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SECTION 2 CESSNA LIMITATIONS MODEL 208B G1000 PLACARDS (Continued) 2-38 20. Near ground service plug receptacle: 21. On access panel on bottom of both wings just forward of aileron: FLUX VALVE USE NON-MAGNETIC TOOLS AND SCREWS 22. On each side of nose strut fairing near tow limit marking (rudder lock placard required when rudder lock installed): WARNING MAXIMUM TOW LIMIT EXTERNAL POWER 28 VOLTS D.C. NOMINAL 800 AMP STARTING CAPACITY MIN. DO NOT EXCEED 1700 AMPS 23. Adjacent to left crew door inside door handle: U.S. (Continued Next Page) CAUTION DO NOT TOW AIRCRAFT WITH RUDDER LOCK ENGAGED FAA APPROVED 208BPHBUS-00
CESSNA SECTION 2 MODEL 208B G1000 LIMITATIONS PLACARDS (Continued) 24. Adjacent to upper passenger door outside pushbutton and door handle (Passenger version only): 25. Adjacent to upper passenger door inside door handle (Passenger version only): 26. At center of lower passenger door on inside and outside (Passenger Version only): (Continued Next Page) FAA APPROVED 208BPHBUS-00 U.S. 2-39
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CESSNA INTRODUCTION MODEL 208B G100
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CESSNA SECTION 1 MODEL 208B G1000 G
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SECTION 3 CESSNA EMERGENCY PROCEDUR
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SECTION 3 CESSNA EMERGENCY PROCEDUR
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SECTION 3 CESSNA ABNORMAL PROCEDURE
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CESSNA SECTION 3 MODEL 208B G1000 A
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CESSNA SECTION 4 MODEL 208B G1000 N
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CESSNA SECTION 5 MODEL 208B G1000 P
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CESSNA SECTION 6 MODEL 208B G1000 W
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SECTION 7 CESSNA AIRPLANE AND SYSTE
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CESSNA SECTION 8 MODEL 208B G1000 H
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