Aircraft GSE and MRO

Features:

• Licensed by Boeing Company to install/remove Pratt & Whitney engines when supported by commercial engine cradles

• Manual & powered bootstrap adapters included with system designed to accommodate several cradles (click on part number link below to find out more):

• Consists of parts consolidated from both manual & powered bootstrap systems (with duplicate parts omitted)

• Manual system components

• Configuration for DC10-30/-40 aircraft used with CF6-50 & JT9D-20/-59 engines also available (click on part number link to find out more): AGSE-B006

Mobility:

• Caster-mounted control panel intended for manual positioning around aircraft in hanger or flight line
• Not towable
• Lifting beams & associated hardware stored in plywood container
• Three (3) powered hoists with bootstrap adapters stored in individual containers with steel bases & fiberglass lids

Dimensions & Weight:

• Main Container (1): 89.0” (Length) x 17.0” (Height) x 32.5” (Width) / 2,000 LBS*
• Hoist Container (3): 34.0” (Length) x 48.0” (Height) x 32.0” (Width) / 400 LBS**
• Console (1): 36.0” (Length) x 51.0” (Height) x 30.0” (Width) / 750 LBS***

*Consists of forward & aft beam assemblies, lever hoists, hangers, wing pylon adapter, dynamometer, miscellaneous tools, wing aft balance & cable assembly
**Consists of steel base, cradle adapter, cable & pulleys, cover & hoist
***Consists of power cable, three (3) hoist cables & pendant control

Designed to provide access to the tail section of all series of DC-10 aircraft including the USAF KC-10 Tanker. The unit is compatible with all power bootstrap hoists for engine removal and does not require repositioning.
The stand's main characteristics:
1. MAIN DECK
The stand consists of a main deck with contoured forward cutout for the tail cone in the raised and open position. Sliders extend to close up the open doors.
2. ROLLING PLATFORM
When the tail cone is down, a track-mounted rolling platform covers deck cutout and provides an inspection and maintenance work area under the engine fan section. When tail cone is UP and aircraft patio doors are open, platform is rolled aft and stowed,
3. MOBILITY
Large diameter casters with brakes and swivel locks permit easy stand positioning, A tow bar is provided.
4. CONSTRUCTION
Bolted and welded structural steel tubing with non-skid Aerodeck stair treads and flooring. Handrails and toe plates are provided on all open sides. The design is in compliance with all OSHA codes.
5. SERVICE OUTLETS
Air and electrical outlets are standard on the main deck.
7. WEIGHT
Approximately 38,000 lbs. with Stelco lifts
Approximately 35,000 lbs. without Stelco lifts
8. DIMENSIONS
Width 24' 8-1/2"
Height 24' deck
Length 32'

Features:

• Licensed by The Boeing Company to support various engine inlets during installation/removal
• Folds to minimize empty shipping volume
• Can be shipped in lower cargo compartment of narrow body aircraft
• Inlet straps securely into place quickly and easily
• Leveling jacks are included to accommodate various engine heights

AM-1441-101 Configuration for following Aircraft / Engines:

• A300-600 / PW4000-94"
• B757 / RB211-535
• B767-200 / CF6-80A
• B767-300 / CF6-80A
• DC10-30 / CF6-6 & CF6-50
• L1011 / All Engines
• MD11 / All Engines
• B767AWACS / CF6-80C2

AM-1441-120 Configuration for following Aircraft / Engines:

• A300-600 / CF6-80C2
• A310 / All Engines
• B757 / PW2037 & PW2040
• B767-200 / CF6-80C2
• B767-200 / PW4000
• B767-300 / CF6-80C2
• B767-300 / PW4000-94"
• B767-300 / RB211-524H

AM-1441-123 Configuration for following Aircraft / Engines:

• A330 / CF6-80E1

Dimensions (Empty Dolly)*:

• Length: 92.0” (Folded) / 87.0” (Extended)
• Height (AM-1441-101): 38.0” (Folded) / 52.0” (Extended)
• Height (AM-1441-120): 38.0” (Folded) / 48.0” (Extended)
• Width: 22.0” (Folded) / 95.0” (Extended)
• Weight: 180 LBS

*All dimensions are with legs retracted.

One-level, adjustable height structure providing access to the windshield area of MD80 and MD90 Aircraft. The stand is used with the AGSE-D101 Nose/Fuselage Dock. The windshield stand rolls along the deck of the nose/fuselage dock on a “V” groove rail (right side of stand only). Each caster leg is adjustable, and bolts in 5 positions spaced 1-1/2 inches apart (6 inches total travel). Handrail is provided around the outside perimeter of the deck, and protective bumpers protect against inadvertent contact with aircraft nose. Two fixed stairways (left/right) provide access to the nose/fuselage dock.

