User's Manual
Table Of Contents
- toc
- TRANSMITTAL INFORMATION
- INTRODUCTION
- 1. How to Use This Manual (TASK 23-15-30-99F-801- a 01)
- A. General (Subtask 23-15-30-99F-001- a 01)
- B. Observance of Manual Instructions (Subtask 23-15-30-99F-002-
- C. Symbols (Subtask 23-15-30-99F-003- a 01)
- D. Units of Measure (Subtask 23-15-30-99F-004- a 01)
- E. Illustration (Subtask 23-15-30-99F-005- a 01)
- F. Application of Maintenance Task Oriented Support System (MTOS
- 2. Customer Support (TASK 23-15-30-99F-802- a 01)
- 3. References (TASK 23-15-30-99F-803- a 01)
- 4. Acronyms and Abbreviations (TASK 23-15-30-99F-804- a 01)
- 5. Process Verification (TASK 23-15-30-99F-805- a 01)
- 1. How to Use This Manual (TASK 23-15-30-99F-801- a 01)
- DESCRIPTION AND OPERATION
- TESTING AND FAULT ISOLATION
- 1. Planning Data (TASK 23-15-30-99C-801- a 01)
- 2. Procedure (TASK 23-15-30-700-801- a 01)
- A. Job Setup (Subtask 23-15-30-810-001- a 01)
- B. BITE (Subtask 23-15-30-810-002- a 01)
- C. LEDs (Subtask 23-15-30-810-003- a 01)
- D. Self-Test (Subtask 23-15-30-810-004- a 01)
- E. Unit Software Load Procedure (Subtask 23-15-30-810-005- a 01)
- F. Fault Isolation (Subtask 23-15-30-810-006- a 01)
- G. Job Close-up (Subtask 23-15-30-810-007- a 01)
- CLEANING
- INSPECTION/CHECK
- 1. Planning Data (TASK 23-15-30-99C-803- a 01)
- 2. Procedure (TASK 23-15-30-210-801- a 01)
- A. Job Setup (Subtask 23-15-30-210-001- a 01)
- B. General Inspection/Check Procedure of the A350 SDU and SCM (S
- C. Instructions for Continued Airworthiness, FAR 25.1529 (Subtas
- D. Inspection/Check Schedule (Subtask 23-15-30-210-004- a 01)
- E. Unscheduled Maintenance (Subtask 23-15-30-210-005- a 01)
- F. Repair Requirements (Subtask 23-15-30-210-006- a 01)
- G. Job Close-up (Subtask 23-15-30-210-007- a 01)
- REPAIR
- FITS AND CLEARANCES
- SPECIAL TOOLS, FIXTURES, EQUIPMENT, AND CONSUMABLES
- REMOVAL
- INSTALLATION
- 1. Planning Data (TASK 23-15-30-99C-808- a 01)
- 2. Procedure (TASK 23-15-30-400-801- a 01)
- A. Job Setup (Subtask 23-15-30-400-001- a 01)
- B. Installation Data (Subtask 23-15-30-400-002- a 01)
- C. Unpacking and Inspecting Equipment (Subtask 23-15-30-400-003-
- D. Customer Acceptance Procedure (Subtask 23-15-30-400-004- a 01
- E. Installation Procedure (Subtask 23-15-30-400-005- a 01)
- F. Test (Subtask 23-15-30-400-006- a 01)
- G. Job Close-up (Subtask 23-15-30-400-007- a 01)
- STORAGE (INCLUDING TRANSPORTATION)
- REWORK
- APPENDIX A (RMA)
- tables
- Table 1. Applicable Components
- Table 2. Revision History
- Table 3. MTOSS Function Code Definitions
- Table 4. Verification Data
- Table 5. SDU Leading Particulars
- Table 6. SCM Leading Particulars
- Table 7. Equipment Description
- Table 8. SDU Rear Connector Pin Deviations
- Table 9. SCM D-Type Connector Pin Assignment
- Table 10. SDU Functional Interfaces
- Table 11. Special Tools, Fixtures, and Equipment
- Table 12. Consumables
- Table 13. LED Status Indicators Table
- Table 14. Special Tools, Fixtures, and Equipment
- Table 15. Consumables
