TGI 38JC258802A01 rev1.pdf

FOUO

FOUO: Public availability to be determined under 5 USC 552

TASK GROUP INSTRUCTION

AIM REV 20.11.4.0 (OCTOBER 2020)

TGI COMPONENT NAME: TYPE: PHASE: REPEAT: CHANGE:

NO.: TIE-DOWN FLIGHT DECK FG A 0 1

SHIP/HULL NO.: SHIP/HULL NAME: SYSTEM: PROJ/WO NO: CASREP CAT:

DDG-83 USS HOWARD 61111 JC2

CU PHASE TITLE:

F/O - REPLACE AIRCRAFT SECURING FITTING ON FLIGHT DECK

PREPARING ACTIVITY:

PREPARED BY: CODE PHONE DATE

HIROYUKI TANAKA 231B 315-243-4491 20-MAR-2024

APPROVED BY: CODE PHONE DATE

RYOUTA TAKAGI 231B 315-243-4502 20-MAR-2024

CONCURRED BY: CODE PHONE DATE

CONCURRED BY: CODE PHONE DATE

CONCURRED BY: CODE PHONE DATE

CONCURRED BY: CODE PHONE DATE

REASON FOR WORK/NEED FOR CHANGE:

Revise reference 2.5 was required.

CHANGE INSTRUCTIONS:

CH1: Revise reference 2.5. (05/20/2024)

SPECIAL REQUIREMENTS:

This work affects a fire zone boundary. Fabrication and/or staging of a non-flammable closure is required.

SURFMEPP

WORK CERTIFICATION SIGNATURES

COMPLETION OF WORK REVIEW: BADGE NO.: SHOP/CODE: PHONE: DATE:

ACCEPTANCE OF COMPLETED WORK

PHYSICAL INSPECTION PHYSICAL INSPECTION COMPLETED: BADGE NO.: SHOP/CODE: PHONE: DATE:

REQUIRED:☐YES ☒NO

RECORDS REVIEW: BADGE NO.: SHOP/CODE: PHONE: DATE:

TGI NO.: TIE-DOWN FLIGHT DECK FG A 0

FOUO

SHIP: DDG-83 CHG/VER: 1/1

LIST OF EFFECTIVE PAGES

SHT NO. CHG NO. SHT NO. CHG NO. SHT NO. CHG NO. SHT NO. CHG NO. SHT NO. CHG NO.

1-5 Sketch (1-2)

J-1 M-1 Engrg Inst (1)

1. SCOPE/PURPOSE

1.1 Title: Aircraft Securing Fitting on Flight Deck; replace

1.2 Location of Work:

1.2.1 Main Deck Weather, Frames between 399 and 473, Port and Starboard (Stbd)

1.3 Identification:

1.3.1 Quantity (20 EA), Aircraft Securing Fitting

Type: Type XIV-A of 2.4 Material: Forged Steel, ASTM A322 GR-8620 Remarks: See Sheet One of 2.4 and Sheet 4 of 2.3

1.3.2 Quantity (5 EA), Aircraft Securing Fitting

Type: Type VII of 2.4 Material:

Fitting Cup: Forged Steel, ASTM A322 GR-8620 Crossbar: Forged Steel, ASTM A322 GR-4130 Remarks: See Sheet One, 2, 5, and 11 of 2.4 and Sheet 3 of 2.3

1.3.3 Quantity (117 EA), Aircraft Securing Fitting on Flight Deck, Frames between 399 and 473, Port and Stbd (Existing)

Type: Type XIV of 2.4 Remarks: See Sheet One, 7, and 10 of 2.4 and 2.6 through 2.9 for material and detail

1.3.4 Quantity (5 EA), Aircraft Securing Fitting on Flight Deck, Frames between 429 and 441, Port (Existing)

Type: Type VII of 2.4 Remarks: See Sheets One, 2, 5, and 11 of 2.4, and 2.7 for material and detail

1.3.5 Quantity (4 EA), GO-NO-GO Gauge for Aircraft Securing Fitting

Material: CRES, QQ-S-766, 0.125 Inch Thickness Sheet Remarks: See Sheet 5 of 2.5 for detail

