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INFORMATION CONTAINED HEREIN MAY BE SUBJECT TO EXPORT CONTROL LAWS. REFER TO INTERNATIONAL TRAFFIC IN ARMS REGULATION (ITAR)
OR THE EXPORT ADMINISTRATION REGULATION (EAR) OF 1979. IT IS THE RESPONSIBILITY OF THE RECIPIENT TO OBTAIN ANY REQUIRED LICENSES
TO EXPORT ANY CONTROLLED DATA.
10 November 2020
417541-99-02-L20-0775,
Revision A
Nill Building Solutions
67 Mariner Drive
Southampton, NY 11968
Attention: Mr. Christopher Gray
Subject: Proof and Ultimate Load Testing Performed on Nine Anchoring Brackets
References: (a) Purchase Order No. 053049
(b) Dayton T. Brown, Inc. Quote # 20-1496, dated 16 October 2020
(c) E-Mail Correspondence between D. Landwehrle of Dayton T. Brown, Inc.
and C. Gray of Nill Building Solutions, dated 30 October 2020
Enclosure: (1) Test Equipment List – 1 Page
(2) Photographs – 2 Pages
(3) Representative Proof Load Graphs – 3 Pages
Mr. Gray,
This test report details the events and calibrated test equipment used for the proof and ultimate load
testing of the two types of Anchoring Brackets in three configurations. The reason for this Revision
A is to describe how the Anchoring Brackets were supplied for testing and to in include
representative graphs as an enclosure. Three NB1C and three NB1S Anchoring Brackets were
supplied bolted to a section of 3/8-inch tube steel for testing. The NB1C steel configuration utilized
six 1.5-inch x ¼-20 bolts into tapped holes in the tube steel to secure the NB1C Anchoring Bracket.
No nuts were used on the back side of the tube steel. The NB1S steel configuration utilized a thru
hole at the center of the tube steel for a 7/8-9 bolt which was welded to the back side of the NB1S
Anchoring Bracket. A 7/8-9 nut was then used to secure the NB1S Anchoring Bracket from the back
side of the tube steel. Three NB1C were supplied affixed to two stacked pieces of wood using (6) 3-
inch x ¼-13 lag screws.
Testing was performed on 30 October 2020 under reference (a) to the requirements of references (b)
and (c). Proof load testing was performed by applying a 250-lbf lateral load, at a distance of 48
inches from the top surface of each Anchoring Bracket tested. The load was applied in 20%
increments up to at least 250 lbf as shown in graphs of Enclosure 3. Once the 250-lbf load was
reached, the load was then decreased in 20% increments. A visual inspection was performed after
each test which checked for any damage or deformation of the Anchoring Brackets. None of the
Anchoring Brackets showed evidence of damage, deformation, or failure of attachment after being
subjected to the proof load test, as summarized in the table below.
20-0775A Pg 2
Ultimate load testing was performed by applying the largest lateral load possible, at a distance of 48
inches from the top surface of each Anchoring Bracket. For both tests, the load was applied through
a 1/2-inch steel panel. The panel was secured to the Unit Under Test (UUT) utilizing a piece of steel
90° angle.
The Anchoring Brackets were originally delivered with “aluminum shoes” to secure the steel panel
to the UUT. During the first proof load test of Serial No. NB1C-S-1, it was found that the aluminum
shoe was failing prematurely at approximately 164.3 lbf due to the aluminum material deforming
around the bolt that secures the shoe to the Anchoring Bracket. As the aluminum shoe was not part
of the UUTs, the shoes were removed from each Anchoring Bracket and replaced with the steel 90°
angle. Serial No. NB1C-S-1 showed no evidence of damage or deformation and was subjected to a
second proof load test utilizing the steel 90° angle.
Proof Load Test Results
Part No. Serial No.
Max Load
Applied (lbf)
Visual Damage/
Deformation
NB1C NB1C-S-1 254.7 None
NB1C NB1C-S-2 256.0 None
NB1C NB1C-S-3 256.4 None
NB1S NB1S-S-1 258.1 None
NB1S NB1S-S-2 255.5 None
NB1S NB1S-S-3 252.2 None
NB1C NB1C-W-1 252.8 None
NB1C NB1C-W-2 254.3 None
NB1C NB1C-W-3 254.5 None
Ultimate Load Test Results
Part No. Serial No.
