Eagle ICA-D212-725, Instructions Manual

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ICA-D212-725 (04)
Page 2 of 2
CHAPTER 04 – AIRWORTHINESS LIMITATIONS (04-00-00)
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COPYRIGHT
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2007 BY DART AEROSPACE LTD.
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THIS DOCUMENT IS PRIVATE AND CONFIDENTIAL AND IS SUPPLIED ON THE EXPRESS CONDITION THAT IT IS NOT TO BE USED FOR ANY PURPOSE OR COPIED OR COMMUNICATED TO
ANY OTHER PERSON WITHOUT WRITTEN PERMISSION FROM DART AEROSPACE LTD.
Revision:
0
Date: 07.05.31
4.1 AIRWORTHINESS LIMITATIONS SCHEDULE
4.1.1
The airworthiness limitations in Chapter 04 of BHT-212-MM apply except as noted in 4.1.2
and 4.1.3 below.
4.1.2
Refer to the following Honeywell T5313B/T5317 Service Bulletins for airworthiness limitations
associated with the T5317A or T5317B engine.
T5313B/17-0001 Time Between Overhaul/Time Between Inspection
T5313B/17-0020 Life Limits
4.1.3
The Main Input Driveshaft p/n 204-040-433-101 has been adopted from the Bell 205A1 in
accordance with Technical Bulletin 205-82-45 and therefore retains the following
airworthiness limitation per TB 205-82-45.
Component Part Number Airworthiness Life
POWER TRAIN DRIVE SYSTEM COMPONENTS
Main Input Driveshaft 204-040-433-101 5000 Hours
The Airworthiness Limitations section is approved by the Minister and specifies maintenance required by
any applicable airworthiness or operating rule unless an alternative program has been approved by the
Minister.
F.J.B. Wright
Regional Manager, Aircraft Certification
Prairie Northern Region