New Misc Mod

8/18/2019 New Misc Mod

1/36

DGCA Mandatory Modifcation ListMODIFIED “ DGCA / NEW-MISC / ” MODIFICATION LIST

DGCA NO Su!"ct #"$"r"nc" AD Co%&'ianc" A&&'icai'ity #"%ar(s

DGCA/NM/01 MAGNETIC PARTICLE INSPECTION OF

UNDERCARRIAGE BOLTS OF AGRICULTURAL

AIRCRAFT.

DGCA LETTER NO.

77-5/69-AI(I) DT.

24/5/1969.

As in AD As in AD

DGCA/NM/02 M-3 TYPE GENERATORS INSPECTION OF

SUPPORT LUG AT COMMUTATOR FRONT

END HOUSING FOR CRACKS.

DGCA LETTER NO.

9-414/AI(II) DT.

11/11/74

As in AD As in AD

DGCA/NM/03 "NO SMOKING" PLACARD TO BE INSTALLED ON

LAVATORY DOOR TO PREVENT FIRES FROMSMOKING MATERIALS BEING DROPPED INTO

LAVATORY PAPER OR LINEN WASTE RECEPTACLES.

SUPERSEDED BY DGCA/NEW MISC/03R1 VIDE LETTER NO. M-

4/48 DT. 25.04.12.

DGCA/NM/04 INSTALLATION OF 'G'-METER DURING CLOUD

SEEDING OPERATION.

DGCA LETTER NO.

4/26/73-AI(I) DT.

20/6/74

As in AD As in AD

DGCA / NM /05 PAINTING OF HELICOPTERS ENGAGED IN AGRO

OPERATION WITH "DAY GLOW" PAINT.

DGCA LETTER

NO.78/111/75-AI(I)

DT. 23/3/77

As in AD As in AD

DGCA / NM / 06 FREQUENCY TOLERANCE LIMIT FOR TRANSMITTERS

REV.1

DGCA LETTER

NO. 4-18/79 AI(1)DT .February 1992

DT 27 TH FEB.,

1992

As in AD As in AD

Updated on 15.09.15 1


2/36

DGCA / NM / 07 IMPROVED LUBRICATION AND INSTALLATION OF

MODIFIED DISTRIBUTOR BLOCK IN BENDIX

SCINTILLA 'S' TYPE MAGNETOS.

BENDIX SB NO.

551A & 566

As in AD & SB As in AD


DGCA / NM / 08 IDENTIFICATION OF AIRCRAFT PIPELINES. ISI SPECIFICATION

NO. IS 6753-1972

As in AD As in AD

DGCA / NM / 09 CANCELLED IN VIEW OF DGCA/NEW MISC/84 VIDE LETTER NO 9-414/04 DATED 06/10/05

DGCA / NM / 10 "FASTEN SEAT BELT WHILE SEATED", SIGN OR

PLACARD ON EACH FORWARD BULKHEAD AND ON

EACH PASSENGER SEAT BACK.

FAR PART

121.317(b)

As in AD As in AD

DGCA / NM / 11 INSPECTION/ REPLACEMENT OF GEAR

DISTRIBUTOR OF BLOCK OF BENDIX S-1200 SERIESMAGNETOS.

FAA AD 82-13-01 &

BENDIX SB NO.613

As in AD As in AD

DGCA / NM / 12 EXAMINATION OF ENGINE INVOLVED IN PROPELLER

STRIKE INCIDENTS.

DGCA LETTER NO.

9-414/81-AI(II) DT.

