PD06WRGBZOENF34_

Support Equipment and Vehicle Management Directorate PD06WRGBZOENF34 Ground Support Equipment Branch Page 1 of 22

642 CBSSS/GBZO-ENF 4/10/2008

CAGE 98752

PURCHASE DESCRIPTION

C-130 ISOCHRONAL (ISO) MAINTENANCE STAND

1.0 SCOPE

This purchase description covers the requirements for the C-130 Isochronal (ISO) Maintenance Stand. Depending on space available and user needs, the C-130 ISO Stand allows maintenance and inspection personnel partial or full access to the wings, fuselage, tail and engines of the C-130 Aircraft during ISO maintenance. The C-130 ISO Stand is a multi-stand structure that shall integrate with one another as well as accommodate the

C-130E, C-130H(2), C-130H(3), C-130J, AC-130E, AC-130H, WC-130H, WC-130J,

MC-130E, MC-130H, and HC-130H(N) models of the C-130 Aircraft. The stands are located in various areas of the Continental United States (CONUS) and overseas locations. Assembly will be required at each base location, which consists of approximately 30 different locations within CONUS and three overseas locations.

2.0 APPLICABLE DOCUMENTS

2.1 Specifications and standards. The documents listed in this section are specified in sections 3 and 4 of this performance description. This section does not include documents in other sections of this performance description or recommended for additional information or as examples. While every effort has been made to ensure the completeness of this list, document users are cautioned that they must meet all specified requirements documents cited in sections 3 and 4 of this performance description, whether or not they are listed.

All other documents required by suppliers in connection with specific procurement functions should be obtained from the procuring activity or as directed by the contracting officer.

AFOSH 91-501 Air Force Consolidated Occupational Safety Standard

AFOSH STD 48-8 Controlling Exposures to Hazardous Materials

FED-STD-595B Colors Used in Government Procurement

MIL-STD-1472F Human Engineering

MIL-STD-810F Environmental Engineering Considerations and

Laboratory Tests

Distribution Statement A. Approved for public release; distribution is unlimited.

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MIL-HDBK-808 Finish, Protective and Codes for Finishing Schemes for Ground and Ground Support Equipment

MIL-HDBK-781A Reliability Test Methods, Plans, and Environments for Engineering Development, Qualification, and Production

(Application for copies are available from the Document Automation and Production Service, Building 4/D (DPM-DODSSP), 700 Robbins Avenue, Philadelphia, PA 19111-5094 or http://astimage.daps.dla.mil/quicksearch/ or www.dodssp.daps.mil.)

AWS D1.1/D1.2 Structural Welding Code

(Application for copies should be addressed to American Welding Society, 550 N.W. LeJeune Road, Miami, FL 33126)

NFPA 70 National Electric Code

(Application for copies should be addressed to National Fire Protection Association, 1 Batterymarch Park, Quincy, MA 02169-7471)

TO 35-1-3 Corrosion Prevention, Painting And Marking Of

USAF Support Equip (SE)

(Application for copies can be downloaded from the following website:

http://www.robins.af.mil/library/technicalorders.asp.)

2.2 Order of Precedence

In the event of a conflict between the text of this document and the references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained. The contractor shall meet all applicable codes, standards, laws and regulations at the revision most current at the time of manufacture of each C-130 ISO Stand set.

3.0 GENERAL REQUIREMENTS

3.1 General

The C-130 ISO Stand shall consist of a multi-stand structure allowing maintenance and inspection access to the wings, fuselage, engines, and tails of the C-130 Aircraft. The entire package shall allow full access around the aircraft, http://astimage.daps.dla.mil/quicksearch/ http://www.dodssp.daps.mil/ http://www.robins.af.mil/library/technicalorders.asp

Ground Support Equipment Branch Page 3 of 22 except the nose area. The ISO stand shall provide electrical and pneumatic utilities as detailed in this specification. Stands shall permit the use of nose, wing and tail jacks, and these stands shall be adjustable in the vertical direction as specified herein. The C-130 ISO Stand shall, as a minimum, be in accordance with the requirements of this specification. The maximum amount of stands shall remain in place during mating operations. All areas on the stand that are positioned next to the aircraft shall be padded. Padded areas (bumpers) shall be a minimum of four (4) inches thick and cover the entire width of the deck sections and shall not allow any stand structure to come in contact with the surface of the aircraft. In addition, bumpers shall be of a contrasting color (yellow) to the deck sections and constructed of a durable, compressible material. Bumpers shall be easily replaceable.

