QID 063Quality Manual

Chapter 0

Issue 2

Bristow Helicopters

Fuel Manual

Commercial in Confidence

Issued by Bristow Helicopters LimitedAberdeen Airport, Dyce, Aberdeen, AB21 0NT

Telephone: 01224 723151FAX: 01224 772401

All Reproduction Rights Reserved.

QID 063FUEL MANUAL

Issue 2 Page 1 of 1

RECORD OF AMENDMENTS

AmendmentNumber

IssueDate

Date ofIncorporation

Incorporated by

Issue 2 August 2006

Issue 2, Am. 1 August 2009 05.08.09 Irena Leonhardt

QID 063Fuel Manual

Chapter 0

Issue 2 1 of 1

List of Chapters

Preface

Chapter 1 Oil company fuel supplies.

Chapter 2 Receiving bulk fuel.

Chapter 3 Barrelled fuel supplies.

Chapter 4 Methods of storing fuel.

Chapter 5 System maintenance, bulk fuel.

Chapter 6 Bulk fuel at remote locations.

Chapter 7 Aircraft fuelling vehicles.

Chapter 8 Hydrant systems.

Chapter 9 Refuelling and defuelling procedures.

Chapter 10 Offshore fuel installations.

Chapter 11 Sampling procedures.

Chapter 12 System maintenance guide.

QID 063Fuel Manual

Chapter 0

Issue 2 1 of 1

PREFACE

Introduction

(1) The purpose of this manual is to ensure that all fuel dispensed to companyaircraft is to the highest possible standard. The contents of this manual adhereto CAP 748. All Chief Engineers and Managers with the ultimate responsibilityfor fuel quality on their base should be aware of the need to adhere to thefollowing guidelines.

(a) Ensure all personnel involved in the handling dispensing and inspecting of fueland associated systems are correctly trained.

(b) The fuel is coming from an approved source, and that all relevant documentationis available.

(c) The correct Personnel Protective Equipment is issued to staff to enable them tofulfil the task

(d) All health and safety issues as laid down in company Health and Safety manual,base ramp procedures, and risk assessments as relevant are complied with,

(e) A maintenance and inspection procedure programme for receipt, storage anddispensation of fuel as relevant to the base and that all paperwork anddocumentation is correctly annotated and filed.

(f) All equipment such as hoses, filters, pumps and dispensing nozzles are to thecorrect standard for the system and subject to regular maintenance.

QID 063Fuel Manual

Chapter 1

Issue 2 1 of 1

Chapter 1

Oil Company Fuel Supplies

1. Oil company standards.

2. Operations using contract suppliers for supplying fuel to hydrants / refuellers

3. Operations using Bristow Helicopter bulk fuel installations

4. Operations using a third party for supplying fuel to aircraft.

5. Operations responsible for off shore fuel installations.

QID 063Fuel Manual

Chapter 1

Issue 2 1 of 3

Oil Company Fuel Supplies

1. Oil Company Fuel Standards

Operation contracted to an oil company, and supplied with fuel by that companyare to ensure the fuel meets the correct specifications as laid down in the FlightManual and Engine Maintenance Manual.

Jet A - or equivalentJet A1 - or equivalent

2. Operations Using Third Party Suppliers For Supplying Fuel To Hydrant /Refuelling Vehicle

Chief Engineers are advised to ensure that the fuel supplied is to the abovestandard and a written statement to this effect should be filed with the DailyCheck certificates.

(a) Daily Checks

Operations using third party fuel suppliers are to check that the supplier hasconducted a fuel sampling process in the form of written certification. If this is notforthcoming a water sediment check as per chapter 11 sects 3 & 4 should becarried out before fuel is uplifted.

(b) Six Month Inspections

Operations supplied with fuel from a third party to the Hydrant / Refuelling vehicleare to conduct a six monthly inspection of Documentation/Certificationmaintenance procedures and standards. Form QAF 104 should be completedand held on file for two years.

(c) When a third party is responsible for supplying fuel to Hydrant / Refuelling vehicleand Bristow Helicopters Limited is responsible for supplying fuel to aircraft fromthe Hydrant / Refuelling vehicle. The following chapters detail the informationand checks required.

Chapter 7 Aircraft fuelling vehicles.Chapter 8 Hydrant systems.Chapter 9 Refuelling and defuelling proceduresChapter 11 Sampling proceduresChapter 12 System maintenance guide.

Third Party Bristow

QID 063Fuel Manual

Chapter 1

Issue 2 2 of 3

3. Operations Using Bristow Operated Bulk Fuel Installations

When Bristow Helicopters is responsible for bulk storage and supply of fuel toaircraft. The following chapters detail the information and checks required.

Chapter 2 Receiving bulk fuel.Chapter 3 Barrelled fuel supplies.Chapter 4 Methods of storing fuel.Chapter 5 System maintenance, bulk fuel.Chapter 6 Bulk fuel at remote locations.Chapter 7 Aircraft fuelling vehicles.Chapter 8 Hydrant systems.Chapter 9 Refuelling and defuelling procedures.Chapter 11 Sampling procedures.Chapter 12 System maintenance guide.

Third Party Bristow

4. Operations Using A Third Party For Supplying Fuel Direct To Aircraft.

(a) Daily Checks

Operations using third party fuel suppliers are to check that the supplier hasconducted a fuel sampling process in the form of written certification. If this is notforthcoming a water sediment check as per chapter 11 sects 3 & 4 should becarried out before fuel is delivered to the aircraft.

(b) When a Third Party is responsible for supplying fuel to aircraft. The followingchapters detail the information and checks required.

Chapter 9 Refuelling and defuelling proceduresChapter 11 Sampling procedures.Chapter 12 System maintenance guide.

Third Party Bristow

5.

QID 063Fuel Manual

Chapter 1

Issue 2 3 of 3

Operations Responsible For Off Shore Fuel Installations.

(a) When an operation is directly responsible for operating an off shore fuelinstallations. The following chapters details the information and checks required.

Chapter 9 Refuelling and defuelling proceduresChapter 10 Off shore fuel installationsChapter 11 Sampling proceduresChapter 12 System maintenance guide

QID 063Fuel Manual

Chapter 2

Issue 2 1 of 1

Chapter 2

Receiving Bulk Fuel

1. Pre-delivery Checks

2. Uplifting Fuel

QID 063Fuel Manual

Chapter 2

Issue 2 1 of 1

Receiving Bulk Fuel

1.(a) The delivery vehicle should be positioned so that in the event of an incident the

vehicle can be quickly driven away.

(b) The Chief Engineer or his qualified representative is to inspect the release noteto ensure the grade and quantity of fuels is as ordered, and sign as acceptable. Acopy of this documentation is to be placed on file to enable a trace to be made inthe event of contamination.

(c) Ensure the seals on the delivery vehicle are intact and the vehicle is annotatedas carrying the grade stipulated on the release note.

(d) Ensure receiving tank has the capacity for quantity to be received. Carry outwater checks on receiving tank prior to start of transfer as per Chapter 11 sects 3& 4.

(e) Allow delivery vehicle to stand for 10 minutes; then take sample from each tankfrom which fuel is to be delivered. Having noted the Gravity reading on therelease note, carry out checks as per Chapter 11 sect 3, 4 & 5. If tests fail, repeatprocess. If it still fails after three tests Chief Engineer to be advised and to liaisewith supplier.

2.(a) On satisfactory completion of the tests and checks, the delivery vehicle should be

bonded to an approved earthing point. Hose connected and fuel transfer to thenominated fuelling tank to begin.

(b) At all times during transfer the driver of the vehicle and the companyrepresentative should remain present and all fire and safety precautions to becomplied with.

(c) On completion, disconnect hose and bonding lead, ensure all valves reset tocorrect position.

(d) A record of tests and inspections should be made and fuel samples retained for aminimum of seven days.

(e) If it is necessary to submit a sample for laboratory tests a duplicate sampleshould be taken and held until results are known.

QID 063Fuel Manual

Chapter 3

Issue 2 1 of 1

Chapter 3

Barrelled Fuel Supplies

1. Material, Identification and Delivery Checks.

2. Storage, Stock Rotation.

3. Sampling.

4. Decanting and dispensing.

QID 063Fuel Manual

Chapter 3

Issue 2 1 of 3

Barrelled Fuel Supplies

1.(a) Material

Barrels used for the storage of aviation fuel must be made from steel.

(b) Identification

Barrels storing aviation fuel should be distinctly coloured according to fuel grade.Do not mix

Jet A1 Body black with white ends.Closure seals should show the grade name in white on a

black background.

Avgas 100 LL.Body olive drab with red ends.

(c) Delivery Checks

Before acceptance, barrels should be examined for damage and seal integrity.Grade marking and traceability should be cross checked with details on thedelivery note,

2.(a) Storage

Barrels should be stored undercover in the horizontal position, with the fuelcovering the bungs, i.e. 3 oclock and 9 oclock position.

Correct Incorrect Incorrect

(b) Barrels whose labels or markings have deteriorated and are no longer legiblemust be discarded. Never try and guess the contents.

QID 063Fuel Manual

Chapter 3

Issue 2 2 of 3

(c) Six months after the filling date, drummed fuel must be checked to verify it stillconforms with its specification by sending a sample to a laboratory for analysis.

(d) Fuel stored in barrels should be downgraded after 24 months

(e) Stock rotation

A storage system should be adopted that will utilise the oldest fuel first accordingto the batch number and filling date.

3. Sampling

Before sampling check that seals are intact, stand the barrel on its end and wipearea clean adjacent to bung. Place a wedge under the bottom rim of drum at theopposite side to the bung. Allow to settle for ten minutes. Using a sample tubecover end with thumb, lower into barrel, remove thumb, allow tube to fill, replacethumb and withdraw. Put contents into a sample container. Carry out tests as perchapter 11, sect 3 & 4. Alternatively detection paste applied to a dipstick can beused. Fresh paste must be used for each test, and dipstick allowed to rest onbottom of barrel for 10 seconds.

4. Decanting and dispensing

(a) Fuel should preferably be decanted into a fuelling vehicle or storage using asuitable pump and micro filter or filter separator,

(b) Bonding

The barrel must be bonded to the receiving vehicle.

(c) Dispensing Direct from Barrel

When refuelling directly from a barrel is the only option, the barrel should bestood on end and allowed to settle for at least 10 minutes before taking a sample.Caution should be taken in positioning the barrels so as not to be a hazard to thehelicopter landing. Once a satisfactory sample is obtained fuel may be dispensedto the aircraft using a suction standpipe designed to ensure fuel cannot be drawnfrom below a depth of 75 mm from the barrel bottom and fitted with a suctionstrainer device.

