User's Manual

Table Of Contents
ABBREVIATED COMPONENT MAINTENANCE MANUAL
1458-A-1101 / 1458-A-1300
Torque in-lb (Nm)
Thread Size Aluminum Fastener CRES Fastener
5/16-18 80 (9.04) 160 (18.08)
3/8-24 140 (15.82) 275 (31.075)
Table 22. Final Torque Data
Thread Size Approximate Turn After Run-Down
6-32
45 degrees
8-32
60 degrees
10-24
40 degrees
1/4-20 40 degrees
5/16-18 40 degrees
3/8-24 60 degrees
D. Specified Torque Values (Subtask 23-15-30-220-004-A01)
(1) Not applicable.
E. Job Close-up (Subtask 23-15-30-220-005-A01)
(1) Not applicable.
SPECIAL TOOLS, FIXTURES, EQUIPMENT, AND CONSUMABLES
1. P
lanning Data (TASK 23-15-30-99C-806-A01)
A. General (Subtask 23-15-30-99C-012-A01)
(1) No special tools, fixtures, or equipment is required. Standard avionics shop tools are the
only equipment required.
SPECIAL PROCEDURES
1. Not Applicable
REMOVAL
1. P
lanning Data (TASK 23-15-30-99C-807-A01)
A. Reason for the Job (Subtask 23-15-30-99C-013-A01)
(1) Use these procedures to remove the A350 SDU and SCM.
B. Job Setup Data (Subtask 23-15-30-99C-014-A01)
(1) You can use equivalent alternatives for the special tools, fixtures, equipment, and consumable
materials. The user must find equivalent alternatives.
(2) Refer to Table 23 for the specified special tools, fixtures, and equipment in this section.
(3) Refer to H4/H8 CAGE Codes (available at http://www.logisticsinformationservice.dla.mil) for
manufacturer’s address.
EFFECTIVITY
ALL
23-15-30
Page 61 of 70
5 Oct 2012
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Interim DRAFT for FCC Approval Purposes
Do Not Use for Maintenance
10-Feb-2013