Overhauled / Exchange — Pneumatic system components
8130-3 — Full traceability
ECS / Pressurization — Environmental control parts

Sub-Categories

Bleed Air Valves

Pre-cooler isolation valves, HP valve (HPV), bleed valve actuators, bleed regulator for Boeing/Airbus and corporate jets

Pneumatic Ducting

Titanium and Inconel ducting (AS18280 / AS1895 specs), flanges, connections, clamp rings, fire-sleeve coverage

Pressurization Controllers

Pressure control boxes (PCB), outflow valve actuators, cabin altitude controllers, safety valve for emergency pressurization

Outflow Valves

Motor-driven outflow valve assemblies, outflow valve position sensors, pressure relief valves for Boeing/Airbus/corporate

Air Cycle Machine (ACM)

ACM turbine wheels, compressor wheels, seals, bearings, ACM controller for environmental control system (ECS)

Anti-Icing / De-Ice Pneumatics

Piccolo tube systems, pneumatic de-ice boots, boot valves, anti-ice system regulators for wing and empennage

Common Part Numbers

Part NumberTypeNotes
312A0040-32Bleed ValveHP bleed valve assembly, Gulfstream application — exchange available
392A9100-14DuctingPneumatic duct assembly, Inconel, -14 size — Gulfstream/Airbus
214A0102-4Outflow ValveOutflow valve motor-driven assembly, Gulfstream G550
390A9226-8Duct ClampTitanium duct clamp ring, 3.5" ID, fire-sleeve required
S-1650-08Pressurization ControllerCabin pressure control box, Gulfstream GIII/GIV — exchange
AR163-7De-Ice Boot ValveAnti-ice pneumatic boot valve, corporate/GA application

What We Source

Pneumatic systems on modern aircraft serve three purposes: engine bleed air for ECS (environmental control system), anti-icing (wing and engine inlet), and backup pneumatic power for hydraulic reservoirs and starter systems. Components range from titanium ducting and clamp rings to complex air cycle machines and pressurization controllers.

The most common procurement scenario is ECS/pressurization problems: outflow valve failure, bleed valve actuator wear, pressurization controller fault, or ducting chafing on a phase inspection. For these situations, exchange and overhauled units are the fastest and most cost-effective path.

System Overview by Platform

Boeing 737/757/767/777

HP bleed air from the compressor section at ~45 PSI. Pre-cooler (heat exchanger) reduces temperature to ~390 deg F. HP valve (HPV) controls bleed pressure to the Pneumatic Distribution System (PDS). Common failure items: HPV actuator, PCV (pre-cooler valve), bleed regulator, and ducting chafing near hot sections.

Airbus A320 Family / A330 / A340

ECAM-controlled bleed system. Three independently-controlled bleed sources (ENG1, ENG2, APU, or HP ground cart). HPV and PRV (Pressure Regulation Valve) control flow. Common: bleed monitoring computer (BMC), HP valve, ducting sensor failures.

Gulfstream G550 / G650

Engine bleed air (HP and LP ports), APU bleed, and external air connection. Pre-cooler and HPV control bleed to ECS. Pressurization controlled by outflow valve motor driven by the pressurization controller. Common: outflow valve motor assembly, pressurization controller PCB, bleed valve actuator.

De-Ice / Anti-Ice Pneumatics

Piccolo tube pneumatic de-ice systems on wings and tail. Boot-type de-ice systems (pneumatic inflation of rubber boots). Boot control valves and timer switches. Common: boot valve failure, timer/relay faults, pneumatic line chafing.

Certification

All pneumatic system components (valves, actuators, controllers) come with 8130-3 or EASA Form 1. Ducting ships with pressure-test certificates from the manufacturing facility. Outflow valve exchange includes functional test data from the exchange facility.

Get a quote on pneumatic parts

Submit a part number or list — our sourcing team responds within 1 business day. AOG requests get priority response within 1 hour.