' 

Gulfstream 

DOCUMENT NO: .;_....;:;....;:;;.;..;.....: -9:....:9....:...3 ____ FAA PROJECT NO: N/A 

CURRENT REVISION: ....:.A.:.::s;..,;N...:..:o:..:.te=..:d=------INITIAL DATE: AUG, 28, 2008 

GAC CAGE CODE: 59734 MODEL: GV, GSOO, G550 

VENDOR REFERENCE: N/A ATA NO: 05 

CERTIFICATION DATA TOP ASSEMBLY NO (if applicable): _:N....::./.:....:A ____ _ _ 

Summary Of Changes To The GV Series Airworthiness Limitations 

DEPARTMENT: Stress 

SECTION: FDT 

PREPARED BY: K. Jones 

CHECKED BY: M. Villar 

PROPRIETARY OTI ~ 

THIS DATA AND INFORMATION DISCLOSED HEREIN IS 

PROPRIETARY DATA OF GULFSTREAM AEROSPACE 

CORPORATION. NEITHER THIS DATA NOR THE DATA 

CONTAINED HEREIN SHALL BE REPRODUCED, USED OR 

DISCLOSED TO OTHERS WITHOUT THE WRITTEN 

AUTHORIZATION OF GULFSTREAM AEROSPACE CORP. 

TECHNICAL APPROVAL: 

TECHNICAL APPROVAL: 

PROJECT ENGINEER: 

MANAGER APPROVAL: 

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M~}!. 1

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Gulfstream 

REVISION APPROVAL 

REV REVISED BY APPROVED BY SIGNATURES DATE 

- - - - -

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DOCUMENT NO. GV-GER-9973 CAGE CODE 59734 PAGE i REV As No -\Ed 
Gulfstream 

REVISION HISTORY 

REV PARA DESCRIPTION OF CHANGE 

- - Initial Release, No Change (NC) 

A 1.0 Updated Revision levels in Section 1.0. 

2.0 Minor wording changes to Section 2.0. 

5.0 Updated table in Section 5.0. 

6.0 Added 6.0 heading and updated inspection interval and affected aircraft information in tables. 

8 4.0 Removed SIN's for aircraft not covered by STC. Changed project numbers to STC numbers. 

5.0 Split FAA and EASA life limits into separate sections. Added missing components. 

6.0 Added missing/older PSE requirements. Changed wording per FAA comments. 

c 5.0 Added references to AMM procedures. 

6.0 Added references to AMM procedures. 

For PSE 55-11-300, changed "New Replacement Requirement" to "New Replace/Restore 

Requirement". 

DOCUMENT NO. GV-GER-9973 CAGE CODE 59734 PAGE ii REVC 
Gulfstream 

TABLE OF CONTENTS 

1.0 INTRODUCTION ......................................................................................................................................... 1 

2.0 DISCUSSION .............................................................................................................................................. 1 

3.0 REPAIRS AND MODIFICATIONS ............................................................................................................. 2 

4.0 EXCLUDED AIRCRAFT DUE TO SPECIAL OPERATION OR MODIFICATIONS ................................... 2 

5.0 LIFE LIMITED COMPONENTS .................................................................................................................. 3 

6.0 PSE INSPECTION INTERVALS ................................................................................................................. 6 

DOCUMENT NO. GV-GER-9973 CAGE CODE 59734 PAGE iii REV C 
Gulfstream 

1.0 INTRODUCTION 

The following provides a summary of changes to the structural aspects of the Airworthiness Limitations 

Section (ALS) of the GV series maintenance manual (Chapter 05-1 0-1 0). This summary is intended to 

alert operators to revisions to the ALS where new structural inspections for Principal Structural Elements 

(PSE) have been added or existing inspection inteNals have been reduced from those previously 

published. 

The primary users of this summary are FAR Part 121 and 135 operators who have approved 

maintenance programs that differ from those specified in the Gulfstream published maintenance manuals. 

Operators who use the Gulfstream maintenance manuals (FAR 43.16 and 91.403) will automatically 

comply with these requirements when they incorporate the revision shown below: 

GV Series AMM: Revision 43 or later FAA approved revision 

G500 Series AMM: Revision 24 or later FAA approved revision 

G550 Series AMM: Revision 24 or later FAA approved revision 

2.0 DISCUSSION 

Gulfstream has completed a significant structural test program for the GV series aircraft. The results of 

these tests and associated analysis indicate changes to the damage tolerance based structural inspection 

program and component life-limits are warranted. 

