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KEMENTERIAN PERHUBUNGAN
DIREKTORAT JENDERAL PERHUBUNGAN UDARA
PERATURAN DIREKTUR JENDERAL PERHUBUNGAN UDARA
NOMOR : KP 223 TAHUN 2017
TENTANG
PETUNJUK TEKNIS PERATURAN KESELAMATAN PENERBANGAN SIPIL BAGIAN
8900-4.10 (STAFFINSTRUCTION 8900-4.10) TENTANG PENERBITAN DANPENGAWASAN UNTUK OTORISASI REDUCED VERTICAL SEPARATION MINIMUM
(RVSM) (ISSUANCEAND SURVEILLANCE FOR REDUCED VERTICAL SEPARATIONMINIMUM (RVSM) AUTHORIZATIONS)
DENGAN RAHMAT TUHAN YANG MAHA ESA
DIREKTUR JENDERAL PERHUBUNGAN UDARA,
Menimbang : a. bahwa dalam rangka mengatur mengenai penerbitandan pengawasan untuk otorisasi Reduced VerticalSeparation Minimum (RVSM), telah ditetapkan Peraturan
Direktur Jenderal Perhubungan Udara Nomor KP 274Tahun 2015 tentang Petunjuk Teknis PeraturanKeselamatan Penerbangan Sipil Bagian 8900-4.10
tentang Penerbitan Dan Pengawasan Untuk OtoritasiRVSM (SI 8900-4.10 Issuance And Surveillance ForReduced Vertical Separation Minimums Authorizations);
b. bahwa untuk melakukan pembaruan sesuai denganstandar internasional penerbangan sipil, perlu dilakukan
pencabutan terhadap Peraturan Direktur JenderalPerhubungan Udara Nomor KP 274 Tahun 2015 tentang
Petunjuk Teknis Peraturan Keselamatan Penerbangan
Sipil Bagian 8900-4.10 tentang Penerbitan Dan
Pengawasan Untuk Otoritasi RVSM (SI 8900-4.10Issuance And Surveillance For Reduced Vertical
Separation Minimums Authorizations) untuk
menyesuaikan dengan perubahan Staff Instruction CASRdimaksud;
c. bahwa untuk melaksanakan ketentuan sebagaimana
dimaksud pada huruf a dan huruf b, perlu menetapkanPeraturan Direktur Jenderal Perhubungan Udara
tentang Petunjuk Teknis Peraturan KeselamatanPenerbangan Sipil Bagian 8900-4.10 (Staff Instruction8900-4.10) Tentang Penerbitan Dan Pengawasan UntukOtorisasi Reduced Vertical Separation Minimum (RVSM)(Issuance And Surveillance For Reduced VerticalSeparation Minimum (RVSM)Authorizations);
Mengingat 1. Undang-Undang Nomor 1 Tahun 2009 tentangPenerbangan (Lembaran Negara Republik IndonesiaTahun 2009 Nomor 1, Tambahan Lembaran NegaraRepublik Indonesia Nomor 4956);
2. Peraturan Presiden Nomor 7 Tahun 2015 tentangOrganisasi Kementerian Negara (Lembaran NegaraRepublik Indonesia Tahun 2015 Nomor 8);
3. Peraturan Presiden Nomor 40 Tahun 2015 tentangKementerian Perhubungan (Lembaran Negara RepublikIndonesia Tahun 2015 Nomor 75);
4. Peraturan Menteri Perhubungan Nomor PM 28 Tahun2013 tentang Peraturan Keselamatan Penerbangan SipilBagian 121 (Civil Aviation Safety Regulation Part 121)Tentang Persyaratan-Persyaratan Sertifikasi Dan OperasiBagi Perusahaan Angkutan Udara Yang MelakukanPenerbangan Dalam Negeri, Internasional Dan AngkutanUdara Niaga Tidak Berjadwal (Certification And OperatingRequirements: Domestic, Flag, and Supplemental AirCarriers) sebagaimana telah diubah terakhir denganPeraturan Menteri Perhubungan Nomor PM 41 Tahun2016;
5. Peraturan Menteri Perhubungan Nomor PM 59 Tahun2015 tentang Kriteria, Tugas dan Wewenang InspekturPenerbangan sebagaimana telah diubah terakhir denganPeraturan Menteri Perhubungan Nomor PM 142 Tahun2016;
6. Peraturan Menteri Perhubungan Nomor PM 94 Tahun2015 tentang Peraturan Keselamatan Penerbangan SipilBagian 91 (Civil Aviation Safety Regulation Part 91)Tentang Pengoperasian Pesawat Udara (GeneralOperating And Flight Rules);
7. Peraturan Menteri Perhubungan Nomor PM 189 Tahun2015 tentang Organisasi dan Tata Kerja KementerianPerhubungan sebagaimana telah diubah terakhir denganPeraturan Menteri Perhubungan Nomor PM 86 Tahun2016;
MEMUTUSKAN
Menetapkan : PERATURAN DIREKTUR JENDERAL PERHUBUNGAN UDARATENTANG PETUNJUK TEKNIS PERATURAN KESELAMATAN
PENERBANGAN SIPIL BAGIAN 8900-4.10 (STAFF
INSTRUCTION 8900-4.10) TENTANG PENERBITAN DAN
PENGAWASAN UNTUK OTORISASI REDUCED VERTICAL
SEPARATION MINIMUM (RVSM) (ISSUANCE ANDSURVEILLANCE FOR REDUCED VERTICAL SEPARATION
MINIMUM (RVSM) AUTHORIZATIONS).
