Page 791 - POH-SUPER KING AIR B200/B200C
P. 791

130-590031-145R7_text.fm  Page 4  Wednesday, February 17, 2010  4:37 PM



                           SECTION 3 - EMERGENCY PROCEDURES

                           (FL-80 AND AFTER; FM-5 AND AFTER; FN-1 AND AFTER)
                           Delivered by Hawker Beechcraft Corporation or Installed by Kit 130-3402-3,
                           130-3408-1 or 130-3408-3:

                           GLIDE
                           After last step in POH/AFM, add the following:

                              • ELT Switch  . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON;
                                                                      Yellow [XMT] - BLINKING

                           SECTION 3A - ABNORMAL PROCEDURES
                           No change.

                           SECTION 4 - NORMAL PROCEDURES

                           PREFLIGHT INSPECTION

                           (FL-80 AND AFTER; FM-5 AND AFTER; FN-1 AND AFTER)
                           Delivered by Hawker Beechcraft Corporation or Installed by Kit 130-3402-3,
                           130-3408-1 or 130-3408-3:

                           Delete reference to arming the ELT.
                           BEFORE ENGINE STARTING


                                                     NOTE
                                 Items marked with an “*” may be omitted at pilot’s discretion after
                                 the first flight of the day.
                           (FL-80 AND AFTER; FM-5 AND AFTER; FN-1 AND AFTER)

                           Delivered by Hawker Beechcraft Corporation or Installed by Kit 130-3402-3,
                           130-3408-1 or 130-3408-3:
                              • ELT Switch  . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ARM;
                                                                Yellow [XMT] - EXTINGUISHED











                                                                             FAA Approved
                                                                        Revised: March, 2010
                           4 of 8                                        P/N 130-590031-145
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