3.2 Chassis/Frame

The chassis/frame of the C-130 ISO Stand shall be constructed of corrosion resistant materials or treated to provide corrosion protection. The size and weight of the frame shall be as small and as light as practical, consistent with meeting the performance requirements of this specification. The frame shall support, at a minimum, 1000 lbs working load. Each section shall have at least a four wheel design.

3.3 Adjustable Deck Sections

Adjustable deck sections shall be a permanent part of the maintenance stand and shall have a positive locking mechanism to allow for proper aircraft interface.

Adjustable decking shall cover all openings that are specified and shall allow proper stand to aircraft interface. Time required to adjust any deck section from fully retracted to fully extended shall be no more than 10 seconds. A bearing support extension system shall not be utilized. Each adjustable deck section shall be capable of being operated by no more than two persons without posing a tripping hazard. The force required to extend the adjustable deck section shall not exceed the requirements of MIL-STD-1472.

3.4 Identification Plate

An identification plate, permanently marked, shall be securely attached to each stand within the C-130 ISO assembly in readily accessible locations. The identification plate shall be in accordance with the latest revision (at the time of contract signing) of MIL-STD-130 and contain the following information:

• Nomenclature

• Tech Order Number (identification plate)

• Manufacturer’s Part Number

• Serial Number

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• Manufacturer’s Name and Cage Code

• Date of Manufacture

• Contract Number

• National Stock Number

• Assigned Stand Number within the entire ISO Set

• Technical Order (TO) Number

• Load rating

• Weight per stand

Six (6) blank lines shall be added after the above information for the purpose of etching future Time Compliance Technical Orders (TCTO).

3.5 Non-Corrosion Enclosure/Materials

The C-130 ISO Stand material design is required to reduce the extensive man-hours and costs expended resolving corrosion-related issues (i.e. rust, fungus, mildew, pitting, etc). Wherever practical, dissimilar metals shall not be used in direct contact with each other. Where such conditions cannot be avoided, suitable protection against galvanic corrosion shall be provided.

3.6 Fire Prevention, Safety, and Design & Construction Practices

The danger to personnel from fire and explosion shall be avoided by separation of hazardous substances from heat sources, suitable vents and drains, and other fire prevention measures. All fastening devices and other parts which may cause hazardous conditions shall be secured or shall have other approved locking means applied. The use of safety wire as a securing method is not permitted.

The C-130 ISO Stand shall conform to all applicable sections and paragraphs of OSHA 29 CFR 1910 and AFOSH 91-501 standards. The contractor shall be solely responsible for ensuring that the C-130 ISO Stand meets all applicable OSHA and AFOSH Standards as they apply to aircraft maintenance stands. The C-130 ISO Stand shall successfully pass an OSHA and AFOSH Inspection Walk down during the First Production Unit Testing. Failure to meet any applicable OSHA or AFOSH Standard, whether listed or unlisted in the contract documents, is a failure to meet the basic requirements of the contract.

3.7 Mobility

Each stand that makes up the ISO stand shall be mobile to allow that section to be independent of other stands. All stands shall have secured locking devices to keep adjacent stands from separating when in use. Unless otherwise stated, all wing, engine, prop and tail stands shall be configured to provide a continuous

Ground Support Equipment Branch Page 5 of 22 walking surface with no steps. The time for any sectional stand to be connected or disconnected from other stands and removed shall be no longer than 1 minute with 4 people. The time to position entire stand into place around aircraft shall be no longer than 1 hour with 6 people. Each section shall be capable of being maneuvered by four (4) female (5th percentile) persons. The force required to move each section shall not exceed the requirements of MIL-STD-1472, and associated tables, Paragraph 5.9.11.4.1 (high traction).

3.7.1 Mobility Concept

The stands shall be capable of being assembled and disassembled to allow for transport or shipping on a flat bed truck.

3.8 Welds and Welding

All welding on the C-130 ISO Stand shall be completed per American Welding Standard (AWS) D1.1 or D1.2. Welds shall be inspected to ensure proper penetration and verified to be free from weld defects including but not limited to, cracks, undercut, and porosity. Inspection shall be completed by an AWS Certified Weld Inspector during and after the construction of all stands.

