GV Tech Eval Example Final

AIRCRAFT TECHNICAL EVALUATION

Gulfstream V
G-V S/N: XXXX

G-V S/N XXXX Page 1
07 AUG XXXX

G-V TECHNICAL EVALUATION PREPAIRED FOR:

AIRCRAFT MANUFACTURER AIRCRAFT DATA SERIAL NUMBER REGISTRATION
Gulfstream Aerospace Corporation
AIRCRAFT MODEL XXXX NXXXX
DATE OF MANUFACTURE: G-V
December 2000 CURRENT A/C TOTAL CYCLES
CURRENT A/C TOTAL TIME
12389.6 4346

AIRCRAFT EMPTY WEIGHT & CG

EMPTY WEIGHT % MAC DATE OF LAST WEIGHT & BALANCE
47,080.4
46.0 21 JUN 2011 (Calculated) (Actual 5/2010)

ENGINE DATA

ENGINE No. 1

Engine Manufacturer: BMW/Rolls-Royce Deutschland
Model: BR710 A1-10
XXXXXX
Serial Number: 12186.6
Total Time: 4416
Total Cycles:

ENGINE No. 2

Engine Manufacturer: BMW/Rolls-Royce Deutschland
Model: BR710 A1-10
XXXXXX
Serial Number:
Total Time: 12187.6 (12188.9 actual, see findings page)
Total Cycles: 4414 (4415 actual, see findings page)

APU DATA

APU Manufacturer: Honeywell
Model/Part Number: RE220-GV/ WE3800700-1

Serial Number: P-XXX
Total Time:: 8273

OPERATIONAL DOCUMENTATION

PUBLICATION LATEST REVISION CURRENT REVISION CURRENT
Aircraft Flight Manual Rev. 36 MAR 2015 STATUS STATUS
Aircraft Flight Manual Supplements GV-2009-03 -REV. 35 & 36
Rev. 36 MAR 2015 Rev. 34 DEC 2012 -REV 2009-02
Operating Manual GV-2009-02 Missing -REV. 33 - 36
Rev. 32 14 JUL 2010

G-V S/N XXXX Page 2
07 AUG XXXX

AIRCRAFT MAINTENANCE STATUS

HOURLY INSPECTIONS DATE C/W TIME/CYCLES C/W NEXT DUE
500 Hr. (1A)
1000 Hr. (2A) 30 MAR 2013 12234.5/4263 12734.5
2000 Hr. (4A)
2500 Hr. (5A) 30 MAR 2013 12234.5/4263 13234.5
3000 Hr. (6A)
5000 Hr. (10A) 30 MAR 2013 12234.5/4263 14234.5
MONTHLY INSPECTIONS
12 Month (1C) 26 SEP 2012 11777.6/4109 14277.6
24 Month (2C)
36 Month (3C) 12 AUG 2013 12267.6/4274 15267.6
48 Month (4C)
60 Month (5C) 28 APR 2010 9445.8/3 306 14445.8
72 Month (6C)
96 Month (8C) DATE C/W TIME/CYCLES C/W NEXT DUE
120 Month (10C)
144 Month (12C) 22 JUL 2015 12386.9/4344 JUL 2016
192 Month (16C)
5000 LANDINGS 22 JUL 2015 12386.9/4344 JUL 2017

12 AUG 2013 12267.6/4274 AUG 2016

12 AUG 2013 12267.6/4274 AUG 2017

02 JUN 2011 10589.9/3678 JUN 2016

12 AUG 2013 12267.6/4274 AUG 2019

18 MAY 2009 8552.4/2992 MAY 2017

22 JUL 2015 12386.9/4344 JUL 2025

12 AUG 2013 12267.6/4274 AUG 2025

N/A N/A JUN 2017 (Initial)

N/A N/A 654 Cycles Remaining (initial)

ENGINE MAINTENANCE STATUS

ENGINE No. 1: BR710 A1-10 ESN:XXXXX - TSN12186.6/ CSN: 4416

INSPECTIONS DATE TIME/CYCLES NEXT DUE
On Condition
On Condition - Rolls-Royce Corporate Care 09 DEC 2008 8123.9/2818
13064.6
1000 Hour Zonal and Detailed Inspection 11 AUG 2013 12064.6

ENGINE No. 2: BR710 A1-10 ESN:XXXXX - TSN: 12187.6/ CSN: 4414

INSPECTIONS DATE ENGINE TIME/CYCLES NEXT DUE
On Condition
On Condition - Rolls-Royce Corporate Care 23 DEC 2008 8125.2/2817
13065.3
1000 Hour Zonal and Detailed Inspection 11 AUG 2013 12065.3

APU MAINTENANCE STATUS

RE220-GV/WE3800700-1 S/N P-XXX TT:8273

INSPECTIONS DATE TIME NEXT DUE VERIFICATION
600 hr Log Book/CMP
24 Month 11 AUG 13 8156 8756 Log Book/CMP
10000 hr Log Book/CMP
22 JUL 15 8268 JUL 17

11 MAR 2003 393.0 10393.0

G-V S/N XXXX Page 3
07 AUG XXXX

G-V CHAPTER 05-10-10 STATUS

Life Limited Components Tables, Discard

Chapter 26 FIRE PROTECTION, FAA/EASA

PART NUMBER DESCRIPTION SERVICE LIFE, STATUS/ REMAINING CMP/REMARKS
51291-195
51291-192 FLIGHT CYCLES 261153
51291-197 261154
Fire Detection Rail Assembly No. 1 2000 FAA/EASA CW 2880/0534 Rem 261159
PART NUMBER 261160
1159SCC474-3 CW 2880/0534 Rem
1159SCC474-7 CMP/REMARKS
1159SCC474-11 Fire Detection Rail Assembly No. 4 2000 FAA/EASA CW 2880/0534 Rem
273517
PART NUMBER CW 2880/0534 Rem 273518
1159HM40120-1, 271217
1159HM40120-7 Chapter 27 FLIGHT CONTROLS, FAA/EASA 271218
1159SCL567-3 272421
1159L50004 DESCRIPTION SERVICE LIFE, STATUS/ REMAINING
1159LM50690 CMP/REMARKS
1159L50801 FLIGHT HOURS
323064
1159LM50521 Elevator Force Sensor 1000 FAA/EASA N/A (No ASC 134)
1159LM50548 NOTE: Aircraft having ASC 134 323066
1159LM30553
Aileron Force Sensor 1000 FAA/EASA N/A (No ASC 134) 322001
NOTE: Aircraft having ASC 134 1000 FAA/EASA N/A (No ASC 134)
Rudder Force Sensor 322401
NOTE: Aircraft having ASC 134
322409
Chapter 32 NOSE LANDING GEAR, FAA/EASA
322311
DESCRIPTION SERVICE LIFE, STATUS/ REMAINING 322419

FLIGHT CYCLES 322421

Rod End, Nose Landing Gear Retract 6470, FAA 2124 Cyc Rem

Actuator 5170, EASA

Nose Landing Gear Retract Actuator 25000, FAA 20654 Cyc Rem

Rod End - Discard 20000, EASA

Nose Landing Gear Assembly 32750, FAA 28404 Cyc Rem
MRB Ref: 32-10-04-05 26200, EASA

Nose Landing Gear Trunnion 22750 FAA 18404 Cyc Rem

18200 EASA

Nose Landing Gear Truss Brace 32750 FAA 28404 Cyc Rem

Assembly 26200 EASA

Nose Landing Gear Axle Assembly 32750 FAA 28404 Cyc Rem
Piston 26200 EASA

Nose Landing Gear Upper Torque 32750 FAA 28404 Cyc Rem
Arm 26200 EASA 28404 Cyc Rem
32750 FAA
Nose Landing Gear Lower Torque 26200 EASA
Arm

G-V S/N XXXX Page 4
07 AUG XXXX

Chapter 32 NOSE LANDING GEAR, FAA/EASA (continued)

PART NUMBER DESCRIPTION SERVICE LIFE, STATUS/REMAINING CMP/REMARKS
1159L50500 322200
1159LM50700-3 FLIGHT CYCLES 322206
(A/C 501-544 Only) *322206
1159LM50700-5 Nose Landing Gear Shock Strut 20000 FAA 15654 Cyc Rem 322403
1159LM50585 322434, *322435, 322436
1159LM40565 16000 EASA 322437
322405
1159LM50611 Nose Landing Gear Shock Strut 18400 FAA N/A by S/N 322407
1159LM50613 322411
1159LM40588-19 Cylinder Assembly 10200 EASA 322413
1159LM50587 322415
1159LM40583 Nose Landing Gear Shock Strut 20000 FAA *C/W AUG 13 322417
1159LM50568 325205
1159SCL500-23 Cylinder Assembly 16000 EASA 19928 Cyc Rem

Nose Landing Gear Drag Brace 32750 FAA 28404 Cyc Rem

26200 EASA

Nose Landing Gear Truss Brace Pin 20000 FAA *C/W AUG 13

16000 EASA *19928 Cyc Rem

15654 Cyc Rem

Nose Landing Gear Trunnion Pin, Left 32750 FAA 28404 Cyc Rem

26200 EASA

Nose Landing Gear Trunnion Pin, 32750 FAA 28404 Cyc Rem

Right 26200 EASA

Nose Landing Gear Upper Drag 5000 FAA 654 Cyc Rem

Brace Pin 4000 EASA

Nose Landing Gear Lower Drag 20000 FAA 15654Cyc Rem

Brace Pin 16000 EASA

Nose Landing Gear Actuator Attach 32750 FAA 28404 Cyc Rem

Pins 26200 EASA

Nose Landing Gear Strut/Trunnion 20000 FAA 15654 Cyc Rem

Pin 16000 EASA

Nose Wheel Steering Collar 20000 FAA 15654 Cyc Rem

Assembly 16000 EASA

Chapter 32 MAIN LANDING GEAR, FAA/EASA

PART NUMBER DESCRIPTION SERVICE LIFE, STATUS/ CMP/REMARKS
321007, 321008
1159L50001 FLIGHT CYCLES REMAINING 321407, 321408
321009, 321010
1159SCL502 Main Landing Gear Strut Assembly 20000 FAA 15654 Cyc Rem 321309, 321310
321203, 321204
1159LM50126 16000 EASA 321215, 321216
321215, 321216
1159LM50140 Main Landing Gear Side Brace 20000 FAA 15654 Cyc Rem

1159L50100 16000 EASA

1159LM50112-11 Main Landing Gear Structural Post 20000 FAA 15654 Cyc Rem
(A/C 501-547)
1159LM50112-13 16000 EASA

Main Landing Gear Axle Fitting 20000 FAA 15654 Cyc Rem

16000 EASA

Main Landing Gear Shock Absorber 20000 FAA 15654 Cyc Rem

16000 EASA

Main Landing Gear Shock Strut 5000 FAA N/A by S/N

Cylinder Nut 4000 EASA

Main Landing Gear Shock Strut 20000 FAA 15654 Cyc Rem

Cylinder Nut 16000 EASA

G-V S/N XXXX Page 5
07 AUG XXXX

Chapter 32 MAIN LANDING GEAR, FAA/EASA (continued)