(d) Bonding

The barrel should be bonded to earth and the pump. The pump bonded to theaircraft.

QID 063Fuel Manual

Chapter 3

Issue 2 3 of 3

(e) Resealing and Disposal

When barrel is empty replace cap tightly. Barrels are not to be refilled with fuelintended for aviation use, but should be returned to the supplier.

(f) Portable Fuel Pumping Equipment

All equipment should be blanked off and stored in a clean facility and maintainedas per manufacturers instructions.

(g) Records should be kept of all barrel and drum deliveries, decanting anddispensing of fuel plus sample checks.

QID 063Fuel Manual

Chapter 4

Issue 2 1 of 1

Chapter 4

Methods of Storing Fuel

1. Introduction.

2. New Sites, Old Sites.

3. Internal Inspections

4. Transportable Tanks.

5. Collapsible tanks.

6. Neoprene Pillow Tanks.

7. Seal Drums.

QID 063Fuel Manual

Chapter 4

Issue 2 1 of 2

Methods of Storing Fuel

1. Introduction

Aviation fuel must always be segregated from other products and differentgrades of aviation fuel must also be segregated.

2.(a) New Sites

If a new bulk fuel storage site is being considered it will be necessary to do a riskassessment I.A.W. Health & Safety and environmental Issues. It is stronglyrecommended that the assistance of a fuel design and installation expert besought before commencing,

(b) Old Sites

To ensure fuel installations operate safely and deliver a high quality product it isnecessary to ensure that regular inspections and maintenance procedures are inplace and are carried out by properly trained personnel. This should be reflectedin the local Base Heath & Safety orders and Ramp Procedures.

3.(a) Tank Internal Inspections

Unlined tanks are to be inspected every 3 years and lined tanks every 5 years orif a problem becomes obvious i.e. corrosion, debris, tank damage. Thisinspection should be carried out by an approved firm using breathing apparatus,and only after the tank has been drained and allowed to vent. On completion anew inspection date should be annotated on the outside of the tank and allcertification paperwork put on file,

4.(a) Transportable Tanks

These are primarily for use on offshore locations. These tanks are manufacturedfrom stainless steel and are designed to a standard as laid down by (I.M.C.O)Intergovernmental Marine Consultative Organisation.

(b) Identification and Capacity

Each tank is stencilled with a serial number and has a capacity for 2,700 litres600 Imp gallons).

(c) Internal / External Inspections

These are carried out every 6 months by an onshore specialist organisation. Thetanks should also be subject to a Trip Inspection each time the tank is offered forrefilling.

QID 063Fuel Manual

Chapter 4

Issue 2 2 of 2

5. Collapsible Tanks

(a) These should as far as possible comply with the same requirements for bulk fueltank installations. Although due to their design condensation is minimal, a bottomdrain fitting is required.

(b) Collapsible fuel tanks should be housed in a bund which is capable of retainingthe fuel in the event of a rupture.

6. Neoprene Pillow Tanks

(a) These should as far as possible conform to the same requirements as permanentbulk fuel tank installation. They should be positioned on a firm flat base with a 1in 60 slope.

(b) Usage

Position tank unit drain at lowest point, fill tank via a water filter separator andfilter monitor to 95% capacity. Allow to stand for seven days, then draw offsample for testing as per chapter 11 sects 3 & 4. Draw off second sample andsend for laboratory testing. The tank should be housed within a bund capable ofretaining 110% of tank capacity in the event of rupture. If used in hot climates ashelter should be provided leaving a one metre gap between shelter and tank forventilation.

7. Seal Drums

(a) Neoprene rubber seal drums come in various sizes specially strengthened fortransportation, either underslung or by road. They can be utilised as a bulk tankand are filled and drained via a filter monitor. It can be collapsed when empty.

(b) When in use they should be housed within a bund capable of retaining 110% ofcontents.

(c) Prior to usage these tanks should undergo a process to leach out any excessiveadhesive from manufacture. It is done by the company filling the drums.

(d) Underslung Seal Drums

They can be connected to each other by lugs between the drums. But experiencehas shown that the best method is the utilisation of a cargo net.

(e) When considering the use of sealed drums for an operation thought should begiven to the fact they are impossible to clean and need to be downgraded afterone year in use, thus making it an expensive alternative.

QID 063Fuel Manual

Chapter 5

Issue 2 1 of 1

Chapter 5

System Maintenance of Bulk Fuel

1. Introduction.

2. Filters.

3. Differential pressure Checks.

4. Static Electricity.

5. Settling Times.

6. Identification of Product.

7. Sampling and Checks.

8. Hoses.

9. Nozzle and Pressure Couplings

QID 063Fuel Manual

Chapter 5

Issue 2 1 of 4

System Maintenance of Bulk Fuel.

1. Introduction

Any system utilised in the distribution of aviation fuel should be totallysegregated. Separate input and output lines provided. Drains fitted at all lowpoints and system securely locked to prevent contamination and unauthoriseduse.

2. Filters

(a) Turbine Fuel Installations

Tank input lines should be fitted with a 5 micron filter or filter separator. Theoutlet line should have a filter separator with a nominal 5 micron rating for solidsand a maximum 15 parts per million for water.

(b) Offshore Installations

Offshore filtration units should provide protection down to 1 micron and beAmerican Petroleum Institute (A.P.I. 1581) approved. It is also recommendedthat a Petroguard Fuel Filter Monitor is installed on the outlet system.

(c) Collapsible Fuel Tanks

To be fitted with 5 micron filter to outlet and a Petroguard Fuel Filter Monitorinstalled also to outlet side.

3.(a) Differential Pressure Checks

Filter separators, filter monitors and microfilters must have the differentialpressure checked daily and recorded weekly. This should be conducted at themaximum possible flow rate. Filter separator elements should be replaced whenmanufacturers recommended limit is reached.

(b) If a sudden significant change in differential pressure is noted from last readingthe microfilter or filter separators should be inspected and possibly replaced. Anincrease in pressure indicates blockage, a decrease would indicate rupturing andbypass.

(e) Filter elements in separators should be replaced after 3 years usage. Wearsurgical gloves to avoid contamination. Filter monitors are replaced whenmanufacturers differential pressures reached. Annotate filter due date on outsideof container. When filling a filter separator vessel the flow should be gradual toavoid a build up of static electric.

QID 063Fuel Manual

Chapter 5

Issue 2 2 of 4

4. Static Electricity

Freshly manufactured fuel has virtually no conductivity, it is an insulator. Toensure safe handling during distribution an additive Stadis 450 is added, prior todispatch from bulk storage to a level of 50 450 Pico Siemens per meter.Because this level can deteriorate due to other additives and time, this can bechecked in the field using a special metre as per Chapter 11 Sect 9. Where theperiod of time between receipts into a tank exceeds 1 month conductivity checksare to be carried out monthly.

5. Settling Times

(a) Horizontal Tanks

Horizontal tanks fitted with floating suction devices require a minimum settlingtime of two hours.

(b) Tanks without suction devices

Jet A1 3 hours per metre depth of fuel or 24 hours, whichever is less. Avgas 1

6. Tank Data Plates

(a) All tanks should have a data plate on the outside giving the following information;

(i) Serial number of tank(ii) Date inspection due(iii) Date cleaning due(iv) Tank capacity

(b) The plate should be painted white on black for Jet A1 and white on red for Avgas.No smoking and danger signs should also be displayed.

(c) Pipeline Identification

Surface fuel carrying pipelines should be marked at 10 metre intervals, to identifyproduct carried.

Jet A1 Two black bands on white background. Avgas 100 A red band on a green background. Avgas 100 A red band on a blue background.

QID 063Fuel Manual

Chapter 5

Issue 2 3 of 4

7.(a) Sampling and Checks

Sampling in accordance with procedures stated in Chapter 11 sects 3 & 4 shouldbe complied with.

(i) Each day before the first delivery from tanks.(ii) Immediately before receipt of fuel.(iii) After receipt, following stipulated settling time.(iv) After prolonged heavy rain or snow.

(b) Failed Samples

If a sample is found to have water or sediment present, a further sample must betaken until a clean sample is obtained. If after 3 attempts no clean sample isachieved the tank should be quarantined, inform Chief Engineer and furtherinvestigations carried out.

(c) Disposal of Samples

Satisfactory samples may be returned to storage, via a storage recovery tank.

(d) Contaminated Samples

Must be disposed of as per local H.S.E. and ramp procedures, but neverreturned to the fuel system.

8. Hoses

(a) Aircraft fuelling hoses must be qualified to A.P.I. 1529 or C EN 1361 (previouslyBS 3158). New hoses should be inspected, flushed and pressure tested prior tousage.

(b) If system is not used for a period of two days a sample should be taken andinspected as per Chapter 11 sects 3 & 4.

(c) Carry out inspection of hose daily and weekly as per maintenance table Chapter12.

(d) All hoses should be given permanent identification on installation and a historyand test sheet raised giving

(i) Date of manufacture(ii) Date of installation(iii) Details of all tests carried out

QID 063Fuel Manual

Chapter 5

Issue 2 4 of 4

(e) Recommended Hose Life

(i) Not to exceed 10 years from date of manufacture provided itpasses daily, monthly and six monthly checks.

(ii) Shelf life should not exceed 2 years.

(iii) Hoses on offshore installations should be tested or replaced after 2years in service and have an ultimate life of 10 years.

9. Nozzle and Pressure Couplings

(a) Gravity Refuelling

A gravity or overwing refuelling system has a trigger operated nozzle which whensqueezed allows fuel to be dispensed. There should be no serrations on thetrigger guard which might prevent the fuel being shut of on release of the trigger.A 150 micron (100 mesh) cone shaped strainer is installed in the spout.

(b) Pressure Refuelling

This utilises a female quick release, self sealing coupling fitted to the refuellinghose that engages with a male coupling on the aircraft. Incorporated within thecouplings are pressure control valves and a (150 micron) filter. The connecting ofthe couplings together opens the valves and allows the fuel to flow.

QID 063Fuel Manual

Chapter 6

Issue 2 1 of 1

Chapter 6

Bulk Fuel at Remote Locations

1. Introduction.

2. Transportation and Underslinging.

3. Neoprene Pillow Tanks and Collapsible Tanks.

QID 063Fuel Manual

Chapter 6

Issue 2 1 of 1

Bulk Fuel at Remote Locations

1. Introduction

Due to the nature of helicopter charter work it is sometimes necessary to operatefrom remote locations. When this occurs serious thought and planning needs tobe given as to how fuel will be made available and problem maintaining quality. Arisk assessment of proposed area should be conducted at an early stage ofproject.

