TM 1-1670-260-12&P 0009 00 __________________________________________________________________________________________  4.    COMPONENTS REQUIRED Components of UMARK utilized during the one-hook, short-line recovery are listed in Table 2.  Common equipment used by the ground rigging crew, such as shockproof gloves, goggles, radios, etc., are not included in UMARK.  No additional tools are required for UMARK assembly or rigging of the helicopters.   Table 2. UMARK Components Required Item Description Qty Item Description Qty Black/White 30 Ft Heavy Weight Sling 1 Box Link Assembly 3 Black/White 30 Ft Heavy Weight Sling with Bridle 1 Shackle Assembly 1 Green/White 150 Inches (12.5 Ft) Light Weight Sling 4 Adjustable Length Tie-Down 2 Yellow/White 153 Inches (12.75 Ft) Light Weight 4 Fixed Length Tie-Down (With Snap) 4 Red/White 208 Inches (17.33 Ft) Light Weight Sling 2 Fixed Length Tie-Down (Without Snap) 1 Blue/White 360 Inches (30.0 Ft) Light Weight Sling 1 Blade Sleeve Assemblies 4 Black/White 120 Inches (10 Ft) Light Weight Sling 1 Blade Pole Assembly 1 Crossbar Assembly 1 Cargo Hook Thimble 1 Sling Link Assembly 2 Drogue Chute 1 5.    DISABLED HELICOPTER RIGGING   6.    Inspect Disabled Helicopter for Damage WARNING To   prevent   death   or   injury   to   personnel,   and/or damage to the recovery and/or recovered helicopter, discontinue   the   disabled   recovery   procedure   if damage is detected and refer to Work Package 0012 00 of this manual as directed.   a.   Check the main rotor assembly and main rotor support, transmission and transmission mounts, and tail-boom for damage in accordan ce with applicable technical manual. b.    If  damage is determined, discontinue procedure and perform  the damaged AH-64A/D recovery procedure outlined in Work Package 0012 00 of this manual. c.    If no damage is detected in the preceding step proceed to the next step. 7.   Install Main Rotor Rigging (Figures 1, 2 and 3, and Table 3) NOTE Figure  1   details   the   disabled   AH-64D   helicopter   and recovery  helicopter  rigging.  Reference  numbers  in  the following text that are outlined in parentheses [i.e., (1), (2), etc.] refer to Figure 1 and Table 3 item numbers. Refer to Figure 1 and Table 3 for configuration guidance. a.    Rotate the main rotor assembly to standard tie-down position. (Figure 1, View B)   b.    If  operable  (helicopter  with  power),  to  minimize  loads  on  the  main and tail  rotor  blades,  set  controls  to collective full down, neutral cyclic and pedals. 0009 00-3 NOTE A  short  line  recovery  of  an  AH-64  helicopter  with  the blades  on  in  bad  weather  or  high  winds  could  result in  main  rotor  blade  damage.