User's Manual Part 6

Page 8-3
3 Mar 2017
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
8.5 Electrical and Mechanical Inspection and Check
Periodic inspections of the mechanical and electrical interfaces of the JetWave™ AES OAE assembly and
LRUs to the aircraft should be completed as defined by the governing airworthiness body (such as
Transport Canada, the FAA, or the JAA) Instructions for Continued Airworthiness for the installation.
For the general guidelines refer to Visual Inspection and Check and Scheduled Maintenance and
Inspections sections.
8.6 Instructions for Continued Airworthiness
This section supplies the special instructions and maintenance requirements for continued airworthiness
of the JetWave™ AES subsystems.
JetWave™ AES OAE assembly and LRUs are considered “On-Condition” units. No additional or
routine maintenance is required for the on-condition JetWave™ AES OAE assembly and LRUs.
If a JetWave™ AES OAE assembly or an LRU is inoperative, do as follows:
(a) Collar applicable switches and circuit breakers
(b) Secure cables and wiring
(c) Remove the unit
(d) Placard the JetWave™ AES LRU and associated items as “
inoperative” in accordance
with the Aircraft Maintenance Manual (AMM)
(e) Before flight, do as follows:
(f) Record the removal of the unit in the aircraft log book
(g) Revise the equipment list. Refer to section 91.213 of the FAR or the aircraft’s Minimum
Equipment List (MEL
)
(h) Revise the weight and balance data as applicable.
(i) In case of Modman replacement, the VAR/DP needs to be notified so that the system is
recomm
issioned to the new terminal ID.
JetWave™ AES system LRUs are not field-repairable. Return the faulty LRU(s) to the Honeywell
authorized facility for repair.
Install repaired or replacement LRUs on the aircraft in accordance with the installation instructions
supplied in this manual. Refer to ARINC 615A Software Data Load Process on page 5-1 for
instructions on how to bring the repaired or replacement LRU up to current software release.
Make sure that all repaired units operate correctly before you approve them for return to service,
with the operational verification tests and procedures provided in this SDIM. Approval for return to
service must be entered in the logbook as required by section 43.9 of the FAR.
Enter the approval for return to service in the appropriate logbook as required by FAR Section 43.9.
Add the scheduled maintenance tasks to the aircraft operator’s appropriate aircraft maintenance
program as follows:
Draft as of 31 May 2017