2.(a) Transportation

This might be by road, air, water or a combination. Depending on terrain roadtransport should be considered as the first alternative using either a bowser ortransportable tanks.

(b) Underslung Loads

In some remote areas underslinging may be the only alternative, in which casethe use of seal drums is strongly recommended.

(c) Seal Drums

These are specially designed, rubberized, transportable containers available invarious sizes to suit type of operation proposed. They must be speciallycommissioned by the fuel supplier prior to use and only have a 1 year life.

(d) Barrelled Supplies

The use of barrelled fuel in steel drums is not recommended for underslinging asthey are not designed for the robust treatment which can be sustained and aremore susceptible to contamination.

(e) Internal Helicopter Transportation

Sealed drums and barrelled fuel are listed as Dangerous Goods cargo andshould not be transported inside the aircraft unless special arrangements are inplace. Never with passengers on board.

3.(a) Neoprene Pillow Tanks and Collapsible Tanks

Remember these will require refilling by either a bowser or barge.

QID 063Fuel Manual

Chapter 7

Issue 2 1 of 1

Chapter 7

Aircraft Fuelling Vehicles

1. Construction.

2. Identification.

3. Product Protection.

4. Filters.

5. Filter Replacement.

6. Sampling.

7. Settling Times.

8. Hoses.

9. Bonding.

10. Records.

QID 063Fuel Manual

Chapter 7

Issue 2 1 of 2

Aircraft Fuelling Vehicles

1. Construction

(a) All fuelling vehicles and accessories shall be of aluminium alloy, stainless steel ormild steel construction protected internally by hot tinning or suitable epoxymaterial.

2. Identification

(a) All fuelling vehicles shall carry only one grade of product and the gradeidentification (A.P.I. system) shall be displayed prominently on each side, on thecontrol panel and all fill points.

3. Product Protection

(a) All hoses and sampling points should be fitted with dust caps and plugswhenever the system is not in use, thus preventing contamination.

4. Filters

(a) Avgas fuelling vehicles should be fitted with 5 micron filters.

(b) Jet A1 fuelling vehicles should be fitted with a filter separator or monitor with a 5micron rating.

(c) Filter monitors shall meet the performance requirements of API / IP spec 1583Filter separators shall meet the performance requirements of API / IP spec 1581

(d) Hose end Filter

A 150 micron (100 mesh) filter to be installed in outlet hose and to be inspectedmonthly.

5. Filter Replacement

(a) Micro filters and filter separator elements should be replaced when thedifferential pressure reaches manufacturers limits, approximately 1 Bar (15 psi)

(b) Filter monitor type elements should be replaced after three years or whendifferential pressure reaches 1.5 Bar (22 psi)

QID 063Fuel Manual

Chapter 7

Issue 2 2 of 2

6. Sampling

(a) All fuelling equipment i.e. drain cocks, tank compartments, filter separators, filtermonitors, micro filters and air separators should be checked for water andsediment contamination as per Chapter 11 Sect 3 & 4 at the following times;

(i) Before first aircraft refuel each day.(ii) After filling of the vehicle.(iii) After vehicle washing, heavy rainfall or snow.

7. Settling Time

(a) After a vehicle is filled it should be allowed to stand for a minimum of 10 minutesbefore samples are taken.

8. Hoses

(a) All hoses should be A.P.I. 1529 or CEN 1361 standard.

9. Bonding

(a) The aircraft must be bonded to earth.

(b) The aircraft must be bonded to the fuelling vehicle. A P.V.C covered bondinglead stowed on a reel should be of sufficient length for easy utilisation.

(c) A short bonding lead should be attached between the refuel nozzle and aircraft.

(d) The fuelling bowser must also be bonded to earth.

10. Recording

A record of all fuel uplifted and delivered by the vehicle should be kept. Alongwith a record of all maintenance and inspections.

QID 063Fuel Manual

Chapter 8

Issue 2 1 of 1

Chapter 8

Hydrant Systems

1. Maintenance.

2. Bonding

QID 063Fuel Manual

Chapter 8

Issue 2 1 of 1

Hydrant Systems

1. Maintenance and Inspection

(a) Hydrant pits should be kept clean and dry and regularly inspected and the coversfirmly secured.

(b) If the system is not used for three months or more the system should be flushedthrough prior to use.

(c) Pits should be clearly marked with contents of system.

(d) All low points in system to be fitted with drains and these flushed through once aweek to ensure removal of water and sediment until a clear bright sample isobtained.

2. Bonding

(a) The aircraft must be bonded to the hydrant system by a P.V.C covered bondinglead of suitable length stored on a reel.

(b) When gravity refuelling a short bonding lead must be attached between nozzleand aircraft.

(c) When pressure refuelling the couplings form a metal to metal contact, thusforming a bond.

(d) The hydrant system must also be bonded to earth.

QID 063Fuel Manual

Chapter 9

Issue 2 1 of 1

Chapter 9

Refuelling and Defuelling Procedures

1. Introduction.

2. Meter reading.

3. Weight of Jet A1.

4. Rotors Running Refuelling.

5. Rotors Running Passengers on Board.

6. Defuelling.

7. General Procedures for Refuelling.

8. General Procedures for Defuelling.

QID 063Fuel Manual

Chapter 9

Issue 2 1 of 6

Refuelling and Defuelling Procedures

1. Introduction

All operations should have a Ramp Procedures Manual which gives correctprocedures for refuelling and defuelling at a particular base. If a new base isbeing set up the following information can be used as guidelines until a R.P.M. isin place.

2. Meter Reading

(a) The meter on the dispenser or fuelling vehicle should be set to zero or if of a nonzero type readings taken prior to commencement. Also note reading on aircraftgauge.

(b) On completion of refuelling check the amount of fuel uplifted tallies with theaircraft gauge indicated contents: +/- 10% this will highlight any gauge indicationproblems.

3. Jet A1 / AVTUR Weight

(a) Jet A1 and AVTUR will vary in weight depending on temperature, less at a hightemperature and more at lower temperature. As a rule of thumb a gallon of JetA1 is taken to be 8 lbs. per imperial gallon, or 1.76 lbs. per litre. A more exactfigure can be gained by establishing the actual Specific Gravity of the fuel.

QID 063Fuel Manual

Chapter 9

Issue 2 2 of 6

3. WEIGHT/VOLUME COMPARISON CHART

Weight of Jet A-1/Avtur is 8 lbs/Imp Gall:

3.6 Kg = 1 Gall = 8 lbs36 Kg = 10 Galls = 80 lbs363 Kg = 10 Galls = 80 lbs

0.8 Kg = 1 lt = 1.76 lbs8 Kg = 10 lt = 17.6 lbs80 Kg = 100 lt = 176 lbs

Conversely:

12.5 Galls = 100 lbs = 57 lts125 Galls = 1000 lbs = 568 lts

Gallons lbs Gallons lbs

1 8 80 6402 16 90 7203 24 100 8004 32 110 8805 40 120 960

6 48 125 10007 56 130 10408 64 140 11209 72 150 120010 80 160 1280

11 88 170 136012 96 175 140013 104 180 144014 112 190 152015 120 200 1600

16 128 225 180017 136 250 200018 144 275 220019 152 300 240020 160 325 2600

25 200 350 280030 240 375 300040 320 400 320050 400 425 340060 480 450 3600

70 560 475 380075 600 500 4000

QID 063Fuel Manual

Chapter 9

Issue 2 3 of 6

3. WEIGHT/VOLUME COMPARISON CHART - Continued

Litres lbs Litres lbs

1 1.76 190 334.42 3.52 200 3523 5.28 225 3964 7.04 250 4405 8.8 275 484

6 10.56 300 5287 12.32 325 5728 14.08 350 6169 15.84 375 66010 17.6 400 704

11 19.36 425 74812 21.12 450 79213 22.88 475 83614 24.64 500 88015 26.4 1000 1760

16 28.16 1500 264017 29.92 2000 352018 31.6819 33.4420 35.2

25 4430 52.840 70.450 8860 105.6

70 123.275 13280 140.890 158.4100 176

110 193.6120 211.2125 220130 228.8140 246.4

150 264160 281.6170 299.2175 308180 316.8

QID 063Fuel Manual

Chapter 9

Issue 2 4 of 6

4. Rotors Running Refuelling

This procedure should not be seen as normal practice, but is quite permissibleprovided all personnel involved are fully conversant with procedures and theneed for diligence. A risk assessment should be carried out and held on base.The following guidelines highlight safety measures to be observed.

(a) Wheeled aircraft should be chocked.

(b) A minimum of 3 people must be used for refuelling.

Person 1 - refuels the aircraft

Person 2 - Provides fire cover with appropriate fire extinguisher overseas andsupervises operation, maintaining visual contact with pilot at alltimes.

Person 3 - Stands by the fuel hydrant or cut off lanyard to shut down system inthe event of a problem.

NOTE: The refuelling hose should not be forward of the engine intake, except forS76A when extra diligence should be exercised.

(c) All passengers are to be disembarked, and outside the refuel zone.

(d) Adequate communication procedures between refuel crew and pilot.

(e) A risk assessment has been carried out and all personnel involved are fullytrained in their role and aware of the need for diligence.

(f) Suitable and sufficient fire extinguishers are readily available.

(g) Prior to delivery of fuel all bonding connections should be made.

(h) Pilot should be made aware when actual fuel delivery is about to commence sohe can monitor aircraft gauges.

(i) On completion of refuelling, hoses and bonding leads to be correctly stowed.Fuel caps replaced, any open doors closed. The overseeing supervisor carriesout a check of aircraft to ensure now ready for flight and advises the pilot.

5. Rotors Running Refuel with Passengers on Board

(a) If a rotors running refuel with passengers on board is unavoidable. The pilot is incharge of the aircraft and passengers. Additional precautions should beobserved.

(b) The Ramp Controller or Helideck Officer is to be informed that refuelling will takeplace with passengers onboard.

QID 063Fuel Manual

Chapter 9

Issue 2 5 of 6

(c) Passengers are to be briefed to remain seated, with seatbelts unfastened, untiladvised fuelling complete.

(d) No smoking sign to be illuminated.

(e) Door on the refuelling side to remain closed. Door on non refuelling side toremain open. On S61 this is to include cargo door.