Contractor shall make available to the Government certifications for all welders being utilized on the C-130 ISO Stand. Welding procedures shall be in accordance with AWS D1.1 or D1.2, and copies shall be provided to the Government prior to start of construction.

3.9 Functional Characteristics

3.9.1 Vertical Actuator: Actuators shall be manually driven and capable of at least two (2) feet of adjustment for all stands. The starting height for the fuselage and tail stands shall be 93 inches. The wing and engine stands shall follow the contour of the wing within 6 inches.

3.9.2 Casters: Casters shall be steerable. They also shall be lockable and durable.

Casters shall be at least 10” in diameter to withstand operation over inclines, storm drains, grounding points or hangar door tracks without causing damage to the caster or stand. Pneumatic tires are unacceptable. Casters must mobilize stands freely inside the hangar without the use of ramps or pry bars. Casters shall have non-skid tread on them and shall have a safety factor of at least 4. Casters shall utilize sealed lubrication bearings.

3.9.3 Electrical Power: Electrical power shall be 120v, 1 phase, 60Hz. Electrical components shall be solid state and commercial off the shelf where possible for electrical plugs, connectors, and receptacles. The lighting circuit shall be

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277/480v, 3 phase, 60 Hz, and 30 Amps. The service circuit shall be 120/208v, 3 phase, 60 Amps. Electrical outlets shall accompany light fixtures. Wherever possible, electrical and air receptacles shall be located beside each other.

Electrical connections shall be available from the trailing edge stands, the fuselage/engine stands and underneath where the main landing gear is located.

The electrical system shall comply with NFPA 70, National Electric Code.

Separated stands shall not effect the basic electrical configuration.

3.9.4 Lighting: Lighting shall be provided on the C-130 ISO Stand for maintenance and inspection operations. Lighting shall be located on the perimeter of the stand and offer the greatest color rendition and illumination possible utilizing the minimal number of fixtures for the application. The lighting shall illuminate the entire engine area (both sides of each engine), the entire underside of the wing trailing edge area, and the main landing gear area. There shall be a control panel for the lights on either side of the airframe and it shall be located on the stand that interfaces with the fuselage underneath the wing. The control panel shall be equipped with 2 receptacles to receive power. One receptacle extends to the front side of the stand and the other extending to the back side of the stand. Separated stands shall not effect basic lighting configuration. Lighting shall not pose a tripping hazard to maintenance personnel.

3.9.5 Air System/Connections: Quick disconnect sockets shall be provided to accommodate all male quick disconnects and capable of supplying regulated air pressure up to 150 psi @ 250 CFM. Wherever possible, electrical and air receptacles shall be located beside each other. Air connection shall be available from every stand and underneath where the main landing gear is located. Air shall be available from two entry points one on each side. Separated stands shall not effect the basic air configuration.

3.9.6 Fall Protection/Railing: Handrails shall comply with all OSHA/AFOSH regulations. The perimeter of stand shall have no chains. All perimeter railing shall be operated by one person and shall be at least 42 inches. When any stand is removed, all of the adjacent stands shall be able to accommodate railings. The railings shall not have any “play” in them. All perimeter railing shall be able to be removed to allow stairs to interface with stands. All rails that can be removed shall have a positive locking mechanism that does not require a tool to be used to disengage the rail from the stand.

3.9.7 Stairs: Three (3) sets of stairs shall be provided on each side of the aircraft. The stairs shall be OSHA/AFOSH compliant regardless of the height of the stand platform. The stairs shall be able to be located anywhere on the perimeter of the stand. The stairs shall be four (4) feet in width. Stairs shall incorporate an anti-skid (non-slip) surface which is self cleaning. An additional set of stairs shall be

Ground Support Equipment Branch Page 7 of 22 provided with each tail stand. One set of stair stands shall be a two tier design to allow access to the stand platform and the top of wing. The over wing bridge retraction system shall be operable by one person.

3.9.8 Deck Surface: All decking surfaces shall be solid, anti-skid and resistant to jet fuel, aircraft hydraulic fluid, and cleaning and degreasing solvents. Anti-skid surfaces shall prevent slipping and allow maintainers to kneel, crouch, and lie down without causing minor injuries such as abrasions during aircraft maintenance. OSHA/AFOSH kick-plates shall be provided around perimeter of the stand and can be installed on any stand when the adjacent stand has been removed. Decking shall follow the slope of the aircraft wing without utilizing steps and shall also be continuous.

