Piper PA-28-181 Archer II User manual

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Manual!
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PIPER
AIRCRAFT
CORPORATION
PA-2&TtT.
ARCHERII SECTIONT GENENAL
sEcTtoN I
GENERAL
I.I INTRODUCTION
ThisPilot'sOpcratingHandbook
is
dcsign.d
formsxirnüm
utilizgtion
asadop€raling
guide
for thcpilot.It includcsthcmatcrielrequircdto bc
furnishedto thepilot by C.A.R. 3 andFAR Part21,SubpartJ. Il also
contains
supplcmcütal
datasupplied by lheairplane
manufactu.er.
This handbookb not dcsigncdas a substitut. for adcquatcsnd
compct.nt
flightinstruction,
knowledgeofcurrentairworthinessdirectivd,
spplicablcfedcral
ai.r€gulationsoradvisorycirculars.It isnotintendedto
beaguidc forbasicflightinstructionoratraining
ma.ualandshouldnotbe
used
for operational
purposes
unlcsskeptin a currentstatus,
Assurancethat the airplaneis in an airworthy condition is thc
rcsponsibilityof th€ owne.. The pilot in commandis rcaponsiblcfor
dctcrminingthatthcsirplan€is
safe
for flight.
The
pilotisalsoresponsiblc
for remaining*ilhin theopcratinglimitatioN asoutlinedby instrument
markings,
placards,
andthishandbook.
Althoughthcarrangemcntofthis handbookis
intendedtoincreascitg
in-flight
capabilities,it shouldnotbeüscdsol.lyas
an
occasional
operating
rcf.rcnc€.
The
pilot
shouldstudythcentirehandbooktofamiliarizehimself
with the limitations,
pcrformancc,proccdures
andoperationalhandling
characteristicsof thc airplanc bcfor. flight.
Thehandbookhas
bceodividedinto numbcrcd
(srabic)
scctions,each
provided
witha
'{ingcr-tip"
tab
dividerforquickr€fercftc.Thclimitations
and emergency
proc€durcs
hav€ been placedaheadof the normal
proccdurcs,performance
and oth€rsections
to provide €asietacccssto
informationthatrnÄybcrequired
in flight.The"Emergency
Procedures"
Section
hasbeenfurnishedwith a redtab dividerro present
an instant
referenceto thesection.Provisionsfor expansion
of thehandbookhave
be€nmadebythedeliberatcomission
ofcertain
paragraph
numb€rs,figure
numbers,
itemnumbcrsand
peges
notedasb€inginrcntionallylefr
blank.
REPORT:
VF1120
t.l
ISSUED:JULY2,1979

sEcnoNr
GENERAL PIPER AIRCRAFT CORPORATION
PA-2&ItI. ARCHER II
THREE
VIEW
Figure
l-l
Min. TurningRadius
(tt.)
(frem pivolpoint10winstjp)
170.0
:10.0
t-_,'.;"..
j1-rronr,
vr-ttro ISSUED:
JULY2,1979

