MIL-PRF-83817B
and to remain securely attached to the forklift during all aircraft loading
operations. The devices shall have a safety factor of at least 2 when the rated load
is equally applied to both devices.
b. A pintle type, towing hitch shall be located at the center, end of the aircraft
loading attachment opposite the fork insertion pockets.
c. The aircraft loading attachment shall be of adequate length, width, height, and
strength to support aircraft loading operations as specified (see 3.3.9.15.1)
d. Unless otherwise specified (see 6.2), the final paint (see 3.3.1.3) and markings
(see 3.3.2) shall be consistent with the colors of the forklift on which the aircraft
loading attachment is attached. The top of the aircraft loading attachment shall
have "XX,XXX LBS" (where XX,XXX equals the final push/pull capacity of the
vehicle) stenciled in 1-1/2 inch high letters with paint.
e. Storage devices to allow the aircraft loading fork attachment to be stored on the
forklift without modification to the forklift.
3.3.9.16 Wheel guards. The forklift shall be designed so that material is not thrown off the
rotating tires onto cab windows or light assemblies. If wheel guards are used, each wheel guard
shall be capable of supporting at least 300 pounds in any one square foot area without evidence
of damage.
3.3.9.17 Boom assembly. The boom shall be designed to provide fore and aft (horizontal)
extension and retraction, and tilting movement for raising and lowering the fork carriage. The
maximum angle that the boom can be tilted, with rated load on the forks, shall be limited to 45
degrees. The forklift shall be capable of meeting all requirements of this document with this
limitation.
3.3.9.18 Boom attachments. The boom shall be designed to accept multiple attachments as
needed. Each attachment shall have its own set of instructions and load chart. Attachments may
have up to one standardized hydraulic fitting to allow for hydraulically powered operations by
the attachment. When specified (see 6.2), the forklift shall be provided with any combination of
an engine installation/removal attachment or a pintle hook attachment. If a pintle hook
attachment is required, then aircraft loading forklift attachment (see 3.3.9.15) is not required.
Attachments shall be easily installed or removed, requiring at most 2 people, and not more than
15 minutes per attachment.
3.3.9.18.1 Engine installation/removal attachment. When specified (see 6.2), the forklift will be
shipped with an engine installation/removal attachment. The engine installation/removal
attachment shall have sufficient capacity to remove a C-130 engine and propeller combination
weighing up to 5,500 lb. at 16 ft. load center (when measured from the forward most part of the
forklift), without the use of outriggers. The attachment shall provide at least 24" of horizontal
travel while the vehicle remains stationary. The horizontal travel shall be hydraulically operated
by the vehicle operator from the cab. The horizontal travel can also be accomplished with a
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