0% found this document useful (0 votes)
95 views6 pages

05 00 00 in

The Gulfstream GVI (G650) Maintenance Manual outlines the maintenance program to ensure compliance with FAA regulations, providing flexibility for operators. It includes detailed sections on time limits, airworthiness limitations, scheduled maintenance, and special inspection requirements, along with guidance for engine maintenance programs. Operators are advised to follow the recommended inspection tasks and consult the relevant documents for maintaining airworthiness and reliability.

Uploaded by

williamzelepukin
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF, TXT or read online on Scribd
0% found this document useful (0 votes)
95 views6 pages

05 00 00 in

The Gulfstream GVI (G650) Maintenance Manual outlines the maintenance program to ensure compliance with FAA regulations, providing flexibility for operators. It includes detailed sections on time limits, airworthiness limitations, scheduled maintenance, and special inspection requirements, along with guidance for engine maintenance programs. Operators are advised to follow the recommended inspection tasks and consult the relevant documents for maintaining airworthiness and reliability.

Uploaded by

williamzelepukin
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF, TXT or read online on Scribd
You are on page 1/ 6

MAINTENANCE MANUAL

TIME LIMITS / MAINTENANCE CHECKS


1. Time Limits / Maintenance Checks — General
A. Introduction
This maintenance program has been prepared by Gulfstream Aerospace Corporation to provide
operators with all information necessary to comply with Federal Aviation Administration (FAA)
requirements of Part 91, Subpart E, Section 91.409, paragraph (f)(3), Part 125, Subpart G, Section
125.247, paragraph (e)(2) and Part 135, Subpart J, Section 135.421, paragraph (a) of the Federal
Aviation Regulations. Additionally, the information contained herein will enable operators to comply
with the requirements of Part 91, Subpart E, Section 91.409, paragraph (f)(4) and Part 135, Subpart
J, Section 135.411, paragraph (a)(2) to construct a suitable maintenance program.
Gulfstream has prepared the Gulftream GVI (G650) maintenance program with the intent of
providing the maximum amount of flexibility for the aircraft operator. The Aircraft Maintenance
Manual (AMM) Chapter 5 contains all requirements of the MSG-3 derived Maintenance Review
Board (MRB) Report, in addition to Gulfstream recommended inspections.
Active customer bulletins are part of Gulfstream’s recommended inspection program and are listed
in the Customer Bulletin Index.
NOTE: For customer bulletin description see Section 05-30-00 Special Inspection Requirements.
Unless otherwise noted, references to ASCs or CBs in chapter 5 apply to the initial release and
subsequent revisions of the identified ASC or CB.
A complete glossary of terms and definitions applicable to the Gulftream GVI (G650) Scheduled
Maintenance Program can be found in the Maintenance Review Board Report section of this
chapter.
Lubrication requirements specified in this section do not represent the total lubrication provisions for
the aircraft. See Chapter 12 - Servicing and appropriate manufacturer maintenance publications for
additional lubrication recommendations.
Aircraft based, or frequently operating, in a tropical zone, high humidity area, marine environment or
area of high industrial pollution should be inspected more frequently.
In order to maintain a sterile potable water system, intervals for water system sterilization should be
established by each operator based upon their operating environment, water servicing resources
and in-service experience.
B. Engine Programs
The Rolls-Royce BR700-725A1-12 MRB Report engine program is an on-wing program only.
On-wing engine maintenance tasks and instructions are provided in the Aircraft Maintenance
Manual. In addition, operators must consult the Rolls-Royce Time Limits Manual (TLM), Publication
Ref. T-725-7BR Airworthiness Limitations Section (ALS) to maintain the continued airworthiness of
the engine.
An operator may use either the “Task Oriented” maintenance program listed in this chapter or a
manufacturer’s “Hard Time” program under the following engine manufacturer recommendations:
NOTE: “Task Oriented” is sometimes referred to as “On Condition”. “Hard Time” is sometimes
referred to as “Fixed Interval”.
• Operators using the Task Oriented Maintenance Program contained in AMM Chapter 5 and
the MRB Report may refer to Rolls Royce Generic EMP document, BR725 Engine for G650
- “Engine Management Programme ‘Task Oriented’ Operated Engines” for the Rolls-Royce
minimum recommended work package.

