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STEEL TUBING (WELDED) Chromium Molybdenum (.27 - .33 Carbon) (Normalized)
STEEL COTTER PINS, GALVANIZED Low Carbon
NUTS, SELF-LOCKING, STEEL High Strength, Prevailing-Torque, All Metal 450 F (232 C) Use, Unified "J" (MIL-S-8879) Thread Form
NUTS, SELF-LOCKING, STEEL High Strength, All Metal 450° F (230° C) Use, Unified "J" (MIL-S-8879) Thread Form
NUTS, SELF-LOCKING, STEEL High Strength, Prevailing Torque, All Metal 450° F (232° C) Use, Unified "J" (MIL-S-8879) Thread Form
Combination Tail and Floodlamp for Industrial Equipment
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
AS6070-6117 Chain (1/2" Pitch) and Fittings Assembly Code Non-Reversible Control
Validation Methods For MIL-STD-1760D Mission Stores
Electronic Design Interchange Format Version 200
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.