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MOHAMMED ABDUL HAKEEM QURESHIMOHAMMED ABDUL HAKEEM QURESHICar Mnotes
WARNINGThis document must be used for training purposes
only
Under no circ*mstances should this document beused as areference
It will not be updated.
All rights reservedNo part of this manual may be reproduced inanyform, by photostat, microfilm, retrieval system, or anyothermeans, without the prior permission of THEAUTHOR.
PLEASE ADDRESS FEEDBACK AND COMMENTS TO
[emailprotected]
NoticeNo responsibility is assumed by the publisher foranyinjury and/or damage to persons or property as amatter ofproducts liability, negligence or otherwise,
or from any use or operation of any methods,products,instructions or ideas contained in thematerial herein.
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MOHAMMED ABDUL HAKEEM QURESHIMOHAMMED ABDUL HAKEEM QURESHICar Mnotes
Continuing Airworthiness Requirements
Initial Issue (Revision 0)2nd March, 2010.
This CAR M provides common technical standards and guidelinesforcontinued airworthiness of an aircraft and its components withan effective
date of 31st July 2010.
FOREWORD
Rule 50A of the Aircraft Rules 1937 stipulates the conditionsnecessary
for a Certificate of Airworthiness to remaining in force
CAR-M specifies certain technical requirements to be compliedbyorganisations and personnel involved in the maintenance ofaircraft and
aeronautical products, parts and appliancesRequirements in orderto demonstrate the capability and means of
discharging the obligations and associated privilegesthereof.The CAR-M also specifies conditions of issuing,maintaining, amending,
suspending or revoking certificates attesting suchcompliance.
Car m requirements which are harmonized with EASA Part Mregulation
The CAR M is applicable to all operators of Indian registeredaircraftirrespective of whether such aircraft are maintained bytheir own
organization or by other approved maintenance organization.
Rule 133B of the Aircraft Rules 1937 stipulates thatorganizationsengaged in the maintenance of aircraft and aircraftcomponents shall beapproved.
is issued under the provisions ofRule 133A of the Aircraft Rules1937
M.1
Dgca is compentent authority.
oversight of the continuing airworthiness of individual aircraftand the
issue of airworthiness review certificates.Oversight ofmaintenance organization.
Oversight of continuous airworthiness managementorganization.(CAMO)Maintanenance programmes approval for
indian reg a/ca/c -comme trans by indian opera if agreed bystate of registry.
a/c-not comm trans but managed by CAMO.
M.2 Objective
common technical requirements and administrative procedures-a/c&comp -cont a/w.
(a) registered in India; or
(b) registered in a foreign country and used by an Indianoperator for
which Indiaensures oversight of operations.
M.3 Definitions
Aircraft, Certifying staff, maintenance, large aircraft,organization, pre-
flight inspection.
continuing airworthiness
means all of the processes ensuring that, at any time in itsoperating life,
the aircraft complies with the airworthiness requirements inforce and is in
a condition for safe operation.
M.4 Continuing Airworthiness Requirements.
M.5 Entry into force.31 july 2010.
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MOHAMMED ABDUL HAKEEM QURESHIMOHAMMED ABDUL HAKEEM QURESHICar Mnotes
SECTION A -TECHNICAL REQUIREMENTS.
SUBPART A GENERAL:
M.A.101 Scope
Requirements and conditions for continuing airworthiness
SUBPART B ACCOUNTABILITY
M.A.201 Responsibilities
a) Owner is responsible.
1. a/c -a/w
2. operational and emer equip correc installed & Serv orident u/s.
3. the airworthiness certificate remains valid, and;
4. the maintenance of the aircraft is performed in accordancewith theapproved maintenance programme.
b) where leased lessee=owner for resp when stipulated in
1.Reg doc /2. leasing contract.
c) person/orgn -resp maint.
d) PIC or oper for comm -resp PFI.e) 1. owner- cont.. CAMO thenCAMO is resp for tasks.
2.owner own a/w limited contract CAMO for maint prog
development and appr.. --resp CAMO.
f) large a/c Owner- cont.. appr CAMO then CAMO is resp fortasks.
g) large a/c and Comm a/c CAR 145 AMO.
h) comm a/c tran opera resp for cont a/w of a/c.1. Be apvd aspart of AOC/AOP issued by dgca as per Car-m Sec A
Subpart-G.
2. Be apve in accordance of CAR-145 or cont such.
Ensure para a is satisfied.
Acceptable Means of Compliance to CAR- M
Section A
Subpart A General
Subpart B Accountability
AMC M.A.201 (h) Responsibilities
1. a/c includes comp fitted or intended.
2. gnd de-icing and anti-icing CAR-145 Appr not req.
3. requirement means oper is resp for what, when, whom andstandard ofmaintenance for cont a/w.
4. oper adq knwldg of AD's modifications, design standardsetc.5. oper resp for coor between operations and maintenance.
6. oper resp for a/w of a/c and ensure all cond are met beforeflight.
7. oper is resp even if he contracts to CAR-145 orgn.
AMC M.A.201 (h) 1- Responsibilities.
1. oper only needs appr for cont a/w mang for a/c in AOC. Apprfor
a/w rev is optnl.
2. The regulatory monitoring is exercised through the operatorsM.A.
Subpart G. Approval.
3. oper resp and accnt.. for cont a/w irrespective of maint contto
AMO.4. .CAR M does not provide for organisations to beindependently
approved to perform continuing airworthiness managementtasks
on behalf of commercial air transport operators.Such activityisvested in AOC.
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MOHAMMED ABDUL HAKEEM QURESHIMOHAMMED ABDUL HAKEEM QURESHICar Mnotes
i)when oper is req to hold a certificate for commercialoperations,
other than for commercial air transport.
1. be apvd in accordance with subpart G CAMO
2. be apvd in accordance with subpart F Maintenance organizationor
CAR-145 or contr such.
3. Ensure owner resp as in a.j) owner/oper grant access dgca forcompliance
5.Sub-cont orgn is considered integral part of oper CAMsys.irrespective
of any appr held by sub-cont including subpart G appr.
oper should satis sub-cont meet standards req by subpart G.6. Inorder to retain ultimate responsibility the operator should limitsub-
contracted task.
7. oper manag controls wrt sub-cont CAM tasks written contractand inaccordance with policy and procedures CAM expo..When suchtasks are sub-contracted the operator's continuingairworthiness
management system is considered to be extended to thesubcontracted
organisation.
8. cont limited to one organisation per aircraft type for anycombination of
the activities except ENG and APU. Where more than oneshoulddemonstrate adq co-ordn controls.
9. Contracts should not authorize the sub-contractedorganisation to sub-
contract to other organisations elements of the continuingairworthiness
management tasks.
10. oper -dgca findings of sub-cont = clsd to satis of dgca andincl in cont.11. sub-cont --notify any changes affect cont. Failurewill invalidate dgca
acpt of cont.
12.
13. oper should only sub-cont to orgn specified in AOC orCA14.
AMC M.A.201 (h) 2- Responsibilities
1. The requirement is intended.
a) oper to be apvd CAR-145 for maintb) oper to be apvd CAR-145for some maint
c) oper not apvd CAR-145 for maint.
