AC Aviation EMB-135BJ Legacy 600 Maintenance Program Issue 1 Revision 0 PDF

Description

This AC Aviation Maintenance Program is the CAAT-approved scheduled maintenance document for the EMB-135BJ (Legacy 600) aircraft, serial number 14501069, registration HS-DID. Issued as document ACA-ENG-MP-DID, Issue 1, Revision 0, effective 05/07/2019, it defines the complete maintenance schedule, inspection intervals, structural requirements, corrosion prevention program, zonal inspections, powerplant rules, and airworthiness limitations necessary to keep this Legacy 600 airworthy and compliant. The program was prepared to meet the requirements of the Air Operator’s Certificates Requirements (AOCR) and CAAT announcements, incorporating the recommendations of the aircraft, engine, and equipment manufacturers.

File Details

• Manual Type: Maintenance Program (MP)
• Brand: AC Aviation / Embraer
• Model: EMB-135BJ (Legacy 600)
• Serial Number: 14501069
• Registration: HS-DID
• Engine: Rolls-Royce AE3007A1E
• APU: Hamilton Sundstrand T-62T-40C14
• Language: English
• Page Count: 301
• File Format: PDF
• Document Number: ACA-ENG-MP-DID
• Issue: 1
• Revision: 0
• Effective Date: 05/07/2019
• Approval: Civil Aviation Authority of Thailand (CAAT)
• Approval Date: 15 January 2020

Chapters and Sections Covered

The manual is organized into five major sections, with the bulk of the content in Section 2’s detailed ATA-chapter task listings:

• Section 0 – General Requirements: Company statements, annual utilization and maintenance review, aircraft application, MP owner and maintenance organization, document references, flying times, CMRs, task escalation, ADs/SBs assessment, fatigue lives and airworthiness limitation items, maintenance practices and procedures, area or zonal inspection, inspection standards, condition monitored maintenance/reliability programme, maintenance requirements, specific structural maintenance programs, repairs and modifications, RVSM and PBN maintenance procedures, ageing aircraft system, CDCCL, EWIS, Limit of Validity, MP amendments and review, ALIs, maintenance CRS, CVR/FDR download procedures, FDR system calibration, pre-flight/post-flight, dent and buckle mapping
• Section 1 – Scheduled Maintenance Requirements General: Introduction, general rules, interval, flexibility, implementation guideline for maintenance plan revisions, system and powerplant requirements, structural requirements, corrosion requirements, powerplant and APU rules, zonal requirements, list of scheduled maintenance requirements presentation, abbreviations, terms and definitions
• Section 2 – Scheduled Maintenance Requirements List of Requirements: Chapter 12 – Serving, Chapter 20 – Standard Practices – Airframe, Chapter 21 – Air Conditioning, Chapter 22 – Auto Flight, Chapter 23 – Communications, Chapter 24 – Electrical Power, Chapter 25 – Equipment/Furnishings, Chapter 26 – Fire Protection, Chapter 27 – Flight Controls, Chapter 28 – Fuel, Chapter 29 – Hydraulic, Chapter 30 – Ice and Rain Protection, Chapter 31 – Indicating/Recording Systems, Chapter 32 – Landing Gear, Chapter 33 – Lights, Chapter 34 – Navigation, Chapter 35 – Oxygen, Chapter 36 – Pneumatic, Chapter 38 – Waste and Water, Chapter 49 – Airborne Power Unit, Chapter 52 – Doors, Chapter 53 – Fuselage, Chapter 54 – Nacelle/Pylons, Chapter 55 – Stabilizers, Chapter 57 – Wings, Chapter 71 – Powerplant, Chapter 72 – Engine, Chapter 73 – Engine Fuel and Control, Chapter 74 – Ignition, Chapter 76 – Engine Controls, Chapter 78 – Exhaust, Chapter 79 – Oil, Chapter 80 – Starting
• Section 3 – National Requirements: Special rules pertaining to FAA certification, special rules pertaining to EASA certification, special rules pertaining to CAAC certification, plus EASA system maintenance requirements, EASA structural maintenance requirements, and CAAC system maintenance requirements
• Section 4 – Appendixes: Appendix A – Airworthiness Limitations (CMRs and ALIs, life limited components, structural maximum inspection interval limits, fatigue threshold limits, CDCCL, fuel system limitations), Appendix B – Aircraft Zoning Component Location, Appendix C1 – Preflight Checklist, Appendix C2 – Postflight Checklist, Appendix D – AO-Maintenance Program Amendment Approval Submission

In practical terms, this document gives a technician or maintenance planner the full scheduled maintenance load for the Legacy 600 – every inspection, functional check, operational check, restoration, lubrication, and discard task – organized by ATA chapter with thresholds, intervals, tolerances, task numbers, and effectivity. The structural section covers SSI-based inspections with fatigue thresholds and inspection interval limits. The zonal section covers general visual inspections by aircraft zone. The airworthiness limitations section lists life limited components with flight cycle limits for landing gear, oxygen cylinders, pneumatic valves, and thrust reverser components.

