Harry Pepper and Associates, Inc.

Armed Services Board of Contract Appeals·Decided November 3, 2021·No. ASBCA No. 62038, 62039, 62040, 62042·Published

Opinion

ARMED SERVICES BOARD OF CONTRACT APPEALS Appeals of - ) ) Harry Pepper and Associates, Inc. ) ASBCA Nos. 62038, 62039 ) 62040, 62042 ) Under Contract No. NNS14AA30T )

APPEARANCES FOR THE APPELLANT: David W. Mockbee, Esq. D. Wesley Mockbee, Esq. Judson R. Jones, Esq. Mockbee Hall & Drake, P.A. Jackson, MS

APPEARANCES FOR THE GOVERNMENT: Scott W. Barber, Esq. NASA Chief Trial Attorney Jeffrey A. Renshaw, Esq. Shannon A. Sharkey, Esq. Jennifer L. Rawls, Esq. Trial Attorneys Stennis Space Center, MS

OPINION BY ADMINISTRATIVE JUDGE O’CONNELL

Harry Pepper and Associates, Inc. (HPA) appeals final decisions by a contracting officer from the National Aeronautics and Space Administration (NASA). The Board conducted a hearing from March 1-12, 2021, at which we heard testimony from 12 witnesses and received into evidence more than 600 exhibits or Rule 4 documents. Only entitlement is before us. The Board sustains appeal No. 62038 in part, and denies Nos. 62039, 62040, and 62042.

FINDINGS OF FACT

1. NASA’s Stennis Space Center in Mississippi awarded HPA an indefinite delivery/indefinite quantity, multiple award construction contract on August 3, 2012 (R4, tab 1 at 3-4 1). The contract contained various relevant clauses, including G.1, Contract Administration, and G.2, Technical Direction, which defined the authority of the contracting officer (CO) and the contracting officer’s representative (COR), respectively (id. at 11-12). The contract also included Federal Acquisition Regulation (FAR)

1 Rule 4 file cites are to the .pdf page number in the electronic file. 52.236-2, DIFFERING SITE CONDITIONS (APR 1984) (the DSC clause), FAR 52.236- 3, SITE INVESTIGATION AND CONDITIONS AFFECTING THE WORK (APR 1984), FAR 52.243-4, CHANGES (JUN 2007), and FAR 52.246-12, INSPECTION OF CONSTRUCTION (AUG 1996) (R4, tab 1 at 9, 26-27).

2. On January 9, 2014, NASA awarded HPA the above-referenced task order in the amount of $36,577,459 for the B2 Test Stand Restoration, Work Package 3, which required HPA to complete the work within 400 days (R4, tab 2 at 2-4).

3. NASA constructed the B2 test stand in the 1960s to test the Saturn V rockets that carried humans to the Moon during the Apollo program. Work Package 3 is part of a program that restored and augmented the stand to test the core stage of NASA’s new Space Launch System (SLS), the cornerstone vehicle for NASA’s Artemis Program that (it is hoped) will return humans to the Moon in the 2020s. (R4, tab 18 at 7; see https://www.nasa.gov/sites/default/files/atoms/files/b-2_test_stand_v1.pdf)

4. HPA performed an earlier contract on the B2 test stand referred to as Work Package 1. Through its work on that contract, HPA had access to the test stand for 15 months prior to award of Work Package 3. (Tr. 6/208-09) In addition, prior to the submission of bids for the task order, NASA allowed bidders to attend a site visit on October 22, 2013 (tr. 6/205; ex. G-20).

5. HPA has filed these appeals on behalf of its subcontractor, Quality Iron Fabricators, Inc. (Quality Iron) and Quality Iron’s sub-subcontractor, River City Erectors, LLC (River City) (app. supp. R4, tabs 7-8, 142). Neither Quality Iron, nor River City, attended the pre-bid site visit (tr. 6/205; ex. G-20).

