Attachment 1 - SOW 11.29.23.pdf

FTFA24-MM01– Repair North and South Hangar Doors B110

Eglin Air Force Base, Florida

DESIGN BUILD

STATEMENT OF WORK

Repair North and South Hangar Doors B110 Project No. FTFA24-MM01

Eglin Air Force Base, Florida

Original Release – 29 November 2023

CEG/CENMPV

Table of Contents

1. Purpose

2. Background

3. Description of Work

3.1 Existing Conditions …………………………………………………………………………10

3.2 Electrical ……………………………………………………………………………………10

4. General Requirements

5. Meetings and Submittals

6. Government Furnished Materials

7. Period of Performance

8. Summary of Required Activities

9. Eglin Specific Requirements

1. Purpose:

This statement of work (SOW) outlines the basic requirements of the Repair North and South Hangar Doors, FTFA24-MM01.

2. Background:

The project is located on Eglin AFB, Building 110. This project resulted from two (2) surveys that were conducted during a previous project (FTFA21-VH43). These surveys were conducted due to the discovery of excessive wear on several operating components of the northside and southside hangar doors. All parts that are to be removed/replaced were identified in these surveys. There are a total of two (2) hangar doors, northside and southside. Each hangar door consists of sixteen (16) wire ropes (.88” or 7/8”) with a 6x36 wire rope construction, sixteen (16) horizontal sheave assemblies, sixteen (16) header sheave assemblies, seven (7) trolley assemblies, and a total of sixteen (16) counterweight sheave assemblies (8 each per counterweight). Each wire rope runs the entire span of the hangar, allowing one end to be connected to the counterweight and one end connected to the front of the hangar door.

The hangar doors are considered a “canopy-style” door. All part numbers were provided by the original manufacturer, International Door, Inc. (Byrne Door Division).

3. Description of Work:

The contractor shall furnish all parts, labor, tools, materials, plans, and transportation necessary to remove and replace the operating components of both the northside and southside hangar doors at Building 110 that have been identified as worn beyond limits. All operating components of both hangar doors are located above ceiling (approx. 50’). Some components of the operating system can weight up to +200 lbs and will require proper aerial lifting equipment for removal/replacement. There are several access doors located throughout the ceiling that will allow for part removal/replacement execution. Only one door should be disabled at a time to allow for continued operational use for aircraft maintenance. On the basis of design, the government used specific OEM parts from International Door, Inc.

(Northside door operating components layout)

For the northside door, the Contractor shall:

• Remove & replace eight (8) each left-hand (LH) counterweight sheave assemblies with part #531-A33. (item A)

(Counterweight sheave assemblies)

• Remove & replace four (4) each LH counterweight guide shoes with part #E-122. (item B)

(Counterweight guide shoes)

• Remove & replace eight (8) each right-hand (RH) counterweight sheave assemblies with part #531-A33. (item H)

• Remove & replace four (4) each RH counterweight guide shoes with part #E-122. (item I)

• Remove & replace two (2) each cable deflector assemblies with part #531-B4. (item F & G)

(Cable deflector assembly)

• Remove & replace seven (7) each horizontal sheave assemblies (#1, 2, 5, 6, 10, 14, 16) with part #531-A33 A/B. (item C)

(Horizontal sheave assembly)

• Remove and replace thirteen (13) cable sets to include fittings and clamps (#1, 2, 3, 4, 6, 7, 8, 9, 10, 12, 14, 15, 16) with part #531-A7.

(Cable sets)

• Remove and replace four (4) each center cable hitch assemblies (#7, 8, 9, 10) with part #E-252. (item E)

(Cable hitch assembly)

• Remove and replace three (3) each intermediate cable hitch assemblies (#4, 6, 12) with part #E-253. (item E)

• Remove and replace six (6) each end cable hitch assemblies (#1, 2, 3, 14, 15, 16) with part #E-254. (item E)

• Remove and replace eight (8) each header (door) sheave assemblies (#1, 4, 5, 6, 12, 13, 14, 16) with part #531-A33 C. (item D)

(Header “door” sheave assembly)

• Remove and replace fourteen (14) closure roller assembly sets with part #E-291.

(Closure roller assembly)

• Remove and replace fourteen (14) closure plate assemblies with part #E-290.

(Southside door operating components layout)

For the southside door, the Contractor shall:

• Remove and replace one (1) each LH counterweight sheave assembly with part #531-A33.

(item A)

• Remove and replace four (4) each LH counterweight guide shoes with part #E-122. (item B)

• Remove and replace four (4) each RH counterweight sheave assemblies with part #531- A33. (item H)

• Remove & replace four (4) each RH counterweight guide shoes with part #E-122. (item I)

• Remove & replace two (2) each cable deflector assemblies with part #531-B4. (item F & G)

(Cable deflector assembly)

• Remove and replace twelve (12) each horizontal sheave assemblies (#1, 2, 3, 4, 5, 8, 11, 12,13, 14, 15, 16) with part #531-A33 A/B. (item C)

(Horizontal sheave assembly)

• Remove and replace seven (7) cable sets to include fittings and clamps (#1, 2, 3, 4, 5, 6, 8) with part #531-A7.

• Remove and replace one (1) each center cable hitch assembly (#8) with part #E-252. (item E)

• Remove and replace three (3) each intermediate cable hitch assemblies (#4, 5, 6) with part #E-253. (item E)

• Remove and replace three (3) each end cable hitch assemblies (#1, 2, 3) with part #E-254.

