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S/N TECHNICAL SPECIFICATION COMPLY NOT COMPLY 1 MAINFUNCTION 1.1 The hi-lift is to be used for transferring all types of catering modules of not more than 4,000 kg into and out of the main decks of all aircraft types, especially for A380 (main deck only), 2 STATUTORY REQUIREMENTS 2.1 The manufacturer of the hi-lifts is responsible for ensuring that: 2.1. the design and structural standards of the hi-lifts meet or exceed those of IATA, OSHA, SAE and any other applicable standard; 2.1. the equipment meet the requirements for registration with the Singapore Land Transport Authority and the Ministry of Environment; 2.1. the hi-lifts meet the requirements of the Singapore Aerodrome Act and the Vehicle and Equipment Construction and Use Rules; and 2.1. the hi-lifts pass the certification test for lifting equipment of the Ministry of Manpower. 3 GENERAL REQUIREMENTS 3.1 E n viro n me n t 3.1. The hi-lift must be designed to function outdoors. Specifically, the nature of operations demand rugged, impact-resistant hardware whose functions and controls must be foolproof and failsafe, consistent with the anticipated level of unskilled labour using the 3.1. As the airport is located by the sea, stringent rust control measures must be observed in the design of the hi-lift. All hydraulic lines shall be of stainless CT1503G 013 Appendi TENDER FOR THE SUPPLY, DELIVERY TESTING AND COMMISSIONING OF A TURNKEY BASIS OF EQUIPMENT FOR FIVE (5) UNITS OF STANDARD HI-LIFTS (4000KG CAPACITY) WITH AN OPTION FOR ANOTHER FIFTEEN (15) UNITS OF STANDARD HI-LIFTS SPECIFICATIONS FOR HI-LIFT WITH AIRCONDITIONED CABIN (4000 KG CAPACITY) COMPLIANCE CHECK- LIST

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Transcript of (49466735zdvzsv6) 7 Appendsdczsdvsvix C4 - Compliance Checklist

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S/N TECHNICAL SPECIFICATION

COMPLY NOT COMPLY1 MAINFUNCTION

1.1

The hi-lift is to be used for transferring all types of catering modules of not more than 4,000 kg into and out of the main decks of all aircraft types, especially for A380 (main deck only), A310,A320,A330,A340,A350,B737, B747, B757,B767,B777B787,DC10,MD11& MD82 aircraft

2 STATUTORY REQUIREMENTS2.1 The manufacturer of the hi-lifts is responsible for ensuring that:

2.1.1the design and structural standards of the hi-lifts meet or exceed those of IATA, OSHA, SAE and

any other applicable standard;2.1.2

the equipment meet the requirements for registration with the Singapore Land Transport

Authority and the Ministry of Environment;2.1.3

the hi-lifts meet the requirements of the Singapore Aerodrome Act and the Vehicle and Equipment

Construction and Use Rules; and2.1.4 the hi-lifts pass the certification test for lifting equipment of the Ministry of Manpower.

3 GENERAL REQUIREMENTS3.1 E n viro n me n t

3.1.1

The hi-lift must be designed to function outdoors. Specifically, the nature of operations demand rugged, impact-resistant hardware whose functions and controls must be foolproof and failsafe, consistent with the anticipated level of unskilled labour using the equipment.

3.1.2

As the airport is located by the sea, stringent rust control measures must be observed in the designof the hi-lift. All hydraulic lines shall be of stainless steel, and all guides and rails

CT1503G013

TENDER FOR THE SUPPLY, DELIVERY TESTING AND COMMISSIONING OF A TURNKEY BASIS OF EQUIPMENT FOR FIVE (5) UNITS OF STANDARD HI-LIFTS (4000KG CAPACITY) WITH AN OPTION FOR ANOTHER FIFTEEN (15)UNITS OF STANDARD HI-LIFTS

SPECIFICATIONS FOR HI-LIFT WITH AIRCONDITIONED CABIN (4000 KG CAPACITY)

COMPLIANCE CHECK-LIST

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Temperature : 20oC to 48oCRelative Humidity : 0% - 100% Exposed to salt water and to heavy

tropical rainstorms, moisture and dust

3.1.3Supplier must certify that the equipment proposed will operate reliably under the requirements

stated above.3.2 S y s t e m S a f e ty 3.2.1 The following are to be observed:

3.2.1

all control methods, circuitry, mechanical equipment and operating procedures must be designed

to provide maximum safety for operating personnel. Designs must minimise potential damage to equipment or the contents of the cargo handled. Failsafe techniques must be employed to prevent the occurrence of unsafe conditions, which could result from an equipment failure, or improper

3.2.2service brake must be of the dual system type and able to have smooth brake at slow speed to

prevent damage of glassware in the catering trolley;3.2.3

for better efficiency of the parking brake, the design must be such that the activation is thru therear axle brake;

3.2.4

safety fence between the van body and the driver's cab beneath the loading platform must be provided for the purpose of preventing equipment from hitting the driver's cab for staff's safety;

3.2.5 Hi-lift not move when stabilisers are down;3.2.6 simultaneous operation of van body and its extension system to be prevented;

3.2.7with stabilisers up, the body to be allowed to rise up to 1 feet only for docking adjustment;

3.2.8two lightweight (5 kg or less) rubber safety chock with chain to be provided for right front tyre

(holder for the chocks to br provided) and3.2.9 indicator light for stabiliser fully down and up position at the control box

3.2.10

Install a green LED indicator lamp at the dashboard near the windscreen to light up when the transmission gear is in neutral position. The indicator lamp should be in the full view of the driver and marshaller who is a meter away to give the all clear signal for the driver to leave his position.

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COMPLY NOT COMPLY3.2.11 1) Travelling speed limit to 30 kmph;

2) Buzzer/alarm to be activated when travelling above 25 kmph; and3) Stabilizers cylinder for the rear and front should be interchangeable; and4) The stabilizer cylinder rod’s diameter should be at least 9cmor 3and a half inches.

3.3 P e r s onn e l S a f e ty

3.3.1

The hi-lift must be convenient and safe to use and control functions to be performed must be simple to minimise possible errors. Convenient means for emergency system shutdown must be provided at both ground and cabin levels. Mushroom head type switch to be used.

3.3.2Easy assess for drivers who are no taller then 5ft 2 inches and for them to get down from the

drivers position by having either of the following optioni Lower drivers cab orii Extra rung of foot step low enough for staff to step down to the floor

3.3.3

The hi-lift must provide adequate means for ensuring the safety of maintenance personnel.Devices such as disconnect switches, circuit breakers, overload control relays and lockouts, both electrical and mechanical, must be provided to prevent the accidental activation of those positions of the system under operation maintenance. These devices must be located in areas where access4 CHARACTERISTICS

4.1 C h a ss i s a n d C on s tru c ti on 4.1.1 The hi-lift must have the following features:

ait is to be powered by a reputable chassis and engine with local after sale service and sparesupport;

b

the chassis be equipped with a reputable diesel engine fitted with operation mode throttle for efficiency and fuel economy, cold starting device, low oil pressure shut off device, overheating cut off devices, starter interlock and any other feature which the manufacturer may find necessary;

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c

automatic transmission fitted with neutral gear power take off interlock; and indicator lamp; to

ensure commonality with existing fleet, the operation of the gears should be in this order when thed the steering system to be of a fully powered system of proven reliability;

ethe chassis to be incorporated with an automatic lubrication system automatically grease all

lubrication points at regular intervals;f the driver's position to have control of all lighting systems;

gthe rear view mirror to be of the convex type to provide a sufficiently wide view for reversing;

hbe able to transverse fully loaded at a cruising speed of 40 km/h and climb a gradient of 1:20 with

even motion after coming to a halt at a gradient;

i

in case of breakdown, there must be facilities for towing by vehicle with a draw bar pull of 1,500 kg and tow eyes are to be provided at the front and rear complete with tow bar on the hi-lift;

j

have a tail overhang of 2.75m to enable docking at the SATS In-flight Catering Centre loading bay at a height of 1.7m. Its overall height when fully lowered must not exceed 4.0 metres;

k

have the front and rear openings to be fitted with insulation lightweight sliding doors with windows. Sliding doors preferably automated with safety sensors and manual override.

l

all sliding and side doors and coverings to be of durable insulated material and to be of types that provide ease in handling, sliding door handle to be rounded and of stainless steel type and both front and rear sliding to be able to be locked from both inside and outside;

mdriver’s cabin to install with 2 passenger seats and to be airconditioned.

