TM 1-1670-260-12&P                           0010  00 __________________________________________________________________________________________ (3) Perform the following inspections listed in table 6 on the recovered     helicopter after a UMARK aerial recovery.   Table 6 Post-recovery inspection list prior to release for flight Structure              Inspection Type    Criteria                  Corrective Action Droop Stop Hardware    Visual             Bent or broken pieces     Replace Hub Lower Shoe         Visual             Abrasion                  Replace or repair                                                                     per DMWR 1-1615-                                                                     312, paragraph                                                                       4-17.5   Landing Gear           Hard Landing       Hard Landing Evidence     Replace or repair                                                                     per DMWR 1-1620-                                                                     248 Tailboom               Visual             Damage or abrasion        Repair per TM                                                                       1-1500-204-23-10                                                                     Vol. 10 Tailboom               Internal Visual    Cracks in # 4, 6, & 7     Repair per TM   (if tail sling is                         stringers between FS      1-1500-204-23-10 improperly rigged)                        436.5 and 450             Vol. 10            Fuselage between and   Visual             Cracks or deformation,    Repair per TM   including frames at                       deformation. Missing      1-1500-204-23-10 FS 176 and FS 230                        sheared, or loose         Vol. 10 (include skin/string-                     fasteners ers, deck and struts) M/R blade (if re-      Visual and         Damage, cracks,           Repair or replace covered w/blades on)  cheesecloth*       abrasion                  DMWR 55-1615-313   Main Rotor blade       Visual             Damage, cracks,           Repair per TM   Tiedown points                            abrasion                  1-1500-204-23-10                                                                     Vol. 10 Tail Rotor Hub         Visual             Bumper stop condition     Repair or replace                                                                     as necessary per                                                                     TM 1-1520-238-23                                                                     -3 Tail Rotor Blade       Visual and         Damage, cracks            Repair or replace                        cheesecloth*                                 per TM 1-1520-                                                                     238-23-3 * Wipe blade with cheesecloth, NSN 8305-00-205-3558. Cloth snagging indicates      possible crack. 0010 00-17 END OF WORK PACKAGE