Super Ximango AMT 200S Technical specifications

· AMT200S ..
FLIG HTMAN UAL
200-24
PR-AMW
N/S 200.175
N175XS

SECTION:O
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GRUPO AEROMOT
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FLIGHT MANUAL
AMT200S
. .
UNITED STATES MOTORGLIDER FLIGHT MANUAL
THIS MANUAL IS
APPROVED IN ACCORDANCE WITH FAR 21.29 FOR U,S.
REGISTERED AIRCRAFT
ANDIS APPROVED BY THE.CTA ON BEHALF OF THE
FEDERALAVIATIONADMINISTRATiON.
THIS MANUAL ISAPPLICABLETO SUPERXIMANGO MOTORGLIDERAMT-200 S,
MODEL: AMT-200S
SERIALNUMBER: 200.175
-'--~~~--,-~~~~--'--'~~~~~~~--'--
REGISTRATION: PR-AMW
----"....:...;:..;=--==~~~~---'-~~---'-~~~~~~~~-
MANUFACTURER: AEROMOT INDUSTRIA MECANICO METALURGICA LTDA.
AV. DASINDUSTRJAS,
1210' .
90200,-290 -PORTO ALEGRE- RS- BRASIL .
CTAAPPROVAL: ---'--j-----,""--'ll------------------------
(
JOst U!ll «. BHDfUAlN·r.n. Uil,_,.
Cnefe do FDH
DATE OF APPR()VAL:_~_r_e._f_T .... ·~-l'J'-B---'-'2.-R.-'..l'-5-". { .... ' ...... ~_<;:_.&eo_._.-'--. --
..
Page O,OIAppr"
Effectiveness -June 26, 2000

SECTION 0
INDEX
FLIGHTMANUAL
AMT 2005 SECTION: 0
PAGE
Approval 0.0
Index , ; 0.1
Ust of Effective Pages ' : · ;.: 0.5
Record of Revisions ;., 0.7
SECTION 1 - GENERAL
1.1 Introduction 1.1
1.2 Certification Basis :: : ' : ,' 1.2
1.3 Warnings, Cautions and Notes :1.3
1.4 MotorgliderThreeViewDrawing , : 1.4
1.5 Aircraft Recorc;ls ~ : : 1.5
1'.6, Definitions , : .' 1.5
. A AirspeedTerminology 1.5
8., WeightTerminology : ' : 1.6
SECTION 2, -LIMITATIONS
,
2.1
2.2
2.3
2.4
2.5
2.6
2.7
2.8
2.9
2.10
-2.11
2.12
2.13
2.14
I
Introduction : ; 2.1
.lndicatedAirspeeds : , , 2.1
Airspeed'lndicatorMarkings .: ; 2.1
Power Plant, Fuel, and oillirilitations 2.2
Power'Plarit Im;trumentMarkings 2.3
Weight Limitations : ; 2.4
Center of Gravity ,' :2.4
Approved Maneuvers ; ' ' 2.4
Maneuvering Load Factors ;; 2.5
Flight Crew : .1. ~ '2.5
Kinds of Operation :2.5
Mini'mum Equipment ' ; 2.5
Other Limitations · : : · 2.5
Placards ~ , .. 2 6
2.14.1 Inside Placards : .. : : ,. : ; 2.11
2.14.2 Outside Placards : ; : 2.24
SECTION 3 - EMERGENCY PROCEDURES
3.1 Introduction ' ; ~ 3.1.
3.2 CanopyJettison ; , ; : ' .. ; 3.1
3.3 Emergency Bail Out : 3.1
3.4 Stall Recovery ; , :3.1 .
3.5 Spin Recovery \3.2
3.6 Eng.ine Failure :;.: , ; ;
3.2
AFM -200-24-FAA
Page 0.1
July 17,2007 -Rev. 14

