Stewart (Newburgh)-Fac 7401 (Tank 1)-FINAL-2017.pdf
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US Army Corps of Engineers Omaha District
API 653 In-Service Inspection Report
Stewart ANG (Newburgh), New York Tank Facility 7401
Tank 39-400 (Tank 1)
US Army Corps of Engineers Center of Expertise for Petroleum, Oils and Lubricants
USACE POL-MCX
1 September 2017
API 653 In-Service Inspection Report Stewart ANG, New York
Table of Contents
ACRONYMS AND ABBREVIATIONS
GENERAL SUMMARY
THIS INSPECTION
PREVIOUS INSPECTION DATES
RECOMMENDED FUTURE INSPECTION DATES
GENERAL TANK INFORMATION
A. GENERAL PROJECT INFORMATION
1. API 653 Inspection
2. Site Information
B. TANK INSPECTION COMMENTS
1. Tank Construction
2. Tank Foundation
3. Tank Shell
4. Tank Appurtenances
5. Tank Coating
6. Tank Piping System
7. Fire Protection System
8. Secondary Containment
C. FINDINGS AND RECOMMENDATIONS
1. Mandatory Repairs per API 653, UFC 3-460-01, or AW 78-24-27 Standards
2. Significant Findings per API 653, UFC 3-460-01, or AW 78-24-27 Standards
3. Repairs to Fully Comply with API 653, UFC 3-460-01, or AW 78-24-27 Standards
4. Recommended Repairs as Part of Regular Maintenance
APPENDIX A: ENGINEERING CALCULATIONS AND DRAWINGS
SHELL ROUNDNESS SURVEY & SETTLEMENT
SHELL SETTLEMENT SURVEY
SHELL THICKNESS CALCULATIONS
SHELL/ROOF ULTRASONIC THICKNESS MEASUREMENTS
TANK DRAWINGS
OSHA ACCESS STRUCTURE REPORT
APPENDIX B: API 653 CHECKLISTS FOR TANK INSPECTIONS
APPENDIX C: PHOTOGRAPHS
ACRONYMS AND ABBREVIATIONS
API American Petroleum Institute
ASME American Society of Mechanical Engineers
ASNT American Society of Non-Destructive Testing
ATG Automatic Tank Gauge
BBL Barrel
CFR Code of Federal Regulations
CP Cathodic Protection
DFT Dry Film Thickness
FAC Facility
HLA High Level Alarm
HLCV High Level Control Valve
HHLA High-High Level Alarm
LLA Low Level Alarm
LLLA Low-Low Level Alarm
MFL Magnetic Flux Leakage
MFE Magnetic Flux Exclusion
MT Magnetic Particle Testing
NA Not Applicable
NACE National Association of Corrosion Engineers
NDT Non-Destructive Testing
NFPA National Fire Protection Association
PSI Pounds per Square Inch
PT Penetrant Testing
P/V Pressure/Vacuum
RP Recommended Practice
PST Product Saver Tank
RT Radiography Testing
TML Thickness Measurement Location
TRV Thermal Relief Valve
UFC Unified Facilities Criteria
UFGS Unified Facilities Guide Specifications
UT Ultrasonic Testing
VT Visual Testing
GENERAL SUMMARY
Austin Brockenbrough & Associates, LLP (Brockenbrough) was retained by Omaha District USACE under Contract No. W9128F-12-D-0006 Delivery Order No. 0025 to perform API Standard 653 In-Service Inspections. As required by this task, Brockenbrough executed a tank inspection site visit to Stewart Air National Guard, located in Newburgh, New York. An API 653 In-Service (visual external) Inspection was conducted for Tank Facility No. 7401 (Tank 39-400/Tank 1) on April 20, 2017. This inspection was performed in accordance with API Standard 653, “Tank Inspection, Repair, Alteration, and Reconstruction,” and the referenced contract. This inspection included a visual examination of the tank exterior, checklist review of all tank components, foundation settlement survey and a roundness survey of the tank shell.
Tank Facility 7401 is a 63-foot diameter by 50-foot and 3-inches tall, single wall, vertical, field erected tank with a nominal storage capacity of 25,000 barrels of jet fuel (F-24). Since, the tank did not have a manufacturer’s data plate attached to the tank shell, the tank manufacturer is unknown. Based on POL design drawings received from the base, the tank appears to be constructed in 1986. Per the tank repair data plate, it is known that a new tank bottom and a 36-inch shell manway were installed in 2010. Secondary containment is provided by a concrete containment area with vertical concrete dike walls. The concrete containment area and dike walls are lined with exposed flexible membrane liner (FML). Also, the tank is equipped with a typical under tank impressed current cathodic protection system. Details of the tank construction and appurtenances are included in Section ‘B’.
There are no mandatory repairs noted that need immediate attention. Additional noted deficiencies are discussed in more detail in Section ‘C’, and should be addressed in a timely manner. Photographs of the tank are included in Appendix ‘C’.
A previous out-of-service inspection for this tank is unable for review. Based on the date of tank cleaning and major repairs/alterations, it can be assumed that an out-of-service inspection was performed in September 2010.
While the current version of UFC 3-460-03 requires the next out-of-service inspection occur after 10 years, an upcoming revision allows the frequency to be extended as determined by a certified API 653 tank inspector.
However, as a new bottom was installed in 2010, a ten-year interval for the next internal inspection is recommended to provide a baseline for the corrosion rate of the new tank bottom. This inspection should include an external and internal inspection and include an examination of the tank bottom by magnetic flux leakage (MFL or MFE) technology and an ultrasonic thickness inspection of the tank shell. The next API Standard 653 In-Service (visual external) Inspection should be performed by an API 653 Inspector five years after the next internal inspection, in April 2025. The next ultrasonic thickness inspection of the shell would be due by April 2022, but should be performed in conjunction with the Out-of-Service Inspection.
GENERAL TANK INFORMATION
ITEM DESCRIPTION
Owner New York Air National Guard
Location Stewart Air National Guard
Facility Number Facility 7401
Tank Number Tank 39-400 (Tank 1)
State / Country New York / U.S.A.