2. An operator or prospective operator may apply for any one oftheseoptions but it will be for DGCA to determine
2.1 To make this determination DGCA will apply the primarycriteria ofrelevant operator experience if carrying out some or allmaintenance on
comparable aircraft.
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MOHAMMED ABDUL HAKEEM QURESHIMOHAMMED ABDUL HAKEEM QURESHICar Mnotes
M.A.202 Occurrence reporting
a) person/orgn rep dgca/state of registry condition whichendangers flt
safety.
b) Rep manner dgca and all info.
c) where maint orgn is contr maint orgn rep toowner/oper/CAMO.d) Rep within 72 hrs of ident.
2.2 similar to 2.1 excpt exp is for some maint.
2.3
2.4 experience means staff who have proven evidence thattheywere directly involved with at least line maintenance ofsimilar aircraft
types for not less than 12 months.
AMC M.A.202 (a) Occurrence reporting
Accnt Mana/orgn TC holder rec occurence rep.
Suitably qua person for occurence rep and investigation.
In respect of maintenance, reporting a condition that couldseriouslyhazard the aircraft is normally limited to:
- serious cracks, permanent deformation, burning or seriouscorrosion of
structure found during scheduled maintenance of the aircraftor
component.
- failure of any emergency system during scheduled testing.
AMC M.A.202 (b) Occurrence reporting
Rep elect, by post or fascimile.
Following information.
Reporter name with approval ref no.
Information-- a/c/equip
date time etc interms of life /overhaul
hours/cycles/ldgs etc.
Details of occurence.
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MOHAMMED ABDUL HAKEEM QURESHIMOHAMMED ABDUL HAKEEM QURESHICar Mnotes
SUBPART C CONTINUING AIRWORTHINESS
M.A.301 Continuing Airworthiness Tasks
cont a/w and ser of oper equip and emer equip.
1. PFI2. Rect of defects and damages(MEL & CDL).
3. Maint Maint Prog.
4. Comm a/c -- analysis of maint prog.
5. Accom of AD'S, oper direct, cont a/w req and measures(dgca).
6. Mods and repairs.
7. Embodiment policy for larger/comm a/c for non-mandmods/insp.
8. Maint Check flights.
Sub Part C Continuing Airworthiness
AMC M.A.301 -1- Continuing airworthiness tasks
1. PFI includes actions a/c is fit for intended flight.
Walkaround insp, insp of cont a/w record sys/oper tech logetc.
2. Tasks such as oil and hydraulic fluid uplift and tyreinflation may beconsidered as part of the pre-flightinspection.
3. task guidance for PFI tasks. trng stnd CAM expo
AMC M.A.301 - 2- Continuing airworthiness tasks
MEL/CDL defects should be rect within limits.
Large a/c/comm a/c sys for analysis of CAMO defect controlsys.
include
Significant incidents and def.
Reptitive incidents and def .Deffered and carried fwd def.
Unschld rem and sys performance.
Deferred defects are defined as those defects reported inoperational
service which is deferred for later rectification.Carriedforward defects are defined as those defects arising during
maintenance and carried fwd.
AMC M.A.301 - 3- Continuing airworthiness tasks
Owner or CAMO ensure that all aircraft maintenance checksare
performed within the limits prescribed by the approvedaircraft
maintenance programme. postpon proc acpt to dgca.
AMC M.A.301 - 4- Continuing airworthiness tasks
Oper/contr CAMO system to analyse the effectiveness of themaintenance
programme.
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MOHAMMED ABDUL HAKEEM QURESHIMOHAMMED ABDUL HAKEEM QURESHICar Mnotes
M.A.302 Aircraft Maintenance Programme
a) maint maint prog.b) maint prog and amnd apvd by dgca.
c) cont a/w CAMO a/c maint prog and amnd indirect apprv proc
Provided submitted to DGCA local office at least 15 days beforetheir
affectivity and pro doc.
1. CAMO CAM Expo apvd by dgca.
2. CAMO indirect apprvl proc when not under oversight of stateofregistry
d) air maint prog compliance with
Dgca, TC holder or TSO CAR 21/EASA 21/FAR 21e) a/c maint progdetails and freq of maint.
(f) For large aircraft, when the maintenance programme is basedon
maintenance steering group logic or on condition monitoring, theaircraft
maintenance programme shall include a reliability programme.
(g) The aircraft maintenance programme shall be subject toperiodicreviews and amended accordingly when necessary.
AMC M.A.301 -5- Continuing Airworthiness Tasks
Oper direc with cont a/w impact included ETOPS/LROPS, RVSM,MNPS,
AWOPS, RNAV AND CMR etc.
AMC M.A.301 - 7- Continuing airworthiness tasks
Oper / contr CAMO dev and work a policy non-mand info.
AMC M.A.302 Maintenance Programme
1. The term maintenance programme is intended for scheduledtasks.
The term maintenance schedule is intended to embrace thescheduledmaintenance tasks alone.
2. The aircraft should only be maintained to one approvedmaintenance
programme at a time.
3. The maintenance programme details should be reviewed atleast
annually.4. a/c maint prog preface contents, insp stnd,variations to task freq.
5. AMP mand reg req TC holder to com CAR 21/ EASA Part 21/FAA
Part 21 requirement.
6. repetitive maint tasks mods and reprs --- AMP.
AMC M.A.302(c) Maintenance programme compliance
1. owner/oper AMP based on MRB, MPD OR AMM if appble.
2. 3. 4. if MRB cont Reliabity then its cons part of AMP.
5.AMP crossref to MRB rep is based.6.
AMC M.A.302 (d) Maintenance programme -reliabilityprogrammes.
1. Rel Prog should be dev when based on MSG/cond mont items ordo not
contain overhaul -- sign comp.7
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M.A.303 Airworthiness directives
Any applicable airworthiness directive must be carried outwithin the
requirements of that airworthiness directive, unless otherwisespecified by
DGCA.
M.A.304 Data for modifications and repairs
Damage shall be assessed and modifications and repairs carriedout using
data approved by DGCA or by an approved CAR -21/ EASA Part21/
FAA Part 21 design organization.
M.A.305 Aircraft continuing airworthiness record system
a) after maint CRS cont a/w rec atleast within 30 days.
b) cont a/w records
1. A/C, eng Log books, eng module log cards, propeller log bookand
log book for any ser life lim comp.
2. Comm air trans tech log.
c) a/c type, reg marks, flt time/cycles etc a/c logbook.
d) The aircraft continuing airworthiness records shall containthe current:1. status of airworthiness directives and measuresmandated by the DGCA
in immediate reaction to a safety problem;
2. status of modifications and repairs;
3.status of compliance with maintenance programme;4. status ofservice life limited components;
5. mass and balance report;
6. list of deferred maintenance.
2. Rel prog not req for not hvy a/c or contain ovhl all sigcomp.
3. The purpose of a reliability programme is to ensure that theAMP tasks
are effective and their periodicity is adequate.4. Rel progesc/del of a task or vice versa.