14/9/82

As in AD As in AD

DGCA / NM / 13 REPLACEMENT OF PAPER INDUCTION AIR FILTERS. FAA AD 84-26-02 As in AD As in AD

DGCA / NM / 14 LIGHTING FOR INTERIOR EMERGENCY EXIT

MARKINGS

FAR 121.310(c) As in AD As in AD

DGCA / NM / 15 SERVICING OF AIRCRAFT TYRES WITH NITROGEN

GAS

FAA AD 87-08-09 As in AD As in AD

DGCA / NM / 16 INSPECTION OF IPECO CREW SEATS. FAA AD 90-09-08 As in AD As in AD



3/36

DGCA / NM / 17 PRECAUTIONARY CHECK FOR CORRECT LOCATION

OF BRIDGE PIECES INSIDE THE MAIN BUOYANCY

TUBES.

CAA AD 001-02-93

AND SB 25-46

As in AD As in AD


DGCA / NM / 18 INSPECTION/REPLACEMENT- EQUIPMENT AND

FURNISHINGS- PASSENGER COMPARTMENT.

CAA AD 006-03-93

AND FLIGHT

EQUIPMENT AND

ENGINEERING SB

25-20-1287R2

As in AD As in AD

DGCA / NM / 19 COLLINS- VHF- 20B TRANSCEIVERS

INDENTIFICATION PLATE

BVAD NO. 93-050

(AB) REV.1

AND SIL 3-92 DT.

DEC. 11' 1992

As in AD As in AD

DGCA / NM / 20 TO PREVENT DISRUPTION OF THE FUEL FLOW TO THE ENGINE RESULTING IN FAILURE TO ATTAIN

RELATED POWER

BLA AD 1998-007- AB& FAA AD 98-01-

06

As in AD As in AD

DGCA / NM / 21 INSPECTION/REPLACEMENT- AFFECTED MAGNETO

CAPACITORS

FAA PRIORITY

LETTER 94-06-09

AND TCM CRITICAL

SB 641 DT. FEB. 1

'1994

As in AD As in AD

DGCA / NM / 22 SIGMA AERO SEAT-PASSENGER SEATS- AFT TRACK

FITTINGS

DGAC AD

1994-085 (AB) R2

As in AD As in AD

DGCA / NM / 23 UP LIMIT POSITION SECURITY. BVAD 94-116(B). As in AD As in AD

DGCA / NM / 24 NAVIGATION - VHF/NAV RECEIVER MODIFICATION. BLA AD

-

As in AD As in AD

- -



4/36


DGCA / NM / 26 TO PREVENT COMPRESSOR WHEEL RUPTURE

WHICH COULD RESULT IN AN UNCONTAINED APUFAILURE AND DAMAGE TO THE AIRCRAFT


DGCA / NM / 27 SIGMA AERO SEAT(PAX SEAT) LEG COLLAR BVAD 97-134(AB) As in AD As in AD

DGCA / NM / 28 TO PREVENT THE TRANSMISSION OF MISLEADING

ENCODING ALTIMETER INFORMATION BETWEEN

AFFECTED AIRCRAFT


DGCA / NM / 29 VACCUM DRY AIR PUMP FLEXIBLE COUPLING -

INSPECTION/REPLACEMENT

BLA AD 1998-

141/2 & FAA AD

98-23-01

As in AD As in AD

DGCA / NM / 30 TO PREVENT SMOKE & A POSSIBLE FIRE IN THECOCKPIT CAUSED BY OVERHEATING OF THE

ELECTRIC DOOR SEAL INFLATION SYSTEMS

FAA AD 98-21-21R1As in AD As in AD M-4/282 Dt.25-04-2000

DGCA / NM / 31 TO PREVENT FAILURE OF THE SEAT RESTRAINT

SYSTEM

FAA AD 98-25-10R1As in AD As in AD M-4/279 Dt.

28-04-1999

DGCA / NM / 32 TO PREVENT DEVIATION FROM AN INTENDED

FLIGHT PATH DURING A NON PRECISION APPROACH

FAA AD 97-05-03R1As in AD As in AD

DGCA / NM / 33 TO PREVENT REDUCED OXYGEN CONSUMPTION WHEN PASSENGERS ARE REQUIRED TO USE

DEFECTIVE OXYGEN MASKS, WHICH COULD RESULT

IN PASSENGER INJURY.




