Attachment J2 - Previous Inspection Report 5017-Tank 2.pdf
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- Attached to
- API Fuel Tank Inspection - Moody AFB, GA Federal contract opportunity
- Solicitation number
- W9128F25QA016
About this file
This is an API 653 Out-of-Service Inspection Report for Tank 2 (Facility 5017) at Moody Air Force Base in Georgia, conducted by Pond on May 4-5, 2020. The report documents a detailed inspection of a 35-foot diameter, 28.5-foot high welded carbon steel vertical aboveground Jet-A (F-24) storage tank with a nominal capacity of 4,500 barrels (189,000 gallons).
The inspection identified several mandatory repairs requiring immediate attention, including repairs to three shell plate pits with depths between 0.060-0.075 inches, horizontal seam weld repairs, and replacement of two internal floating roof panels. Short-term recommended repairs include removal of internal weld projections, replacement of primary wiper seals, and various coating repairs. The report provides extensive documentation of tank measurements, ultrasonic thickness testing results, settlement evaluations, and photographic evidence. Based on the inspection results, the next internal inspection is recommended for May 2040 (contingent on completing mandatory repairs), with an external inspection recommended for May 2025. The tank's cathodic protection system was found operational with acceptable readings, and the tank foundation showed no significant settlement issues.
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Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| Attachment J4 - Previous Inspection Report 5019-Tank 4.pdf | ||
| Attachment J3 - Previous Inspection Report 5018-Tank 3.pdf | ||
| Attachment J1 - Previous Inspection Report 5016-Tank 1.pdf | ||
| Attachment 4-Addendum to 52.212-1.pdf | ||
| Wage Determination.pdf | ||
| Attachment E - Inspection Telecon Briefing Template.docx | DOCX document | |
| Attachment D - MCP and MS Report.xlsx | XLSX spreadsheet | |
| Attachment C - Fuel Storage Tank Data Sheet.xlsx | XLSX spreadsheet | |
| Attachment A - General Installation Security Requirements.pdf | ||
| Attachment 2 - Performance Work Statement (PWS).pdf | ||
| Attachment 1 - CLIN Schedule.pdf | ||
| Attachment I - API External Template.docx | DOCX document | |
| Attachment B - Fuel Storage Tank LIst.xlsx | XLSX spreadsheet | |
| Combined Synopsis-Solicitation Moody AFB.pdf |
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Text version
Gilbane Tanks K1002 and W0003 – Post Repair API 653 Inspections
June 19, 2019
All Pond marketing materials are printed on papers containing post-consumer recycled fibers and are FSC Certified.
June 25, 2020
Ronald J. Weiser
Project Manager ronald.j.wieser@usace.army.mil
USACE, Omaha District
Contract Number: W9128F-17-D-0016
Task Order Number: W9128F20F0026
Submittal Number: 028
Per SOW para 2.4.1 and 2.4.1.2, see attached for the following document(s):
1. Moody AFB – Tank 2 (Facility 5017) API 653 Out-of-Service Inspection Report – Final
2. Attachment C – Tank 2 (Facility 5017) Fuel Storage Tank Excel Document
Respectfully submitted, Pond
Anthony E, Chinn, EIT
Program Manager | Mechanical Integrity chinna@pondco.com
678-591-5242
CC: John Anna - john.anna@us.af.mil
Michael Deeker - michael.deeker@dla.mil
Rueben Watson - ruben.watson@dla.mil
Daniel Cook - Daniel.1.cook@dla.mil
William Delos Santos - william.delossantos@dla.mil
James Lee - james.b.lee85.mil@mail.mil
Larry Frazier - Larry.Frazier.1@us.af.mil mailto:ronald.j.wieser@usace.army.mil mailto:chinna@pondco.com mailto:john.anna@us.af.mil mailto:michael.deeker@dla.mil mailto:ruben.watson@dla.mil mailto:Daniel.1.cook@dla.mil mailto:Larry.Frazier.1@us.af.mil
US Army Corps of Engineers Omaha District
API 653 Out-of-Service Inspection Report
Moody Air Force Base Facility 5017
Tank 2
US Army Corps of Engineers Center of Expertise for Petroleum, Oils and Lubricants
(USACE POL-MCX)
05/05/2020
API 653 Out-of-Service Inspection Report Moody AFB, Georgia
TABLE OF CONTENTS
ACRONYMS AND ABBREVIATIONS
GENERAL SUMMARY
INSPECTION DATE
STATE REGULATIONS
PREVIOUS INSPECTION DATES
RECOMMENDED FUTURE INSPECTION DATES
GENERAL TANK INFORMATION
A. GENERAL PROJECT INFORMATION
1. API 653 OOS (INTERNAL) INSPECTION
2. SITE INFORMATION
B. TANK INSPECTION COMMENTS
1. TANK CONSTRUCTION
2. TANK FOUNDATION
3. TANK BOTTOM
4. TANK SHELL
5. FIXED ROOF
6. TANK APPURTENANCES
7. TANK AND PIPING COATING
8. TANK PIPING SYSTEM
9. FIRE PROTECTION SYSTEM
10. SECONDARY CONTAINMENT
11. CATHODIC PROTECTION
C. FINDINGS AND RECOMMENDATIONS
1. MANDATORY REPAIRS PER API 650/653, UFC 3-460-01/3-460-03, OR DoD AW 78-24-27
2. SHORT-TERM RECOMMENDED REPAIRS
3. LONG-TERM RECOMMENDED REPAIRS
APPENDIX A: ENGINEERING CALCULATIONS AND DRAWINGS
NEXT INSPECTION
API/OSHA ACCESS STRUCTURE REPORT
APPENDIX B: API 653 CHECKLISTS FOR TANK INSPECTIONS
APPENDIX C: PHOTOGRAPHS
ACRONYMS AND ABBREVIATIONS
AFB Air Force Base
AFFF Aqueous Film Forming Foam
API American Petroleum Institute
ATG Automatic Tank Gauge
BBL Barrel
BMP Best Management Practices
CP Cathodic Protection
DB&B Double Block and Bleed
DFT Dry Film Thickness
DoD Department of Defense
FML Flexible Membrane Liner
HHLA High-High Level Alarm
HLA High Level Alarm
HLCV High Level Control Valve
IAW In Accordance With
ICCP Impressed Current Cathodic Protection
IFR Internal Floating Roof
LLA Low Level Alarm
LLLA Low-Low Level Alarm
MFL Magnetic Flux Leakage
NACE NACE International
NDT Non-Destructive Testing
NFPA National Fire Protection Association
OSHA Occupational Health and Safety Administration
OOR Out-of-Roundness
OOS Out-of-Service
PST Product Saver Tank
RMMR Recurring Maintenance and Minor Repair
SS Soil-Side
TLG Tape Level Gauge
TS Top-Side
UFC Unified Facilities Criteria
USACE United States Army Corps of Engineers
UTT Ultrasonic Thickness Testing
VT Visual Testing
GENERAL SUMMARY
Pond was retained by the United States Army Corps of Engineers (USACE) to provide an out-of-service (OOS) tank inspection for Tank 2 (Facility 5017) at Moody Air Force Base (AFB) in Valdosta, Georgia.
The OOS inspection was performed 4-5 May 2020. Results of this inspection identified mandatory and recommended repairs/upgrades to fully comply with applicable sections of American Petroleum Institute (API) 650/653, Unified
Facilities Criteria (UFC) 3-460-01/3-460-03, Department of Defense (DoD) standard AW 78-24-27, National Fire
Protection Association (NFPA) 407, Occupational Safety and Health Administration (OSHA) guidelines, industry standards, and best management practices (BMP).
Tank 2 is a welded, carbon steel, vertical, aboveground Jet-A (F-24) storage tank. The tank is assumed to be constructed to API 12C standards by an unknown manufacture in 1953 and was repaired by Toltest in April 2007 to
API 653, 3rd Edition, Addendum 1. The tank is 35’-0” in diameter and 28’-6” high with a nominal capacity of 4,500
Barrels (BBL) (189,000 gallons).
