SAE ARP1311C
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Landing Gear Structures and Mechanisms
Hardcopy , PDF
11-06-2018
English
27-04-2015
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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.
| DevelopmentNote |
Supersedes SAE AIR 1494. (04/2010)
|
| DocumentType |
Standard
|
| Pages |
32
|
| PublisherName |
SAE International
|
| Status |
Superseded
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| SupersededBy | |
| Supersedes |
This SAE Aerospace Recommended Practice (ARP) applies 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.All axles, wheel forks, links, arms, mechanical and gas/oil shock struts, downlock and uplock assemblies, braces, trunnion beams, and truck beams etc., that sustain loads originating at the ground, and that are not integral parts of the airframe structure, should be designed and validated in accordance with this document. Hydraulic actuators (retraction, main and nose gear steering, positioning, damping, etc.) should also be included in this coverage.System level, non-structural components such as retraction/extension valves, controllers, secondary structure and mechanisms in the airframe (e.g., manual release mechanisms, slaved doors) as well as equipment that is located in the cockpit are not addressed in this ARP.
| SAE AIR 5552 : 2015 | DEVELOPMENT AND QUALIFICATION OF COMPOSITE LANDING GEARS |
| SAE ARP5908 | Landing Gear Servicing |
| SAE AIR5883 | Landing Gear Shock Struts Bearing Selection |
| SAE AS4716B | Gland Design, O-ring and Other Elastomeric 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 AMSQQC320 | Chromium Plating (Electrodeposited) |
| MIL-A-8863 Revision C:1993 | AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES |
| SAE AS6053A | 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 AIR5883 | Landing Gear Shock Struts Bearing Selection |
| SAE ARP4912B | Design Recommendations for Spare Seals in Landing Gear Shock Struts |
| SAE AMSQQN290C | 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 AMSP83461 | 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 |
| 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 ARP5935 | 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 AS8860 | 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 AIR5451 | A Guide to Landing Gear System Integration |
| SAE AIR5479A | Environmentally Compliant Processes for Landing Gear |
| SAE ARP5429A | Landing Gear Fatigue Tests with Equivalent Damage Spectra |
| MIL-A-8860 Revision B:1987 | AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR |
| SAE AIR5358A | Landing Gear Shock Strut Hydraulic Fluid |
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