PART NUMBER DESCRIPTION SERVICE LIFE, STATUS/REMAINING CMP/REMARKS
321013, 321014
1159LM50853 FLIGHT CYCLES 321017, 321018
321021, 321022
1159SCL566-13 Main Landing Gear Trunnion Pin 20000 FAA 15654 Cyc Rem 321403, 321404
321305 321306
1159LM50137 16000 EASA 321207, *321208, 321211,
321212
1159LM50164 Main Landing Gear Trunnion Pin, Aft 20000 FAA 15654 Cyc Rem
CMP/REMARKS
1159LM50148 Fuse Pin 16000 EASA *492002
*492003
1159LM50147 Main Landing Gear Spindle Pins 20000 FAA 15654 Cyc Rem *492001

PART NUMBER 16000 EASA CMP/REMARKS
531730
WK3840141 Main Landing Gear Side Brace Lower 20000 FAA 15654 Cyc Rem 531733, 531734

WE897994 Attach Pin 16000 EASA

WB3822380 Main Landing Gear Axle Fitting Attach 20000 FAA 15654 Cyc Rem
WB3822573
Pin 16000 EASA
PART NUMBER
Main Landing Gear Shock Strut 20000 FAA *C/W AUG 13/
1159BM50024
1159BM50025-11 Attachment Pin 16000 EASA *19928 Cyc Rem
1159BM50025-12
1159BM50025-13 15654 Cyc Rem
1159BM50025-14
1159BM50025-15 Chapter 49 AUXILIARY POWER UNIT, FAA/EASA
1159BM50025-16
1159BM50025-1 DESCRIPTION SERVICE LIFE, STATUS/REMAINING
1159BM50025-2
1159BM50025-3 APU HOURS
1159BM50025-4
1159BM50025-5 APU 1st Stage Turbine Rotor 10000 FAA/EASA *C/W MAR 03
1159BM50025-6
1159BM50033 Assembly *2120 Cyc Rem
1159B50042-61
1159BM50913-13 APU 2nd Stage Turbine Rotor 10000 FAA/EASA *C/W MAR 03
1159BM50913-14
1159BM50913-15 Assembly *2120 Cyc Rem
1159BM50913-16
APU Impeller 10000 FAA/EASA *C/W MAR 03

*2120 Cyc Rem

Chapter 53 FUSELAGE, FAA/EASA

DESCRIPTION SERVICE LIFE, STATUS/REMAINING

FLIGHT CYCLES

Cockpit Center Post 16000 FAA/EASA 11654 Cyc Rem

Cockpit Side Post 10000 FAA/EASA N/A by S/N

NOTE: Applies to Aircraft 501 thru
Aircraft 599.

Cockpit Side Post 16000 FAA/EASA 11654 Cyc Rem 531733, 531734

NOTE: Applies to Aircraft 600 and
subsequent.

Cockpit Lower Rail Fastener 15000 FAA/EASA 10654 Cyc Rem 531741 531742
Cockpit Pressure Floor Angle 12000 FAA/EASA 7654 Cyc Rem 531744
FS 465 Mainframe Fittings - Left 16000 FAA/EASA 531747, 531749
11654 Cyc Rem
NOTE: Applies to Aircraft 505 and
subsequent.

G-V S/N XXXX Page 6
07 AUG XXXX

Chapter 53 FUSELAGE, FAA/EASA (continued)

PART NUMBER DESCRIPTION SERVICE LIFE, STATUS/REMAINING CMP/REMARKS
531748, 531750
1159BM50914-13 FLIGHT CYCLES
1159BM50914-14
1159BM50914-15 FS465 Mainframe Fittings - Right 16000 FAA/EASA 11654 Cyc Rem
1159BM50914-16
1159BM50915-17 NOTE: Applies to Aircraft 505 and 16000 FAA/EASA 11654 Cyc Rem 531753, 531754
1159BM50915-18 subsequent.
1159BM50915-19 FS 576 Mainframe Fittings - Left
1159BM50915-20
1159BM50916-17 NOTE: Applies to Aircraft 505 and 16000 FAA/EASA 11654 Cyc Rem 531757, 531758
1159BM50916-18 subsequent.
1159BM50916-19 FS 576 Mainframe Fittings - Right
1159BM50916-20
NOTE: Applies to Aircraft 505 and
subsequent.

G-V CHAPTER 05-10-10 STATUS

Principal Structural Elements / Procedures

Chapter 53 FUSELAGE, FAA/EASA

DESCRIPTION NDI TYPE INITIAL/REPEAT STATUS/REM CMP
Nose Landing Gear Trunnion Fitting Lug 11654 Cyc Rem 322501
Cockpit Window Skins Eddy Current 16000/6000 Cycles 2054 Cyc Rem 531115, 531116
Nose Landing Gear Skin Cutout 3254 Cyc Rem 531016
Cockpit Skin Splices Eddy Current 6400/3200 Cycles C/W 10/18/2013 531068
Due: 14269.4
FS 119 Frame Eddy Current 8000/8000 Cycles Due: JUN 2017 531215
FS 63 Pressure Bulkhead Due: JUN 2017 531205
Cockpit Pressure Floor (FS 119 -FS 145) Visual 800/800 Cycles C/W 05/18/2009 531020
2000/2000 Hours Due: 05/31/2017
Cockpit Pressure Floor (FS 85 -FS 119) C/W 05/18/2009 531025, 531026
Visual 192/144 Months Due: 05/31/2017
Side Post, Upper Attachment 3254 Cyc Rem 531715, 531716
Side Post, Lower Attachment Visual 192/144 Months N/A by S/N 531717, 531718
NOTE: Applies to Aircraft 501 thru 599.
Side Post, Lower Attachment Visual 96/96 Months
NOTE: Applies to Aircraft 600 and sub
Center Post, Lower Attachment Visual 96/96 Months
Lower Cockpit Rail At Side Post
NOTE: Applies to Aircraft 501 thru 599. Eddy Current 8000/2900 Cycles
Eddy Current 5000/1100 Cycles

Eddy Current 6100/1300 Cycles 1754 Cyc Rem 531717, 531718

Eddy Current 6300/1000 Cycles 1954 Cyc Rem 531721
Eddy Current 5000/1100 Cycles N/A by S/N 531717, 531718

G-V S/N XXXX Page 7
07 AUG XXXX

Chapter 53 FUSELAGE, FAA/EASA (continued)

DESCRIPTION NDI TYPE INITIAL/REPEAT STATUS/REM CMP
Lower Cockpit Rail At Side Post 531717, 531718
NOTE: Applies to Aircraft 600 and sub Eddy Current 6100/1300 1754 Cyc Rem 530025
Fuselage Penetrations (Antennas) 531068
Longitudinal Skin Splices Visual 8000/4000 3254 Cyc Rem 531068
Visual 800/800 Cycles C/W 10/18/2013 532201
Fuselage Stability Frames 2000/2000 Hours Due: 14269.4 532540
Visual C/W 10/18/2013
FS 193 Frame 800/800 Cycles Due: 14269.4 531068
FS 193 and FS 229 Floor Beams Eddy Current 2000/2000 Hours 3254 Cyc Rem 531068
Eddy Current 3254 Cyc Rem 531068
8000/8000 533120, 533122
8000/8000 533202

NOTE: Applies to Aircraft 501 thru 687 and Visual 800/800 Cycles C/W 10/18/2013 533211
Aircraft 699. 2000/2000 Hours Due: 14269.4
Fuselage Skins Visual 800/800 Cycles C/W 10/18/2013
2000/2000 Hours Due: 14269.4
FS 465 / FS 576 Production Splices Visual 800/800 Cycles C/W 10/18/2013
2000/2000 Hours Due: 14269.4
Circumferential Skin Splices X-Ray 8000/2300 Cycles 3254 Cyc Rem
Visual/Eddy
Fuselage Skins At Wing Pressure Box Current 12000/2300 Cycles 7654 Cyc Rem
Cutout Eddy current
FS 426 Bulkhead 4800/2400 Cycles N/A by S/N

NOTE: Applies to Aircraft 625 and sub.
Window Surround Frame Splices

NOTE: Applies to Aircraft 501 thru 599. Eddy current 8000/8000 Cycles 3254 Cyc Rem 533211
Window Surround Frame Splices

NOTE: Applies to Aircraft 600 and sub. Eddy Current 7400/3400 Cycles 3054 Cyc Rem 533220
FS 758 Bulkhead - Below Floor Visual 800/800 Cycles C/W 10/18/2013 531068
Stringer Splices at FS 684 and FS 758 2000/2000 Hours Due: 14269.4
14000/4000 Cycles 9654 Cyc Rem 533305
Dorsal Tee Eddy Current 8000/4000 Cycles 3254 Cyc Rem 533315, 533316
Longerons 7 and 15 at FS 576 Visual 533321, 533322
12000/4000 Cycles 7654 Cyc Rem 533335
Longeron 22 Visual 96/96 Months C/W 05/18/2009 533300
Longeron 24 Visual Due: 05/31/2017
96/96 Months C/W 05/18/2009 531050, 531051
Forward Outboard Wing to Fuselage Fitting Visual Due: 05/31/2017
(Link) 8000/1900 Cycles 3254 Cyc Rem 533421 533422
Forward Wing To Fuselage Fitting Visual/Eddy
Current 96/96 Months C/W 05/18/2009 531050, 531051
Aft Outboard Wing to Fuselage Fitting (Link) Visual Due: 05/31/2017 533416
8000/8000 Cycles 3254 Cyc Rem
Over wing Drag Beam Visual

G-V S/N XXXX Page 8
07 AUG XXXX

Chapter 53 FUSELAGE, FAA/EASA (continued)

DESCRIPTION NDI TYPE INITIAL/REPEAT STATUS/REM CMP
3254 Cyc Rem 533435
BL 6 Forward Wing to Fuselage Attachment Visual 8000/5400 Cycles 533510
N/A by S/N
Link 533510

