A BLEED AIR OVERTEMPERATURE SENSOR, DESIGNED TO LIMIT THE TEMPERATURE OF BLEED AIR ENTERING AN AIRCRAFT PNEUMATIC SYSTEM. THE SENSOR CONSISTS OF A TEMPERATURE SENSOR, A VALVE BODY ASSEMBLY HOUSING AND A BALL VALVE ASSEMBLY. THE TEMPERATURE SENSOR CONSISTS OF A HERMETICALLY SEALED FLUID SURROUNDING A BELLOWS ASSEMBLY AND AN OUTPUT ROD. THE BALL VALVE ASSEMBLY CONSISTS OF A SEAT, BALL, SPRING AND HOUSING. THE BALL VALVE ASSEMBLY IS ACTUATED BY THE OUTPUT ROD OF THE TEMPERATURE SENSOR.

CLASSIFICATION HAS BEEN DETERMINED IN ACCORDANCE WITH THE FOLLOWING:- GENERAL INTERPRETATIVE RULES (GIR)S GIR 1 HAS BEEN USED TO CLASSIFY THIS PRODUCT BY THE TERMS OF HEADING 9032 - AUTOMATIC REGULATING OR CONTROLLING INSTRUMENTS AND APPARATUS GIR 6 HAS BEEN USED TO CLASSIFY THE GOODS TO SUBHEADING LEVEL 903210 - THERMOSTATS CN CODE 90321080 - OTHER THAN ELECTRONIC TARIC 9032108090 - OTHER THAN FOR USE IN CIVIL AIRCRAFT ALSO CLASSIFIED IN ACCORDANCE WITH:- NOTE 7 (A) TO CHAPTER 90 HARMONIZED SYSTEM EXPLANATORY NOTES (HSEN) I(D) T0 HEADING 90.32