Additionally, Gulfstream is adding a reference to normal maintenance inspections that are required to 

prevent failure of critical structures due to corrosion, fatigue or accidental damage. These are identified 

by a reference to the Maintenance Review Board (MRB) inspection number for each GV series aircraft. 

These inspections cannot be changed without FAA concurrence. 

The MRB report is based on an average airplane utilization of 1000 flight hours, 500 flight cycles 

(landings), within 12 months (calendar) time. Operators whose airplane utilization differs significantly from 

these parameters will need to reevaluate the inteNals in this report with their local Regulatory Authority. 

Included in the tables below are changes to the Life Limited Components and PSE Inspections sections 

of the ALS. Unless specifically listed in Section 4.0, aircraft serial numbers that fall within the "Affected 

Serial Numbers" range for each inspection are required to either update their maintenance program with 

the new inteNals or update their maintenance manuals to the latest revision as given in Section 1 of this 

report. 

DOCUMENT NO. GV-GER-9973 CAGE CODE 59734 PAGE 1 REVC 
Gulfstream 

3.0 REPAIRS AND MODIFICATIONS 

The certification basis for the GV has required a damage tolerance assessment for all repairs since the 

original type certificate was issued. The primary means of identifying critical structure is through the ALS 

section of the AMM. Therefore operators are required to review their aircraft history to determine if there 

are any repairs or modifications which would impact these inspections. These would typically be a repair 

or modification to a Principal Structural Element (PSE) that required a special damage tolerance based 

inspection be added to the maintenance program. If this condition arises, additional review and approval 

may be required. 

The following are some guidelines for individual PSE's to assist in determining if further review is 

required. 

Fuselage Skin Repairs: Internal repair doublers and external doublers that cover no more than 1 

stringer/frame bay are covered by PSE 53-31-100. No additional review is required. For external 

doublers greater than 1 stringer/frame bay, no additional review is required if there already is a special 

damage tolerance based inspection approved for the repair or modification. 

Antennas: Any antenna or similar device is covered by PSE 53-21-201 as long as the operator inspects at 

the intervals published in this report. Additional review would be required if the operator desired to use 

another interval. 

4.0 EXCLUDED AIRCRAFT DUE TO SPECIAL OPERATION OR MODIFICATIONS 

The following aircraft are excluded from this report because of their special utilization or modifications. 

These aircraft have an individual damage tolerance based program that has been approved through a 

separate analysis. 

• ST02932AT 

• ST03056AT 

• ST03315AT 

• ST03399AT 

• ST03615AT 

DOCUMENT NO. GV-GER-9973 CAGE CODE 59734 PAGE 2 REV C 
Gulfstream 

5.0 LIFE LIMITED COMPONENTS 

The following are changes to the life limits of the main landing gear, nose landing gear, and fuselage components 

due to additional testing and redesign of parts. The aircraft effectivity reflects the original production configuration 

and is provided for reference only. Tracking of replacement parts should be based on the part number. 

5.1 Fuselage Life Limits 

Fuselage 

Nomenclature PIN Life Limit Affected SIN's 

AMM Reason for 

Reference Char')ge 

Cockpit Center Post 1159BM50024 16,000 Ldgs 501-699, 53-17-00 New Limit 5001 -5084 

Cockpit Side Post 1159BM50025-11, 10,000 Ldgs 501 - 599 53-17-00 New Limit -12,-13,-14,-15,-16 

Cockpit Side Post 1159BM50025-1, 16,000 Ldgs 600-699, 53-17-00 New Limit -2,-3,-4,-5,-6 5001 -5084 

Cockpit Lower Rail 1159BM50033 15,000 Ldgs 501 -699, 53-17-00 New Limit 5001-5084 

Cockpit Pressure Floor 1159850042-61 12,000 Ldgs 501 -633 53-10-00 New Limit Anqle 

1159BM50913-13, 

FS465 Main Frame -14,-15,-16 16,000 Ldgs 505-699, 53-34-00 New Limit Fittings 1159BM50914-13, 5001-5084 

