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Pathfinder Sling Load Written Test questions and answers

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Pathfinder Sling Load Written Test questions and answers

Instelling
PATHFINDER WRITTEN SLING LOAD
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PATHFINDER WRITTEN SLING LOAD










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Instelling
PATHFINDER WRITTEN SLING LOAD
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PATHFINDER WRITTEN SLING LOAD

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Pathfinder Sling Load Written Test questions and
answers


TM 4-48.09 - answer-Multiservice Helicopter Sling Loads: Basic Operations and
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Equipment
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Multiservice Helicopter Sling Loads: Basic Operations and Equipment (Reference) -
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answer-TM 4-48.09
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TM 4-48.10 - answer-Multiservice Helicopter Sling Loads: Single Point Rigging
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Procedures
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Multiservice Helicopter Sling Loads: Single Point Rigging Procedures (Reference) -
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answer-TM 4-48.10
c c




TM 4-48.11 - answer-Multiservice Helicopter Sling Loads: Dual Point Rigging
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Procedures
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Multiservice Helicopter Sling Loads: Dual Point Rigging Procedures (Reference) -
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answer-TM 4-48.11
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FM 3-21.38 - answer-Pathfinder Operations
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Pathfinder Operations (Reference) - answer-FM 3-21.38
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FM 4-20.102 - answer-Airdrop of Supplies and Equipment: Rigging Airdrop Platforms
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Airdrop of Supplies and Equipment: Rigging Airdrop Platforms (Reference) - answer-FM
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4-20.102
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Three elements involved in sling load operations. - answer-- Supported Unit (unit whose
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cequipment will be moved) c c c


- Supporting Unit (the aviation unit that will fly the loads)
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- Receiving Unit (normally an internal element of the supported unit)
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OPTIONAL: Pathfinder Unit (subject matter expert in all aspects of sling load
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operations--separate, organic unit)
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Responsibilities of Supported Unit - answer-- Selecting, preparing, and controlling the
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cpick-up site to include communications
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- Advance coordination with the supporting unit NLT 24 hr prior to the mission
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,- Actual rigging of the loads
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- Provides trained ground crews to guide aircraft and hook up the load
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- Furnishing slings, straps, clevises, and any other slip load equipment required
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- Assuring that the loads are properly rigged and do not exceed ACL of A/C
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Responsibilities of the Supporting Unit - answer-- Ensure that the loads fall within the
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ctransporting aircraft's ACL c c


- Provides assistance in the recovery and return of sling-load equipment
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- Advises the supported unit on load limitations
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- Advise the supported and receiving units on the suitability of selected LZ/PZ's
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- Establish coordination with the supported and receiving units
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Responsibilities of the Receiving Unit - answer-- Selecting, preparing, and controlling the
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clanding site to include communications
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- Receiving and de-rigging the load
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- Ensure proper supervision of the de-rigging
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- Provide the return of lifting equipment and/or personnel
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Responsibilities of the Pathfinder Unit - answer-- Provide advice and aid to thec c c c c c c c c c c c


csupported, aviation, and receiving units c c c c


- Provide expertise in the planning and execution of both PZ and HLZ operations
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- Supervise the rigging and inspection of all the loads
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- Provide ground guidance and air traffic control during the sling load
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- Ensure that the loads fall under the transporting aircraft's ACL
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Types of Loads - answer-- High Density
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- Low Density
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- Aerodynamic
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Unique Characteristic of High Density Loads - answer-Offers best stability
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(ex. HMMWV)
c




Unique Characteristic of Low Density Loads - answer-Offers least stability
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(ex. A22 Cargo Bag)
c c c




Unique Characteristic of Aerodynamic Loads - answer-Unstable until the load is
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cstreamlined, then it becomes stable c c c c


(ex. Downed Aircraft)
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Maximum External Load capabilities... - answer-will vary due to environmental
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conditions and helicopter performance.
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What does ACL mean, what is it, and what is it based on? - answer-Allowable Cargo
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Load - the maximum load capacity for a particular mission and determines what the
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helicopter can lift.
c c c

, Based on type of aircraft, age of airframe, pilot experience, altitude above sea level,
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temperature, humidity, and aviation unit's SOP.
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APEX Requirements for UH-1 Iroquois - answer-A nylon point of attachment, like 3 ft
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apex ring or basket hitch, must be used to attach load to aircraft. In addition, 11k cargo
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hook reach pendant or a polyester round sling can be used as the point of attachment to
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the A/C to a UH-1 series aircraft.
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UH-1N/Y Cargo Hook Rated Capacity - answer-5,000 lbs
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APEX Requirements of UH-60 Blackhawk - answer-When using 10k apex, aluminum
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apex spacer MUST be used. This will center apex on cargo hook and prevent apex from
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lifting the keeper during oscillation of the load, which would result in load being
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jettisoned from cargo hook.
c c c c


When using 25k apex, spacer MUST BE REMOVED. If 25k apex spacer used, air crew
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cannot jettison the load if required and cargo hook must be manually operated by the
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crew chief or ground crew on LZ.
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*NEVER* use nylon point of attachment such as 3 ft apex ring because it will bind on the
c c c c c c c c c c c c c c c c c


load beam of the argo hook and prevent the crew from releasing the load in an
c c c c c c c c c c c c c c c c


emergency situation.
c c




UH-60 Hook System Rated Capacity - answer-- A Model: 8,000 LBS
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- L Model: 9,000 LBS
c c c c


- M Model: 9,000 LBS
c c c c




APEX Requirements for CH-47 Chinook - answer-Requires no special apex in
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preparation and may accept all configurations. (ex. 10k apex with and w/o spacer, 25k
c c c c c c c c c c c c c c


apex with or w/o spacer, nylon multi-point configuration, etc.)
c c c c c c c c c


*DO NOT* attach single point loads to CH-47 D/F if there is nylon point of attachment to
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A/C
c




CH-47 D/F Cargo hook Locations and Rated Capacity - answer-- Center Cargo Hook:
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c26,000 lbs c


- CH-47 D/F Fore and Aft Cargo Hooks:
c c c c c c c


c1. Each: 17,000 lbs
c c c


c2. Combined: 25,000 lbs
c c c


c3. Fore and Aft Cargo Hooks are 13 ft apart
c c c c c c c c c




APEX Requirements for CH-53E Super Stalion - answer-Dual-point suspension system,
c c c c c c c c c


uses a forward and aft cargo hook, located 10 ft apart and must be used for dual-point
c c c c c c c c c c c c c c c c c


loads (A/C maximum lift capacity for this is 32,000 lbs with a max of 60% of sling load on
c c c c c c c c c c c c c c c c c c c


either forward or aft hook). A pendant is designed to be used with the dual-point system
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to provide more clearance between helicopter and hookup team.
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Aircrew can open forward or aft cargo hook electrically or manually. Manual release
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lever is on left side of cargo hook. In emergency, ground crew open hook by moving
c c c c c c c c c c c c c c c c


manual release lever up.
c c c c
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