not less than eighteen (18) kg or equivalent, one of
these extinguishers being so equipped (long lance) as to enable
it to reach the engine area of any helicopter using the deck.
2.12.4 Water hoses
There may be at least two (2) water hoses, with
adjustable nozzles.
2.12.5 Ring line system
The foam forming agents system mentioned above
may be replaced by a ring line system equipped with spray heads that the landing area can be covered with foam in all weather conditions. In such cases the two (2) hose lines mentioned above, must also be able to produce foam. 2.13 Provisions for unmanned mining installations 2.13.1 Transport of persons When persons are transported to or present on an unmanned mining installation, at least 2 persons shall be familiar with and trained in the use of the firefighting equipment and rescue means present on or near the helideck. Before a helicopter will land on an unmanned mining installation, it shall be checked from the operational centre from which the subject installation is operated whether unburned hydrocarbons are present on the helideck to such an extent that it constitutes a danger of explosion.
7
Chapter 2 – Helideck Regulations
2.13.1 Firefighting equipment The quantity of fire-extinguishing agent referred to 2.12.1 may be replaced by quantities set out in the case of a landing area with a diameter of the depicted circle measuring: a) no more than 15 m in size, a quantity of
water with film-forming foam of at least 500 litres is required;
b) between 15 and 24 m, a quantity of water with film-forming foam of at least 1000 litres is required;
The quantity of water referred to above may be replaced up to a maximum of one third by by fire-extinguishing powder in a ratio of 1 kg powder per litre of replaced water. The delivery capacity shall, in the case of water and film-forming agent, be at least 230 litres per minute and, for fire-extinguishing powder, be a minimum of 2 kg per second.
2.14 Safety notice boards
Near the access points to the helideck notice boards shall be prominently placed and written
in the languages that are normally spoken on the platform.
"Safety Notice Boards" shall mention at least
the following:
Safety Notice Board.
No smoking. Beware of the tail rotor. Use the safe approach routes. Do not approach the helicopter while the
anti-collision lights are flashing. No hard hats without chinstraps secured. No loose headgear.
8
2.15 R.A.C.I. Chapter 2
Responsible Accountable Consult
Inform
1
Obstacles above/on the helideck
HLO
HLO
Pilot
OIM/ O.C.
2 Illumination of the helideck and the
surrounding area
HLO HLO/OIM - Pilot/
O.C.
3
Anti slip net / perimeter safety net
HLO
OIM
Pilot Pilot/
O.C.
4 Meteorological equipment
OIM
OIM
O.C. Pilot/
O.C.
5
Fire fighting equipment / crashbox HLO/OIM OIM
O.C. Pilot/
O.C.
6 Personnel requirements
R = Responsible A= Accountable C= Consult I = Inform
Chapter 2 – Helideck Regulations
OIM
OIM
O.C. Pilot /
O.C.
9
Chapter 3
Operating Procedures
Chapter 3 – Operating Procedures
3.1 Introduction. Helicopter safety is the concern of all personnel involved in helicopter operations. The HLO can make his particular contribution to safety with helicopters, and safety in general, by his good example. This includes:
• his ability to act as a leader of a team that
will work for and with each other to ensure a safe and efficient operation;
• his ability to act as a source of information concerning helicopter operations;
• instilling safety awareness to installation staff and passengers;
• his ability to assist the helicopter crew; • his ability to respond quickly and efficiently
to any emergency situation. The HLO will as part of his daily routine organize toolbox meetings with his crew. 3.2 Duties of the Helicopter Landing Officer. The regulations (see chapter 1) define the response- bilities of the HLO, but do not necessarily name all of his duties. The allocation of the duties and tasks to the HLO is the responsibility of the Offshore Installation Manager. 3.3 Routine precautions: When a helicopter has landed on the helideck there are a number of routine precautions that must be observed by all personnel involved in the helicopter operation:
3.3.1 Control of Crane Operations The HLO shall ensure that crane (s) are not operated and clear of the helideck during times when helicopters are landing, taking off or are on deck with rotors running. If a crane is not in the parked position, its status shall be given to the pilot at the time of giving clearance to land.
3.3.2 Approaching the helicopter Only approach the helicopter when the "Anti-collision Light(s)" have been switched "Off".(see Chapter 9 for location(s)). This will indicate that the pilot is satisfied that it is safe to approach the helicopter via the designated approach areas. The pilot will normally confirm this by giving a hand signal “Thumbs Up”.
2
Chapter 3 – Operating Procedures
3.3.3 Rotor blades The different forces of air produced by the running rotor blades can blow off helmets etc. and lift loose particles into the air. Stay well clear of the tail rotor and the main rotor in front of the aircraft (see Appendix 6). 3.3.4 Static electricity Ensure that during the refueling operation the correct bonding procedures are carried out at all times. (Chapter 8)
3.3.5 Engine air intakes and exhausts Stay well clear of the engine air intakes and exhausts at all times. 3.3.6 Fire fighting equipment Helideck fire fighting equipment must be ready for use at all times during helicopter operations. It is the responsibility of the HLO to ensure that the periodic tests have been carried out at the required times, and that the equipment certifications are within date. 3.3.7 Floatation gear
Stay clear of the flotation gear where possible. 3.3.8 High wind conditions: Passenger safety is of prime importance at all times, but special care shall be taken during periods with high wind speeds on the helideck. 3.3.9 Passenger information: The person signing the manifest is expected to ensure that the passengers have been properly briefed. (Safety briefing DVD). The HLO shall ensure that the items listed on the manifest have been transferred. 3.3.10 Before the flight: The passenger Safety briefing DVD shall be shown before each flight, unless the flight is continuing with the same aircraft and the same passengers within 24 hours. 3.3.11 During the flight: Safety information cards are available in the helicopter to inform the passengers of the available emergency facilities. During the flight, passengers are required to follow the procedures as laid down by the helicopter operator, and in particular to follow any instructions given by a member of the helicopter crew. 3
Chapter 3 – Operating Procedures
3.3.12 Seat belts Seat belts must remain fastened at all times during the flight! 3.3.13 Smoking The "No Smoking" sign must be observed at all times.
3.3.14 Survival suits The Oil Company issues survival suits to be worn during the flight. These suits must be worn correctly in order to function properly. Donning of the suits shall be done below helideck or in any other designated area. 3.3.15 Unusual occurrences Any unusual occurrences, such as noises, leaks or smells shall be reported immediately to a member of the helicopter crew. 3.3.16 After the landing
Passengers must remain seated with their seat belts fastened. The seat belts may only be released when the illuminated "fasten seat belts" sign has been switched off and the cabin door has been opened by a member of the helicopter crew or by the HLO. Disembarking of the helicopter is only allowed, when guided by the HLO or HDA. Take-off life-jackets once outside the helicopter. 3.3.17 Operation of cabin doors Cabin doors on the different aircraft all have there specific techniques for operating. The HLO shall receive operating instructions for the types of helicopters landing on his installation. If not familiar the HLO shall ask instructions from the pilot. Ensure never to apply excessive force. 3.4 Recommended checklists for the HLO The following checks are recommended as a general guide for the HLO, to assist him in the daily duties concerning the helicopter operations to and from his, installation, or vessel. The HLO normally carries out most of the checks, but some checks maybe carried out by other personnel under his direct control. (See appendices 1 & 2). 4
Chapter 3 – Operating Procedures
3.4.1 Daily checks of equipment and facilities
The helicopter deck and landing area must be checked each and every day. The following is a list of the items that are to be checked on a routine basis:
• General condition of the landing area; • Condition and tension of the landing net; • Condition of visual aids, marking, lights, and
illuminated windsock; • Condition of perimeter safety nets; • Deck (operational) equipment including helicopter starting equipment; • Emergency equipment; • Refueling facilities (if appropriate); • Availability of fire-fighting equipment; • Safety notices ; • Effect of bird droppings.
For more information, see appendices 1 & 2
Any deficiencies shall be corrected or reported in
the maintenance system and to the helicopter operator.
5
3.5 R.A.C.I. Chapter 3
Responsible Accountable Consult
O.C.
Inform
Pilot / Passengers
1 Routine precautions 2 Daily/Weekly/Yearly checks of
HLO HLO/OIM OIM OIM/O.C.
Pilot/ Passengers
3
equipment and facilities
Pre Landing checks
HLO/OIM
HLO HLO
O.C.
O.C.
OIM/O.C.
Pilot
R = Responsible A= Accountable C= Consult I = Inform
Chapter 3 – Operating Procedures
6
Chapter 4
Special Procedures
4.1 Helideck Emergency Procedures
It is vital that the HLO has well established procedures to deal with any emergency that may arise. Special attention must be paid to access the Company Emergency Procedures to coordinate an efficient system of covering all emergency situations. 4.1.1 Plan of action. It is important to have a plan of action ready for emergency situations; such a plan shall include items such as:
1. 2. 3. 4.
Briefing and alerting of personnel; Positioning of equipment; Communication; Consult the emergency response plan of the responsible oil company.
4.1.2 Examples of potential emergency
situations. 1. 2. 3. 4. 5. 6. 7. 8. 9.
Fire during the refueling operation; Engine fire during start up; Obstructed or damaged helideck; Helicopter heavy landing developing into a fire situation; Helicopter ditching near your installation; Fire alarm on another part of the installation during helicopter operations; Man overboard alarm during helicopter Operations; Evacuation of the installation; Evacuation of an installation close to a nearby one;
Chapter 4 – Special Procedures
10. Transport of sick or injured personnel; 11. Accepting survivors from another installation
or vessel; 12. Fire in helicopter cabin; 13. SAR duties and contingencies; 14. Attempted “wheels up” landing.
4.1.3 Control of helideck emergencies See Appendix 3
2
4.2 R.A.C.I. Chapter 4
Responsible Accountable Consult
Inform
1 Helideck Emergency Procedures
R = Responsible A= Accountable C= Consult I = Inform
Chapter 4 – Special Procedures
HLO
OIM
OIM
O.C.
3
Chapter 5
Communication
5.1 Communication responsibilities of the HLO
Scope of responsibility Before and during the helicopter operations the HLO has to maintain good communications by either one of the following methods: 1. 2. 3.
Radio messages; Light signals; Hand signals.
With possibly one or more of the following person(s): • • • • • • • • • •
Helicopter pilot; Helicopter crew when on the helideck; Radio operator; Crane operators; Standby vessel; Fire and rescue crew; Passengers; Loaders; Refueling crew; HMI or Ships captain.
Chapter 5 – Communication
5.1.1 Communication radiotelephone The HLO should be equipped with a portable transceiver set, operating on the same VHF frequency as the pilot of the visiting helicopter and the Radio Operator. The HLO may only act in advisory capacity e.g. "Deck clear" or "Crane up, but stationary". Note: 1. Radio operators and HLO‟s will not assume the authority of air traffic control, but will only act in an advisory capacity. 2. Correct handover procedures between the Radio
Operator and the HLO must be followed at all times. 3. In practice the Radio Operator will constantly be in contact with the pilot, starting 5 minutes before ETA.
The HLO has a headset with which he can communicate with the pilot about practical issues relating to the helicopter on deck.
2
5.1.2 Phonetic alphabet. When transmitting an helicopter call sign or spelling words the "Phonetic alphabet" must be used at all times. A: Alfa. B: Bravo. C: Charlie. D: Delta.
J: Juliet. K: Kilo. L: Lima. M. Mike.
S: Sierra. T: Tango. U: Uniform. V: Victor.
E: Echo. N: November. W. Whisky. F: Foxtrot. G: Golf. H: Hotel. I: India.
O: Oscar. P: Papa. Q: Quebec. R: Romeo.
X: X ray. Y: Yankee. Z: Zulu.
5.1.3 Phonetic numbers. When transmitting figures, the following pronunciation must be used:
0: Ze-ro. 1: Wun. 2: Too. 3: Three.
4: Fow-er. 5: Fife. 8: Ait. 9: Nin-er.