- Table 16. Special Tools, Fixtures, and Equipment
- Table 17. Consumables
- Table 18. Special Tools, Fixtures, and Equipment
- Table 19. Consumables
- Table 20. Fits and Clearances
- Table 21. Thread Size and Torque Data
- Table 22. Final Torque Data
- Table 23. Special Tools, Fixtures, and Equipment
- Table 24. Consumable Materials
- Table 25. Special Tools, Fixtures, and Equipment
- Table 26. Consumable Materials
- Table 27. Special Tools, Fixtures, and Equipment
- Table 28. Consumables
ABBREVIATED COMPONENT MAINTENANCE MANUAL
1458-A-1101 / 1458-A-1300
2. Procedure (TASK 23-15-30-400-801-A01)
A. Job Setup (Subtask 23-15-30-400-001-A01)
W
ARNING: BEFORE YOU USE A MATERIAL, REFER TO THE MANUFACTURERS’ MATE
RIAL
SAFETY DATA SHEETS. SOME MATERIALS CAN BE DANGEROUS.
C
AUTION: DO NOT USE MATERIALS THAT ARE NOT EQUIVALENT TO HONEYWELL
SPECIFIED MATERIALS. MATERIALS THAT ARE NOT EQUIVALENT CAN
CAUSE DAMAGE TO THE EQUIPMENT AND CAN MAKE THE WARRANTY NOT
APPLICABLE.
C
AUTION: DO NOT DROP OR HIT THE A350 SDU AND SCM DURING THESE PROCEDURES.
THE A350 SDU AND SCM CONTAINS AN ASSEMBLY THAT CAN BE DAMAGED
FROM INCORRECT USE.
C
AUTION: DO THESE PROCEDURES IN A CLEAN ENVIRONMENT TO PREVENT DAMAGE
TO MECHANICAL COMPONENTS.
(1) Obey the precautions.
B. Installation Data (Subtask 23-15-30-400-002-A01)
(1) Installation requirements are based on ARINC 781 specifications.
C. Unpacking and Inspecting Equipment (Subtask 23-15-30-400-003-A01)
(1) Unpack the equipment components from the shipping container. Visually inspect the units for
any shipping damage. Make sure that both the SDU and SCM are available.
• SDU PN 1394-A-1100
• SCM PN 1394-A-1300.
(2) If optional parts have been ordered, these items must be removed from the packaging and
visually inspected for any shipping damage.
D. Customer Acceptance Procedure (Subtask 23-15-30-400-004-A01)
(1) Make sure that the part number on the equipment received is correct as ordered.
(2) Check for physical damage that can occurred during shipping.
(3) Check the operational status of the SDU and SCM before installation on an aircraft by
performing the test procedures described in TESTING AND FAULT ISOLATION (PGBLK
23-15-30-1000).
E. Installation Procedure (Subtask 23-15-30-400-005-A01)
(1) General
(a) Only authorized technical personnel, trained in general aviation workmanship, that have a
basic understanding of SATCOM systems must proceed with the following procedure.
Before performing any installation procedures, read the safety advisories.
(2) SDU Installation
(a) Refer to Figure 11 (GRAPHIC 23-15-30-99B-811-A01).
(b) The A350 SDU uses ARINC 600 size 2 sh
ell receptacles located at the rear of the unit
and requires an ARINC 600 6 MCU tray
for installation.
(c) Refer to the interconnection diagrams to install the correct wiring for the services you
require. The interconnection and pinout drawings are also provided for information
purposes.
EFFECTIVITY
ALL
23-15-30
Page 64 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