Pasal 1
Memberlakukan Petunjuk Teknis Peraturan KeselamatanPenerbangan Sipil Bagian 8900-4.10 (Staff Instruction 8900-4.10) Tentang Penerbitan Dan Pengawasan Untuk OtorisasiReduced Vertical Separation Minimum (RVSM) (Issuance AndSurveillance For Reduced Vertical Separation Minimum (RVSM)Authorizations) sebagaimana tercantum dalam Lampiranyang merupakan bagian tak terpisahkan dari Peraturan ini.
Pasal 2
Pada saat Peraturan ini mulai berlaku, Peraturan DirekturJenderal Perhubungan Udara Nomor KP 274 Tahun 2015tentang Petunjuk Teknis Peraturan KeselamatanPenerbangan Sipil Bagian 8900-4.10 tentang Penerbitan DanPengawasan Untuk Otoritasi RVSM (SI 8900-4.10 IssuanceAnd Surveillance For Reduced Vertical Separation MinimumsAuthorizations), dicabut dan dinyatakan tidak berlaku.
Pasal 3
Direktur Kelaikudaraan dan Pengoperasian Pesawat Udaramengawasi pelaksanaan Peraturan ini.
Pasal 4
Peraturan ini mulai berlaku sejak tanggal ditetapkan.
Ditetapkandi : JAKARTAPada tanggal : 25 AGUSTUS 2017
DIREKTUR JENDERAL PERHUBUNGAN UDARA
ttd
Dr. Ir. AGUS SANTOSO, M. Sc
Salinan sesuai dengan aslinya>ALA BAGIAN HUKUM,
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* \ pfcRHVJBUN
ENDAH PURNAMA SARI
Pembina (IV/a)NIP. 19680704 199503 2 001
LAMPIRAN PERATURAN DIREKTUR JENDERAL PERHUBUNGAN
UDARA
NOMOR : KP 223 TAHUN 2017
TANGGAL : 25 AGUSTUS 2017
Staff Instruction
SI 8900-4.10
Issuance and Surveillance for Reduced Vertical
Separation Minimums (RVSM) Authorizations
Edition
Amendment
Date
REPUBLIC OF INDONESIA - MINISTRY OF TRANSPORTATION
DIRECTORATE GENERAL OF CIVIL AVIATION
JAKARTA - INDONESIA
1. PURPOSE
2. REFERENCE
FOREWORD
This Staff Instruction prescribes responsibilities, policiesand procedures to be used by the Directorate ofAirworthiness and Aircraft Operation for the issuance andsurveillance for Reduced Vertical Separation Minimums
(RVSM). This Staff Instruction may be made available tothe public so that they may better understand theauthority and responsibility of the DGCA
This Staff Instruction handbook should be used in
accordance with the applicable regulations.
3. CANCELLATION : Staff Instruction Number 8900-4.10 (KP 274 Year 2015)issued 8 April 2015 is cancelled.
3. AMENDMENT : Amendment of this Staff Instruction shall be approved bythe Director General of Civil Aviation.
DIREKTUR JENDERAL PERHUBUNGAN UDARA
Salinan sesuai dengan aslinyaKEPALA BAGIAN HUKUM,
• / D'REKTORAl^ubunganSIara'
ENDAH PURNAMA SARI
Pembina (IV/a)NIP. 19680704 199503 2 001
ttd
Dr. Ir. AGUS SANTOSO, M. Sc
TABLE OF CONTENTS
FOREWORD '
TABLE OF CONTENTS "
CHAPTER 1 GENERAL 11.1. Objective *1.2. Requirement *1.3. Authorization 1
1.4. Responsibility 1CHAPTER 2 APPLICATION PROCESS 3
2.1. Aircraft Eligibility 32.2. Maintenance Program 32.3. Operator Evaluation 52.4. Prerequisites and Coordination Requirements 62.5. References 62.6. Procedures 6
CHAPTER 3 AUTHORIZATIONS TO CONDUCT RVSM OPERATIONS 103.1. Issue Authorizations, Conditions, and Limitations (ACL) 10
3.2. Task Outcomes 103.3. RVSM Authorization n
CHAPTER 4 REQUIRED MONITORING 12CHAPTER 5 RVSM APPROVALS DATABASE 13
CHAPTER 1 GENERAL
1.1. Objective
To provide guidance for evaluating applications for an operator to conductflight in airspace where Reduced Vertical Separation Minimums (RVSM) isapplied, evaluating and approving RVSM maintenance programsassociated with an application, and issuing Authorizations, Conditions,and Limitations (ACL), and issuing Operations Specifications (OpSpecs),as appropriate.