5.1.4 Readability scale.
6: Six. 7: Seven.
Chapter 5 – Communication
The following scale should be used when reporting on radio strength and clarity:
STRENGTH 1. = Means unreadable.
STRENGTH 2. = Means readable intermittently. STRENGTH 3. = Means readable with difficulty. STRENGTH 4. = Means readable. STRENGTH 5. = Means perfectly readable.
3
5.1.5 Standard words and phrases. The following list of words and phrases should be used during normal radio communication procedures
WORD OR PHRASE. =
TTHE MEANING.
ACKNOWLEDGE: AFFIRM: APPROVED: BREAK: CANCEL: CHECK: CLEARED: CONFIRM:
CONTACT: CORRECT: CORRECTION: DISREGARD: HOW DO YOU READ: I SAY AGAIN: MONITOR: NEGATIVE: PASS YOUR MESSAGE: GO AHEAD: READ BACK: REPORT: REQUEST: ROGER: SAY AGAIN: SPEAK SLOWER: STANDBY VERIFY: WILCO:
= = = = = = = = = = = = = = = = = = = = = = = = = = =
Let me know that you have received and understood the message. Yes. Permission for proposed action granted. Indicates the separation between messages to different stations. Annul the previously transmitted message. Examine a system or procedure. Authorized to proceed under the conditions specified. Have I correctly received the message, or did you receive my message correctly. Establish contact with. That is correct. An error has been made in this transmission, the correct version is. Consider the transmission as not sent. What is the readability of my transmission. I repeat for clarity or emphasis. Listen out on (frequency) No, or permission not granted, or that is not correct. Proceed with your message. Proceed with your message. Repeat all, or specific part, of the message. Pass requested information. I would like to know, or I wish to obtain. I have received all of your last transmission. Repeat all after, give the last received word. Reduce rate of speech. Wait I will cal you(no onward clearance to be assumed) Check and confirm. I understand and will comply.
Chapter 5 – Communication
4
5.1.6 Frequencies used in the Dutch area of the North Sea.
VHF: North of 53° North, but with the exception of blocks K18, L16 and L17. Primary frequency =
125.175 MHz.
South of 53° North, but with blocks K18, L16 and L17 included. Primary frequency
=
122.950 MHz.
Chapter 5 – Communication
Den Helder frequency = 131,5 MHz 5.1.7 Helicopter call signs.
The helicopter call sign will be the phonetic pronunciation of the registration letters of the helicopter, or a specific company call sign. Once communication has been established the registration may be abbreviated to: e.g. Maple 1, 2, 5, 7, etc. Bristow 53, 56, etc. If your station is called but you are uncertain as to the identity of the station calling, transmit the following: “Station calling (platform name) say again”. 5.1.8 Message content All messages must be short and to the point. 5.1.9 Time Times used should be in UTC (Universal Time Coordinated) but in some areas of the North Sea local time is used, but always using the 24-hour clock.
5
Chapter 5 – Communication
5.1.10 Departure message If the next destination of the helicopter is an onshore airfield, the installation Radio Operator passes a "departure message" to operations on the airfield,giving the following information:
a. Helicopter call sign; b. Destination and estimated time of arrival (ETA); c. Persons on board (POB) /Passengers (PAX); d. Amount of cargo.
Under certain conditions the helicopter pilot may request a “radio watch” until radio contact has been made with the Flight Information Region (FIR) or an other offshore station. 5.1.11 Distress and urgency communications (MAYDAY) Distress and urgency traffic must receive absolute priority over all other transmissions. A distress message should first be passed on the frequency in use. All stations that will hear the distress message must immediately cease all other transmissions that are likely to interfere with the distress traffic. Always acknowledge a distress message, and try to collect as much information as possible including:
a. Aircraft call sign or name of ship; b. Nature of the distress; c. Present position; d. Height (aircraft); e. Heading; f. Speed; g. Number of persons on board (POB); h. Captains intentions; i. Any other information that may help in the rescue.
All subsequent messages concerning the distress should be preceded by the word MAYDAY. The station that takes control of the Mayday should impose silence on all other stations using that frequency (or the distress frequency) by making the following transmission: ”All stations this is (platform name) stop transmitting mayday in progress.” If and when the Mayday is over the "radio silence" should be cancelled by: “All stations this is (platform name) distress traffic ended.”
6
Chapter 5 – Communication
5.1.12 Weather information When the helicopter is approaching your platform the pilot will request a “weather up-date” for specific items of the weather conditions. Weather up-date:
A. Wind direction B. Wind speed C. Any other last minute changes. D. Visibility (best guess) E. Cloud base (best guess)
5.1.13 Hand marshalling signals See Appendix 4
7
5.2 R.A.C.I. Chapter 5
Responsible Accountable Consult
Inform
1 Helideck communication
2 Weather Information
HLO
HLO
HLO
HLO
Radio-
Operator/OIM
Radio-
Operator
Radio-
Pilot/
OIM
Pilot
3 Hand marshalling signals
R = Responsible A= Accountable C= Consult I = Inform
Chapter 5 – Communication
HLO HLO Operator/Pilot Pilot
8
Chapter 6
Helicopter Loading
Chapter 6 – Helicopter loading
6 Introduction
The HLO is responsible for all those engaged in
operations on or near the helicopter landing area
(not the pilots), including those engaged in loading
and unloading duties.
6.1 Loading duties Correct loading of the helicopter is the responsibility of the helicopter crew. Loaders may be detailed to give assistance. Those engaged in loading operations are required to be under the direct control of the HLO
6.1.1 The HLO is responsible for the following operations:
A. Control the movement of all personnel (HDA)
on or near the helideck, including baggage, disembarking and embarking passengers;
B. Control of all personnel engaged in the loading
and unloading duties;
C. The HLO will have control of the passengers
donning survival suits and after boarding the helicopter, the correct way of wearing the life
jacket and before closing the doors that
all the seat belts are secured;
D. Providing the helicopter crew with the correct
manifest.
6.2 Baggage
Due to the limited payload and baggage capacity available in most types of helicopters, it is advisable to reduce personal baggage as much as possible, both in weight and volume. Baggage may not be carried in the cabin of the helicopter. It is not recommended to carry loose baggage this could cause injuries to passengers and crew during a forced landing or hinder evacuation after a ditching.
6.3 Weight of passengers, baggage and cargo
To insure that the available payload is efficiently used and the maximum “take off weight” of the helicopter is not exceeded. It is unacceptable to estimate the weight of passengers, baggage or cargo. Baggage and cargo must be weighed on every occasion prior to being transported by air.
2
Chapter 6 – Helicopter loading
6.4 Cargo handling Cargo shall only loaded into the baggage com- partment of the helicopter. (Not in the cabin!) Care must be taken when loading baggage and cargo to ensure that the helicopter is not damaged in any way 6.5 Manifest 6.5.1 A manifest shall be available covering
destination of passengers & baggage/freight.
It is permitted to use a manifest produced via a
computer at your installation. But it is of great importance that all of the information found on an official manifest is also found on the computerized version.
6.5.2 The HLO must always check the incoming manifest,
to ensure that the correct number of passengers,
baggage & freight have in fact disembarked from
the helicopter.
3
6.6 R.A.C.I. Chapter 6
Responsible Accountable Consult
Pilot
Inform
1 Loading duties
2 Weight of passengers/baggage/cargo
HLO HLO Radio-
Operator / OIM
Radio-
Operator HLO HLO Pilot
OIM
Pilot
3 Passengers manifest
R = Responsible
A = Accountable
C = Consult
I = Inform
Chapter 6 – Helicopter loading
HLO HLO
Radio-
Operator/OIM
4
Chapter 7
Transportation of special Loads
7.1 Dangerous goods may not be shipped by helicopter unless this shipment has been
authorized by a certified dispatcher. Dangerous cargo may only be transported in accordance with ICAO‟s/IATA‟s regulations. Dangerous goods may only be sent when
accompanied by the form “Shippers Declaration for Dangerous Goods”.
The form must be completed and signed by trained and authorized personnel. Trained and
authorized personnel means personnel with and extended course. For more information, see Appendix 5 Persons responsible for shipping goods on helicopters should be trained to recognize dangerous goods and the classification of dangerous goods i.e.: Class 1. Explosives. Class 2. Gases. (Compressed, liquefied, dissolved
under pressure or deeply refrigerated). Class 3. Flammable liquids. Class 4. Flammable solids. (4,1)
Substances liable to spontaneous combustion (4,2) Dangerous when wet, will emit flammable gases. (4,3)
Class 5. Oxidizing substances. (5,1) Organic peroxides. (5,2)
Class 6. Poisonous toxic substances (6,1) Infectious substance (6,2)
Class 7. Radioactive materials. Class 8. Corrosives. Class 9. Miscellaneous dangerous goods, including magnetic materials
Chapter 7 – Transportation of special loads 2
Chapter 8
Refueling Facilities
8. Introduction All personnel who handle and dispense aviation fuel must understand that the safety of the helicopter and its passengers will depend on their ability to supply the correct grade uncontaminated fuel to the helicopter. Flight safety will depend on the skill and knowledge of the personnel, and their carrying out this task correctly and efficiently at all times. Aviation fuels, equipment and handling methods are continually being developed and improved to meet the ever-increasing demand of the modern helicopter. One thing will never change, that is the vital importance of always supplying the correct grade of uncontaminated fuel to the helicopter
This chapter will deal with: • • • •
The characteristics of the fuel; Quality control checks; Components of the fuel system; Refueling procedures.
8.1 Jet A1 aviation fuel - fuel characteristics The grade of fuel that is normally used by helicopters operating to offshore installations and vessels in the North Sea is “JET A1”. Jet A1 is a petroleum distillation blended from kerosene fractions and manufactured to closely defined specifications (D ENG.RD 2494) All tanks and refueling system components must be correctly marked and labeled as to the type of fuel they contain. There are a number of other turbine fuels in existence, but for helicopter operations in the North Sea, Jet A1 is the type used. Always ensure that only "on grade" JET A1 aviation fuel is delivered to the helicopter, and that the correct administration procedures are carried out at all times.
Fuel Characteristics Jet A1
Chapter 8 – Refuel Facilities
Flash Point
Self Ignition Temperature
Density
Freezing Point
≥38 ºC
200 ºC
775-840 Kg/m3
-47 ºC Max.
2
Chapter 8 – Refuel Facilities
8.2 Fuel Additives 8.2.1 Dye
Other fuels may have a dye added to them to help distinguish them from jet fuels. 8.2.2 Anti static additive
An "anti static additive" (ASA 3) may be added to the Jet A1 fuel to assist the dissipation of static charges, which may build up in the fuel as it is pumped.
8.3 Quality control.
Careful control and good documentation must be maintained on all Jet A1 stocks at each stage of the movement from the refinery to the local storage, and by transportable tank to the offshore installation or vessel. Great care is taken to ensure good quality fuel is delivered to the offshore installation or vessel. Even with this high level of quality control, the fuel will still require special care at all times.
8.3.1 Visual check
This check is a simple field test to confirm the acceptability of the fuel. The fuel is checked visually for appearance / colour, particular contamination, and the presence of free water, and chemically for the presence of suspended water.
Samples for a visual check should be drawn into scrupulously clean, clear glass jars. The standard size is 1 Us gal. The jar is then swirled to create a vortex. Any free water or sediment will tend to concentrate in the bottom of the vortex, making it easier to see.
3
8.3.2 Chemical water detection kits. The Shell Water Detector is currently the most common system in the offshore industry. For this reason the description in this manual is limited to this type
8.4 The Shell water detection kit. 8.4.1 Construction The Shell water detection kit consists of a standard, unbreakable, 5 ml syringe, which is fitted to accept a plastic detector capsule in which contains a yellow, water sensitive paper.
