1、_SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising theref
2、rom, is the sole responsibility of the user.” SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2010 SAE International All rights reserved. No part of this publication ma
3、y be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: 724-776-4970 (outside USA)
4、Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AIR5005AAEROSPACEINFORMATIONREPORTAIR5005A Issued 2000-03 Revised 2010-05Superseding AIR5005 (R) A
5、erospace - Commercial Aircraft Hydraulic SystemsRATIONALEAIR5005 has been updated to Revision A for the following reasons: a. Details of additional commercial aircraft hydraulic systems have been provided b. Some business jet aircraft have been added c. Update of references called up in the document
6、 TABLE OF CONTENTS 1. SCOPE . 4 2. REFERENCES . 52.1 Applicable Documents . 52.2 Definitions 7 3. WIDE BODY JET AIRLINERS . 83.1 Airbus A300B/A300-600 103.2 Airbus A310-200/300 . 153.3 Airbus A330-200/300/Airbus A340-200/300 193.4 Airbus A340-500/600 . 253.5 Airbus A380-800 293.6 Boeing 747-100/200/
7、300 343.7 Boeing 747-400 383.8 Boeing 767-200/300/400 423.9 Boeing 777-200/300. 463.10 Boeing MD-11 503.11 Lockheed L-1011-1/100/200/500 . 543.12 McDonnell Douglas DC-10-10/30/40 . 58 4. NARROW BODY JET AIRLINERS 624.1 Aerospatiale/BAC Concorde 644.2 Airbus A318/A319/A320/A321 . 694.3 BAC 111-500 74
8、4.4 BAE Systems 146-100/200/300/Avro RJ70/85/100/115 784.5 Boeing 707-120/320/420 824.6 Boeing 717-200 864.7 Boeing 727-100/200. 904.8 Boeing 737-100/200. 944.9 Boeing 737-300/400/500 984.10 Boeing 737-600/700/800/900 . 1024.11 Boeing 757-200/300. 1064.12 Boeing MD-81/82/83/87/88 110Copyright SAE In
9、ternational Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AIR5005A Page 2 of 2434.13 Boeing MD-90-30 . 1144.14 Bombardier CRJ 100/200 1184.15 Bombardier CRJ 700/900 1224.16 Embraer ERJ-135/140/145 1264.17 Embraer ERJ-170/
10、175/190/195 . 1294.18 McDonnell Douglas DC-8-60/70 1374.19 McDonnell Douglas DC-9-10/20/30/40/50 . 141 5. TURBOPROP/COMMUTER AIRCRAFT . 1455.1 ATR 42/ATR 72 1475.2 BAE Systems ATP/Jetstream 61 . 1505.3 BAE Systems Jetstream 31/32 1535.4 BAE Systems Jetstream 41 . 1565.5 Beechcraft 1900C/D . 1595.6 B
11、ombardier DHC-8 Dash 8 Q100/200/300 1615.7 Bombardier DHC-8 Dash 8 Q400 1665.8 De Havilland DHC-7 Dash 7 1705.9 Dornier 328 1735.10 EADS CASA CN-235 . 1785.11 Embraer EMB-110 Bandeirante . 1815.12 Embraer EMB-120 Brasilia 1845.13 Fairchild Metro . 1875.14 Fokker 50 . 1905.15 Lockheed L.188 Electra .
12、 1935.16 SAAB 340 . 1965.17 SAAB 2000 . 199 5.18 Short 360 203 6. BUSINESS JET AIRCRAFT 2066.1 Bombardier Challenger 300 . 2076.2 Bombardier Challenger 604 . 2116.3 Bombardier Global Express/500 2156.4 Bombardier Learjet 40/45 2196.5 Bombardier Learjet 60 . 2226.6 Cessna Citation Mustang Model 510 .
