Warning_Horn_SOW_Final_20June2013.docx
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Statement of Work for
Warning Horn Replacement Kit
Permanent Modification for the
KC-135 R/T
Date: 20 June 2013
Purchase Request No. GFD2030-12-39994
PREPARING ORGANIZATION: AFLCMC/WKDMB TINKER AFB OK 73145
Table of Contents……………………...…………………………………………. 2
1. Scope……………………………………………………………… 3
| 1.1 Background……………………………………………………………… | 3 |
| 1.2 Problem………………………………………………………………… | 3 |
| 1.3 Solution………………………………………………………………… | 3 |
2. Applicable Documents…………………………………………… 3
| 2.1 Department of Defense (DoD) Specifications………………………….... | 3 | |
| 2.2 DoD Standards…………………………………………………………… | 4 | |
| 3. Program Management Requirements…………………………… 4 | ||
| 3.1 Post Award Conference………………………………………………… | 4 | |
| 4. Technical Requirements………………………………………… | 4 | |
| 4.1 System Requirements……………………………………………………. | 4 | |
| 4.2 Component Requirements…………………………………………. | ……. | 5 |
| 4.3 Assembly Requirements…………………………………………………. | 5 | |
| 5. Production and Delivery ………………………………………… | 8 | |
| 5.1 Kit Production…………………………………………………………… | 8 | |
| 5.2 Physical Configuration Audit (PCA) ……………………………………. | 8 | |
| 5.3 Green Procurement……………………………………………………… | 8 | |
| 5.4 Initial Provisioning Spares……………………………………………… | 8 | |
| 5.5 Packaging and Handling…………………………..………………….… | 9 | |
| 5.5.1 Kit Shipping…………………………………………………….… | 9 | |
| 5.5.2 Spares Shipping…………………………………………………… | 9 | |
| 6. Data/Documentation Requirements…………………………… | 10 | |
| 6.1 Product Drawings……………………………………………………… | 10 | |
| 6.2 Airworthiness Certification Criteria Report…………………………… | 10 | |
| Attachments………………………………………………………… | 11 |
Tables Table 1: Specifications………………………………………………………………. 3 Table 2: Standards…………………………………………………………………... 4 Table 3: Warning Horn Replacement Kit Delivery Schedule ………………………. 9 Table 4: Initial Spares Quantities…………………………………………………… 9 Table 5: Initial Spares Shipping Addresses……….………………………………. 10
Figures
| Figure 1: Aft Mounting Envelope …………………………………………………….. 6 | |
| Figure 2: Forward Mounting Envelope ………………………………………………. 7 | |
| Figure 3: Existing KC-135 Aft Warning Horn ….…………………………………….. 8 | |
| Figure 4: Existing KC-135 Forward Warning Horn…….……………………………... 8 |
1. Scope This Statement of Work (SOW) defines the work to be performed by the contractor necessary to manufacture the Warning Horn Replacement articles. The work performed by the contractor shall consist of providing the following resources: kitted materials, data, and management. These resources are required to acquire, document, and deliver the production of warning horns, forward mounting brackets, aft mounting brackets, and connectors.
1.1. Background
The KC-135 R/T warning horn provides an audible warning signal in case of emergencies.
1.2. Problem
The current KC-135 R/T warning horn is not explosion atmosphere qualified and operates in a known fuel vapor environment.
1.3. Solution
Procure a qualified explosive atmosphere warning horn to replace existing horn.
2. Applicable Documents The requirements for the warning horn are described within MIL-S-6904B and this document. When the requirements of this document and MIL-S-6904B are in conflict, the requirements of this document shall govern. Review Table 1 and Table 2 for specification and standard notes.
Unless otherwise indicated, copies of specifications, standards and handbooks listed below are available from the Standardization Document Order Desk, 700 Robbins Ave, Bldg 4D, Philadelphia PA 19111-5094.
