SAE ARP1311C
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
LANDING GEAR STRUCTURES AND MECHANISMS
Available format(s)
Hardcopy , PDF
Superseded date
06-11-2018
Language(s)
English
Published date
01-01-2015
Publisher
Important note : All end users must be registered with an Account prior to user licenses being assigned.
1. SCOPE
2. APPLICABLE DOCUMENTS
3. DESIGN REQUIREMENTS
4. DESIGN VERIFICATION
5. NOTES
Pertains to landing gear structures and mechanisms (excluding wheels, tires, and brakes and other landing gear systems) for all types and models of civil and military aircraft.
| Committee |
A-5B
|
| DevelopmentNote |
Supersedes SAE AIR 1494. (04/2010)
|
| DocumentType |
Standard
|
| Pages |
32
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| Supersedes |
| SAE AIR 5552 : 2015 | DEVELOPMENT AND QUALIFICATION OF COMPOSITE LANDING GEARS |
| SAE ARP 5908 : 2013 | LANDING GEAR SERVICING |
| SAE AIR 5883 : 2012 | LANDING GEARS SHOCK STRUTS BEARING SELECTION |
| SAE AS4716B | GLAND DESIGN, O-RING AND OTHER SEALS |
| SAE AIR 1752 : 2013 | AIRCRAFT NOSEWHEEL STEERING/CENTERING SYSTEMS |
| FAA AC 23-13 : 2005 | FATIGUE, FAIL-SAFE, AND DAMAGE TOLERANCE EVALUATION OF METALLIC STRUCTURE FOR NORMAL, UTILITY, ACROBATIC, AND COMMUTER CATEGORY AIRPLANES |
| MMPDS 03 : 2006 | METALLIC MATERIALS PROPERTIES DEVELOPMENT AND STANDARDIZATION (MMPDS) |
| SAE AIR1594C | PLAIN BEARING SELECTION FOR LANDING GEAR APPLICATIONS |
| SAE AMS QQ C 320 : 2000 | CHROMIUM PLATING (ELECTRODEPOSITED) |
| MIL-A-8863 Revision C:1993 | AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES |
| SAE AS 6053 : 2012 | TESTS, IMPACT, SHOCK ABSORBER LANDING GEAR, AIRCRAFT |
| SAE AIR 4566 : 2015 | CRASHWORTHY LANDING GEAR DESIGN |
| MS33675 Revision C:1971 | Scraper, Installation, Packing, Gland Ring |
| MIL-T-81259 Revision B:1991 | TIE DOWN, AIRFRAME DESIGN, REQUIREMENTS FOR |
| MIL-PRF-5606 Revision H:2002 | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE |
| SAE AIR 5883 : 2012 | LANDING GEARS SHOCK STRUTS BEARING SELECTION |
| SAE ARP4912B | DESIGN RECOMMENDATIONS FOR SPARE SEALS IN LANDING GEAR SHOCK STRUTS |
| SAE AMS QQ N 290 : 2015 | NICKEL PLATING (ELECTRODEPOSITED) |
| NAS 1613 : 2002 | PACKING, PREFORMED, ETHYLENE PROPYLENE RUBBER |
| MS15003 Base Document:1951 | FITTINGS, LUBRICATION (HYDRAULIC) SURFACE CHECK, 1/8 PIPE THREADS, STEEL TYPE 3 |
| MS33559 Revision E:1989 | ADAPTOR, AIRCRAFT, JACKING POINT, DESIGN AND INSTALLATION OF |
| ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
| SAE AMS P 83461 : 1998 | Packing, Preformed, Petroleum Hydraulic Fluid Resistant, Improved Performance at 275°F (135°C) |
| MS28889 Revision L:1987 | VALVE, AIR, HIGH PRESSURE CHARGING, 5000 PSI |
| MIL-PRF-87257 Revision C:2017 | HYDRAULIC FLUID, FIRE RESISTANT, LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT AND MISSILE |
| SAE ARP 1595 : 2013(R2019) | DESIGN AND VERIFICATION OF AIRCRAFT NOSE WHEEL STEERING SYSTEMS |
| MIL A 8862 : 0 | AIRPLANE STRENGTH AND RIGIDITY, LANDPLANE, LANDING AND GROUND HANDLING LOADS |
| MS15001 Revision A:1959 | FITTINGS, LUBRICATION (HYDRAULIC) SURFACE CHECK, 1/4-28 TAPER THREADS, STEEL, TYPE 1 |
| MIL-PRF-5503 Revision G:2013 | ACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
| MIL-L-22589 Revision D:1991 | LAUNCHING SYSTEM, NOSE GEAR TYPE, AIRCRAFT |
| SAE ARP 5935 : 2013 | USE OF HVOF THERMAL SPRAY COATINGS FOR HARD CHROME REPLACEMENT IN LANDING GEAR APPLICATIONS |
| MIL-L-8552 Revision C:1965 | LANDING GEAR, AIRCRAFT SHOCK ABSORBER [AIR OIL TYPE] |
| MIL-STD-809 Revision B:1986 | ADAPTER, AIRCRAFT, JACKING POINT, DESIGN AND INSTALLATION OF |
| FAA AC 25.571-1 : 2011 | DAMAGE TOLERANCE AND FATIGUE EVALUATION OF STRUCTURE |
| MIL-A-8867 Revision C:1987 | AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS |
| MIL-T-6053 Revision C:1977 | Tests, Impact, Shock Absorber Landing Gear, Aircraft |
| SAE AS1241D | FIRE RESISTANT PHOSPHATE ESTER HYDRAULIC FLUID FOR AIRCRAFT |
| SAE ARP 5936 : 2016 | LANDING GEAR STORAGE |
| MS33651 Revision C:2014 | Boss and Installations - Air Connection |
| MIL-PRF-83282 Revision D:1997 | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 |
| SAE AS 8860 : 2012 | LANDING GEAR STRUCTURAL REQUIREMENTS AS LISTED IN THE MIL-886X SERIES OF SPECIFICATIONS |
| MIL-STD-805 Revision B:1987 | TOWING FITTING AND PROVISIONS FOR FIXED WING AIRCRAFT, DESIGN, REQUIREMENTS FOR |
| SAE AS4941B | AEROSPACE - GENERAL REQUIREMENTS FOR COMMERCIAL AIRCRAFT HYDRAULIC COMPONENTS |
| SAE AS 4052 : 2015 | GLAND DESIGN: SCRAPER, LANDING GEAR, INSTALLATION |
| JSSG-2006 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
| SAE ARP 4915 : 2016 | DISPOSITION OF LANDING GEAR COMPONENTS INVOLVED IN ACCIDENTS/INCIDENTS |
| SAE AIR 5451 : 2016 | A GUIDE TO LANDING GEAR SYSTEM INTEGRATION |
| SAE AIR5479A | ENVIRONMENTALLY COMPLIANT PROCESSES FOR LANDING GEAR |
| SAE ARP 5429 : 2017 | LANDING GEAR FATIGUE TESTS WITH EQUIVALENT DAMAGE SPECTRA |
| MIL-A-8860 Revision B:1987 | AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR |
| SAE AIR 5358 : 2016 | LANDING GEAR SHOCK STRUT HYDRAULIC FLUID |
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