AIRCRAFT LIFTING SYSTEMS FOR CRASH DAMAGE OR DISABLED AIRCRAFT RECOVERY.pdf

AIRCRAFT LIFTING SYSTEMS FOR CRASH DAMAGE OR DISABLED AIRCRAFT

RECOVERY (CDDAR)

8.10.2026

INTRODUCTION & BACKGROUND

The Crash Damage or Disabled Aircraft Recovery (CDDAR) program is expanding in scope as the Department of War’s aircraft �leet, mission tempo, and global operational demands continue to increase. Modern airframes present complex recovery challenges, making it essential for units to have reliable, standardized equipment capable of safely lifting and recovering disabled aircraft without causing additional structural damage. To support this growing mission, the Volk Field CRTC is seeking to procure an equipment package aligned with current Air Force CDDAR standards, ensuring consistency with established capabilities already in use across the force. Procuring the required pneumatic air bag lifting stations and fuselage lifting systems is critical to strengthening this enterprise-wide capability, enhancing interoperability, and enabling safe, ef�icient aircraft recovery operations throughout the Department of War.

This Requirements Document establishes the technical, performance, and delivery requirements for procuring two critical aircraft recovery systems:

1. 15-Ton Pneumatic Aircraft Lifting Air Bag Stations - Part Number: 9314-010 (Model

9314-010) NSN: 5120-01-284-2611.

2. Control Console – Part Number: 9316-010 (Control Console for Model 9314-010)

3. Fuselage Lifting System for Narrow- and Wide-Body Aircraft

***All items must be in accordance with speci�ications listed below.

These systems are essential to Crash Damage or Disabled Aircraft Recovery (CDDAR) operations, enabling safe, controlled lifting of disabled aircraft while preventing secondary airframe damage.

Their use ensures rapid aircraft recovery, supports operational readiness, and enables timely runway clearance.

SCOPE OF REQUIREMENT

The Contractor shall furnish all equipment, components, accessories, documentation, and certi�ications necessary to provide a complete aircraft lifting capability consisting of:

A. Pneumatic Aircraft Lifting Air Bag System - A Model 9314-010 Pneumatic Aircraft Lifting Air Bag Station manufactured by AGE Logistics Corporation. The system shall utilize independent, modular pneumatic elements capable of stacking up to �ive (5) modules high, providing high lateral stability and low-pressure lift distribution beneath certi�ied aircraft lift points. Part Number 9314-101. NSN: 5120-01-284-2611.

B. Control Console Aircraft Lifting Airbags – The Control Console works in conjunction with aircraft lifting bags, Models 9314-010 (15-ton capacity) and 9315-010 (26 -ton capacity) to direct the supply of air to each individual air bag element. Individual control valves located on top of the console, with their corresponding pressure gauges, allow the operator to monitor and control the internal pressure and lift of each element. A system pressure regulator maintains 15 psi internal pressure throughout the console. Legs fold for ease of handling and storage. Part Number 9316-010.

C. Fuselage Lifting System - A complete fuselage lifting system. The system MUST meet Aircraft Recovery Manual / Aircraft Recovery Document (ARM/ARD) standards and IATA recommendations, employing custom load-distribution methods to prevent secondary structural damage during lifting operations.

TECHNICAL & PERFORMANCE REQUIREMENTS

1. PNEUMATIC AIR BAG SYSTEM SPECIFICATIONS

A. Capacity & Dimensions

• Rated Capacity: 15 tons (74,000 lbs.)

• De�lated Footprint: 90 in. x 90 in.

• Operating Pressure: 7 PSI

• Relief Valve Setting: 8–10 PSI (automatic venting required)

• Net Weight: 990 lbs.

• Gross Shipping Weight: 1,569 lbs.

• Crated Dimensions: 105" L x 53" W x 35" H

B. Modular Lift Heights

MODULES COLLAPSED HEIGHT MAX LIFT HEIGHT

1 2.28 in (58 mm) 24 in (610 mm) 2 4.56 in (116 mm) 48 in (1,219 mm) 3 6.84 in (174 mm) 72 in (1,829 mm) 4 9.12 in (232 mm) 96 in (2,438 mm) 5 11.40 in (290 mm) 120 in (3,048 mm)

2. Control Console Aircraft Lifting Airbags

A. Technical Description

• Inlet Pressure Max: 125 PSI (8.62 bars)

• Operating Pressure: 15 PSI (1.04bars)

• Relief Valve Pressure: 17 PSI (1.18 bars)

• Proof Pressure: 50 PSI (3.45 bars)

• Outlet Pressure: 7 PSI (0.49 bars)

• Net Weight: 150 LBS (68kg)

• Console Dimensions: 68.25 (l) x 31.5 (w) x 49 (h) in. (1,734 x 800 x 1245mm)

• Crated Weight: 300 LBS (136kg)

• Crate Dimensions: 72 (l) x 34 (w) x 57 (h) in. (1,829 x 864 x 1448mm)

B. Must Mate with Models 9314-010 (15-Ton) and Model 9315-010 (26-Ton) Aircraft

Lifting Bags.