(f) A nominated person to be stationed at main exit door to assist passengers toevacuate aircraft should an emergency occur.

6. Defuelling

(a) Fuel defuelled from aircraft must not be returned into system until satisfactoryquality checks are obtained. This is particularly relevant if it is a non companyaircraft where the grade of fuel being used is unknown.

(b) The receiving tank should be empty at commencement of defuel, this way anycontamination can be isolated. Or a dedicated defueller used

(c) Bonding

Bonding requirements between aircraft and receiving tank should be observed.

(d) Records

Records are to be maintained of all defuelling tasks. Registration of aircraftamount taken results of any sampling and grade of fuel. The method of disposalshould also be recorded.

7. General Procedures for Refuelling

(a) Ensure adequate fire cover.

(b) Aircraft to be bonded to avoid static electrical build up.

(c) No smoking or naked lights.

(d) Personnel engaged in refuelling shall not carry any means of ignition or footwearwith studs, or exposed metal toe caps.

(e) Aircraft doors to be open whenever feasible.

(f) Under normal circumstances all passengers disembarked and not allowed backon board until fuelling complete.

QID 063Fuel Manual

Chapter 9

Issue 2 6 of 6

(g) The refuel zone should be kept clear of any obstacles to ensure quick removal ofrefuelling equipment in an emergency.

(h) Ensure fuel cap fitted and securely locked on completion.

8. General Procedures for Defuelling

(a) Equipment used for the purpose of defuelling should be properly designed for thetask. A sample taken from each defuel point prior to start.

(b) Conditions of bonding and earthing standards as for refuelling.

(c) Fire extinguishers are available.

(d) No Smoking or naked lights.

(e) All hoses should be blanked and correctly stowed when not in use.

(f) Procedures as laid down in the aircraft maintenance manual should be adheredto.

QID 063Fuel Manual

Chapter 10

Issue 2 1 of 1

Chapter 10

Offshore Fuel Installation

1. Introduction.

2. Transit Tanks.

3. Static Tanks and Sample Reclaim Tank.

4. Delivery system.

5. Recommended Maintenance Schedules.

(c) Transit Tank Trip Inspections.(d) Transit Tank Weekly Inspection.(e) Transit Tank 6 Monthly Inspection.(f) Transit Tank Recertification.

6. Storage Tanks.

7. Delivery System.

8. Daily Checks.

9. Weekly Checks.

10. Three Monthly Checks.

11. Six Monthly Check.

12. Annual Check.

13. Offshore Refuelling.

14. Samples of Offshore Inspection Sheets.

QID 063Fuel Manual

Chapter 10

Issue 2 1 of 13

Offshore Fuel Installations

1. Introduction

Due to the hostile offshore environments in which helicopters have to operate it isessential to ensure the handling, storage and refuelling is of the highest standardto ensure the quality of aviation fuel is maintained.

2. Transit Tanks

(a) Transit tanks should be constructed to satisfy the requirements of theIntergovernmental Marine Consultative Organisation (I.M.C.O) meeting theDangerous Goods Code Type 1 or Type 2 tank.

(b) Tanks may be of stainless steel or mild steel. If the latter the tank should have asuitable epoxy lining. The tank should be encased in a robust steel cage with tiedown points and four main lifting lugs. The assembly should be painted yellow,with a capacity of 600 gallons.

3.(a) Static Tanks

Where static tanks are provided they should be constructed to acceptablestandards including A.SME VIII and B.S 5500. It shall be of cylindrical shape. Itshould have sample points which are easily available. Tanks should be clearlymarked with tank capacity.

(b) Sample Reclaim Tank

If refuelling includes a bulk storage tank good samples are to be disposed of intoa dedicated reclaim tank and returned to storage tank via a water separator. Areclaim tank cannot be used if refuelling is direct from transit tank.

4. Delivery System

The delivery system to transfer fuel from the storage tank to the aircraft shouldinclude the following components.

(a) Pump

This may be electrically or air driven, centrifugal or positive displacement with aflow rate as suitable to the operation. It should be capable of delivering 22 litresper minute under normal flow conditions. A remote stop start button should belocated near the fuel cabinet on the helideck plus a flashing amber light to warnwhen pump is running.

(b) Filtration Units

Filter units including microfilters, filter water separators and fuel monitors shouldbe fitted with automatic air eliminators and sized to suit the discharge rate and

QID 063Fuel Manual

Chapter 10

Issue 2 2 of 13

the pressure of the delivery system. Units should be A.P.I 1581 approved. Filterunits should be fitted with sample lines to enable water to be drained from theunit.

(c) Flowmeter

This should be of a positive displacement type and sized to suit the flow rate.This should be regularly calibrated in accordance with manufacturersrecommendations. It is recommended the Flowmeter includes both a strainer andan air eliminator. It should be read in litres.

(d) Fuel Monitor

This should be situated between the Flowmeter and delivery hose. This unitshould be A.P.I 1583 approved and designed to absorb any water still present inthe fuel and to cut off the flow once a certain amount of water has beenexceeded, It is described as in Aviation Fuel Filter Monitor with absorbent typeelements. It should be fitted with a sample line to enable water to be drained.

(e) Delivery Hose

This should be on approved semi-conducting type to E.N. 1361 Type C standard.This should be stored on a reel suitable for the length and diameter of the hosebeing used.

(f) Bonding Cable

A suitable high visibility bonding cable should be used to earth the helicopterairframe prior to uplifting fuel. The cable should be bonded to the systempipework at one end and be fitted with a correct earthing adaptor to connect tothe aircraft.

(g) Fuelling Nozzle

The fuel delivery to the aircraft may be either by gravity or pressure refuelling. Itis beneficial to have the ability to fuel be both method s depending on type ofaircraft to be refuelled.

(h) Gravity

The nozzle should be 1 spout diameter with 100 mesh strainer. Suitable typesinclude the EMCO G180-GRTB refuelling nozzle.

(i) Pressure

For pressure refuelling the coupling should be 2 unit 100 mesh strainer. ACarter or Avery Hardoll pressure nozzle with regulator / surge control (maximum35 PSI) should be used

QID 063Fuel Manual

Chapter 10

Issue 2 3 of 13

(j) Pressure and Gravity

To meet both requirements a pressure nozzle can be fitted to the hose end. Aseparate length of hose fitted with an adaptor (to fit the pressure nozzle) andalong with the gravity nozzle attached can be used as required. This allows bothtypes of refuelling from the one installation.

5. Recommended Maintenance Schedules

(a) Different elements of the helifuel refilling system require maintenance at differenttimes ranging from daily checks on the delivery system to annual / biannualchecks on static storage tanks.

(b) Transit Tanks

All transit tanks should be subject to a trip examination each time the tank isfilled and additionally they should be checked weekly for condition. The followingsix monthly and twelve monthly inspections should be carried out on all linedcarbon steel tanks. However for stainless steel tanks, the inspections can becombined at twelve monthly intervals.

(c) Trip Inspections

(i) Each time the tank is offered for refilling the following items should be checked

(ii) Tank shell - for condition, has shell suffered any damage since its previous visit.

(iii) Visual check of filling / discharge points and sample points for condition, leakageand that caps are in place.

(iv) Visual check of lifting lugs and four point sling for signs of damage.

(v) Tank tap fittings to be checked for condition, caps in place, dirt free and watertight.

(vi) Check tank identification, serial number and contents are properly displayed.

(vii) Ensure tank certificate is valid and located in the document container.

(d) Weekly Inspections

Each tank whether it is full or empty, onshore of offshore should be given aweekly check similar to the trip inspection, to ensure that the tank remainsserviceable for the purpose. The weekly check should be primarily for damageand leakage. The completion of this check should be signed on the serviceabilityreport.

QID 063Fuel Manual

Chapter 10

Issue 2 4 of 13

(e) Six Monthly Inspection

The six monthly inspection should be carried out onshore by a SpecialistOrganisation such checks should include:

(i) Tank identification plate check details

(ii) Tank shell visual check for damage.

(iii) Paint condition Internal Check for deterioration.

(iv) Paint condition External Check for deterioration.

(v) Lining materials (if applicable) Check for deterioration, lifting.

(vi) Tank fittings (internal) Check condition.

(vii) Tank fittings (external) Check condition.

(viii) Access manhole Check security.

(ix) Pressure release valve Check condition, particularly for leaks.

(x) Dipstick assembly Check markings and cover for security.

(xi) Bursting disc Check for integrity and cover for security.

(xii) Inspection hatch assembly Check seal condition and security.

(xiii) Bonding Measure electrical bonding resistance between tank and shell.

(xiv) General Examination and test procedures as set out in E.N. 12079

(f) Recertification

It is a legal requirement that transit tanks are re-certified by an authorised FuelInspector functioning under the verification scheme at least every five years, withan intermediate check every 2 years. This includes recertification of pressure /vacuum relief valve. The date of certification should be stamped on the tankinspection plate.

6. Storage Tanks

(a) Static storage tanks are subject to an annual or biannual inspection dependingon the type of tank. If mild steel with a lining, every 12 months. If stainless steel,every two years is permitted. When inspected the tanks should be drained andvented with manhole cover removed. The inspection should include the following.

(i) Cleanliness Clean tank bottom as required.

QID 063Fuel Manual

Chapter 10

Issue 2 5 of 13

(ii) Tank internal fittings Check condition.

(iii) Lining material (if applicable) Acetone test on new or repaired linings.

(iv) Paint condition Check for deterioration particularly around seams.

(v) Access to tank top fittings Check condition of access ladders and platforms.

(vi) Inspection hatch Check condition of seal.

(vii) Access manhole cover Check seal for condition and refit cover securely. Refilltank.

(viii) Floating suction Check operation and condition.

(ix) Valves Check condition, operation and material.

(x) Sump / drain line Check condition, operation and material.

(xi) Grade identification Ensure Jet A1 markings applied and clearly visible.

(xii) Contents gauge Check condition and operation.

(xiii) Bonding Measure electrical bonding resistance between tank and systempipework.

7. Delivery System

The offshore delivery system should nominally be inspected by the helicopteroperator every three months. However the inspection may be carried out by aspecialised contractor on behalf of the helicopter operator. No system shouldexceed four months and have daily and weekly checks by offshore fuellingpersonnel.

8. Daily Checks

(a) Microfilter and/or filter/water separator and filter monitor. Drain fuel from sumpuntil clear. The sample should be clear, bright and free of solid matter. Thesample should be further checked by using a syringe and water detectioncapsules. Filter vessel and hose samples should be taken under pump pressure.