PIPTRAIRCRAFTCORPORATION
PA.28.I8I.ARCHERII SECTIONI
G[\ERAI,
I.3ENGINES
(a) Numbcrof Engincs
(b) EngineVanuiaclufef
(c) EngineVodel\umber
(d) TakeoffPoller
- 5MinutcLimir
(BHP)
lc) lakeofiF:n8inc
Spccd 5 Nlinule
Limir
(
RPM)
(f) \4aximum
Conrinuous
Po$er
(BHP)
(g) MäximunrConrrnuousEngine
Specd
(
RPM)
(h)
Bore
(inches)
(i) Srroke (inch€s)
l-t) Displacemenr
(cublc
inch€s)
(k) Compfc\sionRario
(l) EngrneTlpe
PROPELLERS
(a) \umbcf ol Prop.llcß
(b) Propell.rM!nulacturcr
(c) \.4odel
(d) Numb€roi Alades
(c) Prop.llc,Dianrer€f (rnches)
(l) Maximum
(ll \.4inimum
(l) I,ropellerIlpe
t titiL
AVGAS
ONI.Y
(a) Fuel
Capacir)
ltr S.
gal
)
(oral)
(b) UsableFucl
(U
S gal
)(loral)
(c) Fuel
(
1)
Minimum
Ocranc
(2) Alternale
Fuel
I
Lrconlrng
0-160A:lN4
or
o-160A.1A
l8t)
tt00
ITIJ
2650
5.t25
.1.175
-16t.0
E.5:l
Four
Cvlindcr.Direct
Dri\e,H
orizontallv
Opposed.
Air Coohd
1.7
ISSLED:JLL\'2, 1979
REVISED:
Jt \E 29,l9E4
I
l6EM8S5-0-62
2
76
50
48
100
creeno. t00Lt_
Blue
A!ralron
crade
Refer
rolareslissue
of
LJ"comrng
lnsrruciion
No. t070.
REPORT:
VA-1120
l"l

SECTIONI
Gf,NERAL PIPERAIRCRAFT
CORPORATION
PA,28-181,
ARCHf,R
rr
1.9otl,
(a) Oil Capacrly
(U.S.quaftt
(b) Oil Specification
(c) Oil ViscosillperAverageAnbient
Ternp.
for Starting
(l) Above60'F
(2)30"Fto90'F
(3) 0"Fto
70'F
(4)BelowI0'F
8
Referto laiestissue
of Lyconing Service
lnstruction
1014.
Single Multi
S.A.E.
50 S.A.E.40or
50
s.A.E.40 S.A.E..10
S.A.E.l0 S.A.E.40
or
20w_30
s.A.E.20 S.A_E.20W-to
1.11MAXIMUM WEIGHTS
REPORT:VB-1120
l-4
\ormal
2558
2550
2550
200
ISSUED:
JULY
2,
REVISf,D:
JI;LY 2l!
(a) Vaximum Rampweishr(lbs.)
(b) \,aximum
Takeoffweisht
(lbs.)
(c) MaxirnumLandingweight
(1bs.)
(d) \'IaximumWcights
in BaSSage
Compartmenr
(lbs.)
Utility
2138
2l]0
2130
I.13STANDARDAIRPLANEWEIGHTS
Rcferro Figure6-5ior lhe StandardEmptyWeigh!
andthe Useful
Load.
1919
1982

PIPER
AIRCRAFT
CORPORÄTION
PA.2&II1,
ÄRCHERII sEcTtoN
I
GENERAL
r.I5 BAGGAGESPACE
(a) Cornpartm€nr
volume(cubic feet)
(b) Entrywidth (inches)
(c) EntryHeisht (inchet
1.T?SPECIFICLOÄDINGS
(a) wine Loading (lbs.per
sq.fi.)
(b) Power
Loading
(lbs.per
hp)
22
20
15.0
t4.2
Rf,PORTT
VB-1120
l-5
ISSUED:JULY2.r979

PIPER AIRCRAFT CORPORATION
PA.28-T8T,ARCHER II sEcTtoN2 LIMITATIONS
SECTION2
LIMITATIONS
2.1GENERAL
This section
provides
rhe "FAA Approved" operatinglimitarions,
instrumentmarkings.cotor
codingandbasic
placards
necessaryfor opera-
don of theairplaneanditssysiems.
Thisairplanemustbcoperatedasanormalorutilitycat€goryairplane
in compliance
withthe operaringlimitalions
statedin theformof placards
andmarkingsandthose
given
inthissectionandthis
complelehandbook.
Limitationsassociatedwirhthoseopiionalsysrems
andequipmenr
which requirehandbooksuppienents
can be found in Section9
(Supplemen!s).
2.3AIRSPEEDLIMIlATIONS
SPEEI)
Never
ExceedSpeed
(VNE)'Do notexceed
thisspeedinanyoperation.
MaximumStructuralCruisingSpeed
(VNO)'Do notexceedthisspeedexccpt
rn
smoothairandlhenonlyuilh caurion.
KIAS
15,1
KCAS
118
ISSUED:JULY2.1979
REVISED:
JULY21.198?
l2l
REPORT:
vB-1120
125