nadditional mirrors to be mounted on the platform for staff to view the rear of the hi-lift before it islowered.o rims and tyres for the Hi-lift shall be tubeless type with radial tyres;

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pthe 4 ton van body capacity together with the gross unladen weight must not exceed the chassismanufacturer specified gross vehicle weight; and

qsafety stand/bracket be provided to lock the scissor frame with the van body in the raise position

when vehicle is being serviced.

r

Side ladder to be mounted to chassis with safety interlock. The step to be wider with deeper and anti-skid surface. Ladder extends and retracts buttons to be on inside of the side entry door.

4.2 B rid g e L oad in g Plat f o r m 4.2.1 The bridge loading platform must have the following features:

a

it must be designed to allow transfer of loads to the aircraft at a height measured from the level

ground of not more than 2.65m at the lowest and a maximum raised height of not less than 5.90m to match all aircraft types at the loading platform;

bit must be flat, have a forward overhang of 300mm over the driver's cab and have a load capacity

of minimum 1,000 kg;c it must be able to reach B737 to B747 Door 5 height for handling operations;

d

an additional powered extendable full width platform with extension up to 1 metre out and with aload capacity of minimum 400 kg must be provided and it must be flushed with the main platform when fully retracted;

e

the extendable platform must be controlled by a dual failsafe control in the van body and must beequipped with non-marking bright coloured rubber bumper in the front, different in colour to the rubber bumper on the fixed platform (preferably black in colour with yellow marking at both end)

f

it must come with a cushion valve operated awning to cover over the aircraft door, preference will

be given for a fully powered system that provides all round covering and prevent rain from wetting the doorway;

gretractable fully covered side panels to be of mild steel and anti corrosion treated (hot dipped

galvanised);h

materials used for construction of the platform must be non-corrosive i.e. hot dipped galvanised;

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i

a hydraulic-actuated side ladder must be fixed at right side of the vehicle for climbing up into the

van body; the ladder rung must be 10” vertically apart, the step to be at least 2”wide, must be

j

the canopy should be installed with heavy-duty rollers and must be able to prevent, as best as possible, rain from getting into the aircraft cabin without affecting the safety of the aircraft; and

k

a fall arrestor to be provided with anchor point at the front right of the platform and a box for storage of the belt and harness be provided in the van body beside the operation panel.

4.3 V a n Bo d y 4.3.1 The requirements for the van body are as follows:

ait must be manufactured from reinforced insulated panel with a cover of fibreglass and recess forlighting (LED lighting) and air-condition ducting.

b

the floor structure must be insulated and be of sturdy construction to withstand a load density of

7 kg/sq. cm. Special consideration for the floorboard must be given and sample of material to be used must be submitted at time of tender;c it must be provided with insulated sliding doors;

da miniature gutter or curve should be provided at both sides with drain tube to ensure fluid spilled

does not discharge onto the truck chassis;

e

the body must have interior dimensions of length up to 7.05m x width 2.37m and height 2.10m. Reinforce mounting of two rows of lock rails on each side of the van body with two loads lock bars and brackets must be provided. Lock centre at 730mm and 480mm. Four lengths of 7m safety belts, which can be locked onto lock rails, must also be provided; the buckle must be of stainless steel material; hooks to be provided for hanging the safety belts.

f

adequate recessed or wire mesh protected lighting must be provided on both sides 1.9m above thevan body floor level. A floodlight must be provided on each side of the rear top corner of the van body;

grear underrun bumpers and sideguards for the truck must be provided in accordance with the

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h

a ringing buzzer and a warning light are to be incorporated into the system and they should respectively sound and light up when the body is being raised or lowered or reverse;

ithe floor must be durable non-skid without rivets and it must be water proof and be able to

prevent condensation on the surface; andj

there must be no holes on the roof for purpose of mounting the apron light and the mounting

bracket must be welded onto metal frame.k

The side door must have safety interlock and have glass view window below for operator to checkthe hydraulic-actuated ladder4.4 S t a b ili t y