8.4.2 Method of use.
• •
• •
•
Fit the capsule to a closed syringe; Immerse the capsule and approximately half of the syringe into the fuel sample that is to be tested; Withdraw the plunger until the fuel in the syringe reaches the 5 ml mark; Any suspended water in the fuel will collect on the yellow paper, dissolving the dye, thus producing a distinctive color change. A test is said to be positive if there is an observable color change. The capsule should be strongly discolored with as little as 30 ppm of suspended water in the fuel; The portion of the yellow paper that is protected by the plastic moulding will remain unaffected, if there is suspended water in the fuel this will help in giving a clear color comparison.
Chapter 8 – Refuel Facilities
8.4.3 Storage life.
The storage life of the capsules is not longer than 9 months from manufacture. The expiry date is stamped on the side of the box. This expiration date must be strictly observed. Do not use the capsules after the date marked on the tube.
4
8.5 Acceptable fuel
8.5.1 To be acceptable, jet A1 fuel must be: •
•
• •
“Undyed”: the acceptable color may vary from water clear to a light straw color. The presence of any other color may indicate contamination with other fuels, which are “dyed” to aid in identifying them; “Clear and bright”: The phrase is independent of the natural color of the fuel. “Clear” refers to the absence of sediment or emulsion. “Bright” refers to the sparkling appearance of fuel having no cloudiness, fogginess or haze; Free of any particulate matter such as small amounts of rust, dust, scale or fungus; Free from undissolved water.
Phrases used to describe this situation include: • • •
Undyed, clear and bright; Clear, bright and uncontaminated; Clear, bright and free of water.
8.5.2 Action if sample found to be contaminated:
•
•
•
If free water is present in the sample, continue to draw off further samples until all the free water has been drained off; If suspended water is found in the sample, allow a further settling time of 30 minutes per foot (30 cm) of fuel in the tank. At the end of this period re-sample and check if the fuel is still contaminated. Repeat the process once more. If the fuel is still contaminated seal off the tank and return it to the fuel supplier onshore; If dirt or sediment is present in the sample, draw off a further two samples. If these samples are still contaminated seal off the tank and return to the fuel supplier onshore.
Chapter 8 – Refuel Facilities
8.6 Helicopter refueling system.
Typical arrangement of a fuel installation. Each refueling installation as fitted to the different offshore installations and vessels will differ in some way or other, but the operation of the basic components will be the same.
Get to know your own system and be able to name the parts and their function. This is of great importance in faultfinding and in arranging for repairs or spare parts when required.
5
Chapter 8 – Refuel Facilities
8.6.1 Transportable tank
Each installation will have a number of transportable tanks available. There are different types in use ranging from 1900 to 4560 or more litres capacity. A release certificate indicating the quality and quantity of the fuel should accompany each delivery of aviation fuel, by transportable tank, from the supplying company to the offshore installation, or vessel.
Suction hose The suction hose from the tank to the pump is normally made of stainless steel covered by a rubber sheath for protection. The ends of the sheath should be clamped to prevent water build-up in the space between the sheath and the hose or the hose should be positioned in such a way that any water can drain out of this space. Note: All interconnecting pipe work shall be made of stainless steel.
8.6.2 The pump unit
A pump unit contains one, or more, pumps which may be either driven by a compressed air motor or an electric motor.
The pump controls will normally be duplicated in the
refueling cabinet. This allows an emergency shut down capability from both positions.
Typically the capacity of the pump unit should be 200-
250 litres per minute.( 60 Igal.)
8.6.3 Earth proofing unit The pump controls must be coupled to an “earth proofing unit” which is designed to ensure that the fuel system has been electrically bonded to the helicopter before starting the fuel delivery.
6
Chapter 8 – Refuel Facilities
8.6.4 Filter water separator
This is a two-stage filter, designed to ensure a very high degree of cleanliness of the JET A1 fuel. The filter unit is fitted with a "pressure differential gauge" as a method of checking the condition of the filter elements. This pressure must be monitored to ensure that servicing is carried out when required.
8.6.5 The filter monitor
The filter monitor combines filtration and clean up, with the capability to monitor and shut down the refueling system should an unacceptable amount of free water be present in the flowing fuel.
The manufacturer specifies the life limits of the filter elements. Commonly, the limits are 15 psi or 1.1 bar differential pressure or 3 years since manufacture. Any time that a sudden large change in the differential pressure is noted the filters should be re-inspected before further use.
8.6.6 Differential pressure gauges
Filters should always be fitted with a gauge designed to measure the difference in pressure between the upstream and the downstream sides of the filter. Such a gauge can give a global indication of the condition of the filter.
8.6.7 The dispensing cabinet The refueling / dispensing cabinet contains the metering unit, pressure gauges and control switches or levers, also fitted into this cabinet is the hose reel and static earthing reel.
8.6.8 Aviation fuel hoses The hose, which is used to deliver fuel to the helicopter, must meet the specification for aviation hoses for fuel delivery. (BS3158-1985-C) It must not be replaced by any other type of hose that does not conform to the specification. The hose is normally made of rubber with an internal nitril coating
7
Chapter 8 – Refuel Facilities
8.6.9 Gravity nozzle
The “gravity nozzle” is similar to the type used for refueling automobiles. This type of nozzle may be connected directly to the hose, or via an adapter to the pressure coupling. During “gravity refueling”, the fuel is allowed to fall from the nozzle opening into the fuel tank of the helicopter. The combination of high delivery rate and air contact can result in significant amounts of vapor coming free during gravity refueling. To minimize the risks, special care must be taken when gravity refueling to ensure that the bonding connection is correctly made and that no spillage occurs. 8.7 Refueling equipment inspection and
maintenance.
The condition of the refueling system and the transportable tanks is the responsibility of the HLO. He or she must ensure that all items of equipment are inspected and maintained at regular intervals. To ensure that high standards of maintenance are maintained, regulations require independent inspections of all offshore refueling systems to be carried out at 6 monthly intervals (NL).
8
8.8 Summary of routine equipment checks and inspections (example).
Each Company should have a schedule of routine equipment inspections and checks for the refueling system. The following are typical examples of checks, which shall include: 8.8.1 Each day: • • •
• • • •
•
Drain the designated fuel system sumps daily and keep it in store for 24 hours; Transportable tank – ventilate to remove any vacuum. Filter water separator – check for visual damage Filter monitor – sample? Hose end or the clean side of the filter monitor – check for visual damage; Carry out the required quality control checks for contamination of the fuel; Shell Water Detector – available? Measure or calculate the amount of fuel available for use; If possible during the refueling operation, maintain a constant check of the pressure differentials. If there is any sudden change in the readings, the system must be shut down and an investigation made for the cause of the pressure change; If the unit is fitted with two pumps. The pumps must be used alternately each day. This will help to prevent any build up of bacterial growth.
8.8.2 Each week:
Record the pressure differentials across both the
filters. If the pressures are approaching the limits,
arrange for filter replacement. Consult the fuel
system supplier for the filter limits (typically 15 psi).
For pneumatic systems . Check air line lubricant and top
up if required;
Check air lines for pressure and leakage;
For electrical systems. Check the cabling for damage;
Remove any water that may have collected in the
bottom of the cabinets;
Lubricate the roller doors if fitted;
Check the fuel hoses for damage or leaks;
Clean the strainers and hose end filters;
If the unit is fitted with a “hand pump” the pump
must be operated at least once a week, this will help
to prevent the build up of bacterial growth.
Chapter 8 – Refuel Facilities
9
8.8.3 Weekly hose check.
The weekly hose check shall be carried out in the following way: • • • • •
•
Fully extend the hose and apply full pump pressure; Form a loop in the hose so it can be walked along for inspection; Inspect the hose for damage, soft areas, cracking, blistering and leaks; Pay particular attention to the first and the last 2 meters, also checking the coupling.; Check the end couplings for slippage and Misalignment; Clean and check the hose end filters.
8.8.4 Each month.
Each month the following inspection and maintenance checks must be carried out:
•
• • • • •
•
Remove the strainer and clean with JET A1 fuel;
Grease the fuel pump if required; Check the pump unit for leakage; Clean the air line moisture trap; Top up the air line lubricator if fitted; For electrical units check cables and junction boxes; Check the bonding jumpers along the fixed piping for corrosion.
8.8.5 Upon receipt of a transportable tank •
•
•
Each "transportable fuel tank" must be inspected for damage and for contamination of the fuel; The contamination checks must be carried out after the required "settling time" has been observed; Settling time is 1 hour for each 30 cm of fuel in the tank with a minimum of 2 hours.
Chapter 8 – Refuel Facilities
8.8.6 Recording of the checks and inspections
After carrying out the above checks and inspections, record the results in the fuel system administration, and make it available on request to the fuel system inspector. The form "Daily fuel quality check and delivery coupon" must be completed and available for inspection at all times. A member of the helicopter crew as a method of confirming that the required checks have been carried out must also sign the form.
10
8.9 Helicopter refueling procedures
8.9.1 The refueling team
At least two persons must be available and briefed, to carry out the refueling operation. The team will then consist of: •
•
•
The HLO who is in charge of all the operations on the helideck, and is responsible for the fuel quality checks, and the co-ordination with the helicopter crew; Attendant No 1.- “The refueller”, carries out the actual refueling on instructions from the HLO. Controls the hose end, and bonding cable. Attendant No 2.- “The refueling system operator”, controls the pump and monitors system instruments. A member of the fire team/ rescue crew may carry out this function provided the person has also quick access to the fire fighting system controls.
Chapter 8 – Refuel Facilities
A hand held powder extinguisher (normally 9 kg) shall be available close to the refueling position of the helicopter. The pilot will pass on information regarding the fuel requirements of the helicopter to the Radio Operator during the approach to the installation or vessel. During refueling communication between pilot, HLO and HDA are with hand signals. Note 1: See Appendix 7 for refueling points of various helicopters Note 2: Do not refuel during thunderstorm activity.
11
Chapter 8 – Refuel Facilities
8.9.2 Duties of the HLO during the refueling.
A. The HLO is in charge of all helicopter refueling
operations. He should position himself where he
can see the pilot, the refueling system operator
and the refueller; Note: The best place would be near the entrance/stairway to the helideck B. Immediately before refueling, takes a hose end sample in the presence of a crewmember. If
pressure refueling is used, a sample may be taken from the clean side of the filter monitor; C. During the refueling he ensures that the operation is carried out in a safe and efficient manner, checking items such as correct bonding and the use of "safe routes"; D. On the completion of refueling, checks the fuel caps; E. Takes a hose end sample to confirm the quality of the fuel loaded; F. Completes the "Daily fuel quality check and delivery coupon”. Records the amount of fuel loaded, signs the daily log sheet and presents it to a member of the helicopter crew for signature; G. After a member of the helicopter crew has signed the coupon, checks that all refueling equipment has been cleared from the helideck. 8.9.3 Duties of Attendant no 1 – the refueller
A. On instructions from the HLO connects the bonding cable to the designated earthing point on the helicopter; B. After the "hose end sample" has been taken, runs the refueling hose out to the helicopter, connects the nozzle bonding wire to the correct point on the helicopter, opens the tank cap and places the nozzle in the tank; C. On the signal from the HLO commences the refueling; D. On a signal from the HLO, stops refueling – see also chapter 10; E. Removes the refueling nozzle, closes the tank cap, removes the nozzle bonding lead and rewinds the hose; F. On instructions from the HLO, he disconnects the main bonding cable and rewinds it.
12
Chapter 8 – Refuel Facilities
8.9.4 Duties of Attendant no 2 – the refueling system operator
A. Starts and stops the refueling pump on a signal
from the HLO; B. Monitors the differential pressures across the
filters during refueling, and records them on the "daily fuel quality checks and delivery coupon";
C. In the event of any sudden changes in differential pressure, stops refueling;
D. Stands by to shut down the system, if so required.
8.9.5 Duties of the Fire and Rescue team
Depending on the equipment or layout of the helideck it may be necessary to have extra personnel to man the fire fighting equipment during refueling operations to ensure that delay time is minimized in the event of a fire.
