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J1349 Certified Power Engine Data for Ford Expedition / Lincoln Navigator - Level 2
J1349 Certified Power Engine Data for GM LNF as used in 2007 Pontiac Solstice/Saturn Sky Level 1
J1349 Certified Power Engine Data for GM LLT as used in 2010 Cadillac CTS Wagon - Level 2
J1349 Certified Power Engine Data for GM LE5 as used in 2007 Chevrolet HHR
Fuel Fired Engine Preheaters and Their Application
TOLERANCES, METRIC Aluminum Alloy Drawn Tubing
TOLERANCES, METRIC Aluminum Alloy Drawn Tubing
TOLERANCES, METRIC Aluminum Alloy Drawn Tubing
Manufacturing Message Specification – Service Definition and Protocol
Procedure for the Continuous Sampling and Measurement of Non-Volatile Particle Emissions from Aircraft Turbine Engines
Procedure for the Continuous Sampling and Measurement of Non-Volatile Particle Emissions from Aircraft Turbine Engines
Training Program Guidelines for Deicing/Anti-Icing of Aircraft on Ground
J1349 Certified Power Engine Data for GM LE5 as used in 2007 Pontiac G6 Level 2
J1349 Certified Power Engine Data for Ford as used in 2007 J50C / Mazda CX9 Level 2
Megawatt Charging System for Electric Vehicles
Special Considerations for the Application of IVHM to Autonomous Aircraft and Vehicles
Procedure for Mapping Fuel Consumption for small spark ignited engines
Quality Pressure Measurements for Determining Inlet Distortion
Procedure for the Continuous Sampling and Measurement of Non-Volatile Particle Emissions from Aircraft Turbine Engines
This Aerospace Information Report (AIR) is a historical technical record describing procedures, required continuous sampling conditions, and instrumentation for the measurement of non-volatile particle number and mass concentrations from the exhaust of aircraft gas turbine engines. Procedures are included to calculate sampling loss performance. This AIR is not intended for in-flight testing, nor does it apply to engine operating in the afterburning mode.
This Aerospace Information Report is a historical technical record of the initial document detailing the measurement of non-volatile particle emissions at the exit plane of aircraft gas turbine engines. This methodology was adopted by ICAO into Annex 16 Vol II and updated into Aerospace Recommended Practice ARP6320.
Future updates of this document may include explanations of the reasoning and assumptions used to develop this measurement methodology.