City Newburgh
Inspection Date April 20, 2017
Tank Manufacturer Unknown
Design Standard API Std 650 (Per tank repair data plate)
Date of Construction 1986 (Per POL design drawings)
Tank Contents Jet Fuel (F-24)
Tank Serial Number Unknown
Tank Diameter 63’-0” (Per previous tank inspection report)
Shell Height 50’-3” (Per previous tank inspection report)
Product Height 21’ – 4 1/2” (Tape Level Gauge reading at the time of inspection)
Tank Capacity 25,000 barrels (Nominal capacity)
Foundation Concrete Ringwall
Construction
Bottom Unknown
Shell (6) butt-welded shell courses
Floating Roof Aluminum Floating Pan
Fixed Roof Self-supported, lap-welded, cone-up
Material
Bottom Carbon Steel (assumed)
Shell Carbon steel
Floating Roof Aluminum
Fixed Roof Carbon steel
Cathodic Protection Impressed Current Cathodic Protection System
Interior Coating System Epoxy-Epoxy-Epoxy (assumed)
Exterior Coating System Epoxy-Epoxy-Polyurethane (assumed)
Level Gauging Varec Tape Level Gauge; Cameron Automatic Tank Gauge (ATG)
Overfill Protection High Level Control Valve; Independent High-high and High Level Alarms
Piping Receipt 8” Stainless Steel
Issue 12” Stainless Steel
Low Suction 2” Stainless Steel
AFFF 4” Carbon Steel
Water Draw-Off 1” Stainless Steel
Level Alarms Independent High-high, High, and Low Level Alarms
Type of Internal Floating Roof Aluminum Honeycomb Floating Pan
A. GENERAL PROJECT INFORMATION
1. API 653 Inspection
This project will perform API 653 Inspections of various tanks at facilities throughout the United States.
Additional consideration is given to federal, state, and local regulations as well as applicable military criteria and general industry standards.
For Facility 7401, an API Standard 653 In‐service (visual external) Inspection was performed. This inspection also included an ultrasonic inspection of the shell and roof plates, a foundation settlement survey, and a shell roundness assessment.
2. Site Information
On April 20, 2017 Brockenbrough performed an API 653 In‐Service (visual external) Inspection of Tank
Facility 7401 located at Stewart Air National Guard. Stewart Air National Guard is located in the Town of Newburgh, New York. Stewart Air National Guard Base is the home of the 105th Airlift Wing (105
AW), an Air Mobility Command (AMC)-gained unit of the New York Air National Guard and "host" wing for the installation.
3. Future Projects
There is a project in place to repair the deteriorated joints on the angle iron extensions on top of the dike walls as is questionable as to whether they would contain the fuel for the tanks in case of a tank failure. This project has been submitted under Work Order No. 201701041, dated 18 April 2017.
B. TANK INSPECTION COMMENTS
1. Tank Construction
Tank Facility 7401 is a nominal 25,000 barrel, 63-foot diameter by 50-foot and 3-inches tall, F-24, aboveground vertical storage tank. Per the POL design drawings, the tank appears to be constructed to
API 650 design standard in 1986.
2. Tank Foundation
The tank rests on an 18-inch high concrete ringwall foundation. The foundation was visually evaluated during the inspection for broken concrete, spalling, cracks, and vegetation against the bottom of the tank. The concrete ringwall was found to be in good condition with only a few minor hairline cracks.
The bottom-to-foundation seal appears to be in good condition. A shell settlement survey was performed during the inspection in accordance with Appendix B of API Standard 653 and was found to be acceptable. Settlement results are listed in Appendix A.
3. Tank Shell
The vertical and cylindrical shell consists of six butt‐welded courses. The exterior of the shell was visually inspected and evaluated for plumbness, roundness, peaking and banding. The coating was also evaluated for deterioration.
a. Shell Plumbness, Roundness, Peaking, and Banding
The exterior of the shell was visually inspected and evaluated for plumbness, roundness, peaking and banding.
1) API 650, section 7.5.2 allows a maximum out of plumb of the top of the shell relative to the tank bottom of 1/200 the height of the shell, a difference of 3 inches for this 50-foot and 3-inches tall tank. The maximum measured out-of-plumbness was 1-9/16 inches measured towards the center of the tank measured on the east. The out-of-plumbness of the shell is within the tolerance that is allowed by API 650.
2) The shape of the shell appears to exceed the allowable API Standard 650 tolerance of plus or minus 1-inch of shell radius, as measured using laser surveying methods. Based on the circumference of the shell measured near the bottom, the radius of the shell should be 31 feet and 6 inches. However, the measured radius of the shell varies at the bottom from 31 feet and
5-1/16 inches in the southeast to 31 feet and 6-1/4 inches in the west. Also, the measured radii of the shell, varies near the top from 31 feet and 4-3/16 inches in the northeast and to 15 feet and 6-13/16 inches in west. The top of the shell is only slightly out of tolerance for a new tank.
Since the shell did not appear to be significantly distorted and the out-of-roundness does not appear to be detrimental to the structural integrity of the tank, no action is required or recommended at this time.
3) Minor shell deformations were noted on the fifth shell course. While some minor peaking and banding of the butt-welded shell seams was observed, the shape of the shell plates appears to be within the limits allowed by API 650.
b. Shell Coatings
Minor coating failure and corrosion were observed on a few areas of the tank shell, anchor bolts and nuts, intermediate platform frame, etc. However, the exterior shell coating shows no signs of significant deterioration. As the tank is used to store oil and the interior is coated with epoxy, deterioration of the interior of the shell since the previous inspection was performed is extremely unlikely.
c. Shell Ultrasonic Thickness Measurements
The ultrasonic thickness measurements of the shell indicate the shell has more than 30 years of remaining life. API 653 recommends ultrasonic thickness measurements of the shell be taken at least every 15 years.
4. Tank Appurtenances
a. Tank Roof
The tank is constructed with a self-supported lap-welded fixed cone roof. Isolated areas of coating failure and corrosion were observed on the roof flanges and nozzles. However, the coating system on the tank roof appeared to be in overall good condition.
b. Venting
This tank features a 24-inch center vent and four roof-mounted hatches/circulation vents. These hatches/vents provide adequate venting capacity based on the size of the tank. This tank is also equipped with two overflow vents.
c. Gauging
The tank’s Cameron ATG is installed through an 8-inch nozzle mounted on the tank roof. The tank also has a Varec tape level gauge mounted on the side of the tank. This tank is also equipped with an 8-inch dedicated sample hatch/gauging well.
d. Level Alarms
The low and high level alarm chambers are mounted on the exterior of the tank shell. The tank is equipped with low, high, and high-high level alarms independent of the tank gauging system.
However, the low level alarm set point appears to be too low to prevent damage to the floating pan legs.
e. Stairs and Platforms
The tank’s steel roof is accessible by a circumferential stairway mounted on the shell of the tank.
The coating system on the circumferential stairway appeared to be good condition. The width and rise of the stairway steps appear to be in general compliance with OSHA criteria. The height of handrails appears to exceed the maximum limit set by OSHA. However, the difference is small and does not appear to be detrimental to normal base operations.
f. Grounding and Bonding
There are two grounding cables connected to ground lugs welded to the tank shell.