1.2. Requirement
The current regulation CASR 91, section 91.180, 91.706 and appendix G,states the requirements an operator and the operator's aircraft mustcomply with for a person to operate an Indonesian registered aircraft inRVSM airspace.
1.3. Authorization
Aircraft and operators must be authorized by the DAAO to conductoperations in RVSM airspace. The criteria evaluated to issue thisauthorization consist of three basic elements:
1) An aircraft must be determined to comply with the requirements ofCASR 91 appendix G, section 2.
2) The operator's maintenance program must be found to comply with therequirements of CASR 91 appendix G, section 3.
3) The operator must be found to have adopted RVSM operating policiesand procedures for pilots and, if applicable, flight operations officers,that are approved to the DAAO.
1.4. Responsibility
1) The Deputy Director for Engineering assigns team leaders andmembers for certification process. The team members shall be includethe:
- Airworthiness Engineer.- Principal operations inspector (POI) (Operations).- Principal maintenance inspector (PMI) (Airworthiness).
2) The evaluation of the aircraft, maintenance program, and operator'sprogram should be coordinated between airworthiness engineers,maintenance inspectors, and flight operations inspectors. TheAirworthiness Engineer will make the determination of an aircraft'scompliance. The PMI will evaluate the operator's maintenance programfor approval by the Director. The principal operations inspector (POI)will evaluate and accept the required program operational elements.
DAAO will issue an ACL and OpSpecs, as appropriate.
3) The applicant will obtain and submit all documents that establish theeligibility of its aircraft. The applicant will submit to the DGCAevidence that it is capable of operating and maintaining each aircraftor aircraft group for which it applies, and an RVSM maintenanceprogram for approval. The applicant will establish that each pilot hasan adequate knowledge of RVSM requirements and procedures. Theapplicant may also be required to submit for acceptance RVSM policyand procedures, and its initial and recurring pilot trainingrequirements.
CHAPTER 2 APPLICATION PROCESS
2.1. Aircraft Eligibility
A. An Aircraft may be authorized to conduct RVSM operations if theDGCA finds that it complies with the requirements of CASR 91
appendix G, section 2. Aircraft may be produced RVSM-compliant or
brought into compliance through the application of approved ServiceBulletins (SB), Service Letters (SL), or Supplemental Type Certificates(STC), which apply to the specific aircraft type or group and, ifapplicable, the specific aircraft serial number.
B. The Airworthiness Engineer makes the determination of aircraft
RVSM eligibility after reviewing substantiating documents developed
to meet the following applicable requirements.
1) Aircraft not produced under type certificate in accordance withCASR 21 Section 21.123 to meet requirements as stated in
CASR 91 appendix G. The Airworthiness Engineer ensures that
the inspections and/or modifications required to meet thespecified performance have been performed and documented.
2) Aircraft produced under type certificate in accordance withCASR 21 Section 21.123 to meet requirements as stated inCASR 91 appendix G. The Airworthiness Engineer ensures thatRVSM eligibility is denoted in the Airplane Flight Manual (AFM)or aircraft type certificate data sheet (TCDS) and that the initialfinding of conformity with type design has been performed.
NOTE: The determination that an aircraft is RVSM-compliant may
be accomplished entirely through the examination of documentsand/or data. Physical inspection of an airframe may not be requiredif the submitted documentation is sufficient.
C. Upon determination that an aircraft is RVSM compliant, the DAAOwill notify the applicant in writing.
2.2. Maintenance Program
A. Application for Authorization.
The application for authorization to operate within RVSM airspacemust include an approved RVSM maintenance program. Thisprogram must outline procedures to maintain aircraft in accordancewith the requirements of CASR 91 appendix G.
B. Develop and Obtain Approval.
Operators without an approved aircraft maintenance program arerequired to develop and obtain approval of an RVSM maintenanceprogram. The approved RVSM maintenance program is not requiredto include elements not related to RVSM maintenance. Inspectionprograms such as an Approved Aircraft Inspection Program (AAIP) ormanufacturer's recommended inspection program do not satisfy theRVSM requirements because they do not contain procedures tomaintain RVSM aircraft. Operators who maintain their aircraft undera continuous airworthiness maintenance program (CAMP) maychoose to incorporate the RVSM maintenance requirements into theprogram.
C. Approval.
The PMI will indicate approval of the RVSM maintenance program.The approved RVSM maintenance program elements are specific tothe operator and aircraft for which they are approved and are nottransferable.
D. RVSM Maintenance Components.
Each RVSM maintenance program must include the following:
1) Identification of components considered to be RVSM critical, andidentification of structural areas noted as RVSM critical areas.
2) The name or title of the responsible person who will ensure thatthe aircraft is maintained in accordance with CASR 43 under the
approved program.
3) The method the operator will use to ensure that all personnelperforming maintenance on the RVSM system are properlytrained, qualified, and knowledgeable of that specific system.
4) The method the operator will use to notify the crew if the aircrafthas been restricted from RVSM but is airworthy for an intended
flight.
5) The method the operator will use to ensure conformance to theRVSM maintenance standards, including the use of calibratedand appropriate test equipment and a quality assuranceprogram for ensuring continuing accuracy and reliability of testequipment, especially when outsourced.