(item E)

• Remove and replace fourteen (14) header (door) sheave assemblies (1, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16) with part #531-A33 C. (item D)

(Header “door” sheave assembly)

• Remove and replace fourteen (14) closure roller assembly sets with part #E-291.

• Remove and replace fourteen (14) closure plate assemblies with part #E-290.

• Remove and replace components of one (1) each identified trolley assembly to include bottom back brace bearing assembly (part #E-215), top lever pin assembly (part #E-216), bottom lever pin assembly (part #E-216), bottom guide strut bracket assembly (part #E- 260), and cam roller assembly (part #E-277). Trolly assembly is located on the southside door and is positioned at the end of the door near the middle of the hangar.

(Trolly assembly)

• Properly grease and lubricate all parts to include sheaves, cables, and bearings to factory specifications.

• Perform operations check on northside and southside door once components are replaced IAW A13.4. Hangar 110.

3.1 Existing Conditions:

The hangar door operating system was created and installed by International Door, Inc (Byrne Door Division). Occupants in Bldg. 110 are instructed to only operate hangar doors for removal/placement of aircraft inside hangar and/or emergency situations.

3.2 Electrical:

All Lockout Tagout (LOTO) procedures should be performed on the electrical system providing power to both doors during repair of the system components.

4. General Requirements:

The Contractor shall identify and comply with all applicable federal, state, and local statues;

Air Force and Department of Defense instructions, manuals, handbooks, regulations, guidance and policy letters; Executive Orders (EOs); National Fire Protection Association (NFPA);

Uniform Criteria (UFC); International Building Code (IBC); International Plumbing Code (IPC); Vault/Security Compartment Information Facility (SCIF) requirements; International Mechanical Code (IMC) Florida Department of Transportation (FDOT) including all changes and amendments in effect on the date of issuance of this contract.

The area where the work is to be performed will be available for inspection. A pre-proposal site visit will be conducted at a date and time specified by the Contracting Officer. All existing conditions shall be field verified by the Contractor during the site visit(s). The Government is not responsible for providing any surveys or measurements.

Staging areas and haul routes shall be provided by the Contracting Officer. The construction site shall be kept neat and free of trash and debris at all times. This project will be on the airfield and all contractors will have to obtain an Airfield Driver’s License.

5. Meetings and Submittals:

The Contractor shall participate in and facilitate on-site meetings and all design review meetings. The Contractor shall prepare and submit meeting minutes to the Contracting Officer within two (2) calendar days after every meeting.

The Contractor shall submit for approval a complete design schedule, with all submittal and review meeting dates, within seven (7) calendar days after the Notice to Proceed (NTP). The schedule shall be based on the following proposed design agenda.

• Design kick-off meeting shall be same date as NTP.

• 100% final design shall be 14 calendar days from the 95% Government review. The Government review shall be 14 calendar days followed by a pre-construction conference.

All items required in each stage of design shall be submitted as one (1) complete package. No partial submittals will be accepted. The Contractor shall provide the comments from the Government review at each design submittal. A response of “will comply” IS NOT acceptable.

The Contractor shall annotate the comments with the actions taken and incorporate the annotated comments with the next design submittal.

The 100% final design submittal shall include one (1) full size bound set of drawings (24 x 36), two (2) bound sets of half size (12x18) drawings, two bound sets of specifications, two bound sets of design analysis, an electronic version of the complete submittal on one compact disc with the drawings in AutoCAD format and t in Adobe PDF format, specifications, and design analysis in Adobe PDF format.

The as-built drawings and specifications that reflect addendums, field changes and modifications shall be submitted at close out of the project.

REQUIRED ITEMS:

(X) A. Parts/Hardware schedule (submittals)

The Contractor shall identify and have on his staff a State Licensed Designer of Record to develop submittals during design and construction. The Contractor’s Designer of Record shall produce a Submittal Register at each design submittal. The Contractor’s Designer of Record shall be responsible for listing, reviewing, and approving each submittal necessary to ensure the project requirements are in compliance. The Submittal Register shall identify items such as shop drawings, manufacturer’s literature, certificates of compliance, material samples, guarantees, test results, etc. that the Contractor shall submit for Government review and/or approval action. The Designer of Record shall review and approve all submittals they are responsible for prior to submittal to the Government. Upon approval by the Contractor, five

(5) copies of that submittal shall be submitted to the Contracting Officer.

Progress Schedules shall be submitted using AF Form 3064 and Progress Reports shall be submitted using AF Form 3065. All material submittal that are scheduled for government review and approval shall be reviewed by the designer of record (DOR) prior to submitting to the government.

6. Government Furnished Materials:

Project related drawings and data are available for review at 96 Civil Engineering Group, building 634, Eglin AFB and are for informational purposes only. Eglin AFB standard title sheet, drawing sheets, and title block shall be provided to the Contractor in electronic format.

7. Period of Performance:

The Period of Performance is 180 calendar days.

8. Summary of Activities:

9. Eglin Specific Requirements:

Reference the Eglin Design Manual for all Eglin specific requirements.

REQUIED ACTION: TIME FRAME:

Pre-proposal site visit TBD Notice to Proceed Design kick-off meeting

Period of Performance 180 calendar days for construction

Pre-construction conference 21 calendar days after 100% final submission

Meeting minutes 2 calendar days of meeting AF Form 3064 7 calendar days of award AF Form 3065 Weekly AF Form 3000 As required Pre-final inspection 7 calendar days before final inspection Final inspection 180 calendar days after NTP 1354 Real Property Check List 180 calendar days after NTP