3.9.9 Jack Access: Jack access shall cover all jack areas described in attachment labeled “jack access locations”. Jack access shall be a 2.5’ by 2.5’ opening with the center of each jack location. Adjustable decking shall eliminate any open area whether jacks are present or not. Wing jacks shall be utilized on the pad at the two locations of each prescribed wing stations. The substructure of the stands shall accommodate jacks so that the legs can rotate 360 degrees.

3.9.10 Working Load: Platform fatigue in the form of “oil canning” is unacceptable. Each stand within the C-130 ISO Stand set shall safely hold four

(4) times the design operating load. Stand platforms shall be designed for medium duty use and a minimum of 40 lb. per square foot loading criteria.

Toolbox areas must meet a Medium duty (50 pounds per square foot) application.

3.9.11 Service Life: The C-130 ISO Stand shall be designed for a minimum service life of 20 years.

3.9.12 Substructure: The substructure of all stands shall be designed to allow the maximum amount of area for workers to move equipment around and to allow fire suppression systems to operate correctly. Some of the equipment that shall be used underneath stands is as follows:

6’ wheel and tire dolly 6’ X 3’ X 6’ panel dolly External fuel tank dolly AC Pack dolly APU dolly Fuel and oil bowsers

There also needs to be enough area in the substructure to allow the ALL TV Molt to be removed. Its dimension is 168” long X 59” wide X 60” high.

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3.10 Specific Aircraft Areas:

3.10.1 Inboard & Outboard Propeller Area These stands shall access inboard and outboard propeller areas. The stands shall allow access to the crew entry door with a stair step. The stands shall allow the prop to rotate while the stand is in the maintenance position. Spacing shall be wide enough to allow the prop to rotate in feathered or un-feathered positions with additional spacing on either side of the props for all C-130 models. Adjustable decking shall allow any unoccupied spacing to be covered in the prop area. The stands shall have a 4 foot distance from the prop dome to the front edge of the stands. The stands shall be rated so that the stand can accommodate an 800 pound toolbox anywhere in front of the prop area. The stands shall be designed so that the inboard or the outboard engine can be removed without affecting maintenance being performed on other the engine. These stands shall be designed to allow an OSHA/AFOSH compliant walkway between the outboard propeller and the side edge of stand.

3.10.2 Fuselage Area These stands shall access the inner engine and fuselage areas.

Non-marking bumper pads shall be located on any surface that may come in contact with surface adjacent to the aircraft. The length of these stands shall extend to aft of the paratrooper doors. The stands shall have a one (1) foot cut-out to allow the air deflector doors to open. The cut-out shall extend to the end of the stand. The substructure shall allow access to the main landing gear area. Any supporting beams around the main landing gear area shall be at least 40 inches from the end of the stand to allow personnel to perform maintenance tasks in that area. Sufficient room shall be available to allow the main landing gear door to be fully extended. The substructure of the stand shall accommodate the 3 guns on the left side of the AC-130 airframes as described in attachment labeled “gun locations”.

3.10.3 Engine Area These stands shall access the inner and outer engine area. The stands shall be designed to allow spacing underneath the engines. Adjustable decking shall cover spacing and also allow a two (2) foot wide drip pan to be installed underneath the engines. Sufficient room shall be available to allow fuel and oil bowsers to gain access underneath engines.

3.10.4 Wing Flap Area These stands shall access the flap area on the wings. The stands shall have an OSHA/AFOSH compliant walkway behind the flaps when the flaps are fully extended.

3.10.5 Center Wing Area These stands shall access the center area underneath the wing. Spacing shall be available for all jack accesses. Spacing shall be available to accommodate all external tanks. Adjustable decking shall cover any open area

Ground Support Equipment Branch Page 9 of 22 around wing jacks and external tanks, and also allow continuous walkway when jacks/tanks are not installed.

3.10.6 Wing Tip Area These stands shall provide access to the outer wing tip. The walkways around the leading and trailing edges shall be OSHA/AFOSH compliant. A two tier design shall be incorporated around the leading and trailing edges to allow maintenance personnel easy access to those areas and also provide fall protection from the wing. The stand shall not extend past the wing tip. The substructure of stand shall provide an OSHA/AFOSH complaint walkway underneath the wing tip.