Pressure Floor Frame Clips Visual 4800/4800 Cycles 532510
533515
NOTE: Applies to Aircraft 501 thru 599 Visual 6800/4800 Cycles 2454 Cyc Rem 531310
Pressure Floor Frame Clips 531218, 531219
532117
NOTE: Applies to Aircraft 600 and sub Visual 192/144 Months Due: JUN 2017 531068
Pressure Floor Composite Floor Boards FS Eddy Current 2500/2500 Cycles 533817, 533819
426 - FS 632 C/W 2316 Cyc 533620
FS 426 Floor Beam Clips Due: 4816 Cyc 531068
N/A by S/N 553036
BL 6 Breather Beam at FS 570 Visual 1300/1300 Cycles 534005, 534006
NOTE: Applies to Aircraft 501 thru 599 1654 Cyc Rem 534715
Cabin Window Rings Windows 5 and 6 Eddy Current 6000/2500 Cycles C/W 2992 Cyc 535000
Visual 1700/1700 Cycles Due: 4692 Cyc 531068
Baggage Door Fittings C/W 10/18/2013 531068
Due: 14269.4 534920, 534922
Mid-Fuselage Cutouts - Exposed To Exterior Visual 800/800 Cycles 3254 Cyc Rem
2000/2000 Hours C/W 08/12/2013 CMP
FS 465 Wing Link Cutout Eddy Current Due: 08/ 2019 712507, 712508
FS 758 Composite Pressure Bulkhead Visual 8000/1250 Cycles C/W 10/18/2013
72/72 Months Due: 14269.4 712141, 712142
3254 Cyc Rem 712109, 712110
Stringer Splice at FS 820 Visual 800/800 Cycles 712137, 712138
2000/2000 Hours 654 Cyc Rem
Fin to Fuselage Attachments 3254 Cyc Rem
Forward Upper Bulkhead Fitting Visual 8000/8000 Cycles
FS 820 Bulkhead 746 Cyc Rem
Rudder Actuator Attachment Eddy Current 5000/2000 Cycles C/W 10/18/2013
Aft Fuselage Belly Access Cutouts Due: 14269.4
Eddy Current 8000/8000 Cycles C/W 10/18/2013
Aft Fuselage Cutouts - Exposed To Exterior Due: 14269.4
Visual 3600/3600 Cycles 3254 Cyc Rem
Aft Fuselage Cutouts - Covered By Fairings
Visual 800/800 Cycles STATUS/REM
DESCRIPTION 2000/2000 Hours 5854 Cyc Rem
Engine Attach Pins
Visual 800/800 Cycles N/A by S/N
Forward Engine Mount Pt E (Lug B) 2000/2000 Hours
NOTE: Applies to Aircraft 501 thru 539. C/W 01/09/2009
Forward Upper / Lower Engine Links Visual/Eddy 8000/4750 Cycles Due: 01/2025
Current CW 2698 Cyc
Due: 4998 Cyc
Chapter 54 PYLONS, FAA/EASA

NDI TYPE INITIAL/REPEAT

Eddy current / 10200/4200 Cycles
Mag-particle /
Ultrasonic

Eddy Current 4000/1300

Visual 192/192 Months

Forward Upper Fuselage Link Eddy Current 2700/2300 Cycles

G-V S/N XXXX Page 9
07 AUG XXXX

Chapter 55 STABILIZERS, FAA/EASA

DESCRIPTION NDI TYPE INITIAL/REPEAT STATUS/REM CMP
Horizontal Stabilizer Pitch Trim Actuator C/W 08/12/2013 274204
Restore 144/144 Months Due: 08/2025
3254 Cyc Rem 551018
Horizontal Stabilizer Access Cutouts Eddy Current 8000/4000 Cycles 551022
Pivot Fitting Bolts Visual 4800/4800 Cycles 454 Cyc Rem 551014
Horizontal Stabilizer Pitch Trim Actuator Visual 144/96 Months C/W 06/03/2013
Attach Fittings Due: 06/30/2021 552010, 552015
Visual 1800/1800 Cycles C/W 3306 Cyc
Elevator Skins - External Due: 5106 Cyc 552010, 552015
C/W 3306 Cyc
Elevator Hinges - General Visual 1800/1800Cycles Due: 5106 Cyc 552012
3954 Cyc Rem 553040
Elevator Hinge Fitting Bolts/Sleeves Visual 8300/2755 Cycles C/W 3952 Cyc
Vertical Stabilizer - External Visual 4000/4000 Cycles Due: 7952 Cyc 553035
C/W 06/27/2001
Vertical Stabilizer Upper Boomerang Fittings Visual 144/96 Months Due: 06/30/2017 553048
3254 Cyc Rem 554022
Vertical Stabilizer Access Cutouts Eddy Current 8000/4000 Cycles C/W 3306 Cyc
Rudder Skins - External Visual 1800/1800 Cycles Due: 5106 Cyc 554022
C/W 3306 Cyc
Rudder Hinge Fittings - General Visual 1800/1800 Cycles Due: 5106 Cyc 554020
3954 Cyc Rem
Rudder Hinge Fitting Bolts / Sleeves Visual 8300/2755 Cycles

DESCRIPTION Chapter 57 WINGS, FAA/EASA
Wing Lower Surface
NDI TYPE INITIAL/REPEAT STATUS/REM CMP
C/W 07/22/2015 570009, 570010
Visual 24/24 Months Due: 07/2017
C/W 05/18/2009 570205, 570206
Fuel Tank Internal Visual 96/96 Months Due: 05/31/2017
7654 Cyc Rem 571110, 571112
Lower Cover Splice and Coaming Stringers Eddy Current 12000/3600 Cycles
Rear Spar BL 6 - BL 35 Eddy Current 30000/9000 Hours 7654 Cyc Rem 571201 571202
BL 35.8 Rib Shear Tie Visual 12000/2000 Cycles
30000/5200 Hours C/W 05/18/2009 570205, 570206
96/96 Months Due: 05/31/2017 571707
N/A by S/N
Rear Spar Web at BL 91 Sponson Eddy Current 12000/4000 Cycles
NOTE: Applies to Aircraft 501 thru 504 and Eddy Current See Note May 09 571708
Aircraft 506 thru 515. 6646 Cyc Rem
Eddy Current 12000/4000 Cycles
Rear Spar Web at BL 91 Sponson C/W ASC178
NOTE: For Aircraft 505, Aircraft 516 and @2992 Cycles
subsequent not having ASC 178. Initial
Inspection due 5000 flight cycles and every 7654 Cyc Rem 571709
3000 flight cycles thereafter. For Aircraft
505, Aircraft 516 and subsequent having
ASC 178. Initial Inspection due 8000 flight
cycles from time of accomplishment of ASC
178 and every 3000 flight cycles thereafter.

Rear Spar Web at BL 49

G-V S/N XXXX Page 10
07 AUG XXXX

Chapter 57 WINGS, FAA/EASA (continued)

DESCRIPTION NDI TYPE INITIAL/REPEAT STATUS/REM CMP
Rear Spar at Spoiler Actuator Fitting with 3254 Cyc Rem 571301, 571302
1159SB50091-3, -4, -5, -6 Repair per ASC Eddy Current 8000/8000 Cycles
189 (Tension Fittings Only)
20000/20000 Hours
NOTE: Initial Inspection due from time of
accomplishment of ASC 189. Repeat Eddy Current 8000/4000 Cycles 3254 Cyc Rem 571303, 571304
inspection is “time since last inspection” for 20000/10000 Hours
all configurations.
Rear Spar at Spoiler Actuator Fitting with Eddy Current 6560/1500 Cycles N/A by S/N 571401, 571402
1159SB50091-7, -8, 101, 102 Repair per Eddy Current 6000/1370 Cycles
ASC 189 (Doubler Repair) Eddy Current 8800/1440 Cycles 1654 Cyc Rem 571401, 571402
Eddy Current 8000/1270 Cycles
NOTE: Initial Inspection due from time of N/A by S/N 571403, 571404
accomplishment of ASC 189. Recurring
inspection is “time since last inspection” for 3254 Cyc Rem 571403, 571404
all configurations.
Lower Sponson Doubler

NOTE: Applies to Aircraft 501 thru Aircraft
504 and Aircraft 506 thru Aircraft 513.
Lower Sponson Doubler

NOTE: Applies to Aircraft 505, Aircraft 514
and subsequent.
RBS 109.5 Sponson Rib

NOTE: Applies to Aircraft 501 thru Aircraft
504 and Aircraft 506 thru Aircraft 513.
RBS 109.5 Sponson Rib

NOTE: Applies to Aircraft 505, Aircraft 514 Visual 96/96 Months C/W 05/18/2009 571601
and subsequent. Due: 05/31/2017
Wing to Fuselage Lugs 3254 Cyc Rem 575215, 575217
7654 Cyc Rem 575220, 575222
Flap Front Spar at Spoiler Doors Eddy Current 8000/3000 Cycles 575111, 575112
Flap Rear Spar Eddy Current 12000/4000 Cycles 954 Cyc Rem 575113, 575114
Flap Track B Lower Flanges Eddy Current 5300/2000 Cycles 954 Cyc Rem 576010
Flap Track C Lower Flanges Eddy Current 5300/2000 Cycles C/W 06/05/2013
Spoiler Visual 144/96 Months Due: 06/30/2021

G-V S/N XXXX Page 11
07 AUG XXXX

LH ESN:XXXXX BMW/ROLLS-ROYCE BR710 A1-10 ROTATING/NON-ROTATING LIFE LIMITED PARTS

NOMENCLATURE LIFE LIMIT LIFE DATE/ REMARKS

CYCLES REMAINING CYCLES

CYCLES INSTALLED

LP Compressor Disc 6000 2272 DEC 08/2133 Repaired/Exchange (EX ESN:11316)

Fan Shaft Assembly 25000 20586 Engine Build Repaired at overhaul

HP Compressor Rotor Disk Assembly Stages 1-6 15000 10586 Engine Build Inspected at overhaul

HP Compressor Rotor Disk Assembly Stages 7-10 15000 10619 DEC08/12215 Repaired/Exchange (EX ESN:11316)
Curvic Ring 15000 13404 DEC08/“0” Installed “New Material” at overhaul
HP Turbine Rotor Disk , Stage 1 P/N BRR23952 12000 10404 DEC08/“0” Installed “New Material” at overhaul
HP Turbine Rotor Disk , Stage 2 P/N BRR22008 15000 13404 DEC08/“0” Installed “New Material” at overhaul

LP Turbine Rotor Disk, Sage 1 25000 20586 Engine Build Inspected at overhaul

LP Turbine Rotor Disk, Sage 2 25000 20586 Engine Build Inspected at overhaul
LP Turbine Rotor Shaft 25000 23404 DEC08/“0” Installed “New Material” at overhaul

LP Compressor Rotor Blade Assembly 7100 *2686 Engine Build Repaired at overhaul *#8 Renewed 5504 Rem

LP Compressor Annulus Filler P/N BRR22626 9700 7861 DEC08/2818 Installed at overhaul

Intermediate Case 20000 15586 Engine Build Repaired at overhaul

Rear Bearing Support Structure BRR23504 On Cond. N/A Engine Build Repaired at overhaul

No. 4 Stub-shaft 19000 14586 Engine Build Repaired at overhaul

Nose Cone Fairing 12700 8286 Engine Build Repaired at overhaul

RH ESN:XXXXX BMW/ROLLS-ROYCE BR710 A1-10 ROTATING/NON-ROTATING LIFE LIMITED PARTS

NOMENCLATURE LIFE LIMIT LIFE DATE/ REMARKS

CYCLES REMAINING CYCLES

CYCLES INSTALLED

LP Compressor Disc 6000 2386 DEC 08/2019 Repaired/Exchange (EX ESN:11315)

Fan Shaft Assembly 25000 20587 Engine Build Repaired at overhaul

HP Compressor Rotor Disk Assembly Stages 1-6 15000 10587 Engine Build Repaired at overhaul
HP Compressor Rotor Disk Assembly Stages 7-10 15000 13405 DEC08/“0” Installed “New Material” at overhaul

Curvic Ring 15000 10587 Engine Build Repaired at overhaul

HP Turbine Rotor Disk , Stage 1 P/N BRR23952 12000 7587 Engine Build Repaired at overhaul

HP Turbine Rotor Disk , Stage 2 P/N BRR22008 15000 10587 Engine Build Repaired at overhaul

LP Turbine Rotor Disk, Sage 1 25000 20587 Engine Build Inspected at overhaul

LP Turbine Rotor Disk, Sage 2 25000 20587 Engine Build Inspected at overhaul
LP Turbine Rotor Shaft 25000 23405 DEC08/“0” Installed “New Material” at overhaul