(b) Storage tank A fuel sample should be drawn from each compartment of thestorage tank and checked as above (Para a).

(c) A sample should also be drawn from hose end and again checked as for (Paraa).

(d) These daily checks should be recorded (on daily check sheets) and held on file.

QID 063Fuel Manual

Chapter 10

Issue 2 6 of 13

(e) Fuel samples taken should be retained for seven days, so that they may beanalysed in the event of an incident.

9. Weekly Checks

(a) The following checks should be carried out each week (in addition to the dailychecks).

(b) Differential pressure gauge. During refuelling differential pressure gauge readingshould be noted and recorded on filter record sheet.

(c) Entire system including transit tank. Inspect for leaks and general appearance.

(d) Tank tap fillings. Should be checked for security, clean and watertight.Inlet and outlet couplings Check caps in place.

(e) Hose and strainers. Check for condition, inspect strainers.

(f) Floating Suction Check for buoyancy and free movement.

(g) Delivery Hose Inspect for condition, record findings of inspection on the hoseinspector record.

(h) Delivery nozzle / coupling Bonding wire and clip for condition, carry outcontinuity check, should not exceed 0.5 ohms.

(i) Bond reel Check for general condition, carry out continuity check, should notexceed 0.5 ohms.

(j) On completion, record findings on serviceability report.

10. Three Monthly Checks

(a) A three monthly check is the major inspection of the System and should becarried out by an authorised Fuel Inspector. The following is a general guide;systems will vary according to type of installation.

(b) All filtration units, i.e. decant line, dispenser and monitor filter, obtain fuel sample,carry out water and Shell capsule checks, record findings. Further investigationrequired if sample fails.

(c) Check earth bonding between transit tank and main storage.

(d) Inspect fuel hose and coupling for damage, leaks, correct operation and fuel capin place.

(e) Pump unit Remove, clean and inspect strainers. If air driven, service air linelubricator, regulator and water separator unit as per manufacturers instructions.

(f) Hose reel Ensure reel operates correctly, service as required.

QID 063Fuel Manual

Chapter 10

Issue 2 7 of 13

(g) Differential pressure gauge Check for correct operation, renew filter element ifdifferential pressure limit exceeded. Prime unit and check operation of aireliminator.

(h) Delivery Hose Carry out visual inspection of complete hose assembly.Functional check to ensure correct lock off and no leaks. Inspect cone strainer.Check security of bonding leads and carry out continuity check, 0.5 ohms max.Ensure all dust caps are present and secure.

(i) Bonding system Check for security, correct operation of reel and connectors.Carry out continuity check, should not exceed 0.5 ohms.

11. Six Monthly Check

(a) This should again only be carried out by and authorised Fuel Inspector. It is toinclude all items in three monthly check plus additional items.

(b) Ensure all filtration units, pipework and associated system units have correct fuelgrade identity.

(c) Electrical PumpsTo be inspected and maintained in accordance with manufacturers instructions.

(d) Air Driven PumpsTo be inspected and maintained in accordance with manufacturers instructions.

(e) Metering UnitCheck operation of air eliminator, lubricate gears as applicable. Clean andinspect strainer element.

(f) Hose ReelCheck tension on chain drive, lubricate bearings.

12. Annual Check

(a) To be carried out by authorised Fuel Inspector. Consist of all three and six monthinspection items, plus the following.

(b) All filtration units Transfer, water separator and monitor filter. Remove anddiscard existing elements and shrouds. Clean out vessel, check for any signs ofdeterioration. Fit replacement units plus new seal and gaskets. Annotate filterbody with date of last element change, and when next due.

(c) Delivery Hose Ascertain when hose was fitted from system records. Should berecertified every two years, or earlier if defects are found. The hose has a tenyear life from date of manufacture.

(d) Fuel Delivery Meter

This may require calibration, manufacturers instructions to be followed.

QID 063Fuel Manual

Chapter 10

Issue 2 8 of 13

Note. Authorised Fuel inspectors will raise a report for all three, six and annualchecks. These reports should be copied to all relevant offshore helicopteroperators.

13. Offshore Refuelling

(a) Passengers should normally be disembarked and clear of the helideck. Fire crewto be in attendance.

(b) When aircraft captain advises quantity and grade of fuel required, run out deliveryhose. Take sample from nozzle end and carry out water detection check withShell capsules. Pilot or Co-pilot should be shown results of the test

(c) Attach main bonding lead to aircraft, if gravity refuelling connect secondarybonding lead from nozzle to aircraft. Open tank filler and insert nozzle. Forpressure refuelling connect hose to aircraft connection.

(d) The nominated person in charge should operate system pump, second man onthe nozzle, connection end. Pump off switch to be activated if any problemsoccur.

(e) On completion remove nozzle or disconnect pressure coupling replace aircraftfuel cap, disconnect secondary bonding lead. Carry out further water samples,show to pilot.

(f) Remove delivery hose from helideck, remove main bonding lead.

(g) Enter fuel quantity uploaded onto daily refuelling sheet and obtain pilots signaturefor the fuel received.

(h) If for safety reasons the captain of the aircraft decides the passengers cannot bedisembarked the following safety precautions shall apply.

(i) Constant communication between pilot and refuelling crew.

(j) Passengers should be briefed, seatbelts undone.

(k) A Competent person positioned to supervise disembarkment in the event of anemergency.

(l) The emergency exits should be unobstructed and ready for use.

Note:All inspection sheets included in this manual are for general guidance andshould be utilised in conjunction with local additional requirements.

QID 063Fuel Manual

Chapter 10

Issue 2 9 of 13

OFFSHORE HELICOPTER REFUELLING EQUIPMENTWEEKLY AND MONTHLY SERVICEABILITY REPORT

OPERATION / LOCATION MONTH/YEAR

SHEET No.

WEEKLY CHECKS: WEEK

COMPONENT CHECK 1 2 3 4

Fuelling equipment,including Transit Tanks

1. Entire System: Free from leaks, generalappearance satisfactory.

2. Tank Top Fittings: Caps in place, dirt andwater tight.

3. Inlet and Outlet Couplings: Caps in place.

4. Check tank Serial No. and fuel gradeidentification is correct.

* * * *

Transit Tanks 5. Check lifting lugs for damage.

Quality Control TestEquipment

6. Following items available; glass jar,syringe and water detector capsules.

Fire Extinguishers 7. Required number in position.

Microfilter and F/WaterSeparator

8. Record pressure drop on DifferentialPressure Record

Storage Tank 9. Floating Suction: Buoyancy.

Delivery Hose 10. Inspect iaw Hose Inspection Record Format Chp 12

11. Free from leaks, cap in place

12. Strainer: remove, clean, replace ifnecessary

Delivery Nozzle

13. Bonding Wire and Clip: Security andgeneral condition

* Initial column to indicate satisfactory condition.

Record deficiencies and corrective action on reverse of form

QID 063Fuel Manual

Chapter 10

Issue 2 10 of 13

OFFSHORE HELICOPTER REFUELLING EQUIPMENTWEEKLY AND MONTHLY SERVICEABILITY REPORT

OPERATION / LOCATION MONTH/YEAR

SHEET No.

MONTHLY CHECKS:

COMPONENT CHECK * INITIAL

Bonding Reel 1. Electrical continuity.iaw Electrical Bonding Form at Chp 12

* Initial column to indicate satisfactory condition.

Record deficiencies and corrective action below.

RECORD OF DEFICENCIES AND CORRECTIVE ACTION SIGNATURE DATE

QID 063Fuel Manual

Chapter 10

Issue 2 11 of 13

OFFSHORE INSPECTION

OPERATION/LOCATION: DATE SIGNATURE3 MONTHLY1. Filtration Units:

Take water sediment sample, inspect forcontamination and mechanical damage.

2. Pump Unit:Remove, clean and inspect strainers.

3. Air Pump Units:Service the following:-Air line lubricator.Regulator.Water separator unit.

4. Hose Reel:Lubricate mechanism and rewind gears.

5. Delivery Pressure Coupling/Nozzle:Check lock-off operation (Pressure Coupling).Check for leakage.Clean and inspect strainers.

6 MONTHLY1. Differential Pressure Gauge:

Check operation.2. Automatic Air Eliminator, (if fitted):

Check operation.3. Fuel grade Identification:

Check correct identification for fuel type.4. Electrical Drive Motor, (if fitted):

Check gearbox oil level and drive couplings.5. Air Drive Motor, (if fitted):

Lubricate air motor bearings and check gearbox oillevel and drive couplings.

6. Meter Register Head, Drive Gears and CalibrationGears:Lubricate with Vaseline.

7. Metering Unit:Lubricate bearings.

8. Hose Reel:Lubricate bearings

1 YEAR1. Filter Separator:

Replace element and clean housing.

QID 063Fuel Manual

Chapter 10

Issue 2 12 of 13

OFFSHORE FUEL AND ISSUE ACCEPTANCE

PRE DELIVERY NOZZLE SAMPLE CHECKED END DELIVERY NOZZLE SAMPLEGRADE OF FUEL RIG OPERATOR: PILOT FINAL ACCEPTANCE:

DATE TIME HELICOPTERREGISTRATIONMETER

READING

A/C INDICATINGSYSTEMREADING

OPERATORSIGNATURE

QTYISSUE METER

READING

A/C INDICATINGSYSTEMREADING

PILOTSIGNATURE

NOTES:Final acceptance signature acknowledges that the Pilot has seen both samples tested and both were free of contamination and totaluplift of fuel has been checked against Bowser/Dispenser delivery figures and aircraft indicating system figure.

Dispose of Nozzle samples by appropriate means, (satisfactory samples may be returned to storage tank)

QID 063Fuel Manual

Chapter 10

Issue 2 13 of 13

OFFSHORE HELICOPTER REFUELLING EQUIPMENT DAILY CHECKS OF FUEL QUALITY

OPERATION/LOCATION: SHEET No.

STORAGE TANK SAMPLES

DATE TANK No. GRADE P C S FUEL COLOUR &APPEARANCETIME OFCHECK

FLOATINGSUCTIONCHECK

SIGNATURE

P = Presence of free water. C = Detector capsule. S = Sediment. Mark* When storage tanks water checked after heavy rain.

