Eagle ICA-D212-725, Instructions Manual

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ICA-D212-725 (05)
Page 6 of 25
CHAPTER 05 – INSPECTION AND COMPONENT OVERHAUL SCHEDULE (05-00-00)
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COPYRIGHT

2007 BY DART AEROSPACE LTD.

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: 4
Date: 11.06.01
5.3 100 HOUR/12 CALENDAR MONTHS – PART A
Data Reference
Inspection Task Description
Initial
Mech Other
NOTE
Refer to the Bell 212 Maintenance Manual for the 100
Hour/12 Month Inspection – Part A requirements. Those
requirements must be supplemented to include the following
items
5.3.1 GENERAL
5.3.1.1 Refer to Honeywell Maintenance Manual
T5313B and T5317 Series for engine inspection
requirements.
Chapter 26 5.3.2 FIRE PROTECTION
5.3.2.1 Functionally check voltage of engine fire
extinguishing circuit
Manufacturer’s
Data 5.3.2.2 Replace engine fire extinguisher container firing
cartridges in accordance with specified service life.
Chapter 67 5.3.3 FLIGHT CONTROLS
5.3.3.1 Inspect D212-725-1-901 Bellcrank for damage
per Figure 5-1.
Chapter 71 5.3.4 POWER PLANT
5.3.4.1 Chip detector for debris.
5.3.4.2 Clean chip detector.
5.3.4.3 Test chip detector electrical circuit.
Chapter 72-00-00
Engine
Inspection, 1-C NOTE
Refer to engine manufacturer’s manual for engine Inspection
(service) requirements.
Chapter 71 5.3.5 STARTER GENERATOR
Every 3
rd
100 hour inspection or every 12 months