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NR - BRS-ST 82/23 - BIAS WEIGHT LIFTING BARRIER (AUTO) MK II B Organization: NR
NR - BRS-ST 82/25 ISSUE B - BALANCE WEIGHT, LIFTING BARRIER (AUTO) MK II B Organization: NR
Date: 1975-12-12
NR - BRS-ST 82/24 ISSUE A - BALANCE WEIGHT LIFTING BARRIER (AUTO) MK II B Organization: NR
Date: 1966-12-16
NR - BRS-ST 82/21 - STUD BALANCE WEIGHT CARRIAGE LIFTING BARRIER (AUTO) MK II B Organization: NR
AENOR - UNE 001 - UNE STANDARDIZED CONTROLLING SIGNALS. GRANES AND APPLIANCES HANDLING FOR LIFTING AND WEIGHTS TRANSPORT. Organization: AENOR
Date: 1957-02-15
NR - BRS-ST 90/14 - STUD WEIGHT 'C' BALANCE CARRIAGE SUB ASSEMBLY LIFTING BARRIER (AUTO) MK II B Organization: NR
LUL - S1095 - SMVT LIFTS (INCLUDING FIREFIGHTERS AND EVACUATION LIFTS) - ISSUE A4 Organization: LUL
Date: 2016-03-01
Description: This Standard does not apply to the stages of design, manufacture, installation, commissioning and safe use of SMVT lifts in non-operational areas. weight: bold;">Purpose The purpose of this Standard is to define the requirements for all SMVT lifts in LU Stations within operational areas.
LUL - S1093 - PMVT LIFTS (INCLUDING MANAGED EVACUATION LIFTS) - ISSUE A5 Organization: LUL
Date: 2016-03-01
Description: This Standard does not apply to the stages of design, manufacture, installation, commissioning and safe use of PMVT lifts in non-operational areas. weight: bold;">Purpose The purpose of this Standard is to define the requirements for all PMVT lifts in LU stations within operational areas.
FORD W-KA1 - WEIGHT MARKING OF MANUFACTURING EQUIPMENT Organization: FORD
Date: 2006-06-26
Description: Purpose and Scope This standard specifies the requirements for packaging and handling of machinery and equipment shipped into any Ford Motor Company facility that may be subject to lifting or transportation. This standard supplements the requirements of the Global Manufacturing Standard, wKA-1, Weight Marking of Manufacturing Equipment.
SAE J376 - LOAD INDICATING DEVICES IN LIFTING CRANE SERVICE Organization: SAE
Date: 1985-04-01
Description: Purpose - The purpose of this recommended practice is to establish the minimum performance criteria for systems used to measure and display to the operator, and/or other responsible persons, the weight of the load being lifted. It is not the intent of this recommended practice to define the requirements and use of weight measuring devices used in commerce or other industries.
SNZ NZS 4332 - NON-DOMESTIC PASSENGER AND GOODS LIFTS Organization: SNZ
Date: 1997-01-01
Description: NOTE – (1) A conversion or assembly replacement that results in a speed increase will count as new work if the resulting installation can no longer comply with the speed-related requirements of this Standard such as top and bottom clearances etc. A refit of a lift car that significantly increases the car weight may also count as new work.
SAE J959 - LIFTING CRANE, WIRE-ROPE STRENGTH FACTORS Organization: SAE
Date: 2012-06-01
Description: Purpose—The purpose of this document is to set forth wire-rope strength factors that have been proved by design and operating practice to be consistent with safety, economy, space, weight, and other requirements peculiar to mobile, construction-type, lifting cranes.
ABS - 152 - GUIDE FOR CERTIFICATION OF LIFTING APPLIANCES Organization: ABS
Date: 2016-01-01
Description: Process The term certification, as used herein, indicates that a lifting appliance and its equipment have been designed, constructed, installed and surveyed in compliance with this Guide, existing Rules and Guides or other acceptable standards.
SAE/TP - 2011-01-2765 - REFINED PRELIMINARY WEIGHT ESTIMATION TOOL FOR AIRPLANE WING AND TAIL Organization: SAE/TP
Date: 2011-10-18
Description: The implemented method is based on the weight decomposition of each lifting surface into primary and secondary contributions.
SAE AIR1168/8 - AIRCRAFT FUEL WEIGHT PENALTY DUE TO AIR CONDITIONING Organization: SAE
Date: 2011-07-01
Description: Two major criteria need to be considered in arriving at system take-off weight penalties: 1. Air vehicle weight is assumed fixed, and degradation in range occurs as a result of weight displacing fuel.
GMKOREA EDS-T-4528 - TEST PROCEDURE OF VERTICAL IMPACT STRENGTH FOR SEAT LIFTER - VERSION 3; ENGLISH/KOREAN; DO NOT USE ON NEW PROGRAM; NO REPLACEMENT Organization: GMKOREA
Date: 2012-04-01
Description: PURPOSE This standard aims at determining strength of the lifter (height adjuster) against impact ar raising/lowering or by its own weight.
NPFC - MIL-PRF-83817 - TRUCK, LIFT, FORK, 4,000 POUND CAPACITY, VARIABLE REACH, ROUGH TERRAIN Organization: NPFC
Date: 2012-06-15
Description: This document covers a variable reach, rough terrain forklift truck with a 4,000 pound lift capacity at a reach of 23.5 feet which is air-transportable in C-130, C-17, and C-5 aircraft.
ISO 18264 - TEXTILE SLINGS - LIFTING SLINGS FOR GENERAL PURPOSE LIFTING OPERATIONS MADE FROM FIBRE ROPES - HIGH MODULUS POLYETHYLENE (HMPE) - FIRST EDITION Organization: ISO
Date: 2016-10-15
Description: This International Standard is applicable to rope constructions made of High Modulus Polyethylene [HMPE, also referred to as Ultra High Molecular Weight Polyethylene (UHMWPE)] fibre having a minimum reference number of 12 and a maximum reference number of 72, even though there is no direct link between rope reference numbers and the type of lifting operations, either general-purpose or special lifting operations. Parts of the braided load bearing constructions in such slings, or the whole sling, can be enclosed in a protective cover/jacket/sleeve.
AGMA 13FTM13 - GEAR FAILURE ANALYSIS AND LESSONS LEARNED IN AIRCRAFT HIGH-LIFT ACTUATION Organization: AGMA
Date: 2013-09-01
Description: The high lift system of an aircraft, which contains trailing edge flaps and/or leading edge slats, increases lift for takeoff, controls flight during cruise, and reduces speed while increasing lift for shorter landing distance.
SAE/TP - 2006-01-1157 - COMPUTATIONAL AND EXPERIMENTAL STUDY ON LIFT CHARACTERISTICS OF FLAPPING WING MICRO AIR VEHICLE Organization: SAE/TP
Date: 2006-04-03
Description: Recent interest in the development of Micro-Air Vehicles (MAVs) has led to a renewed interest in flapping-wing MAVs, which will produce lift as well as thrust by wing flapping without any excessive size and weight. The present study focused on lift characteristics of a flapping flight with respect to various flapping amplitude, flapping frequency and free stream velocity for different wing planform models.

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