Features:

• Used for towing/steering aircraft by attaching to nose landing gear (NLG) while pulled by tow tractor
• Primarily consists of cylindrical steel body

• Lunette eye at one end of towbar connects to tow tractor

• Mechanical head assembly at opposite end of towbar connects to aircraft NLG
• Towbar mounted on articulated undercarriage with hydraulic pump & retractable spring (to raise/lower towbar)

Configurations:

• 211030-1 attaches to B767 aircraft & includes extra shear pin as part of kit (212000-200)
• 211030-2 attaches to NLG from below for B767 aircraft & includes extra shear pin as part of kit (212000-200)
• 211030-100 with bearing protectors for axles, uses different hydraulic pump for B767 aircraft & includes extra shear pin as part of kit (212000-200)
• 211030-174 for C-17 GLOBEMASTER aircraft & includes extra shear pin as part of kit (211033-1)
• 211030-501 with different adapter head kit, shear pin kit & towbar assembly for C-17 GLOBEMASTER aircraft & includes extra shear pin as part of kit (211033-1)

Mobility:

• Maximum aircraft towing speed of 5 MPH (8 km/h)

Dimensions & Weight:

• Lengths:

• Towbar Body Lengths:

• Width (Maximum at Wheels): 40”
• Width (Maximum at Head): 10”
• Height (Towing Pin on Head): 11” – 28” (28 cm – 71 cm)
• Height (Lunette Eye): 11” – 43” (28 cm – 109 cm)
• Weight: 480 LBS (218 kg)

Designed for use at the aircraft (engine on wing) or in the overhaul shop in conjunction with the AM-1007 workstation. The stand is adjustable from 84" to 102" to accommodate the various work conditions. The work stand deck area is 4'-0" x 12'-0" and is equipped with "Aero Deck" allowing expansion of the width to 6'0" and the capability to conform to contours. This stand is equipped with a side stair.

Features:

• Used for towing/steering aircraft by attaching to nose landing gear (NLG) while pulled by tow tractor
• Primarily consists of cylindrical steel body

• Lunette eye at one end of towbar connects to tow tractor

• Mechanical head assembly at opposite end of towbar connects to aircraft NLG
• Towbar mounted on articulated undercarriage with hydraulic pump & retractable spring (to raise/lower towbar)

Configurations:

• 215050-1/-2 used for A310 or Aeroflot F-OGQU aircraft
• 215050-101 features spring-loaded handle on head assembly to open (when lifted) & automatically shut jaws (when released)

Mobility:

• Maximum aircraft towing speed of 5 MPH (8 km/h)

Dimensions & Weight:

• Length: 126.7” (3.22 meters)
• Height (Towing Pin on Head): 11” – 28” (28 cm – 71 cm)
• Height (Lunette Eye): 11” – 43” (28 cm – 109 cm)
• Width (Maximum at Wheels): 34” (86 cm)
• Width (Maximum at Head): 7” (17.8 cm)
• Weight: 480 LBS (218 kg)

Features:

• Licensed by Boeing Company to install & remove CF6-80C2 & PW4000-94" engines when supported by commercial engine cradles

• Other configurations available (click on part number link below to find out more):

Dimensions & Weight:

• Main Container: 20.0” Height x 26.0” Width x 74.0” Length / 2,000 LBS
• Hoist Container: 23.0” Height x 25.0” Width x 63.0” Length / 600 LBS

Features:

• Used for towing/steering A318, A319, A320 & A321 aircraft by attaching to nose landing gear (NLG) while pulled by tow tractor
• Primarily consists of cylindrical steel body

• Lunette eye at one end of towbar connects to tow tractor

• Mechanical head assembly at opposite end of towbar connects to aircraft NLG
• Towbar mounted on articulated undercarriage with hydraulic pump & retractable spring (to raise/lower towbar)

• Warning flag on head extends when shear pin breaks

• Painted to meet customer specifications

• The following configurations are available:

• Simple “Slide-Lok” mechanism allows quick & easy attachment/detachment

Mobility:

• Maximum aircraft towing speed of 9 MPH (15 km/h)
• Pneumatic tires designed to operate at gauge pressure of 14 psi

Dimensions & Weight:

• Length (Towbar Body): 127” (323 cm)
• Width (Maximum at Wheels): 41” (86 cm)
• Width (Maximum at Head): 7” (18 cm)
• Height (Towing Pin on Head): 11” – 28” (28 cm – 71 cm)
• Height (Lunette Eye): 11” – 43” (28 cm – 109 cm)
• Weight (approximate): 480 LBS (218 kg)

Caster mounted stand specifically designed for American Airlines to service the engine section of the Fokker F100 Aircraft. The engine stand is fixed height with multiple decks to service and maintain the engine. The main deck provides access beneath the engine. The aft deck provides access to the exhaust section of the engine. The forward deck provides access to the engine inlet. The deck surfaces that abut the aircraft (on all deck levels) include movable sliders with non-marking bumpers. Lights, electrical receptacles, and air receptacles are provided around the periphery of each deck level. A jib mounted air operated chain hoist is provided on the outboard side of the stand. A chain basket mounted to the hoist, supports the unused chain.