13、 2256.7 Cessna CitationJet (CJ) Series Model 525 2286.8 Cessna Citation Bravo, Model 550 2316.9 Cessna Citation Ultra Encore+, Model 560 . 2346.10 Cessna Citation XLS+ 2376.11 Gulfstream IV . 240 7. NOTES . 2437.1 Revision Indicator . 243TABLE 1 WIDE BODY AIRCRAFT HYDRAULIC SYSTEM DATA 8TABLE 2 NARR
14、OW BODY JET AIRCRAFT HYDRAULIC SYSTEM DATA . 62TABLE 3 TURBOPROP/COMMUTER AIRCRAFT HYDRAULIC SYSTEM DATA . 145TABLE 4 BUSINESS JET AIRCRAFT HYDRAULIC SYSTEM DATA . 206FIGURE 3.1.1 AIRBUS A300B HYDRAULIC SYSTEM SCHEMATIC . 13FIGURE 3.1.2 AIRBUS A300-600 HYDRAULIC SYSTEM SCHEMATIC 14FIGURE 3.2 AIRBUS
15、A310-200/300 HYDRAULIC SYSTEM SCHEMATIC . 18FIGURE 3.3.1 AIRBUS A330-200/300 HYDRAULIC SYSTEM SCHEMATIC . 23FIGURE 3.3.2 AIRBUS A340-200/300 HYDRAULIC SYSTEM SCHEMATIC . 24FIGURE 3.4 AIRBUS A340-500/600 HYDRAULIC SYSTEM SCHEMATIC . 28FIGURE 3.5 AIRBUS A380-800 HYDRAULIC SYSTEM SCHEMATIC 33FIGURE 3.6
16、 BOEING 747-100/200/300 HYDRAULIC SYSTEM SCHEMATIC 37FIGURE 3.7 BOEING 747-400 HYDRAULIC SYSTEM SCHEMATIC 41FIGURE 3.8 BOEING 767-200/300/400 HYDRAULIC SYSTEM SCHEMATIC 45FIGURE 3.9 BOEING 777-200/300 HYDRAULIC SYSTEM SCHEMATIC . 49Copyright SAE International Provided by IHS under license with SAENo
17、t for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AIR5005A Page 3 of 243FIGURE 3.10 BOEING MD-11 HYDRAULIC SYSTEM SCHEMATIC 53FIGURE 3.11 LOCKHEED L.1011-1/100/200/500 HYDRAULIC SYSTEM SCHEMATIC 57FIGURE 3.12 MCDONNELL DOUGLAS DC-10-10/30/40 HYDRAULIC SYSTEM SCHEMA
18、TIC 61FIGURE 4.1 AEROSPATIALE/BAC CONCORDE HYDRAULIC SYSTEM SCHEMATIC 68FIGURE 4.2 AIRBUS A318/A319/A320/A321 HYDRAULIC SYSTEM SCHEMATIC . 73FIGURE 4.3 BAC 111-500 HYDRAULIC SYSTEM SCHEMATIC 77FIGURE 4.4 BAE SYSTEMS 146-100/200/300/AVRO RJ70/85/100/115 HYDRAULIC SYSTEM SCHEMATIC 81FIGURE 4.5 BOEING
19、707-120/320/420 HYDRAULIC SYSTEM SCHEMATIC 85FIGURE 4.6 BOEING 717-200 HYDRAULIC SYSTEM SCHEMATIC 89FIGURE 4.7 BOEING 727-100/200 HYDRAULIC SYSTEM SCHEMATIC . 93FIGURE 4.8 BOEING 737-100/200 HYDRAULIC SYSTEM SCHEMATIC . 97FIGURE 4.9 BOEING 737-300/400/500 HYDRAULIC SYSTEM SCHEMATIC 101FIGURE 4.10 BO
20、EING 737-600/700/800/900 HYDRAULIC SYSTEM SCHEMATIC 105FIGURE 4.11 BOEING 757-200/300 HYDRAULIC SYSTEM SCHEMATIC . 109FIGURE 4.12 BOEING MD-81/82/83/87/88 HYDRAULIC SYSTEM SCHEMATIC 113FIGURE 4.13 BOEING MD-90-30 HYDRAULIC SYSTEM SCHEMATIC . 117FIGURE 4.14 BOMBARDIER CRJ 100/200 HYDRAULIC SYSTEM SCH
21、EMATIC 121FIGURE 4.15 BOMBARDIER REGIONAL JET 700/900 HYDRAULIC SYSTEM SCHEMATIC 125FIGURE 4.16 EMBRAER ERJ-135/140/145 HYDRAULIC SYSTEM SCHEMATIC . 128FIGURE 4.17 EMBRAER ERJ-170/175/190/195 HYDRAULIC SYSTEM SCHEMATIC 132FIGURE 4.18 FOKKER 70/100 HYDRAULIC SYSTEM SCHEMATIC . 136FIGURE 4.19 MCDONNEL
22、L DOUGLAS DC-8-60/70 HYDRAULIC SYSTEM SCHEMATIC . 140FIGURE 4.20 MCDONNELL DOUGLAS DC-9-10/20/30/40/50 HYDRAULIC SYSTEM SCHEMATIC 144FIGURE 5.1 ATR 42/ ATR 72 HYDRAULIC SYSTEM SCHEMATIC 149FIGURE 5.2 BAE SYSTEMS ATP/JETSTREAM 61 HYDRAULIC SYSTEM SCHEMATIC . 152FIGURE 5.3 BAE SYSTEMS JETSTREAM 31/32
23、HYDRAULIC SYSTEM SCHEMATIC 155FIGURE 5.4 BAE SYSTEMS JETSTREAM 41 HYDRAULIC SYSTEM . 158FIGURE 5.5 BEECHCRAFT 1900C/D HYDRAULIC SYSTEM SCHEMATIC 160FIGURE 5.6.1 BOMBARDIER DHC-8 DASH 8 Q100/200/300 - CURRENT PRODUCTIONSTANDARD - HYDRAULIC SYSTEM SCHEMATIC 164FIGURE 5.6.2 BOMBARDIER DHC-8 DASH 8 Q100
24、/200/300 - IN-SERVICE RETROFITSTANDARD - HYDRAULIC SYSTEM SCHEMATIC 165FIGURE 5.7 BOMBARDIER DHC-8 DASH 8 Q400 HYDRAULIC SYSTEM SCHEMATIC 169FIGURE 5.8 DE HAVILLAND DHC-7 DASH 7 HYDRAULIC SYSTEM SCHEMATIC 172FIGURE 5.9.1 DORNIER 328 - WITHOUT GROUND SPOILERS - HYDRAULIC SYSTEM SCHEMATIC 176FIGURE 5.