A. Acts quickly and efficiently following the
instruction of the HLO according to the fire fighting procedures;
B. Always use the safe areas when refueling; C. Extra personnel must be available in storm
Conditions; D. Always use the correct bonding procedures; E. Always roll up the refueling hose and stow in
the correct manner; F. Know your escape route; G. Refueling is prohibited in case of lightning.
8.10 Refueling with passengers on board the
helicopter Refueling with passengers on board the helicopter is allowed by some offshore operators. If this is the case the refueling section of chapter 10 applies. .
8.11 Fuel spills
In the event of a fuel spill, whether on the airport ramp or an offshore installation, each spill will have to be treated as an individual case because of such variables as size of the spill, type of liquid involved, wind and weather conditions, aircraft occupancy, equipment and personnel available. Within the confines of every fuel spill, there is an area where fuel and air may form an explosive mixture. The only element necessary to produce ignition is a spark. Every spill, no matter how small, shall be treated as a potential fire source.
13
Chapter 8 – Refuel Facilities
8.11.1 Fuel spills less than 0,5 meter in any direction
Usually fuel spills of this nature are considered minor. They can be spread and left to evaporate or can be cleaned up with absorbent cleaning agents, depending on the particular situation. Try to avoid sparks or sources of ignition within 15 meter until the fuel is evaporated or cleaned up.
8.11.2 Spills over 0,5 meter but under 3 meter in any direction and not continuous flowing:
If the fuel spill is within 15 meter of an aircraft, or in an area of high hazard, post a fireguard up-wind of the spill with adequate fire extinguishing equipment at hand. One 45 kg dry powder extinguisher is the minimum required. Avoid sparks or sources of ignition within 15 meter until the spilled fuel is made safe for cleaning up. The fuel spill should be cleaned up with absorbent cleaning agents. 8.11.3 Spills over 3 meter in any direction or
continuous flowing: If the spill is within 15 meter of an aircraft, evacuate the passengers and crew. Post a fireguard up-wind of the spill with adequate fire extinguishing equipment on hand (45 kg dry powder). Neither an idling aircraft, nor any idling automotive, electrical, nor spark producing equipment in the area shall be started before the spilled fuel is removed. The fuel spill can be cleaned up with absorbent cleaning agents. A good safety practice is to not to activate any electrical switches unless absolutely necessary. Fuel soaked absorbents should be placed in a closed metal container and then removed to a safe area. Local regulations will determine the final disposition of these absorbents.
14
8.12 R.A.C.I. Chapter 8
Responsible Accountable Consult
Inform
1 Characteristics of fuel
2 Quality control checks
3 Components of the fuel system
HLO
HLO
HLO
HLO / Pilot Pilot / OIM
HLO / Pilot Pilot / OIM
HLO / Pilot Pilot / OIM
Pilot
Pilot
Pilot
4 Refueling procedures
5 Fuel spills
R = Responsible
A= Accountable
C = Consult
I= Inform
Chapter 8 – Refuel Facilities
HLO / Pilot HLO / Pilot
HLO / HDA HLO / HDA
Pilot
Pilot
Pilot
Pilot / OIM
15
Chapter 9
Helicopters Frequently Used
Eurocopter AS332L Super Puma Technical Specification
3.75m
12ft 4in HELICOPTER SERVICES
5.26m
17ft 3in
16.25m
53ft 4in
18.73m
61ft 5in
3.36m
11ft
15.08m
49ft 6in dia
Engine type
Maximum take-off weight (MTOW)
(Heavy lift operations)
Empty weight, offshore equipped (average)
Passenger seating configuration
Standard fuel tank capacity
Fuel consumption
Normal cruise speed
Maximum range, standard tanks
Maximum range, auxiliary tanks
Maximum hook load
The maximum weight in the tail compartment
is 55 kg‟s. This must not be exceeded. 3.00m
4.87m
16ft
2 x Turbomeca Makila 1A
8600kgs
9350kgs
5475kgs
18
1846kgs
480kgs/h 1020lbs 580l
130kts
460nm
595nm
4500kgs
AS332L.02/SC 19 JAN 2000
9ft 10in Above performance based on 1000ft ASL, ISA, still air conditions.
Range calculated with IFR reserves.
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g l
oad
fac
ilit
y (
26
ft/8
m l
on
g)
•
In
clin
ed r
ear
seat
bac
ks
Sa
fety
fea
ture
s •
E
mer
gen
cy f
lota
tion s
yst
em
•
Str
ong w
ind k
it (
roto
rs e
ngag
e up t
o 5
5kts
for
routi
ne
oper
atio
ns)
•
Full
win
dsh
ield
and f
uel
de-i
cing s
yst
em
•
Ice
det
ecti
on s
yst
em
•
Dual
14 m
an e
xte
rnal
ly m
ou
nte
d l
ifera
fts
(ea
ch w
ith 2
1 m
an o
ver
load
cap
acit
y)
•
Four
sear
ch a
nd r
escu
e bea
cons
(SA
RB
Es)
•
Em
ergen
cy l
oca
tor
bea
con
•
Ici
ng p
rote
ctio
n
•
Hel
icopte
r em
ergen
cy e
gre
ss l
ighti
ng (
HE
EL
)
•
Auto
mat
ic h
eigh
t voic
e al
erti
ng d
evic
e (A
VA
D)
•
Auto
mat
ical
ly d
eplo
yab
le e
mer
gency
loca
tion t
ransm
itte
r (A
DE
LT
)
•
Hig
h v
isib
ilit
y w
hit
e st
robe
coll
isio
n a
vo
idan
ce l
ights
•
Cock
pit
voic
e fl
igh
t dat
a re
cord
er (
CV
FD
R/I
HU
MS
)
•
Auto
nom
ous
seco
ndar
y P
A s
yst
em
AS
33
2L
.03
/SC
1
9 J
AN
20
00
Euro
copte
r A
S332L
Super
Pum
a
Sp
ecif
icat
ion
Sikorsky S61N Technical Specifications
18.90m
62ft
3.73m
3.14m
10ft 4in
5.76m
18ft 10in
2.59m
12ft 3in
5.36m
17ft 7in
HELICOPTER SER VICES
7.16m
23ft 6in
15.03m
49ft 4in
20.95m
68ft 9in
Engine type
Maximum take-off weight (MTOW)
Zero fuel weight
Passenger seating configuration
Standard fuel tank capacity
Auxiliary fuel tank capacity
CT58-
20,500 lbs
15,373 lbs
22
4200 lbs
1100 lbs
8ft 6in
3.64m
11ft 11in
2.32m
7ft 1in
Fuel consumption, fast cruise
Fuel consumption, best range
Fast cruise speed
Best range speed
Maximum range, standard tanks
Maximum range, auxiliary tanks
Maximum hook load
1100 lbs/hr
1050 lbs/hr
120kts
115kts
370
478
8000 lbs
S61N.02 19 JAN 2000
Above performance based on 1000ft ASL, ISA, still air conditions.
Sikorsky S61N Seating/Cargo Layouts 21 seat
configuration
Cargo Door
Liferaft
Cargo configuration
1.98m
6ft 6in
S61N.04 19 JAN 2000
Airstair Door
9.72m
31ft 11in
Liferaft
SERVICES
HELICOPTER
Sikorsky S76A+ Technical Specification 2.46m
8ft 0.8in HELICOPTER SERVICES
5m
16ft 5in
2.13m
7ft
Engine type
16m
52ft 6in
13.41m
44ft
2.31m
8ft 3in
13.22m
43ft 4in
2 x Turbomeca Arriel 1s
2.44m
8ft
4.41m
14ft 6in
1.98m
6ft 6in
3.05m
10ft
3.58m
11ft 9in
Maximum take-off weight (MTOW)
Empty weight, offshore equipped (average)
Passenger seating configuration
Standard fuel tank capacity
Auxiliary fuel tank capacity (boot)
Fuel consumption
Normal cruise speed
Maximum range, standard tanks
Maximum range, auxiliary tank
Maximum hook load
10,800lbs
7100lbs
12
1830lbs
350lbs
630lbs/hr
140kts
360nm
430nm
3300lbs
S76A+.02/SC 19 JAN 2000
Above performance based on 1000ft ASL, ISA, still air conditions.
Range calculated with IFR reserves
S7
6A
+.0
3 1
9 J
AN
20
00
Sik
ors
ky S
76A
+
Spec
ific
atio
n
Safe
ty f
ea
tures
•
Em
ergen
cy
flo
tati
on
sy
stem
•
Dual
10 m
an l
ifer
afts
(ea
ch w
iht
15
man
ov
erlo
ad c
apac
ity)
•
Dual
din
gh
y d
eplo
ym
ent
syst
em,
wit
h d
oo
r je
ttis
on
•
Cab
in e
mer
gen
cy u
nd
erw
ater
esca
pe
lighti
ng (
EX
IS)
•
Thre
e se
arch
an
d r
escu
e b
eaco
ns
(SA
RB
Es)
•
Sonic
lo
cato
r b
eaco
ns
•
Au
tom
atic
ally
dep
loy
able
em
ergency
loca
tion t
ransm
itte
r (A
DE
LT
)
•
Auto
mat
ic h
eig
ht
vo
ice
aler
ting d
evic
e (A
VA
D)
•
Hig
h v
isib
ilit
y w
hit
e st
rob
e co
llis
ion a
vo
idan
ce l
ights
•
Engin
e ic
e/sn
ow
pro
tect
ion
•
Cock
pit
vo
ice
flig
ht
dat
a re
cord
er (
CV
FD
R/I
HU
MS
)
•
Addit
ion
al p
asse
ng
er e
mer
gen
cy p
ush
-out
win
dow
s
Gen
era
l fe
atu
res
•
33
00
lbs
carg
o h
oo
k
•
Tw
o l
and
ing
lig
hts
(o
ne
mo
vab
le)
•
Au
xil
iary
fu
el t
ank
(o
pti
on
al)
Pass
en
ger a
nd
freig
ht
fea
tures
•
12 p
asse
nger
com
fort
sea
ts
•
Cab
in h
eati
ng a
nd v
enti
lati
on s
yst
em
•
Cab
in p
ubli
c ad
dre
ss s
yst
em
•
Air
line
trim
and a
ddit
ional
soundpro
ofi
ng
•
Quic
k-r
elea
se p
asse
nger
sea
ts (
for
frei
gh
t oper
atio
ns)
•
Lar
ge
rear
bag
gag
e bay
(w
ith t
wo d
oors
fo
r ea
se o
f lo
adin
g)
•
Four
doo
rs e
nsu
ring r
apid
and u
nre
stri
cted
pas
senger
acc
ess
•
Wid
e ac
cess
into
cab
in f
or
frei
ght
•
Lar
ge
win
dow
s giv
ing a
ll-r
ound v
isib
ilit
y
H
EL
IC
O
PT
ER
SE
R
VIC
ES
Augusta Westland AW 139
Engine type 2 x Pratt&Whitney PT6C-67C (1679 hp)
MTOW 6400 kg
Empty Weight, offshore
equipped (average)
4400kg
Passenger seating
configuration
12
fuel tank capacity 1650 kg
fuel consumption 410 kg/h
Normal cruise speed 145 mph
Maximum range 550 nm
AB139 Safety features
Emergency Flotation System
Dual 11 man liferaft (each with 17 man overload capacity)
Dual liferaft deployment system
2 external emergency lights
Helicopter Emergency Egress Lighting (HEEL)
Emergency Locator Transmittor (ELT)
CPI (Crash Position Indicator)
AVAD
High Visibility White strobe collision avoidance lights
Cockpit voice data recorder HUMS
All windows Push-out / Push-in
4 point seatbelts
Passenger and freight features
12 passengers confort seats
Cabin heating and ventilation system
Cabin public address system
Additional soundproofing
Individual lighting and ventilation system
Big slidingdoors (2) for passengers entrance
Large windows
Large rear baggage compartment (with 2 doors for ease of loading)
Smoke detection in bagage compartiment
Max. 300 kg freight in compartment
General features
5 main rotor blades
1 point gravity refueling
2 movable landing lights
Eurocopter EC 155 B1
Engine type 2 x Turbomeca Arriel 2C (935 hp)
MTOW 4950 kg
Empty Weight, offshore equipped (average) 3294 kg
Passenger seating configuration 10
fuel tank capacity 1011 kg
fuel consumption 320 kg/h
Normal cruise speed 155 mph
Maximum range 430 nm
EC155 B1 Safety features
Emergency Flotation System
Dual 10 man liferaft (each with 15 man overload capacity)
Dual liferaft deployment system ?