Max Load
Applied (lbf)
Visual Damage/
Deformation
NB1C NB1C-W-3 588.5 Yes, see Note 1
NB1C NB1C-S-3 561.9 Yes, see Note 1
NB1S NB1S-S-3 631.0 None
Note 1: For Serial Nos. NB1C-S-3 and NB1C-W-3, there was concave shape deformation at the
center of the Anchoring Bracket while the anchoring screws remained secured. It was also noted that
the stainless steel bolt that secured the steel 90° angle to the Anchoring Bracket was bent in the
applied load direction.
The test results recorded in this report apply only to the sample(s) as received and relate only to
those items tested.
20-0775A Pg 3
This report shall not be reproduced, except in full, without written approval from Dayton T. Brown,
Inc.
If you have any questions, please do not hesitate to contact the undersigned at (631) 589-6300 ext.
4571.
Very truly yours,
DAYTON T. BROWN, INC.
Don Landwehrle
Engineer
Warren Halbig
Department Manager
DL:rb
20-0775A
Enclosure 1
Test Equipment List
20-0775AEnc1Pg1
Test equipment utilized for the program reported herein was within its assigned interval of calibration.
Details are on file at Dayton T. Brown, Inc. and will be made available upon request.
417541-01Job Sub:
CAL DUE DATEACCURACYMODEL DTB NO.MANUFACTURERITEM
TEST: PROOF AND ULTIMATE LOAD
CONTROL SYSTEM, AERO ST 32
CH. CONTROL, 64 CH. DATA
MTS 10-228493.10/793.00 10/10/2021Mfr
TAPE MEASURE, 25' STANLEY 15-7833-725 05/23/2021± 1/16"
LOAD CELL, 2K LB 5/8 X 18
THREAD
INTERFACE 62-7691210-AF-2K-B 04/03/2022± 0.1% of F.S.
LEVEL, DIGITAL 10" MULTI-
FUNCTION WITH LASER TRAC
CRAFTSMAN 67-22320.48292 09/26/2021± 0.1°
20-0775A
Enclosure 2
Photographs
20-0775A Enc 2 Pg 1
Photo 1 – File No. PA300968
Test Setup with Aluminum Shoe
Photo 2 – File No. PA300986
Typical Test Setup with Steel 90° Angle
20-0775A Enc 2 Pg 2
Photo 3 – File No. PA300990
Serial No. NB1C-W-3 Ultimate Test Deformation
20-0775A
Enclosure 3
Representative Proof Load Graphs
20-0775A Enc 3 Pg 1
-50
0
50
100
150
200
250
300 11:48:44
11:48:50
11:48:56
11:49:02
11:49:08
11:49:14
11:49:20
11:49:26
11:49:32
11:49:38
11:49:44
11:49:49
11:49:55
11:50:01
11:50:07
11:50:13
11:50:19
11:50:25
11:50:31
11:50:37
11:50:43
11:50:49
11:50:55
11:51:01
11:51:07
11:51:13
11:51:19
11:51:25
11:51:31
11:51:37
11:51:43
11:51:49
11:51:55
11:52:00
Load(LBF)
Time Stamp
NB1C-S Sample Data
CONTROL
FEEDBACK
20-0775A Enc 3 Pg 2
-50
0
50
100
150
200
250
300 13:54:46
13:54:40
13:54:38
13:54:44
13:54:49
13:54:55
13:55:00
13:55:06
13:55:11
13:55:17
13:55:23
13:55:28
13:55:34
13:55:39
13:55:45
13:55:50
13:55:56
13:56:01
13:56:07
13:56:13
13:56:18
13:56:24
13:56:29
13:56:35
13:56:40
13:56:46
13:56:52
13:56:57
13:57:03
13:57:08
13:57:14
13:57:19
13:57:25
13:57:31
Load(LBF)
Time Stamp
NB1S-S Sample Data
CONTROL
FEEDBACK
20-0775A Enc 3 Pg 3
-50
0
50
100
150
200
250
300 14:32:53
14:32:47
14:32:41
14:32:35
14:32:29
14:32:23
14:32:17
14:32:11
14:32:05
14:31:59
14:31:53
14:31:47
14:31:41
14:31:35
14:31:29
14:31:23
14:31:17
14:31:11
14:31:04
14:30:58
14:30:52
14:30:46
14:30:40
14:30:34
14:30:28
14:30:22
14:30:16
14:30:10
14:30:04
14:29:58
14:29:52
14:29:46
14:29:40
14:29:34
Load(LBF)
Time Stamp
NB1C-W Sample Data
CONTROL
FEEDBACK

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Lateral load Engineering Report

  • 1. INFORMATION CONTAINED HEREIN MAY BE SUBJECT TO EXPORT CONTROL LAWS. REFER TO INTERNATIONAL TRAFFIC IN ARMS REGULATION (ITAR) OR THE EXPORT ADMINISTRATION REGULATION (EAR) OF 1979. IT IS THE RESPONSIBILITY OF THE RECIPIENT TO OBTAIN ANY REQUIRED LICENSES TO EXPORT ANY CONTROLLED DATA. 10 November 2020 417541-99-02-L20-0775, Revision A Nill Building Solutions 67 Mariner Drive Southampton, NY 11968 Attention: Mr. Christopher Gray Subject: Proof and Ultimate Load Testing Performed on Nine Anchoring Brackets References: (a) Purchase Order No. 053049 (b) Dayton T. Brown, Inc. Quote # 20-1496, dated 16 October 2020 (c) E-Mail Correspondence between