Structural, Corrosion, and Zonal Inspection Coverage

The structural maintenance program is designed to detect corrosion, stress corrosion, minor accidental damage, and fatigue cracking through visual and NDT procedures. Specific structural areas covered include doors, fuselage, nacelles/pylons, stabilizers, windows, and wings. The structural repair data references the SRM manual, and SSID references the Corrosion Control Manual issued by the Type Certificate Holder. The zonal inspection requirements consist of General Visual Inspections (GVI) developed for defined zones in accordance with MSG-3 methodology, with Enhanced Zonal Analysis Procedure (EZAP) applied for zones containing electrical wiring and potential combustible materials.

Corrosion requirements consist of maintenance tasks and associated intervals developed to prevent structural degradation caused by environmental deterioration. The Corrosion Prevention and Control Program (CPCP) is designed to control the aircraft structure to Corrosion Level 1 or better. Detailed inspection tasks for fuselage, wings, stabilizers, and landing gear components are listed with thresholds and repeat intervals in both flight cycles and calendar months.

Airworthiness Limitations and Life Limited Components

The Airworthiness Limitations section contains mandatory actions derived from certification activities including Damage Tolerance Analysis and Fatigue Tests. Life limited components are listed with their part numbers, suppliers, and flight cycle life limits. For the EMB-145 landing gear, these include MLG leg struts, trailing arms, wheel axles, pivots, cardan joints, shock absorber components, main and secondary side struts, and NLG sliding tubes, wheel axles, steering cuffs, torque links, main fittings, and drag struts. Additional life limited items include oxygen cylinders (180 months), low pressure bleed-air check valves (1600 FH), and thrust reverser components with life limits expressed in Thrust Reverser Cycles (TRC). The engine airworthiness limitations for the Rolls-Royce AE3007A engines are listed in Chapter 5 of the Rolls-Royce Maintenance Manual CSP34022.

Preflight and Postflight Checklists

Appendix C provides complete preflight and postflight inspection checklists covering general, left nose and fuselage, nose landing gear and bay, right nose and fuselage, right wing, right main landing gear, right engine and nacelle, aft fuselage right side, empennage, aft fuselage left side, left engine and nacelle, left main landing gear, left wing, cockpit, passenger cabin and toilet, and final items. These checklists include tire pressure specifications (nose gear 84 ± 2 PSI, main gear 160 ± 4 PSI), absorber extension minimums, brake wear indicator limits, and RVSM-specific checks. A recommended walk-around sequence illustration is included.

Who This Maintenance Program Is For

This document is intended for maintenance engineers, technicians, maintenance planners, quality personnel, and continuing airworthiness managers responsible for the EMB-135BJ Legacy 600. It is also useful for operators, CAMO personnel, and MRO organizations supporting this aircraft type. The program is specific to aircraft serial number 14501069 but its task content, intervals, and procedures are relevant to any Legacy 600 operator seeking a reference for scheduled maintenance requirements. The document includes the maintenance organization details (Jet Aviation Asia Pacific Pte. Ltd, CAAT approval No. 92/2533) and the operator’s approved maintenance program structure.

Get the Complete Maintenance Program for Your Legacy 600

With this AC Aviation Maintenance Program for the EMB-135BJ Legacy 600 in PDF format, you can plan and perform scheduled maintenance, inspections, functional checks, structural inspections, corrosion control tasks, and airworthiness limitation compliance with the exact task numbers, thresholds, intervals, and tolerances approved by the Civil Aviation Authority of Thailand. Correct procedures and accurate specifications are critical – using the wrong interval or missing a mandatory inspection task can compromise airworthiness and regulatory compliance. This PDF delivers the full program instantly after purchase, ready to view on any device or print for use in the hangar. Whether you are performing a scheduled check, planning maintenance, or verifying compliance, this document provides the approved maintenance requirements in one printable file.

IMAGES PREVIEW