C130j cargo loading manual

Using its aft loading ramp and door, the C can accommodate a wide variety of oversized cargo, including everything from utility helicopters and six-wheeled armored vehicles to standard palletized cargo and military personnel. In an aerial delivery role, it can airdrop loads up to 42, pounds or use its high-flotation landing gear to land.  · The CJ Super Hercules offers superior performance and new converts the current PDF technical manual product that supports the baseline stretch and delivery of the C technical publications. Publications Lockheed Martin RSP answers the requirement to keep manuals updated by offering tailored. AIRCRAFT LOAD PLANNING AND DOCUMENTATION A. RESPONSIBILITIES (FOR AIR LOAD PLANNERS TRAINING, SEE DTR PART III, APPENDIX B) 1. The mobility force will: a. Assist the deploying unit in developing load plans and advising where there are aircraft limitation changes. While it is the responsibility of the deploying unit to develop load plans.

An operational manual is always to be provided for the loading instrument. Single point loading instruments are not acceptable. (IACS UR S) In addition to an approved loading manual, an approved loading instrument is to be supplied for all ships of Category I of m in length and above. (IACS UR S). Cargo Ramp Pendulum Arm Aft 1 in. 10 ft 9 ft Cross Sections Load Sta (C of Ramp Hinge) L Paratroop Door 9 ft Cargo Floor Static Ground Line 13 ft 11 in. Maximum at 4 ft 6 in. Above Cargo Floor 55 ft 9 ft 2 in. 3 ft 5 in. 10 ft 3 in. Bottom of A-Frame Litter Stanchion Bracket 13 ft 5 in. 10 ft Cargo Compartment. CEF was able to use our existing capabilities and expertise to build and assemble complete guide rails, conveyor rollers, ramp ADS (Aerial Delivery System) arms, lockboxes and the like. Today, we supply each CJ with over 75 component LRU parts. This is a true success story for both CEF Industries and Lockheed Martin.

Show activity on this post. As listed on a CNI-MU emulator designed for use by CJ loadmasters, the following is a list loads and moment arms for the aircraft: Basic weight: 80, lbf/STA Crew weight: lbf/STA Fuel weight: 38, lbf/STA -- this weight is, naturally, variable, although the moment arm appears to stay. Installation Vid: www.doorway.ru?v=ovGR5QzuciwDownload: www.doorway.ru Cargo Ramp Pendulum Arm Aft 1 in. 10 ft 9 ft Cross Sections Load Sta (C of Ramp Hinge) L Paratroop Door 9 ft Cargo Floor Static Ground Line 13 ft 11 in. Maximum at 4 ft 6 in. Above Cargo Floor 55 ft 9 ft 2 in. 3 ft 5 in. 10 ft 3 in. Bottom of A-Frame Litter Stanchion Bracket 13 ft 5 in. 10 ft Cargo Compartment.