User Manual Part 3

Page 3-30

16 Sep 2015

23-15-29

SYSTEM DESCRIPTION AND INSTALLATION MANUAL

JetWave™ System

C. Airworthiness Limitations

(1) Installation of the JetWave™ AES OAE assembly and LRUs on an aircraft by supplemental

type certificate (STC) or Form 337 obligates the aircraft operator to include the maintenance

information supplied by this manual in the operator’s Aircraft Maintenance manual and the

operator’s Aircraft Scheduled Maintenance Program.

(2) It is recommended that this section be appended to the Airplane Maintenance Manuals. The

information contained herein supplements the Airplane Maintenance Manuals in areas

covered by the JetWave™ AES FMA/TMA installation.

(3) It is recommended to consult basic Airplane Maintenance Manuals for limitations and

procedures not contained in this supplement. The inspections and airworthiness limitations

specified in this section are FAA approved.

(4) This section and the sections that follow specifies the inspections and other maintenance

required under sections 433.16 and 91.403 of the Federal Aviation Regulations unless an

alternative program has been FAA approved.

Initial and recurring inspections of the JetWave™ AES OAE assembly and LRUs and its associated

provisions are required. Specific inspection intervals are contained in Table 3-12.

D. General Instructions for Inspection

This section provides general instructions for the inspection of the JetWave™ AES OAE assembly

and LRUs .

(1) Gain access to the installation location on the fuselage for fuselage mount antenna assembly

or to the top of the aircraft vertical stabilizer in the case of tail mount antenna assembly

(2) Clean all visible surfaces of the antenna, radome assembly, and base plate.

(a) Do the inspections and checks presented in Electrical and Mechanical Inspection and

Check.

E. 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.

F. Scheduled Maintenance and Inspections

(1) The JetWave™ AES system does not require routine maintenance for continued

airworthiness.

(2) Scheduled inspections items in Table 3-12 must be done at a minimum of once a year -

preferably scheduled along with the other annual maintenance activities.

(3) It is recommended to periodically check JetWave™ AES cable connectors and, if required,

tighten connectors to recommended value.