Testing and inspection activities were performed in accordance with (IAW) applicable sections of API 653, 5th
Edition. This report contains a detailed account of the tank inspection, non-destructive testing (NDT) methods, and conclusions derived from the inspection and testing activities. Findings from this inspection are further detailed in
Section B – Tank Inspection Comments. Mandatory and recommended repairs/upgrades identified in Section B are further classified and listed in Section C – Findings and Recommendations.
INSPECTION DATE
API Out-of-Service (Internal) Inspection Date: 4-5 May 2020 Equipment Used:
Manufacturer: MFE Enterprises Tank Floor Scanner Model Number: MFE 2412 Mark III Calibration Method: Manufacturer Calibrated
Manufacturer: GE Krautkramer Ultrasonic Thickness Gauge Model Number: DMS GO+ Calibration Method: One-Point Calibration
Manufacturer: Fischer Technologies Dry Film Thickness (DFT) Gauge Model Number: Dual Scope MPOR Calibration Method: Calibration to Known Thickness Standard
Manufacturer: Johnson Model Number: Self-Leveling Rotary Laser Level Calibration Method: N/A
Manufacturer: Fluke Model Number: True RMS Multimeter Calibration Method: Manufacturer Calibrated
Inspector(s):
Chris N. Thompson Christopher A. Walker, EIT Chris R. Peterson
STATE REGULATIONS
State Regulation for API In-Service Tank Inspections: N/A State Regulation for API Out-of-Service Tank Inspections: N/A
PREVIOUS INSPECTION DATES
API Out-of-Service (Internal) Inspection Date: February 2018 API In-Service (External) Inspection Date: February 2018
RECOMMENDED FUTURE INSPECTION DATES
API Out-of-Service (Internal) Inspection Date: May 2040* API In-Service (External) Inspection Date: May 2025 *Twenty (20) year inspection interval is only valid upon completion of all mandatory repairs.
Chris N. Thompson Christopher A. Walker, EIT Chris R. Peterson
API 653 Inspector # 34955 Integrity Engineer Integrity Engineer
ASNT NDT Level III API 570 Inspector # 85282
ASNT NDT Level I/II
GENERAL TANK INFORMATION
ITEM DESCRIPTION
Owner United States Air Force
Location Moody AFB
Facility Number 5017
Tank Number 2
State / Country Georgia / USA
City Valdosta
Inspection Date 4-5 May 2020
Tank Manufacturer Original: Unknown Repaired By: Toltest, Inc.
Design Standard Original: API 12C (Assumed) Repaired: API 653, 3rd Edition, Addendum 1
Date of Construction 1953
Tank Contents Jet-A (F-24)
Tank Serial Number N/A
Tank Diameter 35’-0”
Shell Height 28’-6”
Product Height* 26’-6”
Tank Capacity 4,500 BBL (189,000 Gallons)
Foundation Concrete Ringwall
Construction
Bottom: Lap-Welded
Shell: Butt-Welded
Fixed Roof: Lap-Welded
Floating Roof: Honeycomb Pan
Material
Bottom: Carbon Steel
Shell: Carbon Steel
Fixed Roof: Carbon Steel
Floating Roof: Aluminum
Cathodic Protection (CP) Impressed Current Cathodic Protection (ICCP)
Interior Coating System* Epoxy
Exterior Coating System* Epoxy with Polyurethane Topcoat
Level Gauging Enraf Automatic Tank Gauge (ATG) and Varec Tape Level Gauge (TLG)
Overfill Protection High Level Alarm (HLA) / High-High Level Alarm (HHLA) / High-Level Control Valve (HLCV) Float Pilot
Piping
Receipt: 8-inch Carbon Steel
Main Suction: 16-inch Carbon Steel
Low Suction: 4-inch Carbon Steel
Water Draw-Off: 1 ½-inch Carbon Steel
Level Alarms HLA/HHLA and Low-Level Alarm (LLA)/Low-Low Level Alarm (LLLA)
Notes:
*Repair drawings and the previous OOS inspection reports dated July 2012 and March 2018 were available for review and comparison.
A. GENERAL PROJECT INFORMATION
1. API 653 OOS (INTERNAL) INSPECTION
The OOS inspection was performed 4-5 May 2020. Results of this inspection identified recommended repairs/upgrades to fully comply with applicable sections of API 650/653, UFC 3-460-01/3-460-03, DoD standard AW 78-24-27, NFPA 407, OSHA guidelines, and industry standards.
2. SITE INFORMATION
The Major Command at Moody AFB is the Air Combat Command. The 23rd wing is the home of the world famous “Flying Tigers”, combat search and rescue, and security forces warriors. The 23rd wing consists of “first in” combat search and rescue, close air support, forward air control, interdiction and force protection airmen who conduct worldwide operations in support of United States national security interests and the global war on terror. Additionally, under the wing’s command is the 563rd rescue group at Davis-Monthan AFB with an operating location at Nellis AFB.
B. TANK INSPECTION COMMENTS
1. TANK CONSTRUCTION
Tank 2 is a welded, carbon steel, vertical, aboveground Jet A (F-24) storage tank. The tank is assumed to be constructed to API 12C standards by an unknown manufacture in 1953 and was repaired by
Toltest in April 2007 to API 653, 3rd Edition, Addendum 1. The tank is 35’-0” in diameter and 28’-6” high with a nominal capacity of 4,500 Barrels (BBL) (189,000 gallons).
2. TANK FOUNDATION
Tank 2 is provided a concrete ringwall foundation and is in good overall condition with no signs of spalling or cracking. Four (4) leak detection ports are provided between the new and original bottom.
No fluid was expelled from the leak detection ports during inspection.
A settlement evaluation was performed during the inspection. The settlement evaluation was satisfied based on data collected. See Appendix A for settlement results.
3. TANK BOTTOM
The tank is provided a double bottom. The new tank bottom is cone-down with a 30-inch center sump and constructed of lap-welded carbon steel plates with butt-welded annular carbon steel plates. The tank bottom was examined using magnetic flux leakage (MFL), ultrasonic thickness testing (UTT), and visual testing (VT) methods. Five (5) UTT measurements were taken on each bottom and annular plate.
UTT readings were also taken circumferentially every 2-feet within 3-inches of the shell-to-bottom weld on the annular plates. UTT measurements indicated no significant signs of metal loss on bottom or annular plates. VT was performed at bottom plate lap-welds, annular plate butt-welds, and the shell-to-bottom weld. No significant findings were observed. VT was limited due to internal coating.
An MFL bottom scan was performed on accessible areas of the tank bottom to detect top-side (TS) and soil-side (SS) metal loss. During the internal MFL scan of the tank bottom and annular plates, no TS or
SS indications were identified.
Internal piping is provided with U-bolt pipe supports. Two (2) water draw-off U-bolt pipe supports are not provided isolation between the support and pipe. Contact point corrosion was observed at the time of inspection.
Refer to Drawing A-1, “Bottom Layout”, in Appendix A for bottom plate locations, Table 1, “Bottom UTT
Measurements”, in Appendix A for tank bottom plate UTT measurements, and Table 2, “Bottom
Circumferential UTT Measurements”, in Appendix A for tank bottom circumferential UTT measurements.
4. TANK SHELL
The tank shell is equipped with five (5) fully coated, butt-welded, carbon steel shell courses. Shell plates were examined using UTT and VT methods. Nine (9) UTT measurements were taken on each plate of the 1st shell course, three (3) UTT measurements on each insert plate, and ten (10) UTT measurements on each of the 2nd through 5th shell courses using the spiral staircase for access. UTT measurements indicated no significant signs of metal loss on shell plates.