6) The method the operator will use to verify that components andparts are eligible for installation in the RVSM system, as well asto prevent ineligible components or parts from being installed.
7) The method the operator will use to return an aircraft to serviceafter maintenance has been performed on an RVSMcomponent/system or after the aircraft was determined to benon-compliant.
8) Periodic inspections, functional flight tests, and maintenanceand inspection procedures with acceptable maintenancepractices for ensuring continued compliance with the RVSMaircraft requirements.
- These elements may be listed in detail or described byreference to an acceptable program that is identified andcontrolled by revision or issue number.
- The need for functional flight tests may be limited to onlyafter repairs or modifications that are deemed to warrantsuch testing and may be accomplished through monitoringheight-keeping performance.
9) The maintenance requirements listed in Instructions forContinued Airworthiness (ICA) associated with any RVSMassociated component or modification.
10) Any other maintenance requirement that needs to beincorporated to ensure continued compliance with RVSMrequirements.
E. RVSM Requirements.
Operators using the services of CASR 145 certificated repair stationsmust include provisions to ensure that the requirements of theirRVSM programs are being met.
2.3. Operator Evaluation
A. Obtain Authorization.
To obtain authorization from the DAAO to conduct operations inRVSM airspace, the operator must be found to have adopted RVSMoperating policies and procedures for pilots and, if applicable,dispatchers, and ensure each pilot has adequate knowledge of RVSMrequirements, policies, and procedures. The Minimum Equipment
List (MEL), if used, must incorporate the required changes stated inMaster Minimum Equipment List (MMEL).
B. Recommendation.
Director of DAAO, recommended by certification team will issue theACL and OpSpec, as appropriate, after determination of aircraftcompliance, approval of the RVSM maintenance program, andapprove of operator policies and procedures.
C. Approval.
An applicant who operates under CASR 121 or 135 must submit forapproval the initial and recurrent pilot training requirements andRVSM policies and procedures that will enable it to conduct RVSMoperations safely.
2.4. Prerequisites and Coordination Requirements
A. Prerequisites.
- Knowledge of the regulatory requirements of CASR part 91,appendix G, as applicable
- Successful completion of appropriate Airworthiness Indoctrinationcourse(s)
B. Coordination.
This task requires coordination between Airworthiness Engineer,PMI, and POL
2.5. References
CASRs 43, 91, 145, 121 and 135
2.6. Procedures
A. Determination of Aircraft Compliance.
1) Determine if the aircraft meets the requirements of CASR 91appendix G, section 2 and is RVSM compliant.
2) Review the substantiating documentation for the aircraft and itsassociated systems to identify references to RVSM capability. Foraircraft not produced under type certificate in accordance withCASR 21.123 to meet requirements as stated in CASR 91appendix G, ensure that all required elements of the approveddata through which RVSM airworthiness approval is sought
have been applied. For aircraft produced under type certificate inaccordance with CASR 21.123 to meet requirements as stated in
CASR 91 appendix G, either the aircraft TCDS or flight manual
will state RVSM compliance.
3) If sufficient documentation is available, a determination ofcompliance may be made entirely through the examination ofdocuments and/or data. Physical inspection of an airframe may
not be required.
B. Evaluation and Approval of Operator's RVSM Maintenance Program.
Review the RVSM maintenance program to ensure that it contains
the following:
1) Identification of components considered to be RVSM critical, andidentification of structural areas noted as RVSM critical areas.
2) The name or title of the responsible person who will ensure thatthe aircraft is maintained in accordance with CASR 43 under the
approved program.
3) The method the operator will use to ensure that all personnelperforming maintenance on the RVSM system are properlytrained, qualified, and knowledgeable of that specific system.
4) The method the operator will use to notify the crew if the aircrafthas been restricted from RVSM but is airworthy for an intended
flight.
5) The method the operator will use to ensure conformance to theRVSM maintenance standards, including the use of calibrated
and appropriate test equipment and a quality assuranceprogram for ensuring continuing accuracy and reliability of testequipment, especially when outsourced.
6) The method the operator will use to verify that components andparts are eligible for installation in the RVSM system, as well asto prevent ineligible components or parts from being installed.
7) The method the operator will use to return an aircraft to serviceafter maintenance has been performed on an RVSMcomponent/system or after the aircraft was determined to benon-compliant.
8) Periodic inspections, functional flight tests, and maintenanceand inspection procedures with acceptable maintenancepractices for ensuring continued compliance with the RVSMaircraft requirements.
NOTE: The need for functional flight tests may be limited to onlyafter repairs or modifications that are deemed to warrant suchtesting.
9) The maintenance requirements listed in ICAs associated withany RVSM associated component or modification.
10) Any other maintenance requirement that needs to beincorporated to ensure continued compliance with RVSMrequirements.
C. Operator Authorization.
Provide assistance to the Operations POI as required.
D. RVSM Certification Process
1) Determination of Aircraft Compliance. Determine if the aircraftmeets the requirements of CASR part 91 appendix G, section 2.Airworthiness Engineer will determine of aircraft compliance.
