Piper ARCHER II Pilot Operating Handbook page 229

DQ-17-005
Page: 2 of 8
Table of Contents
Table Of COntents.... cc ccccccecenneee eet e ene c ec te ee er ener Acne eee CCA EEI CREEL DEE EEEECLUEE DECC DOES OHSS EEE EERE Epo nH A ROn EEE Tad ee tae 2
1 GOT alee ccc e n e c t e e e c e s e n e e e c a e s s e s t s e e n e c n e e e e s n a e c e v e e e e a s c o n e e e n e s e n e s e s s n e s e s e c n e e a n s s e s s a n e n a e s u n e v s t e n s a e s n e n i r e n e e s 2
2 LIMITATIONS oe le cate e tec cenee tenses teeereecnecaeen ens eeneeeeeresieeneeneeenesnteeneterersdenneseeetereessenesennesieriagenaee 5
3 Abnormal / Emergency Procedures o o . . . c c c e c c c c c s s c c e e s e r e c e e c e n e n s n e r e e e r e n e e a n e e c r n e e e r t n e t a n e t e e s e a e s e i n e a n e a g s 6
4 Normal Procedures... ccscccecssccsscsseersensrsrenecsseeestecsereeeeesereeasesssereneesnesieasseaeasenasiesecerasietereeres 7
5 POHOPMANCE icc ne ES USERS EOE E EEC er CIEE SOR CC nH Onde Eeadee 7
6 Weight and Balance/Equipment List .... ccc ccecseceesseercertrertenseeseenteseneeesiaeeecadessnnesesiescaey 7
7 SySteM DeSCTIPLIONS oe eccc ce ccc ete ete cnee ener nce Deer UE ERE Erne ETE E rand C cord anne Aco nee pda etredeepaneseautecaaes 8
8 Handling, Servicing and Maintenance... c c e c e n e e c e e c t r e t i e e t c e e t n e r s c s n e s t i i a e a t i n e e c e n i e r e n i e s e a g e s 8
3 SUPPIOMENES.....c cee cesecccsesensseserereeseseeeseeeeeeeeceaseeseeeeeCUeCHeEFOOEE DOE DIEESSEOED LOMAS ECEES HEEL Cen ueeateevaaes 8
10 Safety INPOPM Aton... ccc eter eee nee een OEE OnE COLES COUPE rnE EEE OE DEy OnE e erp S Pree Eco nara de teaaee 8
Amendment record
Issue Reason for Issue DQ reference
1 Initial issue -
Updated text per meeting with the CAA 11-120
3 Document updated to the GAEL template. 14.263
Pilot's Guide: 190-00356-00 updated to Rev J
4 GNS-W is the RNAV primary system and TAW-B capability. 15-076
5 Updates per feedback from EASA 15-140
6 Typo correction page 5. Updated table in 1.2 for TAWS-B 15-183
paragraph references.
7 Updated requirements for remote annunciation. 16-022
8 Amend second Comm and Nav/GPS requirements in 1.1. Add 17-005
ADF and alternate equipment requirements in section 2.3
1 General
1.1. The aircraft is installed with a Garmin GPS, navigation/communication unit in the number one
| system position. A second VHF navigation or certified GPS system is installed in the number
two system position. Garmin units approved within this supplement are: GNS430W,
GNS430AW, GNS530W, GNS5S30AW, GNS530W-TAWS & GNSS30AW-TAWS (hereafter
referred to as the GNS-W).
GPS system status is via the annunciators built-in to the GNS-W unit, unless an MD41-14xx
GPS Annunciation Unit is required due to the position of the GNS-W falling outside the 'Normal'
or 'Primary Maximum' field of view. Alternatively, the aircraft may be equipped with an EFIS
HSI containing the required GPS annunciators.
The GNS-W is a fully integrated panel mounted unit, which contains a VHF communications
transceiver, a VOR/ILS receiver, and a Global Positioning System (GPS) and a navigation
computer.
The GNS-W has Receiver Autonomous Integrity Monitoring (RAIM) to assess the integrity of
Global Positioning System (GPS) signals. RAIM ensures that the available satellite geometry
will allow the receiver to calculate a position within a specified protection limit:
. 4 NM for oceanic
. 2 NM for en route
. 1 NM for terminal
. 0.3 NM for non-precision approaches
DF 2¢
& Copyright Gama Aviation (Engineering) Lid