5. Tank Coating
The interior coating system of the tank is assumed to be epoxy-epoxy-epoxy. The external coating system appears to be a standard military coating system (epoxy-epoxy-polyurethane). Minor coating failure and corrosion were observed on few areas of the tank shell, anchor bolts and nuts, intermediate platform frame, handrails, roof nozzle and flanges, etc.
6. Tank Piping System
Fuel is received through 8‐inch stainless steel piping from an adjacent Truck Off-load Station and is issued through 12-inch stainless steel piping from the adjacent Pumphouse to the Truck Fillstands and
Hydrant System. Corrosion was observed on carbon steel pipe supports that are used for the tank issue and receipt piping.
7. Fire Protection System
There are several fire hydrants noted within 300 feet of this tank. There is also an Aqueous Film
Forming Foam (AFFF) system installed.
8. Secondary Containment
Secondary containment is provided by a concrete containment area with vertical concrete dike walls lined with flexible membrane liner. Also, there is a 3-inch by 3-inch angle iron extension installed on top of the dike walls along the perimeter of the containment area. The secondary containment was visually evaluated during the inspection. The containment is of sufficient size to contain a total tank loss plus one foot of freeboard.
C. FINDINGS AND RECOMMENDATIONS
Tank Facility 7401 was found to be in generally good condition. The tank is fully serviceable. However, several items were observed that are not in full compliance with federal, state, and local codes or military criteria.
1. MANDATORY REPAIRS per API 653, UFC 3-460-01, or AW 78-24-27 Standards
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. No mandatory repairs are required to be performed.
2. SIGNIFICANT FINDINGS per API 653, UFC 3-460-01, or AW 78-24-27 Standards
The following information identifies the significant findings found during the tank inspection.
a. Repair Hairline Cracks in Ringwall Foundation
OBSERVATION: Minor hairline cracking was present on a few areas within the concrete ringwall foundation.
CODE REFERENCE: UFC 3-460-03, Section 8-4.3.1 and 8-10.2.1 require all cracks to be cleaned and sealed with a fuel resistant sealant.
RECOMMENDATION: Clean and seal all the hairline cracks within the concrete ringwall foundation with a fuel resistant sealant.
b. Repair Coating System on Tank and Tank Appurtenances
OBSERVATION: Localized coating failure and minor surface corrosion were observed on a few areas of the tank shell, anchor bolts and nuts, handrails, intermediate platform frame, pipe supports, etc. Also, several areas of coating failure and corrosion were observed on the bottom platform frame and access stairway. Some areas of the roof nozzle flanges, nozzle piping, etc. were found to be corroding.
CODE REFERENCE: UFC 3-460-03, Section 8-3.10, requires the exterior of fuel storage tanks and appurtenances to be coated.
RECOMMENDATION: Remove corrosion from all the isolated areas of deterioration. Clean and prep all the areas that require coating repairs and apply a compatible coating system that meets military criteria.
c. Provide Manufacturer’s Nameplate
OBSERVATION: The tank does not have a manufacturer’s nameplate installed on the tank shell.
CODE REFERENCE: UFC 3-460-01 paragraph 8-3.15 requires nameplates for all aboveground storage tanks in accordance with API Standard 650 Section 10.1 Nameplates.
RECOMMENDATION: Provide a manufacturer’s nameplate per the latest edition of DOD Standard
Design AW 78-24-27.
d. Repair Low Level Alarm
OBSERVATION: The tank is not equipped with a low-low level alarm. Also, the low level set point appears to be too low to prevent damage to the floating pan legs.
CODE REFERENCE: UFC 3-460-01, Table 8-1, Item l requires independent high-high, high, low, and low-low level alarms.
RECOMMENDATION: Demolish the existing low level alarm chamber and piping. Provide a new low and low-low level alarm per the DoD Standard Design AW 78-24-27 suitable for existing floating pan configuration.
e. Replace the Roof Inspection Hatches/Circulation Vents
OBSERVATION: The roof inspection hatches/circulation vent openings have been welded shut and therefore, cannot be opened for inspection and maintenance.
CODE REFERENCE: UFC 3-460-01, Table 8-1 Item h and AW 78-24-27 require that the tank roof be provided with four roof inspection hatches/ circulation vents. API 653 External Inspection
Checklist Item C.1.5.7 requires inspection of these roof-mounted vents.
RECOMMENDATION: Demolish the existing roof inspection hatches/circulation vents and replace them in accordance with DoD Standard Design AW 78-24-27.
f. Replace Coating System on AFFF Piping and Equipment
OBSERVATION: The coating system on the AFFF piping and equipment has failed.
CODE REFERENCE: UFC 3-460-01 paragraph 8-3.10 requires the exterior of fuel storage tanks and appurtenances to be coated.
RECOMMENDATION: Replace the entire coating system on the AFFF piping and equipment.
g. Repair Joints on the Angle Iron Extensions
OBSERVATION: Many of the joints on the angle iron extensions on top of the dike walls are deteriorated and would not contain the fuel for the tank in case of a spill.
CODE REFERENCE: N/A
RECOMMENDATION: There is a project in place at the base to perform this repair. However, if the work does not get completed, repair all the joints and joint seals on the angle iron extensions on top of dike walls.
3. REPAIRS to Fully Comply with API 653, UFC 3-460-01, or AW 78-24-27 Standards
These items represent repairs and/or upgrades that could be performed to bring the tank into full compliance with current standards, but that do not represent potential risks to system operators, equipment integrity, or the adjacent environment. Our recommendations to perform or not to perform these repairs and/or upgrades take into consideration the cost of the repair, the operational benefit of the repairs, the age of the tank/system, operator safety, environmental risks, and equipment integrity.
a. Upgrade Thermal Relief System
OBSERVATION: The existing thermal relief valve piping on the tank receipt and issue piping have some threaded piping, include sight flow indicators, and do not have testing tees. Some of the thermal relief valves are installed in horizontal position, which is generally not recommended by the valve manufacturer. Also, the thermal relief discharge piping is connected directly to the tank shell instead of the tank nozzle.
CODE REFERENCE: AW 78-24-27 requires the thermal relief piping to be equipped with isolation valves and testing tees. UFC 3-460-01, Section 9-3.5.1 does not allow sight flow indicators in thermal relief piping. UFC 3-460-01, Section 9-8 requires welded or flanged connections for joining steel pipes.
RECOMMENDATION: Replace all threaded piping and fittings in the thermal relief system with welded connections. Provide testing tees and remove sight flow indicators associated with the thermal relief system. Remove all the thermal relief valves installed in horizontal position and reinstall them per manufacturer’s recommendations. Reroute the thermal relief piping to be discharged to the tank nozzle.
b. Upgrade Water Draw-off Piping
OBSERVATION: The water draw-off piping consists of 1-inch pipe with a ball valve at the tank skin.