2) Evaluation of Operator's RVSM Maintenance Program. Reviewthe RVSM maintenance program to ensure that it contains theelements described in chapter 2, subchapter 2.2, point D. ThePMI evaluates and approves the Operator's RVSM Maintenance
Program.
3) Evaluation of Operator's RVSM Operational Procedure. The POIevaluates and approves the RVSM Operational Procedure.
4) Evaluate RVSM-Knowledgeable Pilots. The applicant mustprovide sufficient evidence of initial and recurring pilot trainingas well as policies and procedures The POI must find theoperator to have adopted RVSM operating policies and/orprocedures for pilots (and, if applicable, dispatchers) and ensureeach pilot has adequate knowledge of RVSM requirements,policies, and procedures. 5) DAAO airworthiness engineer willconduct RVSM equipment inspection that installed on theaircraft.
8
5) DAAO certification team will recommend to Deputy Director forEngineering to issue the RVSM authorization after all RVSMcertification documents and aircraft inspection satisfactory.
RVSM certification process is described on RVSM certificationflowchart.
E. Job Aid For RVSM
DAAO certification team use DAAO from 410-01, the Job Aid for
RVSM during RVSM certification program
9
CHAPTER 3 AUTHORIZATIONS TO CONDUCT RVSM OPERATIONS
3.1. Issue Authorizations, Conditions, and Limitations (ACL)
The DAAO may grant a certificate holder the authority to conduct RVSMin accordance with Part 91. Authority to conduct RVSM is granted
through the issuance of OpSpecs. Authorizations, Conditions, andLimitations B46 is issued to certificate holders who have been granted
approval to conduct RVSM.
3.2. Task Outcomes
A. Determine Aircraft RVSM Compliance.
1) If it is determined that an aircraft is RVSM compliant, the SubDirectorate of Engineering will complete the record with date ofmodification or RVSM compliance date and notify the applicant
in writing.
2) If it is determined that an aircraft is not RVSM compliant, advisethe operator/applicant by letter of the determination with anexplanation.
B. Approve or Reject Aircraft Maintenance Program/Revision.
1) Upon approval or rejection of the applicant's RVSM program, theSub Directorate of Maintenance will notify the applicant.
2) If it is determined that the RVSM maintenance program orrevision meets all of the regulatory requirements, the approvalprocess is as follows:
a. Approved maintenance programs shall include a list ofeffective pages and a revision log as future revisions areincorporated.
b. Indicate approval of RVSM maintenance program elementsthat will be incorporated into an existing accepted orapproved program for each element or group of elements bythe inspector's signature, date of approval, office name,number, and location.
c. Other approval controls may be used.
3) If it is determined that the aircraft maintenance program/revision is not acceptable, advise the operator/applicant by letterthat the program is rejected. Return it to the operator/ applicant
10
with the reasons for the rejection.
3.3. RVSM Authorization
Deputy Director for Engineeringwill issue RVSM Airworthiness andOperational Authorization by DAAO form 410-02.
11
CHAPTER 4 REQUIRED MONITORING
After finish initial RVSM certification, DAAO may issue temporary RVSM
authorization to operator. Operators have six months from the date thetemporary RVSM authorization is issued to conduct the height keeping
performance monitoring.
In accordance with Annex 6 Part I Section 7.2.7, Operators that have been
issued an RVSM authorization by DAAO are required to have their aircraft
RVSM height monitored every two years or within intervals of 1,000 flighthours, whichever period is longer.
The number of aircraft must be monitored are based on the RVSM Minimum
Monitoring Requirement (MMR) that published by Regional Monitoring Agency
(RMA).
Evidence of previous successful monitoring of an aircraft transfers to a newowner and or operator and may be used to meet the monitoring requirements.
If an operator does not complete the requirements within the allotted time:
a) It is the operator's responsibility to contact DGCA to discuss the situationand provide an updated plan for completing the monitoring requirements.DGCA will notify RMA about the situation.
b) The operator's updated monitoring plan must provide for the operatorcompleting minimum monitoring requirements for its aircraft group(s)within 3 months after the original due date. During this time, DAAO mayextend RVSM Operational Approval within 3 months and the operator maycontinue to operate in RVSM airspace.
c) Failure to complete monitoring requirements within the additional 3months will result in operators being excluded from RVSM airspace and theLOA or OpSpecs amended accordingly.
12
CHAPTER 5 RVSM APPROVALS DATABASE
DAAO inspector will update the RVSM approvals database periodically. After theissuance of RVSM authorization, DGCA inspector will insert the aircraft data(Aircraft Type/Model, Serial Number) and date of the approval issuance onIMSIS data base.
DAAO will inform RVSM database to Directorate of Air Navigation - DGCAIndonesia, Air Navigation Service Provider (Perusahaan Umum LembagaPenyelenggara Pelayanan Navigasi Penerbangan Indonesia (Perum LPPNPI)) andRegional Monitoring Agency (RMA).
13
To
Ref.