LP Compressor Rotor Blade Assembly 7100/10000 *4282 Engine Build Repaired at overhaul *#8 Renewed 5505 Rem

LP Compressor Annulus Filler P/N BRR22626 9700 5287 Engine Build Repaired at overhaul

Intermediate Case 20000 15587 Engine Build Repaired at overhaul

Rear Bearing Support Structure P/N BRR23504 On Cond. N/A Engine Build Repaired at overhaul

No. 4 Stub-shaft 19000 14587 Engine Build Modified at overhaul

Nose Cone Fairing 12700 8287 Engine Build Inspected at overhaul

G-V S/N XXXX Page 12
07 AUG XXXX

G-V MANDATORY AIRCRAFT SERVICE CHANGES (ASC’s)

ASC No. TITLE EFFECTIVITY STATUS
ASC-102A Pt. 1 & Pt. 2
ASC-168 Main Entrance Door Handle Modification 0501- 0999 C/W 05/12/2005
ASC-170
ASC-174 RUDDER ACTUATOR FORWARD ATTACH FITTING REPLACEMENT 506 - 634 C/W 05/23/2007
ASC-180A ENHANCED VISION SYSTEM BONDING MODIFICATION STC ST01201LA C/W 08/18/2006
Auxiliary Power Unit (APU) Bond Strap Installation 501 - 693 & 699 C/W 05/19/2008
Nose Gear Up-lock Hook Spring Replacement 501 - 693 & 699 C/W 12/01/2008

ACB No. G-V MANDATORY ALERT CUSTOMER BULLITENS (ACB’s) STATUS
ACB-001 C/W 01 DEC 2000
ACB-001A TITLE C/W 01 DEC 2000
ACB-002 Flight Controls (ATA 27), Replacement - Flap “D” Track Download Catch C/W 01 DEC 2000
ACB-003 Flight Controls (ATA 27), Replacement - Flap “D” Track Download Catch C/W 01 DEC 2000
ACB-004 C/W 01 DEC 2000
ACB-004A Landing Gear (ATA 32), Inspection - Nose Landing Gear Door Actuator C/W 01 DEC 2000
ACB-004A/Am1 C/W 01 DEC 2000
ACB-005 Flight Controls (ATA 27), Inspection - Elevator Hardover Prevention System C/W 01 DEC 2000
ACB-005A C/W 01 DEC 2000
ACB-005B Electrical Power (ATA 24), Inspection - Oxygen Bottle Wire Chafe Condition C/W 08 APR 2003
ACB-006 C/W 01 DEC 2000
ACB-007 Electrical Power (ATA 24), Inspection - Oxygen Bottle Wire Chafe Condition C/W 01 DEC 2000
ACB-007A C/W 01 DEC 2000
ACB-008 Electrical Power (ATA 24), Inspection - Oxygen Bottle Wire Chafe Condition C/W 22 JUL 2001
ACB-008A Engine (ATA 72), Inspection – Engine Core Fairing Installation C/W 01 DEC 2000
ACB-009 Engine (ATA 72), Inspection – Engine Core Fairing Installation C/W 01 DEC 2000
ACB-009A Engine (ATA 72), Inspection – Engine Core Fairing Installation C/W 01 DEC 2000
ACB-010 C/W 01 DEC 2000
ACB-010A Auxiliary Power (ATA 49), APU Oil Heater Circuit - Modification C/W 01 DEC 2000
ACB-011 C/W 01 DEC 2000
ACB-011A Engine Fuel And Control (ATA 73), Replacement - Fuel Metering Unit (FMU) C/W 27 JUN 2001
ACB-011B C/W 22 JUL 2001
ACB-011C Engine Fuel And Control (ATA 73), Replacement - Fuel Metering Unit (FMU) C/W 06 JUN 2002
ACB-011D C/W 13 MAY 2003
ACB-012 Hydraulic Power (ATA 29), Inspection - Hydraulic Fluid C/W 27 JUN 2001
ACB-013 C/W 18 AUG 2001
ACB-014 Hydraulic Power (ATA 29), Inspection - Hydraulic Fluid C/W 26 SEP 2001
ACB-015 Landing Gear (ATA 32), Inspection – Nose Wheel Steering Actuator RVDT C/W 15 NOV 2001
ACB-016 Landing Gear (ATA 32), Inspection – Nose Wheel Steering Actuator RVDT C/W 19 NOV 2001
ACB-017 Landing Gear (ATA 32), Replacement – Nose Wheel Steering Actuator C/W 06 JUN 2002
ACB-018 Landing Gear (ATA 32), Replacement – Nose Wheel Steering Actuator C/W 06 JUN 2002
ACB-019 Engine (ATA 72), Inspection – LP Compressor Fan Disc C/W 21 NOV 2002
ACB-020 Engine (ATA 72), Inspection – LP Compressor Fan Disc C/W 23 FEB 2004
ACB-021 Engine (ATA 72), Inspection – LP Compressor Fan Disc C/W 13 SEP 2004
ACB-022 Engine (ATA 72), Inspection – LP Compressor Fan Disc C/W 15 JUN 2005
Engine (ATA 72), Inspection – LP Compressor Fan Disc
Landing Gear (ATA 32) Modification – Landing Gear Door Control Valve
Landing Gear (ATA 32) Modification – Nose Wheel Steering Hydraulic Line Replacement.(ASC 130)
Fire Protection (ATA 26) Inspection – Engine Fire Ext. Bottle Electrical Connections
Electrical Power (ATA 24), Inspection – Left Integrated Drive Generator (IDG) Wiring Harness Assembly
Doors (ATA 52), Inspection – Main Entrance Door (MED) Secondary Lock Handle Installation
Landing Gear (ATA 32), Inspection – Nose Landing Gear Actuator Rod End
Wings (ATA 57), Modification – Wing Rib Stiffener
Electrical Power (ATA 24), Inspection – Pilot’s Overhead Circuit Breaker Panel
Equipment and Furnishings (ATA 25), Removal – Aft Equipment Compartment Ladder Hoist Assembly

Electrical Power (ATA 24), Wiring Harness Contacting Oxygen Bottle
Equipment and Furnishings (ATA 25), De-activation – Adel Wiggins Floor Heater Pad System

G-V S/N XXXX Page 13
07 AUG XXXX

G-V MANDATORY ALERT CUSTOMER BULLITENS (ACB’s) (continued)

ACB No. TITLE STATUS
ACB-023 Wings (ATA 57), Inspection - Wing Rib Reinforcement Angles C/W 28 JUN 2005
ACB-024 Landing Gear (ATA 32), Inspection – Nose Landing Gear Tires C/W 21 OCT 2005
ACB-025 Flight Controls (ATA 27), Inspection – Aileron and Elevator Actuator Load Relief Bungees CANCELLED BY 25A
ACB-025A Flight Controls (ATA 27), Inspection – Aileron and Elevator Actuator Load Relief Bungees C/W 18 DEC 2005
ACB-026 Water / Waste (ATA 38) Inspection – Forward Water System Valves C/W 14 MAY 2010
ACB-027 Landing Gear (ATA 32), Inspection – Nose Landing Gear Door Actuator Shuttle Valve End Cap C/W 14 MAY 2010
ACB-028 Landing Gear (ATA 32), Inspection – Nose Landing Gear Door Actuator Shuttle Valve End Gland (Non-Destructive CANCELLED BY 28A
Testing)
ACB-028A Landing Gear (ATA 32), Inspection – Nose Landing Gear Door Actuator Shuttle Valve End Gland (Non-Destructive C/W 14 JUL 2007
Testing)
ACB-029 Fuselage (ATA 53), Inspection – Auxiliary Power Unit Enclosure C/W 14 MAY 2010
ACB-029A Fuselage (ATA 53), Inspection – Auxiliary Power Unit Enclosure C/W 14 MAY 2010
ACB-030 Fire Protection (ATA 26), Inspection – Third Engine Fire Bottle Installation C/W 07 DEC 2010
ACB-030A Fire Protection (ATA 26), Inspection – Third Engine Fire Bottle Installation C/W 21 DEC 2010
ACB-031 C/W 11 DEC 2011
Airborne Auxiliary Power (ATA 49), Operational Limitations - Auxiliary Power Unit (APU) Enclosure with Thermal
ACB-032 Barrier Coating C/W 17 MAY 2012
Auxiliary Power Unit (ATA 49), Operational Limitations – Auxiliary Power Unit (APU) Enclosure with Thermal Barrier
CB No. Coating – Expanded Effectivity
001
002 G-V CUSTOMER BULLITENS (CB’s) STATUS/INTREVAL DATE C/W
003 Active - One Time 01 DEC 2000
004 TITLE Active/One Time 01 DEC 2000
005 Active/One Time 01 DEC 2000
006 Power Plant (ATA 71) Replacement Fixed Cowl ECS Duct Fire Sea Active/One Time 01 DEC 2000
007 Fuel (ATA 28) Replacement – Wing Tank probe Mounting Clamps Active/One Time 01 DEC 2000
008 Fuel (ATA 28) Replacement – Wing Tank Fuel Cap-Adapter Hardware Active/One Time 01 DEC 2000
009 Flight Controls (ATA 27) Wiring Reroute – Elevator Hard Over Prevention System Active/One Time 01 DEC 2000
010 Engine (ATA 72) Inspection – APT Gearbox Active/One Time 01 DEC 2000
011 Electrical Power (ATA 24) Inspection – AC/DC Power Feeders Active/One Time 01 DEC 2000
012 Electrical Power (ATA 24) Inspection – DC Power Feeders Active/One Time 01 DEC 2000
013 Fuel (ATA 28) Inspection – Fuel/Water Drain Valves Active/One Time 01 DEC 2000
014 Flight Controls (ATA 27) Inspection/Test – Elevator Dual Tandem Hydraulic Actuator Active/One Time 27 JUN 2001
015/015AM1 Landing Gear (ATA 32) Replacement – Main Wheel Spacers Active/One Time 01 DEC 2000
016 Electrical Power (ATA 24) Inspection – Integrated Drive Generator Point Blanking Plug Active/One Time 01 DEC 2000
017 Furnishings and Equipment (ATA 25) Inspection – Side Facing Divan Active/One Time 15 MAY 2003
018 Fuel (ATA 28) Modification – Main Wheel Well Fuel Line Coupling Active/One Time 01 DEC 2000
019 Fuel (ATA 28) Inspection – Main Fuel and Heated Fuel Return Line Couplings Active/One Time 01 DEC 2000
Auxiliary Power (ATA 49) Inspection – Starter Circuits Active/One Time 01 DEC 2000
Flight Controls (ATA 27) Inspection – Ground Spoiler Output Bell-crank Active/One Time 01 DEC 2000
Landing Gear (ATA 32) Inspection – Main Landing Gear Side Brace Actuator
Fuselage (ATA 53) Inspection – Pressure Floorboards
Fuselage (ATA 53) Inspection – Pressure Floorboards

