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