2 external emergency lights
Helicopter Emergency Egress Lighting (HEEL)
Emergency Locator Transmittor (ELT)
CPI (Crash Position Indicator)
AVAD
High Visibility White strobe collision avoidance lights
Cockpit voice data recorder HUMS
All windows Push-out / Push-in
2 pilot doors are jettison type
4 point seatbelts for passengers
5 point seatbelt for pilots
Passenger and freight features
10 passengers confort seats
Cabin heating and ventilation system
Cabin public address system
Additional soundproofing
Individual ventilation system
2 big slidingdoors for passengers entrance
Large windows
Large rear baggage compartment (with 2 doors for ease of loading)
Smoke detection in bagage compartiment
Fire extinghuiser in bagage compartiment
Max. 300 kg freight in compartment
General Features
5 main rotor blades
1 side gravity refueling
2 movable landing lights
Chapter 10
Company Specific Requirement
Subject: Hand Signal “Almost Full” During Refueling
Reason: In response to questions arising out of a fuel spillage on a offshore helideck.
Information: When filling the tanks of the helicopter completely, the rate at which the level of fuel rises
may increase unexpectedly as the level of fuel in the tank approaches maximum. This is particularly so in the case of the S76 models. Because of a time lag in the fuel gauges in the
instrument panel it is difficult for the pilot to see that the tank is full until it is too late. With the EC 155 there is a similar issue. If refueling is stopped rapidly, there may be blow-back from the aircraft fuel system.
Hand Signal: In an effort to prevent fuel spills offshore the pilot will endeavour to give a warning that the
tank is approaching the critical level. He will do this by giving a hand signal as illustrated below: stretched thumb and forefinger in a pinching movement to indicate “a little bit more” or “almost full”. When the signal is given the refueller should reduce the flowrate.
Offshore
a) Fuel samples shall be taken before and after refueling (offshore only), to be checked for
presence of dirt or water; The Shell water detector-kit is recommended to be used to check the fuel for presence of water, no colour change from yellow or spots are
acceptable; b) A portable fire extinguisher shall be available and manned at the refueling side of the
helicopter; c) After refueling the HLO/Flight Attendant shall check that all fuel tanks have been properly
closed and all grounding wires are removed, in the absence of a flight attendant the
Commander must positively confirm with the HLO that the fuel caps are secure. This positive check shall be done by a radio-call from the flight crew to the HLO “HLO –
conform (both) fuel caps are closed”. The HLO may reply with a radio-call or positive thumbs up signal. If there is the slightest doubt as to the security of the fuel filler caps
then a crew member must visually inspect them ;
d) A crew member shall sign for the amount of fuel received and check that the amount stated on the receipt corresponds with the added amount derived from the fuel indicators.
e) In order to prevent damaging of antenna's and other exterior parts, it is not permitted to pass the fuel hose below the tail boom fuselage of the helicopter from one side to another.
Helicopter Refueling with Passengers on board
When there are no limitations on helicopter refueling, it is routine that the helicopter pilot will indicate in his first communications with the Radio Operator of the offshore installation that he
wants to refuel.
The Radio Operator informs the HLO who will in turn inform and instruct the team about the request and discuss the roles depending on the wind directions and expected helicopter position
prior to the arrival of the helicopter.
The sequence of activities will be as follows:
1. The handling of passengers who have just arrived and their luggage. Transit passengers
(and their luggage) will remain in their seat; Passengers are to be briefed to remain seated, but with seat belts/harnesses
unfastened, until refueling has been completed;
Door(s) on the refueling side of the helicopter shall remain closed but unlocked, where
possible; Door(s) on the non-refueling side of the helicopter shall remain open, weather
permitting; (hinged doors unlocked, sliding doors slightly opened);
Sufficient qualified personnel shall be immediately available to move passengers clear of
the helicopter in the event of a fire;
Provision is made for a safe and rapid evacuation;
The ground area beneath the exits intended for emergency evacuation must be kept
clear. 2. Refueling of the helicopter;
If the presence of fuel vapour is detected inside the helicopter, or any other hazard
arises during refueling, fuelling must be stopped immediately. 3. The handling of passengers who are departing and their luggage will only be done when
refuelling has been completed..
During refueling no other activities will take place around the Helideck.
Chapter 11
Appendixes
APPENDIX 1
EXAMPLE OF HELIDECK EQUIPMENT WEEKLY CHECKLIST
Helideck Equipment Record
Weekly Check Form
GENERAL Yes No
1. Helideck clean and free from debris. Drains clear.
2. Landing net in good condition and correctly tensioned (if applicable).
3. Deck-edge safety net in good condition.
4. All helideck perimeter lights and floodlights operational.
5. Helideck correctly marked and paintwork in good condition.
6. Ground power unit operational.
7. Refueling system operational.
8. Pump running warning light operational
9. Fuel test equipment in adequate supply.
10. Wheel chocks and tiedown strops available.
EMERGENCY EQUIPMENT
11. Emergency equipment box in good condition.
12. Aircraft type rescue axe.
13. Safety knife, aircraft type (for each crew member).
14. Heavy duty hacksaw c/w 6 spare blades.
15. Crow bar (large).
16. Grab/boat hook.
17. Lifting strop, aircraft type
18. Tin snip.
19. Bolt cutters.
20. ladder.
21. Fire resistant blanket.
FIREFIGHTING EQUIPMENT
22. 45kg dry powder extinguisher including 100% back-up - serviceable.
23. 20 kg CO2 extinguisher c/w lance including 100% back-up - serviceable.
24. Branch/nozzle available and in good condition.
Platform:
Date:
REMARKS
All enumerated items should be visually inspected and checked daily, though the form should only be completed once a week.
Additional Remarks
Original (White) - Installation Supervisor / Copy (Blue) - Helideck Records Book
Helicopter Landing Officer Signature
Installation Supervisor Signature
Appendix 2
2 Miscellaneous X
2,1 • Manuals HCA
5.11
Company Emergency response manual
ICAO Annex 14 with supl. Heliport Manual
HLO handbook (training manual)
Dangerous Goods Regulations Manual
2,2 • Helicopter emergency diagrams CHC
• Helicopter Types
• Dangerous Goods
• Other Safety Posters
• Location
2,3 • Passenger briefing equipment HCA
• Type
• Location
2,4 • Scales for baggage and freight 6.9.1
• Type
• Max weight, (lbs/kg)
• Calibration date
• Procedures
3 Radio Equipment X
3,1 • VHF Main 6. 9. 4
• Call sign
• Location
• Quantity
• Approval
• Details:
• Connected to emergency supply/ups
3,2 • VHF Portable 6.9.4
• HLO
• HDA
3,3 • NDB (Not for NL, see toelichting art 16 RBML) 6.9.4
• Approval
• Ident
• Frequency
• Details
3,4 • Radio Log
Record of Departure /Position Reports
(Passenger & Freight manifest).
HCA
4 Meteorological Equipment X
4,1 • Anemometer's 6.4.2.1
• Location
• Calibration date & report every 18
months
KNM I
• In clear air
• Handheld backup
4,2 • Air Temp location 6.4.2
4,3 • Barometer 6.4.2
• Location of sensor relative to helideck level
• Calibration date & report every 18
months
KNM I
4,4 • Visibility, cloud base & cover
• Details of equipment, if available
6.4.2
4,5 • Sea State
• Details of equipment, if available
6.4.2
4. 6 • Location of readouts
• Can the Radio Operator readily refer to all
weather information
HCA
5 Helideck Equipment X
5,1 • Chocks 6.9.1
5,2 • Tie dow n straps/ropes 6.9.1
• Type
• Quantity
5,3 • Helicopter start unit 6.9.1
• Type / Voltage
• Location
• Can lead reach aircraft in any position
5,4 • Snow /ice clearing equipment 6.9.1
5,5 • Prohibited Landing Marker
• 4 x 4m red flag with diagonal yellow cross
4.2.10
5,6 • Windsock 5.1.1
HM 5.2.1
4.1.5
• Location(s)
• Condition
• Illumination 5.1.1.7
• In clear air 5.1.1.2
• Spare windsock
5,7 • Bird deterrent device
6 Helideck Surface X
6,1 • Colour (Green) 4.2.1
6,2 • Condition, paint & cleanliness
6,3 • Non slip characteristic - estimate HM 2.3.1.8 3. 7. 1
6,4 • Last friction test date and result 3. 7. 5
6,5 • Gutter or raised curb HM 2.3.1.9 3. 7. 2
6,6 • Drainage 3.7.2
• Slope HM 2.3.1.9
• Number of down pipes
• Debris filter fitted
6,8 • Aircraft tie dow n points HM 2.3.1.13 3.8.1 & 2
• Location
• Quantity/Pattern
• Flush
• Bar diameter
• Condition
7 Helideck Dimensions X
7,1 • Landing Area dimensions 3.6.1
7,2 • Run off area dimensions
8 Helideck Markings X
8,1 • Name 5.2.9 4.1.3
4.2.1 .1
• Name painted on deck name
• Height (1,20 meter) 5.2.9.4
• Colour (white)
• Position
• Proportions
• Outlined (Alum. Decks only)
• Other names on deck
8,2 • Perimeter Line fig 5.5 4.2.1
• Colour (white)
• Width (0,30 meter)
• Location
8,3 • Aiming Circle 4.2.6
• Colour (yellow) 5.2.8.4
• Width (1meter) 5.2.8.4
• Inner diameter (0.5D) 5.2.8.5
• Location 5.2.8.3
8,4 • Chevron fig 5.5 4.2.2
• Length of arms (0,79 meter)
• Colour (black)
• Angle
• Swung (max = +/- 15°)
• Location
8,5 • D Value fig 5.5 4.2.3
• Declared 'D' value 5.2.10.3
• Height (0,10 meter)
• Colour (black) 5.2.10.5
• Location
8,6 • Perimeter ‘D’ value fig 5.5 4.2.4
• Value
• Quantity (3)
• Colour (white)
• Height (0,60)
• Location
• Orientation
8,7 • ‘H’ 5.2.2.3 4.2.7
• Size
• Location [Concentric with aiming circle]
• Orientation // with bisector
• Swung (max = +/- 15°)
8,8 • Maximum allow able mass 5.2.3 4.2.5
• "t" Value
• Does this agree with the design value
• Size (0,90 meter)
• Colour (white)
• Location
8,9 • Prohibited landing sector 4.2.9
• Location
• Angle (45°)
• Colours (red / white)
• Reason
9Helideck Net
XHM 2.3.1.11
9,1 • Material 3.7.3
9,2 • Type 3.7.3
9,3 • Condition
9,4 • Coverage 3.7.3
• Covers aiming circle
• Obscures: name
• Obscures: t value
9,5 • Rope diameter - 20mm 3.7.3
9,6 • Mesh size -200mm 3.7.3
9,7 • Net size 3.7.4
9,8 • Tension - 2225N (Lift .+0.25m) 3.7.3
9,9 • Tie dow n points - every 1.5m 3.7.3
9. 10 • Methods of securing
10 Perimeter Net X HM 1.4.4
10,1 • Material 3.9.1
10,2 • Width from deck edge - 1.5m 3.9.1
10,3 • Condition - securely attached 3.9.1
10,4 • Detailed visual inspection 3.9.1
10,5 • Hammock effect 3.9.2
10,6 • Slope - 10° (250mm adl) 3.9.1
10,7 • Covers drop dow n areas 3.9.1
11 Access X
11,1 • Locations - suitability HM 1.4.4.4 3.10.1
11,2 • Handrails HM 1.4.4.5 3.10.5
• Fixed/Foldable
• Height
• Conspicuous
11,3 • Safety notices - applicability HCA
11,4 • Access restriction system HCA
12 Turbulence X
12,1 • Structures HM 1.4.1.1 3.2.1
12,2 • Hot emissions HM 1.4.2
HM 1.4.3
3.2.1
12,3 • Cold emissions 3.2.1
12,4 • Air Gap beneath deck HM 1.4.2.2
13 Obstruction Environment X
13,1 • OFS (210º) HM 3.2.3.4 3.6.2
• State items, location and height above
deck level from SLA
13.2.1 • LOS (1 x 150º) HM 3.2.3.9 3.6.4
• From edge of Landing Area to 0.12D
(maximum 25 cm)
• From 0.12 to 0.33D with a 1:2
slope
13.2.2 • LOS (2 x 150°) ships only
• From edge of Landing Area to 1.0 'D' with a
1:5 slope.