G-V S/N XXXX Page 14
07 AUG XXXX

CB No. G-V CUSTOMER BULLITENS (CB’s) (continued) STATUS/INTREVAL DATE C/W
020 Active/One Time 01 DEC 2000
021 TITLE Active/One Time 01 DEC 2000
022 Auxiliary Power (ATA 49) Inspection – Sight Glass, Oil Cooler Inlet Duct Active/One Time 01 DEC 2000
023 Electrical Power (ATA 24) Replacement – IDG Input Oil Seal Active/One Time 01 DEC 2000
024 Air Conditioning (ATA 21) Modification – Trim Air Valve Pneumatic Lines (ASC 91) Active/One Time 01 DEC 2000
025/024AM1 Equipment and Furnishings (ATA 25) Removal – Insulation Bag A Active/One Time 15 MAY 2003
026 Fuselage (ATA 53) Inspection – FS 67.5 Pressure Bulkhead Active/One Time 01 DEC 2000
027 Hydraulic Power (ATA 29) Inspection – Hydraulic Pump EDP (Case Drain) Filter / Bow Active/One Time 01 DEC 2000
028 Landing Gear (ATA 32) Life Limit – Nose Landing Gear Actuator Rod End (ASC 103) Active/One Time 01 DEC 2000
029 Landing Gear (ATA 32) Inspection / Replacement – Landing Gear Selector / Dump Valve Active/One Time 01 DEC 2000
030 Pneumatic (ATA 36) Inspection – Air Ducting GAMAH Couplings Active/One Time 01 DEC 2000
031 Flight Controls (ATA 27) Replacement – Ground Spoiler Secondary Control/Hydraulic Selector Valve (ASC 98) Active/One Time 01 DEC 2000
032/032A Standard Practices – Airframe (ATA 20) Inspection / Cleaning – Wheel Wells and Wing Rear Beams Active/One Time 27 JUN 2001
033 Engine and Fuel Controls (ATA 73) Replacement – Engine Fuel Metering Unit (FMU) Active/One Time 01 DEC 2000
034 Oxygen (ATA 35) Inspection – Passenger Oxygen System Flow Rate Active/One Time 01 DEC 2000
035 Landing Gear (ATA 32) Inspection – Main Landing Gear Door Bearing Installation Active/One Time 01 DEC 2000
036 Pneumatic (ATA 36) Replacement – Air Ducting GAMAH Couplings (ASC 105) Active/One Time 01 DEC 2000
037 Flight Controls (ATA 27) Modification – Elevator HOPS Switch Bracket (ASC 75) Active/One Time 01 DEC 2000
038 Electrical Power (ATA 24) Inspection – Hall Effect Sensor Wiring Active/One Time 01 DEC 2000
039 Navigation (ATA 34) Inspection – Enhanced Ground Proximity Warning Computer (EGPWC) – Mod Status Active/One Time 01 DEC 2000
040 Engine Fuel (ATA 73) Replacement – Engine Fuel Filter Differential Pressure Indication (DPI) Switch Active/One Time 01 DEC 2000
041/041AM! Electrical Power (ATA 24) Inspection – 60 Hz Converter System Aneroid Switch Active/One Time 27 MAY 2005
042 Electrical Power (ATA 24) Modification – Right Engine Integrated Drive Generator (IDG) Power Cable Active/One Time 01 DEC 2000
043/043A Electrical Power (ATA 24) Inspection – Integrated Drive Generator (IDG) Feeder Cable Termination Active/One Time 01 DEC 2000
044 Fuel (ATA 28) Inspection – APU Fuel Shutoff Valve Pressure Line Corrosion Active/One Time 01 DEC 2000
045 Flight Controls (ATA 27) Inspection – Rudder Actuator Forward Attach Fitting Hardware Active/One Time 27 JUN 2001
046 Fire Protection (ATA 26) Inspection – APU Fire Detection Loop Assembly Active/One Time 01 DEC 2000
047 Auxiliary Power (ATA 49) Installation – APU Fire/Overheat Detector Bracket (ASC 116) Active/One Time 27 JUN 2001
048 Auxiliary Power (ATA 49) Installation – APU Enclosure Seal (ASC 109) Active/One Time 27 JUN 2001
049/049A Fire Protection (ATA 26) Relocation – Fire Detection Control Unit (ASC 118) Active/One Time 27 JUN 2001
050 Power Plant (ATA 71) Inspection – Engine Cowling Security Wiring Harness Assembly (ASC 108) Active/One Time 27 JUN 2001
051 Landing Gear (ATA 32) Modification – Nose Wheel Steering Hydraulic Line Replacement (ASC 130) Active/One Time 27 JUN 2001
052 Auxiliary Power (ATA 49) Inspection – APU Air Inlet and Oil Cooler Boots Active/One Time 27 JUN 2001
053 Fire Protection (ATA 26) Inspection – Fire Extinguisher Discharge Outlet Gland Nuts Active/One Time 27 JUN 2001
054 Air Conditioning (ATA 21) Inspection – Cooling Fans (Power Distribution Box and Inertial Reference Unit) Active/One Time 27 JUN 2001
055 Equipment and Furnishings (ATA 25) Inspection – TIA Water Heater Pressure Relief Valve Active/One Time 27 JUN 2001
056 Landing Gear (ATA 32) Replacement – Nose Wheel Steering Rudder Pedal RVDT (ASC 107) Active/One Time 18 AUG 2001
057 Exhaust (ATA 78) Inspection – Thrust Reverser Isolation Control Unit (ICU) Seals Active/One Time 22 JUL 2001
058 Navigation (ATA 34) Inspection – TCAS Computer L-Band Suppression Cable Connection Active/One Time 18 AUG 2001
059 Placards and Markings (ATA 11) Installation – BR710 Engine Static Ground Operation Restriction Placard Active/One Time 05 JUN 2002
060 Windows (ATA 56) Inspection – Cockpit Side Window Aft Radius Surface Finish Active/One Time 26 SEP 2001
061/061A Landing Gear (ATA 32) Inspection – Main Landing Gear (MLG) Shock Absorber Spherical Bearing Active/One Time 26 SEP 2001
062/062A Placards and Markings (ATA 11) Installation – Main Landing Gear (MLG) Axle Jack-pad Adapter Cover Decal Active/One Time 18 OCT 2001
Doors (ATA 52) Inspection – Main Entrance Door Link Attach Fitting (ASC 137)
G-V S/N XXXX Fire Protection (ATA 26) Inspection – Equipment Overheat Sensor
07 AUG XXXX
Page 15

CB No. G-V CUSTOMER BULLITENS (CB’s) (continued) STATUS/INTREVAL DATE C/W
063/063A Active/One Time 14 DEC 2001
064 TITLE Active/One Time 14 DEC 2001
065/065AM1 Fuel (ATA 28) Replacement – Pressure Fueling System Fuel Shutoff Hoses Active/One Time 27 MAY 2005
Flight Controls (ATA 27) Inspection – Aileron Bell Crank
066/066AM1 Flight Controls (ATA 27) Modification – Aileron Cable Pulley Bracket FOD Cover Installation (Air (ATA 75) Active/One Time 23 MAR 2003
067 Modification – HP 8 Handling Bleed Valve Attenuator ASC 132) Active/One Time 06 JUN 2002
068 Air (ATA 75) Modification – HP 8 Handling Bleed Valve Attenuator Active/One Time 05 JUN 2002
069/069AM1 Indicating/Recording (ATA 31) Modification – Digital Flight Data Recorder System Upgrade (ASC 110 AM1) Active/One Time 05 JUN 2002
070 Fire Protection (ATA 26) Inspection – Fire Detection Control Box Active/One Time 05 JUN 2002
071/071A/071A AM1 Power Plant (ATA 71) Modification – Fixed Cowl Re-Identification Active/One Time CANCELED
072/072AM1 Electrical Power (ATA 24) Modification – Generator Control Unit (GCU) and Bus Power Control Unit (BPCU) Active/One Time 21 NOV 2002
073/073AM1 Placards and Markings (ATA 11) Installation – Customer Support Contact Information Placard (ASC 142) Active/One Time 29 OCT 2002
074/074AM1 Ice and Rain Protection (ATA 30) Modification – Windshield Heat Control Relay (ASC 131) Active/One Time 07 JUN 2002
075 Landing Gear (ATA 32) Replacement – Nose Landing Gear Lower Hydraulic Swivel (ASC 140) Active/One Time 21 NOV 2002
076 Flight Controls (ATA 27) Inspection – Aileron Trim Tab Clearance Active/One Time 21 NOV 2002
077 Flight Controls (ATA 27) Modification – Aileron Actuator Tube Replacement Active/One Time 21 NOV 2002
078 Fire Protection (ATA 26) Modification – Fire Bottle Wire Identification and Marker Ties Installation (ASC 138) Active/One Time 21 NOV 2002
079/079AM1 Wings (ATA 57) Survey – Wing Skin Active/One Time 21 NOV 2002
080 Flight Controls (ATA 27) Installation – Rudder Fasteners Active/One Time 21 NOV 2002
081 Flight Controls (ATA 27) Inspection – Aileron Hard Over Protection System (HOPS) Wiring Active/One Time 21 NOV 2002
082 Stabilizers (ATA 55) Inspection – Horizontal Stabilizer Vortex Generators Active/One Time 20 NOV 2002
083 Power Plant (ATA 71) Modification – Upper and Lower Cowl Door Re-Identification Active/One Time 20 NOV 2002
084 Doors (ATA 52) Replacement – Baggage Door Fasteners (ASC 144) Active/One Time 27 SEP 2002
085/085AM1 Landing Gear (ATA 32) Inspection – Main Landing Gear Door Control Valve Blanking Pin Active/One Time 27 NOV 2002
086 Air Conditioning (ATA 21) Inspection – Pack Inlet Valve Operation Active/One Time 20 NOV 2002
087/087AM1 Landing Gear (ATA 32) Inspection – Main Landing Gear Wheel Brake De-spin Restrictor Active/One Time 14 MAY 2010
088 Electrical Power (ATA 24) Modification – IDG Cable/Hydraulic Shutoff Valve Bracket Installation (ASC 143) Active/One Time 22 NOV 2002
089 Landing Gear (ATA 32) Inspection – Main Landing Gear Doors Active/One Time 21 NOV 2002
090 Windows (ATA 56) Inspection – Cabin Windows Active/One Time 22 NOV 2002
091 Ice and Rain Protection (ATA 30) Modification – Cabin Window Heat Installation Active/One Time 22 NOV 2002
092 Ice and Rain Protection (ATA 30) Inspection – Wing Anti-Ice Ducting Active/One Time 14 MAY 2003
093 Flight Control Systems (ATA 27) Inspection – Angle-of-Attack (AOA) Sensors Active/One Time 15 MAY 2003
094 Navigation (ATA 34) Inspection – HUD Computer / Rack Connector Keying Active/One Time 27 MAY 2005
095/095A Water / Waste (ATA 38) Modification – Vacuum Toilet Status Panel Active/One Time 14 MAY 2010
096 Doors (ATA 52) Modification – Main Entrance Door Handle Active/One Time 14 MAY 2003
097 Engine (ATA 72) Inspection – LP Compressor Fan Disc Active/One Time 12 MAY 2003
098 Navigation (ATA 34) Inspection – Total Air Temperature (TAT) Probe Active/One Time 27 MAY 2005
099 Fire Protection (ATA 26) Inspection – Portable Halon Fire Extinguishers Active/One Time 10 MAY 2003
100 Landing Gear (ATA 32) Inspection – Nose Landing Gear Drag Brace Attach Fitting Bearing Active/One Time 12 MAY 2003
101/101AM1 Wings (ATA 57) Inspection – Right Wing Stringer #21 Active/One Time 27 MAY 2005
102 Hydraulic Power (ATA 29) Installation – Power Transfer Unit Check Valve Active/One Time 27 MAY 2005
103 Equipment / Furnishings (ATA 25) Inspection – Cox Floor Heater Mats Active/One Time 28 JUN 2003
104 Electrical Power (ATA 24) Inspection – Feeder Cable Chafe at Fuselage Station (FS) 684 Active/One Time 28 JUN 2003
105 Electrical Power (ATA 24) Modification – Pilot Overhead Circuit Breaker Panel (ASC 111) Active/One Time 27 MAY 2005
Flight Controls (ATA 27) Inspection – Aileron Balance Weights
Fuselage (ATA 53) Inspection – Intercostal Stringer 8L Fuselage Station 490 – 554