-14,-15,-16 

1159BM50915-17, 

FS576 Main Frame -18,-19,-20 16,000 Ldgs 505-699, 53-34-00 New Limit Fittings 1159BM50916-17, 5001-5084 

-18,-19,-20 

5.2 FAA Landing Gear Life Limits 

Nomenclature PIN Life Limit Affected SIN's 

AMM Reason for 

Reference Chanqe 

Main Landing Gear- FAA Certification 

Shock Strut Cylinder 1159LM50112-11 5,000 Ldgs 501 - 547 32-12-01 New Limit Nut 

Shock Strut Cylinder 1159LM50112-13 20,000 Ldgs 548-699, 32-12-01 New Limit Nut 5001 -5084 

Aft Trunnion (Fuse) 1159SCL566-13 20,000 Ldgs 501 , 32-15-01 New Limit Pin 504-548 

Side Brace Assembly 1159SCL502 20,000 Ldgs 501-699, 32-14-01 New Limit 5001-5131 

Nose Landing Gear- FAA Certification 

NLG Retract Actuator 1159HM40120-1 & 6,470 Ldgs 501-699 32-38-03 New Limit Rod End -7 5001-5025 

NLG Retract Actuator 1159SCL567 -3 25,000 Ldgs 501-699, 32-38-03 New Limit Rod End 5026-5084 

Shock Strut Cylinder 1159LM50700-3 18,400 Ldgs 501 - 544 32-22-01 New Limit 

DOCUMENT NO. GV-GER-9973 CAGE CODE 59734 PAGE3 REVC 

c 
Gulfstream 

Nomenclature PIN Life Limit Affected SIN's 

AMM Reason for 

Reference Change 

Shock Strut Cylinder 1159LM50700-5 20,000 Ldgs 545-699, 32-22-01 New Limit 

5001-5084 

Steering Collar 1159SCL500-23 20,000 Ldgs 501-699, 32-52-03 New Limit 5001-5084 

NLG Axle Assembly 1159LM50521 32,750 Ldgs 501-699 32-23-00 New Limit Piston 5001 -5084 

NLG Upper Torque 1159LM50548 32,750 Ldgs 504-535 32-22-03 New Limit 

Arm 

NLG Lower Torque 1159LM30553 32,750 Ldgs 504-535 32-22-05 New Limit Arm 

NLG Truss Brace Pin 1159LM40565 20,000 Ldgs 501-699 32-24-05 New Limit 5001 -5084 

NLG Actuator Attach 1159LM40583 32,750 Ldgs 501-699 32-38-03 New Limit 

Pin 5001-5084 

5.3 EASA Landing Gear Life Limits 

Nomenclature PIN Life Limit Affected SIN's AMM Reason for 

Reference Change 

Main Landing Gear - EASA Certification 

Side Brace Assembly 1159SCL502 16,000 Ldgs 541 -699, 32-14-01 New Limit 5001-5131 

MLG Strut Assembly 1159L50001 16,000 Ldgs 541-612 32-10-00 New Limit 

MLG Structural Post 1159LM50126 16,000 Ldgs 541 - 612 32-10-00 New Limit 

MLG Axle Fitting 1159LM50140 16,000 Ldgs 541-612 32-13-01 New Limit c 

MLG Shock Absorber 1159L50100 16,000 Ldgs 541 -612 32-12-01 New Limit 

MLG Shock Strut 1159LM50112-11 4,000 Ldgs 541-547 32-12-01 New Limit Cylinder Nut 

MLG Shock Strut 1159LM50112-13 16,000 Ldgs 548-699 32-12-01 New Limit Cylinder Nut 

MLG Trunnion Pin 1159LM50853 16,000 Ldgs 541 -612 32-15-01 New Limit 

MLG Aft Trunnion 1159SCL566-13 16,000 Ldgs 541-612 32-15-01 New Limit Fuse Pin 

MLG Spindle Pins 1159LM50137 16,000 Ldgs 541-612 32-14-03 New Limit 

MLG Side Brace 1159LM50164 16,000 Ldgs 541-612 32-14-03 New Limit Lower Attach Pin 

MLG Axle Fitting 1159LM50148 16,000 Ldgs 541-612 32-13-01 New Limit 

Attach Pin 

MLG Shock Strut 1159LM5014 7 16,000 Ldgs 541 -612 32-12-01 New Limit Attachment Pin 

