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Failure modes and effects analysis (FMEA) Exhaust systems Fuel consumption AGE-3 Aircraft Ground Support Equipment Committee Analysis methodologies Parts and Components

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Standard

Technical Manual Development for Ground Support Equipment
2002-07-23
HISTORICAL
AS4828
This document shall serve as a guide for format, style, and method of presentation for all material included in manufacturers' publications for ground support equipment (GSE). These requirements shall be observed throughout all publications except where modified by detail requirements for specific publications. AS4828 is not applicable to the development or revision of electronic test equipment user manuals and documents. This document is written in general terms by intention, and in most cases conform to recognized practices in the industry. In the event there is a question which is not specifically covered by this document, the user engineering department should be contacted for guidance before proceeding to the final phase of manual development. Each manual prepared by a manufacturer shall contain an introduction which shall include a brief statement explaining the organization, content, and method for using the manual.
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

SELECTION CRITERIA FOR RECIPROCATING PRIME MOVERS
1989-10-01
HISTORICAL
ARP1052
This Recommended Practice covers the following categories: a Basic engine rating (requirements for) - (Para. 3) b Suggested minimum conditions for selection - (Para. 4) c Recommended horsepower rating reductions - (Para. 5) d Special considerations - (Para. 6) e Recommended safety devices - (Para. 7) f Recommended minimum instrumentation - (Para. 8) g Recommended selection support data - (Para. 9) h Recommended usage of ARP - (Para. 10)
Standard

Regional Aircraft Towbarless Tow Vehicle - Test Requirements
2022-03-30
CURRENT
ARP5911A
The present Aerospace Recommended Practice specifies for airplane operator and tow vehicle manufacturers the basic testing requirements for towbarless tow vehicles to be used on the nose gear of conventional tricycle type landing gears of commercial civil transport aircraft with maximum ramp weight between 8600 kg (19 000 lb) and 50 000 kg (110 000 lb), commonly designated as “regional aircraft”. Its purpose is to achieve testing results, or equivalent computer modeling, demonstrating that the loads induced by the tow vehicle will not exceed the design loads of the airplane’s nose landing gear and associated structure, reduce the certified safe life limit of the nose landing gear, or otherwise compromise the airplane’s structural integrity and airworthiness certification.
Standard

Regional Aircraft Towbar Attach Fitting Interface
2011-06-20
CURRENT
AS5488A
This SAE Aerospace Standard (AS) specifies the interface requirements for towbar attachment fittings on the nose gear (when towing operations are performed from the nose gear) of conventional tricycle type landing gears of commercial civil transport aircraft with a maximum ramp weight between 8600 kg (19 000 lb) and 50 000 kg (110 000 lb), commonly designated as "regional aircraft". Its purpose is to achieve towbar attachment fittings interface standardization by aircraft weight category (which determines towbar forces) in order to ensure that one single type of towbar with a standard connection can be used for all aircraft types within or near that weight category, so as to assist operators and airport handling companies in reducing the number of different towbar types used.
Standard

Regional Aircraft Towbar Attach Fitting Interface
2002-09-20
HISTORICAL
AS5488
This SAE Aerospace Standard (AS) specifies the interface requirements for towbar attachment fittings on the nose gear (when towing operations are performed from the nose gear) of conventional tricycle type landing gears of commercial civil transport aircraft with a maximum ramp weight between 8600 kg (19 000 lb) and 50 000 kg (110 000 lb), commonly designated as “regional aircraft”. Its purpose is to achieve towbar attachment fittings interface standardization by aircraft weight category (which determines towbar forces) in order to ensure that one single type of towbar with a standard connection can be used for all aircraft types within or near that weight category, so as to assist operators and airport handling companies in reducing the number of different towbar types used.
Standard

Minimum Safety Requirements for Special Purpose Airline Ground Support Equipment
2014-05-29
CURRENT
AIR1375D
This document applies to special purpose equipment which is used in the ground handling, servicing, and maintenance of transport aircraft. Fixed airport facilities and equipment covered under other sections of Part 1910 of Code of Federal Regulations (OSHA) are excluded from the scope of this document.
Standard

Minimum Safety Requirements for Special Purpose Airline Ground Support Equipment
2000-06-01
HISTORICAL
AIR1375C
This document applies to special purpose equipment which is used in the ground handling, servicing, and maintenance of transport aircraft. Fixed airport facilities and equipment covered under other sections of Part 1910 of Code of Federal Regulations (OSHA) are excluded from the scope of this document.
Standard

Method of Evaluating Pneumatic Ground Power Units
2003-11-21
HISTORICAL
AIR4545
This SAE Aerospace Information Report (AIR) covers, and is restricted to, the behavior of air under conditions of critical and subcritical flow at temperatures less than 500 °F.
Standard

Main Line Aircraft Tow Bar Attach Fitting Interface
2021-04-08
CURRENT
AS1614D
This SAE Aerospace Standard (AS) specifies the interface requirements for tow bar attachment fittings on the nose gear (when towing operations are performed from the nose gear) of conventional tricycle type landing gears of commercial civil transport aircraft with a maximum ramp weight higher than 50,000 kg (110,000 pounds), commonly designated as “main line aircraft”. Its purpose is to achieve tow bar attachment fittings interface standardization by aircraft weight category (which determines tow bar forces) in order to ensure that one single type of tow bar with a standard connection can be used for all aircraft types within or near that weight category, so as to assist operators and airport handling companies in reducing the number of different tow bar types used.
Standard

Main Line Aircraft Tow Bar Attach Fitting Interface
2010-08-24
HISTORICAL
AS1614C
This SAE Aerospace Standard (AS) specifies the interface requirements for tow bar attachment fittings on the nose gear (when towing operations are performed from the nose gear) of conventional tricycle type landing gears of commercial civil transport aircraft with a maximum ramp weight higher than 50 000 kg (110 000 lb), commonly designated as “main line aircraft”. Its purpose is to achieve tow bar attachment fittings interface standardization by aircraft weight category (which determines tow bar forces) in order to ensure that one single type of tow bar with a standard connection can be used for all aircraft types within or near that weight category, so as to assist operators and airport handling companies in reducing the number of different tow bar types used.
Standard

MINIMUM SAFETY REQUIREMENTS FOR SPECIAL PURPOSE AIRLINE GROUND SUPPORT EQUIPMENT
1998-09-01
HISTORICAL
AIR1375B
This document applies to special purpose equipment, excluding fixed facilities, which is used in the ground handling, servicing, and maintenance of aircraft. Equipment covered under other sections of the Federal Register Part 1910 is excluded from this document. This document is to establish minimum safety requirements and should not be used for vehicle design criteria. Equipment existing prior to publication date is excluded from the requirements of this document.
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