G-V S/N XXXX Page 16
07 AUG XXXX

CB No. G-V CUSTOMER BULLITENS (CB’s) (continued) STATUS/INTREVAL DATE C/W
106/106AM1 Active/One Time 26 MAY 2004
107 TITLE Active/One Time 10 NOV 2003
108 Fuselage (ATA 53) Inspection – Intercostal Stringer 8L Fuselage Station 490 – 554 Active/One Time 12 NOV 2003
109 Airborne Auxiliary Power (ATA 49) Inspection – Airborne Auxiliary Power Unit Door Actuator Active/One Time 10 NOV 2003
110 Water / Waste (ATA 38) Modification – Water Fill Service Line (ASC 150) Active/One Time 12 NOV 2003
111 Flight Controls (ATA 27) Inspection – Elevator Input/Output Crank Assemblies Active/One Time 11 NOV 2003
112 Flight Controls (ATA 27) Replacement – Outboard Flight Spoiler Idler Assembly Active/One Time 18 JUN 2013
113 Landing Gear (ATA 32) Inspection – Nose Landing Gear Actuator Rod End Active/One Time 17 FEB 2004
114 Fuselage Structure (ATA 53) Inspection – Floor Beam Assembly Fuselage Station 758 Active/One Time 14 MAR 2004
115/115A Airborne Auxiliary Power (ATA 49)Inspection – Load Control Valve Active/One Time 14 MAR 2004
116 Landing Gear (ATA 32) Inspection – Landing Gear Selector Dump Valve Active/One Time 14 MAR 2004
117 Navigation (ATA 34) Modification – Head-Up Display (HUD) Overhead Unit and Mounting Tray Active/One Time 27 MAY 2005
118 Active/One Time 16 AUG 2004
119 Fire Protection (ATA 26) Modification - Fire Detection Control Box Mounting Active/One Time 27 MAY 2005
120 Indicating/Recording Systems (ATA 31) Digital Flight Data Recorder System – Upgrade (ASC 110A AM1) Active/One Time 16 AUG 2004
121 Flight Controls (ATA 27) Lubrication – Horizontal Stabilizer Actuator No-Back Trigger and Lever Mechanism Active/One Time 16 AUG 2004
122 Active/One Time 16 AUG 2004
123 Hydraulic Power (ATA 29) Replacement - Hydraulic System Servicing Placard Active/One Time 29 DEC 2004
124 Wings (ATA 57) Modification – Vortex Generator Installation and Wing Rib Reinforcement (ASC 159) Active/One Time 27 MAY 2005
125 Electrical Power (ATA 24) Modification – External DC Power Receptacle Active/One Time 27 MAY 2005
126 Equipment and Furnishings (ATA 25) Modification – Observer Seat Pan Pivot Bolt Active/One Time 27 MAY 2005
127/127AM1 Flight Controls (ATA 27) Inspection – Aileron and Elevator Actuator Damper Shaft Active/One Time 14 MAY 2010
128 Flight Controls (ATA 27) Retrofit – Aileron and Elevator Actuators Active/One Time 27 MAY 2005
129 Hydraulic Power (ATA 29) Inspection – Hydraulic Reservoir External Servicing Selector Valve Active/One Time 27 MAY 2005
130 Equipment / Furnishings (ATA 25) Modification – Tail Compartment Ladder Active/One Time 27 MAY 2005
131 Indicating / Recording (ATA 31) Modification – Flight Data Recorder (FDR) Download Harness Active/One Time 27 MAY 2005
132 Flight Controls (ATA 27) Replacement – Flap Leading Edge Rivets Active/One Time 27 MAY 2005
133 Wings (ATA 57) Replacement – Outboard Fixed Trailing Edge Fasteners Active/One Time 27 MAY 2005
134 Fuselage (ATA 53) Modification – Enhanced Vision System (EVS) Radome Sealing Improvement Active/One Time 31 AUG 2005
135 Fuselage (ATA 53) Replacement – Enhanced Vision System (EVS) Radome Alignment Pins Active/One Time 31 MAY 2006
136/136A Landing Gear (ATA 32) – Inspection Main Landing (MLG) Shock Strut Active/One Time 08 JUN 2006
137 Ice and Protection (ATA 30) Inspection – Wing Anti-Ice Exhaust Louvers Active/One Time 08 JUN 2006
138 Indicating / Recording Systems (ATA 31) Inspection – Flight Control Sensor Installation Active/One Time 07 SEP 2005
139 Flight Controls (ATA 27) Inspection – Aileron Force Link Assembly Wiring Active/One Time 15 SEP 2005
140 Landing Gear (ATA 32) Inspection – Nose Landing Gear Actuator Rod End Active/One Time 08 JUN 2006
141 Fuselage (ATA 51) Inspection – Left and Right Stringer 6 Between Fuselage Stations 955 - 974 Active/One Time 31 MAY 2006
142 Wings (ATA 57) Inspection / Sealing – Outboard Wing Rib Repair Active/One Time 08 JUN 2006
143/143A Engine Fuel And Control (ATA 73) Inspection – Fuel Servo Tube Clearance Active/One Time 08 JUN 2006
144 Landing Gear (ATA 32) Modification – Nose Landing Gear Downlock Harness Connector Hardware Active/One Time 31 MAY 2006
145/145AM1 Electrical Power (ATA 24) Inspection – Integrated Drive Generator and AC Generator Modification Status Active/One Time 21 DEC 2006
146 Ice and Rain Protection (ATA 30) Modification – LH Wing Anti-Ice Valve Rotation Active/One Time 08 JUN 2006
147 Landing Gear (ATA 32) Modification – Main Landing Gear Doors Active/One Time 08 JUN 2006
148 Equipment & Furnishings (ATA 25) Replacement – Cabin Interior Secondary Structure Components Active/One Time 08 JUN 2006
149 Flight Controls (ATA 27) Replacement – Aileron and Elevator Actuator Load Relief Bungees Active/One Time 01 JUN 2007
Landing Gear (ATA 32) – Inspection Landing Gear Bungees Lubrication and Rigging
G-V S/N XXXX Lights (ATA 33) Inspection – Fluorescent Lighting Connectors
07 AUG XXXX Flight Controls (ATA 27) Inspection – Flap Leading Edge Heat Treatment
Water / Waste System (ATA 38) Modification – Water System Improvement (ASC 165)

Page 17

CB No. G-V CUSTOMER BULLITENS (CB’s) (continued) STATUS/INTREVAL DATE C/W
150 Active/One Time 17 AUG 2006
151 TITLE Active/One Time 01 JUN 2007
152 Navigation (ATA 34) Modification – Enhanced Vision System (EVS) Window Bonding Strap (ASC 170) Active/One Time 01 JUN 2007
153 Flight Controls (ATA 27) Inspection – Rudder Stop Bolts Active/One Time 21 DEC 2006
154 Flight Controls (ATA 27) Modification – Rudder Actuator Forward Attach Fitting Replacement (ASC 168) Active/One Time 02 MAR 2007
Landing Gear (ATA 32) Inspection – Nose Landing Gear Trunnion Pin (Right Side Only)
155 Landing Gear (ATA 32) Modification – Sealant Protection of Nose Landing Gear Weight-on-Wheels Switch, Active/One Time 01 JUN 2007
156 Active/One Time 18 JUN 2013
157 PN 1159SCAV514-1 Active/One Time 01 JUN 2007
158 Electrical Power (ATA 24) Inspection – Battery Chargers Active/One Time 01 JUN 2007
159 Air Conditioning (ATA 21) Inspection – Trim Air Valve Servo Pressure Supply - Check Valve Installation Active/One Time 20 MAY 2008
160 Hydraulic Power (ATA 29) Modification – Auxiliary Hydraulic Boost Pump Circuit Protection (ASC 169) Active/One Time 18 JUN 2013
161 Hydraulics (ATA 29) Inspection – Hydraulic Line Installation at Right Battery Charger Shelf Active/One Time 06 SEP 2008
162 Fuselage (ATA 53) Inspection – Auxiliary Power Unit (APU) Enclosure Sensor Installation Active/One Time 20 MAY 2008
163 Communications (ATA 23) Inspection – Broadband Multi-Link (BBML) Antenna Control Unit (ACU) Installation Active/One Time 20 MAY 2008
164 Engine Turbine / Ducted Fan (ATA 72) Inspection – Low-Pressure (LP) Compressor Annulus Fillers Active/One Time 06 OCT 2007
165 Electrical Power (ATA 24) Inspection – Right Main Battery Lead Installation Active/One Time 05 JUN 2009
166 Hydraulics (ATA 29) Modification – Right Pylon Case Drain Line Routing Active/One Time 20 MAY 2008
167 Water/Waste (ATA 38) Inspection – Forward Drain Valves Active/One Time 20 MAY 2008
168 Wings (ATA 57) Modification – Rear Spar Fatigue Enhancement Active/One Time 14 MAY 2010
169 Landing Gear (ATA 32) Modification – Nose Landing Gear Door Actuator (ASC 176) Active/One Time 20 MAY 2008
170 Doors (ATA 52) Inspection – Main Entry Door Warning Switch Installations Active/One Time 14 MAY 2010
171 Electrical Power (ATA 24) Inspection – Feeder Cable Installation at Fuselage Station (FS) 687 Active/One Time 20 MAY 2008
Oxygen (ATA 35) Inspection – Passenger Oxygen Drop-Down Masks
172 Water / Waste (ATA 38) Inspection – Waste Tank Rinse Nozzles Active/One Time 14 MAY 2010
173 Airborne Auxiliary Power (ATA 49) Modification – Auxiliary Power Unit (APU) Bond Strap Installation (ASC Active/One Time 15 AUG 2008
174 Active/One Time 11 AUG 2008
175/175A/175AM1 174) Active/One Time 11 JAN 2009
176 Engine Fuel Control (ATA 73) Inspection–Fuel Metering Unit - Independent Overspeed Protection Coil Wiring Active/One Time 05 JUN 2009
177/177A Landing Gear (ATA 32) Modification – Nose Landing Gear Uplock Hook Spring (ASC 180) Active/One Time 17 MAR 2009
178/178AM1 Water / Waste (ATA 38) Inspection – Water System Supply Line Motor Drain Valve Active/One Time 05 JUN 2009
179 Wings (ATA 57) Inspection – Wing Rear Beam – Flight Spoiler Actuator Attachment Point Active/One Time
180 Flight Controls (ATA 27) Inspection – Rudder Cable Guide Bracket Active/One Time 16 FEB 2010
181 Equipment / Furnishings (ATA 25) Inspection – Divan Seat Belt Anchor Installation Active/One Time 14 MAY 2010
182 Wings (ATA 57) Modification – Wing Rear Beam – Flight Spoiler Actuator Attachment Point (ASC 189) Active/One Time 14 MAY 2010
183 Equipment / Furnishings (ATA 25) Inspection – WINSLOW Life Raft Active/One Time 03 MAY 2010
Equipment / Furnishings (ATA 25) Inspection – WINSLOW Life Raft
184 Equipment / Furnishings (ATA 25) Modification – Pilot/Copilot Seat - Forward / Aft Adjustment Control Lever Active/One Time 14 MAY 2010
185 Flight Controls (ATA 27) Inspection – Horizontal Stabilizer Actuator Active/One Time 15 OCT 2010
186 Engine (ATA 72) General – Change of Life Counting Method for Touch-and-Go and Overshoot (Rolls-Royce Active/One Time 21 JUN 2011
187 Active/One Time 21 JUN 2011
188 Alert SB-BR700-72- A900504) Active/One Time 02 JUL 2013
189 Landing Gear (ATA 32) Modification – Sealing of Nose Wheel Steering Electrical Connectors Active/One Time 29 SEP 2011
Powerplant (ATA 71) Inspection – Engine Electronic Controller Lane A Harness 1A