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FLIGHT MANUAL
AMT 2005 SECTION:0
AFM -200-24-FAA
SECTION 3 - EMERGENCY PROCEDURES
3.6.1 Engine Failure Prior to Take OFF 3:2
3.6.2 Engine Failure After Take OFF , .. , , 3.2
3.7 Fire , ' : 3.3
3.7.1 .Engine Fire : , ; 3.3
3.7.2 Electrical Fire ,
.' : : 3.3
3.8 Other Emergencies ; : 3.3
3.8.1 Engine InoperativeLanding
~ ; : : 3.3
3.8.2 Water Landing : : :.,
3.4
3.8.3 Low Voltage Warning Light ON : 3.4
3.8.4 StarterEngaged Warning Light ON 3.4
3.8.5 IrregularEngineOperation ;: : : 3.5
3.8.6 Engine Parameters Out
of Normal Operational Ranges 3.5
3.8.6.1 High Oil Pressure , , 3.5
3.8.6.2 Low Oil Pressure , : 3.5
3.8.6.3 Battery Discharge Indication : :
'., 3.5
3.8.6.4 High Oil Temperature "
3~5
3.8.6.5 High Cylinder HeadTemperature 3.6.
3.8~6.6 Abnormal Raise of Engine Speed (RPM) , 3.6
3.8.6.7 Low ethylene glycol level Indication 3.6
SECTION 4 - NORMAL PROCEDURES
,,
4.1 Introduction , ~ : 4.1
4.2 External Inspection , , : 4.1
.'4.2.1 Left Wing : : 4.1
4.2.2 Fuselage ~ Front " : : , --:., 4.1 .
4.2.3 'Right Wing .- : , , 4:2
4.2.4 Fuselage -Rear : ; ; 4.2
4.2.5 Canopy
.. ' :: 4.2
4.3 'Cabin Inspection ,4.2
4.4 Before
~rigine Start 4 .. 3
4.5 Engine Start , , , : 4.3
4.6 Taxiing , : : , 4.4
4.7 Normal Flight ;
4.4' .
4.7.1 Prior to Take
Off 4.4
4.7.2 Take
Off and climb :4.5
4.7.3 Cruise , , :
,· 4.5
4.7.4 .
In Flight Shut Down ' : 4.6
4.7.5
In Flight Engine Start : ; : 4.6 A
4.7.6 In Fliight Engine StartUsing Wind Milling Start , : ; 4.7
4.7.7 Descent With Engine Running :4.7
4.7.8 Approach
and Landing ;. : : / 4.7
4.7.9 Landing Gear Warning System ;
4.8
4.7.10 AfterLanding , , , ; : 4.8
4.7.11 Engine shut down , :
4~8
Page 0.2
October 22, 2004 -Rev. 8

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~XIMANGO=~'" .
FLIGHT MANUAL
AMT 200S SECTION:0
SECTION 5 - PERFORMANCE
.5.1 .Introduction ; : · , .. : 5.1
5.2 Approved Data ~ 5.1
5.2.1' Airspeed correction ' , 5.1
5.2.2 Stall speed at 18741b (850 kg) .. , ~ : : 5.2
5.2.3 'Take-Off Distance ;: -
.. 5.2
5.2.4 Take-OffDistance Variati9n With Altitude and Temperature : ; .. 5.2
5.3 ,Additional Information 5.3
5.3.1 Soaring Performance ; : 5.3
5.3\2' Cruise Flight -Cruise Fuel Consumption ;5.3
5.3.3 Climb ; , · 5.3
5.3.4 Crosswind Landing
~ ;5.3
5.3.5 Spoiler Operation Near
VN~ :, ~ 5.3
5.4 Flight Polar ',
.' 5.4
.,
SECTION 6- WEIGHTAND BALANCE '
6;1 Introduction , ; : ; 6.l
6..2. Center of Gravity (C.G.) Determination : : 6.1
6.2.1 Weighing ; : ; ;, : 6.1
6.2.2 ,Arithmetical calculation 6.2
6.2.3 Calculation Table : ;
.- 6.4
6.3 C.G. Envelope : , , 6.5
.6.4 .List of appr6vedequipm~nt : : 6:6
6.5 Optional Equipment List , , 6.7
SECTION'7' -DESCRIPTION
7.1 Introduction \ ~: ' : ~ , : 7.1·
7;2 Basic Dimensions 7.1
7.2.'1 Wings : : , 7.1
7.2.2 AHerons : , · : 7.1
7.2.3 Spoilers , .- 7.1
7.2.4 HorizontalStabiliter : 7.1
7.2.5 Verticalempennage ; : : 7.2
'7.3, LandingGear ;·7.2 .
7.3.1 Description· : \ 7.2
7.3.2 Landing GearOperation
.. , : , : 7.2
7.3.3 Brake System ~ :7.3
7.4 Power Plant 7.4
7.5 Propeller :: : , 7.5
7.6 Fuel·System·...•
~ , : 7.5
7.7 Cockpit
~ ;.; 7.6
7.8 Seat Belts : ; : ,.7.6
.)
AFM~-200-24-FAA
Page 0.3 .
October 22,2004 - Rev. 8