Nose Landing Gear - EASA Certification 

NLG Retract Actuator 1159HM40120-1 & 5,170 Ldgs 541-699 32-38-03 New Limit 

Rod End -7 5001-5025 

NLG Retract Actuator 1159SCL567 -3 20,000 Ldgs 541 -699, 32-38-03 New Limit 

Rod End 5026 - 5084 

DOCUMENT NO. GV-GER-9973 CAGE CODE 59734 PAGE4 REVC 
Gulfstream 

Nomenclature P/N Life Limit Affected SIN's 

AMM Reason for 

Reference Change 

Steering Collar 1159SCL500-23 16,000 Ldgs 541 -699, 32-52-03 New Limit 5001 - 5084 

NLG Assembly 1159L50004 26,200 Ldgs 541 - 612 32-20-00 New Limit 

NLG Trunnion 1159LM50690 18,200 Ldgs 541 -612 32-24-01 New Limit 

NLG Truss Brace 1159L50801 26,200 Ldgs 541 -612 32-24-05 New Limit Assembly 

NLG Axle Assembly 1159LM50521 26,200 Ldgs 541 - 612 32-23-00 New Limit Piston 

NLG Upper Torque 1159LM50548 26,200 Ldgs 541 - 612 32-22-03 New Limit Arm 

NLG Lower Torque 1159LM30553 26,200 Ldgs 541-612 32-22-05 New Limit Arm 

NLG Shock Strut 1159L50500 16,000 Ldgs 541 - 612 32-22-01 New Limit 

NLG Shock Strut 1159LM50700-3 10,200 Ldgs 541 -544 32-22-01 New Limit Cylinder Assembly 

NLG Shock Strut 1159LM50700-5 16,000 Ldgs 545-699 32-22-01 New Limit Cylinder Assembly 

NLG Drag Brace 1159LM50585 26,200 Ldgs 541-612 32-24-03 New Limit c 

NLG Truss Brace Pin 1159LM40565 16,000 Ldgs 541-612 32-24-05 New Limit 

NLG Trunnion Pin - 1159LM50611 26,200 Ldgs 541-612 32-25-01 New Limit Left 

NLG Trunnion Pin - 1159LM50613 26,200 Ldgs 541-612 32-25-01 New Limit Right 

NLG Upper Drag 1159LM40588-19 4,000 Ldgs 541-612 32-24-03 New Limit Brace Pin 

NLG Lower Drag 1159LM50587 16,000 Ldgs 541-612 32-24-03 New Limit Brace Pin 

NLG Actuator Attach 1159LM40583 26,200 Ldgs 541 -699 32-38-03 New Limit Pin 

NLG Strut/Trunnion 1159LM50568 16,000 Ldgs 541 -612 32-25-01 New Limit Pin 

DOCUMENT NO. GV-GER-9973 CAGE CODE 59734 PAGES REVC 
Gulfstream 

6.0 PSE INSPECTION INTERVALS 

The following are required changes to PSE inspection intervals and affected serial numbers for each change. 

Fuselage Inspections 

AMM Initial Recurring Inspection Affe

Location PSE Reference Inspection Inspection Method Se

(Landings) (Landings) Num

NLG Trunnion Fitting Lug 32-25-001 32-24-01 16,000 6,000 Eddy Current 501 ' 5

Cockpit Window Skins 53-11-101 53-11-00 6,400 3,200 Eddy Current 501' 5

NLG Skin Cutout 53-11-200 53-10-00 8,000 4,650 Eddy Current 501

NLG Skin Cutout 53-11-200 53-10-00 8,000 8,000 Eddy Current 531 

5001

FS 119 Frame 53-12-003 53-12-00 MRB 53.12.04/01 501' 5FS63 Pressure Bulkhead 53-12-004 53-12-00 MRB 53.12.02/01 501 

