Piper ARCHER III Pilot Operating Handbook page 21

PA-28-181, ARCHER III
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1.17 BAGGAGE SPACE
(a) Compartment Volume (cubic feet)
(b) Entry Width (inches)
(c) Entry Height (inches)
1.19 SPECIFIC LOADINGS
(a)
Wing Loading (lbs. per sq.
(h)
Power Loading
1.21 G 1000 GNSS (GPS/SBAS) NAVIGATION SYSTEM EQUIPMENT
APPROVALS
The Garmin G l 000 Integrated Avionics GNSS long range navigation system
installed in this airplane is a OPS system with a Satellite Based Augmentation
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System (SBAS) comprised of two TSO -Cl45d Class 3 approved Garmin GIA
64Ws, TSO-C146d Class 3 approved Garmin GDU Display Units (1050 and
1054), and two Garmin-approved GA36 GPS/SBAS antennas (one is a GA37 if
optional GIJL
version. The Garmin GNSS navigation system in this aircraft is installed in
accordance with AC 20-138D. When all the equipment is operative, the Garmin
G 1000 system has two independent GNSS long-range navigation systems.
Failure of any of the above equipment or the posting of 'BOTH ON GPS I' or
'BOTH ON GPS2' annunciators indicate only one operational GNSS system.
The Garmin G 1000 Integrated Avionics GNSS navigation system as installed
in this airplane complies with the requirements of AC 20-138D and has
airworthiness approval for navigation using GPS and GPS/SBAS (within the
coverage of a Satellite Based Augmentation System complying with TCAO
Annex I 0) for IFR en-route, terminal area, non-precision approach, and
approach procedures with vertical guidance operations.
•
The Garmin GJOO0 Integrated Avionics GNSS navigation system as installed
in this airplane complies with the equipment, performance, and functional
requirements established for the following navigation specifications.
ISSUED: December 22, 2017
REVISED: June 17, 2019
(lbs. hp)
per
69
is installed), and GPS software version 5.1 or later approved
ft.)
SECTION 1
GENERAL
24
22
20
15.0
14.2
REPORT: VB-2749
1-7