Instructions for Continued Airworthiness G600, GNS 530W, GNS 430W, 190-01080-05 Rev. 2
GMA 347, GTX 330D, GMX 200, WSI AV-200 Cessna 208/208B Page 11 of 29
Item Description/Procedure Interval
GDU 620,
GRS 77,
GDC 74A,
GMU 44,
GTP 59,
GAD 43,
GNS 530W
GNS 430W,
GMA 347
Perform an electrical bonding test for each listed LRU:
1. Gain access to the LRU (see General Arrangement
Drawing for LRU location)
2. Disconnect all harness/antenna connectors from the LRU
3. Measure the resistance between the LRU and a nearby
exposed portion of aircraft metallic structure
a. For the GDU 620, verify the resistance is less
than or equal to 40 milliohms
b. For the GTP 59, verify the resistance is less than
or equal to 5 milliohms
c. For the remaining LRUs, verify the resistance is
less than or equal to 20 milliohms
d. If the resistance is higher than values listed
above, remove LRU, clean bonding interfaces,
reinstall, and re-measure until half the resistance
listed above or less is reached.
4. Reconnect all disconnected harness/antenna connectors
and ensure they are secure
Repeat for each listed LRU.
Every 2000
flight hours or
ten (10) years,
whichever is
first
GA 35 GPS
Antennas
An electrical bonding test must be performed on the GA 35
Antennas.
For first GA 35 Antenna:
1. Gain access to the antenna (see General Arrangement
Drawing for location).
2. Disconnect the coaxial cable from the antenna connector.
3. Measure the resistance between the antenna base
connector and a nearby exposed portion of aircraft
structure (example: exposed rivet on fuselage stringer).
4. Verify the resistance is equal to or less than 5 milliohms.
5. Reconnect the coaxial cable to the antenna connector and
ensure it is secured.
Repeat for second GA 35 Antenna.
In the event of bonding test failure, remove antenna, clean and
re-attach using the procedures in Section 2.7.7.
Every 2000
flight hours or
ten (10) years,
whichever is
first
GTX 330D
Regulatory Testing
The GTX 330D transponders must be tested and shown to
comply with 14 CFR Part 91.411, 91.413 and Part 43 Appendix E
and F as described in section 2.5.1.
24 Calendar
Months
GTX 330D
ADS-B Out Testing
The GTX 330D transponders must be shown to comply with 14
CFR Part 91.227 as described in section 2.5.2.
Replacement of
GNS 530W or
GNS 430W
GTX 330D, and
CI 105 Antennas
A visual inspection of the GTX 330D transponders and CI 105
antennas must be performed as described in section 2.5.3.
12 Calendar
Months [1]
GTX 330D, and
CI 105 Antennas
An electrical bonding test of the GTX 330D transponders and CI
105 antennas must be performed as described in section 2.5.4.
Every 2000
flight hours or
ten (10) years,
whichever is
first
Notes: [1] Complete within the preceding 12 calendar months as part of an annual or progressive
inspection program. This inspection interval may be extended to within the preceding 24 calendar months
for aircraft that are inspected in accordance with other approved aircraft inspection programs.
(52 paginas)
(84 paginas)
Manymanuals.com
Manymanuals.de
Manymanuals.fr
Manymanuals.it
Manymanuals.pl
Manymanuals.cz
Manymanuals.es
Manymanuals-pt.com
Comentarios a estos manuales