1.3.6 Quantity (20 EA), Aircraft Securing Fitting

Type: Type XIV-A of 2.4 Material: Forged Steel, ASTM A322 GR-8620 Remarks: See Sheet One of 2.4, Sheet 4 of 2.3 and Engrg Inst Enclosure-01 for detail

FOUO

SHIP: DDG-83 CHG/VER: 1/1

1.3.7 Quantity (5 EA), Aircraft Securing Fitting

Type: Type VII of 2.4 Material:

Fitting Cup: Forged Steel, ASTM A322 GR-8620 Crossbar: Forged Steel, ASTM A322 GR-4130 Remarks: See Sheets One, 2, 5, and 11 of 2.4, and Sheet 3 of 2.3, and 2.7 for detail

1.4 Security Classification: None.

1.5 Initial Condition: None.

1.6 Contractor work start date:

1.7 Contractor work completion date:

2. REFERENCES:

REF.

NO.

DOCUMENT

/DRAWING

NUMBER

DOCUMENT/DRAWING TITLE REV CHG

NO.

COPY

REQ’D

(Y/N)

SOURCE

DOC

(Y/N)

PARA SEC PG CHP

1 NSI FY-25 NAVSEA Standard Items - ORG N 2 LI FY-25 Local Standard Items - ORG N

3 PDD 803-

ELM-210214

SRF-JRMC STD ELM NDT REQT

OF ACFT SECRG FTG FOR

RECEIPT & AFTER INSTL

INSPECTION

A Y AL

L

4 DWG 803-

1916300

Aircraft Securing and Engine Run- Up Fitting

P N

5 MRC 14

8VVK N

Mooring Aids 5882X8 - Y AL L

6 DWG 100-

7026705

UNIT STRL ARR DWG - ASSY

UNIT 3340

H Y 3,3 A

7 DWG 100-

7026708

DDG-51-CLASS UNIT

STRUCTURAL ARR DWG ASSY

UNIT 3440

G Y 3,3 A

8 DWG 100-

7026712

UNIT STRL ARR DWG ASSY UNIT

H Y 3,3 A

9 DWG 169-

7027359

FABRICATION & INSTALL OF

HELICOPTER HANGER DOORS

F Y SE

E N

OT

E

3. APPENDICES:

3.1. Appendix “J” TGI Job Summary Information Sheet

3.2. Appendix "M" TGI Material List

3.3. Appendix “D” Deficiency Form

4. GENERAL REQUIREMENTS:

4.1 Not Applicable.

5. PROCEDURE:

4/16/2025

9/3/2025

C1209.3 Shimizu, 11120180, SS, 9/6/2024

Shinya.Shimizu.ja Line

FOUO

SHIP: DDG-83 CHG/VER: 1/1

5.1 Upon receipt of each new aircraft securing fitting listed in 1.3.1 and 1.3.2, accomplish following non-destructive testing (NDT) inspections.

5.1.1 Accomplish mechanical cleaning of the aircraft securing fittings to remove existing coating and foreign matter for accomplishment of NDT inspection of existing welds and surfaces.

5.1.2 Visual (VT) inspection of the aircraft securing fittings for the existing welds and surfaces in accordance with 2.3, using 2.4 for guidance. The accept or reject criteria must be in accordance with 2.3.

(I) “VT INSPECTION”

5.1.3 Liquid penetrant (PT) inspection and/or magnetic particle (MT) inspection of the aircraft securing fittings for the existing welds and surfaces in accordance with 2.3, using 2.4 for guidance. The accept or reject criteria must be in accordance with 2.3.

(I) “NDT INSPECTION”

5.1.4 Submit one legible copy, in hard copy or approved transferrable media, of a report listing results of the requirements of 5.1.2 and 5.1.3 to the SUPERVISOR.

5.2 Accomplish inspection of each existing aircraft securing fitting listed in 1.3.3 and 1.3.4 in accordance with 2.5, using 2.6 through 2.9 for guidance.

5.2.1 Fabricate each new GO-NO-GO gauge listed in 1.3.5 in accordance with 2.5.

5.2.2 Submit one legible copy, in hard copy or approved transferrable media, of a report listing results of the requirements of 5.2 to the SUPERVISOR.

5.3 Remove existing and install new each aircraft securing fitting listed in 1.3.6 and 1.3.7, at locations listed in 1.2, in accordance with 2.4 and Enclosure-01, using 2.6 through 2.9 for guidance, as designated by the SUPERVISOR.