5. Rel prog --- eff of AMP.
6.
AMC M.A.304 Data for modifications and repairs
Dam or reprs if beyond limits TC holder /FAR21/EASA21/CAR21orgn.
And dgca for apprvl.
AMC M.A.305 (d) Aircraft continuing airworthiness record
system
Where an AD is generally applicable to the aircraft or componenttype but
is not applicable to the particular aircraft or component, thenthis should beidentified.
When owners and operators wish to take advantage of the modulardesign,
then total time in service and maintenance records for eachmodule is to be
Maintained.
AMC M.A.305 (h) Aircraft continuing airworthinessrecordsystem
Owner/oper cont maint still resp for retn of rec. Or trnsf tonew owner.Computer systems should have at least one backup system,which shouldbe updated at least within 24 hours of anymaintenance.
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MOHAMMED ABDUL HAKEEM QURESHIMOHAMMED ABDUL HAKEEM QURESHICar Mnotes
e) In addition to the authorised release document, CA Form 1/EASA
Form1/FAA 8130 or equivalent, the information relevant toany
component installed shall be entered in the appropriate engineor propellerlogbook, engine module or service life limitedcomponent log card.
f) Person resp for cont a/w should control rec.
g) All entries clear and accurate.
h) foll rec for periods specified.
1. detailed maint rec a/c & life lim comp. 24 m fromwithdrawal.
2. Total time & flight cycles 12 m from withdrawal.
3. Time & flight cycles from last sch maint unlesssuperseeded.
4. Curr status of compliance.
5. Curr status of AD's & 12 m from withdrawal.
6. Curr mods and reprs & 12 m from withdrawal.
M.A.306 Operator's technical log system
a) comm air trans tech log.1. info nece for each flt.
2. Current CRS.
3. Current maint status.
4. all outstanding deferred defects rectifications.
5. Any necc. Guidance on maint support arng.
b) apvd by dgca.
c) tech log 36 m from last entry.
AMC M.A.305 (h) 6- Aircraft continuing airworthinessrecordsystem
component vital to flight safety means a component that includescertified
life limited parts or is subject to airworthiness limitations ora majorcomponent such as, undercarriage or flight controls.
AMC M.A.306 (a) Operators technical log system
aircraft technical log is a system for recording defects andmalfunctionsduring the aircraft operation and for recording detailsof all maintenance
carried out on an aircraft between scheduled base maintenancevisits.
Cabin or galley def & mal func safe oper of a/c cons part oftech log.
A/c tech log simple single sect/ complex muti sect. Follinfo
SEC 1. should contain details of the registered name and addressof theoperator the aircraft type and the complete internationalregistration marks
of the aircraft.
SEC 2. info next sch main is due. Curr CRS.
SEC 3. All info flight safety.NOTE 1: Where Section 3 is of themulti-sector part removable type then
such part removable sections should contain all of theforegoing
information where appropriate.
NOTE 2: Section 3 should be designed such that one copy of eachpage
required to be completed after flight and what is required to becompletedin preparation for the next flight.
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MOHAMMED ABDUL HAKEEM QURESHIMOHAMMED ABDUL HAKEEM QURESHICar Mnotes
M.A.307 Transfer of aircraft continuing airworthinessrecords
a) trans rec incl a/c tech log.
b) cont a/w rec trans to orgn if contr to CAMO.c) time per forretn.
SEC 4. all deferred defects that affect or may affect the safeoperation with
cross ref to sect 3 def.
SEC 5. all maint supp info.
AMC M.A.306 (b) Operators technical log system
AMC M.A.307 (a) Transfer of aircraft continuingairworthinessrecords
A permanent transfer does not generally include the drylease-out of an
aircraft when theduration of the lease agreement is less than 6months.
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MOHAMMED ABDUL HAKEEM QURESHIMOHAMMED ABDUL HAKEEM QURESHICar Mnotes
SUBPART D MAINTENANCE STANDARDS
M.A.401 Maintenance data
a) app curr and main data
b) MAIN DATAAppl data req or AD'S or data TC holder.c) orgnshall ensure that all applicable maintenance data is currentand
readily available for use.
M.A.402 Performance of maintenance
a) all maint work Maint data. Unless spec CAR-145.
b) tools and equip Maint data. Unless spec CAR-145.
c) area organised and clean.d) all main in environmetal lim.
e) proper facilites.
f) gen verification after comp of maint.
Sub Part D Maintenance Standards
AMC M.A.401 (b) Maintenance data
1. orgn Maint should have access to and use:
a) CAR'S & asso AMC'S.
b) all appl maint data & dgca notices.c) all appl AD'S.
d) all appr sect of AMP, AMM, SB, SIL, SSID, CPCP etc.In addn toabv
2. vendor main and reprs man SB's, SIL's etc and TC holderdata.
AMC M.A.401(c) Maintenance data
1. Main data readily avbl.
2. suff no. Of comp sys.
3. lengthy maint task -- supplementary work cards or worksheetsto
indicate what was actually accomplished by each individualperson.4. maint data updated.
AMC M.A.402 (a) Performance of maintenance
1. support staff/ personnel under super vis of cert pers.2.pilot owner maint --- appr trng and exp as acpt to dgca.
3. maint and insp stnds type design(maint man) or a/w stnds bydgca.
4. Independent Insp.
4.1 Man inst when Ind Insp is needed.
4.2 In abs of abv maintenance tasks that involve the assemblyor
any disturbance of a control system that, if errorsoccurred,
could result in a failure, malfunction, or defect endangeringthe
safe operation of the aircrat.- Ind Insp.
4.3 Ind insp 2 persons, a tech rec sign of both.1 first person--resp & CRS.
2. Sec person no cert prev but suff qual.
4.4 When AMO pers hav been trained and gained exp.
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MOHAMMED ABDUL HAKEEM QURESHIMOHAMMED ABDUL HAKEEM QURESHICar Mnotes
M.A.403 Aircraft defects
a) Ser def rec before flt.b) only auth cert staff which defectrectification can be deferred.exc
1.MEL apvd by dgca
2. def defined acpt to dgca.
(c) Any aircraft defect that would not hazard seriously theflight safetyshall be rectified as soon as practicable maintdata
d) def not rect a/c maint rec sys or a/c tech log
4.5 When work done cert by ind AME lice holder then heshould
assess the second persons knowledge and exp.
4.6 In summary the following maintenance tasks should primarilybe considered when inspecting aircraft control systems that
have been disturbed.
4.7 that have undergone maintenance the person
AMC M.A.402 (b) Performance of maintenance
All tools requiring calibration should be traceable to anacceptable
standard.
AMC M.A.402 (d) Performance of maintenance.
The working environment should be appropriate for themaintenance task.
AMC M.A.402 (e) Performance of maintenance
Facilities should be provided appropriate for all plannedmaintenance
AMC M.A.403 (b) Aircraft defects
An assessment of both the cause and any potentially hazardouseffect.
AMC M.A.403 (d) Aircraft defects
All deferred defects should be made known to the pilot/flightcrew,
whenever possible, prior to their arrival at the aircraft.
