Eagle ICA-D212-725, Instructions Manual

Page: 30 / 729

ICA-D212-725 (05)
Page 9 of 25
CHAPTER 05 – INSPECTION AND COMPONENT OVERHAUL SCHEDULE (05-00-00)

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
5.4 25 HOURS/30 DAYS – PART B
Data Reference
Inspection Task Description
Initial
Mech Other
5.4.3.5.4 Proper oil level.
Chapter 26 5.4.3.6 Engine compartment fire extinguisher container
for proper charge, condition, and mounting.
Chapter 71 5.4.3.7 Power plant:
5.4.3.7.1 Tail pipe for damage and security.
5.4.3.7.2 Oil and fuel hoses and tubes for chafing, leaking,
and security.
5.4.3.7.3 Electric wiring for fraying, chafing, and security.
Chapter 71 5.4.3.8 Engine firewalls, air intake cowl, and plenum for
cracks, distortion, missing rivets, broken spot welds, and
deteriorating seals and gaskets.
Chapter 71 5.4.3.9 Engine cowling for missing fasteners and cracks.
Latches for proper operation.
5.4.4 TAILBOOM
5.4.4.1 Inspect D212-725-1-901 Bellcrank for damage
per Figure 5-1.
5.4.5 CABIN ROOF
Chapter 63 5.4.5.1 Engine-to-transmission (main) driveshaft:
5.4.5.2 Main driveshaft for corrosion, condition, and
security.
Chapter 71 5.3.6 ENGINE MOUNTS
Every 4
th
25 hour inspection or every 12 months
5.3.6.1 Inspect engine mounts visually for cracks,
damage, corrosion and security. Pay particular attention to
security of turnbuckle jam nuts and to loose or missing
locking wire.
5.3.6.2 Cracked sleeves, studs, bolts and bearings must
be replaced immediately per Chapter 71.