Three (3) isolated pits were observed on the internal tank shell with pit depths of 0.075-inch, 0.070-inch, and 0.060-inch. Remaining life of the deepest pit based on criteria set forth in API 653, Section
4.3.2.2 is 3.23 years. The deepest pit is located within the 2nd shell course, 46-feet circumferentially from Manway 1 and 7 7/8-inches up from the horizontal seam weld and has a remaining thickness of
0.121-inches.
Pin holes were observed on the horizontal seam weld between the 1st and 2nd shell course adjacent to the receipt nozzle penetration. Coating failure with base metal exposure and surface corrosion was observed at the horizontal seam weld pin holes during inspection. An emergency recurring maintenance and minor repair (RMMR) service order will be put in place to repair pitting and horizontal seam weld pin holes before the tank is put back in service.
Three (3) weld projections on the internal tank shell exhibit porosity, lack of fusion, voids, and pin holes, creating crevice corrosion on the tank shell. Weld projections limit accessibility to inspect the tank shell. Corrosion staining was observed at weld projections and corrosion of the tank shell may be present beneath the projections.
Conduit provided for the Enraf ATG and Varec TLG is in direct contact with the tank chime and shell, hindering the ability to inspect the tank shell-to-bottom weld and accelerating coating failure.
An out-of-roundness (OOR) survey was conducted on the internal tank shell. The largest deviation from the tank nominal diameter was 1 1/8-inches at 3-feet above the shell-to-bottom weld. The maximum allowable deviation more than a 1-foot above the shell-to-bottom weld per API 653 Table 10.2 is 3-inches. No significant signs of OOR were observed on the tank shell.
Refer to Drawing A-2, “Shell Layout”, in Appendix A for shell plate locations, Table 3, “Shell UTT
Measurements”, in Appendix A for shell plate UTT measurements, and Table 8, “Shell Out-of-Roundness
Measurements” in Appendix A for OOR results.
5. FIXED ROOF
The tank fixed roof was examined using UTT and VT methods. Five (5) UTT measurements were taken on each fixed roof plate. UTT measurements indicated no significant signs of metal loss on fixed roof plates.
The fixed roof is provided a center support for structural support of the fixed roof. The fixed roof center support is stitch welded, creating a crevice for fluid to collect, potentially accelerating coating failure and surface corrosion. Crevice corrosion and corrosion staining were observed during inspection.
Three (3) conduit supports provided for the Vito temperature/water probe are not sealed to the fixed roof. Minor coating failure was observed at the support-to-roof interface, potentially accelerating contact point corrosion.
Refer to Drawing A-3, “Fixed Roof Layout”, in Appendix A for fixed roof plate locations and Table 4, “Fixed Roof UTT Measurements”, in Appendix A for fixed roof plate UTT measurements.
6. TANK APPURTENANCES
6.1 TANK SHELL
Nozzles and appurtenances associated with the shell were inspected using UTT and VT methods. Four (4) UTT measurements were taken on each nozzle with a welded connection greater than 1-inch at four (4) quadrants (0°, 90°, 180°, and 270°). One (1) UTT measurement was taken on each associated reinforcement pad or thickened insert plate. UTT measurements indicated no significant signs of metal loss on the nozzles, reinforcing pads, or thickened insert plates.
Tank 2 is equipped with fourteen (14) shell nozzle penetrations: two (2) 36-inch manways, one (1) 8-inch receipt, two (2) 1 ½-inch LLA/LLLA nozzle penetrations, two (2) 1 ½-inch
HLA/HHLA penetrations, two (2) 2-inch HLCV float pilot penetrations, one (1) 1 ½-inch threaded plug, one (1) 16-inch main suction, one (1) 4-inch low suction, one (1) 1 ½-inch water draw-off, and one (1) 6-inch aqueous film forming foam (AFFF) discharge chamber penetration.
External coating on the LLA chamber assembly exhibits flaking and base metal exposure with surface corrosion. Manway 1 and Manway 2 are provided hinges rather than davit arms with grease fittings and are not IAW DoD standard design. Current hinges are welded directly to the nozzle flange and are not attached to the tank. Confined space labeling on each manway is faded and peeling.
Refer to Drawing A-2, “Shell Layout”, in Appendix A for shell nozzle locations and Table 6, “Nozzle/Repad UTT Measurement”, in Appendix A for nozzle and associated reinforcement pad/thickened insert plate UTT measurements.
6.2 INTERNAL FLOATING ROOF
Tank 2 is provided with an aluminum honeycomb floating pan with a double wiper seal system for fire protection. The primary wiper seal provided for the internal floating roof (IFR) is brittle, damaged, and no longer attached to the IFR. Vapor seals for the IFR access ladder and stilling well penetrations for the Enraf ATG, Vito temperature/water probe, and manual gauging hatch are damaged or no longer attached. Damaged wiper seals and IFR penetration seals allow for fuel to evaporate into the environment. The bottom skin of two (2) extra flotation panels have disbonded from the inner honeycomb cell, potentially reducing the IFR buoyancy. An emergency RMMR service order will be issued to replace the extra flotation panels before the tank is returned to service.
6.3 FIXED ROOF
Nozzles and appurtenances associated with the fixed roof were inspected using UTT and VT methods. Four (4) UTT measurements were taken on each nozzle with a welded connection greater than 1-inch at four (4) quadrants (0°, 90°, 180°, and 270°). One (1) UTT measurement was taken on each associated reinforcement pad. UTT measurements indicated no significant signs of metal loss on nozzles or reinforcing pads.
The fixed roof is provided twelve (12) nozzle penetrations: one (1) 2-inch Varec TLG, two (2)
1-inch threaded plugs, one (1) 1-inch threaded cap, three (3) 2-inch threaded plugs, one (1)
6-inch Vito temperature/water probe, one (1) 6-inch blind flange, one (1) 36-inch by 36-inch
IFR inspection hatch equipped with a 6-inch manual gauging hatch, one (1) 10-inch Enraf
ATG, and one (1) 72-inch by 24-inch IFR installation hatch.
External coating on the Vito temperature/water probe flange, Enraf ATG, and blind flange nozzles exhibit flaking and base metal exposure with surface corrosion. The IFR inspection hatch is provided with one (1) 6-inch manual gauging hatch. Currently, there is no means of locking the manual gauging hatch cover while not in use. Confined space labeling on the IFR inspection hatch is faded and peeling.
Refer to Drawing A-3, “Fixed Roof Layout”, in Appendix A for fixed roof nozzle locations and
Table 6, “Nozzle/Repad UTT Measurement”, in Appendix A for nozzle and associated reinforcement pad UTT measurements.
6.4 GAUGING
The tank is provided a manual gauging hatch for manual gauging operations. An Enraf ATG and Vito temperature/water probe are provided for automatic tank gauging and sampling operations. The Enraf ATG and Vito temperature/water probe display is attached to the bottom of the spiral staircase for checking product level from the ground. A mechanical Varec
TLG is provided for monitoring product level from the ground and is attached to the IFR. The
Varec TLG passed the field operability test and was visually inspected from the IFR. According to facility personnel, all gauges are fully functional and reading correctly.
6.5 LEVEL ALARMS
The tank is provided with independent, shell mounted alarms in the low, low-low, high, and high-high positions as well as a HLCV float pilot for overfill protection. According to facility personnel, all level alarms and the HLCV float pilot are functioning properly. Piping and nozzle connections for the HLA, HHLA, and HLCV float pilot are provided with threaded connections. Threaded connections are no longer used as they are a potential leak path.
The tank is not provided with a standard product saver tank (PST) with means of testing the level alarms and HLCV system. The PST system should include tubing to the HLA, HHLA, and
HLCV float pilot to facilitate wet testing of the chambers.
6.6 STAIRS AND PLATFORMS
The tank is provided a spiral staircase with one (1) upper platform for fixed roof access. The
HLCV float pilot extends into the path of the spiral staircase, allowing 18-inches clearance between the appurtenance and staircase railing. OSHA mandates a minimum 26-inches clearance between appurtenances and staircase railings. Handrail heights for the spiral staircase are 43-inches tall, where API requires handrails to be between 30-inches and 34-inches high.