25、9.2 DORNIER 328 - WITH GROUND SPOILERS - HYDRAULIC SYSTEM SCHEMATIC . 177FIGURE 5.10 EADS CASA CN-235 HYDRAULIC SYSTEM SCHEMATIC 180FIGURE 5.11 EMBRAER EMB-110 BANDEIRANTE HYDRAULIC SYSTEM SCHEMATIC . 183FIGURE 5.12 EMBRAER EMB-120 BRASILIA HYDRAULIC SYSTEM SCHEMATIC. 186FIGURE 5.13 FAIRCHILD METRO
26、HYDRAULIC SYSTEM SCHEMATIC . 189FIGURE 5.14 FOKKER 50 HYDRAULIC SYSTEM SCHEMATIC 192FIGURE 5.15 LOCKHEED L.188 ELECTRA HYDRAULIC SYSTEM SCHEMATIC 195FIGURE 5.16 SAAB 340 HYDRAULIC SYSTEM SCHEMATIC . 198FIGURE 5.17 SAAB 2000 HYDRAULIC SYSTEM SCHEMATIC . 202FIGURE 5.18 SHORT 360 HYDRAULIC SYSTEM SCHEM
27、ATIC 205FIGURE 6.1 BOMBARDIER CHALLENGER 300 HYDRAULIC SYSTEM SCHEMATIC . 210FIGURE 6.2 BOMBARDIER CHALLENGER 604 HYDRAULIC SYSTEM SCHEMATIC . 214FIGURE 6.3 BOMBARDIER GLOBAL EXPRESS/500 HYDRAULIC SYSTEM SCHEMATIC . 218FIGURE 6.4 BOMBARDIER LEARJET 40/45 HYDRAULIC SYSTEM SCHEMATIC. 221FIGURE 6.5 BOM
28、BARDIER LEARJET 60 HYDRAULIC SYSTEM SCHEMATIC 224FIGURE 6.6 CESSNA CITATION MUSTANG MODEL 510 HYDRAULIC SYSTEM SCHEMATIC . 227FIGURE 6.7 CESSNA CITATIONJET SERIES HYDRAULIC SYSTEM SCHEMATIC . 230FIGURE 6.8 CESSNA CITATION BRAVO HYDRAULIC SYSTEM SCHEMATIC 233FIGURE 6.9 CESSNA CITATION ULTRA ENCORE+ H
29、YDRAULIC SYSTEM SCHEMATIC 236FIGURE 6.10 CESSNA CITATION XLS+ HYDRAULIC SYSTEM SCHEMATIC . 239FIGURE 6.11 GULFSTREAM IV HYDRAULIC SYSTEM SCHEMATIC . 242 Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-
30、,-SAE AIR5005A Page 4 of 2431. SCOPE This SAE Aerospace Information Report (AIR) has been compiled to provide information on hydraulic systems fitted to commercial aircraft. Data has been provided for following aircraft types: a. Wide body jet airliners b. Narrow body jet airliners c. Turboprop/comm
31、uter aircraft d. Business jet aircraft The airliners that have been included in this document are generally in operational service with either airlines or cargo operators. Information on aircraft that have been retired from in-service use has been included for reference purposes. No information is p
32、resented for aircraft that are currently being developed. The following information is provided for each aircraft x Design requirements: Governing airworthiness regulations x System pressure: Fluid power system operating pressure x Hydraulic fluid: Type of fluid the hydraulic system uses x Number of
33、 hydraulic systems: Number and identification of independent hydraulic systems x System temperature: Minimum and maximum design operating temperatures x Main hydraulic pump data: Flow, pressure, displacement x Auxiliary pump data: System auxiliary pump or back-up data x Hydraulic motor data: System
34、hydraulic motor requirements x Accumulator data: Usage, volume and precharge requirements x Reservoir data: Type, volume and pressure x Relief valve data: Usage, crack and reseat pressures, rated flow x Filtration data: Usage, filtration rating x Tubing data: Materials, sizes, wall thicknesses x Fit
35、ting data: Type, size range, material x Schematic diagram: System architecture, services supplied Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AIR5005A Page 5 of 243NOTES1. For some aircraft,
36、the data is incomplete. This is due to difficulties in obtaining the data (particularly for the older aircraft presented in this report). 2. For some aircraft, the pumps may not be those as stated in this document. This is because when they are supplied by more than one vendor for a specific aircraf