SECTION2
LI}IITATIONS PIPER
AIRCRAFT
CORPORATION
PA-2&1ü,
ARCHERII
SPEED
Design
Maneuv€ringSpeed
(VA) - Do not
makefull or abruptcontrolmovcments
KIAS KCAS
abovethisspeed.
At2550lbs.
G.w.
At 1634lbs.G.W. I
13
89
CAUTION
Maneuveringspe€d
decrcases
atlighterwcight
astheeffcctsof aerodynamic
fotces
become
more
pronounced.
Lin€arinterpolation
may
b€
usedfor intermcdiate
g:oss
weights.
Maneuver-
ing sp€€d
shouldnot beexc€ededwhile opera-
tingin rough
air.
Maximum
FlapsExtended
Speed
(VFE)
-
Do notexceedthisspeed*ith thellaps
€xtended. 102
2.5AIRSPEED
INDICATOR
MARKINGS
MARKING
RedRadial
Line(Never Exceed)
YellowArc (Caution
Range
- Smooth
Air Only)
GreenArc (Normal
Operating
Range)
WhiteArc (FlapDown)
REPORT:
VlU20
lll
89
100
IAS
I54KTS
125KTSto
154KTS
55KTSto
I25
KTS
49KTSto
IO2
KTS
ISSUED
JULY2,1979

PIPERAIRCRAI'TCORPORÄ'I'I()N
lä-211-18t,^RCHERtl SI']CTION2
I,IN,IITATIONS
2,? POW}.:RPI,AN'I'I,IMITATIONS
1a)
Nun)bcroltingrnct
(b) linrrncManuhcturer
(c) EnrincModclNo
I
l-ycoming
O :16(lA4M or
O-:l6UA,lA with
l0-3878
(d) EnrrneOperatinS
I-imits
(1) T.rkeollP{,wer5Minulc
Lrnrt
(BIIP)
(21 Txkcoll E gineStecd 5
MinutcI-inrn
(RPM)
(-l) MaximunrConrrnuous
Power
(BHP)
(4) MaxinmmC0nlinuous
E'rgrne
Spccd
(RPMI
(5) MaximumOrl
Tcmpcrature
({t oilPrcssure
Minimum
(red
lrne)
Maximunr
(red
l,ne)
(7) FuclPrcssure
Minimum
(rcd
lrne)
Mrximünr
(rcd
line)
(8) Fucl(AVCASONLY)
(minimum
grade)
(9) Nunrberol Propellers
(
l0)I'ropcll.rManulacturer
(ll)ProfellerModcl
(
l2)PropcllerD'amcle.
I
l.l)I'lol)ellcrlnlcrxncc
(slatrc
RPM
rr m.xinrur
penni\srblc
lhrottlc
sctlrng,serlevel,
ISÄ)
IIJO
2tu)
l]8
2650
245'l:
:5 PSt
90
orlm PSI
0.5PSI
13
PSI
Iin or ltnll-
I
la M8s50 62
?6IN.
?6tN
Not
abole2340RPM
Norhcl,)w
224{)RPM
NOTE
R. f' . rl.r r.rtlJn"
rurnrc',.,n!(
n,dnr.'lli{ r. l
tr .LJIf r.',lfrLrmrnL,ttr.'!c,l
.1.'lr.
rllr
undcrnor slrnda.deordttx,ns
ISS(lnl):
JTJLY
2,1979
REVISBDTAPRIL
2'1998 vB-1120REPORT:

