1、AEROSPACEINFORMATION REPORTAIR1673 REV. BIssued 1986-07Reaffirmed 2013-08Revised 2014-09Superseding AIR1673AAircraft Cargo Door Opening/Sill Details forGround Support Equipment InterfaceRATIONALERevision B incorporates the aircraft cargo door opening and doorsill details for the A300-600, A310, A320
2、 family, A330F, A350, A380, B737-700C, B747-8F, B757F, B777F, and B787.1. SCOPEManufacturers/designers of all aircraft equipped with a pallet/container capability have provided a means of linking the ground loaders/elevators with the aircraft sill for the smoother transfer of pallets and containers
3、into or out of the aircraft holds.Use of the aircraft attachment points may be used as a means of averting damage to the aircraft door frames and other important parts. Latch-on guarantees fore and aft and vertical alignment of the loader bed with the aircraft doorway, when used in conjunction with
4、the appropriate ground equipment.This SAE Aerospace Information Report (AIR) has been prepared by SAE Subcommittee AGE-2A to present a review of the current range of aircraft attachment points on wide body aircraft and those narrow body aircraft with a ULD cargo capability. Airline operators, who ut
5、ilized these facilities, have been faced with a growing number of adaptor bars necessary to suit each type of aircraft and door position. There is also a stowage problem on the elevator compounded by the increasing number of bars necessary to suit each aircraft. Some measure of standardization is ob
6、viously desirable.The adapter bars which have to be fitted to the forward face of the elevators to suit each different type of sill attachment are very heavy and present some handling problems to operators.Where the same elevator services different aircraft types, these bars may have to be changed m
7、any times each day on the ramp.Alternatively, elevators have to be restricted to servicing specific aircraft types or to those aircraft where a common attachment point already exists._SAE Technical Standards Board Rules prov ide that: “This report is published by SAE to adv ance the state of technic
8、al and engineering sciences. The use of this report is entirely v oluntary , and its applicability and suitability f or any particular use, including any patent inf ringement arising theref rom, is the sole responsibility of the user.”SAE rev iews each technical report at least ev ery f iv e y ears
9、at which time it may be rev ised, reaf f irmed, stabilized, or cancelled. SAE invites your written comments and suggestions.Copy right 2014 SAE InternationalAll rights reserv ed. No part of this publication may be reproduced, stored in a retriev al sy stem or transmitted, in any f orm or by any mean
10、s, electronic, mechanical, photocopy ing, recording, or otherwise, without the prior written permission of SAE.TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada)Tel: +1 724-776-4970 (outside USA)Fax: 724-776-0790Email: CustomerServicesae.orgSAE WEB ADDRESS: http:/www.sae.orgSAE val
11、ues your input. To provide feedbackon this Technical Report, please visithttp:/w ww.sae.org/technical/standards/AIR1673BSAE INTERNATIONAL AIR1673B Page 2 of 1341.1 PurposeThe purpose of this document is to provide detailed data of the aircraft attachment points at each door position capable of loadi