9.2.2
13,3 • 180° 5:1- 3:1 falling gradient obstructions
• State items, locations, distance from the
edge of netting and height below deck level
HM 3.2.3.5 3.6.8
13,4 • Landing Area - Maximum 25mm HM 3.2.3.4 3.6.3
13,4 • Temporary items
• e.g. Flare booms, Seismic booms which
may infringe protected surfaces.
14Perimeter Lights X 5.3.8
fig 5.9
14,1 • Colour (green) 4.3.1
14,2 • Type
14,3 • Serviceability 4.3.1
• All working
• Brightness
• Condition of lens
14,4 • Position and height 3.6.1
• Location 5.3.8.5
• Height <250mm
• Distance <3m 5.3.8.6
14,5 • Connected to emergency / ups 4.3.12
14,6 • Sw itching 4.3.8
14,7 • Limit of safe landing area - red lights 4. 3. 2
15 Floodlights X
15,1 • No. and Type of unit HM 5.2.3.12
15,2 • Brightness / Serviceability 4.3.7
• Illumination
• All working
• Condition of lens
• Dazzle protection
15,3 • Position and height 4.3.7
• Location
• Height <250mm
15,4 • Connected to emergency / ups 4.3. 12
15,5 • Sw itching
16 General Lighting X
16,1 • Installation f loodlighting - dazzle 4.3.7
16,2 • Light pollution 4.3.8
17 Obstruction Marking and Lighting X
17,1 • Structures > 15m above deck level
• Omni directional red lights every 10m adl.
(To include all crane booms near flight path)
HM 5.3.3.13 4.4.3
17,2 • Highest point HM 5.2.3.17 4.4.4
• Omni directional
• Colour
• Intensity
17,3 • Crane colours
17,4 • Misc. - give details
18 Status Lights X
18,1 • Units meet spec 4.3.10
18,2 • Visible from all approach directions
• Quantity and location
4.3.10
18,3 • Connected to emergency / ups 4.3.10
18,4 • Sw itching
• Automatic and manual activation
• Remote reset 4.3.10
18,5 • Hazard level initiation 2.3.5
4.3.10
19 Refuelling Package X
19,1 • General comments only 7,3
20 Fire Fighting equipment X
20,1 • Fixed Monitor System (FMS) HM 6.10b 5.2.3
5.2.8
• Quantity
• Type
20,2 • Delivery ( not less than 6L/min, 5 min. per
square meter w ithin "D")
HM 6.10b 5.2.2
5.2.6.1
• Foam production response time (< 15 sec's)
• Delivery rate (lts/min)
20,3 • Concentrate (Performance level 'B') 5.2.5
5.2.6
HCA• Type
• Percentage
• % (marked on container)
• Capacity of tank
• Quantity in tank
20,4 • Certif icate of Conformity
• Cert. of conformity, test report on
concentrate, water and produced foam
HM 6.3.3 5.3.3
20,5 • Back-up concentrate - quantity 5.2.6
20,6 • Deck Integrated Fire Fighting System
(DIFFS)
5.2.10
• Type
• Time to deliver
• Delivery rate (lts/min)
20,7 • Hydrant points - quantity HM 6.10d 5.2.8
20,8 • Hand lines HM 6.10d 5.2.8
• Quantity
• Jet/spray nozzles
• Location
20,9 • Foam hand branch 5.2.8
• Quantity
• Delivery rate
• Location
20.10 • Foam inductors 5.2.8
5.3.2
• Quantity
• Concentrate – quantity
• Percentage setting
• Connection
• Location
20.11 • Tw in agent units HM 6.10b
• No. and capacity of each unit
• Last test date
• Access to helideck
20.12 • Dry pow der (at least 2 units, total not less
than 45 kg)
HM 6.10a 5.4.2
• No. and capacity of each unit
• Last test date
• Access to helideck
20.13 • CO2 (not less than 18 kg) HM 6.10c 5.4.3
• No. and capacity of each unit
• Suitable Applicator
• Last test date
• Access to helideck
20.14 • Back-up DP and CO2 HM 6.6.1
21 Rescue Equipment X HM 6.9
21,1 • Rescue Equipment boxes
• Location (s)
• Quantity
• Condition & Layout
• Lighting
• Accessibility from all access points
21,2 • Check list 5.7.3
21,3 • Adjustable w rench 5.7.2
21,4 • Large rescue axe 5.7.2
21,5 • Bolt cutters 5.7.2
21,6 • Large crow bar 5.7.2
21,7 • Grab or salving hook 5.7.2
21,8 • Heavy duty hacksaw 5.7.2
21,9 • Heavy duty blades 5.7.2
21.10 • Fire resistant blanket 5.7.2
21,11 • Ladder 5.7.2
21,12 • Life-line/rescue harness 5.7.2
21,13 • Tin snips 5.7.2
21,14 • Set of assorted screw drivers 5.7.2
21,15 • Harness knife c/w sheath
• 1 per deck crew
5.7.2
21,16 • Breathing Apparatus sets 5.9.3
5.9.4
• Quantity
• Location
21,17 • Portable safety lamp
• Quantity, location
• Operating life
22 Protective Clothing X HM 6.1.10
22,1 • Stow age type 5,9
• Condition
• Location
22,2 • HLO vest; on front and back 5.8.1
22,3 • Helmet w ith visor 5.9.1
HCA
• Quantity
• Type
• Code (EN443/BS3864)
• Condition
22,5 • Gloves 5.9.1
HCA
• Quantity
• Type
• Code (EN659)
• Condition
22,6 • Boots 5.9.1
HCA
• Quantity
• Type
• Code (EN345/BS1870)
• Condition
22,7 • Fire suit 5.9.1
HCA
• Quantity
• Type
• Code (EN469/BS6249)
• Condition
Supervise helicopter
landing and departure
Prepare for helicopter Prepare for helicopter
landing departure
Brief helideck crew Brief helideck crew
HLO Control Offshore Helideck Routine Operations
Control Offshore
Routine Operations Supervise cargo
handling
Supervise loading and
Co-ordinate preparation unloading passengers,
of freight baggage and freights
Confirm suitability Confirm helicopter is safe to approach
of freight
Prepare for refueling Ensure refueling
systems and equipment
are serviceable
Supervise the refueling
of the helicopter
Refuel the helicopter
Make the helicopter safe
Shutdown refueling
process
Monitor shutdown
sequence and inform appropriate people
Confirm equipment status
Inform appropriate people
of impending operations
and maintain
communications
Helideck area equipment
is manned and
operational
Conduct communication
with helicopter pilot
Take corrective action
Appropriate manner:
With authority and clarity
Procedures:
PPE, crew briefings, full
equipment confirmation,
communications,
loading, helideck
equipment
Communications
Personal radio, vocal,
visual
Appropriate persons:
OIM, RO, helideck
crews,
standby vessel officer,
crane operator
Impending operations:
Helicopter landing and
on deck, vessel or crane
movements, weather,
deck and airspace is
clear
Confirm equipment status
Inform appropriate people
of impending operations
and maintain
communications
Secure and stow
helicopter equipment
Secure and stow
helideck equipment
Rescue and firefighting
equipment is manned and
operational
Communicate departure
clearance
Conduct work safely
Crew briefings:
Equipment security and
stowage, safe working
practices, departure
clearance
Communication
manner:
With authority and clarity
Appropriate persons:
OIM, RO, helideck
crews, standby vessel
officer, passengers,
helicopter crew, crane
operator
Communication
methods:
PA system, telephone,
personal radio, vocal,
group meeting
Helideck equipment:
Chocks, fire
extinguishers, baggage
trolley, external power
Impending operations:
Helicopter on-deck,
cabin restrictions,
weather, deck and
airspace is clear, vessel
or crane movements
Move freight to
helideck area
Complete loading
preparations and notify
appropriate people
Move freight to helicopter
Loading preparations:
Manifest, freight,
personnel
Suitability: Cleanliness,
leakproof, labelling and
packaging, manifest,
load spreading, floor
loading, dangerous
cargo, radioactive,
magnetic
Freight:Large, small,
long
Procedures:
Manual handling,
mechanical handling
COSHH loading
Transfer manifests
Offload baggage
Disembark passengers
Offload freight
Load freight
Embark passengers
Stow baggage
Procedures:
Advising helicopter pilot,
confirming helicopter
safety, cargo,
passengers on helideck,
data collection and
processing, safe working
practices, manual
handling, loading and
unloading
Communications:
Radio, visual
Actual / Potential
conflicts:
Weather conditions, rotor
hazards
Passenger PPE:
Survival suit, lifejacket,
hearing protection
Conduct quality checks
Establish aircraft
requirements and notify
appropriate people
Deploy firefighting
arrangements
Record data and forward
to appropriate people
Monitor operations
Take corrective actions
where necessary
Record data and forward
to appropriate people
Equipment:
PPE
Procedures:
Helicopter bonding and
refueling, refueling
systems and equipment,
aircraft requirements,
quality checks, safe
working practices
Corrective action:
Spillage
Aircraft requirements:
Gravity, pressure,
quantity
Quality checks:
Fuel samples
Monitoring:
Differential pressure,
delivery pressure,
quantity
Stow equipment
Record data and forward
to appropriate people Conduct work safely
Procedures:
Equipment shutdown
sequence, equipment
storage, refueling hose
and bonding lead, data
collection and processing
safe working practices
Equipment:
Refueling package -
nozzle, hose bonding,
lead, fuel caps
Equipment storage:
Refueling hose and
bonding lead
Data:
Written, from meter on
system
Data accuracy limits:
100%, less than 100%
accuracy
Data collection:
Log sheets
Appropriate persons:
onshore, offshore
Refueling operations:
Bonding lead, refueling
hose removal, fuel caps
Monitoring:
Manual, electronic
EX
AM
PL
E –
Ap
pen
dix
3
Contribute to Routine
Offshore Helideck
Operations
(Helideck Assistant)
Handle Cargo
Refuel
helicopter
Contribute to
helicopter landing
and departure
Assist with the
Preparation for helicopter
landing
Assist with the preparation for
helicopter departure
Assist with the preparation of
freight for loading
Assist with the unloading and
loading of bagage passengers
and freight
Assist with refueling the
helicopter
Assist with the shutdown of
the refueling operation
Assist with the preparation for
refueling
Inform HLO of status of
operation
Inform HLO of status of
equipment
Helideck area equipment is
manned and operated as
instructed
Prompt action is taken when
appropriate
Conduct work safely
Procedures:
Full equipment
confirmation,
communications,
helideck equipment
Equipment manned:
Rescue and firefighting,
chocks, baggage
handling equipment
Communications:
Personal radio, verbal,
visual
Appropriate persons:
HLO, RO, other helideck
crew member, crane
operator
Operations and
Conditions:
Helicopter landing and
on deck, vessel or crane
movements, weather,
deck and airspace is
clear
Working Practices:
Individual operation,
team operation, use of
PPE, use of equipment
Helideck Area
Equipment:
Landing net, lights,
rescue and firefighting,
wind sock, chocks,
baggage handling
equipment, helideck
lifeline
Actual or Potentially
Hazardous Situations:
Fuel leaks, oil leaks, fire,
smoke, abnormal noise,
other abnormalities
Secure and stow helicopter
equipment
Secure helideck equipment
Rescue and firefighting
equipment is manned
Observe helicopter operations
Prompt action is taken when
appropriate
Conduct work safely
Appropriate persons:
HLO, RO, other helideck
crew member, helicopter
crew
Communication:
Telephone, personal
radio, verbal, visual
Helideck equipment:
Chocks, portable fire
extinguishers, baggage
handling equipment,
external power supply
Helicopter Operations
observed:
Helicopter on deck,
weather, deck and
airspace is clear, vessel
or crane movement
Helicopter equipment:
Doors, panels, fuel caps
Working Practices:
Individual operation,
team operation, use of
PPE, use of equipment
Actual or Potentially
Hazardous Situations:
Fuel leaks, oil leaks, fire,
smoke, abnormal noise,
other abnormalities
Move freight to helideck area
Complete loading
preparations
Move freight to helicopter
Deliver food/ refreshments to
helicopter