Features:

• Used for towing/steering B787-3, B787-8, B787-9 & B787-10 aircraft with category IV tow fitting by attaching to nose landing gear (NLG) while pulled by tow tractor
• Primarily consists of cylindrical steel body

• Lunette eye at one end of towbar connects to tow tractor

• Mechanical head assembly at opposite end of towbar connects to aircraft NLG
• Towbar mounted on articulated undercarriage with hydraulic pump & retractable spring (to raise/lower towbar)

Mobility:

• Maximum aircraft towing speed of 5 MPH (8 km/h)

Dimensions & Weight:

• Length: 131” (333 cm)
• Height (Towing Pin on Head): 11” – 28” (28 cm – 71 cm)
• Height (Lunette Eye): 11” – 43” (28 cm – 109 cm)
• Width (Maximum at Wheels): 36” (91 cm)
• Width (Maximum at Head): 7” (17.8 cm)
• Weight: 480 LBS (218 kg)

The AM-1015 workstand is designed to provide access to the No.1 and No. 3 engines on the DC-10 aircraft. The stand provides three (3) basic levels, as follows:
a. Fan Section
b. Core Section
c. LPT Section
Pop-up platforms are provided at the fan section and the core section to allow access to the pylon and the upper section of the fan case. The stands are provided in sets, (1) LH and (1) RH and are designed to allow full utilization with the cowl doors in the open position.

The AM-1067B Cabin Entry Access Stand is designed as a maintenance stair for use on the B747, DC10 and L1011 aircraft. The basic stand height is 15.5 Ft. and a pop-up step is provided to accommodate aircraft height variations. The top platform measures 66" x 96" and allows clearance for a B747 door in the open position. Stairway is 48" wide, and a mid-landing is provided at 96" above the floor. Four 10" diameter casters with swivel locks and face brakes are standard. A tow-bar is provided which stows on frame when not in use. Unit breaks down into modular sections for ease of shipment and field erection.

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.

Designed specifically for underwing, leading, and trailing edge access of the Lockheed L-1011 and the Boeing 747 in the jacked and un-jacked condition. Due to their vertical adjustment, excellent access is afforded to other wide-body aircraft, such as Douglas DC-10's, the family of Airbus A300's and new generations such as B767/757. Although designed for underwings, each stand (12 in total) may be used on other areas of the aircraft such as the horizontal stabilizer and elevator. Each stand has an adjustable parallelogram stair with non-skid "AERODECK" treads. Platforms match the nominal dihedral of the aircraft and have "AERODECK" flooring with slider sections at each end. Platforms are elevated by an air-operated twin jackscrew assembly driving a single scissor. Upper and lower limit devices prevent over-travel. Mobility is provided with large diameter swivel casters with locks and full-face contact brakes. Services consist of electrical and air convenience outlets. Lighting is provided in the form of fluorescent light is wired directly into junction boxes. Electrical service to the stand is from hanger power and connects to a pigtail fitting at the base of the stand. Air service to the stands also connects at the base with each stand or interconnecting stands. A connecting hose is supplied so that up to three (3) stands along the leading edge or three (3) sections along the trailing edge may be connected. Air manifolds are located on top of each platform. The elevating system is air-powered with a control valve located on top of the platform next to the stair landing. The air system is protected with a filter and lubricator. Each stand is supplied with a tow bar, but lightweight construction will allow hand movement by three (3) to four (4) personnel.

The AGSE-E009 Tail Stand is a caster mounted stand specifically designed for American Airlines to service the tail section of the Fokker F100 Aircraft. The tail stand is fixed height with multiple decks to service and maintain the vertical and horizontal stabilizers. The first deck provides access to the thrust reverser. A gate is provided on the first deck landing to facilitate removal of tool boxes and other heavy equipment. A hinged deck is provided on the forward end of the tail stand to provide access to the exhaust plug and engine pylon. The deck elevation is adjusted through the use of a cable winch. The second deck provides access to the horizontal stabilizer and upper vertical stabilizer surface. The deck surfaces that abut the aircraft (on all deck levels) include movable sliders with non-marking bumpers. Lights, electrical receptacles, and air receptacles are provided around the periphery of each deck level.