05-00-00
Page 1
October 30/24
MAINTENANCE MANUAL

• Operators using the manufacturer’s Hard Time Program may refer to Rolls Royce Generic
EMP document, BR725 Engine for G650 - “Engine Management Programme ‘Hard Time’
Operated Engines” for the Rolls-Royce minimum recommended work package.
• Operators who choose to transition from one maintenance program to the other, should
consult the appropriate Rolls-Royce EMP document for guidance.
At first “A” Check after entry into service, the operator is required to declare which engine
maintenance program they intend to follow with their local regulatory authority.
C. Time In Service
With respect to maintenance time records, time in service means the time from which an aircraft
leaves the surface of the earth until it touches again at the next point of landing.
NOTE: For the purposes of tracking maintenance requirements, the terms cycles and landings are
equivalent.
D. Subsections within the Time Limits / Maintenance Checks Section
• Time Limits
• Airworthiness Limitations
• Scheduled Maintenance
• Maintenance Review Board Report
• Special Inspection Requirements
• Unscheduled Maintenance Checks
E. Description of the Subsections
(1) Time Limits 05-10-00
This section provides initial inspection requirements for the following items:
• Manufacturer Recommended Items, Restore / Discard
• Fire Extinguisher Bottle Maintenance Schedule
• Emergency Blow-down Bottle Maintenance Schedule
• Oxygen Bottle Maintenance Schedule
(2) Airworthiness Limitations 05-10-10
This section provides FAA / EASA Airworthiness Limitations Instructions for Life Limited
Components and Principal Structural Element Inspection Requirements.
NOTE: Principal Structural Elements Inspection results, both positive and negative should
be returned to Gulfstream Maintainability Engineering, FAX 912-965-4704 or email
results to maintainability.engineering@gulfstream.com.
This section also provides Certification Maintenance Requirements (CMRs).
(3) Scheduled Maintenance 05-20-00
This section provides recommended scheduled maintenance for the following:
• Systems and Powerplant Program
• Structural Inspection Program
• Zonal Inspection Program
• Enhanced Zonal Inspection Program
• High Intensity Radiated Fields / Lightning (HIRF/L)
(4) Maintenance Review Board Report 05-22-00

05-00-00
Page 2
October 30/24
MAINTENANCE MANUAL

This section provides the MSG-3 derived, FAA / EASA approved MRB Report, which details
the minimum scheduled maintenance / inspection requirements necessary to construct a
maintenance program that complies with FAA / EASA regulatory requirements.
(5) Special Inspection Requirements 05-30-00
This section provides the current listing of Alert Customer Bulletins and Customer Bulletins.
(6) Unscheduled Maintenance Checks 05-50-00
This section outlines maintenance checks and inspections which are required as a result of
abnormal conditions encountered during aircraft ground handling, takeoff / landing or airborne
incidents.
F. Manufacturer Recommended Inspection Program Tasks
Manufacturer Recommended Inspection Program (MRIP) tasks are derived external to the MSG-3
process and reflect Gulfstream’s recommendations for enhanced reliability and economic benefit.
MRIP tasks may be in addition to or have a more frequent interval than an MRB task.
Table 1 lists the MRIP tasks contained within AMM Chapter 5 as well as their history. Refer to the
applicable Chapter 5 section for task intervals.

Table 1: MRIP Table


Chapter 5 CMP
Description MRIP History
Reference Reference
05-10-00 Task deleted. 262106 May 2024 - Task deleted.
262107
05-10-00 Task deleted. 262404 May 2024 - Task deleted.
262410
262416
262422
262428
262434
262440
262446
05-10-00 Aileron HA Manifold - Discard 271360 December 2012 - Gulfstream
271361 Engineering added requirement as a
result of qualification testing.
05-10-00 Aileron EHSA Manifold - Discard 271362 December 2012 - Gulfstream
271363 Engineering added requirement as a
result of qualification testing.
05-10-00 Rudder HA Manifold - Discard 272314 December 2012 - Gulfstream
Engineering added requirement as a
result of qualification testing.
05-10-00 Rudder EHSA Manifold - Discard 272315 December 2012 - Gulfstream
Engineering added requirement as a
result of qualification testing.