Prompt action is taken when
appropriate
Conduct work safely
Loading preparations:
Freight, pallets, spreader
boards, loading
equipment
Freight: Large, small,
long, heavy, light, bulky
Procedures:
Manual handling,
mechanical handling,
COSHH loading,
positioning, underslung
loads
Actual or Potentially
Hazardous Situations:
Long items, dangerous
goods
Working Practices:
Individual operation,
team operation, use of
PPE, use of equipment
Offload bagage
Disembark passengers
Offload freight
Prepare helicopter
Load freight
Embark passengers
Stow bagage
Prompt action is taken when
needed
Conduct work safely
Procedures:
Advising HLO,
confirming helicoptersafety, cargo,
passengers on helideck,safe working practices,
manual handling,mechanical handling
loading and unloading
Communications:Visual, verbal
Actual, /Potentialconflicts:Weather
conditions, rotor hazards,underslung andwinching, static
discharge
Passenger PPE:Survival suit, lifejacket,
hearing protection
Working Practices:Individual operation,
team operation, use ofPPE, use of equipment
Confirm refueling systems
and equipment are
serviceable
Conduct quality checks
Receive aircraft requirements
Man fire fighting equipment
Record data and forward to
HLO
Operational
Requirements :
Weather, rotor hazards
Refueling
Requirements:
Quantity, gravity
pressure, filter location
Procedures: Fuel,
sampling and quality
Helicopter is borded
Refuel helicopter and monitor
operations
Take corrective actions where
necessary
Record data and forward to
HLO
Procedures :
Helicopter bonding and
refueling, refuelingsystems and equipment,aircraft requirements,safe working practice
Corrective actions:Spillage, fire, equipment
Malfunction
Aircraft requirements:Gravity, pressure,
Quantity
Monitoring:Differential pressure,
delivery pressure,Quantity
Data:Differential pressure,
delivery pressure,quantity
Conduct quality checks
Shutdown the operation and
inform HLO
Stow equipment
Record data and forward to
HLO
Conduct work safely
Confirm refueling systems
and equipment are
serviceable
Procedures:
Shutdown sequence,
equipment storage,refueling hose, hose endand bonding lead, main
bonding lead, datacollection, safe working
Practices
Equipment storage:Refueling package -nozzle, hose bondingleads, fuel caps, fuelsamples, sampling
Equipment
Data:Written, deliverymeter, totaliser meter,differential pressure
gauges, fuel pressuregauge, dipstick reading
30-9-09
Appendix 2
Control the Response to Offshore
Helideck Emergencies
Prepare for emergencies
Control response to
emergencies
Maintain a state of
readiness
Identify/locate and
operate all relevant
equipment and controls
Conduct emergency
exercises
Identify/locate
operational hazards
hazardous areas and
access
Prepare for helicopter
landing
Prepare to enter the
incident area
Respond to appropriate
alarms
Control the rescue of
personnel
Control the firefighting
operations
Enter the incident area
and work safely
Identify/locate fire
hazards
Identify/locate electrical
hazards
Identify/locate technical
hazards
Fire hazards:
Unignited fuel
Spillage, ignited fuel
Spillage, pyrotechnics
Electrical hazards:
Static electricity
Aircraft electrical system
Technical hazards:
Rotors, flotation device,
hydraulics,
escalation,helicopter
construction
Appropriate persons:
Onshore, offshore
Operate means of
shutting down the engine
Operate helideck fixed
fire systems
Operate helifuel system
control valves
Operate portable fire and
rescue equipment
Procedures:
Aircraft shutdown,
fixed fire systems
(helideck and aircraft)
portable fire and
rescue equipment,
helifuel system
control valves
Helideck fixed fire
systems:
Firewater deluge
valves, inert gas, fire
extinguishing
systems and release
valves, foam system
and release valves,
fire main hydrants
and isolation valves
Portable fire and
rescue equipment:
Hoses, hose reels,
branches, foam,
foam equipment,
extinguishers BA sets
Establish communication
Conduct briefing and
debriefing with helideck
team
Conduct exercises with
helideck team
Record exercise
outcome
Appropriate
people:
OIM/Master, radio
operator, fire team,
company (onshore),
helicopter crew,
emergency helideck
team, fire team,
crane operator,
standby vessel, other
installations, other
Vessels
Lines of
communication:
Command structure
Pre-planned
exercises:
Crash on deck,
emergency/precauti
onary landing, crash
on deck - major
spillage with no fire,
significant fuel
spillage - rotors
running, evacuation
by helicopter, man
overboard, attempted
wheels up landing,
helicopter incident on
landing
Respond to alarms
Report to muster
Procedures:Alarm response,
Muster
Alarms:Bells, klaxon, light,
whistles, siren(continuous/
intermittent), vocal
Monitor environmental
conditions
Brief helideck crew
Confirm equipment status
Inform appropriate
people of impending
operations and maintain
communications
Helideck area equipment is
manned and operational
Conduct communications with
helicopter pilot
Select and wear
appropriate PPE
Select breathing
apparatus
Gain access to incident area
safely
Move through incident area in
a safe & appropriate manner
Maintain a safe means of
escape
Movement:
Upright (BA Shuffle),
crawl,descend/ascend,stairs and ladders
appropriate tohelideck and
associated areas
Circumstances:Smoke, heat,
darkness, poorvisibility, all weather
conditions
Find out if anyone is missing
Locate missing personnel
Rescue personnel
Prioritise and treat casualties
Use to optimum effect fixed
systems
Monitor the effectiveness of
fixed fire fighting systems
Control non firefighting
operations
Take corrective action
Appropriate
manner:
With authority andclarity
Procedures:Crew briefings, full
equipmentconfirmation, comm-unications, helideck
equipmentEquipment: PPE
Communications:Personal radio, vocal,
visualAppropriate
persons:OIM, Radio Operator,
helideck and fireteams, stanby vessel
officer, craneoperator
Impendingoperations:
Helicopter landing ondeck, vessel or cranemovements, weather,deck and airspace is
clear
Use breathing apparatus
Procedures:
PPE, breathing
apparatusoperations, BA
Control
Alarms:Bells, klaxon, lights,
whistles, siren(continuous/
intermittent), vocal
PPE:Fire clothing, boots,helmet and visor,
gloves
Remove casualties to a safe
location
Procedures:
BA search, casualty
treatment, moving
casualties,
equipment, casualty
handling
Missing personnel:
Crew members,
passengers, helideck
team
Appropriate
persons:
Onshore, offshore
Casualty
management:
Treatment of
casualties:
Airway breathing
and circulation,
(ABC)
Resuscitation
Establish breathing
(manually,
automatically)
Cardiac massage
Stop bleeding
(direct, undirect
pressure)
Correct positioning
Reassurance/
comfort
Slings, harnesses,
stretchers, hoists
Equipment:
Slings, harnesses,
stretchers, hoists
Take remedial action where
necessary
Select and use portable fire
fighting equipment
Deal with unignited fuel
spillage
Minimize damage to
helicopter and installation
Clean, service and replenish
equipment stocks
Procedures:
Fuel spillage,
cleaning and
servicing equipment,
stock control
Damage:
water, smoke, heat
Service equipment:
To installation
Requirements
Stock:
To installation
requirements
Operate monitor controls to
optimum effect
Maintain escape routes
Procedures:
Fixed firefighting
ystems, portable
firefighting
equipment, hose and
branches, hose reels,
discharge patterns,
escape routes
Fixed firefighting
systems:
Helideck foam
monitors, monitor
controls, hoses, hose
reels, branches
Deficiencies:
Fixed firefighting
system
Water Pumping
capacity
Water pressure
Control
mechanisms
Standby reserves
\
Appendix 3
6-10-09
EX
AM
PL
E - A
pp
en
di x
3
APPENDIX 4 Marshalling Signals
Engine Fire
APPENDIX 5
Transportation of special loads.
"Special load" is the collective term for those items of cargo
which, due to there nature or value will require special
treatment by all personnel during the stages of acceptance,
storage, stowage and transportation.
Under the heading of "special load" will fall:
- Dangerous goods.
- Live animals.
- Strongly smelling cargo.
- Human remains.
- Perishable cargo. (Including foodstuffs)
- Valuable cargo.
- Wet cargo.
- Living human organs and blood shipments.
- Spare parts for aircraft that are "AOG" coded.
- Undeveloped film.
All of the above items with the exception of "Valuable cargo"
must be entered in the part of the cargo manifest
designated "Special load notification to Captain" (NOTOC)
Either the operations department of the helicopter operator
or the approved dispatcher on an offshore installation or
vessel issues this.
Dangerous goods.
Definition of dangerous goods
Dangerous goods comprise of all articles or substances
which are capable of posing a significant risk to health,
safety or property when transported, and which are
classified according to I.C.A.O. Annex 18, Technical instruc-
tions for the safe transport of dangerous goods by air and
IATA.
For the purpose of transportation dangerous goods have
been divided into three (3) categories. They are:
1. Forbidden:
Those, which are forbidden for transportation by air
2. Acceptable:
Those items, which are acceptable for air transport,
provided all the special provisions concerning packaging;
quantity and compatibility are complied with.
3. Excepted:
Known items in general use such as, after shave lotions,
perfumes etc. this being directed at passengers and
their baggage.
Classification of dangerous goods
Class 1.
Class 2.
Class 3.
Class 4.
Class 5.
Class 6.
Class 7.
Class 8.
Class 9.
Explosives.
Gases. (Compressed, liquefied, dissolved
under pressure or deeply refrigerated)
Flammable liquids.
Flammable solids. (4,1)
Substances liable to spontaneous
combustion (4,2)
Dangerous when wet, will emit flammable
gases. (4,3)
Oxidizing substances. (5,1)
Organic peroxides. (5,2)
Poisonous toxic substances (6,1)
Infectious substances (6,2)
Radioactive materials.
Corrosives.
Miscellaneous dangerous goods, including magnetic
materials
Marking and labelling
All packages containing dangerous goods must have the
correct marking and labelling, as laid down in the IATA
Dangerous goods regulations. In all cases the "Proper
shipping name the "UN" or "ID Number" and quantity must
be noted on the outer packing together with the correct
"Hazard labels".
Further to this a "Shippers declaration of dangerous goods"
is required.
Orientation labels.
In addition to the previous mentioned labels, special
attention must be paid to the following:
“Heavy Freight”
Packages bearing these labels must be stowed accordingly.
Single packages with end closures, containing liquids must
be stowed with the closures upwards.
Appendix 5 – Transportation of special loads
2
Packing.
Dangerous goods must be packed in containers that are
approved according to the packing instructions as laid down
in the I.A.T.A. Dangerous goods regulations. For this
purpose the regulations divide the dangerous goods into
three groups, depending on the degree of danger that they
may present.