Fuel (ATA 28) Replacement - Fuel Quantity Signal Conditioner to Install Revision F Software
Hydraulic Power (ATA 29) – Inspection – Left Engine Hydraulic Pressure Line
Landing Gear (ATA 32) Modification – Landing Gear Door Close – Restrictor Installation (ASC 200)
Fuselage (ATA 53) Inspection – Enhanced Vision System (EVS) Radome Support Strut, P/N 1159SCAM561

G-V S/N XXXX Page 18
07 AUG XXXX

CB No. G-V CUSTOMER BULLITENS (CB’s) (continued) STATUS/INTREVAL DATE C/W
190 Active/One Time 07 JUN 2012
191 TITLE Active/One Time 18 JUN 2013
192 Equipment / Furnishings (ATA 25) Modification – Tail Compartment Ladder Attach Fittings Active/One Time 07 JUN 2012
193 Active/One Time 20JAN 2012
Communications (ATA 23) Modification - Broadband Multi-link (BBML) Antenna
194/194A General (ATA 00) Non-Compliance – Stage 3 Noise Certification Active/One Time 18 JUN 2013
195/195A Fire Protection (ATA 26) Inspection – Engine / Auxiliary Power Unit (APU) Fire Bottle Thermal Relief Active/One Time 16 APR 2012
196 Discharge Port Active/One Time 18 JUL 2012
197 Active/One Time 04 APR 2014
198/198A Flight Controls (ATA 27) Inspection - Elevator Trim Tab Outboard Hinge Fitting Active/One Time 22 SEP 2012
199 Auxiliary Power Unit (ATA 49) Inspection – Auxiliary Power Unit (APU) Enclosure Thermal Barrier Coating Active/One Time 06 FEB 2014
200 Flight Controls (ATA 27) Inspection – Flight Control Surfaces Paint Thickness Active/One Time 18 OCT 2013
201 Fuel (ATA 28) Replacement – Fuel Boost Pumps, P/N 1159SCP500-5 Active/One Time 16 SEP 2014
202/202A Active/One Time 16 NOV 2012
203 Flight Controls (ATA 27) Inspection - Rudder Actuator Pressure Monitoring Port Plugs Active/One Time 17 FEB 2014
204/204A Active/One Time 13 JAN 2015
205 Landing Gear (ATA 32) Replacement - Nose Wheel Steering Collar Hardware Active/One Time 01 FEB 2013
206/A Navigation (ATA 34) Inspection – Mode S Transponder Extended Squitter Not-Inhibited Active/One Time
207 Flight Controls (ATA 27) Removal – Aileron and Elevator Power Disconnect (ASC 202) Active/One Time N/A by S/N
208 Oxygen (ATA 35) Inspection – Oxygen System Decay Check Active/One Time 06 FEB 2014
209 Active/One Time 22 JUL 2015
210 Flight Controls (ATA 27) Modification - Aileron Cable Feed Thru Holes at FS 576.5 (ASC 204) Active/One Time
211 Active/One Time N/A by S/N
212 Fire Protection (ATA 26) Modification - Relocation of Third Engine Fire Bottle (STC ST01822AT-D) Active/One Time Due APR 2016
213/213A Flight Controls (ATA 27) Modification – Stall Barrier Stick Shaker Relocation (ASC 194) Active/One Time 22 JUL 2015
214214A Electrical Power (ATA 24) Replacement – Main Battery Chargers Active/One Time Due JUL 2018
215 Active/One Time 18 MAR 2015
Air Conditioning (ATA 21) Inspection - Wiring Adjacent to ACM Low Limit Valve Active/One Time 22 JUL 2015
216 Oxygen (ATA 35) Replacement – Oxygen System Flexible Hoses, PN O2C20T1 Active/One Time 22 JUL 2015
217 Fuselage (ATA 53) Replacement – Nose Landing Gear Aft Fairing Hinge Fitting Active/One Time
Flight Controls (ATA 27) Modification – Elevator hard-over Prevention Systems (HOPS) Improvement 03 MAR 2015
Air Conditioning (ATA 21) Inspection – Pressure Relief Valve Remote Air Filter 22 JUL 2015
Auxiliary Power Unit (ATA 49) Inspection – Auxiliary Power Unit (APU) Mount Pallet Shimming
Electrical Power (ATA 24) Modification – Aircraft Main Battery Charger
Flight Controls (ATA 27) Inspection – Rudder Actuator Aft Rod End Attaching Hardware
Hydraulic Power (ATA 29) Inspection – Engine Driven Pump (EDP) Case Drain Hydraulic Hose – Left Engine
Pylon (ASC 212)
Landing Gear (ATA 32) Inspection –Main Landing Gear Door Actuator

Inspection - Heated Fuel Return Line Coupling Nut Subassembly

**************************************THIS SPACE INTENTIONALLY LEFT BLANK*****************************************

G-V S/N XXXX Page 19
07 AUG XXXX

AIRWORTHINESS DIRECTIVE STATUS: GULFSTREAM V AIRFRAME SN:XXXX

AD AMENDMENT EFFECTIVE SUBJECT/SYSTEM COMPLIANCE COMPLIANCE METHOD OF ONE TIME/ NEXT AUTHORIZED
NUMBER NUMBER DATE EFFECTED DATE STATUS COMPLIANCE RECURRING DUE FACILITY
39-16951 3/28/2012 Equipment 05 JUN 2013 C/W C/W IAW AD REC 13267.3 GAC/DAL
74-08-09 /Furnishings CRS#VJ1R560K
R3
98-09-01 39-10480 5/5/1998 Elevator Hard-over 01 DEC 2000 C/W C/W IAW AD ONE N/A GAC/SAV
39-10731 9/18/1998 Prevention Sys. 01 DEC 2000 C/W N/A BY P/N ONE N/A CRS#GR4D216M
98-18-15 (HOPS)
Wiring Harness C/W IAW AD GAC/SAV
2001-08-13 Clearance N/A BY P/N CRS#GR4D216M
GAC/SAV
39-12191 5/10/2001 Door Control Valves 04 MAY 2001 C/W C/W IAW ONE N/A CRS#GR4D216M
of the Landing Gear ACB 12

2001-14-16 39-12327 8/21/2001 Nose Wheel 14 DEC 2001 C/W C/W IAW AD ONE N/A GAC/SAV
2001-21-06 39-12477 11/6/2001 Steering Actuator 21 JUN 2011 C/W N/A BY P/N REC AS REQ. CRS#GR4D216M
2002-21-03 39-12909 10/21/2002 24 OCT 2002 C/W N/A
Fire Extinguisher C/W IAW AD GAC/SAV
2003-18-11 39-13302 9/26/2003 Bottles 28 JUN 2003 C/W CRS#GR4D216M
2004-02-01 39-13436 2/6/2004 24 JAN 2004 C/W C/W IAW ACB19 REC
Pilot's overhead NET JETS
2004-22-16 39-13844 11/19/2004 Circuit Breaker 20 DEC 2004 C/W ACC#E7JA688H
2005-16-14 39-14220 8/30/2005 Panel 22 AUG 2005 C/W
2006-11-03 39-14607 6/29/2006 Left and Right 02 APR 2007 C/W C/W IAW CB104 ONE N/A GAC/SAV
Ailerons CRS#GR4D216M
2006-18-08 39-14746 10/11/2006 04 DEC 2006 C/W C/W IAW AD ONE
2006-18-13 39-14752 Landing gear C/W AND CB114 N/A GAC/SAV
selector dump valve CRS#GR4D216M
G-V S/N XXXX (LGSDV)
07 AUG XXXX Crew oxygen C/W IAW AD ONE N/A GAC/SAV
bottle/supports CRS#GR4D216M
C/W IAW AD ONE
Floor heater pad NOT INSTALLED ONE N/A GAC/SAV
system CRS#GR4D216M
C/W IAW
Left and Right CB124 N/A GAC/DAL
Aileron and Elevator CRS#VJ1R560K
Actuators
Nose wheel Tires C/W IAW AD ONE N/A FIRST AVIATION
N/A BY S/N’S ONE CRS#XFRR113L
10/13/2006 Hard-over 01 JUN 2007
prevention system C/W IAW AD N/A GAC/SAV
(HOPS) in the roll N/A BY S/N CRS#GR4D216M
axis due to a short
circuit in the wiring
harness

Page 20

AIRWORTHINESS DIRECTIVE STATUS: GULFSTREAM V AIRFRAME SN:XXXX (continued)

AD AMENDMENT EFFECTIVE SUBJECT/SYSTEM COMPLIANCE COMPLIANCE METHOD OF ONE TIME/ NEXT AUTHORIZED
NUMBER FACILITY
NUMBER DATE EFFECTED DATE STATUS COMPLIANCE RECURRING DUE

2007-12-25 39-15104 7/5/2007 Forward water 21 JUN 2007 C/W C/W IAW ACB26 ONE N/A AP3070473
N/A BY S/N
drain/supply valves

2009-08-01 39-15874 5/14/2009 Honeywell FMSs 05 JUN 2009 C/W C/W IAW AD ONE N/A GAC/SAV
N/A BY P/N CRS#GR4D216M

2009-17-01 39-15991 8/26/2009 Airborne Auxiliary 17 JUL 2009 C/W C/W ACB29 PT.1 ONE N/A GDAS PBI
2011-24-02 39-16866 1/3/2012 Power 18 JUN 2013 P/C/W & PT.2 ONE AP:2158974
2012-13-12 39-17114 8/1/2012 Fire Bottle, fixed 26 JUL 2012 C/W ONE
CMP 994000 N/A GAC/DAL
Flight Controls N/A CRS#VJ1R560K