SECTION
2
I,IMI'TdI'IONS PIPIJR
AIRCRAI.'1'CORPORA'TI0N
PA.2II-IIiI.
ARCTIIiR
II
2.9 POWI'RP[,ANTINS'I'RTJMENT
]\TARKINCS
(!) lich(nrcter
GreenArc
(N('rmal
Openting
Rangc)
Yclk)w
Arc
(5
MrnurcLimir)
Rcd1-irc
(Takeolf
Powcr)
(b) OllTcmpcrrturc
G.cenArc
(Norm.rl
Ol'eraling
Rrngc)
RedLrne
(Miximum)
(c) oi1Prcssurc
Crccn,\rc
(NomalOperatrng
Rangc)
YellowArc
(Caulion
Range)
(Idlc)
YellowAfc(Cround warmUp)
RedL,nc
(Minimunt
Redl.ine
(Maximun)
(d) Fucl
Pressure
OrccnArc
iNormalOperating
Rangc)
Redt.'ne
(M'n'm'rm)
RedL,ne
(Mlximuul)
2.II WEIGHTLIMITS
500ro
1650
RIrNI
2650to270i)
Rl,N4
t7m RPI,I
75'
lo2.1i'l:
215"t:
60
l'SIto90l,SI
25PSI
lo60PSI
None
or90l,Sl
to100
PSI
25PSI
90
(,f
100PSI
0.5PSI
lo8PSI
0,5PSI
IIISI
(a)
(c)
Mrii,rum Rlmp (lbs.)
MaxinlunWeight
(lbs.)
MaximunrBdggrSe
(lbs
)NO,t.u
Refer ro Scction5 (Pcfionrränc.)
weightaslimrred
by
pcrlorman.c.
Nornul
255IJ
2550
200
Llnlirv
2lllJ
2ll0
0
REITORT:Vß-1120 ISSUED:
JTJLY
2,1979

PIPERATRCRAFT
CORPORATION
PA.2&TTT,ARCHER
II SECTION2 LIMITATIONS
2.I3 CENTEROFGRAYITYLIMITS
(a) NormalCategory
Weight
Pounds ForwardLimit InchesAft of Datum RearwardLimit InchesAft of Datum
2550
2050
(and
lcss)
88.6
82.0 93.0 93.0
(b) UtilityCategory
Wcight
Pounds ForwardLimit InchesAft of Datum RearwardLimit InchesAft of Datum
2130
2050
(and 83.0
82.0 93.0 93.0
NOTES
Straight
line variationbctween
poinrsgi\en.
Thedalumused
is
78.4
inchesaheadofthcwinS
leading
edgeattheinboard inrcrscctionof rh€
straightandtapered
section.
It istheresponsibilityoftheairplaneown€rand
the
pilot1o
insure
thattheairplan€is
properly
loaded.
Se€Section6
(
WeightandBalanc€)for
proper
loadinginstructions.
REPORT:VFtl20
2-5
ISSUED:JULY 2, l9?9

sDcrtoN2
LIMITATIONS PIPER ATRCRAFTCORPORATION
PA.28.ItI. ARCHER II
2.15MANEUVER
LIMITS
(a)
(b)
Normal Category
- All acrobaticmaneuvers
includingspins
prohibited.
Utility Cstcgory
-Approvcd
maneuversfor bankanglcs€xcceding
60".
SteepTurns
LazyEights
Chandelles
Entry
Speed
II3
KIAS
II3KIAS
I13KIAS
2,19TYPESOF OPERATION
The
airplan€isapproved
forthefollowing
operations
when
equippedin
accordance
with FAR 9l or FAR 135.
(a) DayV.F.R.
(b) NightV.F.R.
(c) DayI.F.R.
(d) NighrI.F.R.
(e) Non lcinS
2.I7 FLIGIIT LOAD FACTORS
(a) PositiveLoadFactor
(Maximum)
(b) Negative
LoadFactor
(Maximum)
2.2I FUEL LIMITATIONS
(a) Total Capacity
(b) UnusableFu€l
Theunusable
fuelfor ihisairplane
has
beendetermined
as1.0
gallon
in each
wingin crirical
flightattirudes.
(c) Usable
Fuel
The
usablcfu€linthis
airplane
hasbeen
determined
ar24.0
gllons ineach
wing.
REPORT:V&1120
Normal Utility
3.8G 4.4
G
No inverted
maneuvers
apProved
U,S.
CAL,
U,S.GAL.
48U.S.CAL.
50
2
ISSUED:
JULY2,
l9?9