Packing group I
Packing group II
Packing group III
=
=
=
Great danger.
Medium danger.
Minor danger.
Bilateral agreement.
This agreement made between the Civil Aviation Authority of
the Netherlands (Inspectie Verkeer en Waterstaat, divisie
luchtvaart) and the United Kingdom (CAA) ICAO.
Except when otherwise provided for in the "technical
instructions", no person may offer, or accept dangerous
goods of any class for transportation by air, unless those
goods are properly classified, documented, certificated,
described, packed, marked, labelled and in the correct
condition for shipment as required by the technical
instructions.
When all of the required precautions have been taken,
transportation by air of items, which possess potentially
hazardous characteristics, may be carried out in a safe and
acceptable manner.
Loading of dangerous goods.
Dangerous goods that are to be carried on board helicopters
will be stowed in the cargo area only. Special care must be
taken to insure that the dangerous goods are secured in the
correct position and manner.
Appendix 5 – Transportation of special loads
3
Handling of incidents and accidents with
dangerous goods.
For your own protection, and that of other personnel
involved in the transportation of special loads, if confronted
with a leaking or damaged packages containing dangerous
goods. The following procedures must be applied at all
times.
Damaged packages.
(All classes except class 7.)
Warning.
Never load damaged packages.
When a package or packages containing dangerous goods
are damaged but with no spillage, separate the package or
packages and warn a member of the helicopter crew or the
Helicopter Landing Officer.
Spillage of contents.
(Class 1 to 5 and 9.)
Warning.
Never load leaking packages.
In cases of spillage of the contents (liquids, solids, gases or
fumes) if possible place the package or packages in a safe
place preferably in open air, and inform a member of the
helicopter crew or the Helicopter Landing Officer.
Contamination of skin or clothing.
(Classes 1 to 5 and 9.)
Remove contaminated clothing as soon as possible prefer-
ably under a running shower and have the clothing cleaned,
wash the contaminated areas of the body for a period of at
least 10 to 15 minutes with running water. If so required
contact a physician as soon as possible.
Appendix 5 – Transportation of special loads
4
Spillage of contents.
(Classes 6 and 8.)
Never move a damaged package. Insure that contamination
does not spread. Protect your person and inform the Heli-
copter Landing Officer.
Class 6.
In cases of contamination of clothing replace as soon as
possible, if the contamination has penetrated to the skin
wash in running water with soap for a period of at least 15
to 20 minutes. Insure that another person opens doors and
operates taps etc. to prevent any further contamination.
Note.
If the skin is contaminated consult a physician as soon as
possible.
Class 8.
In cases of contamination with this class immediately douse
the affected person with large amounts of running water,
then with great care remove the clothing and continue to
douse the affected parts.
Note.
Use as much water as possible.
Do not rub the skin.
Consult a physician immediately.
Notification to captain (N O T O C)
The captain of the helicopter must be provided with written
information (manifest) as soon as practically possible prior to
the departure time, covering the "special load" that is to be
carried. If dangerous goods are to be transported from an
airfield to an offshore installation or vessel the goods will be
accompanied by a "shippers declaration".
IATA-ICAO Hazard & Handling labels
Appendix 5 – Transportation of special loads
5
IATA/ICAO HAZARD AND HANDLING LABELS Except for Radioactive and Handling Labels, text indicating the nature of risk on label is optional.
Primary Hazard Labels Class 1
Class 4
Class 2
Class 3
*Articles bearing the Explosives labels shown above and falling into Divisions 1.1, 1.2, 1.4F, 1.5 and 1.6 are normally forbidden.
1.1 1
1.2 1
1.4 EXPLOSIVES
F
1
1.6
N
1
1.5
D
1
1.4 EXPLOSIVES
G
1
1.4 EXPLOSIVES
B
1
1.4 EXPLOSIVES
C
1
1.4 EXPLOSIVES
D
1
1.4 EXPLOSIVES
E
1
1.4 EXPLOSIVES
S
1
1.3 1
Non-flammable gas Flammable gas
Spontaneously
combustible
4
Flammable solid4
4
Dangerous when wet
4
Flammable liquid 2
3
Class 5
Oxidizer
5.1
Organic peroxide
5.2
Appendix 5 DANGEROUS GOODS
2
Toxic gas
2
IATA/ICAO HAZARD AND HANDLING LABELS (CONT.) Except for Radioactive and Handling Labels, text indicating the nature of risk on label is optional.
Primary Hazard Labels (cont.)
Class 6 Infectious substance
Secondary Hazard Labels
Toxic
6
RADIOACTIVE I
CONTENTS
ACTIVITY
7
Class 7
In case of damage or leakage
immediately notify Public
Health authority
6
RADIOACTIVE II CONTENTS
ACTIVITY
TRANSPORT INDEX
7
Flammable gas
Flammable liquid
Dangerous
when wet
Oxidizer
Class 8
RADIOACTIVE III CONTENTS
ACTIVITY
TRANSPORT INDEX
7
Class 9
Flammable
solid
Spontaneously
combustible
Toxic
CORROSIVE
CORROSIVE
8
Handling Labels N
W E
9
DANGER
S
MAGNETISED
MATERIAL
KEEP AWAY FROM AIRCRAFT COMPASS DETECTOR UNIT
DO NOT LOAD IN PASSENGER AIRCRAFT
CONTAINS
CRYOGENIC
LIQUID
Appendix 5 DANGEROUS GOODS
SHIPPERS DECARATION FOR DANGEROUS GOODS
Shipper
Air Waybill No.
Page of
Pages
Consignee
Two completed and signed copies of this declaration must be handed to the operator
TRANSPORT DETAILS
This shipment is within the Airport of Departure:
limitations prescribe for
(delete non-applicable) PASSENGER CARGO AND CARGO AIRCRAFT AIRCRAFT ONLY
Airport of Destination:
NATURE AND QUANTITY OF DANGEROUS GOODS
Dangerous Goods Identification
Shippers Referencee Number (optional)
WARNING
Failure to comply in all respects with the applicable Dangerous
Goods Regulations may be in breach of the applicable law, subject to the legal penalties. This Declaration must not, in any circumstances, be completed and/or signed by a consolidator, a
forwarder or an IATA cargo agent.
Shipment type (delete non-applicable)
NON-RADIOACTIVE RADIOACTIVE
(see sub-section of 8.1 of IATA Dangerous Goods Regulations)
Proper Shipping Name
Class UN or Pack- Subsi- Quantity and type of packing
or ID No. ing diary
Divi- Group Risk sion
Packing
Inst
Authorisation
Additional Handling Information
I hereby declare that the contents of this consignment are fully and
accurately described above by the proper shipping name, and are
classified, packaged, marked and labelled/placarded, and are in all
respects in proper condition for transport according to applicable
International and national governmental regulations.
Name/Title of Signatory
Place and date
Signature
(see warning above)
Appendix 5 DANGEROUS GOODS
Dan
gero
us
Go
od
s -
Noti
fica
tio
n T
DA
NG
ER
OU
S G
OO
DS
carrie
d i
n a
ccord
an
ce w
ith
A
rti
cle 4
4 o
f th
e
Air
Na
vig
ati
on
O
rder
19
85
(a
s a
men
ded
).
Ad
vic
e i
s g
iven
of
the f
ol
low
ing D
AN
GE
RO
US
GO
OD
S l
oad
ed
.
All
mate
ria
ls
load
ed
are i
n s
tric
t accord
an
ce w
ith
IC
AO
reg
ula
tio
ns
for t
he s
afe
tra
nsp
ort
of
DA
NG
ER
OU
S G
OO
DS
by
air .
Dat
e:
Inst
alla
tion:
Fli
ght
No.:
Air
craf
t R
eg.:
Des
tinat
ion
Num
ber
of
Pac
kag
es
UN
Num
ber
Pro
per
Ship
pin
g N
ame
Cla
ss
or
Div
isio
n
Subsi
dia
ry
Ris
k
Pac
kin
g
Gro
up
Net
t Q
uan
tity
or
Tra
nsp
ort
Index
No.
IM
P C
ode
Car
go
A/C
Only
Load
ing P
osi
tion
Addit
ional
Info
rmat
ion:
Load
ed a
s sh
ow
n.
Th
ere
is n
o e
vid
ence
th
at
an
y d
am
age
or
leak
ing p
ack
ages
h
ave
bee
n l
oad
ed o
n t
he
air
craft
. N
ame
and P
osi
tion:
Sig
nat
ure
Sig
nat
ure
of
Cap
tain
:
IM
P C
ode
Lab
el
IM
P C
ode
Lab
el
IM
P C
ode
Lab
el
RE
X,
RC
X, R
GX
*
RX
B,
RX
C, R
XD
*
RX
E,
RX
G *
RX
S
RE
X
NR
G o
r R
CT
L *
R
FG
* d
enote
s as
ap
pli
cab
le
Exp
losi
ve
Exp
losi
ve
1.4
Exp
losi
ve
1.4
Exp
losi
ve
1.4
S
Exp
losi
ve
1.5
Non
-Fla
mm
ab
le G
as
Fla
mm
ab
le G
as
RP
G
RF
L
RF
S
RS
C
RF
W
RO
X (
Oxid
iser
) or
RO
P (
Org
. P e
rox)
Pois
on
ou
s (T
oxic
) G
as
Fla
mm
ab
le L
iqu
id
Fla
mm
ab
le S
oli
ds
Sp
on
tan
eou
s C
om
bu
stib
le
Dan
ger
ou
s W
hen
W
et
Oxid
iser
or
Org
an
ic P
eroxid
e
RP
B
RH
F
RIS
RR W
R
R Y
MA
G
RC
M
CA
O
Pois
on
Kee
p A
way F
rpm
Food
In
fect
iou
s S
ub
stan
ce
Rad
ioact
ive
CA
T.
1
Rad
ioact
ive
CA
T 1 1/
1 11
M
agn
etis
ed M
ate
rial
Corr
osi
ve
Carg
o A
ircr
aft
On
ly
F/2
84
8 (
04 A
ug
19
99
) W
hit
e C
opy -
Pil
ot,
Pin
k C
op
y -
UE
SL
/12
, Y
ello
w C
op
y -
Ret
ain
ed i
n b
oo
k
Appendix 5 DANGEROUS GOODS
APPENDIX 6 Helicopter Diagram
Appendix 7 Refuelling points of different helicopters
S76 b
EC155
AW13
9
AS332
L2
Super
Puma
Appendix 8 – Helicopter types & Cargo Holds
HELICOPTER TYPE LDG NET (m)
N/R3.200
2.400 2.4t N/R
3.2t
MAX WT (KG) t-VALUEROTOR DIA. (m)
BOLKOW 117 13.00 (13) 11,00
BOLKOW Bo 105D 12.00 (12) 9,90
D-VALUE (m)
2.6t 9 x 9
DAUPHIN SA 365N2 13.68 (14)
AGUSTA A109 13.05 (13) 11,00 2.600
4.3t11,93
5.3t
4.250 9 x 9
13,80 6.400
12 x 12
12 x 12
4.9t
6.4t 12 x 12
14.30 (14) 12,60 4.850
SIKORSKY S76 16.00 (16) 13,40 5.307
EC155 B1
5.1t N/R
AUGUSTA-BELL 139 / AW139
12 x 12
8.6t 12 x 12
BELL 212 17.46 (17) 14,63 5.080
16.66 (17)
SUPER PUMA AS332 L2 19.50 (20) 16,20
15,00SUPER PUMA AS332 L 18.70 (19) 8.599
BELL 214ST 18.95 (19) 15,85 7.936
12.0t 15 x 15
9.300
8.0t
9.3t 12 x 12
11.0t 12 x 12
SIKORSKY S92 20.88 (21) 17,17 12.020
EC 225 19.50 (20) 16,20 11.000
SIKORSKY S61 N 22.20 (22) 9.3t 15 x 1518,90 9.298
AW 139
EC155
Please watch obstacle at the top of the cargo hold
S76B