3. FUSELAGE LIFTING SYSTEM REQUIREMENTS

C. Aircraft Compatibility - System must support:

• Military: KC-46, C-130, KC-135, E-3, P-8A, �ighter aircraft single-point lifts

• Commercial Wide-Body: B767, MD-11, DC-10, A330, A340

• Commercial Narrow-Body & Regional: B737, B757, B707, B727, A318–A321, MD-80 series, Embraer, Bombardier, regional turboprops, business jets

D. Sling & Rigging Requirements

• Fixed Pitch Sling Technology ensuring precise frame alignment

• Sling Inventory:

o (1) 4-band �ixed pitch sling o (3) Narrow-body slings o (1) Wide-body sling (A300/A310 compatible)

• Spreader Beams:

o (1) 50-tonne beam o (2) 24-tonne beams

• Rigging Con�igurations:

o Single, dual, triple, quad sling o 1-over-2 spreader beam con�iguration for �ighter/light aircraft

E. Design, Safety & Transportability

• Max weight of any single component: ≤ 300 lbs.

• System must be air-transportable and rapidly deployable

• Minimum safety factors:

o Spreader Beams: 2:1 o Slings: 7:1

SYSTEM COMPONENTS & DELIVERABLES

1. PNEUMATIC AIR BAG STATION DELIVERABLES - Each station MUST include:

A. Modular Lifting Bags:

o 4 stations, 5 bags per station (20 total) o Heavy-duty Velcro top/bottom patches for anti-shift stability

B. Pneumatic Supply Hoses:

o 60 hoses, 50 ft each

C. Protective Pads:

o 16 heavy-duty pads

D. Repair Kits:

o 4 rapid-cure �ield repair kits

E. Manifold & Control Consoles:

o 4 multi-valve consoles with quick-release couplers and individual pressure gauges

2. FUSELAGE LIFTING SYSTEM DELIVERABLES

• Three (3) stackable steel stillages for storage and transport

• One (1) sling storage crate (wood, protective)

• Certi�ied test certi�icates for all lifting components

• CE marking for the complete system

QUALITY ASSURANCE & COMPLIANCE

The Contractor shall ensure:

• Compatibility with Technical Order 35D5-5-9-1 and 35DA4-15-1

• All air bag elements include automatic relief valves set to 8–10 PSI

• All fuselage slings meet airframe manufacturer requirements and include bespoke lengths for proper load distribution

Anti-terrorism/ Operations Security/ Information Protection Information

1. Access and General Protection/Security Policy and Procedures. This standard language is for contractor employees with an area of performance within Government controlled installation, facility, or area. The contractor shall comply with all applicable installation/facility access and local security policies and procedures, which may be obtained from the Contracting Of�icer’s Representative (COR). The contractor shall also provide all information required for background checks to meet installation access requirements to be accomplished by the local installation’s Security Forces, Director of Emergency Services or local Security Of�ice. The contractor shall ensure compliance with all personal identity veri�ication requirements as directed by DoD, HAF and/or local policy. Should the Force Protection Condition (FPCON) change, the Government may require changes in contractor security matters or processes.

2. For Contractors that do not require CAC but require access to a DoD Facility and/or Installation.

Contractor and all associated sub-contractors employees shall comply with adjudication standards and procedures using the National Crime Information Center Interstate Identi�ication Index (NCIC-III) and Terrorist Screening Database (TSDB) (DODIO 2000.16V1_DAFI 31-145, DAFI 31-101 and DODM 5200.08v3_DAFMAN 31-101v3), applicable installation, facility and area commander installation/facility access and local security policies and procedures (provided by government representative), or, at OCONUS locations, in accordance with status of forces agreements and other theater regulations.

3. For Contractors Authorized to Accompany the Force. DFARS Clause 252.225-7040, Contractor

Personnel Authorized to Accompany U.S. Armed Forces Deployed Outside the United States. The clause shall be used in solicitations and contracts that authorize contractor personnel to accompany US Armed Forces deployed outside the US in contingency operations; humanitarian or peacekeeping operations; or other military operations or exercises, when designated by the combatant commander. The clause discusses the following AT/OPSEC related topics: required compliance with laws and regulations, pre-deployment requirements, required training (per combatant command guidance), and personnel data required.