12、ng pallets or containers on the current aircraft and on new aircraft, where known.Aircraft designers may utilize this information to enable future designs to fall into one of these categories with a view to keeping the range of elevator adaptor bars to the present level.The design of the aircraft at
13、tachment points is governed by sill design. Two types of attachment provisions for latch-onfittings are available as follows:1. Special fittings in the vicinity of door latch fittings.2. Special door latch fittings (spools) as approved for use by the airframe manufacturers.Ground equipment design ob
14、jective should be to attempt to incorporate latch-on capability of two or more sill types on their adaptor bars.2. APPLICABLE DOCUMENTSThe following publications form a part of this document to the extent specified herein. The latest issue of SAE publications shall apply. The applicable issue of oth
15、er publications shall be the issue in effect on the date of the purchase order. In theevent of conflict between the text of this document and references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a sp
16、ecific exemption has been obtained.2.1 IATA PublicationsAvailable from IATA Head Office, 800 Place Victoria, P.O. Box 113, Montreal, Quebec H4Z 1M1, Canada, Tel: 1-514-874-0202, www.iata.org.IATA AHM 931 Functional Specification for Lower Deck Container/Pallet LoaderIATA AHM 932 Functional Specifica
17、tion for Main-Deck Container/Pallet Loader2.2 ISO PublicationsAvailable from American National Standards Institute, 25 West 43rd Street, 4th Floor, New York, NY 10036-8002, Tel: 212-642-4900, www.ansi.org.ISO 6967 Aircraft - Wide body aircraft main deck container/pallet loader - Functional requireme
18、ntsISO 6968 Aircraft - Wide body aircraft lower deck container/pallet loader - Functional requirements2.3 Aircraft ManualsIn the case of contradiction between this AIR and the aircraft manual, the aircraft manual shall preside as the authority.http:/ (limited access)SAE INTERNATIONAL AIR1673B Page 3
19、 of 1343. DATA CLASSIFICATION3.1. Airbus A300/310Lower deck - Figures 1A through 1E3.2 Airbus A300/310Main deck - Figures 2A through 2C3.3 B707/B727Main deck - Figures 3A through 3B3.4 B737Main deck - Figures 4A through 4D3.5 B747Lower deck - Figures 5A through 5D3.6 B747Main deck - Figures 6A throu
20、gh 6F3.7 B767Lower deck - Figures 7A through 7H3.8 DC8Main deck - Figures 8A through 8G3.9 DC9Main deck - Figures 9A through 9D3.10 DC10/MD11Lower deck - Figures 10A through 10D3.11 DC10/MD11Main deck - Figures 11A through 11E3.12 L1011Lower deck - Figures 12A through 12H3.13 L100Main deck - Figures
21、 13A through 13D3.14 Airbus A300F/310FMain deck - Figures 14A through 14CSAE INTERNATIONAL AIR1673B Page 4 of 1343.15 Airbus A319/320/321Lower deck - Figures 15A through 15F3.16 Airbus A330/A340Lower deck - Figures 16A through 16G3.17 B767FMain deck - Figures 17A through 17C3.18 B757FLower deck Figu
22、re 18A3.19 B757FMain deck Figure 19A3.20 B777Lower deck - Figures 20A through 20E3.21 B777FMain deck Figures 21A through 21B3.22 B787Lower deck Figure 22A through 22B3.23 A330FMain deck Figures 23A through 23B3.24 A350Lower deck Figures 24A through 24D3.25 A380Lower deck Figures 25A through 25DSAE I