5001

Cockpit Pressure Floor 53-15-100 53-10-00 MRB 53-100-04 & -05 501 

5001 

Side Post, Upper Attachment 53-17-003 53-17-00 8,000 2,900 Eddy Current 501

5001 

Side Post, Lower Attachment 53-17-004 53-17-00 5,000 1,100 Eddy Current 501

Side Post, Lower Attachment 53-17-004 53-17-00 6,100 1,300 Eddy Current 600

5001

Center Post, Lower Attachment 53-17-005 53-17-00 6,300 1,000 Eddy Current 501

6

Cockpit Crossbeam (GV-SP) 53-17-008 53-10-00 12,000 3,500 Eddy Current 5001 

Lower Cockpit Rail at Side Post 53-17-202 53-17-00 5,000 1,100 Eddy Current 501 

Lower Cockpit Rail at Side Post 53-17-202 53-17-00 6,100 1,300 Eddy Current 600

5001 

--- --

DOCUMENT NO. GV-GER-9973 CAGE CODE 59734 PAGE S 
Gulfstream 

AMM Initial Recurring Inspection Affe

Location PSE Reference Inspection Inspection Method Se

(Landings) (Landings) Num

Fuselage Penetrations 53-21-201 53-00-00 8,000 4,000 Visual 501

(Antennas) 5001

501 

Longitudinal Skin Splices 53-21-403 53-00-00 See PSE 53-31-100 5

5001

Fuselage Stability Frames 53-22-101 53-00-00 See PSE 53-31-100 501 

5001

FS 193 Frame 53-22-102 53-22-00 8,000 8,000 Eddy Current 501 , 5

FS193/ FS229 Floor Beams 53-25-101 53-25-00 8,000 8,000 Eddy Current 501 -6

Fuselage Skins 53-31-100 53-00-00 800 Landings 800 Landings Visual 501

2,000 Hours<1> 2,000 Hours<1> 5001

FS465/ FS576 Production 53-31-301 53-00-00 See PSE 53-31-100 501 

Splices 5001 

Circumferential Skin Splices 53-31-302 53-00-00 See PSE 53-31-100 501

5001 

Fuselage Skins At Wing Pressure 53-31-303 53-31-00 8,000 2,300 X-Ray 501

Box Cutout (GV) 

Fuselage Skins At Wing Pressure 53-31-303 53-31-00 8,000 Box Cutout (GV-SP) 2,500 X-Ray 5001

FS426 Bulkhead (GV) 53-32-101 53-32-00 12,000 2,300 Eddy Current 501

FS426 Bulkhead (GV-SP) 53-32-101 53-32-00 12,000 2,500 Eddy Current 5001

FS 465 Frame at Stringer 9 and 53-32-302 53-32-00 5,400 2,700 Eddy Current 501 

Below 5

FS 576 Frame 53-32-303 53-32-00 8,000 8,000 Eddy Current 501 

5

Window Surround Frame Splices 53-32-305 53-32-00 4,800 2.400 Eddy Current 501 

5

DOCUMENT NO. GV-GER-9973 CAGE CODE 59734 PAGE 7 
Gulfstream 

AMM Initial Recurring Inspection Affe

Location PSE Reference Inspection Inspection Method Se

(Landings) (Landings) Num

FS758 Bulkhead- Below Floor 53-32-401 53-42-03 7.400 3,400 Eddy Current 501

5001 

Stringer Splices at FS684 & 53-33-101 53-00-00 See PSE 53-31-100 501 

FS758 5001

Dorsal Tee 53-33-102 53-33-00 14,000 4,000 Eddy Current 507

5

Longerons 7 and 15 at FS576 53-33-103 53-33-00 8,000 4,000 Visual 501

5001

Longeron 22 53-33-107 53-23-00 12,000 4,000 Visual 501

5001

Longeron 24 53-33-108 53-43-00 MRB 53.33.00/01 501

5001

Forward Outboard Wing to 53-34-101 53-34-00 MRB 53-100-10 501

FuselaQe FittinQ (Link) 5001

Forward Wing To Fuselage 53-34-200 53-34-00 8,000 1,900 Eddy Current 501Fitting (GV) Forward Wing To Fuselage 53-34-200 53-34-00 7,500 1,400 Eddy Current 5001

FittinQ (GVSP) 

Aft Outboard Wing to Fuselage 53-34-301 53-34-00 MRB 53-100-10 501

Fitting (Link) 5001 

Over-Wing Drag Beam 53-34-501 53-34-00 8,000 8,000 Visual 501

5001 

BL6 Forward Wing to Fuselage 53-34-601 53-34-00 8,000 5,400 Visual 501

Attachment (GV) 

BL6 Forward Wing to Fuselage 53-34-601 53-34-00 8,000 8,000 Visual 5001

Attachment (GV-SP) 