External coating for handrails and balusters provided for two (2) concrete secondary containment access stairs, one (1) concrete main suction crossover stairs, and the spiral staircase stair treads exhibit failure with flaking, base metal exposure, and surface corrosion.
Crossover stairs provided for the main suction piping is in contact with the main suction flanged connection, potentially inducing unintentional stress to the main suction piping system during thermal expansion of the piping, stairway, and normal lateral pipe movement.
No contact point corrosion was observed during inspection.
6.7 GROUNDING AND BONDING
The tank shell is equipped with four (4) grounding cables and are in good overall condition with no signs of deterioration or fraying.
7. TANK AND PIPING COATING
The tank shell, fixed roof, and piping are provided with an epoxy polyurethane coating system. Internal coating for the tank shell exhibit spot coating failure with base metal exposure, surface corrosion, and corrosion staining. For TS corrosion protection, the tank bottom is provided with a three-coat epoxy coating system. Internal coating for the tank bottom and attachments exhibit failure with base metal exposure, surface corrosion, and corrosion staining. External coating provided for the main suction, low suction, water draw-off, and receipt piping within the internal tank exhibit failure with base metal exposure, surface corrosion, and corrosion staining. External coating for the tank shell and fixed roof exhibits widespread chalking, indicating the coating system is near the end of its life cycle. External coating on the receipt, receipt thermal relief crossover piping, PST, and secondary containment drain piping exhibits flaking, cracking, and base metal exposure with surface corrosion. Flow arrows for the receipt piping exhibit fading and peeling.
DFT was taken on the external shell, fixed roof, internal shell, and bottom. Refer to Table 5, “Tank DFT
Measurements”, in Appendix A for complete DFT data.
8. TANK PIPING SYSTEM
Piping within the containment dike is constructed of carbon steel. The low suction nozzle is not provided with a main suction branch connection, limiting the tank low suction system to aid in fuel removal during maintenance and inspection activities.
The receipt diffuser orientation is such that the flow of fuel into the tank encounters appurtenances less than 180°. AW standard design mandates that the receipt diffuser is oriented such that the flow of fuel into the tank does not encounter appurtenances for at least 180°.
Two (2) 8-inch ball valves are located upstream of the HLCV. UFC mandates that double block and bleed
(DB&B) valves are used for positive isolation of the HLCV for maintenance activities. The main suction is provided with adjustable saddle supports and a U-bolt pipe support. One (1) main suction U-bolt pipe support, adjacent to the tank shell, is not anchored to the secondary containment dike floor and may not be adequately supporting the main suction pipe. One (1) pipe support provided for the receipt thermal relief crossover piping is not provided with Teflon isolation, or equivalent, and has a loosened
U-bolt pipe support. Contact point corrosion was observed during inspection.
PST piping is provided threaded connections, one (1) sight flow indicator, and no isolation between pipe supports. Threaded connections and sight flow indicators are no longer used in this application as they are a potential leak path. The PST piping is provided an inadequate pipe supporting system.
Current configuration allows the piping to sag and is using the receipt piping for support with no isolation between the pipe support and receipt/PST piping. Coating failure and surface corrosion was observed during inspection.
9. FIRE PROTECTION SYSTEM
For internal fire protection, an aluminum honeycomb IFR is provided. Prior to the installation of the
IFR, an AFFF system was provided. Currently, the OOS AFFF system is still attached to the tank.
10. SECONDARY CONTAINMENT
Tank 2 is located within a concrete containment dike covered with a flexible membrane liner (FML).
The containment dike is capable of holding approximately 315,000 gallons of liquid, satisfying the 1-foot UFC secondary containment capacity requirement. The secondary containment is in good overall condition with no visual signs of pathways for liquid to escape in the event of a spill.
The drain provided for the secondary containment is equipped with a manually operated valve and was tested during inspection. The drain was filled with water and let sit for 24-hours to test for leaks.
After 24-hours of testing, the valve did not leak, resulting in a sealed draining system.
11. CATHODIC PROTECTION
Tank 2 is equipped with an ICCP system to protect the tank bottom from SS corrosion. The rectifier for
Tank 2 was operating at 23.31 volts and 0.24 amps. Three (3) potential readings were taken for Tank
2. All readings met the -850 millivolt National International (NACE) CP acceptance criteria. CP readings are consistent with the previous CP report dated May 2018.
C. FINDINGS AND RECOMMENDATIONS
Based on the OOS API 653 inspection of Tank 2 located at Moody AFB in Valdosta, Georgia mandatory and recommended repair/upgrades have been identified. The following recommendations outline observations from this inspection. All repair recommendations are based on applicable sections of API 650/653, UFC 3-
460-01/3-460-03, DoD Standard AW 78-24-27, NFPA 407, and industry standards.
1. MANDATORY REPAIRS PER API 650/653, UFC 3-460-01/3-460-03, OR DoD AW 78-24-27
Mandatory repairs represent items that require immediate attention, in order to prevent imminent risk to system operators, equipment integrity, or the adjacent environment. The tank should remain out of service until these repairs are completed.
1.1 Internal Shell Plate Pitting
OBSERVATION: Three (3) scattered pits were observed on the internal tank shell with pit depths of 0.075-inch, 0.070-inch, and 0.060-inch. Remaining life of the deepest pit based on criteria set forth in API 653 is 3.23 years. The deepest pit is located within the
2nd shell course, 46-feet circumferentially from Manway 1 and 7 7/8-inches up from the horizontal seam weld with a remaining plate thickness of 0.121-inches.
REFERENCE: API 653, Section 4.3.2.2
RECOMMENDATION: Provide a lap patch or puddle weld repair at three (3) pitted locations. Repairs shall be performed IAW API 653 requirements. An emergency RMMR service order will be put in place for this recommendation prior to the tank returning to service.
1.2 Horizontal Seam Weld Repair
OBSERVATION: The horizontal seam weld for the first shell course exhibits pin holes and surface corrosion.
REFERENCE: UFC 3-460-03, Section 8-4.1 (E)
RECOMMENDATION: Provide approximately 3 linear feet of weld repair on the horizontal weld seam adjacent to the receipt nozzle penetration. An emergency RMMR service order will be put in place for this recommendation prior to the tank returning to service.
1.3 IFR Flotation Panel
OBSERVATION: The bottom skin of two (2) extra flotation panels has disbonded from the inner honeycomb cell.
REFERENCE: UFC 3-460-03, Section 8-9.1.1
RECOMMENDATION: Replace two (2) extra flotation panels on the bottom side of the IFR. An emergency
RMMR service order will be put in place for this recommendation prior to the tank returning to service.
2. SHORT-TERM RECOMMENDED REPAIRS
Short-term repairs relate to the long-term preservation of the asset. Short-term repairs represent items that should be addressed in a timely manner in order to prevent future potential risks to system operators, equipment integrity, or the adjacent environment. These items may be required by federal, state, and local codes or by military criteria.
2.1 Internal Shell Weld Projections
OBSERVATION: Three (3) weld projections on the internal tank shell exhibit porosity, lack of fusion, and voids, creating crevice corrosion on the tank shell.
REFERENCE: UFC 3-460-03, Section 8-3.2 (E)
RECOMMENDATION: Remove three (3) internal weld projections on shell course 1, adjacent to the low suction, Manway 2, and the manual gauging hatch stilling well. An emergency
RMMR service order will be put in place for this recommendation prior to the tank returning to service.
2.2 IFR Primary Wiper Seal
OBSERVATION: The primary wiper seal provided for the IFR is damaged and no longer attached to the IFR.
REFERENCE: UFC 3-460-03, Section 8-9.1.1 (E)
RECOMMENDATION: Provide the IFR with a new primary wiper seal. No signs of damage or shell gapping were observed on the secondary wiper seal. An emergency RMMR service order will be put in place for this recommendation prior to the tank returning to service.