5/36


6/36


DGCA / NM / 43 TO PREVENT AN UNCONTAINED APU FAILURE &

DAMAGE TO THE AIRPLANE

FAA AD 2000-04-24As in AD As in AD

DGCA / NM / 44 SIGMA AERO SEAT - MODIFICATION OF SEAT BELT

ATTACHMENT FITTING

DGAC AD 2002-471

(AB)R1

As in AD As in AD M-4/323 Dt.

18-04-2002

DGCA / NM / 45 TO PREVENT LOSS OF THE MAIN SOURCES OF

ATTITUDE DATA


DGCA / NM / 46 TO PREVENT FAILURE OF THE MAGNETO IMPULSE

COUPLING, RESULTING IN SEIZURE OF THE ENGINE

FAA AD 99-04-04 As in AD As in AD M-4/1030

Dt. 06-02-

2001

DGCA / NM / 47 CARGO & BAGGAGE COMPARTMENT FAR 121.314 (C) As in AD As in AD

DGCA / NM / 48 TO PREVENT UNDESIRABLE AUTOTRIM COMMAND FAA AD 2001-10-09As in AD As in AD

DGCA / NM / 49 TO PREVENT INACCURATE NAVIGATION DUE TO

INCORRECT BEARING INFORMATION

FAA EMERGENCY

AD 2001-14-51

As in AD As in AD

DGCA / NM / 50 TO MODIFY THE ALTITUDE ENCODER INPUTS OF

THE CTL-92 TRANSPONDER CONTROL PANELS.


DGCA / NM / 51

(R2)

TO PREVENT FAILURE OF THE FUEL REGULATOR

SHUTOFF VALVE.

FAA AD

2004-25-16R1

As in AD As in AD

DGCA / NM / 52 TO PREVENT ENGINE FUEL PUMP FAILURE. FAA AD

2001-17-15

As in AD As in AD



7/36


DGCA / NM / 53 TO PREVENT DAMAGE TO THE FIRE EXTINGUISHING

SYSTEM COMPONENTS


DGCA / NM / 54 MODIFICATION OF AIRCRAFT COCKPIT DOORSSFAR 92-4, FAR 121.583,FAR 25.795 & FAR121.313

As in AD As in AD

DGCA / NM / 55 HYDROLOK PIN ORIENTATION CAA AD 002-11-

2001

As in AD As in AD

DGCA / NM / 56 REVISED VIDE LETTER NO. M-4/342 DT. 23-11-2011.

DGCA / NM / 57 GNS 430 UNITS TO PREVENT INACCURATE COURSE

DEVIATION DISPLAYS


DGCA / NM / 58 TO PREVENT IMPELLER FAILURE FROM CRACKS IN

THE IMPELLER BACK FACE AREA

FAA AD

2002-03-09R1

As in AD As in AD

DGCA / NM / 59 TO PREVENT TRANSMISSION OF INACCURATE DATA

CONCERNING ALTITUDE FROM ONE AIRPLANE TO

ANOTHER

FAA AD 2002-06-05

& FAA AD 2002-06-

06

As in AD As in AD

DGCA / NM/ 60 TO PREVENT UNWARRANTED DISPLAY OF THE ADC

FLAG


DGCA / NM/ 61 TO REPLACE AFFECTED COMPRESSOR WHEELS FAA AD 2002-15-02As in AD As in AD

DGCA / NM/ 62 INSTALLATION OF CVR DGCA LETTER NO.