PIPER AIRCRAFT CORPORATION
PA.2}ltI, ARCHER N SECTION
2
LIMITATTONS
2.23NOISELEVEL
Thenoisclev€l
of thisairc.aftis?3.9d B(A).
No determination has been made by the Fede.al Aviation
Administrationthat the noiselevels
of this airplsnc
ar. or shouldbe
acceptableor unacceptablcfor op.rationat,into,or out of,anyairport.
Theabovestat€ment
notwithstandingth€noiselevel
statedabovchas
beenverifiedbyandapprov.d
bytheFed€ralAviationAdministration
in
noisel€veltest flights conductcdin accordanc€with FAR 36, Noise
Standards
- AircraftTlpe andAi.worthiness
Certification.Thisaircraft
modelisin complianc€withall FAR 36
noise
standardsapplicablcto this
typ€.
REPORT:vlU20
ISSUED:JULY2.l9?9

sEcTtoN
2
LIMITATIONS PIPER AIRCRAFT CORPORATION
PA-2&161,
aRcHER II
2.25PLACARDS
ln full viewof th€pilot:
-IHIS AIRPLANE MUSTBEOPERATED
ASA NOR.
MAL OR UTILITY CATEGORYAIRPLANE IN
COM.PLIANCE WITH THE OPERATING
LIMITATIONS STATED IN THE FORM OF
PLACARDS,
MARK-INGS
AND MANUALS.
ALL MARKINGS
AND PLACARDS
ONTHISAIR.
PLANE APPLY TO ITSOPERATIONASA UTILITY
CATECORY AIRPLANE. FOR NORMAL AND
UTILITY CATECORY
OPERATION
REFER
TOTHE
PILOT'SOPERATING HANDBOOK,
NO ACROBATIC
MANEUVERS
ARE APPROVED
FORNORMAL CATEGORY
OPERATIONS,
SPINS
ARE PROHIBITED
FOR NORMAL AND UTILITY
CATEGORY.'
In full viewof the pilot:
TAKEOFF CHECK LIST
Fuelon pro!'er
tank
Electric
fuelpumpon
Engine
gauges
checked
Flap!- s€t
Carb.heat
off
Mixtures€t
Primer
locked
Fuel
on proper
tank
Mixturerich
Electricfuelpumpon
Seatbacks
erect
Seal
backserect
Fasten
belts/harn€ss
Trim ub - set
controls-free
Door - larched
Air Conditioner
off
LANDING
CHECK
LIST
Flaps
- set
Fasten
belts/harness
Air Conditioner
off
The
"AlR COND OFF" item
in the
abovetakeoff
and
landioc
check
lists
ismandarory
for air conditioned
aircraft
onlv.
REPORT:
VFU20
Lt ISSUED:
JULY2,1979

PIPER AIRCRAFT CORPORATION
PA-28-r8r,
ÄRCHERII SECTION2 LIMITATIONS
In full viewofthe
pilot,in rheareaof theairconditionercontrol
panel
wh€n
theair conditionerisinstall€dr
"WARNINC AIR CONDITIONER
MUST BEOFF
TO INSURE NORMAL TAKEOFF CLIMB PER-
FORMANCE."
Adjacentio upperdoor latchi
"ENCAGE
LATCH BEFOREFLIGHT."
On insideof thebaggagecompanmentdoor.
"BAGGACE
MAXIMUM 2OOLBS."
.UTILITY CATEGORYOPERATION - NO BAG.
GAGE OR AFT PASSENGERSALLOWED. NOR-
MAL CATEGORYOPERATION. SEE PILOT'S
OPERATING HANDBOOK WEIGHT AND BAL-
ANCE SECTION
FOR BAGGACEAND AFT PAS,
SENGER
LIMITATIONS."
In full vi€w of the piloti
"va=I
ll KIASAT
2550ä
(SEE
P.O.H.)"
.DEMO.
X-WINDI7
KTS.'
In full viewof thepilor;
'OIL COOLER WINTERIZATIOT-
PLATE TO BE
REMOVED
WHEN
AMBIENTTEMPERATURE
EX-
CEEDS50'F."
ISSUf,D:JULY 2, 1979
REVISED:JULY 21,1982 Rf,PORT: VB-1120
2-9