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MOHAMMED ABDUL HAKEEM QURESHIMOHAMMED ABDUL HAKEEM QURESHICar Mnotes
SUBPART E COMPONENTS
M.A.501 Installation
(a) No component may be fitted unless it is in a satisfactorycondition, CA
FORM 1.(b) prior to fitment comp is eligible.(c) Standard partsshall only be fitted to an aircraft/comp maint data,
accom by evidence.
d) Material being either raw material or consumable materialmaint
data/CAR-145.
Sub Part E Components
AMC M.A.501 (a) Installation
1. to ensure comp satis inst, perf checks and verification.
2. and before comp is inst.
3. list checks to be perf.4. CA FORM 1 is to release componentsafter manufacture and to release
maintenance work carried out on such components under theapproval of a
DGCA and to allow components removed from one aircraft/componentto
be fitted to another aircraft/ component.
5. equivalent to a CA Form 1.EASA Form ONE - FAA Form 8130-3 -Any other form
acceptable to DGCA.
6. Any item in storage without a CA Form 1 or equivalent cannotbe
installed unless CA FORM 1.
AMC M.A.501 (b) Installation1. Form 1 identifies theairworthiness and eligibility status of an aircraft
component. Block 13 "Remarks" on the CA Form 1 in some casescontainsvital airworthiness related information
2. fitment/replacement person M.A. 801 comp meets req stnds.
3. comp appr stnd ( AD) etc.
AMC M.A.501(c) Installation
1. stnd parts
2. stnd part manl
3. Documentation accompanying standard parts should clearlyrelate to the
particular parts and contain a conformity statement plus boththemanufacturing and supplier source.
4. CA FORM 1 is not normally issued
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MOHAMMED ABDUL HAKEEM QURESHIMOHAMMED ABDUL HAKEEM QURESHICar Mnotes
M.A.502 Component maintenance
a. maint of comp SEC A subpart F / CAR-145.
b. abv maint of a/c main data or comp maint data can be done by'A' rated
orgn whilst comp are fitted on a/c.Component maintenanceperformed in
accordance with this paragraph is not eligible for the issuanceof a CAForm 1 only a/c release.
c. same as 2 but ENG/APU and by 'B'.
d. maint of comp installed/removed for light a/c other than commair trans.
1. overhaul of components other than engines and propellers,and;2. overhaul of engines and propellers for aircraft other thanCS-VLA, CS-
22 and LSA.
No CA FORM 1 only aircraft release req.
M.A.503 Service life limited components
Ser life lim comp > apvd life lim AMP/AD.
M.A.504 Control of unserviceable components
a. comp = u/s
AMC M.A.501 (d) Installation
1. Consumable material is any material which is only used once,such as
lubricants, cements, compounds, paints, chemicals dyes andsealants etc.
2. Raw material is any material that requires further work tomake it into acomponent part of the aircraft such as metals,plastics, wood, fabric etc.
3. must meet specs4. material confirmity statement + manu andsupplier source.
5. NO CA FORM 1.6. Items purchased in batches (fasteners etc.)should be supplied intact in
the original equipment manufacturer (OEM) package
AMC M.A.504 (a) - Control of unserviceable components
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MOHAMMED ABDUL HAKEEM QURESHIMOHAMMED ABDUL HAKEEM QURESHICar Mnotes
1. expi of ser life AMP.
2. Non comp AD & cont a/w req -dgca.
3. Abs of info a/w.
4. Evidence of def/malfunc.
5. Accident/incident serviceability.
b. u/s comp stored secure loctn. A/c -non comm comp trfs toowner and
rev in a/c logbook or eng log or comp log.c. Components whichhave reached their certified life limit or contain a
non-repairable defect shall be classified as unsalvageable.
d. per res retain such comp as abv or mutilate it.
e. may trnfs to training or research dep.
AMC M.A.504 (b) - Control of unserviceable components
1. cert staff ident of u/s comp.
2. Clearly dec on a tag with comp ident data and nec info.
3. Cert staff agree of owner/oper u/s comp to maint orgnforstorage.
AMC M.A.504 (c) - Control of unserviceable componentsunsalvageable components
a) components with non-repairable defects, whether visible ornot to the
naked eye;
b) components that do not meet design specifications, and cannotbe
brought into conformity with such specifications;c) componentssubjected to unacceptable modification or rework that is
irreversible;
d) certified life-limited parts that have reached or exceededtheir certified
life limits, or have missing or incomplete records;
e) components that cannot be returned to airworthy condition duetoexposure to extreme forces, heat or adverse environment;
f) components for which conformity with an applicableairworthiness
directive cannot be accomplished;
g) components for which continuing airworthiness recordsand/or
traceability to the manufacturer can not be retrieved.2.Cautionshould be exercised to ensure that unsalvageable components
are disposed of in a manner that does not allow them to bereturned to
service.
AMC M.A.504 (d) 2 - Control of unserviceable components
1) Mutilation should be accomplished in such a manner thatthe
components become permanently unusable for their originalintended use.
2) Mutilation proc.3) unsuccessful 2 proc.
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MOHAMMED ABDUL HAKEEM QURESHIMOHAMMED ABDUL HAKEEM QURESHICar Mnotes
4) data plate and/or serial number and final disposition of thecomponent
to manufacturer.
AMC M.A.504 (e) - Control of unserviceable components
release an unsalvageable component for legitimate non-flightuses, such as
for training.
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MOHAMMED ABDUL HAKEEM QURESHIMOHAMMED ABDUL HAKEEM QURESHICar Mnotes
SUBPART F MAINTENANCE ORGANISATION
M.A.601 Scope
Req for a/c that r not large /comm a/c.
M.A.602 Application
Appli Issue/variation of appr CA FORM 2F
M.A.603 Extent of approval
a) cert of appr -CA FORM 3.maintenance organisation'smanualScope.
May fabricate in conformity -maint data & ment in Maint orgnman.
M.A.604 Maintenance organisation manual
a)
1. Statement signed by accountable manager.
2. scope of work.
3. Title and names of persons.4. orgn chart chain of resp.
5. List of cert staff with scope of apprvl.
6. List of locations and faci.
7. proc spec maint orgn comp with CAR.8. mom amnd proc.b) MOMamnd apvd by dgca.
c) ind aprvl proc- MOM atleast 15 days before effictivity.
Sub Part F Maintenance Organization
AMC M.A.601 Scope
AMC M.A.602 Application
AMC M.A.603 (a) Extent of Approval
AMC M.A.603 (b) Extent of approval
1) Fabrication process maint orgn manual agreed by dgca.
2)
3) fab data apvd by dgca or TC holder.
4) fab for own facility only.5) not for onward supply orsale.
Adequate records should be maintained of all such fabricationprocesses
including heat treatment and the final inspections.
AMC M.A.604 Maintenance organisation manual
1. man= det proc.
2. CAR-145 format acpt for MOM for large orgn.
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M.A.605 Facilities
a) facilities.
b) office accom.
c)storage facilities.