3.10.7 Forward Fuselage Area These stands shall provide fall protection from top of fuselage and access to side windows on the front of the aircraft. The stand shall allow the nose radome to lift without moving stand away from aircraft and not interfere from gaining access to crew door when installed. Stand shall have non-marking bumper pads located on surface adjacent to aircraft. Shaped decking shall be used to contour to aircraft. Substructure shall allow nose jacks to interface with aircraft.

3.10.8 Aft Fuselage Area These stands shall serve for fall protection from the top of fuselage. Stands shall have two (2) foot sliders to eliminate the opening of flap area on the wings. The platform does not have to be accessible from other stands.

Non-marking rubber bumper pads shall be located on surfaces adjacent to the aircraft. The stand shall have sliders to interface with aircraft when the air deflector door is closed. Sliders shall be used to contour to the aircraft.

3.10.9 Horizontal Stabilizer Area These stands shall access the horizontal stabilizer area. Stands shall meet OSHA/AFOSH standards for fall protection and walkway outside tail sections. Stands shall provide access to the upper door hinge components and not interfere with ramp door operation and allow access in and out of the ramp door. Sliders shall cover jack access openings. The substructure of the stand shall accommodate jacks and the stand shall not exceed 2 feet past beaver tail on H-model aircraft.

3.11 Maintenance

Tools/Test Equipment: Commercial tooling shall be utilized on the C-130 ISO Stand wherever possible to enhance maintainability, decrease maintainer’s cost and reduce airlift requirements. In the event that standard commercial tooling cannot be used and specialized tooling requires the approval of procuring activity and upon approval, four (4) sets of special tool kits shall be provided for each ISO stand.

Metric tools are not considered special tools. The C-130 ISO Stand shall be field maintainable using a minimum number of common standard hand tools or other

Ground Support Equipment Branch Page 10 of 22 equipment. All major components shall be replaceable by field level maintenance technicians. All inspections shall be capable of being performed from a standing position.

Operability: All components shall be selected and located for maximum ease of operation, servicing, inspections, and maintenance. All operator controls and equipment shall be centrally located in an easily accessible and readily available location. Switches and gauges at the operational position shall be located for good visibility and operation from a standing position. In addition, the C-130 ISO Stand design shall allow the user to operate while wearing cold weather gear and/or all Mission Oriented Protective Posture (MOPP) ensembles.

Maintainability: Reducing the time required to access component parts for inspection maintenance enhances maintainability. The C-130 ISO Stand shall be capable of being visually inspected and serviced without removing panels or components. This shall include the incorporation of access doors or removable enclosures and modular design of sub-systems and components. Major components shall be replaceable by field personnel. Maximum use of quick disconnect connections shall be used to allow for rapid removal/replacement of component parts. Electrical systems shall be protected by circuit breaker(s) in lieu of fuses. Enclosure/chassis material shall be field repairable. The maximum total downtime to perform all daily scheduled maintenance and servicing tasks shall be no greater than thirty (30) minutes for the ISO stand. Routine servicing tasks and inspection prior to use shall not require hand tools. Drain plugs and filters shall be directly accessible and oriented to have unimpeded drainage to catch pans. Maximum use of sealed lifetime lubrication bearings is required.

Maintenance Concept: Field Level repair shall support the current Air Force support structure. The C-130 ISO Stand design shall not require removal of other major components to access and replace failed subassemblies. The field shall be capable of repairing 80% of repairable parts. Stand design shall facilitate scheduled maintenance at an interval of not less than six (6) months and shall occur annually.

Reliability: The contractor shall establish, conduct, and maintain a comprehensive reliability program. Guidance is described in MIL-HDBK-781A, section 4.6, Failure Reporting, Analysis, and Corrective Action System (FRACAS). The Threshold Mean Cycle Between Preventative Maintenance (MTBPM) shall be based on 125 cycles at an 80% confidence level. The MCBPM is defined as the total number of cycles performed divided by the total number of preventative maintenance actions. An operation cycle is defined as for the following items:

• Adjustable decking fully extend and fully retract

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• Vertical actuators fully extend and fully retract

• Railing Remove and install

3.12 Environmental Compliance

Hazardous Materials: The C-130 ISO Stand design shall minimize the use of hazardous materials. The use of Ozone Depleting Chemicals (ODCs) and the hazardous materials established by the EPA listing is prohibited from use in any operation, maintenance, repair overhaul, and/or troubleshooting action required of the Government by any C-130 ISO Stand technical order of any kind, whether it be a commercial or Government format.