Also, the piping in the water draw-off system, including the tank nozzle, consists of threaded valves and fittings.
CODE REFERENCE: UFC 3-460-01, Section 9-8 requires welded or flanged connections for joining steel pipes. UFC 3-460-01, Table 8-1 z, requires water draw-off piping to include a 2-inch double block and bleed valve as the tank skin valve.
RECOMMENDATION: Since there is a FY18 MILCON project in place to relocate the facility, along with the storage tanks, we do not recommend any modifications at this time. However, if this project does not move forward, when the tank is taken out-of-service for other major repairs/upgrades, upgrade the water draw-off piping to 2-inch and provide a 2-inch double block and bleed valve at the skin of the tank. Also, replace all threaded fittings and connections with welded or flanged connections.
c. Provide Scaffold Supports
OBSERVATION: There are no scaffold cable supports present on the tank roof.
CODE REFERENCE: UFC 3-460-01, Table 8-1, Item ff requires two scaffold cable supports on the fixed roof in accordance with API 650.
RECOMMENDATION: Provide two scaffold cable supports in accordance with API 650.
d. Provide DBB for Low Suction
OBSERVATION: The tank skin valve for low suction piping is a ball valve.
CODE REFERENCE: UFC 3-460-01 requires all tank skin valves to be double block and bleed type valves.
RECOMMENDATION: Replace the ball valve in low suction piping with a double block and bleed valve at the tank shell.
4. RECOMMENDED REPAIRS as Part of Regular Maintenance
Recommended 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. No recommended repairs are required to be performed at this time.
APPENDIX A: ENGINEERING CALCULATIONS AND DRAWINGS
SHELL ROUNDNESS SURVEY & SETTLEMENT
The shape of the shell appears to exceed the allowable API Standard 650 tolerance of plus or minus 1-inch of shell radius, as measured using laser surveying methods. Based on the circumference of the shell measured near the bottom, the radius of the shell should be 31 feet and 6 inches. However, the measured radius of the shell varies at the bottom from 31 feet and 5-1/16 inches in the southeast to 31 feet and 6-1/4 inches in the west. Also, the measured radii of the shell, varies near the top from 31 feet and 4-3/16 inches in the northeast and to 15 feet and
6-13/16 inches in west. The top of the shell is only slightly out of tolerance for a new tank. Since the shell did not appear to be significantly distorted and the out-of-roundness does not appear to be detrimental to the structural integrity of the tank, no action is required or recommended at this time.
Austin Brockenbrough & Associates, L.L.P. 16-090.02
Location: Tank Facility 7401 Stewart Air National Guard Date: 6/7/17
Subject: Shell Radius Survey
Measured Circumference at Bottom = 197.92
Calculated Diameter = 63.00
Calculated Radius = 31.50
South 31.51 0.01 0.16 48.1 S+N 0.32
31.56 0.06 0.68 45.1 0.92
31.56 0.06 0.70 42.1 0.90
31.57 0.07 0.78 39.1 0.41
31.56 0.06 0.70 36.1 0.11
31.55 0.05 0.58 33.1 1.43
31.56 0.06 0.73 30.1 0.36
31.57 0.07 0.80 27.1 0.04
31.58 0.08 0.98 24.1 0.56
31.55 0.05 0.56 21.1 0.49
31.52 0.02 0.18 18.1 0.18
31.47 -0.03 -0.37 15.1 0.12
31.47 -0.03 -0.38 12.1 0.16
31.46 -0.04 -0.43 9.1 0.32
31.48 -0.02 -0.19 6.1 0.22
31.53 0.03 0.37 3.1 0.44
31.51 0.01 0.08 0.1 0.38
107.96
Southeast 31.44 -0.06 -0.74 48.3 SE+NW 1.79
31.46 -0.04 -0.46 45.2 1.46
31.46 -0.04 -0.49 42.2 1.85
31.45 -0.05 -0.58 39.2 2.11
31.41 -0.09 -1.06 36.3 1.57
31.38 -0.12 -1.49 33.3 1.17
31.40 -0.10 -1.16 30.3 0.39
31.40 -0.10 -1.23 27.3 0.27
31.47 -0.03 -0.32 24.2 0.87
31.50 0.00 -0.04 21.2 0.99
31.52 0.02 0.29 18.2 1.18
31.54 0.04 0.50 15.2 1.63
31.54 0.04 0.44 12.2 1.12
31.52 0.02 0.24 9.2 0.39
31.51 0.01 0.16 6.2 0.14
31.51 0.01 0.11 3.2 0.17
31.42 -0.08 -1.00 0.2 1.00
Weld Elevation 108.04
Diameter Deviation
(in)
Weld Elevation
Distance from
Centerline
Height
Above
Chime
Deviation
Radial
Deviation
(in)
East 31.34 -0.16 -1.92 48.3 E+W 1.14
31.38 -0.12 -1.44 45.3 0.16
31.36 -0.14 -1.69 42.3 0.48
31.34 -0.16 -1.91 39.3 0.58
31.35 -0.15 -1.85 36.3 0.06
31.35 -0.15 -1.75 33.3 0.16
31.38 -0.12 -1.48 30.3 0.18
31.40 -0.10 -1.21 27.3 0.19
31.41 -0.09 -1.07 24.2 0.16
31.44 -0.06 -0.77 21.2 0.14
31.46 -0.04 -0.47 18.2 0.30
31.49 -0.01 -0.08 15.2 0.40
31.48 -0.02 -0.30 12.2 0.29
31.44 -0.06 -0.67 9.2 0.00
31.46 -0.04 -0.54 6.2 0.02
31.49 -0.01 -0.16 3.2 0.52
31.47 -0.03 -0.35 0.2 0.08
Weld Elevation 108.03
Northeast 31.35 -0.15 -1.86 48.4 NE+SW 1.27
31.41 -0.09 -1.03 45.3 0.05
31.40 -0.10 -1.16 42.3 0.26
31.41 -0.09 -1.07 39.3 0.02
31.41 -0.09 -1.03 36.3 0.35
31.38 -0.12 -1.44 33.3 0.10
31.39 -0.11 -1.28 30.3 0.42
31.42 -0.08 -0.95 27.3 0.58
31.43 -0.07 -0.85 24.2 0.23
31.45 -0.05 -0.63 21.2 0.33
31.44 -0.06 -0.78 18.2 0.02
31.42 -0.08 -0.97 15.2 0.20
31.46 -0.04 -0.46 12.2 0.54