M.A.606 Personnel requirements
a) accnt man.
b) person- orgn comp under acnt man.c) abv person rel know andexp.
d) temp sub-cont staff acpt when more work cannot CRS.e) qual ofmaint per demo and rec.
f) Personnel - specialised tasks such as welding, NDTtesting/inspection
other than colour contrast shall hold relevant certificate ofcompetency.
AMC M.A.605 (a) Facilities
1. Where a hangar is not owned by the M.A. Subpart Forganisation, it
may be necessary to establish proof of tenancy.
2. Protection from the weather elements.3. Aircraft maintenancestaff should be provided with an area where they
may study maintenance instructions and completecontinuingairworthiness records.
AMC M.A.605 (b) Facilities
1. can comb off accom one off suff room .
AMC M.A.605 (c) Facilities
1. Storage facilities for serviceable aircraft components cleanwell vent.
2. Adequate storage racks should be provided and strongenough.
3. All aircraft components, wherever practicable, should remainpackaged
in their protective material.
4. Segregation means storing u/s and ser items sep.5.Segregation and management u/s comp.
6. decision process.
7. Unsalvagable comp secure areas in which to segregate suchitems and to
prevent unauthorised access. And final disp.
AMC M.A.606 (a) Personnel requirements
Accnt mang normally CEO and can be for more than one orgn.
Accnt mang direct access to CEO for maint funding.
AMC M.A.606 (b) Personnel requirements;
1.
2.dependent upon the extent of approval, an aircraft maintenancemanager,a workshop manager rep to accnt mang.
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g) suff staff CRS
h) excp of g for comm oper (orgn manl)
1.repetitive pre-flight airworthiness directive- flt crew suchADcommander practical trng.
2. operating away from a supported location commander lim certstaff
auth after pract trng
3. The aircraft maintenance manager is responsible for ensuringthat all
maintenance required to be carried out, and def rect maintstnds.
4. Workshop mang comp
AMC M.A.606(c) Personnel requirements
1. appr qual and exp.2. all nominated persons2.1 practicalexperience and expertise in the application of aviation safety
standards and safe maintenance practices;
2.2 comprehensive knowledge of:
a) CAR M and any associated requirements and procedures;b) themaintenance organisation manual;
2.3 five years aviation experience of which at least three yearsshould be
practical maintenance experience;
2.4 knowledge of the relevant type(s) of aircraft orcomponents
maintained;2.5. knowledge of maintenance standards.
AMC M.A.606 (d) Personnel requirements
1. all staff compliance orgn proce -MOM.2. To have sufficientstaff means directly.
3. Temp sub cont employed by another orgn and contracted bythis.
AMC M.A.606(e) Personnel requirements
1. per maint on the job evaluation.
2. Adequate initial and recurrent training
AMC M.A.606 (f) Personnel requirements1. cont a/w NDT means-spec by TC holder.
2. level 1,2, 3 stnd dgca.
3. 4.
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M.A.607 Certifying staff
a) cert staff can exer their privileges.
1. demo meet req dgca AME lic.
2. Adq understanding of a/c or comp .
b) where an aircraft is grounded at a location other than themain base
where no appropriate certifying staff is available, contr MO oneoff auth
- exposition.1. to one of its employees holding typequalifications on aircraft of similar
technology, construction and systems; or
2. to any person with not less than three years maintenanceexperience and
holding a valid ICAO aircraft maintenance licence rated for theaircraft
type requiring certification provided there is no organisationappropriatelyapproved under this CAR at that location and thecontracted organisation
obtains and holds on file evidence of the experience and thelicence of that
person.
reported to DGCA within seven days of the
M.A.608 Components, equipment and tools
a) orgn shall.1. equip and tools maint data or equiv MOM.2. demoaccess to other tools used occasionally.
b) tools controlled and calib.
5. NDT means FPI, MPI, EDDY CURR , ULTRA-SON AND RAD incl
X-ray and gamma ray.
6. new NDT Thermography and Shearography.7. qual proc for NDTAMO.
8. Boroscoping and other techniques such as delamination cointapping are
non-destructive inspections rather than non-destructivetesting.
9. ref stnds- MOM.10.
AMC M.A.607 Certifying staff
1. Adequate understanding = rec trng and maint exp.2. cert staffassesed -competence, qualification and capability.
3. orgn copies qual and exp of pers.
4. Rel maint exp = privileges of the certification authorisationand/or has
actually carried out maintenance.
AMC M.A.607 (c) Certifying staff
Min info to be kept.
AMC M.A.608 (a) Components, equipment and tools
1.2. clearly identified and listed in a control register.
3.
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M.A.609 Maintenance data
1. orgn app and curr maint data.
M.A.610 Maintenance work orders
written work order shall be agreed between the organisation andthe
organisation requesting maintenance.
M.A.611 Maintenance standards
All maint CAR-M subpart D.
M.A.612 Aircraft certificate of release to service
Comp of maint of a/c CRS subpart H.
M.A.613 Component certificate of release to service
Comp of comp maint CRS CA form 1 excp for stnd part andconsumable
part
AMC M.A.608 (b) Components, equipment and tools
1.procedure to inspect/service A clear system of labelling alltooling,
equipment and test equipment is therefore necessary givinginformation on
when the next inspection or service or calibration is due.2.Inspection, service or calibration equip manu instr.
AMC M.A.609 Maintenance Data
customer provided maintenance data, the scope of approvalindicated inthe MOM should be limited to the individualaircraft.
AMC M.A.613 Component certificate of release to service
1. A/C comp maintained off the aircraft requires the issue of acertificate
of release to service for such maintenance and another CRS toservice in
regard to being installed properly on the aircraft.2. componentsin storage prior to CAR145, CAR M and CAR 21 and not
released on a CA Form 1 or equivalent in accordance withM.A.501(a) or
removed serviceable from active aircraft which have beenwithdrawn fromservice CA FORM 1 issued.
-Which has been released without a CA Form 1 or equivalent-Usedon an aircraft and removed in a serviceable condition. Examples
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include leased and loaned aircraft components.
- Removed from aircraft which have been withdrawn from service,or
from aircraft which have been involved in abnormal occurrencessuch asaccidents, incidents, heavy landings or lightningstrikes.
- Components maintained by an unapproved organisation.
2.2 An appropriately rated M.A. Subpart F maintenanceorganisation-CA
FORM 1.2.3 appropriately rated means an organization with anapproval class rating
for the type of component or for the product in which it may beinstalled.
2.4 issued by signing in block 20 and stating "Inspected" inblock 12.
Block 13 when maint is carr, when manu, list of AD'S reprs andmods,Life used ser life lim parts, ref to history records anddetails.
2.5 New/unused comp.
2.5.1 CA FORM 1 MOM.
Note: maint release is not production release.
a) accp test report or statement.
b) insp for comp with manu instr and lim.c) storage lifeestablished.
2.5.2 if not possible dissassembled and inspected/tested.
2.6 Used aircraft components removed from a serviceableaircraft.
a) comp was rem by appr qual person.
b) deemed serviceable if the last flight operation with thecomponent fitted
revealed no faults.
c) insp.d) researce for any unusual event- servi.
e) history rec
f) comp of mods and rprs.g) flight hours/cycles/landings of anyser life lim comp -established.
h) comp with Ad's.i) block 13 info.