5.3.1 Chip and grind each surface flush in way of each repair.

5.3.2 Prior to installation accomplish a fit test of each new aircraft securing fitting using hook of an aircraft lashing gear chain. Acceptance criteria: The hook will fit in each new aircraft securing fitting.

5.3.3 Record each new aircraft fitting location on Enclosure-02.

5.3.3.1 Submit one legible copy, in hard copy or approved transferable media, of a report listing results of the requirements of 5.3.2 and 5.3.3 to the SUPERVISOR.

5.3.4 Vee-out and weld a total of 10 linear inches of deteriorated and damaged welds at location listed in 1.2, as designated by SUPERVISOR.

5.3.5 Accomplish the requirements of 009-12 of 2.1, including Table 2, Columns A and B, Lines One through 7.

5.3.6 Accomplish the requirements of 009-25 of 2.1 for a local air hose test of each new weld of the aircraft securing fittings. Allowable leakage: None.

5.4 Upon completion of the static load test for each new aircraft securing fitting listed in 1.3.6 and 1.3.7, accomplish liquid penetrant (PT) inspection and/or magnetic particle (MT) inspection of welds and surfaces of each new aircraft securing fitting in accordance with 2.3. The acceptance or reject criteria must be in accordance with 2.3. See 5.6.5.

(I)(G) “NDT INSPECTION”

5.5 Accomplish the requirements of 009-32 of 2.1 for each new and disturbed surface. See 5.6.6.

FOUO

SHIP: DDG-83 CHG/VER: 1/1

5.6 Notes:

5.6.1 Planner: Code 231B H. Tanaka, 243-4491

Engineer: Code 250 Y. Gouriki, 243-4179

5.6.2 Work Integration Manager (WIM): Code 333 T. Yaginuma, 080-5419-0598

5.6.3 This TGI meets the intent of DDG CSWT File No. 130-001.

5.6.4 Removal and installation of interferences, and gas free operation, preservation of boundary spaces relating to front loading structure repair are not included in this TGI. They will be covered by a DL in the future based on Contractor submitted condition report.

5.6.5 The static load test for installed aircraft securing fittings will be covered by separated TGI (T-Phase).

5.6.6 Preservation work for each new and disturbed surface on each area listed in 1.2.1 will be covered by TGI No.

38JC263401A01 (KTR TGI).

5.6.7 Work per this instruction involves cutting an access (or removal of a door) through a fire zone bulkhead, through the hull of the ship above the turn of the bilge, through ventilation components (ducting, plenums, etc.), or through any air-tight, fume-tight or watertight bulkheads normally used to control air flow in the event of a shipboard fire. A non-flammable closure is required in accordance with COMNAVSEASYSCOM MSG R 261400Z JUL 12. The closure, if not continuously in use, shall be staged near the access, readily visible and accessible, so that any emergency responder can install the closure to affect proper air flow onboard the ship.

5.6.8 WPC will copy the following pages in reference.

REF. 2.9: Pages 4C1, 5G, 29A, 29B, 30E, and 55A

5.6.9 JCN OD01-ZAL5 is related to this TGI.

5.7 Government Furnished Material (GFM):

5.7.1 SRF-JRMC will provide GFM listed in Appendix “M”.

5.8 SRF-JRMC will provide the following service work: (TGI No. 38JC258802S02).

5.8.1 [C740] Crane and crane rigging service.

5.8.2 [X99E] Utility service, electrical.

5.8.3 [X99M] Utilities service, including low pressure air supply, water supply, and steam supply.

5.8.4 [C106.1] Safety inspection for SRF-JRMC employees.

5.8.5 [C106.2] Gas free inspection for SRF-JRMC employees.

5.8.6 [C133] QA inspection for (G) symbol(s).

5.8.7 [C135] QA inspection for (G) symbol(s).

5.8.8 [C250] Technical support for front load repair work.