Features:

• Primarily consists of cylindrical steel body

• Lunette eye at one end of tow bar connects to tow tractor

• Mechanical head assembly at opposite end of tow bar connects to aircraft NLG
• Tow bar mounted on articulated undercarriage with hydraulic pump & retractable spring (to raise/lower tow bar)

Configurations:

• 215030-1/-2/-4 for A330, A340, A350, B767, B777, DC-10 & MD-11 aircraft with Category IV tow fitting
• 215030-3/-5 for B777 aircraft only
• 215030-6 for A350 aircraft only

Mobility:

• Maximum aircraft towing speed of 9 MPH (15 Km/h)

Dimensions & Weight:

• Length: 130” (330 cm)
• Width (Maximum at Wheels): 41” (86 cm)
• Width (Maximum at Head): 7” (17.8 cm)
• Height (Towing Pin on Head): 11” – 28” (28 cm – 71 cm)
• Height (Lunette Eye): 11” – 43” (28 cm – 109 cm)
• Weight (approximate): 480 LBS (218 kg)

Features:

• Licensed by Boeing Company to install/remove PW4000-94" & CF6-80C2 tail engines (both used on MD-11 aircraft) while supported by commercial engine cradles
• Customized to run from various power sources or 400Hz aircraft power

• System consists of:

• Powered bootstrap adapters (included with system) designed to accommodate cradles manufactured by various suppliers (click on part number links below to find out more):

o AGSE Cradle (AM-1928) with CF6-80C2 engine:

o AGSE Cradle (AM-1928) with CF6-80C2 engine:

o AGSE Cradle (AM-1928R) with CF6-80C2 engine:

o AGSE Cradle (AM-2371) with PW4000-94" engines:

o AGSE Cradle (AM-2371) with PW4000-94" engines:

o AGSE Cradle (AM-2425) with CF6-80C2/PW4000-94" engines:

o AGSE Cradle (AM-2538) with CF6-80C2 engine:

o Stanley Cradle (111267) with CF6-80C2 engine:

o Stanley Cradle (150950-2) with PW4000 engine:

o Stanley Cradle (111745-3) with PW4000 engine:

o Sabena Cradle (5-82846) with PW4000 engine:

o Sabena Cradle (5-86134) with CF6-80C2 engine:

Mobility:

• Caster-mounted control panel intended for manual positioning around aircraft in hanger or flight line
• Not towable
• Lifting beams & associated hardware stored in plywood container
• Three powered hoists (with bootstrap adapters) stored in individual containers with steel bases & fiberglass lids
• All containers can be raised by forklift

Dimensions & Weight:

• Main Container: 74.0” (Length) x 26.0” (Width) x 20.0” (Height) / 1,000 LBS
• Hoist Container: 34.0” (Length) x 32.0” (Width) x 48.0” (Height) / 250 LBS
• Console: 36.0” (Length) x 30.0” (Width) x 51.0” (Height) / 750 LBS

Features:

• Designed for use on B737-300 through –500 aircraft to install/remove CFM56-3 engine when supported by the following commercial engine cradles (click on part number link below to find out more):

• Bootstrap adapters included to accommodate cradles manufactured by various suppliers
• Functionally equivalent to Boeing part number C71003-190

Mobility:

• Components stored in a plywood container

Dimensions & Weight:

• With Container: 96.5” (Length) x 25.5” (Width) x 22.75” (Height) / 650 LBS

Features:

• Licensed by Boeing Company to install/remove CF6-6/-50 engines employed on DC-10-30 aircraft when supported by commercial engine cradles
• Adapters are included with system that can accommodate cradles manufactured by various suppliers
• Input electrical power can be customized
• Used exclusively for the tail engine

• Single powered source options of:

Dimensions:

• Main Container: 20.0” Height x 26.0” Width x 74.0” Length / 2,000 LBS
• Hoist Container: 48.0” Height x 32.0” Width x 34.0” Length / 250 LBS
• Console: 51.0” Height x 30.0” Width x 36.0” Length / 750 LBS

The AGSE-T027 B777 Nose Landing Gear Dolly is specifically designed for local site transport of the B777 nose landing gear main shock strut with wheels and down lock removed. The dolly consists of a base assembly and fixture designed for securing the gear. A sling is needed to install the gear onto dolly. The gear secures dolly easily using the upper torsion link for an attach point, the axles, and adjustable straps on both sides of yoke. The dolly is towable, with swivel locks and face brakes on the casters.