(b)
Make a mark at the dimension 45 mm (1.7716 in.) on the floor for the points 10 and 13.
(c)
Measure the distance between the points 5L/5R and 10/13.
(3) Angular values
(Ref. Fig. 609/TASK 05-56-00-991-011)
(a)
Make a projection to the floor of the points 11 and 12 with the SET - PLUMBS BOBS (98A08001004000). Put the theodolites in position on these points.
(b)
Make a mark at the dimension 47.36 mm (1.8645 in.) on the floor.
(c)
Write down the angles of the points 2, 4, and 6 in relation to the aircraft centerline from the points 11 and 13 for the left and right wing.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 05-56-00Page 627 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
Measurement of the Wing Points and the Horizontal Stabilizer Points
Figure 608/TASK 05-56-00-991-010
R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 05-56-00Page 628 1 1 May 01/05 1 1 1CES 1
Measurement of the Wing Points and the Horizontal Stabilizer Points Figure 608A/TASK 05-56-00-991-010-A
R 1EFF : 151-199, 401-499, 1 05-56-00Page 629 1 1 Aug 01/05 1 1 1CES 1R Measurement of the Wing Points and the Horizontal Stabilizer Points R Figure 608B/TASK 05-56-00-991-010-B
R 1EFF : 301-399, 1 05-56-00Page 630 1 1 May 01/04 1 1 1CES 1
Angular Values of the Wing Points and the Horizontal Stabilizer Points
Figure 609/TASK 05-56-00-991-011
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 05-56-00Page 631 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
R **ON A/C 301-399,
R Subtask 05-56-00-220-052-A
R C. Position of the Wing Points
R (1) Z values
R (Ref. Fig. 605A/TASK 05-56-00-991-007-A)
R (a) Install the SIGHTING RODS SET (98D08103500000) on the left and
R right points 1, 2, 3, 4, 5 and 6.
R (b) Set the sight tube at Z = -3500 mm (137.7953 in.) from the
R horizontal datum of the fuselage.
R (c) Write down the variations between the reading on the sight rods
R at points 1, 2, 3, 4, 5 and 6 L and R and the sight tube scanning
R plane.
R (2) Measure the distance between the points 5L/5R and the points 10/13.
R (Ref. Fig. 608B/TASK 05-56-00-991-010-B)
R (a) Make a projection to the floor of the points 10 and 13, 5L and 5R
R with the SET - PLUMBS BOBS (98A08001004000).
R (b) Make a mark at the dimension 45 mm (1.7716 in.) on the floor for
R the points 10 and 13.
R (c) Measure the distance between the points 5L/5R and 10/13.
R (3) Angular values
R (Ref. Fig. 609A/TASK 05-56-00-991-011-A)
R (a) Make a projection to the floor of the points 11A and 12 with the
R SET - PLUMBS BOBS (98A08001004000). Put the theodolites in
R position on these points.
R (b) Make a mark at the dimension 47.36 mm (1.8645 in.) on the floor.
R (c) Write down the angles of the points 2, 4, and 6 in relation to
R the aircraft centerline from the points 11A and 13 for the left
R and right wing.
R 1EFF : 301-399, 1 05-56-00Page 632 1 1 May 01/04 1 1 1CES 1R Angular Values of the Wing Points and the Horizontal Stabilizer Points R Figure 609A/TASK 05-56-00-991-011-A
1EFF : 301-399, 1 05-56-00Page 633 1 1 May 01/04 1 1 1CES 1
**ON A/C ALL
Subtask 05-56-00-220-053
D. Position of the Points of the Trimmable Horizontal Stabilizer (THS) NOTE : Make sure that the THS in the neutral position.
____
(1) Z values R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 605/TASK 05-56-00-991-007)
**ON A/C 301-399,
(Ref. Fig. 605A/TASK 05-56-00-991-007-A)
**ON A/C ALL
(a)
Install the SIGHTING RODS SET (98D08103500000) on the points 35, 36, 37 and 38 L and R.
(b)
Adjust a sight tube in a plane through Z = -3500 mm (137.7953 in.) of the horizontal datum of the of the fuselage.
(c)
Write down the variations between the datum indications on the rods and the scanning plane of the sight tube.
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