No technical manual shall contain any of the prohibited materials for either use or information. Toxic products and formulations used or generated by the C-130 ISO Stand shall meet the requirements of AFOSH STD 48-8 and all other applicable environmental, occupational safety and health standards. Personnel shall not be exposed to unsafe amounts of chemicals or other health and safety threatening agents in producing, using, maintaining, storing, disposing, or servicing of the C-130 ISO Stand or its components.

3.13 Corrosion Prevention

Materials used in the construction/design of the C-130 ISO Stand shall be corrosion resistant. Guidance for corrosion prevention and control for the C-130 ISO Stand may be found in MIL-HDBK-808.

3.14 Familiarization

Maximum use of exportable courses is required (i.e., DVD video, computer disc, etc.). Courses shall provide training on servicing, operational checks, theory of operation, adjustment procedures, troubleshooting, and associated diagrams. Two sets of courses shall be delivered to each location with production hardware.

Hands on classroom familiarization shall be presented by the contractor at Youngstown addressing theory of operation, troubleshooting and unique maintenance tasks as required for a seamless full-system integration.

3.15 Painted Color

The C-130 ISO Stand paint shall comply with FED-STD-595, semi-gloss gray, color 26173. Chemical Agent Resistant Coating (CARC) shall not be used. The C-130 ISO Stand shall comply with T.O. 35-1-3 (Corrosion Prevention, Painting, and Marking of USAF Support Equipment). Markings shall be one (1) inch high block letters/numbers unless prohibited by available space. In such cases, the

Ground Support Equipment Branch Page 12 of 22 markings shall be the largest practical size consistent with good appearance and visibility, but shall not be less than one-half (1/2) inch high. Colors used shall be in accordance with the following table.

APPLICATION FED-STD-595 COLOR

Exterior Finish 26173 Semi-gloss Gray Markings, Informational/Caution 37038 Lusterless Black

Markings, Warning/Danger and Adjustable Deck Sections 31136 Lusterless Red

3.16 General Inspections

Inspections will be IAW AFOSH regulations

4.0 PRODUCT CONFORMANCE PROVISIONS

4.1 Responsibility for inspection

The contractor is responsible for the performance of all inspection/test requirements unless otherwise specified to verify compliance with this performance description. Except as otherwise specified in the contract, the contractor may use his own or any other facilities suitable for the performance of the inspection requirements specified herein, unless disapproved by the Government. The Government reserves the right to perform any of the inspections set forth in the performance description where such inspections are deemed necessary to assure supplies and services conform to prescribed requirements.

4.2 Sub-Contracted tests

A copy of all sub-contracted test reports and/or data shall be provided to the Robins ALC engineer. In the event of a disagreement on the analysis of test data, the Robins ALC engineer shall be responsible for the final interpretation/decision.

4.3 Responsibility for compliance

All items must meet all requirements of sections 3, 4, and 5 of this performance description or the technical proposal whichever is greater. The contractor’s overall inspection system or quality program shall include as a minimum the areas

Ground Support Equipment Branch Page 13 of 22 set forth in this performance description. The absence of any inspection requirements in this performance description shall not relieve the contractor of the responsibility of assuring that all products or supplies submitted to the Government for acceptance comply with all requirements of the contract.

Sampling in quality conformance does not authorize submission of known defective material, either indicated or actual, nor does it commit the Government to acceptance of defective material.

4.3.1 Developmental Test and Evaluation (DT&E).

DT&E Tests are required to be accomplished by the contractor after award of the contract but prior to submission of the first production unit to the Government for user testing.

4.3.2 User Testing (OT&E).

User OT&E Tests shall be performed on the first production unit by the Government.

4.3.3 Production Inspection

Production Inspection Test is required for acceptance of the production units.

4.3.4 Test Sample

A first production unit shall be subjected to tests that shall show degree of compliance with Section 3. Tests shall be conducted at prevailing ambient temperatures and utilizing all components and appropriate accessories in place, unless otherwise specified herein. Certification of all tests shall be provided to the Government. Contractor format is acceptable.

4.3.5 Test Rejection/Failure Criteria

Unless otherwise stated, the following shall be cause for rejection:

• Failure to conform to design or performance requirements specified herein.