SECTION2
LIMITATIONS PIPER
AIRCRAFT CORPORATION
PA-28.I8I.
ÄRCHtrR
II
ln Iull\ie\\'ol the
pilor:
,LIILI]Y CATE(iORY
OPERATION
ONLY
"
d) \o AFT PASSENGERSAt_t_OWED.
{2] .\CROB,\TICVA\FUVERS ARE
LIMITf:I)
TO
THEI OLLOWI\Gi
Intull\l€$ of rhe
pilor:
.\\'AR\I\G ILR\ OFF
S]'ROBEI I'iHI S WHEN
I\ ('I.(ISI PROXI]\'JIlYTO
GROLND
OIiDTRINC
FL1(JIII THROI]CiH
CLOTJD.FOC
ORHAZE."
OnLachoüreterfa.e:
'AFIEIt
5 ltll\: Rhl)l
CEPOWER
TO:650
Rp\t -
SPI\SPROH1I]I]ED
S]FI:PII]R\S
I,\ZY EICIITS
CI]ANt)FI.I,IS
ENIRY
SPFTL)
]] KIAS
I] KIAS
I] K
IAS
ISSt:fD: JULY2.
1979
RtrvISED:
JULY 20,1983
R[I'0RTr\ B-1120
l-r0

PIPERAIRCRAFTCORPORATION
PA.28.T8I,ARCHER
NSECTION
2
LIMITATIONS
Adjacentto thefuelfiller caps:
FUEL
- 100or l00LLAVIATIONGRADE.
I.'UEI- IOO.ISO AVIATIONGRADEMIN.
USABLE
CAPACITY24
OAL.
USABLE CAPACITY TO BOTTOM OF FILLER
\ECK INDICATOR17GAL.
Adjacentro thefillercaps
(serial
numbers28-8390016
and
up)
AVGAS
GFADE
iooLl
ONLY
s
GRÄDE
roo
ISSUtrD:JULY20,1983 REPORT:
VB-I120
I

PIPERAIRCRAFT
CORPONATION SECTTON
3
PA.2&.1tI,
ARCHERII EMERGENCY
PROCEDURES
SECTION3
EMERGENCY PROCEDURES
3.I GENERAL
The recommended
proc€dures
for coping with vadous typca of
emergencies
and criticalsituations
ar€ provided by this section.
All of
required
(FAA rcgulationtemergencyprocedures
andtbosenecessary
fot
th€operation
of thcairplan. asdetermincdby theoperatinganddcsign
featurcs
of theairplancare
pr€scnted.
Emergency
procedures
associated
with those
optionalsystems
and
equipmentwhich
requirehandbook
supplem€ntsare
provided
inSection 9
(Supplemcnts).
Thefirst portion
of thisscctionconsists
ofan abbreviated
emergcncy
ch€cklist
whichsuppliesan
actionsequenc.forcritical
situations*ith littl€
emphasis
on theoperationof systems,
The r.mainder of the section
is dcvored
to amplifi€demergrncy
proccdures
containingadditional
informarion
to provide the
pilot wirha
morecompl€te
undeßtandingof theprocedures.
Thes€
procedures
aresuggested
asacourseofaction
forcopingwith
the
I
particular
conditiond€scribed,
butarenot
asubdtitur€forsound
j
udgment
and common sense.Pilors should familiarize themselves
with thel
procedures
given
in
rhhsectionand
b€
prcpared
roule approprialeaclion
snouldaneme.!en.vanse
Vo* Ur"i"-"."rg.n"y procedutcs,
such
as
power
oft landings,
area
normalpart of pilot training.Allhough these
emergencies
arediscussed
h€re.thisInformationisnolinrcndedro replacesuch
rraining.
buronlyro
provldc
a source
ol rclercnce
andreview.
andto provide
information
on
procedur€s
whicharenot rhe
samefor all aircraft.
h issuggested
thatth€
pilo! review
.standard
emergencyprocedur€s
p€riodtcally
to renrain
ISSUED:JULY2,1979
REVISED:JUNE29,l9tl REPORT:VFll20
3-l

