Aircraft GSE and MRO

The AGSE-D160 C130 dock system is designed to provide personnel access to service the aircraft wings, AFT fuselage, and horizontal and vertical tail components. The dock system consists of interlocking elevated platform sections as well as specialized support equipment designed to compliment the platforms. There are three basic platform components; a fixed tail mezzanine, mobile multi-sectional wing stands and AFT fuselage access ramps that allow access between the tail mezzanine and wing stands. Specialized support equipment includes mobile and fixed tool lifts, a rolling sloping longeron stand and deck-mounted wing cradles.
The fixed single deck tail mezzanine structure provides the basis for situating the aircraft and wing stands within the hangar. An access stair and tool lift is provided at the rear corner of the mezzanine deck. The mezzanine deck is reinforced in key locations to allow tail jack placement and use on the deck. The deck is designed to support the repair of a detached Horizontal Stabilizer.
Aft fuselage access ramps provide access to the fuselage and connection between the mezzanine and wing stand. The ramp deck has a sloped transition to accommodate the elevation change between the mezzanine and inboard fuselage stand raised deck. Slider panels are provided along the inboard edge to conform to the fuselage contour. The ramps are caster mounted for precise positioning and relocation within the facility. A hinged deck section is located at the AFT end to allow the unit to be moved into location without requiring movement of other stand sections.
The wing dock system consists of six caster mounted mobile stands per side. Sliders at the inboard and outboard fuel pod locations allow pod removal and installation with the aircraft docked in stands. Slider panels are incorporated along the inboard edge of the inboard stands to provide a deck surface which conforms to the aircraft contour. An access stair and tool lift is provided along the trailing edge of the left and right wing stand set. Deck slider panels are provided at wing and engine jack shoring positions. Cover plates at each wing jack location conceal gaps between jack legs and sliders. Removable and adjustable handrail sections are provided along the perimeter of the assembled wing stands. All stands lock together at the inner corners using bolt or turnbuckle connections.
The mobile tool lifts are provided for convenience at the tail stand and wing stand locations. The wing stand tool lifts are mobile to allow roll-away in the event the wing stands are to be moved or additional aircraft or equipment clearances are required.
The Sloping Longeron stand allows technician access along the full length of the main cargo bay longerons during repair or replacement. It is specifically designed to collapse for a low profile such that it may be rolled under the tail mezzanine and into the cargo bay area. Once positioned along the edge of the cargo bay, it is hydraulically raised into position.
For each wing stand, a set of specially designed wing cradles is provided. These cradles are designed to quickly set-up and allow the detached outer wing to rest directly on the wing stand deck. The cradles are fitted with screw jacks and are manually height adjustable.

The AGSE-M046 Cargo Bay Access Stands are a single level structure providing access to the forward and aft cargo bays of B767 and B777 Aircraft. The deck height is adjustable and offers two preset deck heights (72 inches for B767 and 108 inches for B777). A fixed stairway provides access to the ground. The B777 height requires use of a portable stairway extension included with the stands. Electrical and air outlets are included with the stands.

The AGSE-V086-G01 pedestal assembly is designed to support the weight of a B747 aircraft. It requires eight main gear pedestal assemblies and one nose gear pedestal to fully support the weight of a B747.

The AGSE-D102 Tail Stand is a fixed height, caster mounted, one piece, multi-level stand that provides access to the tail of MD80/90 series aircraft. The first level is accessed from two stairways (located on either side). Level two is a suspended trolley mounted platform that traverses forward and aft. Access is provided by a single stairway from level 1, and a brake secures the level’s position. Two mechanically driven sliders protrude forward from the deck to provide access to the engine pylon. Level 3 is accessed from two fixed stairways (located on either side). The inboard edge has contour adjustable panels (sliders) that provide docking clearance. The sliders are mechanically driven in the rudder swing area. Two vertically adjustable finger decks (with sliders) provide access above the engines. The decks are adjusted using pendant controls that control the motor driven jackscrews. Level 4 is access from the ground using two stairways (located on either side). Sliders are provided on the inboard deck edge.

