nose landing gear
DESCRIPTION
CYLINDER 24-4201-225. MAJOR ASSY. NOSE LANDING GEAR. THE ITEM IS FITTED IN NOSE LANDING GEAR SHOCK STRUT. THE FUNCTION OF THE COMPONENT IS TO ACCOMMODATE NOSE SHOCK ABSORBER AND PROVIDE ATTACHMENT OF NLG LEVER AND CONNECTED ACCESSORIES. WORKING TEMPERATURE - 40°C TO 80°C - PowerPoint PPT PresentationTRANSCRIPT
![Page 1: NOSE LANDING GEAR](https://reader033.vdocuments.mx/reader033/viewer/2022061418/56812cb2550346895d916521/html5/thumbnails/1.jpg)
NOSE LANDING GEARMAJOR ASSY
CYLINDER 24-4201-225
![Page 2: NOSE LANDING GEAR](https://reader033.vdocuments.mx/reader033/viewer/2022061418/56812cb2550346895d916521/html5/thumbnails/2.jpg)
THE ITEM IS FITTED IN NOSE LANDING GEAR SHOCK STRUT
THE FUNCTION OF THE COMPONENT IS TO ACCOMMODATE NOSE SHOCK ABSORBER AND PROVIDE ATTACHMENT OF NLG LEVER AND CONNECTED ACCESSORIES
![Page 3: NOSE LANDING GEAR](https://reader033.vdocuments.mx/reader033/viewer/2022061418/56812cb2550346895d916521/html5/thumbnails/3.jpg)
WORKING TEMPERATURE - 40°C TO 80°CWORKING PRESSURE - 25± 1 KG/CM²MEDIUM – NITROGEN AND GREASE
MADE OF HIGH ALLOY STEEL
ASSEMBLY FAILURE DUE TO HOLE ENLARGEMENT CAN LEAD TO NOSE LANDING GEAR COLLAPSE AND SUBSEQUENT DAMAGE TO AIRCRAFT
![Page 4: NOSE LANDING GEAR](https://reader033.vdocuments.mx/reader033/viewer/2022061418/56812cb2550346895d916521/html5/thumbnails/4.jpg)
THE ASSEMBLY IS COMPLEX IN DESIGN, CRITICAL IN FUNCTION AND REQUIRES MANUFACTURING BY HOT FORGING METHOD
THE REQUIREMENT FOR FIVE YEARS IS 60
![Page 5: NOSE LANDING GEAR](https://reader033.vdocuments.mx/reader033/viewer/2022061418/56812cb2550346895d916521/html5/thumbnails/5.jpg)
BACK TO LIST