23、NTERNATIONAL AIR1673B Page 5 of 1343.1 Airbus A300 and A310 - Lower DeckCargo Door Sill Attachment FittingDetails for Ground Loading EquipmentSee Figures 1A through 1E.SAE INTERNATIONAL AIR1673B Page 6 of 134FIGURE 1A - LOWER DECK - HOLD 1 DOOR (PRE. MOD. 2295)A300 AIRCRAFTSAE INTERNATIONAL AIR1673B
24、 Page 7 of 134FIGURE 1B - LOWER DECK - HOLD 1 DOOR (POST MOD. 2295)A300 AIRCRAFT AND A310 AIRCRAFTSAE INTERNATIONAL AIR1673B Page 8 of 134FIGURE 1C - LOWER DECK - HOLD 2 DOORA300 AIRCRAFT AND A310 AIRCRAFTSAE INTERNATIONAL AIR1673B Page 9 of 134FIGURE 1D - LOWER DECK - HOLD 1 AND 2 DOORSLATCH AND SP
25、OOL GEOMETRY/DIMENSIONSA300 AIRCRAFT AND A310 AIRCRAFTSAE INTERNATIONAL AIR1673B Page 10 of 134FIGURE 1E - LOWER DECK - HOLD 1 AND HOLD 2 DOORSDOOR SPOOLS - POSITIONING DETAILSA300 AIRCRAFT AND A310 AIRCRAFTSAE INTERNATIONAL AIR1673B Page 11 of 1343.2 Airbus A300 and A310 - Main DeckCargo Door Sill
26、Attachment FittingDetails for Ground Loading EquipmentSee Figures 2A through 2C.SAE INTERNATIONAL AIR1673B Page 12 of 134FIGURE 2A - UPPER DECK - CARGO DOORA300 - C4 AIRCRAFT AND A310 AIRCRAFTSAE INTERNATIONAL AIR1673B Page 13 of 134FIGURE 2B - UPPER DECK - CARGO DOORBOLT GEOMETRY AND DIMENSIONSA300
27、 - C4 AIRCRAFT AND A310 AIRCRAFTSAE INTERNATIONAL AIR1673B Page 14 of 134FIGURE 2C - UPPER DECK - CARGO DOORBOLT - POSITIONING DETAILSA300 - C4 AIRCRAFT AND A310 AIRCRAFTSAE INTERNATIONAL AIR1673B Page 15 of 1343.3 Boeing 707 and 727 - Main DeckCargo Door Sill Attachment FittingDetails for Ground Lo
28、ading EquipmentSee Figures 3A through 3B.SAE INTERNATIONAL AIR1673B Page 16 of 134FIGURE 3A - BOEING 707 AND 727 LOADER ATTACHMENTMAIN DECK CARGO DOORSAE INTERNATIONAL AIR1673B Page 17 of 134FIGURE 3B - B707 AND B727 LOADER ATTACHMENTSAE INTERNATIONAL AIR1673B Page 18 of 1343.4 Boeing 737 - Main Dec
29、kCargo Door Sill Attachment FittingDetails for Ground Loading EquipmentSee Figures 4A through 4D.SAE INTERNATIONAL AIR1673B Page 19 of 134FIGURE 4A - B737-200 - LOADER ATTACHMENTMAIN DECK CARGO DOORSAE INTERNATIONAL AIR1673B Page 20 of 134FIGURE 4B - B737-200 LOADER ATTACHMENTSAE INTERNATIONAL AIR16
30、73B Page 21 of 134B737FIGURE 4C - B737-700C - MAIN DECK CARGO DOORSAE INTERNATIONAL AIR1673B Page 22 of 134B737FIGURE 4D - B737-700C - MAIN DECK CARGO DOOR SWINGSAE INTERNATIONAL AIR1673B Page 23 of 1343.5 Boeing 747 - Lower DeckCargo Door Sill Attachment FittingDetails for Ground Loading EquipmentS
31、ee Figures 5A through 5D.SAE INTERNATIONAL AIR1673B Page 24 of 134FIGURE 5A - BOEING 747 LOWER LOBEFORWARD CARGO COMPARTMENTSAE INTERNATIONAL AIR1673B Page 25 of 134FIGURE 5B - BOEING 747 LOWER LOBEAFT CARGO COMPARTMENTSAE INTERNATIONAL AIR1673B Page 26 of 134FIGURE 5C - BOEING 747 LOWER LOBEGENERAL
32、 ARRANGEMENT OF DOOR LATCH FITTINGSSAE INTERNATIONAL AIR1673B Page 27 of 134FIGURE 5D - BOEING 747 LOWER LOBEALLOWABLE LOADSSAE INTERNATIONAL AIR1673B Page 28 of 1343.6 Boeing 747 - Main Deck, Nose and SideCargo Door Sill Attachment FittingDetails for Ground Loading EquipmentSee Figures 6A through 6F.SAE INTERNATIONAL AIR1673B Page 29 of 134FIGURE 6A - BOEING 747 F AND C MAIN DECK NOSE DOORGENERAL ARRANGEMENT DOOR SILL INTERFACESAE INTERNATIONAL AIR1673B Page 30 of 134FIGURE 6B - BOEING 747 F AND C MAIN DECK NOSE DOORDOOR SILL INTERFACE
