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 23-15-30-550-801-A01)
A. Job Setup (Subtask 23-15-30-550-001-A01)
W
ARNING: BEFORE YOU USE A MATERIAL, REFER TO THE MANUFACTURERS’ MATERIAL
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. Preservation (Subtask 23-15-30-550-002-A01)
(1) Not applicable.
C. Packing (Subtask 23-15-30-550-003-A01)
(1) Not applicable.
D. Storage (Subtask 23-15-30-550-004-A01)
(1) Store the A350 SDU and SCM equipment in a cool, dry place [ground survival temperature
range is
67 to 185 F( 55 to +85 C)] in its original shipping container.
E. Transportation (Subtask 23-15-30-550-005-A01)
(1) Not applicable.
F. Job Close-up (Subtask 23-15-30-550-006-A01)
(1) Not applicable.
REWORK
1. P
lanning Data (TASK 23-15-30-99F-806-A01)
A. General (Subtask 23-15-30-99F-014-A01)
(1) Rework is not supported in the field. Return any SDU or SCM units that fail the test procedures
provided in this document to the manufacturer for fault isolation and repair. Refer to APPENDIX
A (RMA) (PGBLK 23-15-30-1700) for the return procedure.
APPENDIX A (RMA)
1. P
lanning Dat
a (TASK 23-15-30-99F-807-A01)
A. General (Subtask 23-15-30-99C-019-A01)
(1) To return the equipment to Honeywell for repair, this RMA procedure must be followed. Failure
to comply with this procedure can result in shipping delays and additional charges.
EFFECTIVITY
ALL
23-15-30
Page 68 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