TTP B1-L2 ATA 44 Beech 90 Series B2-L3 Cabin S ystems 44 CABIN SYSTEMS -00 General -10 Cabin Core System -20 Inflight Entertainment System -30 External Communication System -40 Cabin Mass Memory System -50 Cabin Monitoring System -60 Miscellaneous Cabin System PTP Beech 90 Series B1 LOC B2 LOC FOT SGH R/I MEL TS
TTP B1-L1 ATA05 Beech 90 Series B2-L1 Time Limit/ Maintenance Check Inspection Requirements (1) 200-Hour Phase inspection program - A complete inspection is 800 hours or 24 months, w hich e v er occurs first. The inspection c ycle is d i vided into four phases and each inspection c ycle is accomplished at 200 hours. Section 5-10-01 . (2) Alternate Phase inspection program F or operators f l ying less than 400 hours b ut more than 200 hours in 24 months. P erfo r m scheduled phase inspections 1 and 2 t o gether within 12 months after the last inspection. P erfo r m scheduled phase inspections 3 and 4 t o gether within 12 months after complet - ing the phase 1 and 2 inspections. Section 5-20-00. (3) Biennial inspection program F or operators f l ying less than 200 hours in 24 months. ...
TTP B1-L3 ATA 27 Beech 90 Series B2-L2 Flight Controls INTRODUCTION The aircraft uses co n v entional three-axis flight controls; ailerons, el ev ators, and a r udde r . T w o electr i cal l y dr i v en flaps are on each wing. Ground steering is accomplished b y the r udder pedals through a mechanical steering rod attached to the nose landing gea r . GENERAL LJ-1 AND AFTER; L W-1 AND AFTER Flight-control m o v ement is accomplished through single non-redundant ca b les, push rods, and bell cranks, and are non-p o w ered (with the e xception of the r udder boost). The ailerons and el ev ators are controlled b y co n v entional control columns interconnected to a T -column behind the inst r ument panel. The r udder is operated with co n v entional r udd...
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