A330 200 Freighter [PDF]

Zitiervorschau

A330-200F

A330-200 Freighter Brochure Issue 5

A330-200F

Reference

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document Prepared and authorized by: The Airbus program department Document reference no.:

A330-200 Freighter - Brochure issue 5, April 2013

G25M13017173

A330-200F

Contents

page

page Reference Contents Introduction Chapter 1 - General Airbus aircraft commonality General aircraft features General overview Chapter 2 - Courier area ATA 25.20 - Courier area ATA 25.20 - Aft customizable area ATA 25.20 - Fwd customizable area ATA 25.23 - Courier area lining ATA 25.30 / 25.35 - Galleys / Catering equipment ATA 25.40 / 38.31 - Lavatory ATA 25.60 - Emergency equipment ATA 33.20 - Courier area lighting ATA 53.00 - Barrier wall

Chapter 3 - MD & LD cargo compartment ATA 25.50 - Cargo compartments lining ATA 25.50 - Cargo drainage system 4 ATA 25.56 / 25.51 - Cargo loading system ATA 33.36 - MD cargo compartment lighting ATA 52.30 - Cargo doors 5 Chapter 4 - Associated information 6 ATA 12.00 - Ground handling & servicing 7 ATA 21.00 - Air conditioning ATA 23.73 - CIDS ATA 26.00 - Fire protection 8 ATA 35.00 - Oxygen 11 14 Chapter 5 - Appendix 18 General overview 23 Live animals transportation 29 Perishables goods transportation 33 Dangerous goods transportation 36 42 Glossary of abbreviations Legal notice

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A330-200F

Introduction

Introduction The A330-200F brochure provides an overall general description on Airbus design solutions for A330-200 Freighter courier area, main deck and lower deck compartments. It shall be seen as an additional general information to the Airbus Freighter Configuration Guide (FCG), providing a better understanding on the A330-200F customization. Any option outside the A330-200F brochure and FCG shall be covered via specific customer request to ensure technical feasibility and lead time compliance.

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A330-200F

Chapter 1 – General

Airbus aircraft commonality The A330-200F is a medium to long range freighter able to load 70 t up to 3200 NM (5926 km) and 65 t up to 4000 NM (7408 km). The A330-200F is derived from the passenger aircraft A330-200 and gives a high level of commonality. The A330-200F combines the technical expertise gained in several previous wide body freighter projects to an optimized cargo aircraft. The cross section is compatible with all other Airbus wide body freighter.

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A330-200F

Chapter 1 – General

General aircraft features The A330-200F is based on a successful passenger variant. The following picture shows the principal changes when compared to the A330-200 passenger variant.

A330-200 Freighter - Brochure issue 5, April 2013

Span

197 ft 10.0 in

60.30 m

Length

192 ft 11.6 in

58.81 m

Height

55 ft 4.5 in

16.88 m

Fuselage diameter

18 ft 6.0 in

5.64 m

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A330-200F

Chapter 1 – General

General overview The A330-200F is designed to offer the flexibility needed to operate in the worldwide cargo business, especially with the payload flexibility. The courier area offers transportation of 4 (up to 12) persons for the basic configuration and is equipped with a lavatory and galleystowage. The courier area is delivered in Airbus cool basic colors according to ref. ICS 07/04. The main deck cargo compartment provides a maximum cross section that allow transportation of Unit Load Devices (ULD) up to 96" width in side by side configuration. Due to the large doors in lower deck forward and aft compartment ULDs can be carried up to a size of 96"x125". Cargo loading systems, ventilation, temperature control, CIDS, smoke detection & fire protection, courier area... have been developed to fulfill the freighter requirements and to satisfy the different customer needs.

MTOW

Basic payload mode 227 t

Optional range mode 233 t

MLW

187 t

182 t

MZFW

178 t

173 t

OWE

108 t

Engine

PW 4170 RR Trent772B

Max. structural gross payload

70 t

65 t

Range capability

3200 nm

4000 nm

Common parts with the passenger A330-200 are covered in other brochures which are dedicated to specific topics (placards, lower deck…).

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A330-200F

Chapter 2 – Courier area

ATA 25.20 - Courier area • ATA 25.21 - Seats: General overview • ATA 25.21 - Seats: Standard layout - Double economy class seats ATA 25.20 - Aft customizable area • ATA 25.21 - Seats: Options available - Triple economy class seats • ATA 25.21 - Seats: Options available - Double business class seats ATA 25.20 - Fwd customizable area • ATA 25.22 - 2 HCCAS on lavatory wall • ATA 25.30 - Galley / Stowage with 4 HCCAS • ATA 25.74 - Double bunk FCRC ATA 25.23 - Courier area lining

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A330-200F

Chapter 2 – Courier area

ATA 25.21 – Seats: General overview Description The standard courier area layout provides 2 double economy class seats installed forward facing in front of the barrier wall. The following picture shows this standard layout:

• Full compliance to JAR/FAR 25.562 – Tested according to AS8049 • No electrical installation – Mechanical actuation • The double and triple E/C seats are each equipped with the following comfort features: ◦ a 6" (152.4 mm) seat back recline, ◦ an adjustable headrest, ◦ a deployable in-armrest table. • The double B/C seats are each equipped with the following comfort features: ◦ a 13" (330.2 mm) seat back recline, ◦ an adjustable headrest, ◦ a deployable in-armrest table, ◦ a deployable legrest. Options available The 2 double economy class seats can be replaced by 2 triple economy class seats or 2 double business class seats.

Additional seating capacity can be provided in the area aft of the cockpit wall on High Comfort Cabin Attendant Seats (HCCAS). All Alternate seat layouts can be selected. these options are selectable in the Freighter Configuration Guide The basic function of the standard and optional seats is to provide (FCG). seating for the courier area occupants during all flight phases.

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A330-200F

Chapter 2 – Courier area

ATA 25.21 – Seats: Standard layout – Double economy class seats Two double economy class seats are installed in front of the barrier wall. A bustle is installed above each double seat. The bustle includes reading lights, electrical outlet and courier-cockpit communication.

Vendor

Seat characteristics BE Aerospace

Part number

Spectrum PN 1010859-10XJB01

Seat width

41.25"

Personal space between arms

17.5"

Seat depth

26.4"

Recline

6" (13°)

Weight

32.24 kg

In-armrest table Adjustable headrest Lumbar Note: Pictures show option 1: seats layout with center galley

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A330-200F

Chapter 2 – Courier area

ATA 25.20 – Aft customizable area

Customizable area AFT

A330-200 Freighter - Brochure issue 5, April 2013

Center galley

4 business seats with 2 overhead stowage compartments

6 economy seats with 3 overhead stowage compartments

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A330-200F

Chapter 2 – Courier area

ATA 25.21 – Seats: Options available – Triple economy class seats The installation of 2 triple economy class seats in front of the barrier wall includes a third bustle.

Vendor

Seat characteristics BE Aerospace

Part number

Spectrum PN 1010860-10XJB01

Seat width

61"

Personal space between arms

17.5"

Seat depth

26.4"

Recline

6" (13°)

Weight

46.50 kg

In-armrest table Adjustable headrest Lumbar

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A330-200F

Chapter 2 – Courier area

ATA 25.21 – Seats: Options available – Double business class seats Basic provisions in front of the barrier wall allow the installation of 2 double B/C seats.

Vendor

Seat characteristics BE Aerospace

Part number

Millenium PN 8874300X9021S01

Seat width

48"

Personal space between arms

19.5"

Seat depth

31.3"

Recline

13" (30°)

Weight

68.2 kg

Swiveling deployable in-armrest table Adjustable headrest Deployable leg-rest Lumbar

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Chapter 2 – Courier area

ATA 25.20 – Fwd customizable area

Customizable area FWD

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2 wall mounted HCCAS

Galley / stowage with 4 HCCAS

Flight crew rest compartment

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A330-200F

Chapter 2 – Courier area

ATA 25.22 – 2 HCCAS on lavatory wall • 2 HCCAS can be installed on lavatory wall • re-use of 16g seat from PAX

Vendor

Seat characteristics Goodrich

Part number

2072-119FF 2072-122FF

Seat width

20"

Personal space between arms

17"

Seat depth

27"

Weight

25.4 kg

Recline

27°

Plug-in table

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A330-200F

Chapter 2 – Courier area

ATA 25.30 – Galley / Stowage with 4 HCCAS This monuments provides: • stowage capacity • 4 wall mounted HCCAS (with plug-in table) • galley area described in galley part (ATA 25.30)

Vendor

Seat characteristics Goodrich

Part number

2072-119XX

Seat width

20"

Personal space between arms

17"

Seat depth

27"

Weight

25.4 kg

Recline

27°

Plug-in table

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A330-200F

Chapter 2 – Courier area

ATA 25.74 – Double bunk FCRC The dual bunk FCRC, in place of the galley G1, provides: • two sleeping surfaces, arranged transversely one above the other and screened by curtains • a stowage compartment (approximately 0.325 m³) with door Note: The upper bunk can be folded down to provide seating for two occupants that is certified for use during take-off and landing.

Vendor

FCRC characteristics BE Aerospace

Part number

M8500-1-2-0001

Upper bunk width

23"

Upper bunk length

69" to 76"

Upper height ceiling

32"

Lower bunk width

23"

Lower bunk length

81" to 85"

Lower height ceiling

25"

Weight

527.25 kg

Storable headrests Literature pockets Privacy curtains Handset Folding tables

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Chapter 2 – Courier area

ATA 25.23 – Courier area lining • • • •

General overview Sidewall lining Ceiling Barrier wall lining

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Chapter 2 – Courier area

ATA 25.23 – Courier area lining: General overview Description Sidewall linings are installed between frames C18 and C20 LH and RH sides. On the lower RH and LH sidewall is a heated air outlet (HAO) which ensure circulation at foot level for the courier area. On the LH sidewall, an access panel for the manual hydraulic override valve of the MDCD is located on the lower portion of the window panel. The location of the access panel is purposely located under the window on the sidewall for better visibility of the open or closed position of the MDCD. On the upper portion of the LH sidewall panel there is an air temperature sensor for courier area. This sensor regulates the temperature within the courier area. The ceiling panels are installed between frame C13A and C19. Incorporated within the ceiling panels are systems such as oxygen, lighting, attendant information panel and air conditioning. The access to the systems in the ceiling panels are easily accessible by removing the decor panels. The barrier wall lining is installed on the barrier wall structure. The lining serves as an insulation and sound barrier from the MDCC. Also included on the bottom side of the barrier wall lining is an air return passage through the floor structure to ensure adequate air circulation. Options available The ceiling panel offers an oxygen container located on forward RH ceiling panel when 4 HCCAS seats are on G1 galley. Also, different decor panels are available when FCRC, G2 galley and bustles are being used in different configurations. The barrier wall lining offers different panels to accommodate the different bustle configurations. A330-200 Freighter - Brochure issue 5, April 2013

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A330-200F

Chapter 2 – Courier area

ATA 25.23 – Courier area lining: Sidewall lining The following pictures present typical sidewall lining between frames C18 and C20 and are valid for all configuration layouts.

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Chapter 2 – Courier area

ATA 25.23 – Courier area lining: Ceiling The following pictures (bottom up view) present typical ceiling. Equipment from ATA 21, 33 and 35 are installed in this ceiling.

1 Integrated ballast unit 2 Oxygen container (type II) 3 DOLLI (Dome LED Light) 4 NS / FSB 5 Temperature sensor under grill 6 Air outlet 7 AIP (Attendant Info Panel) 8 EXIT identifiers 9 Loudspeakers

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Chapter 2 – Courier area

ATA 25.23 – Courier area lining: Barrier wall lining The following pictures (against flight direction) present typical barrier wall linings (with 2 bustles).

Barrier wall door, doorframe lining and barrier wall lining A330-200 Freighter - Brochure issue 5, April 2013

ATA 21 Air extraction area 22

A330-200F

Chapter 2 – Courier area

ATA 25.30 / 25.35 – Galleys / Catering equipment • • • • •

General overview Galley G1 (basic) Galley G2 (optional) Galley stowage configurations Catering equipment

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Chapter 2 – Courier area

ATA 25.30 – Galleys: General overview Description Galleys provide space for storing food and drinks. Further equipment Galleys are installed with a potable / waste water supply and electrical supply and equipped with the following equipment: can be installed for preparing cold / hot meals and drinks. Two galley positions are proposed as shown in the figure here below:

• • • • • • •

a sink area with water faucet a sliding table a circuit breaker panel a waste compartment a working light and PC power outlet stowage compartments standard units

Options available The galley G2 can be selected as an alternative if the galley G1 is replaced by a stowage with 4 C/A seats or a flight crew rest compartment (option presented in the FCG). Depending on the needs in terms of flight range, courier area accommodation, number of occupants and stowage capacity, it is proposed to install different and predefined configurations of inserts and catering equipment for both galleys G1 and G2. Galley G1, located between the cockpit and door 1 RH, is installed on the basic aircraft. Provisions for the installation galley G2 are basically provided in front of the barrier wall.

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A330-200F

Chapter 2 – Courier area

ATA 25.30 – Galleys: Galley G1 (basic) FWD galley / stowage monument (SFE) Monument equipped with: • • • • • • •

wardrobe sliding table standard units waste compartment laptop power supply stowage compartments sink area with water tap

Standard units, capable of 4 Atlas full size trays or 8 Atlas half size trays (used on basic configuration): • up to 32 Atlas HS trays • 6 full size bottles per standard unit Space provisions for selectable catering equipment (SFE): • beverage maker • convection / microwave oven • chilling capability (fridge or plugin air chiller)

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Chapter 2 – Courier area

ATA 25.30 – Galleys: Galley G2 (optional) Small center galley (SFE) Basic provisions in front of the barrier wall allow the installation of a small galley. Monument equipped with: • • • • •

sliding table standard units waste compartment stowage compartments sink area with water tap

Standard units, capable of 4 Atlas full size trays or 8 Atlas half size trays (used on basic configuration): • up to 32 Atlas HS trays • 6 full size bottles per standard unit Space provisions for selectable catering equipment (SFE): • beverage maker • convection oven • chilling capability (fridge or plug-in air chiller)

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Chapter 2 – Courier area

ATA 25.30 – Galleys: Galley stowage configurations Stowage / galley + 4 HCCAS (SFE) Space provisions for selectable catering equipment (SFE): • Beverage maker. • Convection oven.

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Chapter 2 – Courier area

ATA 25.35 – Catering equipment Beverage maker characteristics Vendor B/E AEROSPACE

Fridge characteristics Vendor B/E AEROSPACE

Part number

4511-2611-00

Part number 600-1

Capacity

1.36L

Capacity

31.1L / 20.4 kg

Brew time

3 minutes

3 Modes

refrigeration / wine / chiller freezer

Convection oven characteristics Vendor B/E AEROSPACE

Air chiller characteristics Vendor B/E AEROSPACE

Part number

4313100-01-6600

Part number

377-2

Capacity

32 Atlas standard meals

Capacity

2400 BTU / Hr

Preparation time max. 28 minutes

Microwave characteristics Vendor TIA ELECTRICO INC. Part number

400-2383-01

Capacity

11.9L (6" x 11" x 11")

Power

1000 W

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Chapter 2 – Courier area

ATA 25.40 / 38.31 – Lavatory • General overview • Standard interior equipment • Recirculation system

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Chapter 2 – Courier area

ATA 25.40 – Lavatory: General overview Description The lavatory is fitted with a recirculation toilet assembly. The toilet shroud provides a decorative cover for the toilet unit and includes the seat with cover. For ventilation system, ambient air is supplied from the courier area through an air inlet grill near the floor area. Fresh air comes through an individual air outlet which is supplied via a tapping point from the main distribution duct for the FWD TEMP zone. Extracted air from the lavatory is exhausted overboard through a separate duct system to eliminate unpleasant odours. A smoke detector and appropriate warning system in the flight compartment is installed. A fire extinguisher for the waste bin is on the top of the waste compartment. Pressurized water system is designed to comply with United States public health standards. The upper / lower attachments are made by means of tie rod / hard points. These are accessible when the lavatory is installed to enable removal without disassembly via split line. The module weight is around 140 kg.

Lavatory module A330-200 Freighter - Brochure issue 5, April 2013

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Chapter 2 – Courier area

ATA 25.40 – Lavatory: Standard interior equipment Shown features: 1 recirculation toilet assembly enclosed by a rigid decorative cover 2 oxygen box (at least 15 minutes supply duration) 3 water supply; water faucet 4 one ashtray inside, one ashtray outside 5 mirror 6 coat hook 7 hand–grip installed on the wall 8 toilet roll holder 9 paper towel dispenser 10 waste bin with airtight self closing lid 11 flush button 12 seat cover dispenser 13 bi–folding door 14 door lock 15 return to seat sign / attendant call button / razor socket / individual air outlet 16 air inlet grill Note: Loudspeakers for crew communicatons are situated in the ceiling (not visible in this picture). Kick strips are located on the outside of the monument, they are about 100 mm high and made of stainless steel. A330-200 Freighter - Brochure issue 5, April 2013

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Chapter 2 – Courier area

ATA 38.31 – Lavatory: Recirculation system The recirculation toilet system consists of functional groups for: • waste reception • waste storage • waste servicing The recirculation toilet system receives waste from the users (A/C cabin occupants and crew) in the lavatory. The waste matter is directly discharged from the bowl to the waste holding tank by gravity and with support of the introduced flush fluid. The toilet system stores the waste matter throughout the whole flight mission. On ground, the disposal of the stored waste matter can be carried out by usual airline / airport practices using servicing cars.

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Chapter 2 – Courier area

ATA 25.60 – Emergency equipment • General overview • Emergency layout

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Chapter 2 – Courier area

ATA 25.60 – Emergency equipment: General overview Description Emergency equipment is stowed in various locations throughout the Evacuation signalling equipment, providing acoustic and visual warnings, is installed and is operated by the flight crew if evacuation of cockpit (identical to the PAX) and courier area compartment. the aircraft should become necessary. The standard cockpit and courier area are equipped with the following To protect the aircraft structure against the effects of fast emergency equipment: decompression, the courier area, main deck compartment and cargo • two portable fire extinguisher compartments are fitted with a system of decompression panels. (one in the courier area and one in the cockpit). Options available • two flashlights in the courier area and two in the cockpit. • two manual release tool Optional emergency equipments are presented in the FCG. (one in the courier area and one in the cockpit). • one first aid kit. • eight life vests located under each seat (BFE items, 4 in the courier area and 4 in the cockpit). • two Protective Breath Equipment (PBE) (one in the courier area and one in the cockpit). • one light-weight portable oxygen cylinder assembly (with oxygen mask and stowage pouch). • two portable Emergency Locator Transmitter (ELT). • two fireproof gloves (one pair in the courier area and one pair in the cockpit). • one crash axe in the cockpit. • two cockpit escape ropes. The main deck / crew doors are fitted with inflatable escape slide-rafts to facilitate the evacuation off all couriers and crew in the shortest time.

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Chapter 2 – Courier area

ATA 25.60 – Emergency equipment: Emergency layout The following picture shows an example of the emergency layout for the standard configuration.

A330-200 Freighter - Brochure issue 5, April 2013

POS 1

Equipment reference (courier area) portable halon fire extinguisher

QTY 1

2

oxygen cylinder / mask assembly

1

3

protective breathing equipment

1

4

first aid kit

1

6

fireproof gloves

1

7

flashlight

2

8

manual release tool

1

9a

portable ELT

2

9b

bracket ELT

2

life vests for passengers

4

POS 50

Equipment reference (cockpit) portable halon fire extinguisher

QTY 1

51

protective breathing equipment

1

52

life vest for cockpit crew

4

53

flashlight

2

54

crash axe

1

55

fireproof gloves

1

56

escape rope

2

57

manual release tool

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A330-200F

Chapter 2 – Courier area

ATA 33.20 – Courier area lighting (plus ATA 33-51 Emergency Lighting) • • • • •

General overview General illumination Reading lights Lighted signs Emergency lighting

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Chapter 2 – Courier area

ATA 33.20 – Courier area lighting: General overview Description The freighter specific courier area lighting consists of: General illumination:

Fasten seat belt signs:

The general illumination is controlled by the FAP and AAP. The The signs switch on when the control switch in the cockpit is moved to brightness of the general illumination can be dimmed in three steps the SEAT BELT position. In the event of rapid decompression the (10%, 50% and 100%). signs switch on automatically irrespective of the control switch position. Lavatory lighting: The lavatory lighting system consists of a fluorescent lamp installed in Return to seat sign: lavatory and controlled by a switch fitted on the FWD circuit breaker panel. The lamp is on at maximum intensity whenever the lavatory door is closed and locked and the selector switch is on. The lighting reduces to 50% brightness when the lavatory door is closed and unlocked. Reading lights:

This sign is installed in the lavatory and switch on when the FASTEN SEAT BELT control switch is placed to the SEAT BELT position. Emergency lighting: The emergency lights will illuminate the courier area in case of emergency. The electrical power is automatically provided by the Emergency Power Supply Unit (EPSU) in case of a power loss.

These lights are positioned in the bustles above each cabin occupants Options available seat. Each unit consists of a high-intensity light and control pushbutton No specific customization for the lighting. Adaptations can be required switch. depending of options taken. No smoking sign: The signs switch on when the control switch in the cockpit is placed to ON or automatically when in the AUTO position and the landing gear is extended. In the event of decompression the signs switch on automatically irrespective of the control switch position.

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Chapter 2 – Courier area

ATA 33.20 – Courier area lighting: General illumination The general illumination is controlled by CIDS. The lighting controls: • are located in the FAP and AAP. • are provided to control the general cabin lighting and to select 10 %, 50 % or 100 % intensity levels.

1 Integrated ballast unit 3 DOLLI (Dome LED Light) 4 NS / FSB 8 AIP (Attendant Info Panel) 9 EXIT identifiers

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Chapter 2 – Courier area

ATA 33.20 – Courier area lighting: Reading lights The individual reading lights and their switch are located in the bustles above the cabin occupants seats.

Reading light (standard layout) Reading light (customized layouts) Attendant work light

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Chapter 2 – Courier area

ATA 33.20 – Courier area lighting: Lighted signs The fasten seat belt / no smoking signs are visible from all seats. The lighted signs are controlled by CIDS. The controls are located in the cockpit.

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Chapter 2 – Courier area

ATA 33.51 – Courier area lighting: Emergency lighting All emergency lights are connected to an EPSU. The electrical power The emergency lighting is controllable from the cockpit. is automatically provided by the EPSUs internal battery pack in case of A control-switch "EMER" is provided in the FAP. power loss. The internal battery pack allows the emergency lights to operate a specified time. The exit marking and exit location signs will be activated automatically when either the landing gear is extended or in case of excessive depressurisation. In the last case the emergency lights will also be turned on automatically.

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Chapter 2 – Courier area

ATA 53.00 – Barrier wall • • • •

General overview Implementation Interfaces Access doors

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Chapter 2 – Courier area

ATA 53.00 – Barrier wall: General overview Description The safety barrier wall is designed to meet international airworthiness A space provision between the barrier wall and the 1st containers row regulations. is provided, allowing courier moving from one side to the other during flight. Compliance to CS25 561(c) has been shown by considering the forward inertia factor of 9g as a static condition for the barrier wall The module weight is around 430 kg. using the entire cargo. The fixed safety barrier wall is installed between frames C19 - C20 along the surrounding structure on the main deck cargo compartment. An additional space provision in front of the barrier wall (courier compartment) is provided due to the deformation (70 mm) of the barrier wall. Courier access to the class "E" cargo compartment during flight is possible on both sides through RHS and LHS access doors (optional). RH and LH side cargo compartment doors allow access to the cargo compartment when ULD are loaded in single row configuration. The cargo compartment access doors open into the courier area.

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Chapter 2 – Courier area

ATA 53.00 – Barrier wall: Implementation

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Chapter 2 – Courier area

ATA 53.00 – Barrier wall: Interfaces The barrier wall has interfaces with lining & insulation, seat rails, floor panels, sealing profile. The lower part of the barrier wall provides air circulation between courier area and the main deck cargo compartment (air extracted from the courier area to MD).

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Chapter 2 – Courier area

ATA 53.00 – Barrier wall: Access doors Access doors opening direction into courier area.

The door and door frame structure is aluminium. The complete courier area lining including doors and door frame is composite.

Door cut-outs have a total height of min. 1650 mm and a minimum width of 627.5 mm allows an almost upright passage. The installation of rapid decompression panels in the cargo compartment access doors allow optional installation of seats and Door surrounding is made of aluminum to avoid damage during monuments in the customizable area. frequently door passage.

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Chapter 3 – MD & LD cargo compartment

ATA 25.50 – Cargo compartments lining • • • •

General overview MDCC lining overview MDCC lining characteristics LDCC lining overview

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Chapter 3 – MD & LD cargo compartment

ATA 25.50 – Cargo compartments lining: General overview Description The MDCC lining is provided between frame C20 and C80 and up to Installation, replacement or rectification of the lining and system 90" high in the cylindrical section. Side walls and rear area is covered components is possible without the use of specialized tools / by lining components which are made of high impact resistant GFRP equipment. (Glass Fiber Reinforced Plastic) laminates and finished in light color. The MDCC lining fulfill the FAR/EASA §25.857 (e) and §25.855 (d) – The LDCC lining, based on S-Glass lay-up, protects surrounding class E compartment and fulfill low smoke and toxicity requirements. structure and systems against fire, temperature air tightness, handling The LDCC lining fulfill the requirements for: loads of loading personnel, and has to be damage resistant (withstand • "fire containment – class C", according to EASA certification handling, impact and decompression loads). specification 25.855 (c) The lining ensures pressure compensation between cabin and cargo during ascent and descent in the LDCC by using pressure • "air tightness", according to FAR/EASA 25.857 (c) • "rapid decompression", according to FAR/EASA 25.365 (e) initial compensation valves. release It ensures baggages load flow over the airframe structure during the Options available bulk cargo loading and unloading. Installation of sidewall protections in LDCC. Enlarging protection sheet by approximately 30%, this option further enhances cargo lining impact tolerance at most exposed areas to inadvertent damage.

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Chapter 3 – MD & LD cargo compartment

ATA 25.55 – Cargo compartments lining: MDCC lining overview Below sketches represent typical overview of the MDCC lining. The same philosophy is applicable to the lining all along the MDCC. In the cargo door area, reinforcements are provided to avoid damage during ULD loading operations.

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ATA 25.55 – Cargo compartments lining: MDCC lining characteristics The basic function of MDCC lining are: • To cover the cargo hold with respect to the surrounding area. • To ensure the pressure compensation between surrounding areas in the event of a rapid decompression by means of decompression devices (dado panels) on both sides at the main deck from frame C20 – C80 above floor level. • To withstand handling loads by operative personnel during on-/offloading. • To protect against fire and temperature. • To ensure the component installation or serve as an interface for specific systems (rapid decompression device, marking & placards, air conditioning / temperature control, electrical power, smoke detection / portable fire extinguishing, lighting, MDCC CLS (payload systems), main deck cargo door, fuselage structure).

Dado panels – rapid decompression devices i.e. CFRP or metallic grids are integrated (see figure previous page). Covers are installed to close the gaps between primary structure and lining installation. The vital systems in the ceiling located between the two close-out covers are protected against fire.

All lining components at the opposite of the MD cargo door are reinforced in a way to accept impacts from oversized ULD and operational handling of loading personnel. The lining panel parts are attached by quick release fastener to the secondary structure.

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ATA 25.50 – Cargo compartments lining: LDCC lining overview Same LDCC as the passenger A/C, for detailed information please refer to the A330 / A340 Cargo Compartment Brochure.

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ATA 25.50 – Cargo drainage system • • • •

General overview Schematic drawing Main deck drainage system Lower deck drainage system

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ATA 25.50 – Cargo drainage system: General overview Description The cargo compartment drainage systems of the A330-200F drain all fluids, which may occur inside the MDCC and the LDCCs due to rain or snow via opened cargo doors or due to water or snow on transported freight, out of the A/C via the drain masts. Fluids are collected in drain pans and funnels in the MDCC and the LDCCs. The design and location of the drain pans and funnels correspond to other system and structural installations. All pans and funnels are connected with a heated pipe system, which is installed within the floor grids, the triangle areas and the bilge. The pipe system is connected with the FWD and with the AFT drain masts. Due to possibly low temperatures in these areas the complete pipe system, including funnels, is heated and insulated. The performance of the cargo drainage system facilitates to drain about 1.500 l water (or melted snow) from the main deck cargo compartment and about each 500 l from the FWD and aft lower deck cargo compartment during a flight cycle.

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ATA 25.50 – Cargo drainage system: Schematic drawing The main deck drainage system consists of drain channels and The lower deck drainage system drains all fluids, which are funnels, which are located in areas, where an accumulation of collected in the PDU drain panels (power drive units) and at the roller undesired fluids could occur. tracks end.

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ATA 25.55 – Cargo drainage system: Main deck drainage system The basic main deck drainage system consists of four rows of lateral All drain funnels on the MD are connected to the heated piping up to drain channels equipped with drain funnels. Additional drain funnels the drain masts. are installed in the cargo door entrance area and between C72/C73 RH and LH. A protection angle is installed on the bulk head lining lower part near C80 in transversal orientation.

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ATA 25.50 – Cargo drainage system: Lower deck drainage system This drainage system consists of: • • • • •

PDU drain pans with funnels in the roller tracks below each PDU (1) drain pans with funnels below the splitters (2) ball mat drain pans with funnels below the ball mats in the door areas (3) funnels at each end of each roller track (4) a heated pipe system (5) including air-stop valves (6)

All funnels are connected to the drain mast (7) via the heated pipe system.

PDU drain pan (1)

Splitter drain pan (2) & pipe-connection

Principle of FWD lower deck drainage system A330-200 Freighter - Brochure issue 5, April 2013

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ATA 25.56 / 25.51 – Cargo loading system • Unit load devices (ULD) • Main deck cargo loading system, general overview • • • •

Main and lower deck cross sections General main deck ULD configuration and running loads Integrator configuration Military pallet configuration

• Lower deck, general description • General lower deck layout • Volume, tare and densities • MD flexible floor structure concept • MD CLS typical components • Cargo compartment floor panels and anti-skid surface • MDCC placards (ATA 11.39) • MDCC floor marking overview

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ATA 25.56 / 25.51 – Cargo loading system: Unit load devices (ULD) Unit Load Devices (ULD) characteristics taken into account in this brochure in terms of ULD internal volume and ULD tare weight. Note: According to products market, those values may vary from one ULD manufacturer to the other. Type LD3

Volume 4.3 m³ / 153 ft³

Tare weight 200 lb / 91 kg

LD3 lexan

4.3 m³ / 153 ft³

215 lb / 97.5 kg

AAY

11.6 m³ / 410 ft³

496 lb / 225 kg

AAD

14.6 m³ / 515 ft³

636 lb / 288 kg

AMJ

16.6 m³ / 586 ft³

557 lb / 253 kg

AMV

15.1 m³ / 533 ft³

542 lb / 246 kg

AYY

5.7 m³ / 202 ft³

298 lb / 135 kg

SAA

12.6 m³ / 448 ft³

580 lb / 263 kg

AMA

17.5 m³ / 619 ft³

712 lb / 323 kg

16ft pallets

24 m³ / 870 ft³

728 lb / 330 kg

20ft pallets

32.5 m³ / 1147 ft³

882 lb / 400 kg

96"x125" winged pallets

13.81 m³ / 488 ft³ (LD)

388 lb / 176 kg

88"x125" winged pallets

12.65 m³ / 447 ft³ (LD)

361 lb / 164 kg

96"x125" pallets

11.52 m³ / 407 ft³ (LD)

287 lb / 130 kg

88"x125" pallets

10.53 m³ / 372 ft³ (LD)

264 lb / 120 kg

(reference : IATA ULD technical manual Oct 10 & ULD manufacturers)

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ATA 25.56 / 53.61 – Main deck cargo loading system: General overview – Structural provisions and MDCLS BFE Depending on the floor structural provisions, a BFE manual cargo Optional secondary floor structure is necessary for each of following loading system can be installed on top of it on either all, or on a part of CLS configuration: the interfaces for the selected ULD configurations. SR 96" / 88" x 125" The main deck cargo loading system is a BFE equipment and is • 16 ULD 96" x 125" SR, crosswise provided by a supplier of the customers choice based on Airbus • 17 ULD 88" x 125" SR, crosswise interface and frame specifications. Airbus established with several BFE CLS manufacturers a frame agreement, confirming the way of AMA and 16ft / 20ft pallets working and required qualification as a BFE vendor for a CLS • 9 ULD 96" x 125" SR, lengthwise (AMA) + 4 SR installation on Airbus aircraft. • 3 ULD 20ft lengthwise (SR) + 7 SR The MDCLS assures loading, in-flight transport, and offloading of • 4 ULD 16ft lengthwise (SR) + 6 SR standard Unit Load Devices (ULD). • 8 ULD 16ft SBS + 6 SR The system restrains ULDs in the longitudinal, lateral and vertical Integrator transport directions during flight and landing. The maximum system height, or roll plane, is 2 inch (distance between • 42 ULD 62" x 88" in triple rows (AYY) + 6 in SBS. the top of the cargo tracks and the top of the conveyance • 20 ULD 62" x 88" (AYY) + 10 ULD 96" x 125" (AMJ). • 17 ULD 88" x 125" (SAA) SR + 14 ULD 62" x 88" (AYY) SR. components). • 18 ULD 96" x 125" (AMV) SBS + 5 ULD 88" x 125" (AAY). Depending on CLS configuration the main deck floor is equipped with adapters (secondary structure) which provide fitting points for a cargo • 23 ULD 88" x 125" (AAY). • 16 ULD 88" x 125" (AAD) SBS + 6 ULD 88" x 125" (AAY). loading system. Structural provisions part of basic aircraft allows 3 CLS SBS Options available configurations. The adapter sets needed to load a certain ULD configuration can be selected out of the option catalogue, the Freighter Configuration Guide Basic (FCG). • 18 ULD 96" x 125" SBS + 4 SR (basic) • 20 ULD 88" x 125" SBS + 3 SR (basic) • 22 ULD 88" x 108" SBS + 4 SR (basic) A330-200 Freighter - Brochure issue 5, April 2013

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ATA 25.56 / 25.51 – Cargo loading system: Main and lower deck cross sections The following pictures show typical ULD loading configurations in cross section of the A330-200F.

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ATA 25.56 / 53.61 – Cargo loading system: Configuration 1 and running loads (basic structural provision)

Note: BFE CLS certified A/C volume example MD volume:

11 894 ft³ (337 m³)

LD volume* :

3 562 ft³ (101 m³)

Bulk volume**: Total volume: A330-200 Freighter - Brochure issue 5, April 2013

348 ft³

(10 m³)

* LD configuration : 8 ULD 96"x125" +2 LD3 ** 50 % of bulk volume (695 ft³) taken into account

15 804 ft³ (448 m³) 61

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ATA 25.56 / 53.61 – Cargo loading system: Configuration 2 and running loads (basic structural provision)

Note: BFE CLS certified A/C volume example MD volume: LD volume* : Bulk volume**: Total volume: A330-200 Freighter - Brochure issue 5, April 2013

11 743 ft³ (333 m³) 3 282 ft³

(93 m³)

* LD configuration : 8 ULD 96"x125" +2 LD3

348 ft³

(10 m³)

** 50 % of bulk volume (695 ft³) taken into account

15 373 ft³ (435 m³) 62

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ATA 25.56 / 53.61 – Cargo loading system: Configuration 3 and running loads (optional structural provision)

Note: BFE CLS certified A/C volume example MD volume:

9 502 ft³ (269 m³)

LD volume* :

3 562 ft³ (101 m³)

Bulk volume**: Total volume: A330-200 Freighter - Brochure issue 5, April 2013

348 ft³

(10 m³)

* LD configuration : 8 ULD 96"x125" +2 LD3 ** 50 % of bulk volume (695 ft³) taken into account

13 412 ft³ (380 m³) 63

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ATA 25.56 / 53.61 – Cargo loading system: Configuration 4 and running loads (optional structural provision)

Note: BFE CLS certified A/C volume example MD volume:

9 258 ft³ (262 m³)

LD volume* :

3 282 ft³

(93 m³)

* LD configuration : 8 ULD 96"x125" +2 LD3

348 ft³

(10 m³)

** 50 % of bulk volume (695 ft³) taken into account

Bulk volume**: Total volume: A330-200 Freighter - Brochure issue 5, April 2013

12 888 ft³ (365 m³) 64

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ATA 25.56 / 53.61 – Cargo loading system: Configuration 5 and running loads (optional structural provision)

Note: BFE CLS certified A/C volume example MD volume:

7 837 ft³ (222 m³)

LD volume* :

3 562 ft³ (101 m³)

Bulk volume**: Total volume: A330-200 Freighter - Brochure issue 5, April 2013

348 ft³

(10 m³)

*** for the last single row positions the normal running load is used * LD configuration : 8 ULD 96"x125" +2 LD3 ** 50 % of bulk volume (695 ft³) taken into account

11 747 ft³ (333 m³) 65

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ATA 25.56 / 53.61 – Cargo loading system: Configuration multiple choice (=1+2+3+4+5) The CLS "Multiple Choice" concept allows the operators to load ULDs in a mix configuration : SBS and/or SR and/or AMA.

Example of mixed configurations which can be loaded :

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Example of mix configuration and optimized volume

Optimized volume MD volume*:

12 295 ft³

(348 m³)

* MD configuration: 18 96x125" SBS + 2 88x125" SBS + 3 96x125" SR

LD volume** :

4 513 ft³

(128 m³)

** LD configuration (with winged pallets): 8 WINGED pallets 96x125" + 2 LD3

348 ft³

(10 m³)

*** 50 % of bulk volume (695 ft³) taken into account

17 156 ft³

(486 m³)

Bulk volume***: Total volume:

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ATA 25.56 / 53.61 – Cargo loading system: 20ft pallet configuration (optional structural provision)

Note: BFE CLS certified

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ATA 25.56 / 53.61 – Cargo loading system: 16ft pallet configuration (optional structural provision)

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ATA 25.56 / 53.61 – Cargo loading system: Integrator configuration (optional structural provision)

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ATA 25.56 / 53.61 – Cargo loading system: Integrator configuration (optional structural provision)

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ATA 25.56 / 53.61 – Cargo loading system: Military pallet configuration (basic structural provision)

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ATA 25.51 – Cargo loading system: Lower deck, general description Lower deck compartment The lower deck cargo loading system is the same as on the passenger The usable volume per compartment based on a aircraft version. 88" x 125" pallets (10.52 m³ (372 ft³)) is: A330-200F forward and aft lower deck cargo compartment are • LD FWD compartment 42.10 m³ (1488 ft³) equipped with a semi-automatic, electrically powered cargo loading • LD aft compartment 42.10 m³ (1488 ft³) system. This CLS is compatible with ULDs designed to meet class II The usable volume per compartment based on a requirements according to NAS 3610. 96" x 125" pallets (11.51 m³ (407 ft³)) is: The lower deck CLS provide individual ULD restraint in each • LD FWD compartment 46.10 m³ (1628 ft³) compartment for the following ULDs / base plate sizes: • LD aft compartment 46.10 m³ (1628 ft³) • 88" x 125" The usable containerized volume based on a • 96" x 125" LD3 container volume of 4.30 m³ (153 ft³) is: • 60.4" x 125" (LD6 container) • 60.4" x 61.5" (LD3 container) • LD FWD compartment 60.65 m³ (2142 ft³) • LD aft compartment 51.98 m³ (1836 ft³) (reference: IATA ULD technical manual Oct 10 & ULD manufacturers)

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ATA 25.51 – Cargo loading system: General lower deck layout No change compared to the passenger version FWD compartment

Aft compartment

14x LD3 or 4x 88" Pallets + 2x LD3 or 4x 96" Pallets + 2x LD3

12x LD3 or 4x 88" Pallets or 4x 96" Pallets

ULD

ATA

NAS 3610

IATA

Half-size Half-size 60.4 x 61.5 in 60.4 x 61.5 in Full-size 60.4 x 125 in 88 x 125 in

LD3 LD1

2K2C 2K2C 2K3P 2K3P 2K2C 2L3P/2L4P 2A1P/2A4P 2A3P/2A4P/2A6P 2M1P/2M2P/2M3P

E/G C/H X/G/E H F F F F F

LD6

96 x 125 in

* option: additional container / 2K3 pallet in bulk cargo compartment A330-200 Freighter - Brochure issue 5, April 2013

Allowable MGW [lb] [kg] 3500 1587 3500 1587 3500 1587 3500 1587 7000 3174 7000 3174 10200 4626 11250

5103

Maximum number FWD aft bulk 14 12 1* 7 6 14 12 1* 7 6 7 6 7 6 4** 4 4**

4

** plus two LD3 container in the entrance area 74

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ATA 25.56 – Cargo loading system: Volume, tare and densities The following table summarize for each configuration typical values (volume, tare, density). MDCLS calculated weight derivated from a multiple choice system: approx. 1975 kg (4355 lb). A330-200F

Basic Aircraft (SBS Conf) config. 1 (96" SBS) config. 2 (88" SBS) config. 3 (96" SR) config. 4 (88" SR) config. 5 (AMA) Integrator 1 Integrator 2 Integrator 3 Integrator AAY Integrator AAD / AAY Integrator AMV / AAY A330-200F

Basic Aircraft (SBS Conf) config. 1 (96" SBS) config. 2 (88" SBS) config. 3 (96" SR) config. 4 (88" SR) config. 5 (AMA) Integrator 1 Integrator 2 Integrator 3 Integrator AAY Integrator AAD / AAY Integrator AMV / AAY

MD configuration

MD volume (ft³ / m³)

LD configuration

LD volume (ft³ / m³)

Bulk 695ft³ (19.7m³)*

22 ULD 96"x125" SBS pallets 22 ULD 96"x125" SBS pallets 23 ULD 88"x125" SBS pallets 16 ULD 96"x125" SR pallets 17 ULD 88"x125" SR pallets 9 AMA 96''x125'' SR + 4 ULD 96"x125" 20 AYY + 10 AMJ 48 AYY 88''x62'' 14 AYY + 17 SAA 23 AAY 88''x125'' SBS container 16 AAD 88''x125'' SBS container + 6 AAY 88''x125'' 18 AMV 96''x125'' SBS container + 5 AAY 88''x125''

11894 (336.8) 11894 (336.8) 11741 (332.5) 9502 (269.1) 9258 (262.2)

8 ULD 96"x125" +2 LD3 8 ULD 96"x125" +2 LD3 8 ULD 88"x125" +2 LD3 8 ULD 96"x125" +2 LD3 8 ULD 88"x125" +2 LD3

3562 (100.9) 3562 (100.9) 3282 (92.9) 3562 (100.9) 3282 (92.9)

348 (9.9) 348 (9.9) 348 (9.9) 348 (9.9) 348 (9.9)

7837 (221.9)

8 ULD 96"x125" +2 LD3

3562 (100.9)

348 (9.9)

9900 (280.3) 9696 (274.6) 10444 (295.7) 9430 (267.0)

26 LD3 lexan 26 LD3 lexan 26 LD3 lexan 26 LD3

3978 (112.6) 3978 (112.6) 3978 (112.6) 3978 (112.6)

348 (9.9) 348 (9.9) 348 (9.9) 348 (9.9)

10700 (302.9)

26 LD3

3978 (112.6)

348 (9.9)

11644 (329.7)

26 LD3

3978 (112.6)

348 (9.9)

payload in lb (T) (range mode / payload mode)

Total tare (lb / T)

Total volume (ft³ / m³)

Density net (lb/ft³ - kg/m³) (range mode)

Density net (lb/ft³ - kg/m³) (payload mode)

143300 (65) / 154323 (70)

9010 (4.09) 9010 (4.09) 8584 (3.89) 7288 (3.31) 7000 (3.18) 10212 (4.63) 17120 (7.77) 19894 (9.02) 19622 (8.90) 16654 (7.55) 18862 (8.56) 17446 (7.91)

15804 (447.52) 15804 (447.52) 15371 (435.26) 13412 (379.79) 12888 (364.95) 11747 (332.64) 14226 (402.84) 14022 (397.06) 14770 (418.24) 13756 (389.53) 15026 (425.49) 15970 (452.22)

8.5 (136) 8.38 (134) 8.64 (138) 10 (160) 10.43 (167) 11.17 (179) 8.69 (139) 8.62 (138) 8.2 (131) 9.21 (147) 8.28 (133) 7.88 (126)

9.19 (147) 9.08 (145) 9.36 (150) 10.82 (173) 11.29 (181) 12.11 (194) 9.45 (151) 9.41 (151) 8.95 (143) 10.01 (160) 9.05 (145) 8.57 (137)

141426 (64.15) / 152449 (69.15)

140765 (63.85) / 151788 (68.85) 143300 (65) / 154323 (70)

* 50% of bulk volume (695 ft³) taken into account

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ATA 25.56 – Cargo loading system: MD flexible floor structure concept Fully equipped floor grid including all options for adapter (FWD part shown only)

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ATA 25.56 – Cargo loading system: MD flexible floor structure concept BFE cargo loading system components

Adapter with 2 point attachment

Adapter with 3 point attachment

Adapter with 4 point attachment

Adapter with 4 point attachment

Side by side configuration

Single row configuration AMA configuration

Triple row configuration

Side by side configuration

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ATA 25.56 – Cargo loading system: MD flexible floor structure concept BFE cargo loading system components

Note: Roller units are not shown in schemes A330-200 Freighter - Brochure issue 5, April 2013

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ATA 25.56 – Cargo loading system: MD flexible floor structure concept Reinforced adapter concept provides robust floor to support ground handling loads. T and + shaped adapter provide fittings for 3-4 point lock attachment. Adapter are connected with support beam in x-direction to take ground handling loads during loading and unloading.

Adapter crossbeam to crossbeam connector A330-200 Freighter - Brochure issue 5, April 2013

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ATA 25.56 – Cargo loading system: MD CLS typical components The MDCLS consists of components for the conveyance of ULDs, components for the guidance of ULDs and components to restrain the ULDs in the correct position. Conveyance components are ball mats, ball trays, roller rails, loading bridge and the door sill protector. Guidance components include guide rails, side guides, centerline splitter, pivot guides and door guides. Restraining components include cargo locks, outboard and centerline restraints, and forward and aft end stops. The conveyance components installed in the ball mat area provide omni-directional handling of ULDs to facilitate loading the units. Conveyance components installed in areas other than the ball mat area permit ULD transport in the longitudinal direction. For the 16 / 20 ft pallets use of pivot guides are necessary. The use of the pivot Guides make the loading of the 16 / 20 ft pallets easy and saver. This pivot guide in the door area also act as a guide for the side by side loading and protect the door frame. Placards, mounted on the walls of the MDCC indicate weight, operating, and safety data relevant to the CLS.

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ATA 25.56 – Cargo loading system: MD CLS typical components Ball mats The ball mats provide support, and permit omnidirectional movement of the ULDs in the MDCC door area. The ball mats are installed between FR20 and FR27, and extend across the full width of the MDCC. The ball mats are usually bonded and riveted assemblies of aluminium alloy parts. These parts include skin panels, channel-section profiles, edge rails, ball unit housings, and a number of four attachment brackets. Cut-outs in the ball mats allow accommodation of other CLS components. The top surface of each ball mat is coated with antiskid paint. Individual low-friction ball units are installed in rows across each ball mat. Each ball unit is spring-loaded, and held in its housing with a retainer. The ball mats are fastened to the cargo tracks with studs and retainers.

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ATA 25.56 – Cargo loading system: MD CLS typical components Ball trays (optional depending on the CLS suppliers) The ball trays provide support, and permit omnidirectional movement of the ULDs in areas other than ball mat. They can be installed between FR27 and FR32 to extend the ball mat area for the 16 / 20 ft pallets loading capability. The ball tray assemblies are made of an extruded aluminium tray and two or more low-friction ball units. The ball trays are fixed to the cargo tracks.

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ATA 25.56 – Cargo loading system: MD CLS typical components Roller trays The roller trays are installed down the cargo compartment, apart from the ball mat area, to transport the ULD in their loading position. Each roller tray assembly is equipped with roller assemblies installed at intervals along its length, allowing an ease longitudinal movement of ULD in the cargo compartment. The roller pitch within the system does not exceed 10 inch. The roller rail assemblies are fastened to the cargo tracks with two or more tension studs.

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ATA 25.56 – Cargo loading system: MD CLS typical components Loading bridge and door sill protector The forward and aft door sill protectors are installed in the MDCC door entrance area to: • protect the aircraft structure at the door sill area from damage • permit lateral conveyance of the ULDs to and from the ball mat area during loading and unloading operations The door sill protectors are attached to the outboard cargo tracks, and are independently hinged. They are manually operated and rest on the spools of the MDCC door mechanism in their lowered positions. The door sill protectors must be in their fully raised positions before the MDCC door is closed. A lateral side-guide is installed at the end of the assembly facing towards the door frame to protect the aircraft structure. Ball and roller units are installed on the loading bridge to allow movement of ULDs in this area. A gas spring is installed adjacent to each support mechanism to ease lowering and raising the bridge. The gas springs provide the pressure to hold the door sill protector in its raised position.

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ATA 25.56 – Cargo loading system: MD CLS typical components Center guide restraint / retractable The retractable center line restraints, installed in the ball mat area provide lateral and vertical restraint of the ULDs between positions ABR and ABL. Each restraint assembly has a base plate and inner and outer restraint pawls. The restraint pawls can be manually retracted towards the MDCC door, where they lie below the CLS rollplane during ULD on-loading and off-loading operations. The restraint is fixed in the cargo track adapter via shear and tension studs.

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ATA 25.56 – Cargo loading system: MD CLS typical components Center guide restraint / overrideable The overrideable guides, installed on the center cargo track, provide lateral and vertical restraint of the ULDs loaded on side by side positions. Each unit is equipped with rollers or ball units to assure optimal conveyance of the ULDs. The latch-pawls are maintained in the up position by means of spring tension and can be overridden by a pallet in case the units are not needed for an ULD loading configuration. Units have a manual lock-down feature to keep them always in down position or to allow transportation of non unitized loads (ULD tiedowned to the floor without using latches) in the cargo compartment. Units can be joined with either roller trays or ball trays: • single latch with roller or ball trays • double latches connected together with ball or roller trays • triple latch connected with four roller trays (in the kink area) The guides are fixed to the cargo track and adapter with tension and shear studs.

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ATA 25.56 – Cargo loading system: MD CLS typical components Overrideable side guide The overrideable guides provide lateral guidance and alignment for the ULDs in single-row positions. Each guide assembly consists of a base and a guide pawl. The forward and aft wings allow the pawl to retract (down) below the CLS roll-plane level, when the guide is overridden for SBS loading. Some side guides have a manual lock system that allows the pawl to be permanently locked in the down position. The pawl can be unlocked with a lever. The guides are installed in the floor adapters with tension and shear studs.

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ATA 25.56 – Cargo loading system: MD CLS typical components Overrideable side guide Cross tracks are installed along the outboard sides of the MDCC. These cross tracks have side guides (rails) attached to their outboard side for guidance of the ULDs in side by side layout for 96" ULDs. The 96 inch cross tracks can also have an overrideable guide pawl inboard for the 88 inch wide ULDs when loaded in the side by side layout. The cross tracks are equipped with horizontal rollers to support the ULDs during loading operation. The units are fastened on floor adapter and cargo track.

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ATA 25.56 – Cargo loading system: MD CLS typical components Retractable cargo latches The retractable cargo latches, installed across the MDCC between the ULD loading positions, provide longitudinal and vertical restraint of the ULDs. Each latch assembly has an aluminium base, inner and outer locking pawls. The unit can be manually lowered when not required for ULD restraint. The latches are fastened to the cargo tracks with the tension studs and the shear studs.

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ATA 25.56 – Cargo loading system: MD CLS typical components End stops The fixed end stops provide aft and vertical restraint of the ULDs loaded on the last ULD positions in the main deck cargo compartment. The fix end stop are fastened to the cargo tracks.

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ATA 25.55 / 25.50 – Cargo compartment floor panels and anti-skid surface The MDCC floor consist of honeycomb - sandwich panels with antiskid surface. On the LDCC, the panels (LH and RH of aircraft centerline) have an anti-skid surface. Optionally, all cargo floor panels (4 in total) in the lower deck forward and aft cargo compartments can have enhanced anti-skid characteristics by application of corrugated paint as top coating (refer to the FCG for further information).

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ATA 25.56 – Cargo loading system: MDCC placards (ATA 11.39) CLS related placards will be furnished by the BFE CLS supplier (i.e: loading chart, ULD position indication, etc). Related optional requests for 2nd language and weight indication in kg and lbs, need to be addressed to the CLS supplier. Airbus will only take care for placard set installation.

MDCC placards

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ATA 25.56 / 11.39 – Cargo loading system: MDCC floor marking overview To enhance the readability of ULD positions in MDCC, an ULD floor marking option can be selected from Airbus. The floor markings will be installed to ease the ULDs positioning over the main deck cargo loading system.

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ATA 33.36 – Main deck cargo compartment lighting • General overview • MDCC lighting • Cargo door light

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ATA 33.36 – Main deck cargo compartment lighting: General overview Description The main deck cargo compartment lights and the cargo door light controls are located in the inside and outside CDOP (Cargo Door Operation Panel) and can be operated with gloves. A separate lighting system is installed in each cargo compartment. All lights are manually controlled by a switch, located on a service panel in the respective doorway. The control switch is located adjacent to the cargo door for the respective compartment. Each cargo compartment has an adequate light level for cargo operation. The loading area light provides sufficient light to allow the reading of labels on the ULDs. The lighting of the lower deck cargo compartment is similar to the PAX A330-200. For further information concerning this part, refer to the PAX brochure.

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ATA 33.36 – Main deck cargo compartment lighting: MDCC lighting 14 HID (High Intensity Discharge) lights are installed in the MDCC. Weight 1,4 kg Operating voltage115 VAC Operating load 69 VA Housing Aluminum Illumination on floor level ~ 100 lx

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ATA 33.36 – Main deck cargo compartment lighting: Cargo door light 1 HID light is installed in cargo door lining to support cargo loading equipment operation in this area. The CDL is the identical MD CCL type with same P/N. Installed in the cargo door lining

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ATA 52.30 – Cargo doors • • • •

General overview Main deck cargo door Lower deck cargo doors Bulk cargo door

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ATA 52.30 – Cargo doors: General overview Description The A330-200F main deck cargo door is located on the forward left hand side of the fuselage. It is electrically controlled, hydraulically operated and has a manual backup mode. Lower deck cargo doors are located on the lower deck right hand side of the fuselage (as for passenger aircraft). Forward and aft cargo doors are electrically controlled, hydraulically power operated and have a manual backup mode. The bulk door is plug type door, operated by hand. Main deck cargo door can be operated (opening / closing) during wind gusting up to 60 knots. Lower deck cargo door can be opened and closed up to 40 knots and can left open up to 60 knots. All hydraulically operated cargo doors are supplied by the electrically driven hydraulic pump of the yellow hydraulic system. In case of no electrical and / or hydraulic power the locking and / or latching shaft can be operated manually using a separate tool which can be connected to the shaft. All cargo doors can be operated simultaneously.

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ATA 52.30 – Cargo doors: Main deck cargo door The main deck cargo door is located between frame C20 and C29. It provides a clear opening of: • height : 2.62 m (103.1 in) • width : 3.58 m (141 in) The opening angle is 65°.

The door is mechanically locked in the latched position. The locking is operated electrically and the latching hydraulically. Door controls are fitted on panels located inside (1) and outside the aircraft. Individual locking indicators (flags) for each hook are provided outside the door, visible from the ground (2).

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ATA 52.30 – Cargo doors: Lower deck cargo doors The forward cargo door is located between frame C20 and C26A. It provides a clear opening of: • height : 1.70 m (66.9 in) • width : 2.70 m (106.3 in)

The aft cargo door is located between frame C59A and C65. It provides a clear opening of: • height : 1.68 m (66.1 in) • width : 2.72 m (107.2 in)

The bulk cargo door is located between frame C67 and C69. It provides a clear opening of: • height : 1.07 m (42.2 in) • width : 0.95 m (37.4 in)

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ATA 52.30 – Cargo doors: Lower deck cargo doors The doors are opened outwards and upwards hydraulically. They are manually locked and unlocked by means of two operating handles: • a latching handle which activates 10 latches • a locking handle which operates a locking shaft with fitted cams The doors are designed to carry the hoop tension loads from internal pressure. They are of conventional design, having an outer and inner skin with an internal structure of machined frames and sheet metal beams. This structure upper ends form hinges for the door. Its lower ends are connected to the latching hooks. The individual control mechanism for the hooks has an over-centering system which guaranties hook latching irreversibility; when the fuselage is pressurized, a torque is created which tends to hold each hook in the closed position. This locking stability has been confirmed on the fatigue test airframe. A dual electric warning system in the flight deck indicates: • positive locking of the handle in its recess • that the door is flush with the fuselage profile and locked

Aft cargo door

In addition, this system enables the crew to identify the locking of each door separately.

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ATA 52.33 – Cargo doors: Bulk cargo door The bulk cargo door is operated, latched and unlatched manually from The door is counterbalanced by a tension spring (1). The door is outside and inside. It is opened by being pushed inwards and upwards connected to the door locking warning system. It is possible to open and is locked in the open position on the ceiling of the compartment. the door from the inside. This door is of plug-type design.

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ATA 12.00 – Ground handling and servicing • • • • •

General overview Ramp layout Turn around time Aircraft ground stability Tail stanchion interface

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ATA 12.00 – Ground handling and servicing: General overview Description

Options available

This section provides an overview on the various interfaces between Installation of an additional refuel panel on the right wing. the freighter and the associated ground service equipment used on the Installation of an additional refuel panel on the left wing. ramp during aircraft turn-around. Aim is to offer flexibility in terms of aircraft servicing by a refuelling selection and control capability from the right wing. Basic aircraft is The time frame covered by this part, called turn around time, is only equipped with one refuel / defuel panel. "chocks on – chocks off", with a limited of over-lap into preparation for push-back. For further information, please refer to FCG. Information included in this brochure does not replace or supersede the data given in the aircraft official documents such AMM (Aircraft Maintenance Manual), WBM (Weight and Balance Manual) etc.

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ATA 12.00 – Ground handling and servicing: Ramp layout For ground services, typical vehicles can be used.

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ATA 12.00 – Ground handling and servicing: Turn around time For a basic configuration, i. e. 18 96"x125" ULDs side by side and 4 96"x125" ULDs single row on main deck and 8 88"/96" pallets with 2 LD3 on the lower deck, the turn around time is about 62 minutes. This time is based on manual ULD handling on the main deck and powered ULD handling lower deck.

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ATA 12.00 – Ground handling and servicing: Aircraft ground stability

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ATA 12.00 – Ground handling and servicing: Tail stanchion interface Even if A330-200F is not likely to tail down, a tail stanchion can be used. Provisions are provided on the basic aircraft.

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Chapter 4 – Associated information

ATA 21.00 – Air conditioning • General overview • System overview 1. Air generation 2. Air distribution & ventilation 3. Temperature control 4. Pressure control • Detailed system description 1. Flight deck & courier area 2. Main deck cargo compartment 3. Lower deck cargo compartment

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ATA 21.00 – Air conditioning: General overview Description

Options available

The air conditioning and pressurization system design is compliant Air conditioning system provides: with the requirements of FAR 25.857 class "E" for the main deck cargo • F/D, courier area and main deck cargo: compartment requirements and class "C" for the lower deck cargo ◦ ventilation and temperature control as baseline compartment requirements. • Lower deck bulk cargo: Air conditioning system provides following functions: ◦ ventilation and heating as baseline • Lower deck FWD cargo: • air generation ◦ ventilation and temperature control available as catalog option ◦ condition outside air • Lower deck aft cargo: ◦ provide cold air and hot air ◦ ventilation and heating available as catalog option • ventilation ◦ distribute air to all consumers ◦ ventilate cargo compartments • temperature control ◦ to maintain the temperature selected at every location by mixing cold and hot air • pressure control ◦ control pressure inside aircraft by regulating the air outflow In case of MDCC smoke detection, the air ventilation flow shut-off to isolate the MDCC. The air conditioning system retains ventilation and heating of cockpit and courier area in shut-off mode by operation of one pack.

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ATA 21.00 – Air conditioning: System overview Air generation • Hot bleed air is taken from the engines, the APU or high pressure ground air supply units. • One part is guided to the air conditioning packs and is cooled down there. • The other part remains as hot trim air and is supplied to the hot air manifold. • The amount of airflow taken from the engines can be selected: ◦ NORM (100%) approx. 1,9 kg/s in cruise ◦ LOW (80%) approx. 1,5 kg/s in cruise ■ SFC reduction by approx. 0,5 % (compare to NORM mode) ■ slightly decreased air conditioning performance ■ decreased outside air supply ■ e.g. for for flights with no live animals, perishable goods or dry ice presence ◦ HIGH (115%) approx. 2,3 kg/s in cruise (to increase system performance) ■ SFC increase by approx. 1,0 % (compare to NORM mode) ■ shorter time for cool down or heat up ■ increased outside air supply

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ATA 21.00 – Air conditioning: System overview Air distribution • Outside air and recirculated air are mixed in the mixer and supplied as mixed air to the consumers / compartments.

Ventilation • The ventilation system allows to have homogenous air distribution to all compartments ◦ avoids "dead corners" ◦ avoids hot and cold spots

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ATA 21.00 – Air conditioning: System overview Temperature control • F/D, courier area and main deck cargo: ◦ ventilation and temperature control as baseline • lower deck bulk cargo: ◦ ventilation and heating as baseline • lower deck FWD cargo and aft cargo: ◦ options available • The temperature inside the temperature control zones is regulated by modulating the temperature of the supplied air. • Hot trim air or electrical heaters (bulk compartment) are used to heat the supply air. Schematic temperature control system

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ATA 21.00 – Air conditioning: System overview Pressure control • The Cabin Pressure Control System (CPCS) controls the cabin pressure to safe and comfortable values by modulating the air pressure sinks (outflow valves) according to an optimized pressure schedule. • The CPCS protects the A/C from negative and positive overpressure. • The CPCS protects the A/C from residual pressure at door opening. • The pressure control system is the same system as it is used in the passenger aircraft. • In case of fire, the aircraft inside pressure can be reduced manually to 20.000 ft to extinguish the fire in the main deck in accordance to class "E" requirements. Schematic CPCS equipment

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ATA 21.00 – Air conditioning: F/D and courier area General • Supply air is conditioned outside air from the air-conditioning packs (no recirculation). ◦ no recirc air to avoid smell or other contaminations from the load in main deck cargo compartment. • For heating hot trim air will be used. • selectable temperature range 18°C–30°C ◦ F/D via selector in the OVHD panel ◦ courier area via FAP in the courier area.

Air extraction system • G&T (Galley and Toilet) air extraction ◦ extracts the air out of the lavatories and galleys to avoid / reduce odor in the courier area ◦ ventilates the courier area

Flight crew rest compartment (optional) • independent ventilation and temperature regulation system • digital control panel integrated in the AAP ◦ temperature selection between 15°C and 25°C • individual air for each bunk

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ATA 21.00 – Air conditioning: Main deck cargo compartment Temperature zones • 2 temperature control zones: MD FWD CC and MD AFT CC • Air is supplied via 4 supply zones. This allows to create 4 "internal control zones". ◦ improved temperature distribution within the long zones ◦ improved redundancy for temperature sensors

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ATA 21.00 – Air conditioning: Main deck cargo compartment Main deck cargo compartment Ventilation • Ventilation in the MDCC will be achieved by an enhanced piccolo ducting (improved version of widebody freighter ducting). • 2 dimensional airflow vortices provides controlled air circulation in the cargo compartment.

Temperature control • Selectable temperature range: 5°C to 25°C for each main deck cargo zone ◦ selectable from OVHD - panel in the cockpit ◦ temperature indication in courier area via FAP • Main deck cargo isolation valves push button to stop the air supply in case of fire. ◦ selectable from OVHD - panel in the cockpit ◦ F/D and courier area air supply will not be stopped.

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ATA 21.00 – Air conditioning: Lower deck cargo compartment Lower deck FWD cargo compartment

Ventilation • Lower deck cargo compartment ventilation is based on negative differential pressure. ◦ Air is extracted out of the cargo compartment. ◦ Due to negative differential pressure air follows into the compartment. ◦ The extracted air is fed towards the valve and leaves the aircraft.

• optional ventilation + temperature control system ◦ selectable temperature range 5°C to 25°C ◦ Ventilation can be switched off by P/B.

Note: Baseline aircraft without installed LD aft cargo heating and LD FWD cargo temperature control may have very low temperatures in LD cargos if MD cargo is selected to cold temperatures.

Example of overhead panel principle

Schematic LDCC ventilation A330-200 Freighter - Brochure issue 5, April 2013

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ATA 21.00 – Air conditioning: Lower deck cargo compartment Lower deck aft cargo compartment • A heating system using hot trim air is available as an option. ◦ Allowing heating temperature selection of 5°C to 25°C. ◦ Similar to bulk compartment heating system, it provides heating air only, there is no active cooling capability within the system.

Lower deck bulk cargo compartment • ventilation system as baseline • heating as baseline ◦ Supplied air is heated by an electrical heater. ◦ max. compartment temperature 25°C ◦ no cooling possible ◦ piccolo blow out below bulk CC floor to reduce the heat exchange through the cargo floor

Schematic bulk cargo A330-200 Freighter - Brochure issue 5, April 2013

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Chapter 4 – Associated information

ATA 23.73 – CIDS • General overview • Courier area layout (basic) • FAP functions

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ATA 23.73 – CIDS: General overview Description

Options available

The Cabin Intercommunication Data System (CIDS) (ATA 23-73) is CIDS components layout will be adapted to each courier area the microprocessor-based cabin management system, installed on all configuration. versions of the A330-200F aircraft, and provides most of the required No option offered in the FCG. cabin related functions for the cockpit, courier area occupants, cargo loaders and maintenance teams. CIDS is the cabin network used to accomplish the functional control, operation, data transmission, testing and monitoring of various courier area systems, both on ground and in flight. CIDS is designed to provide maximum performance with minimum customer configuration needs, whilst remaining flexible enough to accommodate changing market demands without the need for time consuming and expensive hardware modifications. The CIDS controls the following courier area related systems: • • • • • • • •

courier and service interphone public address public lighted signs reading and working lights general illumination emergency evacuation signaling smoke indication indication and control of air conditioning

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ATA 23.73 – CIDS: CIDS courier area layout (basic) Note: The EPO describes the accurate equipment positions.

AAP A330-200 Freighter - Brochure issue 5, April 2013

Handset

AIP 123

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ATA 23.73 – CIDS: FAP functions • The FAP (Flight Attendant Panel) is the interface to the CIDS for cabin occupants. • It is installed on lavatory wall. The FAP is used for: • control of courier and cargo area systems • indication of courier area system status Note: FAP pages are shown for information only and are subject to change.

FAP : Flight Attendant Panel

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Chapter 4 – Associated information

ATA 26.00 – Fire protection • • • •

General overview Class E and procedure in MD Detailed description of SDS Fire suppression system

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Chapter 4 – Associated information

ATA 26.00 – Fire protection: General overview Description

Options available

The fire protection system consists of 2 sub-systems:

Basic lower deck cargo compartment fire suppression bottles can be replaced with alternate equipment. Courier area is customized and offered with a baseline and 2 options.

• smoke detection system • fire suppression system Smoke is detected in the avionics, main deck cargo, lower deck cargo compartments and in the lavatory and customizable areas (FCRC, stowage, stowage / galley). Fire suppression system is provided for the lower deck cargo compartments and in the lavatory waste bin A built-in fire suppression system is controllable by the pilot. A separate smoke detector system gives warning to pilot for all cargo compartments. The smoke detection system and fire suppression system operates also on the ground if APU or ground power is available. The fire protection system for the forward and aft lower deck cargo compartments is conform to class "C" requirements, the main deck cargo compartment to class E requirements according to JAR/FAR 25.857.

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Chapter 4 – Associated information

ATA 26.00 – Fire protection: Class E and procedure in MD Class E

Procedure for the MD

A330-200F main deck cargo compartment is a class E compartment.

In case of smoke detection in MDCC the following procedure applies:

A class E cargo compartment is one on airplanes used only for the carriage of cargo and in which: • there is a separate smoke or fire detector system to give warning to the flight deck crew • there are means to shut off the ventilating airflow to, or within, the compartment, and the controls for these means are accessible to the flight crew in the crew compartment • there are means to exclude hazardous quantities of smoke, flames, or noxious gases, from the flight crew compartment • the required crew emergency exits are accessible under any cargo loading condition

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• call from cockpit to inform all A/C occupants to return to their seat and put their oxygen mask • manual depressurisation to 20 000 ft cabin altitude (from cockpit) • oxygen system provides 180 min of autonomy • land on the next suitable airport

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ATA 26.00 – Fire protection: Detailed description of SDS The smoke detection system has optical-multicriteria type smoke detectors installed in the ceiling of each LD cargo hold. One cavity houses two smoke detectors for dual loop detection system. On A330-200F, there are 2 cavities in the forward hold and 3 in the aft. Smoke in one cavity activates the cargo smoke warning if: both smoke detectors detect it or one smoke detector detects it and the other is inoperative. With a detector failure, the system will revert to a singleloop operating condition. If LDCC ventilation is installed, and the cargo smoke warning is activated in either hold, the associated isolation valves automatically close and the extraction fan stops. The SDS of the MDCC is designed with 15 active smoke detectors. In case of smoke the ventilation system will be shut off and the depressurization process would be initiated. In addition to the LDCC & MDCC, smoke detectors are located in the following courier area monuments: lavatory, galley G1 (or FCRC / galley stowage S1). The smoke detection system gives a visual and aural warning in the cockpit. A dual loop system has been provided to improve dispatch reliability.

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Chapter 4 – Associated information

ATA 26.00 – Fire protection: Fire suppression system The lower deck cargo compartment fire suppression system for When the CIDS-SDF receives a smoke signal from the smoke A330-200F is equipped with two fire suppression bottles. detectors it sends a signal to: The bottles are installed behind the forward cargo compartment side wall panel. Each bottle has two discharge outlets, one for the forward cargo compartment and one for the aft cargo compartment. The discharge outlets are sealed with metal diaphragms and each outlet has a discharge head. Distribution pipes connect the discharge heads to the spray nozzles in the cargo compartments.

• the Flight Warning Computer (FWC) engages the master warning light, the continuous repetitive chime sounds and the Engine / Warning Display (EWD) shows smoke • the ventilation controller so that the related cargo compartment isolation valves be closed • the related AGENT pushbutton • CIDS through internal link

The bottles are pressurized to 360 psi (24.8 bar) and can operate After pushing the related AGENT button, electrical power will be between temperatures from 70°C (158°F) to -40°C (-40°F). supplied to the squibs, the cartridges rupture the metal diaphragms and opens the related discharge outlets of the fire suppression bottles. Bottle 1 has a volume of 2170 in³ and contains 43.09 kg (35.56 l) of halon 1301. Bottle 2 has a volume of 1600 in³ and contains 31.75 kg The fire suppression agent from bottle 1 flows directly to the related (26.22 l). The standard suppression system is certified for 240 minutes cargo compartment spray nozzles. Halon from bottle 2 flows through a suppression time. flow metering system FMS) installed for each discharge outlet. The FMS ensures the agent is released slowly and sufficient agent concentration is maintained for 240 minutes.

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Chapter 4 – Associated information

ATA 35.00 – Oxygen • General overview • Oxygen storage & container implementation

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ATA 35.00 – Oxygen: General overview Description A common source gaseous oxygen system for cockpit and courier area occupants is provided with three oxygen cylinders (118 m³) installed in the forward lower cargo compartment behind the sidewall lining. The crew oxygen distribution system provides supplemental oxygen and smoke protection (1) to all cockpit occupants. The courier area oxygen distribution system provides supplemental oxygen to all courier area occupants. In the standard configuration, PAX-style oxygen containers (2) with continuous flow masks (automatically presented when required) provide supplemental oxygen to four courier area occupants. The common source gaseous oxygen system is designed for 180 min ETOPS operation. First aid oxygen and fire protection is provided by portable oxygen equipment. Two protective breathing equipment units (TSO-C116 certified, cockpit and courier area) and one portable (3) oxygen cylinder (11 m³, courier area) are installed.

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ATA 35.00 – Oxygen: Oxygen storage & container implementation The common source gaseous oxygen storage is installed in the forward lower cargo compartment (similar to the A330 PAX gaseous oxygen system for passengers). The design provides a convenient servicing location and design flexibility to install 3 standard 118 m³ oxygen cylinders. With the use of 3 cylinder, up to twelve courier area occupants are supported under standard operating procedures. Oxygen mask installation in the cockpit is identical to the PAX version aircraft. Courier area occupant oxygen mask containers and portable equipment for the standard option are installed as shown below. In addition, the courier area oxygen distribution system layout easily supports all optional courier area configurations.

Oxygen storage layout

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Chapter 5 – Appendix

Appendix • • • •

General overview Live animals transportation Perishable goods transportation Dangerous goods transportation

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Appendix: General overview Description The transportation of live animals (AVI) and PERishable goods (PER) requires appropriate environmental conditions to be met on ground and in flight. For live animals in general, high temperature in combination with high humidity level could cause serious stress for animals and shall be avoided. Perishable goods need to be transported within specified environmental conditions, as maintaining the cool chain is key to product quality and shelf life.

Options available • FWD cargo installation of ventilation plus temperature control system (refer to ATA 21.00 ventilation and temperature control) • AFT cargo installation of ventilation plus heating system • access capability to the main deck cargo compartment during flight: Additional equipment and alerting system (aural and visual) in response to the Airworthiness Authority requirements for access to the main deck cargo compartment during flight can be installed on top of aircraft basic provisions.

Furthermore dry-ice, when transported in important quantities, could require a ventilation system in order to evacuate the sublimated CO2 from the cargo hold. Dry ice, classified as dangerous good commonly is used as refrigerant e.g. for frozen meat transportation. Systems exist to adapt the environmental conditions of A330-200F main deck and lower deck cargo holds as required for sensitive cargo transportation. • Applicable regulations IATA Live Animals Regulations (LAR), Perishable Cargo Regulations (PCR), CITES, government regulations.

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Appendix: Live animals MD cargo compartment • ventilated & temperature controlled, 2 zones, each 5 to 25°C (41 to 79°F) • 9 AMA/HMA ULD loading capability • courier area for max. 12 animal attendants

LD cargo compartment • FWD: Optional ventilation or ventilation & temp. control available (5 to 25°C) • aft: Optional ventilation & heating system (5 to 25°C) • bulk: Basic ventilation & heating system (5 to 25°C)

Likes to travel at 18°C

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Appendix: Perishable goods Environmental Control Systems (ECS) to: • maintain the required temperature range for transport • evacuate detrimental gases (e.g. CO2, ethylene) • prevent from too high relative humidity levels Perishable goods frequently transported by air: • • • •

flowers meat, dairy products, fish vegetables and fruits pharmaceutical products

Temperature categories (IATA perishables classification): • • • •

ambient : 15 to 20°C cool : 2 to 15°C cold : -9 to 2°C frozen : below -10°C

Refer to IATA Perishable Cargo Regulations (PCR) for environmental conditions required for the different types / commodities of perishable goods transported by air.

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Chapter 5 – Appendix

Appendix: Dangerous goods • The A330F can transport any dangerous goods if in accordance to the valid ICAO and IATA applicable regulations. • As for specifics: ◦ dry ice goods: SIL 00-081 applies ◦ magnetic materials, limitations as per SIL 00-087 ◦ radioactive goods, distance and quantity limitations as per ICAO / IATA guidelines

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Glossary of abbreviations

Glossary of abbreviations (1/2) A/C AAP ACP AHM AIP AMM AMU APU ASPSU AVI B/C BFE BITE C/A CAM CC CCL CDL CDOP CFRP CIDS CLS CMC CMD CPCS DEU DOLLI ECAM ECS

Aircraft Additional Attendant Panel Audio Control Panel Airport Handling Manual Attendant Information Panel Aircraft Maintenance Manual Audio Management Unit Auxiliary Power Unit Autonomous Standby Power Supply Unit Live Animals Business Class Buyer Furnished Equipment Built-In Test Equipment Cabin Attendant (Seats) Cabin Assignment Module Cargo Compartment Cargo Compartment Lighting Cargo Door Light Cargo Door Operation Panel Carbon Fiber Reinforced Plastic Cabin Intercommunication Data System Cargo Loading System Central Maintenance Computer Command Cabin Pressure Control System Decoder/Encoder Unit Dome LED Light Electronic Centralized Aircraft Monitoring Environmental Control System

A330-200 Freighter - Brochure issue 5, April 2013

ELT EPSU ETOPS EVAC EWD F/D FAP FCG FCRC FL FSB FWC FWD G&T GFRP GMF GSE HAO HCCAS HID IATA ICAO ICS IPCU LD LDCC LH LR LRU

Emergency Locator Transmitter Emergency Power Supply Unit Extended Range Twin Engine A/C Operations Evacuation Engine Warning Display Flight Deck Flight Attendant Panel Freighter Configuration Guide Flight Crew Rest Compartment Flight Level Fasten Seat Belts Flight Warning Computer Forward Galley &Toilet Glass Fiber Reinforced Plastic General Market Freighter Ground Support Equipment Heated Air Outlet High Comfort Cabin Attendant Seat High Intensity Discharge International Air Transport Association International Civil Aviation Organization Interior Color Spec Ice Protection Control Unit Lower Deck Lower Deck Cargo Compartment Left Hand Long Range Line Replaceable Unit

A330-200F

Glossary of abbreviations

Glossary of abbreviations (2/2) MCU MD MDCC MDCD MFC MLW MTOW MZFW NM NS OBRM OH OMS OVHD P/N PAX PBE PCR PDU PER PISA RH RTS S/W SAR SBS SDAC SDCU SDF

Master Control Unit Main Deck Main Deck Cargo Compartment Main Deck Cargo Door Maximum Fuel Capacity Maximum Design Landing Weight Maximum Design Takeoff Weight Maximum Design Zero Fuel Weight Nautical Mile No Smoking On Board Replaceable Module Operational Hours On board Maintenance System Overhead Display Part Number Passenger Protective Breathing Equipment Perishables Cargo Regulations Power Drive Unit Perishable goods Passenger Interface and Supply Adapter Right Hand Return To Seat Software Search And Rescue Side by Side System Data Analog Converter Smoke Detection Control Unit Smoke Detection Function

A330-200 Freighter - Brochure issue 5, April 2013

SDS SFC SFE SR STWG ULD

Smoke Detection System Specific Fuel Consumption Supplier Furnished Equipment Single Row Stowage Unit Load Device

A330-200F

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Disclaimer © Airbus S.A.S, 2013 – All rights reserved – Proprietary document.

This licence is governed by French law and exclusive jurisdiction is given to the courts and tribunals of Toulouse (France) without By taking delivery of this Brochure (hereafter “Brochure”), you accept prejudice to the right of Airbus to bring proceedings for infringement of on behalf of your company to comply with the following: copyright or any other intellectual property right in any other court of No other property rights are granted by the delivery of this Brochure competent jurisdiction. than the right to read it, for the sole purpose of information. Airbus, its logo, A300, A310, A318, A319, A320, A321, A330, A340, This Brochure, its content, illustrations and photos shall not be A350, A380 and A400M are registered trademarks. modified nor reproduced without prior written consent of Airbus S.A.S.

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A330-200 Freighter - Brochure issue 5, April 2013

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Credits Graphics and layout by Sonovision Deutschland GmbH. Photos by Sonovision Deutschland GmbH and EXM: Hervé Berenger, Hervé Goussé and Philippe Masclet

AIRBUS S.A.S. 31707 Blagnac Cedex, France © AIRBUS S.A.S. 2013. All rights reserved, Airbus, its logo, and product names are registered trademarks. Concept design by Multi Media Support 20131370. Photos by EXM Company: H. Beranger, H. Gousse, P. Masclet, P. Jalby. Computer renderings by Fixion. Reference G25M13017173, Issue 5. April 2013. Printed in France by Airbus Print Centre. Confidential and proprietary document. This document and all information contained herein is the sole property of AIRBUS S.A.S.. No intellectual property rights are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of AIRBUS S.A.S. This document and its content shall not be used for any purpose other than that for which it is supplied. The statements made herein do not constitute an offer. They are based on the mentioned assumptions and are expressed in good faith. Where the supporting grounds for these statements are not shown, AIRBUS S.A.S. will be pleased to explain the basis thereof. This brochure is printed on Triple Star Satin. This paper is produced in factories that are accredited EMAS and certified ISO 9001-14001, PEFC and FSC CoC. It is produced using pulp that has been whitened without either chlorine or acid.The paper is entirely recyclable and is produced from trees grown in sustainable forest resources. The printing inks use organic pigments or minerals. There is no use of basic dyes or dangerous metals from the cadmium, lead, mercury or hexavalent chromium group. The printer, Airbus Print Centre (France 31707), is engaged in a waste management and recycling programme for all resulting by-products.