2.3 Fixed Roof Center Support
OBSERVATION: The fixed roof center support is stitch welded. Crevice corrosion and corrosion staining was observed during inspection.
REFERENCE: UFC 3-460-01, Section 8-3.9 (a)
RECOMMENDATION: Provide sealant at the fixed roof center support crevice, approximately 75 linear feet.
2.4 IFR Penetration Seals
OBSERVATION: IFR vapor seals for the IFR access ladder and stilling well penetrations for the Enraf
ATG, Vito temperature/water probe, and manual gauging hatch are damaged or no longer attached.
REFERENCE: UFC 3-460-03, Section 8-9.1.1 (E)
RECOMMENDATION: Provide IFR vapor seals at the IFR access ladder and stilling well penetrations for the Enraf ATG, Vito temperature/water probe, and manual gauging hatch.
2.5 Tank Shell Internal Coating
OBSERVATION: Internal coating for the tank shell exhibits spot failure with base metal exposure, surface corrosion, and corrosion staining.
REFERENCE: UFC 3-460-01, Section 8-3.9 (a)
RECOMMENDATION: Provide approximately 60 ft2 of spot coating repair to the internal tank shell.
2.6 Tank Internal Piping Coating
OBSERVATION: External coating for the tank receipt diffuser, main suction, low suction, and water draw-off, including pipe supports, exhibit failure with base metal exposure, surface corrosion, and corrosion staining.
REFERENCE: UFC 3-460-01, Section 8-3.9 (c)
RECOMMENDATION: Provide approximately 60 ft2 of external coating repair to the tank internal piping.
2.7 Tank Bottom Internal Coating
OBSERVATION: Internal coating for the tank bottom and appurtenances exhibit failure with base metal exposure, surface corrosion, and corrosion staining.
REFERENCE: UFC 3-460-01, Section 8-3.9 (a)
RECOMMENDATION: Provide approximately 870 ft2 (75%) of coating repair to the internal tank bottom and appurtenances.
2.8 Tank Shell External Coating
OBSERVATION: External coating for the tank shell exhibits widespread chalking. Chalking indicates the coating system is near the end of its life cycle.
REFERENCE: UFC 3-460-01, Section 8-3.10 (a)
RECOMMENDATION: Provide a full recoat of the tank shell, approximately 3,800 ft2 (100%). Prior to recoat, perform a coating condition survey, including an adhesion test, to determine if a full recoat is required or if a topcoat reapplication is sufficient.
2.9 Shell Nozzle External Coating
OBSERVATION: External coating on the LLA/LLLA chamber assembly exhibits flaking and base metal exposure with surface corrosion.
REFERENCE: UFC 3-460-01, Section 9-10
RECOMMENDATION: Provide approximately 10 ft2 of spot coating repair on the LLA/LLLA chamber assembly.
2.10 Tank Fixed Roof External Coating
OBSERVATION: External coating for the tank fixed roof exhibits widespread chalking with minor surface corrosion. Chalking indicates the coating system is near the end of its life cycle.
REFERENCE: UFC 3-460-01, Section 8-3.10 (a)
RECOMMENDATION: Provide a full recoat of the tank fixed roof, approximately 1,150 ft2 (100%). Prior to recoat, perform a coating condition survey, including an adhesion test, to determine if a full recoat is required or if a topcoat reapplication is sufficient at locations that do not have surface corrosion.
2.11 Fixed Roof Nozzles External Coating
OBSERVATION: External coating on the Vito temperature/water probe flange, Enraf ATG, and one
(1) blind flange nozzles exhibit flaking and base metal exposure with surface corrosion.
REFERENCE: UFC 3-460-01, Section 9-10
RECOMMENDATION: Provide approximately 20 ft2 of spot coating repair on the Vito temperature/water probe flange, Enraf ATG, and one (1) blind flange nozzles.
2.12 Receipt and PST Piping External Coating
OBSERVATION: External coating on the receipt, receipt thermal relief crossover piping, PST, and drain piping exhibits flaking, cracking, and base metal exposure with surface corrosion.
REFERENCE: UFC 3-460-01, Section 9-10
RECOMMENDATION: Provide approximately 5,000 ft2 of external coating repair on the receipt, PST, and drain piping.
2.13 Access and Crossover Stairs External Coating
OBSERVATION: External coating for the handrails and balusters provided for the secondary containment and crossover stairs and the spiral staircase stair treads exhibit failure with flaking, base metal exposure, and surface corrosion.
REFERENCE: UFC 3-460-03, Appendix F, Item 6
RECOMMENDATION: Provide approximately 100 ft2 of external coating repair on the for the handrails and balusters provided for the secondary containment and crossover stairs and spiral staircase stair treads.
2.14 Main Suction Crossover Stair Clearance
OBSERVATION: Crossover stairs provided for the main suction piping are in contact with the flanged connection, potentially inducing unintentional stress to the main suction piping system during thermal expansion of the stairway and normal lateral pipe movement. No contact point corrosion was observed during inspection.
REFERENCE: UFC 3-460-03, Section 6-1.5
RECOMMENDATION: Rework the main suction crossover stairs to allow clearance between the piping and the structure.
2.15 Water Draw-Off Piping
OBSERVATION: PST piping is provided threaded connections, one (1) sight flow indicator, no isolation between pipe supports, and an inadequate pipe supporting system.
REFERENCE: UFC 3-460-01, Section 9-8
RECOMMENDATION: Provide flanged or socket welded connections, remove one (1) sight flow indicator, and provide the piping system with pipe supports IAW UFC requirements.
3. LONG-TERM RECOMMENDED REPAIRS
Long-term repairs that relate to repair/upgrade of an asset to bring it up to the current standard from the standard at time of construction. Long-term repairs represent items that should be addressed in a timely manner in order to prevent future potential risks to system operators, equipment integrity, or the adjacent environment.
3.1 Low Suction Nozzle
OBSERVATION: The low suction nozzle is not provided with a main suction branch connection.
REFERENCE: UFC 3-460-01, Table 8.1 (Z)
RECOMMENDATION: Provide a branch connection between the low suction nozzle and main suction pipeline IAW AW DoD standard design.
3.2 Main Suction Pipe Support
OBSERVATION: One (1) main suction U-bolt pipe support, adjacent to the tank shell, is not anchored to the secondary containment dike floor.
REFERENCE: UFC 3-460-03, Section 6-1.5 (D), AW 78-24-33, Sheet CD.11
RECOMMENDATION: Anchor one (1) main suction pipe support to the secondary containment dike floor.
3.3 Internal Receipt Diffuser
OBSERVATION: The receipt diffuser orientation is such that the flow of fuel into the tank encounters appurtenances less than 180°.
REFERENCE: AW 78-24-27, Sheet D-08, Detail 1, Note 2
RECOMMENDATION: Orientate the receipt diffuser such that the flow of fuel into the tank does not encounter appurtenances for at least 180°.
3.4 HLCV DB&B Valves
OBSERVATION: The HLCV is equipped with two (2) 8-inch ball valves upstream of the HLCV.
REFERENCE: UFC 3-460-01, Section 6-5.D.3
RECOMMENDATION: Replace two (2) 8-inch receipt ball valves with DB&B valves.
3.5 Receipt Thermal Relief Crossover Piping
OBSERVATION: One (1) pipe support provided for the receipt thermal relief crossover piping is not provided with Teflon isolation, or equivalent, and has a loosened U-bolt pipe support.
REFERENCE: UFC 3-460-03, Section 6-1.5, AW 78-24-33, Sheet CD.11
RECOMMENDATION: Provide the receipt thermal relief crossover piping with Teflon isolation, or equivalent, and tighten the U-bolt pipe support.
3.6 Manual Gauging Hatch
OBSERVATION: The cover for the manual gauging hatch is not provided a latch.
REFERENCE: BMP
RECOMMENDATION: Provide a latch for the manual gauging hatch to secure the cover while not in use.