2.1. Department of Defense (DoD) Specifications
| Original Specification |
| Superseding Specification |
| Notes |
| MIL-E-5272 |
| MIL-STD-810G |
| None |
| MIL-S-6904/1 |
| None |
| Not Applicable |
| MIL-S-6904/2 |
| None |
| Not a prerequisite |
| MIL-S-6904/3 |
| None |
| Not a prerequisite |
| MIL-S-7742 |
| None |
| Not for new design |
| MIL-E-17555 |
| None |
| Cancelled with no replacement |
| MIL-D-70327 |
| None |
| Cancelled, refer to MIL-STD-31000 |
Table 1: Specifications
2.2. DoD Standards
| Original Standards |
| Superseding Standard |
| Notes |
| MIL-STD-2073-1E W/Change 1 |
| Not Applicable |
| None |
| MIL-STD-31000 |
| Not Applicable |
| None |
| MIL-STD-105 |
| None |
| Refer to MIL-STD-1916, DOD PREFERRED METHODS FOR ACCEPTANCE OF PRODUCT |
| MIL-STD-129 |
| Not Applicable |
| None |
| MIL-STD-130 |
| Not Applicable |
| None |
| MIL-STD-704 |
| Not Applicable |
| None |
| MIL-STD-831 |
| None |
| Refer to MIL-HDBK-831 |
| MS33586 |
| None |
| Use MIL-STD-889B |
| MS3102 |
| None |
| Cancelled, refer to SAE AS31021 |
Table 2: Standards
3. Program Management Requirements The contractor shall designate a single point of contact (POC) to the contracting officer for all tasks required for the program. The POC shall be responsible and shall have authority for the control and coordination of all work performed and kits delivered under this SOW.
3.1. Post Award Conference
A post award conference shall be held in accordance with (IAW) FAR Part 15.
4. Technical Requirements This section provides a description of the Warning Horn Replacement Kit.
4.1. System Requirements
The warning horn system shall be qualified to operate within a fuel vapor bearing area that meets or exceeds MIL-STD-810G, Method 511.5, Procedure I or equivalent industry standard.
The test article shall be placed in a chamber and exposed to an environment containing percentage volumetric fuel vapor, air/vapor ratio (AVR) by weight. The test article shall be turned on and off as many times as can be completed during the test interval. The test shall be conducted in an atmosphere equivalent to 30,000 ft and at ground level. No ignition must occur during this test.
The contractor shall provide the government with all necessary technical data/information used in the development of the system. This information will be used to satisfy airworthiness and defense stock listing requirements.
At a minimum the technical data required shall address the following:
1. Proof of explosion proof testing per MIL-STD0810G, Method 511.5, Procedure 1, or equivalent.
2. Structural integrity paperwork to satisfy KC-135 crash loading service bulletin (Attachment 1) 11 Oct 2001
3. Drawings as stated in section 6.1 of this document.
4. Copies of all technical information used to satisfy section 6.2, airworthiness criteria certification report, of this document.
4.2. Component Requirements
A kit shall consist of a forward horn, aft horn, any necessary forward and aft mounting brackets, mounting fasteners, and electrical connectors.
The forward horn shall direct sound aft and the aft horn shall direct sound forward. The aft horn must bolt into 4 nut plates, NAS680A3, in the dimensions shown in Figure 1. The forward horn must mount into the dimensions shown in Figure 2; there are no nut plates currently in this area. Mounted warning horn shall be able to withstand a crash loading of 9G forward, 1.5G aft, 8G down, 4G up, and 4G inboard and outboard.
The current horns operate on a 28VDC circuit using a MS3102C-10SL-4P connector. Replacement horns must not exceed 28VDC and must use a two wire connector as long as connector is sealed to be operated in a fuel vapor bearing area, as described in section 4.1. If connector MS3102C-10SL-4P is used the male connector shall be provided. If a connector other than a MS3102C-10SL-4P is used, both female receptacle and male connector must be provided in the kit for both horns.
Replacement horns must produce an audible warning signal of at least 100 dB at a distance of 3 feet, measured on a standard sound meter in a soundproof room.
4.3. Assembly Requirements
The warning horn assembly shall mount in the existing locations. Current warning horn fits within a 12.000 x 5.375 x 8.500 inch envelope; replacement assembly is not constricted to this envelope but must not create interference with surrounding structures. Figure 1 and Figure 2 display the maximum envelope available for the new warning horn, and shall not exceed this limit. The current warning horns used on the KC-135 at the aft and forward locations are shown in Figure 3 and Figure 4 with general location of the mounting areas.