QID 063Fuel Manual

Chapter 11

Issue 2 1 of 1

Chapter 11

Sampling Procedures

1. Introduction & Water Contamination

2. Microbiological Contamination.

3. Visual Water Checks.

4. Chemical Capsule Water Checks.

5. Density Check.

6. Bulk Fuel Samples.

7. Aircraft Fuel Samples.

8. Storage of Samples.

9. Conductivity Test.

10. Millipore Test.

QID 063Fuel Manual

Chapter 11

Issue 2 1 of 5

Sampling Procedures

1. During the handling of aviation fuel sampling checks will be required to ensurethat fuel intended for use is fit for that purpose.

Water Contamination

(a) Dissolved Water

Water molecules are present in Jet A1 as part of its chemical structure. Providedthe water remains chemically combined with the fuel it prevents no hazard toaircraft.

During manufacture the fuel is hot and is therefore able to hold a relatively largequantity of water. Once it is put into storage tanks it cools and the watercondenses to form water droplets. Any rise in temperature will allow the fuel toreabsorb the droplets.

(b) Suspended Water

A very fine mist of water droplets suspend in fuel, which can cause it to take on acloudy appearance, if present in sufficient quantity. At very low concentration thefuel will appear clear. Suspended water will gradually settle to the bottom of thetank, forming large droplets of free water.

(c) Free Water

When sampling fuel, free water will appear as a layer lying on the bottom of theglass sample jar, or on the side.

2. Microbiological Contamination

Micro organisms (microbes) are microscopic living forms, including bacteria andfungi.

(a) Bacteria

Bacteria are single celled organisms. Certain types of bacteria can use aviationfuel for growth.

(b) Fungi

Larger than bacteria, they produce spores which germinate in the presence ofwater and then uses fuel for food.

(c) Clasdosporium Resinae

Most common fungi in aviation fuel, recognised as a green/brown slime.

QID 063Fuel Manual

Chapter 11

Issue 2 2 of 5

(d) Filter Contamination

Microbiological contamination may cause spots to form and grow. Severe growthcan cause clogging of filters and render coalescer elements ineffective.

(e) Biocide Agent

Micro biological growth can be treated by using Biobar J.F. But correctapplication of this product is only to be used under strict guidance by the aircraftor fuel manufacturer. It is much better to eliminate the presence of water withoutwhich it cannot form.

3. Water Contamination Checks

(a) Drain fuel sample into clear clean glass container, minimum 0.5 litres for aircraftfuel tanks. 2.5 litres for bulk storage, i.e. Bowsers and Bulk Storage.

(b) Swirl container to create vortex, any free water and solids will tend to collectbeneath the vortex. Check for:

(i) Sediment.(ii) Globules of water.(iii) Cloudiness.

(c) If nothing abnormal noted and sample clean and bright fuel satisfactory toproceed to chemical water detection fuel inspection. If it fails, repeat up to amaximum of 3 times. If still not satisfactory, further investigation is required.

4. Chemical Water Detection

(a) Check capsules to ensure they are in date; this is normally annotated of the endof tube. Stocks last 9 months from the date of manufacture.

(b) Place capsule on the end of a syringe, immerse in the fuel and draw 5mls of fuelin to syringe and withdraw.

(c) In the event of contamination the capsule will have changed colour from yellow togreen. If no colour change observed fuel is deemed to be satisfactory. A doublecheck to ensure capsule working correctly is to spit on it. This should immediatelyresult in a colour change.

(d) If test fails draw another sample to a maximum of three and retest, failure isreason for further investigation.

QID 063Fuel Manual

Chapter 11

Issue 2 3 of 5

5. Density Check

Also referred to as S.G. (Specific Gravity)

(a) Pour sample into a clean clear hydrometer jar, stand on level surface.

(b) To carry out this test a thermometer with a scale not greater than 0.5C will berequired, also a hydrometer with a scale no greater than 0.0005 Kg/litre. Theaccuracy of these instruments should be checked every six months against areference instrument.

(c) Check thermometer and hydrometer to ensure they are undamaged.

(d) Place thermometer in jar, allow to stabilise. Read temperature and record.

(e) Lower hydrometer gently into jar, spin to ensure it is not sticking to the side.Read hydrometer at the point where it penetrates the fuel surface and recordobserved density.

(f) Convert observed density to a corrected standard value of 15C using anapproved set of tables as published by the A.S.T.M. (American Society forTesting and Materials.)

(g) If taking a delivery of fuel, the figure obtained should be compared to that on therelease note. This should not vary by more than 0.003 Kg/litre. If this is not thecase contamination may be present and further investigation required prior toacceptance.

6. Retained Samples

Bulk Fuel

(a) A sample of 2.5 litres should be retained for 7 days.

(b) From all deliveries.

(c) From bulk tanks, hydrant system, or bowser prior to start of days refuelling orpossible defuelling.

(d) Whenever samples are for laboratory testing and should be retained until resultof analysis is known.

7. Aircraft Samples

(a) Minimum sample of 0.5 litres taken from aircraft fuel tank. Retain for 24 hours

(b) To be taken before first flight of the day.

(c) Before defuelling.

QID 063Fuel Manual

Chapter 11

Issue 2 4 of 5

(d) This applies to all aircraft that are fit to fly with fuel onboard. Only aircraft onextended maintenance are excluded. But must have sample taken prior torunning engines and return to line.

8. Storage of Samples

All samples should be stored in a cool fireproof environment out of daylight andlabelled with the following information.

(a) Grade of fuel.

(b) Reason for sample.

(c) Date and the sample taken.

(d) Location sample drawn from, i.e. Aircraft registration, number of bulk tank.

(e) Name of person doing sampling.

9. Conductivity and Millipore Tests.

These are two other tests that can be carried out in the field should they berequired. An outline or how to conduct these is given. Special test equipment isrequired.

(a) Conductivity Check

Freshly manufactured fuel has virtually no conductivity, it is an insulator. Toensure safe handling during distribution, refuelling and whilst onboard the aircraftrequires the dissipation of static charges. Fuel is therefore dosed with approvedadditive Stadis 450 prior to dispatch from bulk storage to the level for Jet A1 of50 450 Pico-Siemens per metre.

(b) Because the procedure can be adversely affected by additives and time, theselevels need to be monitored.

(c) The equipment required to carry out this test is an Emcee meter it is hand heldand before use the zero and internal calibration should be checked prior to useas per manufacturers instructions.

(d) Emcee meters should only be immersed up to the probe nut. Readings should betaken within 2 3 seconds of immersion. Meters are normally accurate to 5Ps/m

QID 063Fuel Manual

Chapter 11

Issue 2 5 of 5

10. Millipore Test

This test is used to asses the cleanliness of fuel as it passes through a system.

(a) To carry out this test a Millipore test kit is required. Connect kit into the system,within the kit a single and double filter membrane is utilised.

(b) Pass five litres of fuel through the membranes in order to determine colorimetricor gravimetric levels of contamination either compare with sample pads or sendaway for analysis.

QID 063Fuel Manual

Chapter 12

Issue 2 1 of 2

Chapter 12

Maintenance

1. Introduction.

2. Daily Inspection on Bulk Tank Systems.

3. Two Day Inspection on Bulk Tank Systems.

4. Weekly inspection on Bulk Tank Systems.

5. Monthly Inspection on Bulk Tank Systems.

6. Six Monthly Inspection on Bulk Tank Systems.

7. 1 Year Inspection on Bulk Tank Systems.

8. 3 Year Inspection on Bulk Tank Systems.

9. 5 Year Inspection on Bulk Tank Systems.

10. 10 Year Inspection on Bulk Tank Systems.

11. Daily Inspection on Fuelling Vehicles.

12. 2 Day Inspection on Fuelling Vehicles.

13. Weekly Inspection on Fuelling Vehicles.

14. 6 Monthly Inspection on Fuelling Vehicles.

15. 1 Year Inspection on Fuelling Vehicles.

16. 3 Year Inspection on Fuelling Vehicles.

17. 10 Year Inspection on Fuelling Vehicles.

18. Daily Inspection Hydrant Systems.

19. Two Day Inspection Hydrant Systems.

20. Weekly Inspection Hydrant Systems.

21. Monthly Inspection Hydrant Systems.

22. 3 Monthly Inspection Hydrant Systems.

QID 063Fuel Manual

Chapter 12

Issue 2 2 of 2

Chapter 12

Maintenance

23. 6 Monthly Inspection Hydrant Systems.

24. 1 Year Inspection Hydrant Systems.

25. 3 Year Inspection Hydrant Systems.

26. 10 year Inspection Hydrant Systems.

27. Hydrant Hose Couplings.

28. Records and Filing.

29. Daily Inspection Portable Pumping Equipment.

30. Two Day Inspection Portable Pumping Equipment.

31. Weekly Inspection Portable Pumping Equipment.

32. Monthly Inspection Portable Pumping Equipment.

33. 3 Monthly Inspection Portable Pumping Equipment.

34. 6 Monthly Inspection Portable Pumping Equipment.

35 1 Year Inspection Portable Pumping Equipment.

36. 3 Year Inspection Portable Pumping Equipment.

37. 10 Year Inspection Portable Pumping Equipment.

38. Inspections of Hoses.

39. Samples of Inspection Sheets.

QID 063Fuel Manual

Chapter 12

Issue 2 1 of 34

Maintenance

1. Introduction

The information contained within this section and the inspection criteria quoted isa guideline to assist in determining that maintenance levels are kept to anacceptable standard throughout the company. As an international companydifferent priorities will be relevant at certain locations. Chief Engineers thereforeneed to adopt their own maintenance work packs as appropriate. Someinspection sheets are included at the back of this chapter which may prove usefulin compiling this.

2. Daily on Bulk Tank Systems

(a) Flush sample lines.

(b) Purge water and sediment from drain cocks and filtration equipment.

(c) Carry out water and sediment check from tank sample points, Ensure sampleclean and bright.

(d)(i) Inspect refuelling hoses for cuts, abrasions and security.(ii) Nozzle strainer for cleanliness.(iii) Security of bonding lead.

(e) Record filter separator differential pressure.

3. Two Days on Bulk Tank Systems

(a) If system not used for 2 days recirculate fuel in hose back to storage tank. Beforecarrying this out it would be prudent to carry out sample check.

4. Weekly on Bulk Tank Systems

(a) Check and record buoyancy of floating suction by operating check wire.

(b) Check zero flow = zero pressure on filter separator differential pressure gauge(do not record).

(c) Check and record filter separator differential pressure at maximum flow rate.

(d) Inspect hose for cuts, abrasions, fuel nozzle filter for contamination.

(e) Inspect entire system for leaks and general condition.