9-414/2002-AI(2)

As in AD As in AD



8/36


DGCA / NM/63 INSTALLATION OF FDR DGCA LETTER NO.9-414/2002-AI(2)

DATED 30.09.2002

As in AD As in AD

DGCA / NM/64 PASSENGER SEATS- CENTRAL SPREADERS

MODIFICATION

DGAC AD

2002-504 (AB)

As in AD As in AD

DGCA / NM/65 TO PREVENT DISPLAY OF ERRONEOUS PRIMARY

FLIGHT AND ENGINE PARAMETER INFORMATION

FAA AD

2002-20-09

As in AD As in AD

DGCA / NM/66 TO PREVENT THE FMC FROM RETAINING INCORRECT

INFORMATION

FAA AD

2002-22-13

As in AD As in AD

DGCA / NM/67 TO PREVENT FAILURE OF HOSE WHEN EXPOSED TO

FIRE

FAA AD 2002-22-12

(Corrected)

As in AD As in AD

DGCA / NM/68 TO PREVENT FAILURE OF THE EMERGENCY

EMERGENCY EVACUATION SLIDE RAFT


DGCA / NM/69 EQUIPMENT: BABIES BASSINETS DGAC AD

2001-351(B)

As in AD As in AD

DGCA / NM/70 TO PREVENT MOOUNTING BRACKET FAILURE AND

SEPARATION OF THE RESCUE HOIST FROM THE

HELICOPTER


DGCA / NM/71 REVISED TO DGCA/NM/71(R1)



9/36

DGCA / NM/72 KIDDLE AEROSPACE HAND HELD HALON FIRE

EXTIGENISHES-

DGCA letter No.

9-414/2003-AI(2)

dated 22-5-03

As in AD As in AD


DGCA / NM/73 TO DETECT UNSAFE CONDITIONS THAT COULDRESULT IN SEPARATION OF A PROPELLER BLADE

FAA AD2003-13-17

As in AD As in AD

DGCA / NM/74 AIR CARGO PALLETS AND AIR CARGO NETS LBA AD

2002-303

As in AD As in AD

DGCA / NM/75 TO PREVENT APU COMPARTMENT FIRES AND FUEL

VAPOUR EXPLOSION

FAA AD

2003-15-07

As in AD As in AD

DGCA / NM/76 TO DETECT AND CORRECT DEFECTIVE SAFETY

BELTS AND RESTRAINT SYSTEMS.

FAA AD 2003-26-06

DGAC AD

2002-104(AB)R2 &

2002-105(AB)R2

As in AD As in AD

DGCA / NM/77 TA/RA VSI-TCAS INDICATOR THALES AVIONICS DGAC AD

F-2004-053

As in AD As in AD

DGCA / NM/78 TO PREVENT THE LOADING OF THE BARO SET

POTENTIOMETER WHICH COULD RESULT IN AN

UNACCEPTABLE ALTITUDE.

FAA AD

2004-08-15

As in AD As in AD

DGCA / NM/79R1 TO PREVENT INTERROGATING AIRCRAFT FROM

POSSIBLY RECEIVING INACURRATE REPLIES.

FAA AD 2005-01-19

(Original FAA AD

2004-10-15 is

As in AD As in AD

DGCA/NM/80 TO PREVENT THE GPS NAVIGATION UNIT UNDERCERTAIN CONDITION, FROM PROVIDING

ERRONEOUS CROSS NAVIGATION INFORMATION.

FAA AD2004-13-20

As in AD As in AD



10/36

DGCA/NM/81 OPERATIONAL ORDER ON INSTRUCTION FOR

CONTINUED AIRWORTHINESS FOR LARGE AIRPLANE

CERTIFICATED UNDER JAR-25.

DGAC -AD -F

2004-083

As in AD As in AD


DGCA/NM/82 EQUIPMENT/ FURNISHINGS-LERMER GmbH

WATER BOILERS.