3.7 Fixed Roof Conduit Support
OBSERVATION: Three (3) conduit supports for the Vito temperature/water probe are not sealed to the fixed roof. Coating failure was observed at the time of inspection.
REFERENCE: UFC 3-460-01, Section 8-11
RECOMMENDATION: Seal three (3) conduit supports for the Vito temperature/water probe to the fixed roof.
3.8 AFFF System
OBSERVATION: The tank is provided an AFFF and an IFR for fire prevention.
REFERENCE: UFC 3-460-01, Section 2-13.4.2
RECOMMENDATION: Remove the AFFF system, to include the discharge chamber, as it is no longer in use. Before AFFF removal, consult the local Fire Chief for approval. If approval is not granted, coat piping red IAW MIL-STD-161H.
3.9 HLA, HHLA, and HLCV Float Pilot Piping
OBSERVATION: Piping and nozzle connections for the HLA, HHLA, and HLCV float pilot are provided with threaded connections.
REFERENCE: UFC 3-460-01, Section 8-11 and 9-8 (E)
RECOMMENDATION: Provide the HLA, HHLA, and HLCV float pilot with flanged or socket welded connections.
3.10 PST System
OBSERVATION: The tank is not provided a standard PST with means of testing the level alarms and
HLCV.
REFERENCE: AW 78-24-27, Sheet D.13 Detail 5
RECOMMENDATION: Provide the tank with a PST IAW AW standard design. The PST system should include tubing to the HLA, HHLA, and HLCV float pilot to facilitate wet testing of the chambers.
3.11 Manway 1 and Manway 2 Davit Arms
OBSERVATION: Manway 1 and Manway 2 are not equipped with davit arms provided with grease fittings.
REFERENCE: API 650, Section 5.8.3.5
RECOMMENDATION: Provide Manway 1 and Manway 2 davit arms with grease fittings.
3.12 Receipt Piping Flow Arrows
OBSERVATION: Flow arrows for the receipt piping exhibit fading and peeling.
REFERENCE: UFC 3-460-01, Section 2-17
RECOMMENDATION: Replace flow arrows for receipt piping.
3.13 Confined Space Labeling
OBSERVATION: Confined space labeling on IFR inspection hatch and two (2) manways exhibit fading and peeling.
REFERENCE: API 650, Section 5.7.2.10
RECOMMENDATION: Replace confined space labeling for the IFR inspection hatch and two (2) manways.
3.14 Spiral Staircase Clearance
OBSERVATION: The clearance between the HLCV float pilot and spiral staircase handrail is approximately 18-inches, less than OSHA required 26-inch clearance. Additionally, handrail heights are 43-inches tall, where API requires handrails to be between
30-inches and 34-inches high.
REFERENCE: OSHA 1910.25 (d)(1)
RECOMMENDATION: Extend the stair treads or provide a work platform at the HLCV float pilot to allow for minimum 26-inches of clear space between the spiral staircase handrail and appurtenance and rework the handrails to achieve a height of 30-inches to 34-inches IAW API.
3.15 Internal Pipe Supports
OBSERVATION: The internal pipe supports for two (2) water draw-off supports are not provided with isolation.
REFERENCE: AW 78-24-27, Sheet D.08 Detail 6
RECOMMENDATION: Provide Teflon isolation or Teflon coated u-bolts at two (2) water-draw supports.
3.16 Enraf ATG and Varec TLG Conduit
OBSERVATION: Conduit provided for the Enraf ATG and Varec TLG is in direct contact with the tank chime and shell. No contact point corrosion was observed.
REFERENCE: BMP
RECOMMENDATION: Rework the conduit provided for the Enraf ATG and Vito temperature/water probe to avoid direct contact with the tank chime and shell.
APPENDIX A: ENGINEERING CALCULATIONS AND DRAWINGS
3 4 56
14 15
MW1
MW2
WATER DRAW-OFF
SUPPORT (TYP.2)
FIXED ROOF
SUPPORT (TYP.4)
RECEIPT, MAIN SUCTION,
LOW SUCTION SUPPORT
(TYP.6)
ENRAF ATG
IFR ACCESS
LADDER/MANUAL GAUGE
HATCH (TYP.2)
ANTI-ROTATION CABLE
(TYP.2)
IFR LEG SUPPORT
(TYP.5)
VITO PROBE
SUPPORT (TYP.2)
SUMP
LAP PATCH
(TYP.3)
C O
N T
R A
C T
N
O
F I L E
A M
E
D W
N
B
Y
C K
D
B
Y
D E
S I G
N E
D
B
Y
D E
S C
R I P
T I O
N
D
2 3
C
A
B
M A
R K
A P
P R
D A
T E
F I
U M
B E
R
S I Z
E
S U
B M
I T
T E
D
B
Y
P L O
T
S
C A
L E
P
L O
T
D
A T
E
D A
T E
M A
R K
D E
S C
R I P
T I O
N
D E
L I V
E R
Y
O
R D
R
SHEET
IDENTIFICATION
D A
T E
A P
P R
SHEET OF
U S
A
R M
Y
C
O R
P S
F
E
N G
I N
E E
R S
O M
A H
A
N
E
O M
A H
A
D
I S
T R
I C
T
V A
L D
O S
T A
G
A
M O
O D
Y
A
F B
T A
K
Y
O U
T
N T
S
N A
W
F
D
W
F
F
A N
S I
B
P a r k w a y
L a n e
S u i t e
P e a c h t r e e
C o r n e r s
G
A
P h o n e
F a x
J O
B
N
O
A E
C
A E
C
C A
W
N A
TANK INFORMATION
TANK NO.: TANK 2 (FACILITY 5017)
MANUFACTURER: UNKNOWN
YEAR BUILT: 1953
TANK DIAMETER: 35'-0"
TANK HEIGHT: 28'-6"
NOMINAL CAPACITY: 4,500 BBL
PRODUCT: JET-A (F-24)
PRODUCT SPECIFIC GRAVITY: 0.84
GPS COORDINATES: 30.970092°, -83.210410°
N A
B O
T T
M
Y
O U
T
A-1
C O
N T
R A
F I
M
E
D W
N
B
Y
C K
D
B
Y
D E
S I G
N E
D
B
Y
D E
S C
R I P
T I O
N
D
2 3
C
A
B
M A
R K
A P
P R
D A
T E
F I
M
B E
R
S I Z
E
S U
B M
I T
T E
D
B
Y
P L O
T
S
C A
L E
P
L O
T
D
A T
E
D A
T E
M A
R K
D E
S C
R I P
T I O
N
D E
L I V
E R
Y
O
R D
SHEET
IDENTIFICATION
D A
T E
A P
P R
SHEET OF
U S
A
R M
Y
C
O R
E
N G
I N
E E
R S
O M
A H
A
N
E
O M
A H
A
D
I S
T R
I C
T
V A
L D
O S
T A
G
A
M O
O D
Y
A
F B
T A
Y
O U
T
N T
S
N A
W
F
D
W
F
F
A N
S I
B
P a r k w a y
L a n e
S u i t e
P e a c h t r e e
C o r n e r s
G
A
P h o n e
F a x
J O
B
N
O
A E
C
A E
C
C A
W
N A
TANK INFORMATION
TANK NO.: TANK 2 (FACILITY 5017)
MANUFACTURER: UNKNOWN
YEAR BUILT: 1953
TANK DIAMETER: 35'-0"
TANK HEIGHT: 28'-6"
NOMINAL CAPACITY: 4,500 BBL
PRODUCT: JET-A (F-24)
PRODUCT SPECIFIC GRAVITY: 0.84
GPS COORDINATES: 30.970092°, -83.210410°
N A
LEGEND:
- UTT READING (INCHES)
NOTES:
1. REFER TO TABLE 2, "BOTTOM CIRCUMFERENTIAL UTT
MEASUREMENTS", IN APPENDIX A FOR BOTTOM
CIRCUMFERENTIAL UTT MEASUREMENTS.