31.50 0.00 -0.05 9.2 1.10
31.52 0.02 0.23 6.2 0.93
31.51 0.01 0.15 3.2 0.40
31.45 -0.05 -0.63 0.2 1.18
Weld Elevation 107.98
North 31.46 -0.04 -0.48 48.3
31.52 0.02 0.24 45.2
31.52 0.02 0.20 42.2
31.47 -0.03 -0.37 39.2
31.43 -0.07 -0.80 36.3
31.33 -0.17 -2.00 33.3
31.41 -0.09 -1.09 30.3
31.44 -0.06 -0.77 27.2
31.47 -0.03 -0.42 24.2
31.49 -0.01 -0.07 21.2
31.50 0.00 0.00 18.2
31.52 0.02 0.25 15.2
31.55 0.05 0.54 12.2
31.56 0.06 0.76 9.2
31.53 0.03 0.41 6.2
31.51 0.01 0.07 3.2
31.46 -0.04 -0.47 0.2
Weld Elevation 107.95
Northwest 31.41 -0.09 -1.05 48.3
31.42 -0.08 -1.01 45.3
31.39 -0.11 -1.36 42.3
31.37 -0.13 -1.53 39.3
31.46 -0.04 -0.51 36.3
31.53 0.03 0.32 33.2
31.56 0.06 0.77 30.2
31.58 0.08 0.96 27.2
31.60 0.10 1.19 24.2
31.59 0.09 1.03 21.2
31.57 0.07 0.89 18.2
31.59 0.09 1.13 15.2
31.56 0.06 0.69 12.2
31.51 0.01 0.15 9.2
31.50 0.00 -0.01 6.2
31.50 0.00 0.05 3.2
Weld Elevation 107.95
West 31.57 0.07 0.78 48.2
31.61 0.11 1.28 45.2
31.60 0.10 1.21 42.2
31.61 0.11 1.33 39.2
31.65 0.15 1.79 36.2
31.66 0.16 1.91 33.2
31.64 0.14 1.66 30.2
31.62 0.12 1.40 27.2
31.58 0.08 0.91 24.2
31.58 0.08 0.91 21.2
31.56 0.06 0.77 18.2
31.54 0.04 0.48 15.2
31.55 0.05 0.59 12.2
31.56 0.06 0.67 9.2
31.55 0.05 0.56 6.2
31.56 0.06 0.67 3.2
31.52 0.02 0.26 0.2
Weld Elevation 107.93
Southwest 31.55 0.05 0.59 48.1
31.58 0.08 0.99 45.1
31.58 0.08 0.90 42.1
31.59 0.09 1.05 39.1
31.62 0.12 1.39 36.1
31.63 0.13 1.54 33.1
31.64 0.14 1.70 30.1
31.63 0.13 1.53 27.1
31.59 0.09 1.08 24.1
31.58 0.08 0.96 21.1
31.56 0.06 0.76 18.1
31.56 0.06 0.77 15.1
31.58 0.08 1.00 12.1
31.60 0.10 1.15 9.1
31.56 0.06 0.70 6.2
31.52 0.02 0.26 3.2
31.45 -0.05 -0.56 0.2
Weld Elevation 107.93
SHELL SETTLEMENT SURVEY
Austin Brockenbrough & Associates, L.L.P.
Job No. 16-090.02 Location: Stewart ANG
Date: 06/08/2017 Subject: Tank Fac 7401 Shell Settlement Evaluation By: Bryan Strayer
API 653 Appendix B Optimum cosine curve, B 2.2.4.e)
Z = a + b x cos(theta + c)
Diameter (D) = 63 (ft)
Number of equally spaced data points (ft)= 8 L = Arc length between measurement points (ft) = 24.74 Tank Height (H) = 50.25 (ft)
Survey Height of
Position Weld * Z U S 0 7 107.93 0.00 -0.01 -0.01 0.00 1 8 107.93 0.00 0.01 0.01 0.01 2 1 107.96 0.03 0.04 0.01 0.03 3 2 108.04 0.11 0.08 -0.03 -0.04 4 3 108.03 0.10 0.09 -0.01 -0.01 5 4 107.98 0.05 0.08 0.03 0.02 6 5 107.95 0.02 0.04 0.02 0.02 7 6 107.95 0.02 0.01 -0.01 -0.02 8 7 107.93 0.00 -0.01 -0.01 0.00
Maximum out-of-plane deflection = 0.04
* = measured elevation
*HI (Height of Instrument) Z = calculated rigid body tilt (in)
U = out-of-plane settlement = S = out-of-plane deflection = z-y
Y = yield strength of shell material (PSI) = 30,000 E = Youngs modulus of elasticity (lbf/in2) = 29000000.00 S allowable (in) (API 653 B.3.2.1) = (L^2*Y*11)/(2EH)*12 = 0.83 in
R^2 =(Syy - SSE)/Syy = 0.80 not >=0.9 therefore cosine curve is invalid.
Evaluation by the Arc Length Method described in API 653 B.2.2.5.1 is required.
Austin Brockenbrough & Associates, L.L.P.
Job No. 16-090.02 Location: Stewart ANG
Date: 06/08/2017 Subject: Tank Fac 7401 Shell Settlement Evaluation By: Bryan Strayer
API 653 B.2.2.5.1 Evaluation by Settlement Arc Length Method
Per B.3.2.2, K = 10.5
Settlement arc length (ft), Sarc
Out of plate settlement at Point i (Si)
Allowable settlement at point i (Smax) = MIN[K*Sarc*(D/H)*(Y/E), 4]
Point Sarc (ft) Si (in) Smax
0 99.0 0.043 1.35 Si < Smax → OK
6 99.0 0.023 1.35 Si < Smax → OK
Evaluation of the settlement by the arc length method indicates the settlement is within acceptable limits.
-0.05
0.00
0.05
0.10
0.15
0 2 4 6 8 10
Measured Elevation (in)
Si6 Si0
SHELL THICKNESS CALCULATIONS
It is noted that because of the way technology has evolved, and as the exact location of the measurements vary, the measured minimum thickness of some of the shell plate may be less than, or even greater than, the previous measured thickness. There are a few locations on the tank roof and tank shell where we were unable to take accurate UT measurements. Additionally, in some cases the measured thickness is greater than the nominal thickness due to steel plate tolerances, which allow plus or minus 30 thousandths of an inch. However, this may not indicate a corrosion rate, unless there is significant coating failure and corrosion, which is unlikely with oil storage. Thinning of coated steel is due to abrasive blasting and not deterioration. Therefore, since the interior and exterior of the shell are coated and the current measurements indicate the same nominal thickness as the previous measurements with no significant deviation, the current corrosion rate is zero. Also, since the remaining thickness is greater than the required thickness, the expected service life is greater than 30 years. Therefore, per
API 653 the next ultrasonic thickness inspection of the shell should be performed in 15 years.
