188.8.131.52 Add to Paragraph 12, Post Recovery Disabled Helicopter Procedures
additional checks as follows:
184.108.40.206.a Perform main rotor blade Sudden Stoppage inspection in accordance with
220.127.116.11.b Airframe Inspections - Using Aircraft Weight and Balance Record calculate
the weight and center of gravity of the aircraft at time of recovery. Plot resulting point
on graph below.
UH-60A/L Airframe Static Capability - Retrieval by UMARK
UH-60 Allowable - UMARK
18.104.22.168.c If point is below the line above no airframe inspections are required.
22.214.171.124.d If point is above the line perform the following airframe inspections:
126.96.36.199 Inspect cabin area for cracks, permanent deformation, and loose or missing
fasteners in the following areas:
188.8.131.52.1 Inspect Frame at Station 327.115
184.108.40.206.2 Inspect Beams at Buttline 16.5 from Station 308.0 to Station 343.5
220.127.116.11.3 Inspect Forward absorber supports from Station 308.0 to 327.115