Figure 1: Aft Mounting Envelope
Figure 2: Forward Mounting Envelope
Figure 3: Existing KC-135 Aft Warning Horn
Figure 4: Existing KC-135 Forward Warning Horn
5. Production and Delivery
5.1. Kit Production
The contractor shall provide 398 Warning Horn Replacement Kits (NSN: 1560-K0-109-343A FL) to the Government IAW Table 3.
| Days after Contract Award |
| 75 |
| Kits |
| 3 |
| Days after approval of Government PCA and Val/Cert |
| 75 |
| 105 |
| 135 |
| 165 |
| Kits |
| 100 |
| 100 |
| 100 |
| 95 |
Table 3: Warning Horn Replacement Kit Delivery Schedule Note: Expedition of kits deliveries will be accepted
5.2. Physical Configuration Audit (PCA)
The contractor shall provide three production representative Warning Horn Replacement Kits for a PCA. The government will facilitate the PCA at Tinker AFB, contractor participation is required. No Functional Configuration Audit will take place.
5.3. Green Procurement
The Contractor shall comply with the Green Procurement Program (GPP). GPP is a mandatory federal acquisition program that focuses on the purchase and use of environmentally preferable products and services. FAR 23.404 applies and states the GPP requires 100% of EPA designated product purchases that are included in the Comprehensive Procurement Guidelines (CPG) list that contains recovered materials, unless the item cannot be acquired: a) competitively within a reasonable timeframe; b) within appropriate performance standards; or c) at a reasonable price. The prime contractor is responsible for ensuring that all subcontractors comply with this requirement.
5.4. Initial Provisioning Spares
The contractor shall provide initial provisioning spares quantities IAW Table 4. All initial provisioning spares will be individually packaged for shipment. All spares will be provided with first lot delivery.
Warning Horn Initial Provisioning Spares
| Nomenclature |
| Spare Requirement |
| Horn, Warning |
| 12 |
| Mounting Plate, Forward |
| 6 |
| Mounting Plate, Aft |
| 6 |
| Connectors |
| 12 |
Table 4: Initial Spares Quantities
5.5. Packaging and Handling
The contractor shall package the Warning Horn Replacement Kits and initial spares for shipment in accordance with ASTM-D-3951, Commercial Packaging or MIL-STD-2073-1E W/Change 1, the Standard Practice for Military Packaging. The contractor shall mark the packages for shipping and storage in accordance with MIL-STD-129P, Military Marking for Shipment and Storage. Shipping will operate under the FOB Destination structure, with the contractor paying for shipping and retaining ownership of all packages until they are accepted by the government at their destination.
5.5.1. Kit Shipping Location
Ship all 398 Warning Horn Replacement Kits to the following address:
FB2039 OC-ALC
Bldg. 506 CML PH (405) 739-2349 7401 Arnold St. Door 22 Tinker AFB, OK 73145-9013 Mark for: Account 09
5.5.2. Spares Shipping Location
Ship all initial spares in accordance with Table 5. (12 horns/6 sets)
| Description: |
| Quantity: |
| Address: |
| Horn, Warning |
| 4 |
| FB4620 92 LRS LGS |
BLDG 2045 CML PHN 509 247 3828
400 S GATE 35 RD
FAIRCHILD AFB WA 99011-9685
| Forward Mounting Bracket |
| 2 |
| Aft Mounting Bracket |
| 2 |
| Connector |
| 4 |
| Horn, Warning |
| 6 |
| FB6151 184 ARW LRS |
CML PHN 316 759 7622
57330 MUSTANG DR STE 13
MCCONNELL AFB KS 67221-9013
| Forward Mounting Bracket |
| 3 |
| Aft Mounting Bracket |
| 3 |
| Connector |
| 6 |
| Horn, Warning |
| 2 |
| FB4814 6 LRS LGRDDC MACDILL AFB |
BLDG P49 CP 813 828 1800
8307 CYPRESS STAND DR
TAMPA FL 33621-5511
| Forward Mounting Bracket |
| 1 |
| Aft Mounting Bracket |
| 1 |
| Connector |
| 2 |
Table 5: Initial Spares Shipping Address
6. Data/Documentation Requirements
6.1. Product Drawings
The Contractor shall deliver all production level (3) technical data for the aft mounting bracket and forward mounting bracket to the Government IAW CDRL A001.
The Contractor shall deliver all conceptual level (2) technical data for the Warning Horn Replacement Kit and the warning horn and connector to the Government IAW CDRL A001.
6.2. Airworthiness Certification Criteria Report
The Contractor shall deliver initial and final MACC IAW CDRL A002.
Attachments:
1. KC-135 Crash Loading Requirements Memo.pdf (11 Oct 2001)
2. Warning Horn Modified Airworthiness Certification Criteria (MACC) image2.jpeg image3.png image4.png image1.jpeg
File details come from the government source that posted it. Updated .