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M.A.614 Maintenance records
a) all details/rec prove all requirements have been met.
(b) The approved maintenance organisation shall provide a copyof each
certificate of release to service to the aircraft owner, withappr mod data.
c) copy of all maint rec 3 yrs from a/c was released.
1. 2.3. 2 yrs record dist last owner incase termination.
2.6.2 CA FORM 1 non dgca reg a/c leased/loaned by M.A SubpartF
orgn
2.7 Used aircraft components removed from an aircraft withdrawnfrom
service.
a) disman accomplished under the control of an organisationapproved
under M.A. Subpart F,b) following a satis assess.
c) satis components were removed and stored are compatible withthe
standards required by M.A. Subpart F.
d) Structured plan for dismant cert staff.
f) rec def should be rev.g) Dedicated control documentationdisassembly plan.
h) suitable removal and storage cond.
2.8. Used aircraft components maintained by organisations notapproved in
accordance with M.A. Subpart F. CAR 145 should establishsatisfactory
Dismantling, replacing ser life lim parts, reassem, and compcert req,
3. A certificate should not be issued for any component when itis known
that the component is unserviceable except in the case of ancomponentundergoing a series of maintenance processes-- block13.
AMC M.A.614 (a) Maintenance records
1. Properly executed and retained records.
AMC M.A.614 (c) Maintenance records
Only mods and rpr data. AMM CMM etc no retn but should indrevisionstatus.
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M.A.615 Privileges of the organisation
Maint orgn CAR M SEC A Subpart F.
(a) maintain any aircraft and/or component aprvl cert.
b) specialized services under the control of the maintenanceorganisation atanother organisation appropriately qualified- MOMapvd by Dgca.
c) a but at any loc MOM .
M.A.616 Organisational review
Orgn rev AMO cont CAR REQ
M.A.617 Changes to the approved maintenance organisation
approved maintenance organisation shall notify it of anyproposal to
carryout changes to persons accnt mang. Tools and equip. Nameand
location.
M.A.618 Continued validity of approval
a) Rem valid for max one year
Orgn comp with CAR, dgca granted access, appr not sus orrevoked.
M.A.619 Findings
(a) A level 1 finding is any significant non-compliances CARM
AMC M.A.616 Organisational review
1. AMO can deliver safe product.
2. The approved maintenance organisation should identify:
2.1. The person responsible for the organisational review,and;2.2. The frequency of the reviews, and;
2.3. The scope and content of the reviews, and;2.4. Thepersons
accomplishing the reviews, and;
2.5. The procedure for planning, performing and processingreview
findings.2.6. The procedure for ensuring corrective actions arecarried out in the
appropriate time frame.
3. Quality Sys CAR-145 is acptl sys. For orgn < 10.
AMC M.A.617 Changes to the approved maintenanceorganization
Without this paragraph the approval would automatically besuspended in
all cases.
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Lower safety stnds and hazard flt safety.
(b) A level 2 finding is any non-compliance with the CAR-Mrequirements
which could lower.demonstrate corrective action to thesatisfaction of DGCA within a period
of 7 days and 30 days for level 1 & level 2 findingsrespectively.
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SUBPART G CAMO
M.A.701 Scope
Requirements to qualify for the issue or continuation of anapproval for
CONT A/W MANG
M.A.702 Application
Issue or Variation - CA FORM 2 F
M.A.703 Extent of approval
a) appendix VI CA Form 14 CAMO Appro Cert and Appr Schedule.
b) Comm a/c opera CAMO Appr part of AOC/AOP issued by dgca.
c) scope CAM exposition
M.A.704 Continuing airworthiness management exposition
a) Information.1. Statement signed by Accnt Manager- all work-CAR & Expo.
2. The orgn scope of work.
3. names of personnel.
4. Organization Chart Chains of resp.
5. List of A/W review staff.
6. A gen desc and loc of facilities.
7. Procedures CAMO compliance with CAR-M.
8. CAM expo ammnd proc.
9. List of a/c Maint prog for non-comm generic and base.linemaint
prog.
b) CAM expo -apprv by Dgca.c) minor ammend- indirect approval,15 days before effectivity & proc
documented.
Subpart G - CONTINUING AIRWORTHINESS MANAGEMENT
ORGANISATION
AMC M.A.704 Continuing Airworthiness Management Exposition
1. Compliance with its contents will assure compliance with CARM
requirements.
2. A continuing airworthiness management exposition shouldcomprise:Part 0 General organisation
Part 1 Continuing airworthiness procedures
Part 2 Quality system or organisational review (asapplicable)
Part 3 Contracted maintenance (for operators) management of
maintenance (liaison with maintenance organisations in the caseof noncommercial air transport)
Part 4 Airworthiness review procedures (if applicable)
3.example for a combined CAR -145 and M.A. Subpart Gorganisation:CAR -145 Exposition
Part 1 ManagementPart 2 Maintenance Procedures
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M.A.705 Facilities
Suitable offfice accom.
M.A.706 Personnel requirements
a) Acct Man Corporate authority CAM activities can be financedand
carried out CAR-M.
b) For comm a/c oper Acct Man activi as per AOC/AOP.
Part L-2 Additional line maintenance procedures
Part 3 Quality system and/or organisational review (asapplicable). It
should also cover the functions specified by M.A.712 qualitysystem.Part 4 Contracts with owners/operators. It should also covercontracted
maintenance (for operators) Management of maintenance (liaisonwith
maintenance organisations in the case of non commercial airtransport)
Part 5 Appendices (sample of documents)Part 7 Other Regulatorysupplement (if applicable)
Part 8 Reserved
Additional parts should be introduced covering thefollowing:
Part 0 General organisation
Part 6 Continuing airworthiness proceduresPart 9 Airworthinessreview procedures (if applicable).
4. pers familiar expo.
5. Per resp for amnd -expo.
6. the person responsible for the management of the qualitysystem or for
the organisational review should be responsible for monitoringand
amending -expo; unless agreed by dgca.Amnd contr section of expoclass of amnd prior consent of dgca.
7. EDP .
8. Part 0 statement of acnt mang.9. abv statement.
10. change of acnt mang new acnt mang should sign abvstatment.
AMC M.A.705 Facilities
can be in office subj suff room.
AMC M.A.706 Personnel requirements
1. The person or group of persons cont a/w mang structure.Individualmang or combined. quality system is in place it should beindependent
from the other functions.
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c) group of persons.
d) Post holder under 'c'.
e) The nominated post holder referred to in paragraph (d) shallnot beemployed by a CAR -145 approved organisation under contractto the
operator.
f) Sufficient approp qualified Staff.
g) All paragraph (c) and (d) persons shall be able to showrelevantknowledge, background and appropriate experience related toaircraft
continuing airworthiness.
h) qualification of all perso shall be recorded.
i) orgn exten ARC nominate person acceptable to dgca.
j) names of perso a, c, d & i updated in CAMO Expo.