D. Landwehrle of Dayton T. Brown, Inc. and C. Gray of Nill Building Solutions, dated 30 October 2020 Enclosure: (1) Test Equipment List – 1 Page (2) Photographs – 2 Pages (3) Representative Proof Load Graphs – 3 Pages Mr. Gray, This test report details the events and calibrated test equipment used for the proof and ultimate load testing of the two types of Anchoring Brackets in three configurations. The reason for this Revision A is to describe how the Anchoring Brackets were supplied for testing and to in include representative graphs as an enclosure. Three NB1C and three NB1S Anchoring Brackets were supplied bolted to a section of 3/8-inch tube steel for testing. The NB1C steel configuration utilized six 1.5-inch x ¼-20 bolts into tapped holes in the tube steel to secure the NB1C Anchoring Bracket. No nuts were used on the back side of the tube steel. The NB1S steel configuration utilized a thru hole at the center of the tube steel for a 7/8-9 bolt which was welded to the back side of the NB1S Anchoring Bracket. A 7/8-9 nut was then used to secure the NB1S Anchoring Bracket from the back side of the tube steel. Three NB1C were supplied affixed to two stacked pieces of wood using (6) 3- inch x ¼-13 lag screws. Testing was performed on 30 October 2020 under reference (a) to the requirements of references (b) and (c). Proof load testing was performed by applying a 250-lbf lateral load, at a distance of 48 inches from the top surface of each Anchoring Bracket tested. The load was applied in 20% increments up to at least 250 lbf as shown in graphs of Enclosure 3. Once the 250-lbf load was reached, the load was then decreased in 20% increments. A visual inspection was performed after each test which checked for any damage or deformation of the Anchoring Brackets. None of the Anchoring Brackets showed evidence of damage, deformation, or failure of attachment after being subjected to the proof load test, as summarized in the table below.
  • 2. 20-0775A Pg 2 Ultimate load testing was performed by applying the largest lateral load possible, at a distance of 48 inches from the top surface of each Anchoring Bracket. For both tests, the load was applied through a 1/2-inch steel panel. The panel was secured to the Unit Under Test (UUT) utilizing a piece of steel 90° angle. The Anchoring Brackets were originally delivered with “aluminum shoes” to secure the steel panel to the UUT. During the first proof load test of Serial No. NB1C-S-1, it was found that the aluminum shoe was failing prematurely at approximately 164.3 lbf due to the aluminum material deforming around the bolt that secures the shoe to the Anchoring Bracket. As the aluminum shoe was not part of the UUTs, the shoes were removed from each Anchoring Bracket and replaced with the steel 90° angle. Serial No. NB1C-S-1 showed no evidence of damage or deformation and was subjected to a second proof load test utilizing the steel 90° angle. Proof Load Test Results Part No. Serial No. Max Load Applied (lbf) Visual Damage/ Deformation NB1C NB1C-S-1 254.7 None NB1C NB1C-S-2 256.0 None NB1C NB1C-S-3 256.4 None NB1S NB1S-S-1 258.1 None NB1S NB1S-S-2 255.5 None NB1S NB1S-S-3 252.2 None NB1C NB1C-W-1 252.8 None NB1C NB1C-W-2 254.3 None NB1C NB1C-W-3 254.5 None Ultimate Load Test Results Part No. Serial No. Max Load Applied (lbf) Visual Damage/ Deformation NB1C NB1C-W-3 588.5 Yes, see Note 1 NB1C NB1C-S-3 561.9 Yes, see Note 1 NB1S NB1S-S-3 631.0 None Note 1: For Serial Nos. NB1C-S-3 and NB1C-W-3, there was concave shape deformation at the center of the Anchoring Bracket while the anchoring screws remained secured. It was also noted that the stainless steel bolt that secured the steel 90° angle to the Anchoring Bracket was bent in the applied load direction. The test results recorded in this report apply only to the sample(s) as received and relate only to those items tested.