Job No.: 16-090.02
Job Title: Stewart ANG
Subject: Tank Facility 7401 Shell Thickness Evaluation
By: Bryan Strayer Date:
API 653
SHELL CALCULATIONS
Diameter 63 feet
Shell Height 50.25 feet
Freeboard 0 feet
Design Fill Height 50.25 feet
Specific Gravity 1.00 API 650
0.84 API 653
Joint Efficiency 0.85 API 650 Appendix A 7th Edition Assumed
Material unknown
Yield Strength 30,000 psi (assumed)
Tensile Strength 55,000 psi (assumed)
Original Design Corrosion Allowance
0.000 in (0 mm)
Required thickness:
Lower Upper
Two
Courses Courses
23600 26000
Height Product Required Thickness
Course (feet) Depth 1/4" min
6 10.00 8.25
5 8.00 16.25
4 8.00 24.25
3 8.00 32.25
2 8.00 40.25
1 10.00 50.25 min 2017 Corrosion Estimated UTM current net 1986 Rate Service Life Inspection
Course UTM thickness thickness * in/yr yrs. Interval
6 0.256 0.256 0.257 0.00002 >30 15
5 0.253 0.253 0.258 0.00015 >30 15
4 0.311 0.311 0.316 0.00015 >30 15
3 0.312 0.312 0.326 0.00046 >30 15
2 0.446 0.446 0.448 0.00005 >30 15
1 0.496 0.496 0.509 0.00041 >30 15
* The original thicknesses are assumed based on required design thicknessess, overtolerance, and the range of the UTMs.
0.131
0.199
0.1000.123
0.188
0.338
0.269
SE
2.6(H-1)D 2.6HDG
0.422
0.336
4/20/2017
Visual
Inspection
Interval
SE
2.6(H-1)DG
0.145
0.399
API-650 API-653
0.253 0.268 0.195
SE
20000 22500
Original
Design
0.059 0.062 0.100
Allowable Stress (psi)
Original
Hydro
0.318
SHELL/ROOF ULTRASONIC THICKNESS MEASUREMENTS
Brockenbrough personnel recorded the ultrasonic thickness measurements, shown on the following page, on 20
April 2017. There are a few locations on the tank roof and tank shell where we were unable to take accurate UT measurements. Refer to the tank drawings by others, which are included for reference in the pages that follow, for location of the shell plate measurements and layout of the tank. The values are in thousandths of an inch.
Job No.: 16-090.02
Job Title: Stewart ANG
Subject: Tank Facility 7401 Shell Thickness Evaluation
By: Bryan Strayer Date:
SHELL UTM DATA (0.001 inches)
DFT = 0.000 inches
Course 6 256 257 257 at Stairs
Course 5 257 263 253 at Stairs
Course 4 316 320 311 at Stairs
Course 3 352 315 312 at Stairs
Course 2 446 448 449 at Stairs
UTM's include 0 inch DFT coating.
1 4 7
2 5 8
3 6 9
Typical Shell Plate UTMs.
Course 1 1 2 3 4 5 6 7 8 9
1-1 497 507 498 511 519 512 513 517 515
1-2 503 500 511 514 506 521 513
1-3 498 508 498 499
1-4 535 526 514 507 510 519
1-5 511 505 508 504 500 508 503
1-6 504 508 507 496 498 511 511 506
* Unable to take UT measurements at certain places on the tank shell
Roof 188 186 198 194 188 192 193 190 195
UTs 194 196 197 189 189 190 192 189 199
4/20/2017
TANK DRAWINGS
The following tank drawings are taken from a previous API 653 Out-of-Service Inspection Report prepared by.
This data is included as a reference and should be used for informational purposes only.
OSHA ACCESS STRUCTURE REPORT
OSHA Stairway Data
Handrail Actual
(in)
OSHA Rq’d min (in) max (in)
Handrail Height 44 44 30 34 Step Width 30 30 22 NA Step Rise 9 9 NA NA
Bottom Step Rise 9 9 8 8
APPENDIX B: API 653 CHECKLISTS FOR TANK INSPECTIONS
UL SWRI
API Other
Protected
63'-0" diameter by 50'-3" tall
Type: Type:
Size: Date Installed:
SS End Conn: Size: 8" Material: SS End Conn: Size: 12"
Issue To:
Release Prevention Barrier
Overfill Protection / Level Alarms:
Independent High-high, High, Low Level Alarm & ATG Alarms High Level Control Valve (HLCV)
Receipt Piping Configuration Issue Piping Configuration
Tank Piping
Secondary Containment
September 2010 (assumed)
Tank Specifications
Previous Tank Inspection Date:
Continuous Release Detection Monitoring
Type:
Date Installed:
Current Product: N/A
Inspection Date:
Design Std
Tank Inspector Name:
Inspector Certification Number:
Overfill Protection:
NA
NA
NA
Useable Capacity:
Tank Construction and Configuration
Insulated
Coated
Plastic / Fiberglass
Other:
Jet Fuel (F-24)
25,000 BBL
Unknown
Butt Welded
70720
Horizontal Single Wall
Butt Welded
Pumphouse to Truck Fillstand/Hydrant System
Unknown
API 653 EXTERNAL INSPECTION CHECKLIST
Stewart ANG, NYProject Site:Project Name:
Project Location:
Brockenbrough Job No.:
SPCC Mandated AST Inspections - Group 3
Various Locations
General Inspection Information
16-090.02
Submitted to:
Contract No.:
USACE - Omaha
W9128F-12-D-0006
Tank Facility No.:
Local Tank ID No.:
April 20, 2017
Facility 7401
Tank Manufacturer:
Tank Construction Date:
Tank 39-400 (Tank 1) Bryan Strayer
Vertical
Rectangular
Double Wall
Fire Resistant
Closed Top Dike
Change of Service:
Last Repair:
Tank Coatings:
Exterior Coating:
Epoxy/Epoxy/Polyurethane
Epoxy (assumed)
Interior Coating:
Double Bottom
Unknown
Concrete Dike
180'-0" X 180'-0" X 6'-0"
Level Alarms:
Material:
Tank Outside Dimensions:
Nominal Capacity:
Secondary Containment, Overfill, and CRDM
Open Type Dike
September 2010
Receipt From: Truck Off-Load
API 653 EXTERNAL INSPECTION CHECKLIST
Stewart ANG, NYProject Site:Project Name: SPCC Mandated AST Inspections - Group 3
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A c)
TASK
Check for:
Tank Settlement
C.1.1.1 Concrete Ring
C.1.1.4 Rock
Review cathodic protection potential readings
Check for:
e)
Measure foundation levelness and bottom elevations (See Annex B) See survey data.