• Structural failure of any component, including permanent deformation, or evidence of impending failure.

• Evidence of excessive wear.

• Interference between stand components or between the stand, the ground, and all required obstacles, with the exception of normal contact by the tires.

• Misalignment of components.

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• Conditions which present a safety hazard to personnel during operation, service, or maintenance.

4.3.6 Reliability and Maintainability Information

The following information shall be included as an appendix to the test report:

• All failures, servicing, adjustments, maintenance, and irregular functioning shall be identified by accumulated operating time, cycles, miles, or position in the test procedure, as appropriate. Test conditions at the time of the events identified shall be recorded.

• A summary of the engineering analysis and of any tests conducted to determine assignable causes for any failure or irregular functioning.

• A summary of the engineering analysis leading to any corrections made to design, construction, quality control, or other procedures, or leading to any corrections to be made or proposed to be made to production items. The summary shall also include an analysis of the predicted effectiveness of such corrections.

• Clock time and person-hours required for each maintenance and servicing action taken during the tests. A brief description of the experience and qualifications of the personnel taking such actions.

• Test activity or contractor comments on item features or requirements that, if modified, should improve the item.

• Test activity or contractor comments on use or maintenance conditions to be avoided or cultivated to increase the reliability or useful life of the item.

• Any of the above information that is already included in the test report body need not be repeated in the information required by the paragraph, but clear reference to the location of the data shall be included.

4.4 DT&E

The contractor is responsible for the areas set forth below prior to shipping the first production unit to the Government. Testing set forth herein shall be witnessed by the Government QAR at the contractor’s facility or test site. The

Ground Support Equipment Branch Page 15 of 22 contractor is responsible to provide certification of testing and test results to the contracting officer concurrent with the submission of the first production unit.

Visual damage inspection and acceptance will be accomplished at destination.

Contractor format for submission of test results is acceptable.

4.4.1 Examination of Product

The C-130 ISO Stand unit shall be inspected to determine compliance with the requirements specified herein with respect to parts, tightness of fittings, screws, bolts, workmanship, finish, materials, color, marking, safety, and identification and instruction plates. Specific areas are, but not limited to: identification plate (3.4), non-corrosion materials (3.5), fire prevention, safety, and design & construction practices (3.6), casters (3.9.2), deck surface (3.9.8), tools (3.11), painted color (3.15), and number of stairs (3.9.7)

4.4.2 Welds and Welding

All welds shall be inspected by an American Welding Society (AWS) Certified Weld Inspector (CWI) as detailed in section 3.8 of this document.

4.4.3 Adjustable Deck Sections

The adjustable deck sections shall operate in accordance with paragraph 3.3 of this document. All requirements of paragraph 3.3 shall be met.

4.4.4 Stairs

The stairs shall able to accommodate personnel at any stand height. Each set of stairs shall be positioned in no less than 3 different positions. The over wing bridge retraction system shall be operable by one person.

4.4.5 Maneuverability Tests

The largest and/or the heaviest stands section shall be maneuvered by 4 persons in accordance with paragraph 3.7. Any failure of these tests shall be cause for rejection.

4.4.6 Rolling Force/Rolling Resistance Test

The C-130 ISO Stand unit shall be moved from a resting position on a semi-smooth surface (paved surface) with a force no greater than the specified limitations in MIL-STD-1472. Any failure of these tests shall be cause for

4.4.7 Platform Load Test

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One sectional stand within the C-130 ISO Stand set shall be loaded to four (4) times its maximum load capacity. Upon completion of this test, no plastic deformation shall have occurred. Any failure of these tests shall be cause for

4.4.8 Sectional Stand Test

All sectional stands shall be connected/disconnected to ensure the 1 minute requirement with 4 people.

4.4.9 System Tests

The electrical system (3.9.3) and pneumatic system (3.9.5) shall be tested as complete systems. Any failure resulting from these tests shall be cause for

4.4.10 Electrical System and Controls

The electrical system shall provide sufficient power to operate all electrical components outlined in this document. Each stand receptacle shall be tested to ensure proper operation and power output. Lighting fixtures shall also be tested to ensure proper operation and illumination. Controls within the control panel shall operate properly and perform the required function to which each has been assigned.

4.4.11 Pneumatic System

The pneumatic system shall provide pressure and flow rate in accordance with paragraph 3.9.5 of this document. All pneumatic connections shall be tested to ensure compliance with this document.