4.4.1 The following are necessary for stability of operations:

athe hi-lift must be certified to be safe for operation and driving in wind velocity of up to 75 km/hand 160 km/h gust conditions;

bthe van body must be stable at the maximum raised height during operation and load transfer;

c

the hi-lift must be structurally designed to operate efficiently with no noticeable vibration and

noise under uneven load distribution where the centre of gravity of 1.25 times design load is shifted to 1/3 of the body;

d

certified calculations of Professional Engineer on stability of hilift under varying conditions are to be made available e.g. uneven distribution during carriage and during lifting;

e all stabilisers must be interchangeable (i.e. front left, front right, rear left and rear right)4.5 Oper at ion

4.5.1 The following features are needed for efficient operations:

a

failsafe dual-control actuated all-weather proof switches to operate the body and these must be aviation-approved switches i.e. Honeywell micro-switch, limit switch;

b

the control for stabiliser jacks and for the van body is to be mounted outside the driver's cab in a position where the operator can easily operate the system while standing on the ground; and

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c

a dual-controlled panel for the operation of the hi-lift body, extension platform, dual engine start

and emergency stop button must be mounted inside the van body on the front of the right side wall. Guardrails must be provided to protect panels from being hit by high trolleys from front and4.6 Co nt r o l Sy s t e m s

4.6.1 Control systems must have the following features:

a

all controls must be grouped in console to minimise operating points throughout the system.

Groupings must generally be in accordance with the group, subgroup and component specifications. However, additional controls, as required by the vendor, may be adapted to theb console must:

i be designed in accordance with sound human engineering principles;

iiconform to the environmental requirements specified in para 2.1 and must employ weatherproof

boxes, switches and lights;iii

contain the specified control elements such as selector switches and indicator lights, which will

augment operations; andiv

have functions identified in English using elementary concise terms and supplemented by graphic

symbols.c all identification plates must be mechanically affixed to the console face;d controls must be arranged to logically reflect the equipment movements required; and

e

mushroom head emergency stop push buttons, disrupting electrical power, must be employedwhere an emergency may require immediate shutdown. Drawings indicating locations of such buttons must be submitted to SATSCAT for approval

4.7 In t erl o ck s a n d Limi t s

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4.7.1

Fail-safe interlocks and limits such as check valves, must be provided in the system to ensure safe operation as specified in the groups, subgroups and component specifications. However, the Supplier will be further responsible for the integration of all additional interlocks and limits that may be necessitated by the characteristics of the elements selected for combination into a total system. Interlocks and limits must be included for the protection of personnel, equipment and cargo in the performance of the operational functions specified for the sub-groups and elements comprising the group. A low skill level of operator competence and intelligence, and conditions of personnel inattention must be assumed in the design of such interlocks and limits.

4.8 Emerg en c y O p er at ion

4.8.1

An alternative system, preferably powered by the truck battery, for the basic operation of raising the stabiliser and lowering of van body must be fitted. A manual pump for the hydraulic system must also be made available for emergency operations. A diagram to show the location and procedure shall be displayed on a weather proof panel at the emergency operation station.

4.9 H yd r a u lic Sy s t em 4.9.1 The hydraulic system:

a) must not exceed 2000 p.s.i. in operating pressure; andb) its components such as pump, motor, cylinder and valve banks must be of reputable make andhave sales and service representatives in Singapore. Information on these must be submitted together with other tender submissions.4.10 Re p air Ki t s ( Seals) Repair kits (seals) must be available for all hydraulic components and part numbers of themanufacturer provided

4.11 El e c t rical Sy s t em

4.11.1

It is to be of double insulated loom wiring with colour codes and number tags for easy

identification at the electrical enclosure circuit box. It must be capable of recharging up to 720 watts at least.4.12 Air - c o nd i t io n i n g Sy s t em

4.12. The following are required of the air-conditioning system:

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ait must be chassis mounted and be operated by the vehicle’s engine. Be protected from side

impact and vehicle exhaust.b

it must be able to cool the interior of the van body from about 34C to 16C within 25 minutes;

cthe cooling unit must be mounted with a protecting fence and the distance from the floorboard tothe cooling unit must be at least 1.7m;

d

the control panel for the air-conditioning system is to be located inside the driver's cabin and it

must be covered. The controller must be so designed that only maintenance crew would be allowed to do any adjustment; and

e

it is preferable that minimum ducting be installed inside the cabin. The ducting must be protectedby metal cover and secured with metal bracket and not on to fibreglass panel. Preference is for concealed types.4.13 Lig ht i n gs