2. REFER TO TABLE 1, "BOTTOM UTT MEASUREMENTS", IN
APPENDIX A FOR BOTTOM PLATE UTT MEASUREMENTS.
.XXX
SUMP DETAIL
.486
.488
.482
.484
.526
.531
.525 .522
ROOF PERIMETER HANDRAIL
GROUNDING
CABLE (TYP. 4)
VAREC TLG
VAREC
VAREC TLG SUPPORT
(TYP.4)
LEAK DETECTION
PORT (TYP. 4)
CONCRETE
RINGWALL
NEW BOTTOM
ORIGINAL BOTTOM
LLA/LLLA
SUPPORT (TYP.2)
CONDUIT SUPPORT
(TYP.10)
AFFF SUPPORT
(TYP.2)
OVERFLOW VENT
(TYP.2)
1-2 1-3 1-41-1
2-1
3-1
4-1
5-1
5-4 5-2 5-3
2-2 2-3 2-4
3-43-33-2
4-4 4-2 4-3
MW1
N1
N3
N2
N4
N5
N6
N7
N8
MW2
N9
N10
N12
N11
4'-6"
6'-0"
6'-0"
6'-0"
6'-0"
1'-6"
NAMEPLATE
.244
.243
.242
.264
.265
.259
.245
.244
.244
.345
.247
.249
UPPER PLATFORM
C O
N T
R A
F I
M
E
D W
N
B
Y
C K
D
B
Y
D E
S I G
N E
D
B
Y
D E
S C
R I P
T I O
N
D
2 3
C
A
B
M A
R K
A P
P R
D A
T E
F I
M
B E
R
S I Z
E
S U
B M
I T
T E
D
B
Y
P L O
T
S
C A
L E
P
L O
T
D
A T
E
D A
T E
M A
R K
D E
S C
R I P
T I O
N
D E
L I V
E R
Y
O
R D
SHEET
IDENTIFICATION
D A
T E
A P
P R
SHEET OF
U S
A
R M
Y
C
O R
E
N G
I N
E E
R S
O M
A H
A
N
E
O M
A H
A
D
I S
T R
I C
T
V A
L D
O S
T A
G
A
M O
O D
Y
A
F B
T A
Y
O U
T
N T
S
N A
W
F
D
W
F
F
A N
S I
B
P a r k w a y
L a n e
S u i t e
P e a c h t r e e
C o r n e r s
G
A
P h o n e
F a x
J O
B
N
O
A E
C
A E
C
C A
W
N A
TANK INFORMATION
TANK NO.: TANK 2 (FACILITY 5017)
MANUFACTURER: UNKNOWN
YEAR BUILT: 1953
TANK DIAMETER: 35'-0"
TANK HEIGHT: 28'-6"
NOMINAL CAPACITY: 4,500 BBL
PRODUCT: JET-A (F-24)
PRODUCT SPECIFIC GRAVITY: 0.84
GPS COORDINATES: 30.970092°, -83.210410°
N A
S H
E L
L
L
A Y
O U
T
A-2
NOTES:
1. REFER TO TABLE 3, "SHELL UTT MEASUREMENTS", IN APPENDIX
A FOR INDIVIDUAL SHELL PLATE UTT READINGS.
2. REFER TO TABLE 6, "NOZZLE / REPAD UTT MEASUREMENTS", IN
APPENDIX A FOR INDIVIDUAL SHELL PLATE UTT READINGS.
NOZZLE
SCHEDULE
NOZZLE SIZE NOTES
MW1 36" MANWAY
N1 8" RECEIPT
N2 1
" LLA/LLLA
N3 1
" LLA/LLLA
N4 1
" HLA/HHLA
N5 1
" HLA/HHLA
N6 1
" HLCV FLOAT PILOT
N7 1
" THREADED PLUG
N8 1
" HLCV FLOAT PILOT
MW2 36" MANWAY
N9 16" MAIN SUCTION
N10 4" LOW SUCTION
N11 1
" WATER DRAW-OFF
N12 6"
AFFF DISCHARGE
CHAMBER
LEGEND:
- UTT READING (INCHES).XXX
SPIRAL
STAIRCASE
MANUAL GAUGING
HATCH
1 2 3 4
5 6 7
8 9
10 11
15 16
17 18
N16
N13
N14
N15
N17
N18
N19
N20
N21
N22
N23
N24
LAP PATCH
(TYP.12)
CONDUIT SUPPORT
(TYP.3)
WELDED NUT
PERIMETER VENT
(TYP.2)
C O
N T
R A
F I
M
E
D W
N
B
Y
C K
D
B
Y
D E
S I G
N E
D
B
Y
D E
S C
R I P
T I O
N
D
2 3
C
A
B
M A
R K
A P
P R
D A
T E
F I
M
B E
R
S I Z
E
S U
B M
I T
T E
D
B
Y
P L O
T
S
C A
L E
P
L O
T
D
A T
E
D A
T E
M A
R K
D E
S C
R I P
T I O
N
D E
L I V
E R
Y
O
R D
SHEET
IDENTIFICATION
D A
T E
A P
P R
SHEET OF
U S
A
R M
Y
C
O R
E
N G
I N
E E
R S
O M
A H
A
N
E
O M
A H
A
D
I S
T R
I C
T
V A
L D
O S
T A
G
A
M O
O D
Y
A
F B
T A
Y
O U
T
N T
S
N A
W
F
D
W
F
F
A N
S I
B
P a r k w a y
L a n e
S u i t e
P e a c h t r e e
C o r n e r s
G
A
P h o n e
F a x
J O
B
N
O
A E
C
A E
C
C A
W
N A
TANK INFORMATION
TANK NO.: TANK 2 (FACILITY 5017)
MANUFACTURER: UNKNOWN
YEAR BUILT: 1953
TANK DIAMETER: 35'-0"
TANK HEIGHT: 28'-6"
NOMINAL CAPACITY: 4,500 BBL
PRODUCT: JET-A (F-24)
PRODUCT SPECIFIC GRAVITY: 0.84
GPS COORDINATES: 30.970092°, -83.210410°
N A
F I X
D
O
F
L
A Y
O U
T
A-3
C O
N T
R A
F I
M
E
D W
N
B
Y
C K
D
B
Y
D E
S I G
N E
D
B
Y
D E
S C
R I P
T I O
N
D
2 3
C
A
B
M A
R K
A P
P R
D A
T E
F I
M
B E
R
S I Z
E
S U
B M
I T
T E
D
B
Y
P L O
T
S
C A
L E
P
L O
T
D
A T
E
D A
T E
M A
R K
D E
S C
R I P
T I O
N
D E
L I V
E R
Y
O
R D
SHEET
IDENTIFICATION
D A
T E
A P
P R
SHEET OF
U S
A
R M
Y
C
O R
E
N G
I N
E E
R S
O M
A H
A
N
E
O M
A H
A
D
I S
T R
I C
T
V A
L D
O S
T A
G
A
M O
O D
Y
A
F B
T A
Y
O U
T
N T
S
N A
W
F
D
W
F
F
A N
S I
B
P a r k w a y
L a n e
S u i t e
P e a c h t r e e
C o r n e r s
G
A
P h o n e
F a x
J O
B
N
O
A E
C
A E
C
C A
W
N A
TANK INFORMATION
TANK NO.: TANK 2 (FACILITY 5017)
MANUFACTURER: UNKNOWN
YEAR BUILT: 1953
TANK DIAMETER: 35'-0"
TANK HEIGHT: 28'-6"
NOMINAL CAPACITY: 4,500 BBL
PRODUCT: JET-A (F-24)
PRODUCT SPECIFIC GRAVITY: 0.84
GPS COORDINATES: 30.970092°, -83.210410°
N A
LEGEND:
- SURFACE CORROSION
NOTES:
1. REFER TO TABLE 4, "FIXED ROOF UTT MEASUREMENTS",
IN APPENDIX A FOR INDIVIDUAL SHELL PLATE UTT
READINGS.