Date
Expired Date
Subject
CC. :
ATTACHMENT 1 FORMS
XXX
/DKUPPU/REK/XX/XXX
date month year
date month year and 1000 Flight HoursRVSM Operational Approval
1. Referring to XXX request No.: XXX concerning RVSMimplementation. Please be informed that based upon ourevaluation, we have decided to issue a RVSM OperationalApproval in accordance with ICAO Doc. 9574, CASR 91 andIG-91 RVSM.
2. This approval covers XXX operating aspect including thefollowing aircraft model:
No. Aircraft Type/Series Registration
Mark
Serial Number
1. XXX PK-XXX XXX
3. Furthermore XXX shall maintain to comply with RVSMrequirements, otherwise will be suspended
On behalf Director of Airworthiness
and Aircraft Operation
XXX
Deputy Director for Engineering
Director of Airworthiness and Aircraft Operation
DAAO Form 410-02
14
To
Ref.
Date
Subject
CC:
XXX
/DKUPPU/REK//XX/XXX
date month year
RVSM Airworthiness Approval
TO WHOM IT MAY CONCERN
This is certifying that the following aircraft:
No. Aircraft
Type/Series
Registration Mark Serial Number
1. XXX PK-XXX XXX
Has been assessed and examined for RVSM readiness in
accordance with applicable Service Bulletin, RVSM ICAODocument No. 9574, CASR 91 and Interim Guide (IG 91- RVSM)on implementation of a 300 m (1,000 ft) vertical separationminimum.
On behalf Director of Airworthiness
and Aircraft Operation
XXX
Deputy Director for Engineering
Director of Airworthiness and Aircraft Operation
DAAO Form 410-02
15
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eta
keof
f,eq
uip
men
tre
qu
ired
for
flig
htin
toR
VSM
airs
pac
esh
ou
ldb
eo
per
atio
nal
an
dm
alf
un
cti
on
sre
solv
ed
.
Pro
ced
ure
Pri
or
toA
irsp
ace
En
try
Lis
tR
VSM
equ
ipm
ent
that
mu
stb
eo
per
atio
nal
pri
or
toR
VSM
airs
pac
een
try
.O
per
atin
gT
ran
spo
nd
er.
Th
eo
per
ato
rsh
ou
ldas
cert
ain
the
req
uir
emen
tfo
ran
oper
atin
gtr
ansp
on
der
inth
eai
rspa
cew
here
oper
atin
g.
In-F
lig
ht
Pro
ced
ure
s
Fli
ght
crew
sho
uld
com
ply
wit
hai
rcra
fto
per
atin
gre
stri
ctio
ns
rela
ted
toR
VSM
airw
orth
ines
sap
prov
al_
_E
mph
asis
shou
ldbe
plac
edon
prom
ptly
sett
ing
the
sub-
scal
eo
nal
lpr
imar
yan
dst
and
by
alti
met
ers
to2
9.9
2in
.H
g/1
01
3.2
hP
aw
hen
pas
sin
gth
rou
gh
the
Tra
nsi
tio
nA
ltit
ud
ean
dre
chec
kin
gth
ep
rop
eralt
imete
r
sett
ing
wh
enre
ach
ing
the
init
ial
clea
red
flig
ht
lev
el(C
FL
).
Hi.
Inle
vel
cru
ise
itis
essen
tial
that
the
air
cra
ft
isfl
ow
nat
the
CF
L.
Cle
ara
nces
mu
st
be
full
yu
nd
erst
oo
dan
dfo
llow
ed.
iv.
Du
rin
gcl
eare
dtr
ansi
tio
nb
etw
een
leve
ls,
the
air
cra
ftsh
ou
ldn
ot
be
all
ow
ed
to
ov
ers
ho
ot
or
un
ders
ho
ot
the
CF
Lb
ym
ore
than
15
0ft
.(4
5m
).
v.
Un
less
cir
cu
msta
nces
dic
tate
oth
erw
ise,
an
auto
mat
icalt
itu
de
con
tro
lsy
stem
sho
uld
be
oper
ativ
ean
den
gag
edd
uri
ng
cru
ise,
etc.
vi.
An
alti
tud
eal
erti
ng
syst
emsh
ou
ldb
e
op
erat
ion
al.
vii
.
At
inte
rval
so
fap
pro
xim
atel
yo
ne
ho
ur,
cro
ss-c
heck
sb
etw
een
the
pri
mary
alti
met
ers
an
dth
est
an
db
yal
tim
eter
sho
uld
be
mad
e.A
min
imu
mo
ftw
op
rim
ary
alti
met
ers
mu
stag
ree
wit
hin
20
0ft
.o
ra
less
erv
alu
eif
spec
ifie
din
the
airc
raft
op
erat
ing
man
ual
.
vii
i.
Wh
eno
per
atin
gu
nd
er
posi
tive
rad
arco
ntr
ol,
the
init
ial
alti
met
ercr
oss
-ch
eck
sho
uld
be
per
form
edaf
ter
leve
lof
f.O
nC
lass
IIn
avig
atio
nle
gs,
acr
oss
-ch
eck
sho
uld
be
per
form
edan
dre
cord
edin
the
vici
nity
of
the
po
int
wh
ere
Cla
ssII
nav
igat
ion
isb
egu
n(e
.g.,
on
coas
tou
t).
Th
ere
adin
gs
ofth
ep
rim
ary
and
stan
db
yal
tim
eter
ssh
ou
ldb
ere
co
rded
an
dav
ail
ab
lefo
ru
se
in
con
tin
gen
cysi
tuat
ion
s.
ix.
Nor
mal
lyth
eal
tim
eter
syst
emb
ein
gu
sed
toco
ntr
ol
the
air
cra
ftsh
ou
ldb
ese
lecte
dto
prov
ide
the
inp
ut
toth
eal
titu
de
rep
ort
ing
tran
spo
nd
erth
at
istr
ansm
itti
ng
the
info
rmati
on
toA
TC
.
X.
Ifth
epi
lot
isno
tifi
edby
AT
Cof
an
assi
gn
edalt
itu
de
dev
iati
on
(AA
D)
err
or,
wh
ich
exce
eds
30
0ft
.,th
en
the
pil
ot
sho
uld
tak
e
acti
on
tore
turn
toth
eC
FL
as
qu
ick
lyas
po
ssib
le.
xi.
Co
nti
ng
ency
Pro
ced
ure
saf
ter
ente
rin
gR
VSM
airs
pac
e.T
he
pil
ot
sho
uld
no
tify
AT
Cof
con
tin
gen
cies
,w
hic
haf
fect
the
abil
ity
tom
ain
tain
the
CF
Lan
dco
ord
inat
ea
pla
no
f
acti
on
.
d.
In-f
ligh
tP
roce
du
res,
Spe
cial
Em
ph
asis
Item
s
i.
Are
ao
fO
per
atio
ns
Sp
ecif
icO
per
atio
nal
Pol
icy
&P
roce
du
res,
Incl
ud
ing
Sta
nd
ard
AT
CP
hra
seo
log
y.
ii.
Imp
ort
ance
ofcr
ewm
emb
ers
cro
ssch
eck
ing
each
oth
er
toen
su
reth
at
AT
Ccle
ara
nces
are
pro
mp
tly
an
dco
rrec
tly
com
pli
edw
ith
.
iii.
Use
an
dli
mit
ati
on
so
fst
an
db
yalt
imete
rsin
co
nti
ng
en
cie
s.
iv.
Pro
ble
ms
of
vis
ual
per
cep
tio
no
fo
ther
air
cra
ftat
1,0
00
ft.
ver
tica
lse
para
tio
n.
v.
Ch
ara
cte
rist
ics
of
air
cra
ftalt
itu
de
cap
ture
syst
ems
that
may
lead
toth
eo
ccu
rren
ceo
f
ov
ers
ho
ots
vi.
TC
AS
op
erat
ing
ch
ara
cte
rist
ics
inR
VS
M
airs
pac
e,if
equ
ipp
ed.
vii
.
Rel
atio
nsh
ipb
etw
een
the
alti
met
ry,
au
tom
ati
calt
itu
de
con
tro
l,an
dtr
an
spo
nd
er
syst
ems
inn
orm
al
an
dab
no
rmal
situ
atio
ns.
vii
i.A
ircr
aft
op
erat
ing
rest
rict
ion
s(o
nly
if
ap
pli
cab
leto
the
airc
raft
).
ix.
Fo
rth
ose
op
era
tors
auth
ori
zed
toco
nd
uct
oce
anic
op
erat
ion
s—u
seo
fS
trat
egic
Lat
eral
Off
set
Pro
ced
ure
s(S
LO
P)in
oce
anic
airs
pac
eto
mit
igat
eth
eef
fect
of
wak
e
turb
ule
nce
an
dth
eef
fect
of
op
erat
ion
al
erro
rs.
e.
Po
stF
lig
ht
Pro
ced
ure
(if
any
).
Inm
ak
ing
main
ten
an
ce
log
bo
ok
en
trie
s
agai
nst
mal
fun
ctio
ns
inh
eig
ht
kee
pin
gsy
stem
s,th
ep
ilo
tsh
ou
ldp
rov
ide
suff
icie
nt
deta
ilto
en
ab
lem
ain
ten
an
ce
toef
fect
ivel
y
tro
ub
lesh
oo
tan
dre
pair
the
syst
em
.
4.
Main
ten
an
ce
a.
Mai
nte
nan
ceP
rog
ram
(CA
MP
/AA
IP-
co
mp
on
en
tsco
nsi
der
edto
be
RV
SM
crit
ical
)
i.
Iden
tifi
cati
on
of
RV
SM
co
mp
on
en
tsan
d
iden
tifi
cati
on
of
str
uctu
ral
areas
no
ted
as
RV
SM
cri
tical
areas.
ii.
Th
em
eth
od
the
op
era
tor
wil
lu
seto
en
sure
that
all
per
son
nel
per
form
ing
main
ten
an
ce
on
the
RV
SM
syst
emare
pro
per
lytr
ain
ed,
qu
alif
ied
,an
dk
no
wle
dg
eab
leo
fth
at
spec
ific
sy
ste
m.
iii.