4.13.1 airport roof light (static flashing amber beacon light)4.13.2 headlights (front and rear), sidelights (front and rear)4.13.3 flashing indicator (front and rear)4.13.4 rear reflector4.13.5 reversing light with horn4.13.6 horn4.13.7 Side and body light to use LED marker light.4.14 Lo a d Tes t i n g

Proof of passing and registration of load tests must be presented. A certified copy, from arecognised third party professional engineer, of the calculations of uneven load distribution for the4.15 A dd i t io n al Re qu ire m e nt s

4.15.1 The following are additional requirements:a fuel tank cap to be of lockable type;b ignition start switch to be key-controlled;

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c

hourmeter, oil pressure gauge, temperature gauge, voltmeter, fuel gauge, low water and low pressure cut-off device, auto drain valve for air tank and other applicable instruments to be fitted;

dvehicles to be painted in SATSCAT’s colour scheme and livery with two coats of marine primer andanti-corrosive coating agent;

e

driver's cabin, chassis and undercarriage, van body flooring and underside of the main and

extendable platform must be preserved against corrosion with quality anti-rust agent of a reputable brand such as Tuff Kote Dino; and

fsafety messages e.g. “Safe Working Load – 4000 Kg” and “Distribute Loads Evenly” should be

painted inside the van body.g rims and tyres size for the Hi-lift shall be 27.5/70R22.5 tubeless type with radial tyres.5 After Sales Responsibility

5.1

The supplier must provide his factory engineer to commission the equipment on delivery. Theengineer is required to provide practical training to SATSCAT’s staff for 2 weeks on the following:

5.1.1 Operations;5.1.2 Preventive maintenance; and5.1.3 Repair/Overhaul of components5.2 The Supplier is required to furnish the following manuals, preferably in CD-ROMs:

5.2.1 Twenty-four sets of operator’s handbook;5.2.2 Eight sets of operating manual;5.2.3 Eight sets of workshop repair manual;5.2.4 Eight sets of parts manual;5.2.5 Three sets of accurate "as built" drawings; and

5.2.6Three sets of detailed components manual comprising of engine, main pump, hydraulic cylinder &motor, starter motor, alternator etc.5.3 A dd i t io n al It e ms t o b e s upp lied

5.3.1 One set of repair kit per unit for all main hydraulic assemblies and components;5.3.2 One unit 6kg dry powder fire extinguisher per unit;5.3.3 Four sets of keys per unit;

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COMPLY NOT COMPLY5.3.4 One set of spare tyres and rims per unit; and5.3.5 Rear view camera to be mounted for driver to see

a) rear of hi-lift when reversing (note: camera to be mounted at top of van body)5.4 CCTV camera

5.4.1

Up to 4 video cameras with recording function ( to be locally installed) to be mounted in driver’s

cabin hilift front platform inside vanbody plus a 4th location to be advised; tampered-proof and concealed wirings to be provided6 ACCEPTANCE TESTS

6.1 Ge n er a l

6.1.1

The supplier must perform all necessary inspections and tests to demonstrate that the hi-lift meetsall requirements of this specification. Supplier's records of inspections and tests must be kept complete and available to SATSCAT at all times. Records or reports of inspections and tests must be signed and approved by the supplier. SATSCAT reserves the right to witness any test to determine if the hi-lift meets all specified requirements. An acceptance test shall be conducted in accordance with a test plan and procedure provided by the supplier and approved by SATSCAT. The supplier must provide adequate personnel to assist SATSCAT in inspecting and testing the hi-lift

6.1.2

Reasonable notice must be given to SATSCAT prior to the performance of final acceptance test.SATSCAT or its appointed representatives will witness all acceptance tests and indicate acceptance by signing and dating the test data sheet.

6.1.3

The tests and inspections identified in this Specification represent the minimum requirement for hi lift acceptance and do not necessarily represent the complete final test requirements as variations in equipment types and designs, which will evolve under a competitive bid, may require additional specific tests. The supplier must develop a test plan and procedure that will insure performance of the specified tests as well as the additional tests, which may become necessary.