STATUS COMMENTS
Settlement around perimeter of tank
Check for:
d) a) b)
C.1.1.6 Housekeeping
Build-up of trash, vegetation, and other inflammables
Leaching of oil which has left rock filler exposed indicating hydrocarbon leakage
Tank settlement into asphalt base
Site drainage away from the tank, associated piping, and manifolds
Cavities under foundation; vegetation against bottom of tank
Broken concrete, spalling, and cracks, especially under backup bars used in welding butt-welded annular rings under the shell
Indications of bottom leakage at drain openings in ring, back of water-draw basins, and top surface of ring
ITEM
C.1.1 Foundation a) b)
Run-off rainwater from shell draining away from the tank
Check for:
b)
Settlements into the base
C.1.1.5 Site Drainage
Proper operation of dike drains
Check for:
Presence of crushed rock under the steel bottom which usually results in severe underside corrosion.
Check for :C.1.1.3 Oiled Dirt or Sand
C.1.1.7 Cathodic Protection a)
C.1.1.2 Asphalt
There are minor hairline cracks in some areas of the ringwall.
C.1.2.1 External Visual Inspection
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
C.1.2.3 Riveted Shell Inspection
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
C.1.2.4 Wind Girder (Floating Roof
Tanks) a)
Rivet and seam leaks on external surface
Check for:
Corrosion and thinning on plate and weld after cleaning the bottom angle area
Paint failures, pitting, and corrosion
Full fillet lap-welded vertical seams to increase joint efficiency b) c) c) b)
Reinforcing pads welded to shell at supports
Leaks and identify the location by sketch or photo
Check for:
Check for:
Broken welds and corrosion damage
(paint failure, pitting, corrosion, product build-up), especially where it occurs at tack-welded junction d)
Corrosion loss and wear on the rivets a) b)
c) Bottom-to-Foundation Seal
e) Drawings of riveted seams if available. Otherwise, dimension and sketch (or photograph) the rivet pattern: no. of rows, rivet size, pitch length, butt-riveted or lap-riveted joints a)
Grooving, corrosion, pitting, and coating failures
C.1.2.2 Internal (Floating Roof
Tank)
Some minor areas of coating failure and surface corrosion.
The seal was difficult to inspect due to the coating but appeared to be in good condition.
C.1.2. Shells
Check for:
Pitting on support welds to shell, especially on shell plates
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
ITEM TASK
a) Leaks at piping manifolds, flanges, and valves
Flange leaks and leaks around bolting
Shell plate dimpling around nozzles, caused by excessive pipe deflection c)
Check for:
C.1.3.3 Autogauge System Check for:
b)
COMMENTS
Cracks or signs of leakage on weld joint at nozzles, manholes, and reinforcing plates
Fire fighting system componentsb) c) d) e) f) g)
Anchored piping which would be hazardous to the tank shell or bottom connections during earth movement
Adequate thermal pressure relief of piping to the tank
Proper operation of regulators for tanks with purge gas systems
Leaks at sample connections and proper valve operation
Damage and test the accuracy of temperature indicators h)
C.1.3.1 Manholes and Nozzles
C.1.3.2 Tank Piping Manifolds
C.1.3 Shell Appurtenances
Damage on welds on shell-mounted davit clips above valves 6 inches and larger
Sealing of insulation around manholes and nozzles
e) Adequate manholes flange and cover thickness on mixer manholes
AFFF piping showed signs of coating failure.
d)
a) (2) Ground Level - 36-inch round manholes with davit arm.
(1) Pan Access - 36-inch round manhole with davit arm.
STATUS
a) Leaks on autogauge tape guide and lower sheave housing (floating swings)
b) Damage on autogauge head
Thermal relief piping is threaded in a few places, contains sight flow indicators, and does not have tetsing tees. Some valves are installed in horizontal position.
Check for:
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
c) Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
1 1/2"ø coated carbon steel.
h) Condition of board and legibility of board-type autogauges
Freedom of movement of marker and float i)
C.1.3.3 Autogauge System c) d)
C.1.3.4 Shell-mounted Sample
Station a) b)
Check for:
Function of valves and plugging in sample lines, including drain or return-to-tank line
Leaks in circulation pump and operating problems
Inspect condensate drain for presence of oil indicating leakage
C.1.3.5 Heater (Shell Manhole
Mounted)
C.1.3.6 Mixer Check for:
c) Condition of power lines and connections to mixer
Bracing and supports for sample lines and equipment b)
Proper mounting flange and support
Leakage e) f) g)
Proper movement of tape by bumping the checker on autogauge head
Size and construction material of the autogauge tape guide and make note
(floating roof tanks)
Proper movement of tape. Ask the operator if the tape tends to hang up during tank roof movement (floating roof tanks).
Actual product level compared to the reading on the autogauge. Make note. (max. variation is 2 in.)
No more than 2 feet of tape are exposed at the end of the tape guide when the roof is in lowest position
(floating roof tanks) a)
ITEM TASK STATUS COMMENTS
Varec = 21'-4 1/2"
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
b) Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Target should indicate direction of swing opening (up or down) and height above bottom where suction will be lost with swing on bottom support
Floating: With tank half full or more, lower the swing line, then let out the cable and check if the swing has pulled cable tight, indicating that the winch is operating properly
ITEM TASK
Non-floating: Raise, then lower the swing line with the winch and check for cable lightness to confirm the swing line lowered properly
COMMENTS
C.1.3.7 Swing Lines: Winch a)
Operation
Indicator: Check that the indicator moves in the proper direction.
Floating swing line indicators show a lower level as cable is wound up on the winch. Non-floating swing line indicators show the opposite b) c)
C.1.3.8 Swing Lines: External
Guide System
Check for leaks at threaded and flanged joints
C.1.3.9 Swing Lines: Identify
Ballast Varying Need
Check for significant difference in stock specific gravity
Check for:C.1.3.10 Swing Lines: Cable
Material and Condition a) Corrosion over entire length, for non-stainless steel cable
Wear or fraying on all types of cable
C.1.3.11 Swing Lines: Product
Sample Comparison
Check for water or gravity differences that would indicate a leaking swing joint
C.1.3.12 Swing Lines: Target
STATUS
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
C.1.4 Roofs
C.1.4.1 Deck Plate Internal
Corrosion
For safety, before accessing the roof, check with ultrasonic instrument or lightly use a ball peen hammer to test the deck plate near the edge of the roof for thinning. (Corrosion normally attacks the deck plate at the edge of a fixed roof and at the rafters in the center of the roof first.)
