Stanley Aviation

The P/N 220200 and 220230 series Towbar Assemblies are used for towing and pushback of the Airbus A300 and Boeing B727 aircraft.

Features:

• Tow bar used for towing & steering aircraft by attaching to aircraft's Nose Landing Gear (NLG) & pulled by tow tractor

• Consists of a cylindrical steel body

• Mounted on articulating undercarriage with hydraulic pump & retract spring to raise/lower tow bar

Mobility:

• Not to exceed 15 Km/h or 9 MPH when towing aircraft
• Pneumatic tires designed to operate at gauge pressure of 14 psi

Dimensions & Weight:

• Length: 130” (330 cm)
• Width (maximum at wheels): 41” (86 cm)
• Width (at head): 7” (18 cm)
• Height (from towing pin on head): 11” – 28” (28 – 71 cm)
• Height (from lunette eye): 11” – 43” (28 – 109 cm)
• Weight: 480 LBS (approximate)

110655 Bootstrap Hoist System consists of forward and aft crossbeams with hangers, pulleys, a balance cable , forward beam support, two aft and two forward manual hoists, and three
dynamometers. It is used for bootstrapping the General Electric CF6-50 and CF6-80 engines and the Pratt & Whitney JT9D-7R4 and JT9D-59 engines on Airbus A300, A300-600, and A310 aircraft.

Features:

• Tow bar used for towing & steering aircraft by attaching to aircraft's Nose Landing Gear (NLG) & pulled by tow tractor

• Consists of a cylindrical steel body

• Mounted on articulating undercarriage with hydraulic pump & retract spring to raise/lower tow bar

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

• Warning flag on head extends when shear pin breaks

• Painted to meet customer specifications

Mobility:

• Not to exceed 15 Km/h or 9 MPH when towing aircraft
• Pneumatic tires designed to operate at gauge pressure of 14 psi
Dimensions & Weight:

• Length: 127” (323 cm)
• Width (maximum at wheels): 7” (18 cm)
• Height (at towing pins): 11” – 28” (28 – 71 cm)
• Height (at lunette eye): 11” – 43” (28 – 109 cm)
• Weight: 480 LBS (approximate)

The Stanley 200470 towbar is used for towing and steering the Boeing Business Jet (BBJ) (B737) by attaching to the aircraft's Nose Landing Gear (NLG) and being moved by a tow tractor. The towbar body consists of a cylindrical aluminum body. At one end of the tow bar is a lunette eye which connects to the tow tractor. At the opposite end of the tow bar is a mechanical head assembly which connects to the aircraft front landing gear .

CRADLE ASSEMBLY FOR CF6-80A/A1 ENGINES.

P/N 110513-1, -1A, -101

The Stanley Part Number 114800-1 & -2 Engine Shipping Systems are designed specifically for transportation ground handling and maintenance of IAE V2500-A5 Engines used on the Airbus A319 20 and 21. The 114800-1 is composed of the 114701-1V Stand and the 114802-1 Cradle. The 114800-2 uses the 114802-2 cradle.

The 114701-1V Stand rides on swivel casters. The casters may be mounted at either of two heights. The lower position provides one inch clearance for engine installation and removal and the upper position provides six (6) inches for towing. The casters may be stowed on the stand for shipping. The aft casters are equipped with locking brakes. The mounts for the cradle are shock absorbing. The shock mounts prevent unwanted vibration or shock loads from being transmitted to the engine during handling and shipping. There are twelve (12) tie-down rings located around the stand for convenience in shipping.

The 114802-1 & -2 Cradles provide forward and aft engine mount assemblies. They are intended for low speed (3 MPH [5 KPH] or less) ramp and hanger smooth surface use only and can be used with the engine manufacturer-approved engine slings or bootstrap hoists to install and remove V2500 engines. The cradles are equipped with four (4) pivoting legs that enable them to be used as a shop work stand. The forward and aft engine mounting supports may be removed to facilitate shipping and storage.

The 114802-1 & -2 Cradles utilize a turnbuckle system that absorbs any rotational stress that is placed on the engine. The aft engine mount of the cradles are designed to pivot thereby eliminating stress caused by rotational inertia. Once the engine is placed onto the cradle and secured to the stand the engine can be moved without fear of damage.

Once the flight mounts are removed the Propulsor Only Shipping System allows truck Shipment of the propulsor and bi-fi. Air shipment of the propulsor and bi-fi in a 747 aircraft. Four sixteen inch shock absorbing casters swivel inboard/outboard for clearance and easy deployment. Each caster has the capability of separate manual steering. Towbar that is capable of steering the unit from ether end and is stored directly on the unit.

The Stanley V2500-D5 Engine Cradle is designed for use with the IAE V2500-D5 engines used on McDonald Douglas MD90 aircraft. The Engine Cradle is composed of the Cradle and Roller Shoe Assemblies. When combined with a shipping stand these components facilitate ground and air transport of the V2500-D5 engines. This manual provides operational and service instructions for the Stanley V2500-D5 Engine Cradle.

The cradle features:
· Forward and aft mount assemblies are included.

· Can be truck shipped as a standard size load.

· Hoist and bootstrap provisions.

· Roller Shoe assemblies are included in the –2 configuration which allow movement while on the engine stand.

· Removable mount adapters.

· Universal design can be used with a variety of shipping stands.

The Cradle Assembly is available in the following configurations:
· P/N 113401-1 Designed for a stand with rails 90” apart but does not include roller shoe assemblies.

· P/N 113401-2 Designed for a stand with rails 90” apart and does include roller shoe assemblies.

Note: Both configurations utilize the same component parts. The only difference is the presence 
or lack of Roller Shoe assemblies.