6.1.4

Each system and its elements will be tested using airborne unitised load devices of various sizes loaded to their maximum capacities. Specifically, the hi-lift will be tested to 1.5 time the designed load. On site testing, a pressure water hose of 80 p.s.i. will be used to simulate raining

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6.1.5

The test program must verify system compliance with the requirements specified herein. In

general, load capabilities, speed, stop and guide function, sensors, controls, ruggedness, deflection, smoothness of acceleration and deceleration, noise, continuous cycling, unitised load flow and

6.1.6

During the performance of the specified tests there must be no damage to the cargo, containers or equipment. All mechanisms and stops must operate as described. None of the components must overheat and shut down due to overload, malfunction or misapplication.

6.2 Test Re p or t s

6.2.1

Fifteen days after completion of the tests, the contractor must submit a report summarising thedetailed results of the test. The contractor must make available to SATSCAT, upon request, the results of all tests conducted.6.3 Fi n al Ac c e pt a n c e

6.3.1Final acceptance of the hi-lift will be made only after all the following conditions have been

fulfilled:a the hi-lift has been successfully tested as specified;b the hi-lift is found to comply with all specifications;

cthere has been no experience of any failure, irregular operation abnormal wear after the hi-lift hasbeen operated by SATSCAT a month;d the requirements of Clause 5.2 have been met;

e spare parts, as approved by SATSCAT, have been delivered; and

f

the supplier has provided the names, addresses, and 24-hour phone numbers of at least 2 staff of the local representative (approved by SATSCAT) of the supplier with authority and experience to make replacements and repairs immediately for the full life of all warranties.

g Pre-delivery inspection to be arranged by vendor6.4 Co nd i t io n al Ac c e pt a n c e

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6.4.1

If the hi-lift is found to be unacceptable at the time of final inspection, SATSCAT will inform the supplier of the particular defects that must be remedied before final acceptance will be made. At this time, SATSCAT may at its sole discretion elect to advise the supplier in writing that a conditional acceptance has been made. The conditional acceptance will to the extent set forth herein, relieve the supplier of responsibility for the security and insurance on the hi-lift and will also be used to initiate the time of warranty of the hi-lift. In no case, however, will a conditional acceptance relieve the supplier of the responsibility for performing all the work set forth in the contract documents, including the correction of deficiencies noted at the time that the conditional acceptance is made; and SATSCAT will be entitled to retain from the supplier's payments an amount commensurate with the work remaining to be accomplished. Further, SATSCAT may elect to put the hi-lift into operation subsequent to th

6.5 6.5 P a r t s Availa b ili t y

6.5.1

The supplier must guarantee the availability of all spares and replacement parts and sub-assemblies required by any equipment items supplied for a minimum fifteen-year operational period. Such parts must be either available from component manufacturers when an unmodified commercial component is required or from sub-contractors when "special" components are required.

6.5.2

Should the supplier, sub-contractor, or such suppliers as the supplier may specify, fail to make such parts available during the fifteen-year operation period, or should the supplier's pricing become unreasonably high on a competitive basis, SATSCAT has the right to use the supplier's drawings, at its sole discretion, for fabricating such parts, or having such parts fabricated.

6.5.3

The supplier must provide a recommended spare parts list and must hold stock of value no lessthan 10% of the contract value (items and numbers as approved by SATSCAT) in Singapore for the duration of the warranty period.7 Option Purchase

7.1If the option is to be exercised, please provide a quotation for the unit price for the following items

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COMPLY NOT COMPLY7.1.1 engine module;7.1.2 main hoist cylinder; and7.1.3 sliding door

8 Warranty8.1 The main chassis shall have a warranty period of not less than twelve years,

8.2The sub chassis such as scissor beam and pin support the van body shall have a warranty period ofnot less than ten years.

8.3All other parts that failed prematurely will be cover by the supplier for a period of 24 months or

more.9 Submission Checklist9.1 Unit price of the firmed and optional unit of hilift9.2 Unit price of the optional purchase spare parts and recommended part lists9.3 IATA Standard of Total Cost of Ownership (TCO) for the hilift9.4 Specification Compliance Form9.5 Delivery Lead Time9.6 Warranty Period

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Tenderer’s business/company stamp:

Signature of Tenderer or its authorised signatory:

Full Name and Designation of Tenderer’s

authorised signatory:

Date: