Aircraft Characteristics Publication ACP

eral maintenance proce- dure BD500-A-J10-10-02-01AAA-913A-A 2017-08-08 5 50001-54999, 55001-59999 Forward cargo compart- ment volume, weight and BD500-A-J14-20-00-01AAA-030A-A 2023-03-23 12 50001-54999, 55001-59999 BD500-3AB48-13800-00 Applicable to: All 2025-11-27 Page 2 Document title Data module code Issue date No. of pages Applicable to maximum item dimen- sions - Technical data Aft cargo compartment volume, weight and max- imum item dimensions - Technical data BD500-A-J14-20-00-02AAA-030A-A 2023-03-23 12 50001-54999, 55001-59999 Aircraft touch and no- touch zones - Technical data BD500-A-J15-30-00-00AAA-030A-A 2019-10-21 5 50001-54999, 55001-59999 Aircraft antennas - Tech- nical data BD500-A-J23-00-00-00AAA-030A-A 2024-08-23 2 50001-54999, 55001-59999 Aircraft performance - Technical data BD500-A-J00-00-00-13AAA-030A-A 2024-12-06 14 50001-54999 Aircraft performance - Technical data BD500-A-J00-00-00-13AAB-030A-A 2024-12-06 12 55001-59999 Operating conditions - Technical data BD500-A-J00-00-00-17AAA-030A-A C 2025-10-29 13 50001-54999 Operating conditions - Technical data BD500-A-J00-00-00-17AAB-030A-A 2020-07-08 12 55001-59999 Ground maneuvering - Technical data BD500-A-J00-00-00-19AAA-030A-A 2019-10-22 33 50001-54999 Ground maneuvering - Technical data BD500-A-J00-00-00-19AAB-030A-A 2019-10-22 33 55001-59999 Ground maneuvering, turning radii - Technical data BD500-A-J09-20-01-00AAA-030A-A 2018-02-05 4 50001-54999, 55001-59999 Ground maneuvering, visibility from flight com- partment - Technical data BD500-A-J09-20-01-01AAA-030A-A 2016-01-13 3 50001-54999, 55001-59999 Wheel chocks - Handling procedure BD500-A-J10-16-01-01AAA-912A-A 2024-05-15 6 50001-54999, 55001-59999 Terminal servicing - Technical data BD500-A-J00-00-00-18AAA-030A-A 2022-09-30 40 50001-54999 Terminal servicing - Technical data BD500-A-J00-00-00-18AAB-030A-A 2022-09-30 40 55001-59999 Refueling - rate and time - Technical data BD500-A-J12-10-28-01AAB-030A-A 2017-01-16 6 55001-59999 Deicing/Anti-icing - Remove ice BD500-A-J12-31-00-00AAA-261A-A C 2025-10-29 2 50001-54999, 55001-59999 Crew safety precau- tions - dangerous areas - Technical data BD500-A-J15-30-10-00AAA-030A-A 2019-12-03 3 50001-54999 BD500-3AB48-13800-00 Applicable to: All 2025-11-27 Page 3 Document title Data module code Issue date No. of pages Applicable to Pavement data - Techni- cal data BD500-A-J00-00-00-11AAA-030A-A 2025-01-28 89 50001-54999 Pavement data - Techni- cal data BD500-A-J00-00-00-11AAB-030A-A 2025-01-28 66 55001-59999 Principal dimensions, landing gear footprint - Technical data BD500-A-J06-10-32-00AAA-030A-A 2016-05-02 3 50001-54999, 55001-59999 Scaled drawings - Tech- nical data BD500-A-J00-00-00-21AAA-030A-A 2019-10-22 2 50001-54999 Scaled drawings - Tech- nical data BD500-A-J00-00-00-21AAB-030A-A 2019-10-22 2 55001-59999 Aircraft scaled down dimensions - Technical data BD500-A-J06-10-00-01AAA-030A-A 2019-10-21 3 50001-54999, 55001-59999 Emergency exits and evacuation - Technical data BD500-A-J15-41-00-01AAA-030A-A 2019-11-05 4 50001-54999, 55001-59999 Fire-fighting - Fire-fight- ing and rescue BD500-A-J15-41-00-02AAA-989A-A 2014-11-07 6 50001-54999, 55001-59999 Cargo compartment and fire protection system safety risk assessment - Technical data BD500-A-J26-00-00-00AAA-030A-A 2025-07-29 9 50001-54999, 55001-59999 BD500-3AB48-13800-00 Intentionally left blank Applicable to: All 2025-11-27 Page 4 BD500-3AB48-13800-00 Applicable to: All 2025-11-27 Page 1 Table of contents The listed documents are included in Issue 013, dated 2025-11-27, of this publication. Document title Data module code Issue date Applicable to Chapter 1: Scope A220-100 Aircraft Characteristics - Introduction BD500-A-J00-00-00-20AAA-018A-A 2023-09-15 50001-54999 A220-300 Aircraft Characteristics - Introduction BD500-A-J00-00-00-20AAB-018A-A 2023-09-15 55001-59999 Chapter 2: Aircraft description Aircraft characteristics - Technical data BD500-A-J00-00-00-00AAA-030A-A 2023-09-12 50001-54999, 55001-59999 Analysis of necessary equipment - Technical data BD500-A-J00-00-00-03AAA-030A-A 2019-08-12 50001-54999, 55001-59999 Necessary hangar space - Technical data BD500-A-J00-00-00-05AAA-030A-A 2016-04-14 50001-54999, 55001-59999 Equipment needs - Technical data BD500-A-J00-00-00-06AAA-030A-A 2019-08-13 50001-54999, 55001-59999 Utilities - Technical data BD500-A-J00-00-00-07AAA-030A-A 2019-08-13 50001-54999, 55001-59999 A220 Aircraft Characteristics - Introduction BD500-A-J00-00-00-09AAA-018A-A 2023-09-15 50001-54999, 55001-59999 Aircraft description - Technical data BD500-A-J00-00-00-12AAA-030A-A 2025-10-29 50001-54999 Aircraft description - Technical data BD500-A-J00-00-00-12AAB-030A-A 2024-11-19 55001-59999 Aircraft dimensions - Technical data BD500-A-J06-10-00-00AAA-030A-A 2023-11-01 50001-54999, 55001-59999 Nacelle and pylon stations - Technical data BD500-A-J06-20-03-01AAA-030A-A 2014-11-13 50001-54999, 55001-59999 Jacking for maintenance - Technical data BD500-A-J07-11-00-00AAA-030A-A 2025-09-10 50001-54999, 55001-59999 Slinging and hoisting - Function, data for plans and description BD500-A-J07-30-00-00AAA-000A-A 2019-10-21 50001-54999, 55001-59999 Aircraft grounding - General maintenance procedure BD500-A-J10-10-02-01AAA-913A-A 2017-08-08 50001-54999, 55001-59999 Forward cargo compartment volume, weight and maximum item dimensions - Technical data BD500-A-J14-20-00-01AAA-030A-A 2023-03-23 50001-54999, 55001-59999 Aft cargo compartment volume, weight and maximum item dimensions - Technical data BD500-A-J14-20-00-02AAA-030A-A 2023-03-23 50001-54999, 55001-59999 BD500-3AB48-13800-00 Applicable to: All 2025-11-27 Page 2 Document title Data module code Issue date Applicable to Aircraft touch and no-touch zones - Technical data BD500-A-J15-30-00-00AAA-030A-A 2019-10-21 50001-54999, 55001-59999 Aircraft antennas - Technical data BD500-A-J23-00-00-00AAA-030A-A 2024-08-23 50001-54999, 55001-59999 Chapter 3: Aircraft performance Aircraft performance - Technical data BD500-A-J00-00-00-13AAA-030A-A 2024-12-06 50001-54999 Aircraft performance - Technical data BD500-A-J00-00-00-13AAB-030A-A 2024-12-06 55001-59999 Chapter 4: Ground maneuvering Operating conditions - Technical data BD500-A-J00-00-00-17AAA-030A-A 2025-10-29 50001-54999 Operating conditions - Technical data BD500-A-J00-00-00-17AAB-030A-A 2020-07-08 55001-59999 Ground maneuvering - Technical data BD500-A-J00-00-00-19AAA-030A-A 2019-10-22 50001-54999 Ground maneuvering - Technical data BD500-A-J00-00-00-19AAB-030A-A 2019-10-22 55001-59999 Ground maneuvering, turning radii - Technical data BD500-A-J09-20-01-00AAA-030A-A 2018-02-05 50001-54999, 55001-59999 Ground maneuvering, visibility from flight compartment - Technical data BD500-A-J09-20-01-01AAA-030A-A 2016-01-13 50001-54999, 55001-59999 Wheel chocks - Handling procedure BD500-A-J10-16-01-01AAA-912A-A 2024-05-15 50001-54999, 55001-59999 Chapter 5: Terminal servicing Terminal servicing - Technical data BD500-A-J00-00-00-18AAA-030A-A 2022-09-30 50001-54999 Terminal servicing - Technical data BD500-A-J00-00-00-18AAB-030A-A 2022-09-30 55001-59999 Refueling - rate and time - Technical data BD500-A-J12-10-28-01AAB-030A-A 2017-01-16 55001-59999 Deicing/Anti-icing - Remove ice BD500-A-J12-31-00-00AAA-261A-A 2025-10-29 50001-54999, 55001-59999 Chapter 6: Operating conditions Crew safety precautions - dangerous areas - Technical data BD500-A-J15-30-10-00AAA-030A-A 2019-12-03 50001-54999 Chapter 7: Pavement data Pavement data - Technical data BD500-A-J00-00-00-11AAA-030A-A 2025-01-28 50001-54999 Pavement data - Technical data BD500-A-J00-00-00-11AAB-030A-A 2025-01-28 55001-59999 Principal dimensions, landing gear footprint - Technical data BD500-A-J06-10-32-00AAA-030A-A 2016-05-02 50001-54999, 55001-59999 Chapter 8: Scaled drawing Scaled drawings - Technical data BD500-A-J00-00-00-21AAA-030A-A 2019-10-22 50001-54999 Scaled drawings - Technical data BD500-A-J00-00-00-21AAB-030A-A 2019-10-22 55001-59999 Aircraft scaled down dimensions - Technical data BD500-A-J06-10-00-01AAA-030A-A 2019-10-21 50001-54999, 55001-59999 Chapter 10: Aircraft rescue and fire fighting BD500-3AB48-13800-00 Applicable to: All 2025-11-27 Page 3 Document title Data module code Issue date Applicable to Emergency exits and evacuation - Technical data BD500-A-J15-41-00-01AAA-030A-A 2019-11-05 50001-54999, 55001-59999 Fire-fighting - Fire-fighting and rescue BD500-A-J15-41-00-02AAA-989A-A 2014-11-07 50001-54999, 55001-59999 Chapter 11: Fire Protection Cargo compartment and fire protection system safety risk assessment - Technical data BD500-A-J26-00-00-00AAA-030A-A 2025-07-29 50001-54999, 55001-59999 BD500-3AB48-13800-00 Intentionally left blank Applicable to: All 2025-11-27 Page 4 BD500-3AB48-13800-00 Applicable to: All 2025-11-27 Page 1 Chapter 1: Scope BD500-3AB48-13800-00 Intentionally left blank Applicable to: All 2025-11-27 Page 2 BD500-3AB48-13800-00 See applicability on the first page of the DM BD500-A-J00-00-00-20AAA-018A-A BD500-A-J00-00-00-20AAA-018A-A 2023-09-15 Page 1 A220-100 Aircraft Characteristics - Introduction Applicability: 50001-54999 Table of contents Page A220-100 Aircraft Characteristics - Introduction....................................................................... 1 References................................................................................................................................ 1 Description................................................................................................................................. 1 1 Scope of the publication............................................................................................. 1 2 Publication organization.............................................................................................. 1 3 Dimensions and weight............................................................................................... 2 4 Correspondence.......................................................................................................... 2 5 Translation of publication............................................................................................ 2 6 Standard term definitions............................................................................................ 2 7 Acronyms.................................................................................................................... 3 List of tables Page 1 References.................................................................................................................. 1 References Table 1 References Data Module/Technical Publication Title None Description 1 Scope of the publication The A220-100 Aircraft Characteristics , prepared by Airbus, contains general data on the airport facilities, ramp, and runway areas necessary to operate the Airbus commercial aircraft model BD-500-1A10 (A220-100). Since operational practices vary among airlines, specific data should be coordinated with the user airlines prior to facility design. For additional information, please contact Airbus. The content of this publication will change as options and aircraft changes occur. Make sure that you refer to the latest release of this publication. If there is a difference between the data contained in this publication and that given by the local regulatory authority, the data from the local regulatory authority must be obeyed. 2 Publication organization This publication is divided into eight sections: - Aircraft description - Aircraft performance - Ground maneuvering BD500-3AB48-13800-00 See applicability on the first page of the DM BD500-A-J00-00-00-20AAA-018A-A BD500-A-J00-00-00-20AAA-018A-A 2023-09-15 Page 2 - Terminal servicing - Operating conditions - Pavement data - Derivative aircraft - Scaled drawings 3 Dimensions and weight Linear dimensions given in this publication are in inches. The metric equivalents are given in parentheses ( ). Weight measures is given in pound (lb) with the metric equivalent in parentheses ( ). 4 Correspondence The publications change request form is available online and is used to request technical changes to rectify any errors, omissions, or procedural inconsistencies (if applicable), etc. using the Airbus A220 Interactive Electronic Technical Publication (IETP) viewer. 5 Translation of publication If all or part of this publication is translated, the official version is the English language version by Airbus. 6 Standard term definitions Maximum design Taxi Weight (MTW) Maximum weight at which an aircraft can move safely on the ground. This in- cludes the fuel for these displacements and the takeoff run. Maximum de- sign Landing Weight (MLW) Maximum weight for landing as limited by aircraft strength and airworthiness requirement. Maximum de- sign Take- Off Weight (MTOW) Maximum weight for take off as limited by aircraft strength and airworthiness requirements. This includes weight of fuel for taxi and run-up. Operational Weight Empty (OWE) Weight of structure, power plant, furnishings, systems, unusable fuel and other items of equipment that are a necessary part of a particular aircraft configuration. Also included are certain standard items, personnel, equip- ment and supplies necessary for full operations, but does not include usable fuel or payload. Maximum design Zero Fuel Weight (MZFW) Maximum weight permitted before usable fuel and other usable agents must be loaded in defined sections of the aircraft, as limited by strength and air- worthiness requirements. Maximum car- go volume The maximum space available for cargo. BD500-3AB48-13800-00 See applicability on the first page of the DM BD500-A-J00-00-00-20AAA-018A-A BD500-A-J00-00-00-20AAA-018A-A End of data module 2023-09-15 Page 3 Maximum seating capac- ity The maximum number of passengers permitted based on certification re- quirements. Usable fuel Fuel available for aircraft propulsion and the Auxiliary Power Unit (APU). 7 Acronyms The first time an acronym is used it will be defined, and all subsequent uses will be in blue. When you mouse over the acronym the definition will appear. Acronyms are not plural in this publication. BD500-3AB48-13800-00 Intentionally left blank See applicability on the first page of the DM BD500-A-J00-00-00-20AAA-018A-A BD500-A-J00-00-00-20AAA-018A-A 2023-09-15 Page 4 BD500-3AB48-13800-00 See applicability on the first page of the DM BD500-A-J00-00-00-20AAB-018A-A BD500-A-J00-00-00-20AAB-018A-A 2023-09-15 Page 1 A220-300 Aircraft Characteristics - Introduction Applicability: 55001-59999 Table of contents Page A220-300 Aircraft Characteristics - Introduction....................................................................... 1 References................................................................................................................................ 1 Description................................................................................................................................. 1 1 Scope of the publication............................................................................................. 1 2 Publication organization.............................................................................................. 1 3 Dimensions and weight............................................................................................... 2 4 Correspondence.......................................................................................................... 2 5 Translation of publication............................................................................................ 2 6 Standard term definitions............................................................................................ 2 7 Acronyms.................................................................................................................... 3 List of tables Page 1 References.................................................................................................................. 1 References Table 1 References Data Module/Technical Publication Title None Description 1 Scope of the publication The A220-300 Aircraft Characteristics prepared by Airbus, contains general data on the airport facilities, ramp, and runway areas necessary to operate the Airbus BD-500-1A11 (A220-300). Since operational practices vary among airlines, specific data should be coordinated with the user airlines prior to facility design. For additional information, please contact Airbus. The content of this publication will change as options and aircraft changes occur. Make sure that you refer to the latest release of this publication. If there is a difference between the data contained in this publication and that given by the local regulatory authority, the data from the local regulatory authority must be obeyed. 2 Publication organization This publication is divided into eight sections: - Aircraft description - Aircraft performance - Ground maneuvering - Terminal servicing BD500-3AB48-13800-00 See applicability on the first page of the DM BD500-A-J00-00-00-20AAB-018A-A BD500-A-J00-00-00-20AAB-018A-A 2023-09-15 Page 2 - Operating conditions - Pavement data - Derivative aircraft - Scaled drawings 3 Dimensions and weight Linear dimensions given in this publication are in inches. The metric equivalents are given in parentheses ( ). Weight measures is given in pound (lb) with the metric equivalent in parentheses ( ). 4 Correspondence The publications change request form is available online and is used to request technical changes to rectify any errors, omissions, or procedural inconsistencies (if applicable), etc. using the Airbus A220 Interactive Electronic Technical Publication (IETP) viewer. 5 Translation of publication If all or part of this publication is translated, the official version is the English language version by Airbus. 6 Standard term definitions Maximum design Taxi Weight (MTW) Maximum weight at which an aircraft can move safely on the ground. This in- cludes the fuel for these displacements and the takeoff run. Maximum de- sign Landing Weight (MLW) Maximum weight for landing as limited by aircraft strength and airworthiness requirement. Maximum de- sign Take- Off Weight (MTOW) Maximum weight for take off as limited by aircraft strength and airworthiness requirements. This includes weight of fuel for taxi and run-up. Operational Weight Empty (OWE) Weight of structure, power plant, furnishings, systems, unusable fuel and other items of equipment that are a necessary part of a particular aircraft configuration. Also included are certain standard items, personnel, equip- ment and supplies necessary for full operations, but does not include usable fuel or payload. Maximum design Zero Fuel Weight (MZFW) Maximum weight permitted before usable fuel and other usable agents must be loaded in defined sections of the aircraft, as limited by strength and air- worthiness requirements. Maximum car- go volume The maximum space available for cargo. Maximum seating capac- ity The maximum number of passengers permitted based on certification re- quirements. BD500-3AB48-13800-00 See applicability on the first page of the DM BD500-A-J00-00-00-20AAB-018A-A BD500-A-J00-00-00-20AAB-018A-A End of data module 2023-09-15 Page 3 Usable fuel Fuel available for aircraft propulsion and the Auxiliary Power Unit (APU). 7 Acronyms The first time an acronym is used it will be defined, and all subsequent uses will be in blue. When you mouse over the acronym the definition will appear. Acronyms are not plural in this publication. BD500-3AB48-13800-00 Intentionally left blank See applicability on the first page of the DM BD500-A-J00-00-00-20AAB-018A-A BD500-A-J00-00-00-20AAB-018A-A 2023-09-15 Page 4 BD500-3AB48-13800-00 Applicable to: All 2025-11-27 Page 1 Chapter 2: Aircraft description BD500-3AB48-13800-00 Intentionally left blank Applicable to: All 2025-11-27 Page 2 BD500-3AB48-13800-00 See applicability on the first page of the DM BD500-A-J00-00-00-00AAA-030A-A BD500-A-J00-00-00-00AAA-030A-A 2023-09-12 Page 1 Aircraft characteristics - Technical data Applicability: 50001-54999, 55001-59999 Table of contents Page Aircraft characteristics - Technical data.................................................................................... 1 References................................................................................................................................ 1 Description................................................................................................................................. 1 1 Introduction.................................................................................................................. 1 2 Aircraft characteristics................................................................................................. 1 3 System fluid capacities............................................................................................... 2 4 Service fluid capacities............................................................................................... 3 List of tables Page 1 References.................................................................................................................. 1 2 Aircraft characteristics................................................................................................. 1 3 System fluid capacities............................................................................................... 2 4 Service fluid capacities............................................................................................... 3 References Table 1 References Data Module/Technical Publication Title None Description 1 Introduction This data module contains general data about the BD-500-1A10 (A220-100) and BD-500-1A11 (A220-300) aircraft characteristics. The structural weight limits, such as maximum ramp weight, and zero fuel weight are dependent on configuration. Refer to each aircraft’s specified Weight and Balance Manual (WBM BD500-A-J00-00-00-00AAA-030A-A) and weight and balance report for structural limits and other weight information. Refer to Table 2 for the aircraft characteristics. Refer to Table 3 for the system fluid capacities. Refer to Table 4 for the service fluid capacities. 2 Aircraft characteristics Table 2 Aircraft characteristics Description BD-500-1A10 (A220-100) BD-500-1A11 (A220-300) Engines QTY: 2 Pure Power™ PW1519G QTY: 2 Pure Power™ PW1521G Mode Passenger Passenger BD500-3AB48-13800-00 See applicability on the first page of the DM BD500-A-J00-00-00-00AAA-030A-A BD500-A-J00-00-00-00AAA-030A-A 2023-09-12 Page 2 Description BD-500-1A10 (A220-100) BD-500-1A11 (A220-300) Standard seating capacity 120 140 Maximum Ramp Weight (MRW) 135,000 lb (61 235 kg) 150,000 lb (68 039 kg) Maximum Take-Off Weight (MTOW) 134,000 lb (60 781 kg) 149,000 lb (67 585 kg) Maximum Landing Weight (MLW) 115,500 lb (52 390 kg) 129,500 lb (58 740 kg) Operating Weight Empty (OWE) 77,650 lb (35 221 kg) 81,750 lb (37 081 kg) Maximum Zero Fuel Weight (MZFW) 111,000 lb (50 349 kg) 123,000 lb (55 792 kg) Maximum fuel tank capacity 5,790 USG (21 918 L) 5,790 USG (21 918 L) Unusable fuel 240 lb (109 kg) 240 lb (109 kg) Maximum wet cargo volume - Aft cargo compartment 474 cu. ft (13,4 cu. m) 627 cu. ft (17,75 cu. m) Maximum wet cargo volume - Fwd cargo compartment 349 cu. ft (9,88 cu. m) 473 cu. ft (13,39 cu. m) Maximum cargo volume - Over- head bins 280 cu. ft (7,93 cu. m) 332 cu. ft (9,40 cu. m) 3 System fluid capacities Table 3 System fluid capacities Description Volume Weight Engine fluids calculated with 7.7 lb/US gal (0,920 kg/L) Engines oil tank at 60 °F 12.9 US gal (49,0 L) 99 lb (44,9 kg) Lines and internal engine oil 3.3 US gal (12,6 L) 26 lb (11,8 kg) Total 16.2 US gal (61,6 L) 125 lb (56,7 kg) APU fluids calculated with 7.7 lb/US gal (0,920 kg/L) APU 3.3 US gal (12,3 L) 25 lb (11,3 kg) Hydraulic fluids at 77°F (25 °C) low density 8.43 lb/US gal (1,01 kg/L) System 1 reservoir 4.98 US gal (18.85 L) 41.98 lb (19.04 kg) System 2 reservoir 4.33 US gal (16.39 L) 36.50 lb (16.55 kg) System 3 reservoir 3.46 US gal (13.10 L) 29.17 lb (13.23 kg) Total 12.77 US gal (48.34 L) 107.65 lb (48.82 kg) BD500-3AB48-13800-00 See applicability on the first page of the DM BD500-A-J00-00-00-00AAA-030A-A BD500-A-J00-00-00-00AAA-030A-A End of data module 2023-09-12 Page 3 Description Volume Weight Hydraulic fluids at 77°F (25 °C) high density 8.86 lb/US gal (1,06 kg/L) System 1 reservoir 4.98 US gal (18.85 L) 44.12 lb (20.01 kg) System 2 reservoir 4.33 US gal (16.39 L) 38.36 lb (17.40 kg) System 3 reservoir 3.46 US gal (13.10 L) 30.65 lb (13.90 kg) Total 12.77 US gal (48.34 L) 113.13 lb (51.31 kg) 4 Service fluid capacities Table 4 Service fluid capacities Description Volume Weight Potable water at 60 °F (15,5 °C) Galley/Lavatory tank 42.0 US gal (159,0 L) 350.5 lb (159.0 kg) Chemical toilet fluid at 60 °F (15,5 °C) Waste tank 42.0 US gal (159,1 L) 350 lb (158,8 kg) BD500-3AB48-13800-00 Intentionally left blank See applicability on the first page of the DM BD500-A-J00-00-00-00AAA-030A-A BD500-A-J00-00-00-00AAA-030A-A 2023-09-12 Page 4 BD500-3AB48-13800-00 See applicability on the first page of the DM BD500-A-J00-00-00-03AAA-030A-A BD500-A-J00-00-00-03AAA-030A-A 2019-08-12 Page 1 Analysis of necessary equipment - Technical data Applicability: 50001-54999, 55001-59999 Table of contents Page Analysis of necessary equipment - Technical data................................................................... 1 References................................................................................................................................ 1 Description................................................................................................................................. 1 1 General........................................................................................................................ 1 1.1 Hangar areas for maintenance................................................................................... 2 1.2 Aircraft apron.............................................................................................................. 2 1.3 Aircraft maintenance support shops........................................................................... 2 1.4 Component overhaul shops........................................................................................ 3 1.5 Stock rooms................................................................................................................ 3 1.6 Administrative offices and auxiliary facilities............................................................... 4 1.7 Utilities......................................................................................................................... 4 List of tables Page 1 References.................................................................................................................. 1 References Table 1 References Data Module/Technical Publication Title None Description 1 General This section identifies and gives an analysis of the equipment necessary to do maintenance on the A220 aircraft. Refer to the lists that follow for the equipment and facilities that you must have for aircraft main- tenance and servicing. These lists show the different functions that a maintenance or service center (or an approved external subcontractor) must provide to support the operator’s aircraft. Usually, it is best for a maintenance facility to have all the shops and equipment necessary on- site to do maintenance. But, to try to lower repair costs and decrease turnaround times, it can sometimes be more cost-effective to use the facilities and services of approved external ven- dors as an alternative to your own service or repair facilities. If an operator decides to use an external service or repair facility, they must first examine how much of the aircraft maintenance to keep on-site and how much to contract out to an external services facility. The operator should first identify what equipment, components, or parts are necessary to do repairs and/or an overhaul at their own maintenance facility. If some of the nec- essary equipment is not available, or it is not cost-effective to purchase/rent, then the operator should probably use an external (off-site) maintenance or services facility to do these mainte- nance functions. BD500-3AB48-13800-00 See applicability on the first page of the DM BD500-A-J00-00-00-03AAA-030A-A BD500-A-J00-00-00-03AAA-030A-A 2019-08-12 Page 2 During the initial planning stage, it is important that the operator look at the type of the mainte- nance to be done at the operator’s facilities and the overhaul equipment that is necessary to do the job. After a check of the work flow processes, the operator must calculate the space alloca- tion necessary and what equipment and supplies for the shop facilities must be purchased, in order to calculate an approximate cost estimate. As the planning stage continues, more accu- rate costs will become known which will give a more accurate estimate of the total costs neces- sary in the production of the operator’s maintenance facility. The typical maintenance facility has the areas, shops and rooms that follow, as applicable: - Hangar areas for maintenance - Aircraft apron - Aircraft maintenance support shops - Component overhaul shops - Stock rooms - Administrative offices and auxiliary facilities - Utilities. 1.1 Hangar areas for maintenance These are the areas that should be provided: - Hangar - Work stands and docks - Cranes, stands and docks - Service pits for electricity, air and fuel 1.2 Aircraft apron These are the areas that should be provided: - Aircraft maintenance aprons - Aircraft parking aprons - Taxiways - Wash rack - Blast fences and noise suppressors 1.3 Aircraft maintenance support shops These are the areas that should be provided: - Wheels, brakes and tires - Power plant and Auxiliary Power Unit (APU) (quick engine change) - Sheet metal/composites - Avionics - Interiors and seats - Aircraft cleaners BD500-3AB48-13800-00 See applicability on the first page of the DM BD500-A-J00-00-00-03AAA-030A-A BD500-A-J00-00-00-03AAA-030A-A 2019-08-12 Page 3 1.4 Component overhaul shops These are the areas that should be provided: - Sheet metal - Composite structures - Parts cleaning - Painting - Plating - Welding - Heat treating - Machining - Engine / power plant • Module replacement • Module overhaul • Test cell - Auxiliary power unit - Hydraulic - Pneumatic - Mechanical accessories - Fuel components - Battery - Electrical - Landing gear - Wheels, brakes and tires - Avionics • Communications • Navigation - Instruments, electrical - Instruments, mechanical - Bottled gas (O2, N2, CO2) - Seats and interiors - Galley refrigeration - Non-destructive testing and laboratories 1.5 Stock rooms These are the areas that should be provided: - Aircraft spares - Consumable materials - Combustible materials BD500-3AB48-13800-00 See applicability on the first page of the DM BD500-A-J00-00-00-03AAA-030A-A BD500-A-J00-00-00-03AAA-030A-A End of data module 2019-08-12 Page 4 - Tool cribs - Receiving and shipping - Quarantine area (for faulty or rejected items) 1.6 Administrative offices and auxiliary facilities These are the areas that should be provided: - Maintenance administration office - Maintenance support office - Quality control and reliability - Engineering - Manufacturer’s representatives - Computer services - Medical station - Security - Cafeteria - Toilets, washrooms, and lockers - Building maintenance 1.7 Utilities These are the areas that should be provided: - Electricity (main and emergency) - Water - Sewage and wastewater - Telephone - Heating, ventilation, and air conditioning - Compressed air BD500-3AB48-13800-00 See applicability on the first page of the DM BD500-A-J00-00-00-05AAA-030A-A BD500-A-J00-00-00-05AAA-030A-A 2016-04-14 Page 1 Necessary hangar space - Technical data Applicability: 50001-54999, 55001-59999 Table of contents Page Necessary hangar space - Technical data............................................................................... 1 References................................................................................................................................ 1 Description................................................................................................................................. 1 1 General........................................................................................................................ 1 List of tables Page 1 References.................................................................................................................. 1 2 Hangar arrangement legend for Ground Support Equipment (GSE) and tools.......... 1 List of figures Page 1 Hangar arrangement................................................................................................... 4 References Table 1 References Data Module/Technical Publication Title BD500-A-J06-10-00-00AAA-030A-A Aircraft dimensions - Technical data Description 1 General The first facility an operator may want to consider is the maintenance hangar. The number of hangar positions is dependant on the number of aircraft types, the number of aircraft per type, aircraft utilization, maintenance check frequency (scheduled, unscheduled, equalized), the elapsed time required to perform maintenance checks, and the number of working hours avail- able per day. Hangar proposed arrangement is provided in Fig. 1 to assist in determining location, size, and clearance requirements for Ground Support Equipment (GSE) , tools and workstands, refer to Table 2 for a legend. Aircraft parking space requirements can also be determined from Fig. 1 and to BD500-A-J06-10-00-00AAA-030A-A for aircraft dimensions. Table 2 Hangar arrangement legend for Ground Support Equipment (GSE) and tools. Reference letter Description A Desks and reference tables B Tool boxes C Eye wash station D Spill kit BD500-3AB48-13800-00 See applicability on the first page of the DM BD500-A-J00-00-00-05AAA-030A-A BD500-A-J00-00-00-05AAA-030A-A 2016-04-14 Page 2 Reference letter Description E Main Landing Gear (MLG) ladder station F Avionic station G Garbage and recycling station H Ladder storage/parking J Mule K Ladders parking L Oxygen/nitogen M Racks and shelves N Carts and charging stations P Sanding room Q Used oil tank R Oil warehouse S Store office T Rack and shelves U Kitchen V Office W Washrooms X Sprinkler room Y Nacelles parking Z Electrical room AA Conference room AB Avionic lab AC Service desk AD Lockers AE Printing room AF Ground Power Unit (GPU) AG Hydraulic cart AH Latchways vaccuum anchor BD500-3AB48-13800-00 See applicability on the first page of the DM BD500-A-J00-00-00-05AAA-030A-A BD500-A-J00-00-00-05AAA-030A-A 2016-04-14 Page 3 Reference letter Description AJ Supports and jacks AK Coffee area AL Cleaning room AM Air conditioning room AN Servicing carts AP Drop area for parts AQ Oxygen and nitrogen BD500-3AB48-13800-00 See applicability on the first page of the DM BD500-A-J00-00-00-05AAA-030A-A BD500-A-J00-00-00-05AAA-030A-A End of data module 2016-04-14 Page 4 B C A G A K J K A B D C G Y K B AQ AP AN B G A D C K AF AF AG AH E F AJ P Q R AC T AK AD AE AB U W V W AA Z X AJ AJ B B AL ICN-BD500-A-J000000-A-3AB48-29850-A-001-01 Figure 1 Hangar arrangement