Integrated maintenance step on helicopter fuselage
View Patent ↗Maintenance steps on helicopters ( 10 ) comprising a casing ( 1 ), integrated into a lateral shell of a fuselage of a helicopter ( 11 ) for access from outside and a step ( 2 ) being pivotably mounted in the casing ( 1 ). The invention relates as well to methods for mounting and dismounting of such maintenance steps.
1. A method for mounting a maintenance step on a fuselage of a helicopter comprising:
a casing, integrated into a lateral shell of the fuselage of the helicopter with access from outside; and
a step being pivotably mounted in the casing;
the casing being provided with an essentially rectangular frame and a rearward extension with lateral sides, the rearward extension with lateral sides being integrated into the lateral shell of the fuselage of the helicopter;
the lateral sides have coaxial borings;
the step being provided with corresponding coaxial borings in lateral flanges;
two pins being provided for insertion through the corresponding coaxial borings into the coaxial borings in the lateral sides of the rearward extension for pivotable mounting of the step in the casing; and
a retaining profile being provided for securing the inserted pins in their position; wherein said method comprises the following steps:
inserting the rearward extension of the essentially rectangular casing of the maintenance step into the prepared fuselage of the helicopter;
riveting the essentially rectangular frame of the casing flat against the lateral shell of the prepared fuselage of the helicopter;
inserting pins from within a mid box through the corresponding coaxial borings into the coaxial borings in the lateral sides of the rearward extension;
clipping the retaining profile into the grooves at the inwardly pointing ends of the inserted pins to fix the pins in their position; and
screwing the step cover onto the step to fix the retaining profile relative to the grooves in its clipped position.
2. A method according to claim 1 , wherein the step has an interface that is geometrically equivalent to the lateral shell.
3. A method according to claim 1 , wherein a backside of the rearward extension is formed with an overhang.
4. A method according to claim 1 , wherein a full flat stepping area with anti-skid painting is provided on the surface of the step.
5. A method according to claim 1 , wherein a step cover is mounted to the step by at least one safety screw.
6. A method according to claim 5 , wherein an opening is provided in the step cover for mounting of a lock to the step cover.
7. A method according to claim 1 , wherein wear resistant bearings are provided for insertion into the borings of the lateral sides of the rearward extension of the casing.
8. A method according to claim 1 , wherein washers are provided at the inside of the lateral sides and coaxially with the bearings.
9. A method according to claim 1 , wherein mounting of bearings into coaxial borings in the lateral sides of the rearward extension of the essentially rectangular casing before insertion of the pins from within the mid box through the corresponding coaxial borings into the coaxial borings in the lateral sides of the rearward extension.
10. A method according to claim 9 , wherein arranging washers on the inside of the lateral sides and coaxially with the bearings before insertion of the pins.
11. A method according to claim 1 , wherein covering the surface opposite the full flat stepping area of step with a step cover screwed with safety screws.
12. A method for dismounting a maintenance step on a fuselage of a helicopter comprising:
a casing, integrated into a lateral shell of the fuselage of the helicopter with access from outside; and
a step being pivotably mounted in the casing;
the casing being provided with an essentially rectangular frame and a rearward extension with lateral sides, the rearward extension with lateral sides being integrated into the lateral shell of the fuselage of the helicopter;
the lateral sides have coaxial borings;
the step being provided with corresponding coaxial borings in lateral flanges;
two pins being provided for insertion through the corresponding coaxial borings into the coaxial borings in the lateral sides of the rearward extension for pivotable mounting of the step in the casing; and
a retaining profile being provided for securing the inserted pins in their position; wherein said method comprises the following steps:
unscrewing and removing the step cover from the step;
taking a retaining profile out of the grooves at the inwardly pointing ends of the inserted pins;
removing the pins from their positions in the coaxial borings; and
taking the step out of the prepared fuselage of the helicopter.
13. A method according to claim 12 , wherein the step has an interface that is geometrically equivalent to the lateral shell.
14. A method according to claim 12 , wherein a backside of the rearward extension is formed with an overhang.
15. A method according to claim 12 , wherein a full flat stepping area with anti-skid painting is provided on the surface of the step.
16. A method according to claim 12 , wherein a step cover is mounted to the step by at least one safety screw.
17. A method according to claim 16 , wherein an opening is provided in the step cover for mounting of a lock to the step cover.
18. A method according to claim 12 , wherein wear resistant bearings are provided for insertion into the borings of the lateral sides of the rearward extension of the casing.
19. A method according to claim 12 , wherein washers are provided at the inside of the lateral sides and coaxially with the bearings.