(f) Check operation of high level alarm system if fitted.

QID 063Fuel Manual

Chapter 12

Issue 2 2 of 34

5. Monthly Check on Bulk Tank Systems

(a) Remove and check vent filter.

(b) Carry out bonding check on bonding lead reel.

6. Six Monthly Check on Bulk Tank Systems

(a) Pressure test on fuel hose.

7. 1 Year Check on Bulk Tank Systems

(a) Newly lined tanks inspect internally.

(b) Examine pipelines for leaks.

(c) Electrical pump, inspect connections.

(d) Inspect paintwork of system, reprotect as appropriate.

(e) Inspect hatch seals for condition.

(f) Check all hand valves for security and correct operation. All caps and cover inplace.

(g) Calibrate fuel quantity gauges I.A.W. manufacturers recommendations.

8. 3 Year Inspection on Bulk Tank Systems

(a) Replace filter elements and clean housing.

(b) Internally inspect tanks, record inspection date on outside of tank.

(c) Calibrate fuel flow gauges I.A.W. manufactures recommendations.

9. 5 Year Inspection on Bulk Tank Systems

(a) Inspect lined tanks internally, record inspection date on outside of tank.

10. 10 Year Inspection on Bulk Tank Systems

(a) Replace fuel hoses.

QID 063Fuel Manual

Chapter 12

Issue 2 3 of 34

11. Daily Inspection Fuelling Vehicles

(a) Purge water and sediment from drain cocks, tanker components and all filtrationequipment.

(b) Carry out water and sediment check, from tank bottom sample point or sump.

(c) Draw sample, until a clear and bright sample is obtained.

(d) Hoses visual inspection for general condition. Check nozzle strainer forcleanliness. Ensure bonding leads are secure.

(e) Ensure all open ended hoses, pipes and sampling points are fitted with dustcovers and caps.

(f) Carry out general inspection of vehicle.

12. Two Day Inspection Fuelling Vehicles

(a) If fuel has not been dispensed for 2 days take sample and inspect, if satisfactoryrecirculate remainder in hose back to storage tank.

13. Weekly Check Fuelling Vehicles

(a) Check and record filter separator differential pressure at maximum flow rate.

(b) Inspect hose for cuts, abrasions and general condition. Check nozzle filter.

(c) Inspect system for leaks.

(d) Carry out bonding check on bonding lead end reel.

14. 6 Monthly Inspection on Fuelling Vehicles

(a) Carry out bonding check from dispenser to nozzle.

(b) Carry out pressure test on hose,

15. 1 year Inspection on Fuelling Vehicles

(a) Inspect internal condition of tank compartment, record findings.

(b) Examine pipelines for leaks.

(c) Calibrate fuel quantity gauges.

QID 063Fuel Manual

Chapter 12

Issue 2 4 of 34

16. 3 Year Inspection Fuelling Vehicles

(a) Replace filter elements, clean housing.

(b) Calibrate fuel flow gauges.

17. 10 Year Inspection Fuelling Vehicles

(a) Replace hoses.

18. Daily Inspection Hydrant System

(a) Carry out water drain of all filter separators, filter monitors, micro filters and otherdrain

points.

(b) Draw sample, until a clear and bright sample is obtained.

(c) Hoses - visual inspection for general condition. Check nozzle strainer forcleanliness. Ensure bonding leads are secure.

(d) Ensure any open ended hoses, pipes and sampling points are fitted with dustcaps or

plugs.

19. Two Day Inspection Hydrant System

(a) If fuel has not been dispensed for two days take sample, if satisfactory recirculatefuel in hose to storage tank.

20. Weekly Inspection Hydrant System

(a) Check and record filter separator differential pressure at maximum flow,

(b) Ensure hydrant pits are clean.

(c) Flush all low print drains, with the line under pressure, until a clear bright sampleis obtained.

(d) Inspect hose for general condition.

21. Monthly Inspection Hydrant System

(a) Carry out bonding check on lead end reel.

QID 063Fuel Manual

Chapter 12

Issue 2 5 of 34

22. 3 Month Inspection Hydrant System

(a) If hydrant pit has not been used for 3 months flush contents of spur line.

23. 6 Month Inspection Hydrant System

(a) Carry out bonding check, from dispenser to nozzle.

(b) Clean hydrant pit cover seal.

(c) Carry out pressure test on hose,

24. 1 year Inspection Hydrant System

(a) Examine pipelines for leaks.

(b) Calibrate fuel quantity gauges.

25. 3 Year Inspection Hydrant System

(a) Replace filter separator element and clean housing.

(b) Calibrate fuel flow gauges.

26. 10 Year Inspection Hydrant System

(a) Replace hoses.

27. Hydrant Hose Couplings

Selector pins or set screws are installed to prevent the possibility of incorrect fuelselection. These must be correctly installed in the coupling lug ring. A newcoupling will not have these pins fitted.

Position 1 Avgas 100 (100/130 grade)Position 2 Formerly used for 108/135 gradePosition 3 Avgas 115 (115/145 grade)Position 4 Jet A1 (AFT 650)Position 5 Jet B (JP 4)

28.Records should be kept of all fuel deliveries into and from hydrant, allmaintenance and inspections carried out plus history of hose inspections, andheld on file.

QID 063Fuel Manual

Chapter 12

Issue 2 6 of 34

29. Daily Inspection Portable Pumping Equipment

(a) Check last grade of fuel used, flush if necessary.

(b) Carry out water drain of all filter separators, filter monitors, micro filters and anyother drain points on the equipment.

(c) Hoses Carry out visual inspection for general condition, check filter in fuelnozzle, check bonding leads are secure.

(d) Ensure all open hoses, pipes and sampling points have dust caps or plugs fitted.

(e) Check and record filter separator differential pressure when dispensing fuel.

(f) Examine suction strainer filter.

30. Two Day Inspection Portable Pumping Equipment

(a) If fuel has not been dispensed for two days, take sample. If satisfactory,recirculate hose contents back to tank.

31. Weekly Inspection Portable Pumping Equipment

(a) Check zero flow = zero pressure on filter separator differential. (Do not record.)

(b) Check and record filter separator differential pressure at maximum flow rate.

32. Monthly Inspection Portable Pumping Equipment

(a) Carry out bonding check on bonding lead.

33. 3 Monthly Inspection Portable Pumping Equipment

(a) Carry out Millipore check if fuel quality is suspect.

34. 6 Monthly Inspection Portable Pumping Equipment

(a) Carry out external inspection of all equipment.

(b) Pressure test hoses.

QID 063Fuel Manual

Chapter 12

Issue 2 7 of 34

35. 1 Year Inspection Portable Pumping Equipment

(a) Inspect mechanical condition of pump.

(b) Inspect electrical condition of pump (as applicable).

(c) Examine pipelines for leaks.

(d) Check all valves within the system operate correctly.

(e) Calibrate fuel quantity gauges.

36. 3 Year Inspection Portable Pumping Equipment

(a) Calibrate fuel flow gauges.

(b) Replace filter separator element and clean housing.

37. 10 Year Inspection Portable Pumping Equipment

(a) Replace hoses.

38. HOSE INSPECTIONS

Weekly Inspection and 3 Monthly Offshore Inspections (CAP 437 refers)

(a) Fully extend the hose and apply full pump operating pressure with the deliverynozzle closed.

(b) With hose under pressure, inspect for external damage, soft areas, blistering,leakage and other signs of weakness.

(c) Inspect 45 cm, (18 inch), section of hose at coupling end for soft spots, blistering,coupling slippage, etc.

2 Years OFFSHORE

(a) Replace hose or pressure test, (iaw Pressure test method Below).

6 Months ONSHORE

(a) Carry out pressure test as below

10 Years ONSHORE and OFFSHORE

(a) Replace hose.

QID 063Fuel Manual

Chapter 12

Issue 2 8 of 34

Pressure Test Method

(a) Remove the hose form the unit and lay on the ground in a straight line. Removethe delivery nozzle or coupling. Connect one end of the hose to a hydrostatic testpump and fit a plug incorporating a mall air bleed valve, to the other end of thehose.

(b) Open the small air bleed valve and start to fill the hose with fuel, (the grade offuel currently in use). Continue to fill the hose until all the air is bled form thehose and close the air bleed valve.

(c) Gradually apply 1 times working pressure and maintain for not less than 3minutes.

(d) With the hose under pressure, examine as per items 2 and 3 of the WeeklyInspection.

(e) Release pressure in the hose. Drain the hose and refit the coupling(s). Carry outleak check on refitted coupling(s). Drain test pump, (to prevent contamination offuture tests).

QID 063Fuel Manual

Chapter 12

Issue 2 9 of 34

AIRCRAFT FUELLING VEHICLE DAILY INSPECTION

VEHICLE MAKE MONTH..

VEHICLE NUMBER .. DATE SIGNATURE11. CHECK DERV.

Top up as required with correct fluid. See * 232. CHECK MENGINE OIL LEVEL

Top up as required. 453. CHECK RADIATOR WATER LEVEL

Top up as required with correct fluid. See* 6

74. CHECK BRAKE FLUID LEVELTop up as required with correct fluid. See* 8

5. CHECK ALL LIGHTS, HORNS, WIPERS 9106. CHECK FIRE EXTINGUISHERS

For condition and security. 11127. CHECK NOZZLES & COUPLING CAPS

For condition and security 13148. CHECK TANK AND PUMP EQUIPMENT

For leaks; Report any to duty fuel fitter. 15169. CHECK REFUEL HOSE

For obvious damage. 171810. CHECK BONDING LEADS AND CLIPS

For condition and security. 192011. CHECK TYRE AND WHEEL NUTS

For condition. 212223

12. CHECK CAB CLEANLINESS.CHECK EYEWASH BOTTLEFor cap seal damage, replace bottle if seal

broken. 242513. CHECK ALL WATER DRAIN CAPS

Are fitted and secure. 262728

14. CHECK EXHAUST SYSTEMFor condition and security. Check system does

not emit sparks or flames. 293015. CHECK GENERAL CONDITION OF VEHICLE31

* IF IN DOUBT SEE MT SECTION

QID 063Fuel Manual

Chapter 12

Issue 2 10 of 34

STORAGE TANKS CHECKS BEFORE AND AFTER REPLENISHMENT

GRADE MONTH YEAR OPERATION / LOCATION SHEET No.

BEFORE REPLENISHMENT AFTER REPLENISHMENT AFTER SETTLEMENT

SUMP SUMP

DATE

DELIVERYNOTE orTICKET

NUMBER

TANKNo.

C SCOLOUR TIME SIGNATURE

FUELUPLIFT

(LITRES)TIME

CLOSED SIGNATURE C SCOLOUR TIMEREADY

DATEREADY

SIGNATURE

01

02

03

04

05

06

07

08

09

10

11

12

13

14

15

C = Detector Capsule S = Sediment

QID 063Fuel Manual

Chapter 12

Issue 2 11 of 34

STORAGE TANKS CHECKS BEFORE AND AFTER REPLENISHMENT

GRADE MONTH YEAR OPERATION / LOCATION SHEET No.

BEFORE REPLENISHMENT AFTER REPLENISHMENT AFTER SETTLEMENT

SUMP SUMP

DATE

DELIVERYNOTE orTICKET

NUMBER

TANKNo.

C SCOLOUR TIME SIGNATURE

FUELUPLIFT

(LITRES)TIME

CLOSED SIGNATURE C SCOLOUR TIMEREADY

DATEREADY

SIGNATURE

16

17

18

19

20

21

22

23

24

25

26

27

28

29

30

31

C = Detector Capsule S = Sediment

QID 063Fuel Manual

Chapter 12

Issue 2 12 of 34

WEEKLY DISPENSER/BOWSER INSPECTION REPORTBowser Number Month: Sheet Number:

Tank InternalCheck

Gauge andControls

Nozzle andFilter Hose and Reel Bonding Check Date Due ReplacementWeek

No.SAT UNSAT SAT UNSAT SAT UNSAT SAT UNSAT SAT UNSAT FILTER FRONTHOSE

REARHOSE

SIGNATURE

1

2

3

4

5

NOTES: 1. The hose pressure is checked with the delivery pump running (Refer to Chapter 12 Para 38).2. Clean the filter housing when replacing the filter element.3. Record Defects:

............................................

4. Action Taken: ..

QID 063Fuel Manual

Chapter 12

Issue 2 13 of 34

DAILY RAMP WATER TESTS (MOBILE & STATIC UNITS)

DATE MONDAY

DISPENSERS BOWSERS

No. FILTER NOZZLE No. SUMP FILTER NOZZLE LOW POINTS

C S C S SIGNATURE C S C S C S SIGNATURE C S SIGNATURE

N/A

TIME CHECKS COMPLETED: TIME

DATE TUESDAY

DISPENSERS BOWSERS

No. FILTER NOZZLE No. SUMP FILTER NOZZLE LOW POINTS

C S C S SIGNATURE C S C S C S SIGNATURE C S SIGNATURE

N/A

TIME CHECKS COMPLETED: TIME

DATE WEDNESDAY

DISPENSERS BOWSERS

No. FILTER NOZZLE No. SUMP FILTER NOZZLE LOW POINTS

C S C S SIGNATURE C S C S C S SIGNATURE C S SIGNATURE

N/A

TIME CHECKS COMPLETED: TIME

C = Detector Capsule S = Sediment

QID 063Fuel Manual

Chapter 12

Issue 2 14 of 34

DAILY RAMP WATER TESTS (MOBILE & STATIC UNITS

DATE THURSDAY

DISPENSERS BOWSERS

No. FILTER NOZZLE No. SUMP FILTER NOZZLE LOW POINTS

C S C S SIGNATURE C S C S C S SIGNATURE C S SIGNATURE

N/A

TIME CHECKS COMPLETED: TIME

DATE FRIDAY

DISPENSERS BOWSERS

No. FILTER NOZZLE No. SUMP FILTER NOZZLE LOW POINTS

C S C S SIGNATURE C S C S C S SIGNATURE C S SIGNATURE

N/A

TIME CHECKS COMPLETED: TIME

DATE SATURDAY

DISPENSERS BOWSERS

No. FILTER NOZZLE No. SUMP FILTER NOZZLE LOW POINTS

C S C S SIGNATURE C S C S C S SIGNATURE C S SIGNATURE

N/A

TIME CHECKS COMPLETED: TIME

DATE SUNDAY

DISPENSERS BOWSERS

No. FILTER NOZZLE No. SUMP FILTER NOZZLE LOW POINTS

C S C S SIGNATURE C S C S C S SIGNATURE C S SIGNATURE

N/A

TIME CHECKS COMPLETED: TIME

C = Detector Capsule S = Sediment

QID 063Fuel Manual

Chapter 12

Issue 2 15 of 34

HYDRANT DISPENSER DAILY SAMPLING AND PURGING

GRADE MONTH YEAR OPERATION / LOCATION SHEET No.

VEHICLE No. TYPE

1 2 3 4 5 6 7 8 9 10

FILTER/SEPARATOR MONITOR MAIN DRAINDAT

E

INPUTLINE

DRAIN

MAINGAUZEFILTER INLET OUTLET SUMP INLET OUTLET

RELAXTANK

DUMPTANKDRAIN

SHOCKALLE-

VIATORFRONT REAR

DELIVERYLINE

FUELColour

*CHECKTYPE /TIME

SIG

P C S P C S P C S P C S P C S P C S P C S P C S P C S P C S P C S P C S P C S

P = Paper Columns appropriate to Vehicle:- * Annotate CheckC = Capsule F11-1 columns 1, 3 (Inlet / Outlet) 4, 6, 9 (top deck), 10 (Enter under type)S = Sediment Hamble columns 1, 3 (Outlet / Sump), 6, 10 A All drain points

Kennet columns 1, 3, 6, 7, 8, 10 C After defuellingTigris columns 1, 2, 3 (Sump), 5, 6, 9 (Hose reel), 10 D After heavy rain or snowTamar Mk3 columns 3 (Inlet), 10Taycor columns 3 (Inlet), 10

QID 063Fuel Manual

Chapter 12

Issue 2 16 of 34

HOSE INSPECTION RECORD

FUEL GRADE ... HOSE DIAMETER..LOCATION...

DATE HOSE DUE REPLACEMENT (OR PRESSURETEST).

HOSE ULTIMATE LIFE EXPIRY DATE..

(Refer to Chapter 5)

DATE RESULT SIGNATURE

Note: Retain record for the life of the hose.

QID 063Fuel Manual

Chapter 12

Issue 2 17 of 34

HYDRANT DISPENSER WATER GRADE CHECK AFTER AIRCRAFT FUELLING

OPERATION / LOCATION SHEET No.

FILTER / SEPARATOR* DRAIN POINT HYDRANT POINT

DATE AIRCRAFTREG. No.AIRCRAFT

TYPEP C S

FUELCOLOUR &APPEARANCE

TIME OFCHECK STAND

No.INNEROUTER

ACTION SIGNATURE

P = Paste C = Detector Capsule S = Sediment* If water found, Chief Engineer and Pilot to be advised immediately, filter / separator purged and investigation made to discoverreason for presence of water. Carry out Daily Inspection iaw Chapter 12 Para 18.

QID 063Fuel Manual

Chapter 12

Issue 2 18 of 34

GAUZE FILTER INSPECTION

OPERATION / LOCATION..

DATE FILTERNUMBER

GRADE FILTERCONDITION

ACTIONTAKEN

TIMECHECKED

SIGNATURE

QID 063Fuel Manual

Chapter 12

Issue 2 19 of 34

FUEL FILTER MONITOR DIFFERENTIAL PRESSURE GRAPH RECOR SHEET No.

GRADE OF FUEL LOCATION ELEMENT TYPE SER No.

DATE ELEMENT DUE CHANGE MANUFACTURER MAX. DIFF.PRESS.

MAX RATED FLOW OF FILTER MAX DIFF PRESS RECORDED

Notes: 1. Change element when Date Element Due Change or manufacturer Max. Differential Pressure is reached.2. Investigate, if differential pressure changes suddenly.3. Place X in box for date and Differential Pressure indicated

INITIALSDATEDIFFERENTIAL PRES(PSI)222120191817161514131211109876543210MONTH DAY 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31

QID 063Fuel Manual

Chapter 12

Issue 2 20 of 34

FUEL FILTER SEPARATOR DIFFERENTIAL PRESSURE GRAPH RECOR SHEET No.

GRADE OF FUEL LOCATION ELEMENT TYPE SER No.

DATE ELEMENT DUE CHANGE MANUFACTURER MAX. DIFF.PRESS.

MAX RATED FLOW OF FILTER MAX DIFF PRESS RECORDED

Notes: 1. Change element when Date Element Due Change or manufacturer Max. Differential Pressure is reached.4. Investigate, if differential pressure changes suddenly.5. Place X in box for date and Differential Pressure indicated

INITIALSDATEDIFFERENTIAL PRES(PSI)222120191817161514131211109876543210MONTH DAY 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31

QID 063Fuel Manual

Chapter 12

Issue 2 21 of 34

FUEL QUALITY CONTROL RECORD DAILY CHECKS

GRADE MONTH YEAR OPERATION / LOCATION TANKERBOWSER No.

HOSE SAMPLE

DATE TIMEWATER SEDIMENT COLOUR

FILTERAND

DRAINPURGE

SUMPDIP

HOSEENDFILTER

FAULTS AND CHECKS AFTERPROLONGED HEAVY RAIN /SNOW ETC.

SIGNATURE

01

02

03

04

05

06

07

08

09

10

11

12

13

14

15

V = Satisfactory X = Unsatisfactory (Record Corrective Action) N = Not Applicable

QID 063Fuel Manual

Chapter 12

Issue 2 22 of 34

FUEL QUALITY CONTROL RECORD DAILY CHECKS

GRADE MONTH YEAR OPERATION / LOCATION TANKERBOWSER No.

HOSE SAMPLE

DATE TIMEWATER SEDIMENT COLOUR

FILTERAND

DRAINPURGE

SUMPDIP

HOSEENDFILTER

FAULTS AND CHECKS AFTERPROLONGED HEAVY RAIN /SNOW ETC.

SIGNATURE

16

17

18

19

20

21

22

23

24

25

26

27

28

29

30

31

V = Satisfactory X = Unsatisfactory (Record Corrective Action) N = Not Applicable

QID 063Fuel Manual

Chapter 12

Issue 2 23 of 34

ELECTRICAL BONDING METHOD

Maximum resistance between fuel system and earth must not exceed one ohm: theresistance between bonded points of the system must not exceed 0.05 ohms.Measurements are to be made using low voltage type bonding tester.

BONDING AND ELECTRICAL RECORD

DATE POSITION ITEM TEST OR WORK CARRIEDOUT

RESULT

QID 063Fuel Manual

Chapter 12

I