2. REFER TO TABLE 6, "NOZZLE / REPAD UTT
MEASUREMENTS", IN APPENDIX A FOR INDIVIDUAL SHELL
PLATE UTT READINGS.
NOZZLE
SCHEDULE
NOZZLE
SIZE
NOTES
N13 1" THREADED PLUG
N14 1" THREADED CAP
N15 1" THREADED PLUG
N16 2" VAREC TLG
N17 6" BLIND FLANGE
N18 6" VITO TEMPERATURE/WATER PROBE
N19 2" THREADED PLUG
N20 2" THREADED PLUG
N21 72"x24" IFR INSTALLATION HATCH
N22 36"x36" IFR INSPECTION HATCH
N23 10" ENRAF ATG
N24 2" THREADED PLUG
TABLE 1 – BOTTOM UTT MEASUREMENTS
Plate 1 Plate 2 Plate 3 Plate 4 Plate 5 .313 .312 .313 .308 .315 .317 .314 .314 .311 .316 .311 .312 .317 .316 .316 .311 .312 .312 .310 .315 .314 .315 .313 .313 .316
Avg. .312 .311 .316 .314 .314 Plate 6 Plate 7 Plate 8 Plate 9 Plate 10 .311 .313 .310 .315 .311 .312 .305 .310 .315 .313 .313 .311 .312 .310 .312 .311 .314 .309 .313 .311 .313 .308 .309 .315 .312
Avg. .312 .312 .312 .308 .313 Plate 11 Plate 12 Plate 13 Plate 14 Plate 15 .311 .311 .314 .311 .314 .310 .309 .312 .312 .311 .319 .311 .311 .310 .311 .311 .314 .315 .309 .315 .310 .312 .310 .313 .311
Avg. .313 .312 .312 .311 .312 Plate 16 Plate 17 Plate 18 Plate 19 Plate 20 .307 .308 .310 .306 .307 .309 .307 .309 .308 .307 .309 .306 .308 .302 .306 .309 .308 .307 .307 .313 .308 .309 .307 .307 .309
Avg. .308 .307 .309 .307 .307 Plate 21 Plate 22 Plate 23 Plate 24 Plate 25 .307 .307 .304 .308 .305 .307 .309 .308 .308 .309 .308 .308 .310 .307 .307 .308 .302 .308 .310 .309 .308 .310 .308 .308 .309
Avg. .306 .308 .308 .308 .308 Plate 26 Plate 27 .308 .309 .309 .310 .309 .308 .307 .309 .308 .308
Avg. .308 .309
Thickness represented in inches.
Average bottom plate thickness: .310”
TABLE 2 – BOTTOM CIRCUMFERENTIAL UTT MEASUREMENTS
Ultrasonic Thickness Survey of Tank Floor 0' 2' 4' 6' 8' 10' 12' 14' 16' 18' 20' 22' 24' 26' 28' 30' 32'
.308 .308 .307 .309 .309 .309 .309 .308 .308 .310 .308 .307 .309 .309 .308 .308 .310 34' 36' 38' 40' 42' 44' 46' 48' 50' 52' 54' 56' 58' 60' 62' 64' 66'
.307 .306 .306 .307 .307 .313 .308 .309 .308 .307 .309 .302 .309 .307 .308 .307 .306 68' 70' 72' 74' 76' 78' 80' 82' 84' 86' 88' 90' 92' 94' 96' 98' 100'
.307 .309 .307 .308 .308 .307 .302 .304 .308 .308 .308 .310 .305 .309 .310 .307 .308 102' 104' 106' 108' 110' .309 .310 .307 .308 .308
0’ = Manway 1 Locations are within 3-inches of the shell-to-bottom weld. Thickness measurements are taken at 2 feet increments around the circumference of the tank.
Thickness measurements are in inches.
Average Bottom Circumferential Readings: .308”
TABLE 3 - SHELL UTT MEASUREMENTS
Roof
Shell Course 5
Plate 5-1 Plate 5-2 Plate 5-3 Plate 5-4
.186 .194 .193
.190 .195 .191 N/A
.194 .193 .191 .189
Avg. .192
Circumferential Weld C5
Shell Course 4
Plate 4-1 Plate 4-2 Plate 4-3 Plate 4-4
.199 .204 .205
.203 .207 .205
.203 .206 .203 .195
Avg. .203
Circumferential Weld C4
Shell Course 3
Plate 3-1 Plate 3-2 Plate 3-3 Plate 3-4
.180 .189 .189
.185 .188 .188
.191 .188 .187
.182
Avg. .187
Circumferential Weld C3
Shell Course 2
Plate 2-1 Plate 2-2 Plate 2-3 Plate 2-4
.187 .198 .200
.193 .199 .199
.196 .201 .195
.196
Avg. .196
Circumferential Weld C2
Shell Course 1
Plate 1-1 Plate 1-2 Plate 1-3 Plate 1-4
.248 .243 .263 .248 .251 .257 .244 .245 .249 .241 .243 .249
.251 .243 .263 .249 .250 .244 .243 .246 .250 .242 .244 .250
.250 .242 .256 .244 .244 .252 .239 .244 .246 .234 .239 .244
Avg. .251 .249 .245 .243
Circumferential Weld C1
Thickness represented in inches.
Average shell course 1: .247”
Average shell course 2: .196”
Average shell course 3: .187”
Average shell course 4: .203”
Average shell course 5: .192”
TABLE 4 – FIXED ROOF UTT MEASUREMENTS
Plate 1 Plate 2 Plate 3 Plate 4 Plate 5
.179 .178 .187 .179 .190 .193 .197 .196 .197 .199
.183 .186 .199 .197 .199
.180 .179 .185 .182 .189 .190 .199 .198 .198 .195
Avg. .180 .184 .192 .197 .198
Plate 6 Plate 7 Plate 8 Plate 9 Plate 10
.194 .193 .189 .187 .189 .187 .192 .188 .182 .182
.195 .187 .191 .195 .187
.195 .193 .191 .188 .188 .191 .197 .191 .184 .185
Avg. .194 .188 .189 .193 .184
Plate 11 Plate 12 Plate 13 Plate 14 Plate 15
.190 .190 .201 .201 .199 .194 .192 .194 .182 .185
.191 .202 .197 .192 .179
.187 .189 .199 .192 .197 .196 .193 .193 .183 .185
Avg. .189 .199 .197 .193 .183
Plate 16 Plate 17 Plate 18 .181 .184 .199 .199 .196 .197 .187 .200 .199 .184 .186 .200 .197 .199 .196 Avg. .184 .199 .197
Thickness represented in inches.
Average fixed roof: .191”
TABLE 5 – TANK DFT MEASUREMENTS
External Shell Coating Thickness Average Standard Deviation Number of Readings Minimum Maximum
13.24 2.78 20 8.79 18.66
Internal Shell Coating Thickness
18.08 3.54 20 13.42 25.18
Fixed Roof Coating Thickness
9.558 1.58 15 6.36 12.78
Tank Bottom Coating Thickness
19.51 4.55 15 10.62 30.43
Thicknesses are represented in mils.
TABLE 6 - NOZZLE / REPAD UTT MEASUREMENTS
Nozzle Nozzle Size
(Diameter or Width/Height)
Repad Shape
Repad Size (W X H)
Repad Thickness
Nozzle Thickness H1 H2
Nozzle Location (Measured circumferentially from Manway 1)
Notes
0⁰ 90⁰ 180⁰ 270⁰
MW1 36" B 72" .252 .246 .249 .248 .246 3'-6'' 0'-6" 0'-0" Manway 1
N1 8'' D 23" x 26" .237 .497 .481 .490 .495 1'-3'' - 26'-6'' Receipt
N2 1 ½" - - - TH TH TH TH 4'-2'' 4'-1'' 40'-0'' LLA/LLLA
N3 1 ½" - - - TH TH TH TH…
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