Torque Box 53-34-701 53-30-00 MRB 53.34.03/01 501

5001

BL6 Aft Wing to Fuselage Fittings 53-34-704 53-30-00 MRB 53.34.03/01 501

5001 

Pressure Floor Frame Clips 53-35-003 53-35-00 4,800 4,800 Visual 501 

Pressure Floor Frame Clips 53-35-003 53-35-00 6,800 4,800 Visual 600

5001 

Pressure Floor Composite Floor 53-35-004 53-30-00 MRB 53.25.00B/01 501

Boards (FS426-FS632) --- 5001 

DOCUMENT NO. GV-GER-9973 CAGE CODE 59734 PAGES 
Gulfstream 

AMM Initial Recurring Inspection Affe

Location PSE Reference Inspection Inspection Method Se

(Landings) (Landings) Num

FS426 Floor Beam Clips 53-35-005 53-35-00 2,500 2,500 Visual 501-6

BL 6 Breather Beam at FS 570 53-35-100 53-45-00 1,300 1,300 Visual 501

Cabin Window Rings 5 & 6 (GV) 53-37-101 B 53-37-00 6,000 2,500 Eddy Current 501

Cabin Window Rings 6 & 7 (GV- 53-37-101B 53-37-00 4,700 1,800 Eddy Current 5001

SP) 

Baggage Door Fittings 53-38-101 53-43-00 1,700 1,700 Visual 501

6

501

Mid-Fuselage Exposed Cutouts 53-38-201 53-00-00 See PSE 53-31-100 5001

FS465 Wing Link Cutout (GV) 53-38-203 53-34-00 8,000 1,250 Eddy Current 501 

FS465 Wing Link Cutout (GV-SP) 53-38-203 53-34-00 8,000 900 Eddy Current 5001

FS758 Composite Pressure 53-42-101 53-42-03 72 Months 72 Months Visual 501

Bulkhead 5001

Stringer Splice at FS820 53-43-102 53-00-00 See PSE 53-31-100 501

5001

Fin to Fuselage Attachments 53-46-001 53-56-00 8,000 8,000 Visual 501 , 

5

FS 820 Bulkhead 53-47-001 53-52-00 8,000 8,000 Eddy Current 501

5001

Forward Upper Bulkhead Fitting 53-47-201 53-57-00 5,000 2,000 Eddy Current 501

Rudder Actuator Attachment 53-48-001 53-50-00 3,600 3,600 Visual 501 

Aft Fuselage Belly Access 53-49-101 53-00-00 See PSE 53-31-100 501

Cutouts 5001

Aft Fuselage Cutouts- Exposed 53-49-202 53-00-00 See PSE 53-31 -100 501 

To Exterior 5001 

Aft Fuselage Cutouts- Covered 53-49-203 53-50-00 8,000 I 4,750 I Eddy Current 501 

By Fairings (GV) 

DOCUMENT NO. GV-GER-9973 CAGE CODE 59734 PAGE 9 
Gulfstream 

Initial Recurring Inspection Affe

Location PSE AMM Inspection Inspection Se

Reference (Landings) (Landings) Method Num

Aft Fuselage Cutouts- Covered 53-49-203 53-50-00 8,000 3,200 Eddy Current 5001

By Fairinqs (GV-SP) 

Eddy 

4,200 CurrenUMag 501

Engine Attach Pins 54-53-001 71-20-00 10,200 Particle/ 5001

Ultrasonic 

Forward Engine Mount PtE 54-53-101 71-21-01 4,000 1,300 Eddy Current 507

(Lug B) 5

Forward Upper/Lower Engine 54-53-201 71-23-00 MRB 71 .23.03/01 501 ' 5

Links 

2,300 Eddy Current 501 

Forward Upper Fuselage Link 54-53-401 71-23-00 2,700 

Wing Inspections 

Initial Recurring Inspection Affe

Location PSE AMM Inspection Inspection Se

Reference (Landings) (Landings) Method Num

MRB 57.02.00/05, 57-500-05 & 57-600-05 501 

Lower Cover 57-11-001 57-00-00 

5001

Lower Cover Splice & Coaming 57-11 -003 57-14-00 12,000 Ldgs 3,600 Ldgs Eddy Current 501