M.A.707 Airworthiness review staff
a) appro a/w rev staff- issue a/w rev. Cert for approval.
1.comm air transstaff for a/c> 2730 MTOW except balloonsshall have.
a) atleast 5 yrs cont a/w exp.
b) appr AME Licence or aeronautical degree or equivalent.c)formal aero maint training.
d) A postn in orgn -appr resp.
e) 'b' may be replaced by additional 5 yrs exp.
2. comm air trans staff for a/c < 2730 MTOW exceptballoons.a) atleast 3 yrs cont a/w exp.
b) appr AME LIC or aero degree or equivalent
c) appro aero maint training.
2. abv task, size and complexity.
3. analysis of the tasks to be performed. No of persons andqual.
4. Nomn pers -4.1 practical exp.
4.2Knwldg of oper req and proc. AOC oper holder specs. Oper manlof
AOC holder.
4.3. knowledge of quality systems;4.4. five years relevant workexperience of which at least two years- aero
indus -appr pstn.
4.5 rel engg degree.
4.6 knwldg CAM expo.
4.7 a/c type.4.8 maint mehods
AMC M.A.706 (e) Personnel requirements
1. nominated post holder be employed by the organisationapproved underCAR 145- only person avbl.
2. only applies to contracted maintenance
AMC M.A.707 (a) Airworthiness review staff
1. A/W rev privileges
2.
3. An appropriate Rule 61 licence. It is not necessary tosatisfy the
experience requirements of Rule 61 at the time of the review.4.pstn means pstn as overall auth or indp from a/w mang proc.
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QQCar M notes
d) postn in orgn with appr resp.
e) b may be replace by addi cont a/w 4 yrs exp in.
b) a/w rev staff shall be given authorization when formally acptby dgcaafter comp of a/w rev under supervision.
c) orgn a/w rev staff demonstrate CAM exp.
d) orgn record of a/w rev staff for atleast 2 yrs fromtermination.
M.A.708 Continuing airworthiness management
a) cont a/w mang carried out CAR-M Section A subpart C.
b) for every a/c managed should have
1. devl and control maint programme for a/c man. As wellasreliability prog.if any.
2. Present maint prog to dgca for appro. or ammnd. Exceptfor
indirect appro. And provide a copy to owner not involved incomm
air trans.
3. Mana the appr of modi and repairs.
4. Maint carried out and CRS issued thereof as per CAR-M SectA
subpart H.5. AD's and oper directives are carried out.
6. Def discovered during scheduled maint are rep and correctedby
appr AMO.
7. A/c AMO when neccessary.
8. coordinate scheduled maintenance, the application of AD'S,the
replacement of service life limited parts, and componentinspection
9. to ensure the work is carried out properly.
10. manage and archive all continuing airworthiness recordsand/or
operator's technical log.
ensure that the mass and balance statement reflects the currentstatus of
the aircraft.c) incase of comm oper- not CAR 145 appr thenwritten maint contractwith CAR-145 for maint., AD's oper direc,etc. All contra shall be appr by
dgca.
AMC M.A.708 (c) Continuing airworthiness management
1. same as M.A. 708 c
2. Both the specification of work and the assignment ofresponsibilities
should be clear, unambiguous and sufficiently detailed. -- a/wis affect.3. Special attention should be paid to procedures andresponsibilities.
4. For line maintenance, the actual layout of the contract theIATA
Standard Ground Handling Agreement may be used as a basis.
5. contract another operator that is not directly approved underCAR -145
CAM expo such proc and list of CAR 145 contr.6. does not absolvethe operator- cont a/w resp.
7. all maint CAR-145 does not preclude a primarymaintenancearrangement with an operator that is not such anorganisation, when it
proves that such an arrangement is in the interest of theoperator by
simplifying the management.
AMC M.A.708 (c) (1) Continuing airworthiness managementunscheduled maintenance
maint contr are not neces rel maint act work orders.
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QCar M notes
Unscheduled line maint and comp maint shall be in individualwork
orders to CAR-145 AMO.
M.A.709 Documentation
a) appr CAMO shall hold and use applicable current maint data.Data
-owner insuch case CAMO keep such data for duration ofcontract.
b) for a/c not comm air tran may dev generic and baseline maintprog forinitial appr and this does not preclude need for A/c maintprog.
M.A.710 Airworthiness review
Full documented review of a/c records.1. airframe, engine andpropeller flying hours and associated flight cycles
have been properly recorded, and;
2. the flight manual is applicable to the aircraft configurationand reflects
the latest revision status, and;3. all the maintenance due onthe aircraft according to the approved
maintenance programme has been carried out, and;
4. all known defects have been corrected or, when applicable,carried
forward in a controlled manner, and;
5. all applicable airworthiness directives have been applied andproperlyregistered,
6. all modifications and repairs applied to the aircraft havebeen registered
and are approved according to CAR 21 or equipment, and;
7. all service life limited components installed on the aircraftare properlyidentified, registered and have not exceeded theirapproved service life
limit, and;
8. all maintenance has been released in accordance with thisPart of CAR ,
and;
9. the current mass and balance statement reflects theconfiguration ofthe aircraft and is valid, and;
10. the aircraft complies with the latest revision of its typedesign
approved/ accepted by the DGCA.
AMC M.A.710 (a) Airworthiness review
1. A full documented review is.
2. develop procedures for the airworthiness review staff toproduce a
compliance report that confirms comp rev and comp of CAR- M.
AMC M.A.710 (b) and (c) Airworthiness review
1. Phy survey maint.
2. - verf in flt.
3.
4. sample checks.
AMC M.A.710 (e) Airworthiness review
a copy of comp rep and phy sur dgca along with recom.
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b) CAMO a/w rev staff- physical survey.
c) phy survey.
d) the airworthiness review can be anticipated by amaximumperiod of 90 days without loss of continuity of theairworthiness review
pattern, to allow the physical review to take place during amaintenance
check.
e) airworthiness review certificate (CA Form 15b) when a/w revcompsatis.
f) a copy state of regis within 10 days
g) cannot sub contr.
h) inconcl dgca infor.
M.A.711 Privileges of the organization
a) CAMO
1.manage cont a/w of non comm appr cert.
2. comm AOC.3. arng contr lim cont a/w tasks under its qualitysys appr cert.
4. ext A/W RC.
M.A.712 Quality system
a) Quality sys Quality Mang to mont compliance.
b) -- mont all acti, mont contr maint. Mont comp with CAR.
c) rec stored atleast two yrs.
d) CAMO appr another CAR quality another CAR.e) In case ofcommercial air transport the M.A. Subpart G quality system
shall be an integrated part of the operator's qualitysystem.
f) small orgn qual sys = orgn rev.
AMC M.A.711 (b) Privileges of the organisation
When cont a/w rev it shall every year.
AMC M.A.712 (a) Quality system
1. proc ref best practices.
2. veri and vali before use.
3. feedback sys who rect and time scales.
4. indp qual audit repo rel depa for corre and rect time.5. Theaccountable manager should hold regular meetings with staff to
check progress on rectification. For large orgn qual mang day today basis
and accnt mang twice a year.