6. The existing test stand structure included a booster support frame, which is referred to as the “battleship” and is made of heavy steel plates reminiscent of a naval vessel (tr. 1/48-51, 6/118; R4, tab 5 at 6, tab 18 at 8). The Saturn V rocket was placed in the interior of the battleship during testing (tr. 6/118). Above the battleship was the main propulsion test article (MPTA) structure, the top of which is the “corvette,” also in the naval sense, and made of steel plate like the battleship (tr. 1/46-47, 51, 6/118).

7. The contract required placement of temporary steel track to relocate the MPTA structure by moving it 20-feet north (R4, tab 18 at 7). HPA had to lift the structure, which weighed about 1.2 million pounds, place it on the track, carry out the move, and then remove the track (id. at 7-8; tr. 1/61; app. supp. R4, tab 26).

8. Due to the loads applied during the move, and those to be applied in the future, the contract also provided for the battleship to be reinforced. To accomplish this, HPA

2 had to weld 28 structural steel shapes to the existing steel plates. These steel shapes are referred to as “WTs” or “split tees” because they are an I-beam that has been cut in half (forming a tee shape). (R4, tab 18 at 8; tr. 1/85, 237-38, 4/94) As detailed below, a variety of issues with the WTs form the basis of request for equitable adjustment (REA) nos. 1 and 4, which are at issue in ASBCA No. 62038.

9. The contract called for the addition of plates (doubler plates) at the bottom of existing columns in the MPTA structure to carry the increased loads, as well as the thrust from the core stage engine tests (R4, tab 4 at 17 (S-505), tab 18 at 8; tr. 1/112-13, 4/94). HPA alleges in REA Nos. 9 and 10 that it performed additional work on these baseplates (ASBCA Nos. 62039 and 62040).

10. The contract provided for construction of a new SLS Support Tower on top of the existing structure for testing larger and more powerful rocket engines, as well as an Access Tower directly on top of the SLS Support Tower. This new structure (described in the specifications as a “space truss”) was 93-feet tall and more than 300-feet above grade. (R4, tab 18 at 8; tr. 4/94-95) In REA 12 (ASBCA No. 62042), HPA alleges that it encountered unexpected thermal movement of the structure above the top of the battleship during the construction of the SLS structure.

ASBCA No. 62038 (REAs 1 & 4)

11. NASA issued a notice to proceed on February 7, 2014 (R4, tab 3 at 2).

A. REA 4

12. The WTs were 27-feet long, which was only a few inches shorter than the interior height of the battleship, and weighed 99 pounds per foot (tr. 1/62, 71). To bring them inside, the contract drawings provided that HPA could cut a 36-inch diameter hole in the top or bottom plate of the battleship (although the specifications mentioned only the top plate) (R4, tab 6 at 7, tab 18 at 8).

13. During the hearing, there was a sharp difference of opinion between HPA and NASA with respect to the feasibility of lowering the WTs by crane through holes cut in the top plate of the battleship. The Quality Iron and River City witnesses testified that there were too many obstructions inside and above the battleship to do so. (Tr. 1/69-71, 93, 98-99, 225) The HPA witnesses also testified that it was impossible to bring the WTs in through the bottom (e.g., tr. 1/89-91, 240). NASA believed that both were possible (e.g., tr. 8/38, 107-08).

3 14. The witness whose testimony the Board found most credible on this issue was Charles Stewart, who was Head of Construction for NASA at Stennis Space Center from 1986 to 2003 (tr. 6/157-58). According to CO Jason Edge, Mr. Stewart knew the B2 test stand “like the back of his hand” (tr. 7/137). More than a decade after he left NASA, Mr. Stewart became Head of Field Operations for HPA on this task order, supervising the field superintendents and subcontractors and coordinating with NASA (tr. 6/124-25).

15. Mr. Stewart characterized lowering the WTs through the top plate by crane as “doable.” He agreed that there were obstructions in a few places, but testified that HPA could have worked around them. (Tr. 6/128-29) Mr. Stewart was more concerned with cutting through the 2.25-inch thick steel plate, which he characterized as “doable ... but very complicated” because it required “heat stress and a tremendous amount of welding” (tr. 6/127; R4, tab 6 at 7 (“EXIST 2 1/4 TOP PL”)). Mr.

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