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FLIGHTMANUAL
AMT 200S SECTION:0
Introduction .
Schedubed Maintenance . . ,
8.1
Prior to firstflight ofthe d~;::::::::::::::::::::::::.::::::::::::::· · .. · · 8.1
Ground Handl"ing :............... . 8.1
, : "- 8.1
SECTION 7 -' DESCRIPTION
7.9 Air pressure ports .
7.10 InstrumentF:anel............. .7.6
7.11 "Electrical Circuit # •••••••••••••••••••••••••••••••••••••••••••• : ••••••••••••••••••••••••••••••••••••••••••• 7.7
..................................................../ / : ' ;· ;7.14
SECTION 8 - MAINTENANCE .
8.1
8.2
'8.3
8.4
\
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July 17, 2007 -Rev. 14 AFM -200-24- FAA

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AMT 2005 SECTION:a
REVISION
3- EMERGENCYPROCEDURES
4- NORMALPROCEDURES
5- PERFORMANCE
6- WEIGHTANDBALANCE
7- DESCRIPTION
B- MAINTENANOE
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AFM-200-24-FM

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FLIGHT·MANUAL
AMT 2005 SECTION: a
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.. RECORD OF REVISIONS
November 23, 2000
CTA
·iJ'.··.·.
••
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DATE
,
Aygust25,2000
DESCRIPTION OF REVISION
Revisionadded
Placard (40) added
Caution revised anditem4.7.7added
Revisionadded
Revision ~gure 2.3
. Instrumentpaneldrawingadded
RevisionPlacards(14), (16), (18),(36)
.(37), (38) and (39)
. '. .
Placards added(40),(41) and (42)
RevisionOutsid~ Placard (9) .
Outside Placardsadded (12), (13) and(14)
In flightenginestartrevised
Instrumentpaneldrawingadded
Added,of optional electrical circuit
4.6
7:7
7.12
REVISED
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0.5, 0.6,0.7
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4.5,4,6,4:7,4.8
2.8, 2.9, 2.12, 2.13
2
. REVISION'
No.
30.5, 0.7
2.2 Revision added
Revision item 2.4"
January,29,2001
..
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AFM -200-24 ·FAA
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Ja~uary 29,2001 -Rev. 3

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AMT 2005 SECTION:O
RECORDOFREVISIONS'
,.-
REVISION REVISED DESCRIPTIONOF REVISION
CTA
No. PAGES DATE SIGN
'4
0.1,0.4 Indexrevised
0.5, 0.6, 0.8 Revision added
2.5 Reyisionitem(2.10)
2.7 Instrumentpaneldrawingadded
'2.11 Placardsadded
(21 A)
2.12,2.15,2.16
Placards added(25A), (43), (44) (45), 'July 26, 2001
and (46)
10
6.6 Listof approvedequipmentrevised
,7.7 Notes added
7.8 Instrumentpaneldrawin,gadded
7.9 Item (43.;44,45,46,47,48) added'
50,2 Indexrevised
0.5,0.6, 0.8 Revisionadded
2.10 Revision InsidePlacard (15)
2.12 PlaCards added (25B) and (25C)
2.13
Placard!;> added (30A) and (32A),
~I
2.19 Placard ad,ded (15)
3.3 ,
Revision item(3.7.1:)
3.6 Item 3.8.6.5revised, item 3.8.6.7 added Mar08,2002
6.6 'Listof approvedequipmentrevised
6.7 Optional equipmentlistrevised
7.8 Instrumentpaneldrawingrevised
7.9 '
~ Item (48,49,50,51)added
7.10
to 7.16 Revisedelect(ical circuit
'"
60.5, 0.6, 0.8 Revision added "
2.7 Instrumentpaneldrawingadded
2.B; 2.12, 2.13 Placardsadded (5-A),(25-D),(30-B), (32-B)'
-1P'
2.16,2.19 Placardsadded (45~B),(47),(48) and (11-A)
.. \~\ ,
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7.9 Item (52)
addedahd Itern(32,47)reviSed
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7.11,'7.16 Revi.sed electrical circuit
~age 0.8 "Appr"
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FLIGHT MANUAL
AMT 200S SECTION:0
REVISION REVISED DESCRIPTION OF REVISION CTA
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: AND DATE DATE SIGN
0.5.0.6
Revision ofEffectivepages
·0.9
Revision n° "7'i added ,
2.2 Item (2.4) revised 7
2.6 Instrumentpaneldrawing
revised·
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£1
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~
August 22, 2002 4.2 Item (4.2.2) revised
.~I".
5.2 Item (5.2.4)tablerevised
\fO
5.3 Items (5.3.1) and (5.3.3) revised Q\
7.1, 7:2 and 7.4 Items (7.2), (7.2.1), (7.2.2), (7.3.1)
and(7.4) revised
7.7 Instrumentpaneldrawingrevised
7.17,7.18 Electrical circuit added .
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-October Ol, 2002 -Rev. 7

