Airbus Helicopters

NH90

S8607S435M2102E01 : HEADSET ADAPTOR EXTENTION / US

Code Article P/N Constructeur Programme Désignation S8607S435M2102E01 AIRBUS Helicopters NH90 HEADSET ADAPTOR EXTENTION / US…

S8608S670A0101E01 : DROOP STOP TOOL V2

Code Article P/N Constructeur Programme Désignation S8608S670A0101E01 AIRBUS Helicopters NH90 DROOP STOP TOOL V2 Produits…

S956V7001101 : EFS FUSE DISC CABLE & SELECTOR

This AGE, “EFS FUSE DISC CABLE & SELECTOR”, allows connecting the mili-ohmeter (see
AGEIF V26501: SQUIB TEST SET) to the Emergency Flotation System’s Fuses disc in order to
measure its.

S463V4001101 : CONDITIONNEMENT FAISCEAU VALISE DMD TOOL

Code Article P/N Constructeur Programme Désignation S463V4001101 S463V4001101 AIRBUS Helicopters NH90 CONDITIONNEMENT FAISCEAU VALISE DMD…

S463V4001231 : HARNESS DMD TOOL

Code Article P/N Constructeur Programme Désignation S463V4001231 AIRBUS Helicopters NH90 HARNESS DMD TOOL Produits apparentés

S243V7003101 : HARNAIS ADAPTATEUR 28V

Code Article P/N Constructeur Programme Désignation S243V7003101 S243V7003101 AIRBUS Helicopters NH90 HARNAIS ADAPTATEUR 28V Produits…

S262V5001101 : CABLE FOR SQUIB TEST SET AND S

The “CABLE & SELECTOR SQUIBS” allows to connect the squib with the squib test set
and this without to remove it. The squib must stay mounted on extinguishing bottle for safety
reasons.

S262V5002102 : FIRE EXTINGUISHING TEST SET

Code Article P/N Constructeur Programme Désignation S262V5002102 S262V5002102 AIRBUS Helicopters NH90 FIRE EXTINGUISHING TEST SET…

S262V5003101 : SQUIB TEST SET

Code Article P/N Constructeur Programme Désignation S262V5003101 S262V5003101 AIRBUS Helicopters NH90 SQUIB TEST SET Produits…

S331V7002102 : CABLE ASSEMBLY,SPECIAL PURPOSE

The tool « LIGHTING HARMONISATION » allows putting the two LPU Boxes (LPU1 or 2) in the
cockpit by means of one support (« LPU support” to hold the two LPU boxes) and one cable of 4 m
(« LPU Harness ») to connect it in the “Cockpit chin windows” under cockpit instead of LPU 1 or 2.
This is consisting in an interface between the aircraft and the LPU 1 or 2.