DGAC- AD- F

2004-132

As in AD As in AD

DGCA/NM/83

TO PREVENT SHIFTING OF UNRESTRAINEDCARGO IN THE CARGO COMPARTMENTWHICH COULD CAUSE AN UNEXPECTEDCHANGE IN THE AIRPLANE’S CENTER OF

GRAVITY

FAA AD2004-22-01

A !" AD A !" AD

DGCA/NM/84TO PREVENT FAILURE OF TE !A"NETO I!PUL#E$OUPLIN" A##E!%L& AN' PO##I%LE EN"INE

FAILURE

FAA AD200#-12-0$ A !" AD A !" AD

DGCA/NM/8#

TO CORRECT PRO%LEMS WITH THE STAND%YVACUUM SYSTEMS &SVS' %EFORE FAILURE ORMALFUNCTION DURING INSTRUMENT FLIGHTRULES &IFR'

FAA AD2005-11-05 A !" AD A !" AD

DGCA/NM/8$

E(UIPMENT / FURNISHINGS INSPECTION ANDREPLACEMENT OF THE READING LIGHTS

ELECTRICAL POWER SUPPLIES OF SOME SICMAAERO SEATS)

DGAC AD

F-2005-135 A !" AD A !" AD

DGCA/NM/8* TO PREVENT CERTAIN AIR DATA COMPUTERS&ADC' FROM DISPLAYING INCORRECT ALTITUDEINFORMATION &SHADIN ADC 2000'

FAA AD200#-2#-08 A !" AD A !" AD



11/36

DGCA/NM/88 TO PREVENT VACCUM PUMP FAILURE ORMALFUNCTION DURING INSTRUMENT FLIGHTRULES IFR' FLIGHT)

FAA AD200$-03-08

A !" AD A !" AD

DGCA/NM/8+ TO IDENTIFY AND PROVIDE CORRECTIVE A,TIONFOR A POTENTIALLY INOPERATIVE SMOEDETECTOR)

FAA AD2006-04-04

A !" AD A !" AD

DGCA/NM/+0

TO PREVENT LOSS OF PRESSURE IN THE ESCAPESLIDES/RAFTS AFTER ANEMERGENCY EVACUATION

FAA AD2006-12-08 A !" AD A !" AD



12/36


DGCA/NM/91TO PREVENT A BEARNG ERROR, !"C"CO#$D $EAD TO AN ARP$ANE DEPARTNG

FROM TS SC"ED#$ED F$G"T PAT".

FAA AD2006-16-18

A% ' AD A% ' AD

DGCA/NM/92TO PREVENT T"E TRANSPONDER OF T"E COM#NT FROM GONG NTO STANDB( MODE

FAA AD2006-19-04 A% ' AD A% ' AD

DGCA / NM/ 93E)#PMENT & F#RNS"NG - PASSENGERSEATS REAR FTTNG ASSEMB$( ATTAC"MENT - REP$ACEMENT

EASA AD2006-0264 A% ' AD A% ' AD

DGCA / NM/ 94TO PREVENT TREAD SEPERATON FROM ANOSE!"EE$ TRE D#RNG TA*EOFF OR$ANDNG

FAA AD2006-18-08 A% ' AD A% ' AD

DGCA/NM/95$ANDNG GEAR MAN $ANDNG GEAR !"EE$ ASSEMB$(-NSPECTON/REPAR.

EASA AD2006-0328

A% ' AD A% ' AD

DGCA/NM/71+R1 REVSED TO DGCA/NM/71+R2

DGCA/NM/96E)#PMENT & F#RNS"NGS-PASSENGER SEATBAC*REST NSPECTON/ REP$ACEMENT.

EASA AD2008-0135

A% ' AD A% ' AD

EASA AD

2006-0350

#UPER#EE'E

' %& d()a

LETTER NO.A*31+514 'T.

29*08*08

DGCA/NM/97TO PREVENT DETAC"MENT OF PASSENGERSEATS ASSEMB$ES D#RNG EMERGENC(CONDTONS.

FAA AD2007-04-15

A% ' AD A% ' ADM-4/187 .

