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Boeing 737-300, 737-400, 737-500 Continuous Airworthiness Maintenance Program (CAMP Rev 40)

Original price was: $44.95.Current price is: $27.95.

Official Garuda Indonesia Continuous Airworthiness Maintenance Program (CAMP Rev 40, Doc No. MZ-TD-04-737) for Boeing 737-300, 737-400, and 737-500 aircraft powered by CFM56-3 engines. Features full task cards, inspection intervals, ATA breakdowns, and regulatory compliance specifications.

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Description

Garuda Indonesia Boeing 737-300, 737-400, 737-500 Continuous Airworthiness Maintenance Program (CAMP Rev 40)

The Boeing 737-300, 737-400, 737-500 Continuous Airworthiness Maintenance Program (CAMP Rev 40) is an exhaustive, engineering-approved technical document (Doc No. MZ-TD-04-737) establishing mandatory scheduled maintenance intervals, routine checks, and detailed task breakdowns for commercial Boeing 737 Classic fleets. Formulated in compliance with DGCA requirements, Boeing Maintenance Planning Data (MPD D6-38278), MRBR recommendations, Certification Maintenance Requirements (CMRs), and Airworthiness Limitations (AWLs/CDCCLs), this document serves as the regulatory operational baseline for heavy maintenance planning, line transit handling, and structural integrity oversight.

File Details

  • Document Type: Continuous Airworthiness Maintenance Program (CAMP)
  • Document Number: MZ-TD-04-737
  • Revision / Date: Revision 40 (03 April 2013)
  • Operating Airline / Organization: PT Garuda Indonesia / GMF-AeroAsia Engineering
  • Applicable Aircraft: Boeing 737 Classic Series (B737-300, B737-400, B737-500)
  • Specified Fleet Effectivity: PK-GHW (B737-3M8, S/N 25039) and PK-GHX (B737-3L9, S/N 26440)
  • Powerplant Application: CFM56-3 Series Turbofans (CFM56-3B-2 on wing)
  • Format & Language: PDF / English

Program Structure & Letter Check Intervals

This technical program establishes strict standard intervals and release protocols across all minor and major checks:

  • Minor Inspections: Before Departure (BD) / Preflight (PF), Transit Walkaround Check (TR), and 24-Clock-Hour Daily Check (DY) under GA-Authorization release.
  • A-Check Base Interval: 500 Flight Hours (FH)
  • C-Check Base Interval: 5,000 Flight Hours (FH)
  • D-Check Heavy Overhaul Interval: 24,000 Flight Hours (FH)
  • Structural Sampling: S1 (24,000 FH at 1/2 fleet) and S2 (24,000 FH at 1/4 fleet) tracking corrosion and structural fatigue under Boeing CPCP and SSID guidelines.

Chapters Covered & Technical Systems Breakdown

Section 1 — Introduction & Regulatory Rules: Overhaul and check time limits, structural sampling programs (CPCP/SSID), Short Term Escalation rules (OpSpec Part D-76 limits), unscheduled maintenance instructions, Required Inspection Items (RII), and Reliability Program authorizations (MZ-TD-05).

Special Operational Requirements: Airworthiness Limitation Items (Fuel System AWLs/CDCCLs), Certification Maintenance Requirements (CMRs), Extended-Range Twin-Engine Operations (ETOPS/CMP), and Reduced Vertical Separation Minimum (RVSM) airframe critical items.

Section 2 — EDP Coding & Task Formatting: 10-digit CAMP item breakdown, MSG-3 categorization (Categories 5 through 9), and task code definitions (FUC, OPC, GVC, TVC, REM, RPL, SRV, LUB, SPC).

ATA 05 — Time Limits & Scheduled Line Checks: Routine walkaround inspections, transit checklists, and daily ground-handling certifications.

ATA 06 — Zonal Inspection Program: Complete internal and external zonal surveillance spanning Upper Fuselage (Zone 100), Flight Deck (Zones 101/102), Galleys & Lavatories (103/104/109/113/114), Passenger Cabin (107/108), Lower Nose Compartment & Radome (201/202), Wheel Wells (203/204/216/217), E/E Bay (205), AC Distribution & Equipment Bays (210/211/212/213/214), Wings (300/400), Engines & Nacelles (500/600), and Empennage/Tailcone/APU Bay (700 series).

ATA 08 — Weighing: Mandatory 4-year fleet weight and balance verification.

ATA 11 — Placards & Markings: Passenger cabin, emergency exit, baggage bin, and lavatory safety placard inspections.

ATA 12 — Servicing & Lubrication: CSD oil replenishment (250 FH) and drain/chip detector inspections (1,200 FH), APU lubrication, engine starter servicing, shock strut inflation (MIL-H-5606), flight control jackscrews, trailing edge flap tracks and carriages, leading edge slats, and landing gear pivot points.

ATA 20 — Standard Practices / Airframe & EZAP: Detailed visual inspections of Electrical Wiring Interconnection Systems (EWIS) under Enhanced Zonal Analysis Procedures, flight control cable wear/tension measurements, and primary structural bonding checks.

ATA 21 — Air Conditioning & Pressurization: Pressure controllers, recirculation fan filter replacements (P196555 / P199753), safety and vacuum relief valves, heat exchanger cleanings, and turbofan/air cycle machine shop visits.

ATA 22 — Autoflight: Autopilot servo actuator shear rivets, elevator PCU linkages, and yaw damper rudder pressure reducer operational tests.

ATA 23 — Communications: CVR readouts, ULB battery expirations, static discharger resistance tests, and ELT self-tests.

ATA 24 — Electrical Power: Generator drive systems, CSD filter replacements, external power receptacle pin wear checks, main aircraft battery shop bench testing, and standby power functional runs.

IMAGES PREVIEW

Boeing 737-300, 737-400, 737-500 Continuous Airworthiness Maintenance Program (CAMP Rev 40) — PDF page 1 preview
Boeing 737-300, 737-400, 737-500 Continuous Airworthiness Maintenance Program (CAMP Rev 40) — PDF page 4 preview
Boeing 737-300, 737-400, 737-500 Continuous Airworthiness Maintenance Program (CAMP Rev 40) — PDF page 14 preview

ATA 25 — Equipment & Furnishings: Flight crew seat rails/locks, passenger seating, cargo compartment liners and barrier nets, and emergency slide/megaphone inspections.

ATA 26 to ATA 80 — Systems, Powerplant & Structures: In-depth maintenance job allocation tables across fire protection, hydraulics, landing gear, fuel feed and storage, pneumatics, flight control actuators, CFM56-3 on-wing powerplants, and GTCP 85-129 APU modules.

By compiling every scheduled task, interval, zone access panel, part reference, and engineering authorization note, this comprehensive maintenance program gives airline operators, MRO planning engineers, and licensed maintenance technicians the definitive blueprint for airworthiness compliance.

Instant Professional Access
Ensure total regulatory compliance and flawless scheduled maintenance operations with the Boeing 737-300, 737-400, 737-500 Continuous Airworthiness Maintenance Program (CAMP Rev 40). Whether planning base overhaul visits, setting up line transit check routines, or auditing structural inspection task cards, having verified engineering data is critical for flight safety. Download your copy immediately following checkout—delivered instantly with no waiting, fully printable, and viewable across any computer, tablet, or mobile device.

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