05-00-00
Page 3
October 30/24
MAINTENANCE MANUAL

Table 1: MRIP Table


Chapter 5 CMP
Description MRIP History
Reference Reference
05-10-00 Flap Hydraulic Control Module - 275507 December 2012 - Gulfstream
Discard Engineering added requirement as a
result of qualification testing.
05-10-00 Left System Manifold Filter - Discard 291487 2012 ISC - Gulfstream Engineering
thru added requirement as a result of
291492 qualification testing.
05-10-00 Right System Manifold Filter - Discard 291525 2012 ISC - Gulfstream Engineering
thru added requirement as a result of
291527 qualification testing.
05-10-00 Auxiliary Hydraulic Pump Manifold 292511 2012 ISC - Gulfstream Engineering
Filter - Discard added requirement as a result of
qualification testing.
05-20-00 Wing Anti-ice Temperature Switch - 301137 February 2011 - G650 ISC Meeting -
Temperature Trip Point Functional Added to align task interval with other
Check maintenance procedures in the same
zones.
05-10-00 Nose Landing Gear Middle Electrical 322618 November 2016 - Gulfstream
Harness - Discard Engineering added requirement as a
result of qualification testing.
05-10-00 Main Landing Gear Door Actuator - 323209 December 2012 - Gulfstream
Discard 323210 Engineering added requirement as a
result of qualification testing.
05-10-10 Brake Inlet Self-Sealing Coupling 324314 November 2015 - Requirement added
Re-torque - Restore thru to address compliance with ACB 4
324317 and ACB 4A.
05-10-00 Nose Landing Gear Down and Lock 322603 November 2016 - Gulfstream
Harness - Discard Engineering added requirement as a
result of qualification testing.
05-10-00 Task deleted. 351203 May 2024 - Task deleted.
05-10-00 Task deleted. 352303 May 2024 - Task deleted.
05-10-00 Task deleted. 353102 May 2024 - Task deleted.
353106
05-10-10 HP Stage 5 Air Nonreturn Valve - 361110 August 2013 - Requirement added to
Restore 361111 address valve corrosion.
05-10-00 Main Entrance Door Damper - Discard 521410 December 2012 - Gulfstream
Engineering added requirement as a
result of qualification testing.

05-00-00
Page 4
October 30/24
MAINTENANCE MANUAL

Table 1: MRIP Table


Chapter 5 CMP
Description MRIP History
Reference Reference
05-20-00 Radome to Structure Perimeter Steps 531036 August 2012 - Gulfstream
- Detailed Inspection Maintainability Engineering added
requirement to meet operator RVSM
flight operations requirements.
05-20-00 Baggage Compartment Below Floor 534001 June 2013 - Gulfstream Maintainability
HIRF/L - Detailed Inspection added 4C interval for task / calendar
alignment.
05-20-00 Horizontal Stabilizer Pivot Fitting - 551502 May 2023 - Inteval reduced via MRIP
Detailed Inspection to align with 55.30.00 / 04 due to
service experience of corrosion at the
horizontal stabilizer and vertical
stabilizer interface.
05-20-00 Wing Tank (Internal) BL 0 - RBS 135 - 571027 February 2011 - G650 ISC Meeting -
Detailed Inspection 571028 Added to align task interval with other
maintenance procedures in the same
zones.
05-20-00 Wing Tank (Internal) RBS 135 - WS 571029 February 2011 - G650 ISC Meeting -
551 - Detailed Inspection 571030 Added to align task interval with other
maintenance procedures in the same
zones.
05-20-00 Flap Upper Surface - Detailed 575301 June 2012 - Gulfstream Fatigue and
Inspection 575302 Damage Tolerance Engineering added
requirement as a result of fatigue
testing.
05-20-00 Nacelle, T/Rev and Exhaust External 710035 June 2012 - G650 ISC Meeting -
(Viewed From Platform) - Zonal 710036 Added to align task interval with other
Inspection maintenance procedures in the same
zones.
05-20-00 Engine Maintenance Program 710039 September 2013 - Gulfstream
Declaration Maintainability added “One time
inspection” task in 1A Check
Scheduled Maintenance Table per
review.
05-20-00 Engine Internal - Zonal Inspection 711002 June 2012 - G650 ISC Meeting -
711003 Revised task interval to incorporate
Low-Utilization Maintenance Program
(LUMP) into the Aircraft Maintenance
Manual (AMM) Chapter 5.

05-00-00
Page 5
October 30/24
MAINTENANCE MANUAL

Table 1: MRIP Table


Chapter 5 CMP
Description MRIP History
Reference Reference
05-20-00 T/Rev HIRF/L - Detailed Inspection 783114 June 2012 - G650 ISC Meeting -
783115 Added to align task interval with other
maintenance procedures in the same
zones.

05-00-00
Page 6
October 30/24

You might also like