4.4.12 Vertical Actuator

Tests shall ensure that actuators shall be manually driven and capable of at least two (2) feet of adjustment for all stands.

4.4.13 Reliability Test

The C-130 ISO Stand shall be tested to and shall comply with the requirements specified in paragraph 3.11. Acceptance can occur only at discrete times, while rejection can occur at any time after 3 failures has occurred. At the end of the test, all items shall parts shall be inspected to verify that there is no deformation.

MCBPM 125 @ 80% Confidence level

Number of Acceptance

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Failures Cycles 0 349 1 450 2 552

4.5 OT&E

After all other tests specified herein have been successfully performed, the C-130 ISO Stand shall be tested on the C-130 Aircraft at Youngstown MAP Ohio Air Force Reserve Air Base. The operational test shall consist of the full mating of the C-130 ISO Stand set to the C-130 Aircraft. The inability of the C-130 ISO Stand to satisfactorily meet any requirement specified in paragraph 3.10.1 –

3.10.9 shall be cause for rejection. After the stands have been assembled, the timeline for this test is 60 days. Below are the following tests:

4.5.1 Interface Test

All sectional stands shall be positioned together around aircraft. The set-up time shall be no longer than 1 hour with 6 people. All stands shall be inspected to confirm that stands will interface with airframe.

4.5.2 Substructure

The following equipment shall be used to demonstrate that substructure will not interfere with normal operation:

6’ wheel and tire dolly 6’ X 3’ X 6’ panel dolly External fuel tank dolly AC Pack dolly APU dolly Fuel and oil bowsers Simulate the ALL TV Molt by confirming a 168” long X 59” wide X 60” high substance can be maneuvered in the substructure.

All jacks

4.5.3 Starting heights

The starting height for the fuselage and tail stands shall be 93 inches. The wing and engine stands shall follow the contour of the wing within 6 inches.

4.5.4 Production tests

The contractor is responsible for maintaining an approved quality and inspection system. Each ISO stand shall be subjected to the same tests as the first production

Ground Support Equipment Branch Page 18 of 22 test on the following areas: examination of product, welds and welding, adjustable deck sections, stairs, sectional stand test, system tests (both electrical and pneumatic), and interface test in accordance with paragraph 3.10.1 – 3.10.9.

These tests shall be done at each stand destination.

5.0 DOCUMENTATION

5.1 Warranty and Service Information

The manufacturer shall include, with each unit delivered, a document indicating the warranty and service agreement provided and the telephone numbers, addresses, electronic mail addresses and the points of contact for warranty issues, technical assistance and routine and emergency service.

5.2 Installation and Operation

The manufacturer shall supply all manuals such as operating instructions, parts lists, diagrams, and any other data pertinent to the operation of the unit.

Manufacturer will required to assemble each production at various locations within the Continental United States (CONUS).

5.3 Technical Data

5.4.1 Engineering Calculations

The contractor shall complete all supporting engineering calculations for the design development and execution phases of this program. All supporting engineering calculations, both formal and informal, shall be provided to the Government. These calculations include, but are not limited to, load bearing calculations, static and dynamic stress analysis, finite element analysis, electrical load calculations, equipment sizing calculations, hydraulic calculations, and wire sizing calculations. All engineering calculations that are utilized for any portion of the design development of the C-130 ISO stands shall be submitted to the Government.

Structural calculations and analysis including load bearing calculations, static and dynamic stress analysis, finite element analysis, electrical load calculations, and calculations for pressurized systems (pneumatic and hydraulic) shall be formal calculations with statements of purpose, methods, assumptions, analysis, and conclusions clearly defined and presented. All calculations associated with the design of the C-130 ISO stand shall be stamped by a registered Professional Engineer (PE) in the respective engineering discipline of the particular portion of the design being developed. Structural engineering calculations shall be stamped

Ground Support Equipment Branch Page 19 of 22 by a registered Structural Engineer or a registered Mechanical Engineer with appropriate background. All Professional Engineers shall have an active and current license throughout the entire design and production phases of this program.

6.0 NOTES

6.1 Travel

The contractor shall arrange and execute all travel necessary for the performance of the requirements of this purchase description.

6.2 Installation Locations for Fielding Stands

Locations shall be provided in the RFP submittal.