AMC M.A.712 (b) Quality System
1. obj ensure comp CAR.
2. essntl elem of qual sys is indp audit.
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M.A.713 Changes to the approved continuing airworthiness
organisation
notify proposal to carr changes to dgca.
Name, location, addt loc, accnt mang, persons and facilities
M.A.714 Record-keeping
b) where privi a copy of a/w rev cert it has exte.
c) until two years after the aircraft has been permanentlywithdrawn.f) when CAM is trans all rec trans.
g) where terminates rec trans to owner.
M.A.715 Continued validity of approvala) maximum period of oneyear unless spec . Valid
orgn remaining in comp CAR, DGCA granted access, appr not suspor
revoked,
3. indp audit -routine sample checks of all aspects of orgncapability
4.
5. complete single exercise or subdivided over the year periodinaccordance with a scheduled plan. not require each procedure tobe
checked against each product line- proc common to lines.theaudit time
periods specified in this AMC may be increased by up to 100%-dgca.
6. more than 1 loc- sys how these r intg and audit every locevery yr.7. rep should be raised.
8. carried out by personnel not responsible for the function,procedure.
9. quality plan orgn acpt to dgca.
AMC M.A.712 (f) Quality system
small orgn
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upon surre returned to dgca.
M.A.716 Findings
(a) A level 1 finding is any significant non-compliance withCAR-M-
lowers.
(b) A level 2 finding is any non-compliance with the CAR-M whichcould
lower safety stnds and haz flt safety.CAMO appr corr action planand demonstrate corrective action to the
satisfaction of the DGCA within a period of 7 days and 30 daysfor level 1
& level 2 findings.
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SUBPART H CERTIFICATE OF RELEASE TO SERVICE CRS
M.A.801 Aircraft certificate of release to service
a) excp for orgn CAR-145. CRS issued accor this part.
b) cert staff CAR-M SEC A subpart- F
DGCA AME lic excp for complex maint tasks.
Pilot owner
c) for light comm a/c AME Lic complex maint tasks.
d)unforeseen situations authorise any person, with not less thanthree years
of appropriate maintenance experience and holding prop qual.owner
1. keep in a/c rec details of work and qual of person.
2. Maint rechecked & rele by appr auth pers within 7days.
3. Notify CAMO or Dgca(no contr) within 7 days.
(f) A certificate of release to service shall contain as aminimum:
1. basic details of the maintenance carried out; and2. the datesuch maintenance was completed; and
3. the identity of the organisation and/or person issuing therelease toservice, the appr ref of orgn and cert staff if pilot orAme lic holder CRS
licence no.
4. a/w lim /oper lim.g) when the maintenance prescribed cannotbe completed, a certificate of
release to service may be issued within the approved aircraftlimitations.
h) CRS not iss when non comp or flt safety endng.
M.A.802 Component certificate of release to service
1. CRS comp of a/c maint.
2. auth rel cert CA Form 1 comp of maint on comp. Excp m.a.502 b& d.
Subpart H-CERTIFICATE OF RELEASE TO SERVICE
AMC M.A. 801 (b) Aircraft certificate of release to service
A certificate of release to service is necessary before flight,at the
completion of any defect rectification, whilst the aircraftoperates a flight
between scheduled maintenance checks.
AMC M.A.801 (d) Aircraft certificate of release to service
1.CRS statement
2. CRS -crss ref to AMP or manu inst/oper inst.3. date and lifeas appr.
4. ext maint crss ref to work pack
5. per sign normal sign or electronical means acpt to dgca.
6. clear, concise, legible record of the work.
7. AME Lic per should retain records req have been met.
AMC M.A.801 (e) Aircraft certificate of release to service
1. una to esta comp maint not comp avbl a/c maint downtime isless.
2. The aircraft owner or M.A. Subpart G organisation isresponsible forensuring that all required maintenance has beencarried out before flight.
3. If a certificate of release to service is issued withincomplete
maintenance a record should be kept stating act mech/engi tobring this
to notice of owner/subpart G orgn.
AMC M.A.801 (f) Aircraft certificate of release to service
Hazard seriously the flight safety means any instance wheresafe
operation could not be assured or which could lead to an unsafecondition.
AMC M.A.802 Component certificate of release to service
CA Form 1 not neces for inte rels proc. But all info CRS.
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M.A.803 Pilot-owner authorization
a) pilot- owner maint.
1. valid pilot licence for the type or class rating.
2. own the aircraft, either as sole or joint owner.b) priv opernon-complex motor powered a/c
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SUBPART IAIRWORTHINESS REVIEW CERTIFICATE
M.A.901 Aircraft Airworthiness Review
a) CA Form 15a DGCA or b M.A. Subpart G after comp of a/wrev.
b) cont environment.
i) last 12 mnts CAMO.ii) Last 12 mnts AMO subpart f orCAR-145.
c) a/c comm air trans > 2730kg excp balloons MTOW cont a/wmang by
CAMO in cont envi.
-- issue ARC
-- ARC it issued extend twice the validity of theairworthinessreview certificate for a period of one year eachtime;
d) abv a/c not in cont envir or cont a/w mang by CAMO(with ARCpriv).
Dgca ARC based on recomm from approved CAMO.
e) a/c non comm
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M.A.902 Validity of the airworthiness review certificate
(a) An airworthiness review certificate becomes invalid if:
1. suspended or revoked; or
2. the airworthiness certificate is suspended or revoked; or3.the aircraft is not on the aircraft register of DGCA; or
4. the type certificate under which the airworthinesscertificate was issued
is suspeded or revoked.
M.A.903 Transfer of aircraft registration within India.
a) 1. inform DGCA;
2. apply to DGCA for the amendment of the Certificate of
Registration in accordance with CAR Section-2, Series F,PartI.
b) notwithstanding the formerairworthiness review certificateshall remain
valid until its expiry date.
M.A.904 Airworthiness review of aircraft imported into India
a) importing a/c into india applicant- apply C OF A, for useda/c ARC and
all maint AMP
b) CAMO doc recomm to dgca for ARC
d) new C OF A dgca.e) ARC valid for one year unless dgcaless.
AMC M.A.903 (a) - 1 Transfer of aircraft registrationwithinIndia.
Notify dgca for proper trnsf
AMC M.A.903 (b) Transfer of aircraft registration withinIndia:
owner/oper verify that DGCA has entered the new aircraftregistration, if
any, on the existing airworthiness review certificate andvalidated thechange.
AMC M.A.904 (a)-1 Airworthiness reviews of aircraft importedintoIndia
inform dgca 10 working days in adv time and loc of rev.
AMC M.A.904 (a)-2 Airworthiness reviews of aircraft importedintoIndia
when no CAMO avbl DGCA a/w rev. Req with 30 days notice.
AMC M.A.904 (b) Airworthiness review of aircraft importedinto
IndiaThe recommendation sent to DGCA should contain at least
(a) General information.
(b) Aircraft information.
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M.A.905 FINDINGS.
( c) Documents accompanying the recommendation.
(d) Aircraft status.
(e) Aircraft survey.(f) Findings.
Maint and Aircraft check flight
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