The AGSE-D002 Tail Dock is designed to service the tail sections of the Boeing 737 and 767 aircraft. The tail dock is vertically adjustable from a low position which services the B737 when on tires to a high position for servicing the B767 while stabilized on aircraft jacks. The AGSE-D002 Tail Dock is designed to service the tail sections of the Boeing 737 and 767 aircraft. The tail dock is vertically adjustable from a low position which services the B737 when on tires to a high position for servicing the B767 while stabilized on aircraft jacks. The tail dock is a split type crane rail mounted system which separates laterally to allow the aircraft to be positioned tail first into the hangar. Each half of the tail dock is composed of three main structures. The main framework is mounted on the crane wheels and provides the support and guides for the level 1 structure and the levels 2 through 5 structures. This design allows for minimal space restriction around the lower bulk cargo doors while still providing a stable system. The level 1 structure and the levels 2 through 5 structures have independent motorized vertical travel. The level 1 structure provides access to the aft cabin door and full coverage around the horizontal stabilizer and elevators. Slider deck panels are provided on the inboard edge of the platform to adjust the contour to fit snugly against the aircraft skin. The slider deck panels aft of the tail cone extend to the center line of the aircraft providing continuous access around the rear of the aircraft. The APU compartments of both aircraft may be accessed from the hangar floor by retracting the slider panels below the APU. Separate caster mounted platforms are provided for access to the leading and trailing edges of the horizontal tail. the platforms are sloped to match closely the angle of the horizontal tail. Wheel brakes are provided to secure the platforms in position. A double gate is provided along the outer board handrail to allow materials to be raised or lowered to or from the level 1 deck by means or fork lift.

Levels 2, 3, 4 and 5 are combined into a single structure and provide access to the vertical fin and rudder. Each level has slider deck panels provided on the inboard edge of the platforms which adjust to fit snugly against the vertical tail or to extend to the center line of the aircraft providing continuous access around the front or rear. Additional slider panel travel is made where required to allow for full rudder swing. All slider panels are fitted with non marking; Skydrol resistant, bright yellow bumpers to protect the aircraft. Telescoping handrails and gates are provided at the ends of the platforms to provide fall protections. All decking and slider panels are Aerodeck, skid resistant steel. All smooth decking is coated with a high profile non-skid coating.

The AGSE-D019 Tail Dock has four deck levels and provides access to the vertical and horizontal stabilizers of the aircraft. The inboard edges include sliders (with bumpers) to adjust to the aircraft contour. The forward edge has a bumper similar to the one on the individual sliders. The stand has electrically powered vertically adjustable legs and manually translates inboard/outboard on casters. An articulating stairway provides access from the ground. A series of steps provide access to the Aft Fuselage Access Stands. Two jib hoists on swinging booms are optional. The forward hoist services the aircraft aft cabin doors, while the aft hoist services the elevator assemblies.

The AGSE-M114 windshield access stand is designed to provide a work platform to service the B747 windshield. Two cantilevered extension decks supported by a fixed center section provide a continuous deck surface. The extension decks are horizontally adjustable to conform to the aircraft contour at a comfortable working elevation to the windshield. A ramp provides access and support of the work platform and is designed to raise and lower the platform to working and storage positions. Control of the air motor driven vertical travel is located on the upper tower platform to provide the operator with a clear view of the aircraft contour and work platform. A 250 lbs. capacity jib crane is provided for windshield removal and installation. The platform is designed for two working personnel with hand tools and one windshield section or 650 lbs. maximum.

The AM-2764 Inlet Cowl Dolly supports the General Electric GE90 and Pratt & Whitney PW4084 thru PW4098 Inlet Cowls used on Boeing B777 Aircraft. It is designed specifically for site installation/removal, and transport/stowage of inlet cowl. The dolly supports the inlet cowl by three points on the bottom, turnbuckles, and straps connected to GSE points on the cowl. The dolly is caster mounted with telescoping jacking legs. The dolly folds when empty and is suitable for shipment on the lower cargo compartment of wide body aircraft.

The dolly is supported by three caster assemblies. Each caster assembly offers a 3 inch wide by 12 inch diameter wheel for easy mobility and a weight capacity of 1,500 pounds each. Shock absorbing polyurethane tread wheels, position locks, and face brakes are standard.

The AM-2764 Dolly consists of a steel welded frame that folds when empty to minimize shipping volume. The inlet is supported by three firm rubber pads, and is secured by turnbuckles and straps connected to GSE points on the inlet.

 See

AM-2764-1200, INLET COWL DOLLY FOR GE90-115B