N/A BY S/N N/A NET JETS
AP:3326025

AIRWORTHINESS DIRECTIVE STATUS: BMW/ROLLS-ROYCE BR710A1-10, No.1 ESN:XXXXX

AD AMENDMENT EFFECTIVE SUBJECT/SYSTEM COMPLIANCE COMPLIANCE METHOD OF ONE TIME/ NEXT AUTHORIZED
NUMBER FACILITY
NUMBER DATE EFFECTED DATE STATUS COMPLIANCE RECURRING DUE

2013-05-13 04/24/2013 Fuel pump spline 18 APR 2012 C/W C/W IAW BRR REC 15096.9 NET JETS
39-17385 couplings C/W ASB-BR700-72- ONE ENGINE CRS#DXTR401D
A900509 Rev.1 HOURS
2013-03-17 39-17351 03/21/2013 High-pressure 15 FEB 2013 C/W IAW AD - N/A JAYSON KOELZER
turbine (HPT) stage N/A BY S/N N/J
1 and stage 2 discs AP:3158649

39-16842 11/23/2011 Touch-and-go and 15 DEC 2011 C/W C/W IAW AD ONE N/A NET JETS
2011-22-01 01/13/2011 overshoot on life 16 DEC 2010 C/W CRS#DXTR401D
cycle counting C/W IAW AD ONE
2010-25-05 39-16538 Turbine Discs Tracking Disks N/A C. Benenati
AP:3070473

2005-21-05 11/25/2005 22 SEP 2012 C/W C/W IAW AD REC ENGINE NET JETS
39-14343 01/31/2001 13574.0/ CRS#DXTR401D
Fan discs and fan 11 JAN 2009 C/W C/W IAW AD ONE 5670
2001-01-01 39-12071 blades 13 JUN 2001 C/W N/A BY P/N ONE N/A GAC/SAV
CRS#GR4D216M
98-24-03 R1 39-11425 Oil Filter C/W IAW SB N/A GAC/SAV
BR700-72- CRS#GR4D216M
12/27/1999 Combustion Core 100900 REV. 1
Fairings

G-V S/N XXXX Page 21
07 AUG XXXX

AIRWORTHINESS DIRECTIVE STATUS: BMW/ROLLS-ROYCE BR710A1-10, No.2 ESN:XXXXX

AD AMENDMENT EFFECTIVE SUBJECT/SYSTEM COMPLIANCE COMPLIANCE METHOD OF ONE TIME/ NEXT AUTHORIZED
NUMBER NUMBER DATE EFFECTED DATE STATUS COMPLIANCE RECURRING DUE FACILITY
2013-05-13 04/24/2013 18 APR 2012 C/W REC 15098.2 NET JETS
39-17385 Fuel pump spline C/W IAW BRR CRS#DXTR401D
2013-03-17 couplings C/W ASB-BR700-72- ONE N/A
A900509 Rev.1 JAYSON KOELZER
03/21/2013 High-pressure 15 FEB 2013 C/W IAW AD - N/J
turbine (HPT) stage N/A BY S/N AP:3158649
39-17351 1 and stage 2 discs

39-16842 11/23/2011 Touch-and-go and 15 DEC 2011 C/W C/W IAW AD ONE N/A NET JETS
2011-22-01 01/13/2011 overshoot on life 16 DEC 2010 C/W CRS#DXTR401D
cycle counting C/W IAW AD ONE
2010-25-05 39-16538 Turbine Discs Tracking Disks N/A C. Benenati
AP:3070473

2005-21-05 11/25/2005 22 SEP 2012 C/W C/W IAW AD REC ENGINE NET JETS
39-14343 13574.0/ CRS#DXTR401D
Fan discs and fan 5670
blades

2001-01-01 39-12071 01/31/2001 Oil Filter 11 JAN 2009 C/W C/W IAW AD ONE N/A GAC/SAV
98-24-03 R1 39-11425 13 JUN 2001 C/W N/A BY P/N ONE CRS#GR4D216M
12/27/1999 Combustion Core
Fairings C/W IAW SB N/A GAC/SAV
BR700-72- CRS#GR4D216M
100900 REV. 1

FAA FORM 337, STC, FMS and Repair Data

FAA FORM DESCRIPTION STC NUMBER STC FMS FMS ICA ADDITIONAL DRAWINGS/ ADD’L ON FILE
337 DATE Repair of RH N/A COVER NUMBER/DATE LOCATED ICA LOCATED DOCUMENTS/REMARKS DOC’s WITH
02/19/2012 elevator trim tab SHEET LOCATED FAA
Wing to fuselage N/A N/A N/A N/A N/A GAC DWG SE50000625
02/15/2012 fairing repair/Flight ST04216AT-D N/A Rev.E NO YES
06/22/2011 spoiler actuator
bushing repair, N/A N/A N/A N/A N/A GAC DWG SE50000625 YES YES
Rear Beam Mod CE51303A021 YES Rev.E NO YES
RBS263-272, LH YES CE51303M012 YES SE55202101,
Fixed cowl repair SE55812103,
1159SB50091, CMP GV
ATG 5000 Install 925401

CE513038016 REV. A

G-V S/N XXXX Page 22
07 AUG XXXX

FAA FORM 337, STC, FMS and Repair Data (continued)

FAA FORM DESCRIPTION STC NUMBER STC FMS FMS ICA ADDITIONAL ADD’L ON FILE
337 DATE COVER NUMBER/DATE LOCATED ICA LOCATED DOCUMENTS/REMARKS DOC’s WITH
Wing to fuselage SHEET LOCATED FAA
06/22/2011 fairing repair/Flight
03/21/2011 spoiler actuator GAC DWG SE50000625 YES
10/19/2008 bushing repair, YES
Rear Beam Mod Rev.D YES
RBS263-272, LH
Fixed cowl repair SE55202101, YES
LH Fixed cowl YES
repair SE55812103,
LH Fixed cowl YES
repair 1159SB50091, CMP GV
YES
N/A N/A N/A N/A N/A N/A 925401 NO YES
N/A N/A N/A N/A N/A YES
N/A N/A N/A N/A N/A GAC DWG SE50000625 YES
YES
N/A N/A N/A N/A N/A N/A Rev.C NO YES
YES
GAC DWG SE50000625 YES
YES
N/A Rev.B NO YES
YES
Radome Shell FAA approved data: 4276-
attachment/cut-off PCS-R2, DWG 4276X’
Flight ID Upgrade
12/20/2007 Mode-S ATC N/A PS-200 NO
05/25/2005 Wiring Deviation,
FWD/AFT ST02884AT-D YES CE51 126M000 YES CE51 126A000 YES GAC DWG CE511260070 NO
09/02/2005 Galley/Lav
Galley Outlet/CB N/A N/A N/A N/A N/A CE514960095, NO
12/21/2006 Panel, Coffee N/A CE515480024
06/18/2001 Maker MODS
06/18/2001 Custom Executive N/A N/A N/A N/A N/A N/A CE514960095 NO
06/18/2001 Interior/Avionics N/A N/A GC51 4696140 Electrical NO
06/18/2001 Cockpit Lighting ST02324AT-D YES N/A N/A N/A N/A Load Analysis NO
Mod N/A N/A NO
Pulselite ST01399AT YES N/A N/A N/A N/A GC11796132 NO
Installation GC51188 N/A N/A NO
ST01397AT YES M001/Rev 1 YES N/A N/A GC511886123 NO
AFIS w/SAT Link ST01384AT-D YES GC51306M001 YES N/A N/A GC513066126 NO
ST01523AT-D YES GC51318M002 YES N/A N/A NO
06/18/2001 FMS No. 3 ST00924LA-D YES GC51318M004 YES N/A N/A GC513186069 NO
Cockpit GC51129A001 NO NO
06/18/2001 Arrangement ST01398AT-D YES N/A N/A GC514018001 Rev. 4
Bag Compartment
06/18/2001 Equip. Relocation ST01635AT-D YES GC51468M001 NO GC514686070 Rev. A
Emergency
06/18/2001 Lighting ST01385AT-D YES N/A N/A GC514866129
06/18/2001 ST01382AT-D YES GC52712M001 YES GC527126007
06/18/2001 Oxygen System ST00673AT-D YES GC51129M001 YES GC511298001 Rev. E

TCAS 7.0

G-V S/N XXXX Page 23
07 AUG XXXX

AIRCRAFT TECHNICAL EVALUATION FINDINGS

TECHNICAL EVALUATION FINDINGS

AIRCRAFT MANUFACTURER AIRCRAFT MODEL SERIAL NUMBER REGISTRATION

Gulfstream Aerospace Corporation G-V XXXX NXXXX
Manufacturing Date: Current A/C Total Time:
DEC 2000 Current A/C Total Cycles:
12389.6
4346

UNSCHEDULED SPECIAL INSPECTIONS

INSPECTION DESCRIPTION DATE FINDINGS RESOLUTION
None Noted
N/A N/A N/A

DATE REFERENCE AIRFRAME DAMAGE HISTORY RESOLUTION
12/20/2007 Form 337 Replaced Radome Shell
10/19/2008 Form 337 DESCRIPTION Repaired
03/21/2011 Form 337 Radome Shell Attachment/Cut-off Repaired
06/22/2011 Form 337 LH Fixed Cowl Repair Repaired
02/15/2012 Form 337 LH Fixed Cowl Repair Repaired
02/19/2012 Form 337 Wing-Fuselage fairing/Flight Spoiler Actuator Bushing/Rear Beam/ Fixed Cowl Repaired
Wing-Fuselage fairing/Flight Spoiler Actuator Bushing/Rear Beam/ Fixed Cowl
Repair of RH Elevator Trim Tab

ITEM AD’s/ACB’s/CB’s/ASC’s/LOG BOOK ENTRIES STATUS/INTERVAL REQUIREMENT
CB 210
CB 212 TITLE Active/One Time Due APR 2016
Flight Controls (ATA 27) Modification – Elevator hard-over Prevention Systems (HOPS) Improvement
Auxiliary Power Unit (ATA 49) Inspection – Auxiliary Power Unit (APU) Mount Pallet Shimming Active/One Time Due JUL 2018

ITEM REFERENCE MANUAL REVISIONS
01. A/C Operating Manual
02. A/C Flight Manual DESCRIPTION
03. A/C Flight Manual Sup. Revisions 33 , 34, 35 and 36 Required
04. AFMS Revision 35 and 36 Required
05. ICA Requires Rev 2009-02
Baggage Compartment FMS GC51468M001 Not Located
TCAS 7.0 ICA GC51129A001 Not located

MISCELANEOUS

NOTE: RH ESN:XXXXX requires 1 (one) cycle added to the current Total Cycles and .3 hrs added to current Total Time. This engine was initially installed on
aircraft SN:XXXX and removed due FOD for repair. It was installed on aircraft SN:XXXX (RH) @ 5.8 TAT/4 TAC (LHESN:XXXXX times were the same as
A/C). This is a difference of +1.3 hrs/-1 cycle for ESN:XXXXX compared to ESN:XXXXX. Additionally, there is a log entry by GAC dated 02/24/2009 for RH
ESN:XXXXX that has incorrect hours and cycles documented.

END OF REPORT

G-V S/N XXXX Page 24
07 AUG XXXX