30.03.07



13/36

DGCA NO Su!"ct#"$"r"nc"

ADCo%&'ian

c"A&&'icai'it

y#"%ar(s

DGCA/NM / 98 R1 TO PREVENT C($NDER SEPARATON FAA AD2007-04-19 +R1

AS N AD AS N AD '.M-4/311

. 07-05-07.DGCA/NM / 99 O(GEN---O(GEN RESERVE C($NDERS----

REMOVA$/EMPT(NGEASA AD

2006-0286R1 AS N AD AS N AD

M-4/262 . 24-04-07

DGCA/NM / 100 TO PREVENT S"FT N FMS COMP#TED POSTON FAA AD2009-08-01

AS N AD AS N AD $ '. A-31/310. 22-05-09

DGCA/NM / 101 AR TRANSPORT ASSOCATON OF AMERCA +ATACODE 34 NAVGATON.

FAA AD2007-14-06

AS N AD AS N AD '. A-31/535. 19-09-07.

DGCA/NM / 102 E)#PMENT & F#RNS"NG- SEAT RESTRANTS(STEM P$ASTC ROTAR( B#C*$E "AND$E-

NSPECTON/ REP$ACEMENT.

EASA AD2007-0256

AS N AD AS N AD '. A-31/18

. 23-10-07

DGCA/NM / 103 CVR- T"E B#$* ERASE FAC$T( S"O#$D BEDEACTVATED REMOVNG T"E RE$EVENT CARDFROM T"E CVR #NT.

DGCA $ETTERNO. 9-414/96-A+2 DT. 24T" SEP.

AS N AD AS N AD

R ''.

DGCA/NM / 104 RS* OF "G" PRESS#RE O(GEN C($NDERTEARNG.

FAA AD2007-26-11

AS N AD AS N AD '. A-31/141. 22-02-08

DGCA/NM/105 TO PREVENT FA$#RE OF AN EVAC#ATONS(STEM.

FAA AD2008-06-27

AS N AD AS N AD $ N. A-31/267. 30-04-08

DGCA/NM/106 NAVGATON S(STEMS- MODES TRANSPONDER-

MODFCATON/ REP$ACEMENT

EASA AD

2008-0159

AS N AD AS N AD

$ '. A-31/601. 15-10-08

DGCA/NM/107 AR CONDTONNG-:ONA$ DR(NG S(STEMDEACTVATON.

EASA AD2006-0140R4

AS N AD AS N AD$ '. A-31/346. 25-05-09



14/36


ADCo%&'ian

c"A&&'icai'it

y#"%ar(s

DGCA/NM/108 TO PREVENT T"E POTENTA$ OF GNTONSO#RCES NSDE F#$E TAN*S, !"C" NCOMBNATON !T" F$AMMAB$E F#E$ VAPORSCO#$D RES#$T N F#E$ TAN* EP$OSONS AND

CONS)#ENT $OSS OF T"E ARP$ANE.

FAA AD2008-22-01

AS N AD AS N AD $ '. A-31/37. 02-12-08

DGCA/NM/109TO PREVENT AP# COMPARTMENT FRES & F#E$VAPO#R, EP$OSON.

FAA AD2003-15-07

AS N AD AS N AD $ '. A-31/235. 02-04-09

DGCA/NM/110 TO PREVENT CONDTON FROM ESTNG !"ENPFD% DSP$A( NCORRECT ATTT#DS, A$TT#DES AND ARSPEED NFORMATON.

FAA AD2009-05-05

AS N AD AS N AD $ '. A-31/300dt. 11*05*09

DGCA/NM/111COMM#NCATONS T"A$ES COMM#NCATONV"F DATA RADO MODFCATON.

EASA AD2006-0334 R1

AS N AD AS N AD $ '. A-31/354. 01-05-09

DGCA/NM/112

REVSED TO DGCA/NM/112+R1.

DGCA/NM/113 MP$EMENTATON OF FEDRA$ AVATON ADMNSTRATON +FAA R#$ES REGARDNGCRAS" !ORT"NESS STANDARD FORPASSENGER OPERATON.