C.1.4.2 Deck Plate External
Corrosion
ITEM TASK
C.1.4.4 Level of Floating Roof At several locations, measure distance from roof rim to a horizontal weld seam above the roof. A variance in the readings indicates a nonlevel roof with possible shell out-of-round, out-of-plumb, leaking pontoons, or hang-up. On small diameter tanks, an unlevel condition can indicate unequal loading at that level.
C.1.4.5 Gas Test Internal Floating
Roof
Test for explosive gas on top of the internal floating roof, Readings could indicate a leaking roof, leaking seal system, or inadequate ventilation of the area above the internal floating roof.
Visually inspect for paint failure, holes, pitting, and corrosion product on the roof deck.
C.1.4.3 Roof Deck Drainage Look for indication of standing water.
(Significant sagging of fixed roof deck indicates potential rafter failure.
Large standing water areas on a floating roof indicate inadequate drainage design or, if to one side, a nonlevel roof with possible leaking pontoons.)
STATUS
No access.
COMMENTS
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
STATUS COMMENTS
C.1.4.6 Roof Insulation Check for:
a) b) c)
Crack and leaks in the insulation weather coat where runoff rain water could penetrate the insulation
C.1.4.7 Floating Roof Seal a)
Systems
Inspect the condition of the seal, measure and record maximum rim spaces and seal-to-shell gaps around the full roof circumference at the level of inspection. NOTE: Inspection of the seal and measurement of the rim spaces and seal-to-shell gaps at more than one level may be necessary to more fully determine if any problems exist at other levels of tank operation).
Wet insulation under the weather coat
Corrosion on the roof plate and holes near the edge of the insulated area by removing small test sections of insulation
ITEM TASK
b) c) d) e) f) g)
Check if seal fabric on primary shoe seals is pulling shoes away from shell (fabric not wide enough).
Inspect fabric for deterioration, holes, tears, and cracks.
Inspect visible metallic parts for corrosion and wear.
Inspect for openings in seals that would permit vapor emissions.
Inspect for protruding bolt or rivet heads against the shell.
1) ____________Opposite Pair 1; 2) ____________Opposite Pair 2Measure and record annular space at
30-ft spacing (minimum of four quadrants) around roof and record.
Measurements should be taken in directly opposite pairs.
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Check for:
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A 52' - 10 5/8"
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
ITEM TASK STATUS COMMENTS
C.1.4.7 Floating Roof Seal h)
Systems i) j)
Pull both primary and secondary seal systems back all around the shell to check their operation.
Inspect secondary seals for signs of buckling or indications that their angle with the shell is too shallow.
Inspect wedge-type wiper seals for flexibility, resilience, cracks, and tears.
C.1.5 Roof Appurtenances
C.1.5.1 Sample Hatch g) h)
Operation of system
Presence and condition of protective coating or liner inside sample hatch
(preventing rust from pipe getting into sample) on ultra clean stocks such as JP4 a) b) c) d) e) f)
Condition and functioning of sample hatch cover.
Condition of seal inside hatch cover on tanks governed by Air Quality
Monitoring District rules
Corrosion and plugging on thief and gauge hatch cover.
Marker and tab stating hold-off distance, where the sample hatch is used to reel gauge stock level
Reinforcing pad where sample hatch pipe penetrates the roof deck.
Operation of recoil reel and condition of rope on floating roof sample hatch and recoil systems
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
No scaffold supports.
ITEM TASK STATUS COMMENTS
No access.
b) Corrosion on the tape guide's and float guide's wire anchors
Corrosion and missing bolts on the hatch
Check for:
Check for:C.1.5.4 Autogauge: Inspection
Hatch & Guides (Fixed Roof) a)
C.1.5.2 Gauge Well Check for:
Valve leakage and for presence of a bull plug or blind flange, if the tank has a gauge well washer a) b) c) d) e)
Thinning, size of slots, and cover condition of the visible portion of the gauge well
A hold-off distance marker and tab with hold-off distance (legible)
Condition of roof guide for gauge well, particularly the condition of the rollers for grooving on floating roofs
The distance from the gauge well pipe to the tank shell at different levels, if accessible
C.1.5.5 Autoguage: Float Well
Cover a) Corrosion
Wear or fraying caused by rubbing of the tape cable on the cover b)
Inspect scaffold support for corrosion, wear and structural soundness.
C.1.5.3 Fixed Roof Scaffold
Support
C.1.5.6 Sample Hatch (Internal
Floating Roof) a) Overall conditions
Automatic sealing after sampling, when equipped with a fabric seal
Proper operations when equipped with a recoil reel opening device b) c)
C.1.5.7 Roof-Mounted Vents
(Internal Floating Roof)
Check for:
C.1.5.8 Gauging Platform Drip
Ring
Check condition of screens, locking and pivot pins.
On fixed roof tanks with drip rings under the gauging platform or sampling area, inspect for plugged drain return to the tank.
The roof-mounted vents were welded shut and could not be opened.
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
No access but appeared to be in good condition.
1 1/2"ø handrail (carbon steel coated pipe).
Some minor spots of coating failure and light surface corrosion.
STATUS COMMENTS
c) If pontoon hatches are equipped with locked down coves, check for vent tubes. Check that vent tubes are not plugged up. Inspect lock-down devices for condition and operation.
ITEM TASK
b)
C.1.6 Access Ways - See Tank Out-of-Service Inspection Checklist Item C.2.12
C.2.12 Access Structures
C.2.12.1 Handrails a) b) c)
Check for:
a) Condition of the screen on the rim vent cover
b) Plating off or removal of rim vents where jurisdictional rules do not permit removal
C.1.5.13 Pontoon Inspection a)
Hatches
Open pontoon inspection hatch covers and visually check inside for pontoon leakage.
C.1.5.9 Emergency Roof Drains
C.1.5.10 Removable Roof Leg
Racks
C.1.5.11 Vacuum Breakers
C.1.5.12 Rim Vents
Inspect vapor plugs for emergency drain: that seal fabric discs are slightly smaller than the pipe ID and that fabric seal Is above the liquid level.
Check for leg racks on roof d)
Identify and report type (steel pipe, galvanized pipe, square tube, angle) and size of handrails.
Inspect for pitting and holes, paint failure.
Inspect attachment welds.
Identify cold joints and sharp edges.
Inspect the handrails and midrails.
Test for explosive gas (an indicator of vapor space leaks).
Report size, number, and type of vacuum breakers. Inspect vacuum breakers. If high legs are set, check for setting of mechanical breaker in high leg position.
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Pass Fail N/A
Some minor spots of coating failure and light surface corrosion.
Valve Access Platform: 15' X 5' ; Pan Access Platform: 8'-4" X 36" ; Roof
Access Platform: 36" X…
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