  • 3. 20-0775A Pg 3 This report shall not be reproduced, except in full, without written approval from Dayton T. Brown, Inc. If you have any questions, please do not hesitate to contact the undersigned at (631) 589-6300 ext. 4571. Very truly yours, DAYTON T. BROWN, INC. Don Landwehrle Engineer Warren Halbig Department Manager DL:rb
  • 5. 20-0775AEnc1Pg1 Test equipment utilized for the program reported herein was within its assigned interval of calibration. Details are on file at Dayton T. Brown, Inc. and will be made available upon request. 417541-01Job Sub: CAL DUE DATEACCURACYMODEL DTB NO.MANUFACTURERITEM TEST: PROOF AND ULTIMATE LOAD CONTROL SYSTEM, AERO ST 32 CH. CONTROL, 64 CH. DATA MTS 10-228493.10/793.00 10/10/2021Mfr TAPE MEASURE, 25' STANLEY 15-7833-725 05/23/2021± 1/16" LOAD CELL, 2K LB 5/8 X 18 THREAD INTERFACE 62-7691210-AF-2K-B 04/03/2022± 0.1% of F.S. LEVEL, DIGITAL 10" MULTI- FUNCTION WITH LASER TRAC CRAFTSMAN 67-22320.48292 09/26/2021± 0.1°
  • 7. 20-0775A Enc 2 Pg 1 Photo 1 – File No. PA300968 Test Setup with Aluminum Shoe Photo 2 – File No. PA300986 Typical Test Setup with Steel 90° Angle
  • 8. 20-0775A Enc 2 Pg 2 Photo 3 – File No. PA300990 Serial No. NB1C-W-3 Ultimate Test Deformation
  • 10. 20-0775A Enc 3 Pg 1 -50 0 50 100 150 200 250 300 11:48:44 11:48:50 11:48:56 11:49:02 11:49:08 11:49:14 11:49:20 11:49:26 11:49:32 11:49:38 11:49:44 11:49:49 11:49:55 11:50:01 11:50:07 11:50:13 11:50:19 11:50:25 11:50:31 11:50:37 11:50:43 11:50:49 11:50:55 11:51:01 11:51:07 11:51:13 11:51:19 11:51:25 11:51:31 11:51:37 11:51:43 11:51:49 11:51:55 11:52:00 Load(LBF) Time Stamp NB1C-S Sample Data CONTROL FEEDBACK
  • 11. 20-0775A Enc 3 Pg 2 -50 0 50 100 150 200 250 300 13:54:46 13:54:40 13:54:38 13:54:44 13:54:49 13:54:55 13:55:00 13:55:06 13:55:11 13:55:17 13:55:23 13:55:28 13:55:34 13:55:39 13:55:45 13:55:50 13:55:56 13:56:01 13:56:07 13:56:13 13:56:18 13:56:24 13:56:29 13:56:35 13:56:40 13:56:46 13:56:52 13:56:57 13:57:03 13:57:08 13:57:14 13:57:19 13:57:25 13:57:31 Load(LBF) Time Stamp NB1S-S Sample Data CONTROL FEEDBACK
  • 12. 20-0775A Enc 3 Pg 3 -50 0 50 100 150 200 250 300 14:32:53 14:32:47 14:32:41 14:32:35 14:32:29 14:32:23 14:32:17 14:32:11 14:32:05 14:31:59 14:31:53 14:31:47 14:31:41 14:31:35 14:31:29 14:31:23 14:31:17 14:31:11 14:31:04 14:30:58 14:30:52 14:30:46 14:30:40 14:30:34 14:30:28 14:30:22 14:30:16 14:30:10 14:30:04 14:29:58 14:29:52 14:29:46 14:29:40 14:29:34 Load(LBF) Time Stamp NB1C-W Sample Data CONTROL FEEDBACK