191486-1 — Primary/Secondary Air/Air Heat Exchanger Repair & Overhaul

Component Overview

A primary/secondary air-to-air heat exchanger is a staged cooling unit within the air cycle pack that progressively removes heat from compressed bleed air using ram or fan air as the cooling medium. The primary stage cools incoming bleed air ahead of the air cycle machine compressor, while the secondary stage cools the recompressed air before turbine expansion, together maximizing the system's cooling capacity. Typically a brazed plate-fin aluminum core, it handles high differential temperatures and pressures. Overhaul is driven by core fouling, fin corrosion and erosion, thermal-fatigue and vibration cracking, braze-joint separation, header distortion, and internal leakage between hot and cold passages, all of which reduce heat-transfer effectiveness and can degrade overall pack performance and downstream temperature control.

Aircraft Application

Part number 191486-1 (Primary/Secondary Air/Air Heat Exchanger) is installed on the Bombardier Challenger 601. QTC supports operators and MROs servicing this platform with certified repair and overhaul.

Our Repair Capability

QTC repairs and overhauls 191486-1 to the original manufacturer's specifications under our FAA and EASA Part 145 approvals. Our team — including former OEM heat transfer engineers — performs teardown, inspection, cleaning, component replacement, functional testing, and certification, returning a serviceable unit with the appropriate airworthiness release. We also develop repairs for rejected and beyond-economic-repair (BER) hardware.

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Related Parts

Other primary/secondary air/air heat exchanger part numbers we repair — view all Primary/Secondary Air/Air Heat Exchanger parts →

Frequently Asked Questions