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FLIGHTMANUAL
AMT 2005 SECTION:0
.DESCRIPTION:
This page introducesthe Revision n° 8of FLiGHTMANUAL PIN 200-24 ..
REASON: .
Textcorrections andrevision of instrumentpanel configuration.
REVISEDPAGES: .
0.1 to 0.6, 0.10,1.1,1.5, 1.6, 2.1to 2.5, 2.8 to 2.22,. 3;1 to 3.6, 4.1 to 4.8; 5.2, 5.3,6.1 to 6.7, 7.1 to 7.20
and 8.1.
CTAAPPROVAL: .
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.................. - .... e,£J.
N~me~
cU.uI:Jio 1NIOI8IMl· .:C4l, ....
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October 22, 2004 -Hev. B . AFM -200-24-FAA

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RECORDOFREVISIONS
.FLIGHTMANUAL
AMT 200S' SECTION: 0
DESCRIPTION:
This page introducesthe Revision
n° 9of FLIGHT MANUALP/N200-24.
REASON:
Text correctionsandrevision ofinstrumentpanel configuration.
REVISED PAGES:
0.1,0.5,0.6,0.11,0.12, 2.9 to 2.22, 6.6, 7.9
CTAAPPROVAL:
Date:
Name/Signature: .
CLAUDIO PASSOS StMAO
Ten. Cel. Eng.
Cnlf.,CTAI",'OAYC
'Page 0.11 "Appr"
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GRUPO AEROMOT
RECORD OF REVISIONS
FLIGHTMANUAL
AMT 2005 -SECTION:°-
DESCRIPTION: .
This page introduces the Revision n° 10.of FLIGHT MANUAL PIN 200-24. ~
REASON:
Revision ofinstrumentpanelconfigurationand instrumentpanel newconfiguration drawing added. '
REVISEDPAGES:
0.1,004,0.5, 0.8,0.12, 2,9 t6 2.24, 7.9 to 7.20
/ooe tZ CJIJ,J
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Name/Signature:
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AFM -200-24-FAA

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.FLIGHTMANUAL
AMT2005 SECTION: °
DESCRIPTION:
This page introduces the Revisionn° 11 of FLIGHTMANUAL PIN 200-24.
REASON:
Revision ofinstrumentpanel configuration and instrumentpanel newconfiguration drawing added.
REVISEDPAGES:
0.1,0.4,0.5,0.6,0.13, 0.14, 2~2, 2.3, 2.10, 2.16 to 2.18, 2.21 to 2:25,6,7,7.4,7.11 to 7.22
10 tJC.T ZOtJS-
Date:
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AMT 2005 SECTION:0
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DESCRIPTION:
This paQe introduces the Revision n° 12of FLIGHT MANUAL PIN 200-24 ..
REAsON: ..
Revision ofinstrument panel configuration arid instrument panel new configuration drawingadded.
REVISED PAGES:
0.5.0.6,0:14,2.11 to 2.26,6.7,7.11.7.12
CTAApproval on behalf of FAA - USA
Sebast:o~ G. '1 Gavali
.. len ~ ...... '
Chefe 9!J CAvC
Page O.14"Appr"
AFM -200·24 FAA.

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FLIGHT MANUAL
AMT 2005 .SECTION: 0
DESCRIPTION:
Thispage introduces.theRevision n° 13 of FLIGHT MANUAL PIN 200-24.
REASON:.
.Adding new model ofthe Rotax Engine;
Revisingprocedure oftemperature
in the head ofthe cylinder;
Revisingapprovedequipment
list;' .
,
REviSEDPAGES:
0.5, 0.6; 0.15, 0.16,2.2, 2.3, 2.24, 2.25; 3.6,6.6, 7.4
Date:
Name/Signature:
enuj' /\.n,/"tHG da S1 va /
Coonkn~v~ll ~:1!~~> '.llt~Jmo
. ANACApproval on b~~t JOAA.o+,~USAhtice;
Page 0.15 "Appr"l
AFM •200-24- FAA

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RECORD OFREVIS'IONS
FLIGHT MANUAL
.AMT200S, SECTION: 0
,I .
DESCRIPTION:
This page introduces the Revision n? 14 of FLIGHT MANUAL PIN 200-24.
REASON:
Revision of instrumentpanel configuration and instrument panelnew 'configuration drawingadded;
Revising approvedequipmentlist;
Electrical
drcuit added;
REVISED PAGES:
0.1, 0.4, 0.5,0.6, 0.16, 2.11, 2.17 to 2.23, 6.7, 7.9, 7.10, 7.12 to 7.22
,Date: .
.Name/Signature: .
ANACApproval on behalf.
of FAA - USA
i
AFM -200-24- FAA
Page 0.16
IAppr"

