25-11-00Page 17
Safety Harness Figure 009
R EFF : CES ALL 25-11-00 Page 18 May 01/03
The translation movement is given by two guide tubes attached to the rear upper and lower sections of the seat. The tubes are guided by ball-sleeves attached to the rear panel. The seat is held in position by a locking pin which engages in the upper guide tube (Part 1). (Ref. Fig. 010) The seat bottom folds down and locks automatically in the low position. The opening of the seat bottom can be done only when the seat is in utilization position on the aircraft centerline. Locking is achieved by a hook attached to the right upright of the seat which locks one of the rollers guiding the seat bottom movement. The headrest is folded up into its extended position where it automatically locks in place. It is held in position by two locking pins which engage in lateral holes.
(2) Return to stowed position (Ref. Fig. 010) To fold down the headrest, simultaneously operate the two controls located in the center of bottom section of the headrest. When the system unlocks, fold down the headrest into its stowed position. To return the assembly to its stowed position:
-move the control handle marked SEAT UNLOCK upwards and move the seat to stowed position. As soon as the seat detects this movement and if the seat is not occupied, the seat bottom will then rise automatically. This prevents any interference with the First Officer seat when it is moved backwards. or
-pull up the seat bottom to override the locking force then the seat bottom will rise automatically. Move the control handle marked SEAT UNLOCK upwards and move the seat to the stowed position.
R **ON A/C 106-149, 151-199, 201-299, 301-399, 401-499,
(1) Deployment from stowage position to utilization position on aircraft centerline. To move the seat to its utilization position on the aircraft centerline, the handle called SEAT UNLOCK, located on the left of the seat, must be pulled upwards in order to unlock the system and enable the seat to slide sidewise into its utilization position. When the utilization position is reached, the system locks. The translation movement is given by two guide tubes attached to the rear upper and lower sections of the seat. The tubes are guided by ball-sleeves attached to the rear panel. The seat is held in position by a locking pin which engages in the upper guide tube (Part 1). (Ref. Fig. 010A)
EFF : ALL
25-11-00Page 19
Stowage and Deployment of the Third Occupant Seat Figure 010
R EFF : 001-049, 051-099, 101-105, 25-11-00 Page 20 May 01/05
CES
Stowage and Deployment of the Third Occupant Seat Figure 010A
R EFF : 106-149, 151-199, 201-299, 301-399, 401-499, 25-11-00 Page 21 Aug 01/05
CES
The seat bottom folds down and locks automatically in the low position. The opening of the seat bottom can be done only when the seat is in utilization position on the aircraft centerline. Locking is achieved by a hook attached to the right upright of the seat which locks one of the rollers guiding the seat bottom movement. The armrests are folded down manually. The headrest is folded up into its extended position where it automatically locks in place. It is held in position by two locking pins which engage in lateral holes.
(2) Return to stowed position (Ref. Fig. 010A) To fold down the headrest, simultaneously act the two controls located in the center of the bottom section of the headrest. When the system unlocks, fold down the headrest into its stowed position. To return the assembly to its stowed position:
-move the control handle marked SEAT UNLOCK upwards and move the seat to the stowed position. As soon as the seat detects this movement and if the seat is not occupied, the seat bottom and the two armrests will then rise automatically. This prevents any interference with the First Officer seat when it is moved backwards. or
-pull up the seat bottom to override the locking force then the seat bottom and the two armrests will rise automatically. Move the control handle marked SEAT UNLOCK upwards and move the seat to the stowed position.
**ON A/C ALL
(3) Safety harness (Ref. Fig. 011) The straps can be clipped into the buckle in any order. Turning the unlocking control through a 1/4 turn, either clockwise or anticlockwise, releases the two shoulder straps and the lap belt. Pressing the control located on the top of the buckle releases the shoulder straps alone. A control lever, located behind the seat on the left side, serves to lock the inertia reel. To lock the mechanism, the lever must be the in up position.
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