Stringers (GV) 30,0000 Hrs<1> 9,000 Hrs<'> 

Lower Cover Splice & Coaming 57-11-003 57-14-00 12,000 Ldgs 4,000 Ldgs Eddy Current 5001 

Stringers (GV-SP) 30,000 Hrs<1> 10,000 Hrs<1> 

12,000 Ldgs 2,000 Ldgs Eddy Current 501

Rear Spar BL6- BL35 57-12-002 57-12-00 30,000 Hrs<'> 5,200 Hrs<'> 5001

MRB 57.02.00/05 501 

BL35 Rib 57-12-007 57-00-00 

5001

DOCUMENT NO. GV-GER-9973 CAGE CODE 59734 PAGE 10 
Gulfstreaxn 

AMM Initial Recurring Inspection Affe

Location PSE Reference Inspection Inspection Method Se

(Landings) (Landings) Num

501-

Rear Spar Web At BL91 Sponson 57-12-014 57-12-00 12,000 4,000 Eddy Current 506

5001 

Rear Spar Web At BL91 Sponson 57-12-014 57-12-00 12,000 4,000 Eddy Current 5085

Rear Spar Web At BL91 Sponson 57-12-014 57-12-00 5,000 3,000 Eddy Current 5

Without ASC 178 516

Rear Spar Web At BL91 Sponson 505, 

57-12-014 57-12-00 8,000(2) 3,000 Eddy Current 699 w

With ASC 178 1

Rear Spar Web At BL49 57-12-015 57-12-00 12,000 4,000 Eddy Current 501

5001

Rear Spar Web At BL49 57-12-015 57-12-00 12,000 4,000 Eddy Current 5085

Lower Sponson Doubler 57-14-001 57-14-00 6,560 1,500 Eddy Current 501 

506

5

Lower Sponson Doubler 57-14-001 57-14-00 6,000 1,370 Eddy Current 514

5001

RBS109.5 Sponson Rib 57-14-002 57-13-00 8,800 1,440 Eddy Current 501

506

5

RBS109.5 Sponson Rib 57-14-002 57-13-00 8,000 1,270 Eddy Current 514

5001

Wing to Fuselage Lugs 57-16-001 57-16-01 MRB 57.16.01/01 501 

5001

Flap Front Spar at Spoiler Doors 57-52-002 57-53-00 8,000 3,000 Eddy Current 501

5001

Flap Rear Spar 57-52-005 57-53-00 12,000 4,000 Eddy Current 501

5001

DOCUMENT NO. GV-GER-9973 CAGE CODE 59734 PAGE 11 
Gulfstream 

AMM Initial Recurring Inspection Affe

Location PSE Reference Inspection Inspection Method Se

(Landings) (Landings) Num

Flap Track B Lower Flanges (GV) 57-55-005 57-53-00 5,300 2,000 Eddy Current 501

Flap Track B Lower Flanges (GV- 57-55-005 57-53-00 7,200 3,400 Eddy Current 5001 

SP) 

Flap Track C Lower Flanges (GV) 57-55-006 57-53-00 5,300 2,000 Eddy Current 501

Flap Track C Lower Flanges (GV- 57-55-006 57-53-00 7,200 3,400 Eddy Current 5001

SP) 

Spoiler (GV) 57-72-002 57-56-00 MRB 57.50.02/04 501 

Spoiler (GVSP) 57-72-002 57-56-00 MRB 57.50.02/03 5001

Empennage Inspections 

AMM Initial Recurring Inspection Affe

Location PSE Reference Inspection Inspection Method Se

(Landings) (Landings) Num

Horizontal Stabilizer- External 55-11-100 55-10-00 4,000(3) 4,000(3) Visual 501 

Visual 6

Horizontal Stabilizer Pitch Trim 

55-11-300 27-42-01 MRB 27-54-00/06 501

Actuator (GV) 

Horizontal Stabilizer Pitch Trim 

55-11-300 27-42-01 MRB 27-54-00/05 5001 

Actuator (GVSP) 

