Type Certificute

Transcription

Type Certificute

REPUBLIC OF INDONESIA
MINISTRY OF TRANSPORTATION
DIRECTORATE GENERAL OF CIVI AVIATION
ENGINE
TypeCertificute
VALIDATION
Number E 037
Thiscertificateissuedto: CFM International,S.A.
2 Boulevard du GeneralMartial Valin
75015Paris, France,
certiJiesthat the typedesignfor thefollowing productswith the operatinglimitationsand
conditionsthereforeas specifiedin the Civil AviationsSafetyRegulationsand the Type
CertiJicateData Sheet,meetsthe airworthinessrequirementsof part 33 of Civil Aviation
SafetyRegulationsfor AirworthinessStandards:Aircrafi Engines,and part 34 of Civil
Aviation SafetyRegulationsfor Fuel Ventingand ExhaustEmissionRequirements
for
TurbineEnginePoweredAirplanes.
ENGINEMODELS: CFM56-5A series
ThisCertfficate,and the TypeCertificateData Sheetwhich ispart hereof shall remainin
effect until suruendered,suspended,revoked, or a termination date ls otherwise
establishedbv Director Generalof Civil Aviation.
Dateof application : November16, 2005
: August25, 2006
Dateof issuance
On Behalf of Director Generalof Civil Aviation
Capt. CHRISTIAN BISARA
Director of Airworthiness Certiftcation
Note: The issuanceof this Type Certificateis basedon the FederalAviation AdministrationType
CertificatenumberE28NEandType CertificateDataSheetnumberE28NERevision6 , date:
S.A.
April2,1998to CFM Intemational,
REPUBLIC OF INDONESIA
MINISTRY OF TRANSPORTATION
DIRECTORATE GENERAL OF CIVIL AVIATION
No. E 037
Revision: 0
CFM INTERNATIONAL
Models: CFM56-5
CFM56-5A3
CFM56-5A.4
CFM56-5A5
cFMs6-5-AllF
CFM56-5A4/F
CFM56-5A5/F
25.2006
TYPE CERTIFICATE
DATA SHEET NO. E 037
This data sheetwhich is a part of Type Certificate Validation No. E 037 prescribesconditionsand
limitations under which the product for which the type certificate was issued meets the ainvorthiness
requirementsof the Civil Aviation SafetyRegulations.
TYPE CERTIFICATE HOLDER:
I. MODELS:
TYPE:
RATINGS (SeeNote 4)
Take-off(5 min. seeNote
16),sealevel staticthrusl lb
Maximum Continuous,
sealevel static thrust, lb.
Flat Rating
Take-off
Maximum Continuous
CFM Intemational,S.A.
2 Boulevarddu GeneralMartial Valin
75015Paris.France
cFMs6-5
cFM56-5A3
CFM56-5.AI/F
High bypassturbofan;coaxial front fanlboosterdriven by multi.
stagelow pressureturbine,multi-stagecompressor
with one-stage
high pressure
turbineandannularcombustor.
25,000/
I I,120daN
23,7001
10,540
daN
26,5001
11,787
daN
23,7001
10,540
daN
25,0001
I 1,120daN
23,7001
10,540
daN
Ambient Temoerature
86 "F/ 30 0C
77 "Fl 25 "C
86 0F/30 'C
77 "F/25 "C
86 'F/ 30 'C
"C
77 0F125
FUELSYSTEM
SeeNote7 for approvedfuels
Fuel Pump / SNECMA PN
301-78s-501-0
301-78s-501-0
(Combinedboostand single
30r-785-s02-0
30r-785-502-0
elementgear-typepump)
Hydro Mechanical Unit
(GE PN)
T C D S N o .E
: 037
RevNo. :O lDate:
1348M79P04
1348M79P06
thruP09
1348M79P04
1348M79P06
thruP09
301-785-501-0
301-785-502-0
1348M79P04
1348M79P06
thru P09
MODEL (Continued)
ELECTRONIC ENGINE
CONTROL
ElectronicControl Unit
(GE PartNumber)
IdentificationPlugs
(SNECMA PartNumber)
OIL
IGNITION SYSTEM
Ignition Unit
Unison and Simmons
Two Igniter Plugs
Unison and Champion
CFM56-5
1459M55P11
ThruPl8
1519M83P01
Thru P05
l820lvI27P0llP02
320-586-001-0
320-s86-201-0
320-586-301-0
CFM56-5,A3
CFM56-5-AI/F
1459M55P15
l459M55Pts
ThruPl8
ThruPl8
1519M83P02
1519M83P02
ThruP05
Thru P05
1820M27P01/P02 l820lvI27P0llP02
320-586-03
l-0
320-586-02r-0
320-586-23r-0
320-s86-22r-0
Synthetictype conformingto GE SpecificationD5OTFI, Type I and
Type II. CFM ServiceBulletin CFM56-5 79-001 list approvedoil
brands.
GE PafiNumber
1538M69P01
9238M66P05
9238M66P07
9238M66P08
t374Mt2P0l
l374Ml3P0l
l374Ml3P0s
1538M69P01
9238M66P05
9238M66P07
9238M66P08
l374Mt2P0l
l374Mt3P0l
1374M13P05
1538M69P01
9238M66P05
9238M66P07
9238M66P08
l374I0/4t2P0l
l374Mt3P0l
1374M13P05
PRINCIPAL DIMENSIONS Inches/ Millimeters
Length, (fan caseforward
95.3/2422
95.3/2422
95.312422
flange to LPT rear frame aft
flange)
Width, (fan casingforward
75.121
190.8
75.121
190.8
75.121
190.8
flange diameter)
Height,(bottomof accessory
82.73t2r0.r
82.7312t0.1
82.731210.1
gearboxto top offan casing
forward flanse)
Includesbasicengineaccessories
and optional equipmentas listed in
(DRY)
WETGHT
manufacturer'senginespecification,and engine-mountedportionsof
the conditionmonitoring instrumentation.
Pounds
5139
5r39
sl39
Kilograms
2331
2331
2331
CENTEROFGRAVITY
LOCATIONS
Inches
Millimeters
TCDSNo. : E037
RevNo. :O lDate:
Station,Engineonly (Referto InstallationDrawing)
206.9
!l
5255x25
206.9*l
5255+ 25
206.9
!l
5255!25
II. MODELS:
TYPE:
CFM56-5A4
RATINGS (SeeNote 4)
Take-off (5 min. seeNote
22,0001
16),sealevel staticthrust, lb.
9786daN
Maximum Continuous,
sealevel staticthrust, lb.
20,6701
Flat Rating
9195daN
Take-off
Ambient Temperature
Maximum Continuous
I 13.F/ 45 .C
77 "F/25 "C
FUEL SYSTEM
SeeNote 7 for approvedfuels
Fuel Pump/ SNECMA PN
301-785-501-0
(Combinedboostand single
301-785-502-0
Hydro MechanicalUnit
(GEPAr)
ELECTRONIC ENGINE
CONTROL
(GE PartNumbers)
Identification Plugs
(SNECMA PartNumbers)
OIL
IGNITION SYSTEM
23,500/
10,453
daN
20,670/
9195daN
98.6"F/37"C
77 "F/25 "C
301-785-501-0
301-785-502-0
1348M79P04
1348M79P06
thru P09
1348M79P04
1348M79P06
thruP09
1519M83P10
r820M27P07
l5l9M83Pl0
1820M27P07
336-414-20t-0
336-414-20s-0
336-414-220-0
336-414-225-0
Synthetictype conformingto GE SpecificationD5OTFI, Type I and
Type II. CFM Service Bulletin CFM56-5 79-001 list approvedoil
brands.
GE PartNumber
Two lgnition Units
UnisonandSimmons
ls38M69P0l
9238M66P05
9238M66P07
9238M66P08
t374Mt2P0l
t374Ml3P0t
1374M13P05
Two IgniterPlugs
UnisonandChampion
95.312422
flange to LPT rear frame aft
flange)
Width, (fan casing forward
75.121
190.8
flange diameter)
Height,(bottom of accessory
82.731210.1
gearboxto top offan casing
forward flanse)
TCDSNo. : E037
RevNo. :O lDate:A
CFM56-545
High bypassturbofan;coaxial front fanlboosterdriven by multi-stage
low pressureturbine, multi-stage compressorwith one-stagehigh
pressureturbine and annular combustor.
2006
ls38M69P0l
9238M66P0s
9238M66P07
9238M66P08
t374Mt2P0l
r374Ml3P0l
1374M13P05
9s.3/2422
75.t2tt90.8
82.7312t0.1
MODEL (Continued)
CFMs6-5A4
WETGHT(DRY)
Pounds
Kilogams
CENTER OF GRAVITY
LOCATIONS
Inches
Millimeters
206.9+ |
5255!25
cFMs6-544/r'
III. MODELS:
TYPE:
22,0001
9786daN
20,6701
9195daN
FUELSYSTEM
FuelPumpi SNECMAPAI
(Combined
boostandsingle
HydroMechanical
Unit
(GEPN)
IGNITION SYSTEM
23,5001
10,453
daN
20,6701
9195daN
301-785-501-0
301-785-502-0
301-785-501-0
301-785-502-0
1348M79P04
1348M79P06
thruP09
1348M79P04
1348M79P06
thruP09
r519M83P10
1820M27P07
1519M83P10
r820M27P07
336-414-210-0
336-414-230-0
336-414-215-0
336-414-235-0
Synthetictypeconformingto GE Specification
D5OTFI,TypeI and
TypeII. CFM ServiceBulletinCFM56-579-001listapproved
oil
brands.
GE PartNumber
Two IgnitionUnits
UnisonandSimmons
1538M69P01
9238M66P05
9238M66P07
9238M66P08
t374Ml2P0l
1374M13P01
1374M13P05
Two IgniterPlugs
UnisonandChampion
T C D S N o .E
: 037
RevNo. :O lDate:
cFM56-54.5/r'
Ambient Temperature
I 13 .F/ 45 .C
98.6"Fl 37 "C
"F|25
"C
77
77 "F/25 0C
SeeNote 7 for approvedfuels
ELECTRONIC ENGINE
CONTROL
(GE PartNumbers)
oIL
206.9+ |
5255!25
High bypassturbofan;coaxial front fan/boosterdriven by multi-stage
low pressureturbine, multi-stage compressorwith one-stagehigh
pressureturbine and annularcombustor.
RATINGS (SeeNote 4)
Take-off (5 min. seeNote
16),sealevel staticthrust,lb
Maximum Continuous,sea
level staticthrust,lb.
Flat Rating
Take-off
Maximum Continuous
IdentificationPlugs
(SNECMA PartNumbers)
CFM56-5A5
Includesbasic engineaccessories
manufacturer'senginespecification,and engine-mountedportions of
the condition monitoring instrumentation.
5139
5139
233r
2331
25,2006
1538M69P01
9238M66P05
9238M66P07
9238M66P08
l374Ml2P0r
1374M13P01
1374M13P05
MODEL (Continued)
cFM56-5A4/F
CFM56-5A5/F
95.312422
95.3/2422
flange to LPT rear frame
aft flange)
Width, (fan casing forward
75.12/190.8
75.r21190.8
flangediameter)
Height,(bottomof
82.73/210.r
82.73/210.1
accessorygearboxto top of
fan casins forward flanse)
Includesbasicengineaccessories
WETGHT(DRY)
manufacturer'senginespecification,and engine-mountedportionsof
the conditionmonitoring instrumentation.
Pounds
5r39
51 3 9
Kilosrams
2331
2331
CENTEROFGRAVITY
LOCATIONS
Inches
Millimeters
206.9! |
5255x25
CERTIFICATION BASIS
206.9+ |
5255+ 25
Pursuantto CASR 2l-29 Type Certification of Import ProductEngine
Type CertificateNo. E 037 was issuedin validation to the FAA Type
Certification to provide an appropriatelevel of safety consistentwith
IndonesianCivil Aviation SafetyRegulation.
The basis certification that was consideredapplicableto the CFM565A enginesis:
Civil Aviation SafetyRegulations(CASR) Part33, Revision 0, issued
27 December 1993 that is equivalent to FAR 14 CFR Part 33
Amendment 14. In addition, the enginesare in compliancewith the
emissionsrequirementsof CASR Part34.
IMPORT REOUIREMENTS
To be consideredeligible for installationon Republicof Indonesiaregisteredaircraft, eachengineto
be exportedto the Republic of Indonesiashall be accompaniedby Certificate of Airworthinessfor
exportnor certifying statementendorsedby the exporting cognizantCivil Airworthiness Authority,
which containsthe following language:
l. This engineconformsto its Indonesiatype design(EngineType CertificateNumber E 037) and is
in conditionfor safeoperation.
2. This enginehas been subjectedby the Manufacturerto a final operationcheck and is in proper
Stateof Airworthiness.
ReferenceCASR Section 21.500, which provides the Airworthiness acceptanceof airuaft engine
manufacturedoutsideof the Republic of Indonesiafor which an IndonesianType Certificatehasbeen
issued.
ServiceBulletin, vendormanuals,maintenancemanualsapprovedby United StateFAA are accepted
and considerablyapprovedby DGCA Indonesia.Theseapprovalspertainto the type designonly.
TCDSNo. : E037
RevNo. :O lDate:
2s,2006
NOTES
NOTE 1
TurbineExhaustGas
(T495)(SeeNote l7)
MAXIMUM PERMISSIBLETEMPERATURE
For engine configuration designated by a suffix for specific
installations(see Note I l), refer to the appropriateS.O.I. for max.
OperatingTemperatures.
As measuredby a harnessof nine thermocoupleslocated at the
secondstagelow pressureturbine vane :
CFMs6.5
Take-off (5 min.)
Maximum Continuous
Starting
- DAC In Flight
Time Temperature
Envelope
Referto model'sS.O.l
Fuel PumpInlet
Oil Supply
ContinuousOperation
Transient(15 minutes)
890.C
955 "C
725'C
CFM.TP.Ol.II
Refer to the AppropriateInstallationManual
140'c 1284"F
1550c/311'F
NOTE 2
Fuel Limits
FUEL AND OIL PRESSURELIMITS
Operation and airl gtound starting pressure limits extend from a
minimum fuel pressureof not lessthan 5.5 psia (37.9 kPa absolute)
above the true fuel vapor pressureto a maximum of 60 psig (413J
kPa gauge)for CFM56-5A, relativeto atmosphere,with vapor/ liquid
ratio of zero at all conditions.For limits. seeInstallationManual.Part
A, Section5, and
A2 throuehA5.
Oil Limits
Theminimumpressure
limit at idle is 13psid(89.6kPadifferential)
andvariesup to 45 psid(310.2kPadifferential)at cruisethrust.The
maximumpressurelimit during cold startsis 300 psid (2069kPa
differential).limited
NOTE 3
Electrical
Rotation(1)
SpeedRatio to Core
PadRating (kW)
ShearTorque(in-lb)
Max. Overhung Moment
(inJb)
Hydraulic Pump
Rotation(l)
SpeedRatio to Core
PadRating (kW)
ShearTorque(in-lb)
Max. OverhungMoment
(in-lb)
T C D S N o .E
: 037
RevNo. :O lDate:A
a Dressure-relief
valve.SeeNote l3
ACCESSORYDRIVE PROVISION
CFM56-5
ccw
0.5947
135
9,492
1,000
ccw
0.256
1,500
4,400
160
NOTE 4
Engine ratings are basedon calibratedstand performanceunder the
following conditions:
Take-off thrust is nominally independentof ambient temperature(flat
rated) up to ambienttemperatureof :
Std+ 15'C (30 oC, 86'F): CFM56-5,-5A3,& -sAl/F
Std + 30 'C (45 "C, I 13 "F): CFM56-5A4& -5A4lF
Std + 22 "C (37 oC, 98 'F): CFM56-5A5& -5A5/F
Maximum continuous is nominally independent of ambient
temperature(flat rated) up to ambient temperatureof Std + 10oC
(25"C,77'F) for all models.
Zero customerbleedand horsepowerextraction.
No scrubbingdrags.
100Yoinlet recovery.
Based on CFM Intemational referee separateflow exhaust system
with primary (core) exhaust nozzle PAI 15-25200-2014and fan
nozzlePA{ 4013356-302for all CFM56-5Aenginemodels.
NOTE 5
MAXIMUM PERMISSIBLEENGINE ROTOR SPEEDS
CFMs6-5
RPM
Low PressureRotor (Nl)
High PressureRotor (N2)
5,100
15.183
NOTE 6
MAXIMUM PERMISSIBLEAIR
MODELS)
Location
FanCorrectedSpeed
Fan Discharge
All speedsaboveminimum idle
HPC Stage5 only
All speedsaboveminimum idle
Compressor Discharge M i n i m u m i d l e t o 6 l% N l K
only
6l o/oto82.5% NIK
Above82.5%NlK
HPC Stage5 &
Compressor
DischargeCombined
Minimumidleto6l %NlK
6l o/oto82.5% NIK
Above82.5%NlK
%
100.2
105.0
BLEED EXTRACTION (ALL
Flow Limit
2%ofanairflow
l0 o/ocoreairflow
14 Yocoreairflow
Linear variation from 14 o/oto7
o/ocorc airflow
7 %ocore airflow
14 %ocoreairflow
Linear variation from 14 o/otol0
Vocorcairflow
l0 o/ocoreairflow
NOTE 7
Approvedfuel conformingto GE SpecificationD50TF2.MIL-T5624,GradesJP-4or JP-5,ASTM D 1655,JET A, Al and B are
consistentwith this GeneralElectricSpecification.
Primaryfuel is
JET A, with otherfuels listedbeingacceptable
altemates.
No fuel
control adjustmentis required when changing from primary to
altematefuels.Use of aviationgasolineis not authorized.Consult
SpecificOperating
Instructionfor additiveusage.
NOTE 8
Life limits established
for criticalrotatingandstaticcomponents
are
publishedin Chapter5 of the CFM56-5ShopManual,CFMI-TPSM.7,for theCFM56-5enginemodels.
TCDSNo. : 8037
RevNo. :O I Date:Aueust25
NOTE 9
Power setting,power checksand control of enginethrust output in all
operations are to be based on CFM Intemational engine charts
refening to fan speed.Fan speedsensorsare included in the engine
assemblyfor this purpose.
NOTE 10
The type certificate holder, CFM Intemational, S.A., is a company
establishedand jointly owned by Societe Nationale I'Etude et de
Constructionde Moteurs d'Aviation (SNECMA) of France and the
GeneralElectric Companyfor the certification, sale, and supportof
CFM56 series engines. With respect to the benefits of type
certification for production,GeneralElectric and SNECMA function
as licenseesof CFM International,S.A.
This type certification applies to engines produced in the United
Statesunder Type Certification No. E28NE. Engines of the same
model designationproducedin Franceunder Import Type Certificate
No. E29NE are identical to and fully interchangeablewith engines
producedunderthis type certificate.
Similarly, modules, assemblies,or parts produced in France are
eligible for use in engines produced under this type certificate
provided an airworthinessapproval tag, EASA Form l-Authorized
Release Certificate or JAA Form l, issued by SNECMA under
authority of EuropeanAviation Safety Agency (EASA) Production
Certificate No. FR.21G.007 is attached to each item or invoice
coveringa shipmentof similaritems(Ref. 14 CFR g 21.502).
CFM56-5EnsineModels:
Theseengines,when producedby GeneralElectric, are identified by
the serialnumberprefix "730 and732", when producedby
SNECMA, they are identifiedby the prefrx"T3l and733"
NOTE 11
The suffix may be addedto the basic engine model number on the
engine nameplate to identiff minor variations in engine
configuration,installationcomponentsor reducedratings peculiarto
aircraft installationrequirements.For example: CFM56-5xx.
Enginesthat have a suffix to the basicmodel numberare identified in
CFM Intemational Service Bulletin No. CFM56-5 72-001, and are
summarizedbelow:
(l). CFM56-5-Al, basicmodelfor Airbus A320.
NOTE 12
The minimumpermissibleidle in flight corresponds
to N2:58.8 %
(8,500rpm) which is a non-adjustable
limit, presetinto the ECU
ControlSchedule.
NOTE 13
During negative-goperationonly, it is permissibleto operatebelow
minimum oil pressure(13 psid) for a maximum of l0 seconds.See
SpecificOperatingInstruction,Section6.
TCDSNo.:E037
RevNo. :O lDate:
2
NOTE 14
The models shown on this TCDS have the following general
characteristics:
MODEL
CHARACTERISTICS
CFM56-5
Basicmodel.
CFM56-5AI/F
Same as CFM56-5 except EGT limits increased
through introduction of hot section modification.
This model was originally certified as CFM565A2, but that designation was changed at the
requestof the manufacturer.
cFM56-5A3
Sameas CFM56-5A1ff exceptfor increasedtakeoffthrust rating.
cFM56-5A4
Same as CFM56-5A3 except for reducedthrust
takeoff rating and lower EGT limits.
CFM56-5A4/F Sameas CFM56-5A4 except for increasedEGT
limits.
cFM56-5A5
Same as CFM56-5A3 except for reduced thrust
takeoff rating and lower EGT limits.
cFMs6-5As/F Sameas CFM56-5A5 except for increasedEGT
limits.
NOTE 15
All CFM56-5A FADEC series engines have been approved to
operate with certain faults present in the control system based on
satisfactionof 14 CFR $ 33 requirementsand appropriateengine
control system reliability requirements. FAA approved criteria
pertaining to dispatch and maintenancerequirements for the engine
confol systemare specifiedin GeneralElectric DocumentNo. GEK
98455 (-5A family). These documents define the dispatch able
configurationsand maximumoperatingintervals.
A control systemreliability monitoring programhas beenestablished
with CFM, as a contingency of the dispatch criteria approval, to
ensure that overall engine control system and specific component
failure rates do not exceed the maximum values permitted by the
reliability analysis.
NOTE 16
The normal5 minutestake-off rating may be extendedto l0 minutes
for engineout contingency.
NOTE T7
FortheCFM56-5A3,-5A1/F,-5A4lF& -5A5/Fseriesengines,
the
actualmaximumpermissible
takeoffredlineturbineexhaustgas
(EGT)arel5oChigherthantheindicatedEGTandmax
temperatures
continuous
EGTratingis 25oChigher.Indicated890oCEGTtakeoff
redlinecorresponds
to actualof 9l5oC,andindicated855'CEGT
maxcontinuous
EGTcorresponds
to actualof 880"C.
...END...
TCDSNo. : E.037
RevNo. :O lDate:

Type Certificute

Transcription

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