37、t application, the pumps displacement and running speed may differ. 3. Electric motor pumps are fixed frequency type unless otherwise stated. 4. The schematic diagrams for each aircraft have been simplified for clarity and ease of understanding. For example:- The return side of each system has not b
38、een shown - Specific features such as internal leak measuring systems are not shown - Single accumulators are shown at locations where multiple accumulators are used However, the complete power generation system and elements of the supply system for each aircraft is shown using symbols in accordance
39、 with AS1290. 5. The filtration ratings that are presented in this report are the absolute rather than nominal ratings. However, it should be noted that there is no consistent definition of the absolute rating for the filters for the aircraft hydraulic systems that are described in this report. 2. R
40、EFERENCES 2.1 Applicable Documents The following publications form a part of this standard to the extent specified herein. The latest issue of the SAE documents shall apply. The applicable issue of the other documents shall be the issue in effect at the date of the purchase order. In the event of co
41、nflict between the text of this document and the references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained. 2.1.1 SAE Publications Available from SAE International,
42、400 Commonwealth Drive, Warrendale, PA 15096-0001. Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org.ARP4386 Terminology and Definition for Aerospace Fluid Power, Actuation and Control Technologies AS1241 Fire Resistant Phosphate Ester Hydraulic Fluid for Aircraft
43、AS1290 Graphic Symbols for Aircraft Hydraulic and Pneumatic Systems AMS4071 Aluminum Alloy, Drawn, Round, Seamless Hydraulic Tubing 2.5Mg - 0.25Cr (5052-0) Annealed AMS4083 Aluminum Alloy Tubing, Hydraulic, Seamless, Drawn, Round, 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-T6), Solution and Precipitatio
44、n Heat Treated AMS4928 Titanium Alloy Bars, Wire, Forgings, Rings, and Drawn Shapes 6Al - 4V Annealed AMS4944 Titanium Alloy Tubing, Seamless, Hydraulic, 3.0Al-2.5V, Cold Worked, Stress Relieved Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networ
45、king permitted without license from IHS-,-,-SAE AIR5005A Page 6 of 243AMS4945 Titanium Alloy Tubing, Seamless, Hydraulic 3Al-2.5V, Controlled Contractile Strain Ratio Cold Worked, Stress Relieved AMS5561 Steel, Corrosion and Heat-Resistant, Welded and Drawn or Seamless and Drawn Tubing 9.0Mn - 20Cr
46、-6.5Ni - 0.28N High-Pressure Hydraulic AMS5566 Steel, Corrosion Resistant, Seamless or Welded Hydraulic Tubing 19Cr - 10 Ni (SAE 30304) High Pressure, Cold Drawn AMS-WW-T-700/4 Tube, Aluminum Alloy, Drawn, Seamless, 5052 AMS-WW-T-700/6 Tube, Aluminum Alloy, Drawn, Seamless, 6061 2.1.2 ADS Publicatio
47、ns: Available from ADS Group Ltd., Salamanca Square, 9 Albert Embankment, London, SE1 7SP, United Kingdom. Tel: +44 207-091-4500, www.sbac.co.uk.AGS 1100 Pipe Couplings, Typical Joints 2.1.3 BSi Standards Available from BSi Standards, BSI British Standards, 389 Chiswick High Road, London W4 4AL, United Kingdom, United Kingdom, Tel: +44 208-996-9001, www.bsi-.BS 1471 Specification for Wrought Aluminum And Aluminum Alloys for General Engineering Purposes - Drawn TubeBS L56