Horizontal Stabilizer Access 55-13-100 55-10-00 8,000 4,000 Eddy Current 501 

Cutouts 6

Pivot Fitting Bolts 55-14-101 55-10-00 4,800 4,800 Visual 501

'--- - ------- 6

DOCUMENT NO. GV-GER-9973 CAGE CODE 59734 PAGE 12 
Gulfstream 

AMM Initial Recurring Inspection Affe

Location PSE Reference Inspection Inspection Method Se

(Landings) (Landings) Num

Horizontal Stabilizer Pitch Trim 55-14-200 55-10-00 MRB 55.1 0.00/03 501

Actuator Attach Fittings 5001 

Elevator Skins - External Visual 55-21-100 55-20-00 1 ,800(4) 1 ,800(4) Visual 501

6

Elevator Hinges- General Visual 55-24-101 55-20-00 1 ,800(5) 1,800(5) Visual 501 

6

Elevator Hinge Fitting 55-24-102 55-23-00 8,300 2,755 Visual 501

Bolts/Sleeves 6

Vertical Stabilizer- External 55-31-100 55-30-00 4,000(3) 4,000(3) Visual 501Visual 6Vertical Stabilizer Pitch Trim 55-32-400 55-10-00 MRB 55.10.00/03 501

Actuator Attach Fittings 5001 

Vertical Stabilizer Access Cutouts 55-33-100 55-30-00 8,000 4,000 Eddy Current 501

6

Rudder Skins - External Visual 55-41-100 55-40-00 1 ,800(6) 1 ,800(6) Visual 501

6

Rudder Hinge Fittings - General 55-44-101 55-40-00 1 ,800(7) 1 ,800(7) Visual 501

Visual 6

Rudder Hinge Fittings 55-44-102 55-40-00 8,300 2,755 Visual 501

Bolts/Sleeves 6

Notes: 

(1) -Whichever occurs first 

(2) - Threshold is "time since ASC incorporation" for ASC178. 

(3) -Aircraft with landings beyond the stated initial interval shall perform inspections at the recurring interval beginning a

most recent compliance with GV AMM Chapter 05-20-00 task (Ref 53-00-00), "External Aft Fuselage and Empennag

Zonal Inspection", CMP 531090 (MRB inspection 53-300-02). Aircraft that have not yet complied with the MRB inspe

either the MRB inspection or stated initial inspection within 24 months of receipt of this report. 

(4) -Aircraft with landings beyond the stated initial interval shall perform inspections at the recurring interval beginning a

most recent compliance with either GV AMM Chapter 05-20-00 task (Ref 53-00-00), "External Aft Fuselage and Emp

-Zonal Inspection", CMP 531090 (MRB inspection 53-300-02) or GV AMM Chapter 05-20-00 task (Ref 55-20-00), "E

Delamination- Detailed Inspection", CMP 552001/552002 (MRB inspection 55.20.00/01 ). Aircraft that have not yet c

MRB inspections shall comply with either one of these MRB inspections or the stated initial inspection within 24 mont

(5) -Aircraft with landings beyond the stated initial interval shall perform inspections at the recurring interval beginning a

most recent compliance with GV AMM Chapter 05-20-00 task (Ref 55-23-00), "Elevator Hinge- Detailed Inspection", 

DOCUMENT NO. GV-GER-9973 CAGE CODE 59734 PAGE 13 
Gulfstream 

(MRS inspection 55.20.00/03). Aircraft that have not yet complied with the MRS inspection shall comply with either th

initial inspection within 24 months of receipt of this report. 

(6) -Aircraft with landings beyond the stated initial interval shall perform inspections at the recurring interval beginning a

most recent compliance with either GV AMM Chapter 05-20-00 task (Ref 53-00-00), "External Aft Fuselage and Emp

-Zonal Inspection", CMP 531090 (MRS inspection 53-300-02) or GV AMM Chapter 05-20-00 task (Ref 55-40-00), "R

Delamination- Detailed Inspection", CMP 554005 (MRS inspection 55.40.00/01). Aircraft that have not yet complied 

inspections shall comply with either one of these MRS inspections or the stated initial inspection within 24 months of 

(7) -Aircraft with landings beyond the stated initial interval shall perform inspections at the recurring interval beginning a

most recent compliance with GV AMM Chapter 05-20-00 task (Ref 55-40-00), "Rudder Assembly Hinges, Bushings, a

554015 (MRS inspection 55.40.00/04). Aircraft that have not yet complied with the MRS inspection shall comply with 

or stated initial inspection within 24 months of receipt of this report 

DOCUMENT NO. GV-GER-9973 CAGE CODE 59734 PAGE 14