Th
em
eth
od
the
op
era
tor
wil
lu
se
toen
sure
co
nfo
rman
ce
toth
eR
VS
Mm
ain
ten
an
ce
stan
dard
sin
clu
din
gth
eu
seo
fcali
bra
ted
an
dap
pro
pri
ate
test
eq
uip
men
t,an
da
qu
alit
yass
ura
nce
(QA
)p
rog
ram
for
en
suri
ng
the
co
nti
nu
ed
accu
racy
an
d
reli
abil
ity
of
test
equ
ipm
ent,
esp
ecia
lly
wh
en
ou
tso
urced
.
iv.
Th
em
eth
od
the
op
era
tor
wil
lu
seto
ver
ify
that
co
mp
on
en
tsan
dp
art
sare
elig
ible
for
inst
alla
tio
nin
the
RV
SM
syst
em,
as
wel
las
top
rev
en
tin
stal
lati
on
of
inel
igib
le
co
mp
on
en
tso
rp
art
s.
V.
Th
em
eth
od
the
op
era
tor
wil
lu
se
tore
turn
an
air
cra
ftto
serv
ice
aft
er
an
ap
pro
pri
ate
ly
rate
dp
ers
on
has
perf
orm
ed
main
ten
an
ce
on
an
RV
SM
co
mp
on
en
t/sy
stem
or
aft
er
the
air
cra
ftw
as
dete
rmin
ed
tob
en
on
co
mp
lian
t.
vi.
Per
iod
icin
specti
on
s,fu
ncti
on
al
flig
ht
test
s,
an
dm
ain
ten
an
ce
an
din
specti
on
pro
ced
ure
sw
ith
accep
tab
lem
ain
ten
an
ce
pra
cti
ces
for
en
suri
ng
co
nti
nu
ed
co
mp
lian
ce
wit
hth
eR
VS
Mair
cra
ftre
qu
irem
en
ts.
vii
.
Th
em
ain
ten
an
ce
req
uir
em
en
tsli
sted
inth
e
ICA
ass
ocia
ted
wit
han
yR
VS
Mass
ocia
ted
co
mp
on
en
to
rm
od
ific
atio
n.
vii
i.
An
yo
ther
main
ten
an
ce
req
uir
em
en
tth
at
the
op
era
tor
need
sto
inco
rpo
rate
toen
sure
co
nti
nu
ed
co
mp
lian
ce
wit
hR
VS
M
req
uir
em
en
ts.
b.
Min
imu
mE
qu
ipm
en
tL
ist
(ME
L)
c.
Train
ed
Perso
nn
el
5.
Tra
inin
gP
erso
nn
el
a.
Fli
gh
tC
rew
Init
ial
an
dR
ecu
rren
tT
rain
ing
Sy
llab
us
b.
Dis
pat
cher
Tra
inin
gS
yll
abu
s
c.
Tra
inin
g/C
ou
rse
Cer
tifi
cate
s
6.
SS
RM
ode
S(D
irec
tora
teo
fA
irN
avig
atio
n)
7.
Las
tR
VS
MO
per
atio
nal
Ap
pro
val
/p
ast
per
form
ance
(if
any
)8
.P
lan
for
RV
SMH
eig
ht
Kee
pin
gP
erfo
rman
ceM
on
ito
rin
g(G
MU
/AD
SB
)
Pre
pare
db
y:
Pre
vie
wb
y
DA
AO
Fo
rm4
10
-01
ATTACHMENT 2 RVSM CERTIFICATION FLOW CHART
APPLICANT
Application Letter/ Letter of Intent
Applicant prepare Application DataPackages consist:1. AFM,TCDS;
2. Servive Bulletine (if applicable);3. Description of Aircraft Equipment;4. Operation Manual/Checklist;5. Maintenance Program;6. Training Personnel (syllabus,record) : Flight Crew, Dispacther,Maintenance personnel;7. SSR Mode S;8. Past Performance (if any);9. Plan for Height KeepingPerformance Monitoring.
Submit ApplicationData Package on
Meeting
-No-
DGCA-DAAO
Sub Directorate of Engineering-DAAO will establish RVSM
certification team that consist:1. Team Leader
2. Team Members: POI,PMI,Avionic Specialist, and Performanceand Flight Test Specialist
Invitation Letter for
Initial Meeting
DAAO team will
evaluate ApplicationData Package
Yes
RVSM equipmentsInspection
No
APPLICANT
Applicant ConductHeight Keeping
Performance
Monitoring (ADSB/GIVILJ) witnessed by
DAAO team
Yes-
DGCA-DAAO
®
DAAO issue
Temporary RVSMAuthorization
DAAO issue RVSIVI
Authorization
within two years andlOOO flight hours
END
DIREKTUR JENDERAL PERHUBUNGAN UDARA
ttd
Dr. Ir. AGUS SANTOSO, M. Sc
Salinan sesuai dengan aslinyaKEPALA BAGIAN HUKUM,
DIREKT0RA1 JZNOWPERHUBUNGAN UP'
ENDAH PURNAMA SARI
Pembina (IV/a)>680704 199503 2 001