TGI NO.: TIE-DOWN FLIGHT

DECK

FG A 0

FOUO

M-1

SHIP: DDG-83 CHG/VER: 1/1

APPENDIX “M”

TGI MATERIAL LIST

SYSTEM: PLANT NO.: COMPONENT NAME: TYPE: PHASE: REPEAT: CU PH

VERSION:

CASREP

CAT:

61111 TIE-DOWN FLIGHT DECK FG A 0 1

CU PHASE TITLE:

F/O - REPLACE AIRCRAFT SECURING FITTING ON FLIGHT DECK

MATERIAL REFERENCES

REF

NO.

DOCUMENT/DRAWING

NUMBER

DOCUMENT/DRAWING TITLE REV

JOB ORDER: KEY OP:

38JC258802 A01

MATERIAL LIST

ITEM

NO.

PC

NO.

REF

NO.

M

C DESCRIPTION

STOCK

NUMBER

GENERIC

MATL

TYPE LVL QA

HAZ

MAT

DOC

NO.

QTY

REQD/

UNIT

QTY

USED/

UNIT

001 M SECURING FITTING, ORDER

FOR KTR

ORIG: C231B, H.TANAKA, 243-

AIRCRAFT SECURING

FITTING, TYPE XIV-A

9B 2090 LL9605636 NA 4 N 40447466 30/EA

001 M SECURING FITTING, ORDER

FOR KTR

ORIG: C231B, H.TANAKA, 243-

AIRCRAFT SECURING

FITTING, TYPE XIV-A

9B 2090 LL9605636 NA 4 N 40477456 30/EA

002 M MOORING EYE,AIRCRAF,

ORDER FOR KTR

ORIG: C231B, H.TANAKA, 243-

9B 1730 016830506 NA 4 N 40445101 10/EA

003 M SHEET,ME, ORDER FOR KTR

ORIG: C231B, H.TANAKA, 243-

9B 9515 011166776 NA 4 N 40795215 1/SH

NOTES:

FOUO: Public availability to be determined under 5 USC 552 SHEET_____OF_____

☐ NUCLEAR APPENDIX "D"

DEFICIENCY FORM

☐ NON-NUCLEAR

1. SHIP/HULL NO.: 2a. DL or DR No.

(Circle One)

2b. REVISION: 3a. COMPONENT NAME: 3b. TYPE: 3c. PHASE: 3d. REPEAT:

DDG-83 TIE-DOWN FLIGHT DECK FG A 0

4a. ICN: 4b. KEY OP: 5. LOC SPACE/LVL: FRAME: P/S/C: 6. CAUSED BY:

38JC258802 A01

7. DESCRIPTION:

8. ORIGINATOR: NAME: BADGE: SHOP/CODE: DATE: PHONE NO.:

9. CORRECTIVE ACTION:

10. EVALUATOR: NAME: BADGE: SHOP/CODE: DATE: PHONE NO.:

FOR NON-NUCLEAR USE ONLY

11. RFD/RFW REQ’D ☐ LAR REQ'D ☐

ILS MOD REQ’D ☐

SRD/PLAN REV REQ'D ☐

DWG NO.: _____________________ S/A NO.: ___________________

12. ISOLATION SIGN: BADGE: SHOP/CODE: DATE: PHONE NO.:

SATISFACTORY:

13. SUBSAFE OQE RECORD? SIGN: BADGE: SHOP/CODE: DATE: PHONE NO.

YES ☐ NO ☐

14. CORRECTIVE ACTION SIGN: BADGE: SHOP/CODE: DATE: PHONE NO.

COMPLETE:

15. INSPECTION REQ’D? INSPECTION COMPLETE/SIGN: BADGE: SHOP/CODE: DATE: PHONE NO.

_________:YES ☐ NO ☐

16. RECORDS REVIEW SIGN: BADGE: SHOP/CODE: DATE: PHONE NO.

COMPLETE (DR ONLY)

DL’s ISSUED

(DR ONLY)

FOUO: Public availability to be determined under 5 USC 552 SHEET_____OF_____

☐ NUCLEAR Deficiency Form Continuation Sheet ☐ NON-NUCLEAR

1. SHIP/HULL NO.: 2a. DL or DR No.

(Circle One) 2b. REVISION: 3a. COMPONENT NAME: 3b. TYPE: 3c. PHASE: 3d. REPEAT:

DDG-83 TIE-DOWN FLIGHT DECK FG A 0

38JC258802A01

SKETCH

ENCLOSURE-02

38JC258802A01

SKETCH

ENCLOSURE-02