Standard
ADAPTER, AIRCRAFT, JACKING POINT, DESIGN AND INSTALLATION OF
1998-05-01
HISTORICAL
AS33559
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Standard
ADAPTER, AIRCRAFT, JACKING POINT, DESIGN AND INSTALLATION OF
2014-05-29
CURRENT
AS33559A
Standard
CUSHION TOW HITCHES TEST
1974-05-01
HISTORICAL
AIR1353
The main purpose of this test was to determine the application advantages of cushion tow hitches in comparison to the commonly used rigid tow hitch type fitted on heavy aircraft towing tractors. As diverse opinions emerged about its suitability since the introduction on the market of this new tow hitch type, it was intended to physically measure and evaluate the damping capability of this cushioned tow link when applied in practice.
Standard
SOLID-STATE FREQUENCY CONVERTER 400 HERTZ, 3-PHASE OUTPUT
1989-09-01
HISTORICAL
ARP1940
This specification covers the requirements for solid-state frequency converters with 480 [or 380] V 3-phase, 60 [or 50] Hz input and 115/200 V, 3-phase, 400 Hz output capable of powering aircraft type loads requiring MIL-STD-704D quality power. The frequency converter shall be a self-contained unit suitable for the environment of intended use. Typical applications include dedicated use at passenger loading bridges (mounted under the bridge in telescoping bridge applications or fixed installation at base of stationary type loading bridges) with weatherproof enclosures or hangar/lab use where indoor fixed or portable units can be used.
Standard
Design Specification for Towbarless Push-Back Tow Vehicles
2000-11-01
HISTORICAL
ARP4852B
Standard
Design Specification for Towbarless Push-Back Tow Vehicles
2012-12-17
CURRENT
ARP4852C
Standard
AEROSPACE GROUND EQUIPMENT CRITERIA FOR UMBILICAL SYSTEMS PROPELLANT QUICK-DISCONNECTS
1970-09-01
HISTORICAL
ARP1206
This Aerospace Recommended Practice includes the following areas: basis for system requirements; selection of materials coupled with hazards and safety; configuration of design; system operation; and evalua tion testing.
Standard
Aerospace Ground Equipment Criteria for Umbilical Systems Propellant Quick-Disconnects
2012-11-21
CURRENT
ARP1206A
This Aerospace Recommended Practice includes the following areas: basis for system requirements; selection of materials coupled with hazards and safety; configuration of design; system operation; and evaluation testing.
Standard
Marking of Aircraft Ground Support Equipment and Other Flight Line Vehicles with Retro-Reflective Materials; Process For
2002-02-13
HISTORICAL
AS81807
This specification prescribes general requirements for marking of aircraft ground support equipment and other vehicles (i.e., runway sweepers, firetrucks, refulers, etc.), used on or near the flight line area with retro-reflective materials.
Standard
Aural Protector, Sound
1999-05-01
HISTORICAL
AS23899
This specification covers the design and performance requirements for one type of sound aural protector.
Standard
Aural Protector, Sound
2012-01-24
CURRENT
AS23899A
This specification covers the design and performance requirements for one type of sound aural protector.
Standard
Method of Testing Pre-Conditioned Air Equipment
2008-04-15
HISTORICAL
ARP5374A
This SAE Aerospace Recommended Practice (ARP) applies to Point-Of-Use, Central and Mobile Pre-Conditioned Air Equipment. It does not apply to aircraft mounted equipment.
Standard
Hook Filler Cap Chain
1999-04-01
CURRENT
AS29523
Standard
EFFECTS OF NO-BREAK POWER TRANSFER ON 400 HZ AUXILIARY-POWER UNITS AND GROUND-POWER UNITS
1992-02-01
CURRENT
AIR4651
This SAE Aerospace Information Report (AIR) describes the characteristics and effects of using no-break power transfer (NBPT) methods when switching between auxiliary-power unit (APU) and ground-power unit (GPU). The GPU may be: a Point-of-use solid-state frequency converter, engine-generator, or motor-generator b Central system powered by motor-generator or solid-state frequency converter
Standard
400-CYCLE GROUND POWER UNIT PROVISIONS FOR AIRCRAFT ELECTRICAL SYSTEM PROTECTION
2002-12-16
CURRENT
ARP760
This SAE Recommended Practice which defines the terms and tabulates the limits of the characteristics for various protective devices used in conjunction with 400-cycle ground power for civil aircraft is intended to assist the airlines in standardizing on 400-cycle protective systems. The limits found to be acceptable in the civil aircraft industry are presented.
Standard
Air Intake Covers - Aircraft
2002-12-16
CURRENT
ARP762
Standard
Towbarless Towing Vehicle Operating Procedure
1997-12-01
HISTORICAL
ARP5285
This document describes:
Standard
Towbarless Towing Vehicle Operating Procedure
2003-05-27
HISTORICAL
ARP5285A
This document describes:
Standard
Towbarless Towing Vehicle Operating Procedure
2022-09-30
CURRENT
ARP5285B
This document describes:
Standard
Nose Gear Towbarless Tow Vehicle Basic Test Requirements
2005-02-10
HISTORICAL
ARP5283
The purpose of this specification is to provide airplane operators and tow vehicle manufacturers with: a General design and operating requirements pertinent to test and evaluation of towbarless tow vehicles. Specific design requirements are provided in ARP4852A and ARP4853A. b Test and evaluation requirements. The results of these test evaluations will determine if the loads induced by the tow vehicle will exceed the design loads of the nose gear, reduce the certified safe life limit of the nose gear, or induce a stability problem during pushback and/or maintenance towing operations. This document specifies general test requirements and a test evaluation procedure for towbarless tow vehicles (TLTV) intended for pushback and maintenance towing only. It is not meant for dispatch (operational) towing (see definitions in Section 3). Dispatch towing imposes greater loads on nose gears and structure due to additional passenger, cargo, and fuel loads.