SECTION: 1
. ~. . . . FLIGHTMANUAL
";"XIM¥if;-O=.;s' " AMT200S
SECTION 1 - GENERAL
.The AMT 2008 isatWoplace(sidebyside) motorglider with a IT' taildesign. Itisequipped
with retractable main landing gear
and airbrakes on the upperwingsuiiace. Italso has
.removablewinglets, asoptionalequipment. "< • .". •
Thefuselageisa.sandwichtypeconstructionwithfiberglass, epoxyresin andPVCfoam: Th.e
wing isdividedintotwoparts-:theinnerwingisfixed andthe outerwingisfbldable.Bothwings
have"I" -shapedspars.Theinnerwing sparisasandwichtypeconstruction withfiberglass,
.carbonfiberand PVC foam. The o\,Jter wingspi:uis alsoasandwichtypeconstruction with
fiberglass,epoxy resin and PVCfoam.
I• Thismotorglideris designedforsoaring andtraining.
\
AFM -200-24-FAA
Page 1.1
October 22,2004 - Rev.S

~'"
~
GRUPOAEROMOT
FLIGHTMANUAL
AMT 2005 SECTION: 1
1.2 CertificationBasis
FederalAviation Regulattons (FAR) Part 21 includingAmendmentsthrough 21 ,,68, Sections
21.17,21.29 and 21.50 '. , , '
,
JointAirworthiness requirementsforsailplanes and powered sailplanes, JAR-22Amend-
ment2eftective Sept. 13,1982,
plLiS thefollowing paragraphs of JAR 22Change4:
.... -. -
22.1
,22.175
22.395 '
22.397
22.411
22.441
22.443
22.477
,22.483
_22.591
22.785
.~ 22]86
22.857
22.925
"22.1529
22.1581
Applicability, Amdt 22/85/1 eft. Dec12,1985 "
Demonstration ofstaticlongitudinalstability, Amdt 22/8511 eft. Dec 12,1985
Control system loads
Amdt 22/85/1 eft. Dec 12,1985. '
Loads resulting from limitpilotforces, Amdt 22/85/teft. Dec 12,1985
Control systemstiftnessand stretch, Amdt22/84/1eft. Dec 14,1984
Manellveringload, Arndt22/86/1 eft. Oct22,1986
Gustloads, Amdt 22/86/1 eft. Oct22,1986
Landing geararrangement, Amdt 22/86/1 eft. Oct22,1986
One-wheellanding, Amdt22/86/1 eft.'Oct22,1986
Rigging aridde-rigging IQads, Amdt 22/86/1 eft. Oct22,1986
Seatsand safetyharnesses,Amdt. 22/86/1 eft. Oct22,1986
,'
Protectionfrom injury, Amdt 22/86/1 eft. Oct22 ,1986
Electricalbonding, Amdt22/86/1 eft. Oct22,1986
PropellerClearance, Amdt 22/85/1 eft: Dec 12,'1985
MaintenanceManual, Amdt22/84/1 eft. Dec
14,1984.
,FlightManual.;general,Amdt22/86/1 eft. Oct22,1986
,
Plusthe following paragraphsto be incorporated in Change5
,.
22.375
22.221
22.779
Winglets, Arndt 2,2/90/1 eft~ June30,1990 ' '
Spinning-general,Amdt22/90/1 eft. June30;1990
Motion and eftectofcockpitcontrols, Amdt22/90/1 eft. June30,1990
Plusthefollowing requirementsfrom FAAadvisorycircular21.17.;2,datedJuly13,1989:
JAR 22.177(b)
,JAR 22.777
JAR22~903(b)
JAR 22.1093
FAR 23.1153
JAR 22.1555
including AC 21.17-2PAR
6;c~(6)(i)(A),(B),(C) and (D)
including AC 21.17-2PAR6.c.(7)(i)(A),(B),(C) and
(D)
including AC 21.17-2 PAR6.c. (7) (iii) ,
including AC 21.17-2 PAR6.c.(7)(iv)
including AC 21.17-2PAR6.c.(7)(vi)
including AC21.17-2
PAR 6.G.(7)(vii)
.'..-
Plusthe special condition establishedin letternumber 54085 SFAT rrC;issued by DGAC
.and dated
Oct 15,1984, to provideadditional requirementsfor composites.
Exemption from
F~R 45.11 (a) and (d) as specified in exemption number 4988 (external
',marking of gliders):' .
Page 12
Effectiveness -June 26, 2000 AFM -200-24 -F.M