Page 457 - (KU)01-75GAJ-1.5 - Change 1
P. 457

INTRO


   EP'S                                                              (KU)01-75GAJ-1.5                       FIGURES

                             Last
                             Resort    CAN NORMAL AIRDROP PROCEDURES BE                                      ACAWS
                                   Q3
                                       USED?


                                       NO   O. Airdrop procedures........................................ Utilize  GROUND

                                                If the normal airdrop system is operative, cargo
                                         R                                                                  TAKEOFF
                                                may be jettisoned using the aerial delivery system
                                                and normal airdrop procedures.

                                                If an extraction system malfunction is known to             FIRE/SMK
  NORM                                          have occurred prior to the initiation of airdrop,
                                                the cargo may be jettisoned the same as cargo
                                                palletized on rollers but not rigged for airdrop.           PRES/OXY

                                            (End of Procedure)
                                                                                                           ENG/PROP
                                     P. AUX PUMP switch..........................................................ON

                                     R. Cargo ramp and door.....................................Clear to open  FUEL

                                     S. Aircraft attitude..................................................10° nose up
                                                                                                               AAR
                                           Ten degrees nose up will allow gravity to extract the load.

                                     T. Power............................................Accelerate (as required)
  SPEC                              NOT FOR FLIGHT                                                             ELEC
                                           Acceleration will assist in extracting the load.

                                                                                                               HYD
                                                             CAUTION

                                                                                                            FLT CTRL
                                           During cargo jettison, move the elevator control
                                           slowly, smoothly and no more than necessary to
                                           avoid exceeding structural limits.                                 GEAR

                                     U. Cargo ramp and door................................................. Close
                                                                                                            DOR/RMP
  PERF                               V. AUX PUMP switch...................................................... OFF

                                     (End of Procedure)                                                     JETTISON

                            Jettison of large heavy palletized or unpalletized cargo resting on the
                            ÀRRU VKRXOG EH DWWHPSWHG RQO\ DV D ODVW UHVRUW                                  LANDING


                                                         WARNING                                            DITCHING


                                   +HDY\ FDUJR UHVWLQJ RQ WKH ÀRRU PD\ PRYH VORZO\ DQG                      BAILOUT
                                   or become misaligned and wedged in the aft area and
                                   could cause an out of limit CG condition resulting in loss
  OPER                             of aircraft control.                                                     FAULT LG

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