PIPER AIRCRAFT CORPORATION
PA-2&181,ARCHER ll sEcTtoN3 EMERGENCYPROCEDURDS
3.3 EMERGENCY PROCEDURESCHECK LIST
ENGINEFIRE DURING STÄRT
Starter
,.. ..,.... ..... ... ...., crankengine
Mixtur€,.........,.. ........... idlecut-off
Throttl€.....,....,.. ................ open
Electricfuel
pump ............. ........ OFF
Fuel
selector ...,..,.................. OFF
Abandonif fir€continucs.
ENGINE POWERLOSS DURING TAKEOFF
If sufficicntrunwayrcmainsfor a normallanding,
landstraightahcad.
If insufficient
runwayremains:
Maintginsafeairspecd.
Makeonlyshallowturn to avoid obstructions.
Flapsassituationr€quires.
If sufficient
altitudehasbeen
gained
ro attempt
a restart:
Maintainsafeairspe€d.
Fu€ls€lector swtchto tank
containingfuel
Electricfuel
pump .... .. ... ... .. ,, ch€ckON
Mixture.............. ......
..,checkRICH
Carburetorh€at ......
....,.,.......... ON
Primer............... .........
,,...
locked
If power isnot regained,
proceed
with power
off landing.
ISSUED:
JULY2,1979
REVISEDT
MAY 29.l9t0 REPORT:VB-1120
3.3

SECTION3 PTPERAIRCRAFT
CORPORATTON
EMERGENCY
PROCEDURES PA-2t.IEI,
ARCHER
II
ENGINEPOWERLOSSIN FLIGHT
Fuelsclcctor switch
to tank
Erectricrüer
pump ....... ::::i':l::3il
Mixture
,,,........... ...........,...
RICH
Carburetor
heat ........
........
,,..... ON
Engine
gaugcs.
.... .,.. .. . check
forindication
primer...........,.. .:i::::::i:"'üi1T
Ifno fuel
pressure
isindicated,
checktank
selector
positionto
besur€i(is
on
a tankcontainiDgfuel.
When
pow.r i5
restored:
Carburetorhcat ,.,.......
,,......
,,.. OFF
Elcctricfuel
pump .,........ .... .... .. OFF
If power isnorrestoredprepare
for power
ott landinS.
Trim for 76KIAS
POWER
OFF LANDING
Locatcsuitable
ficld.
Establishspiral
patrern.
i000
ft.abo!cfieldat_do*nwind
posirion
for normal
landing
approach.
whcn ficldcancasily
bereached
dow to 66K|AS for shonel ünding.
Touchdowns
shouldnormally
b€
madeatlowestpossible
airspeed
wirh
full
flaps.
Whcn
commitredro landing:
lgnition
.....
,........ .....
.....,..
..
OFF
Masterswitch ..
..........
..........
.. oFF
Fuelsclcctor ..........,.......,,.....
OFF
Mixtur€
..,.......
.... ......
....idle
cut-off
S€atb€lt
andharness.
,. ....... .... .., ,.light
REPORTT
Vllr20
T4 IssUEDr
JULY
4 1979