FAR PART121.311

AS N AD AS N AD $ ' A-31/761DT.15-09-09;


15/36


ADCo%&'ian

c"A&&'icai'it

y#"%ar(s

DGCA/NM/117

REVSED TO DGCA/NM/117+R1

DGCA/NM/117+R1

ARTRANSPORT ASSOCATON ATA OF AMERCACODE26 FRE PROTECTON

FAA AD 2010-01-03

AS N AD AS N AD $ETTER NO. A-31/132DT. 09-02-2010

DGCA/NM/120

FRE PROTECTON-PORTAB$E "A$ON 1211 FREETNG#S"ERS, DENTFCATON/ REP$ACEMENT.

EASA AD2009-0278

AS N AD AS N AD V; ''

DGCA/NM/121 EMERGENC( $OCATOR TRANSMTTER-POTENTA$, FA$#RE TO TRANSMT T"E

RE)#RED 406 M": CODED SGNA$.

TC AD CF2009-44

AS N AD AS N AD VDE DGCA $ETTERNO. A-31/

. 09-02-10

DGCA/NM/122

REVISED TO DGCA/NEW MISC/122R1 VIDE DGCA LETTER NO. S-4/ 182 DT. 11.11.14

DGCA/NM/114R1 TO PREVENT FA$#RE OF A "OO* D#RNGRESC#E "OST OPERATONS, $OSS OF T"ERESC#ED PASSENGER AND S#BS)#ENTSERO#S N=#R( OR FATA$T(.

FAA AD2010-03-02

AS N AD AS N AD $ ' A-31/307DT. 8-3-2010

DGCA/NM/118R1 TO PREVENT AN O(GEN C($NDER FROMR#PT#RNG, !"C", DEPENDNG ON T"E

$OCATON, CO#$D RES#$T N STR#CT#RA$DAMAGE & RAPD DECOMPRESSON OF T"E

FAA AD2009-10-10R1

AS N AD AS N AD VDE DGCA $ETTERNO. A-31/299

DT. 08-03-10

DGCA/NM/119R1

FRE PROTECTON-"A$ON 1211 FREETNG#S"ERS, DENTFCATON/ REP$ACEMENT.

EASA AD2009-0262R1

AS N AD AS N AD VDE DGCA $ETTERNO. A-31/291

. 08-03-10



16/36


ADCo%&'ian

c"A&&'icai'it

y#"%ar(s

DGCA / NM/71 R2 TO ENSURE THAT THE FLIGHTCREW HAS AN

ACCURATE GLIDESLOP DEVIATION INDICATION

FAA AD

2010-07-02

As in AD As in AD Letter n o. A-31/482 dt.

07-05-10

DGCA/NM/112R1

NAVGATON-MODES TRANSPONDER-C"EC*/MODFCATON.

EASA AD2009-0067

AS N AD AS N AD $ '. A-31/455. 11-05-10

DGCA/NM/123 TO PREVENT SEPERATON OR SE:#RE OF T"ET#RBOC"ARGERT#RBNE !"C" CO#$D RES#$TN F#$$ OR PARTA$ ENGNE PO!ER $OSS, $OSSOF ENGNE O$& SMO*E N T"E ARP$ANE CABN.

F AA AD2010-07-08

AS N AD AS N AD VDE $ETT. NO. A-31/496DT. 11-05-10

DGCA/NM/124O(GEN C($NDER-NSPECTON / REP$ACEMENT-TO PREVENT O(GEN C($NDER FROMR#PT#RNG

F AA AD2010-11-05

AS N AD AS N AD VDE DGCA $ETTERNO. A-31/ 568

. 07-07-10

DGCA/NM/125 TO PREVENT $OSS OF PROPE$$ER PTC"CONTRO$ ,DAMAGE TO T"E PROPE$$ERGOVERNOR AND NTERNA$ DAMAGE TOT"EENGNE !"C" CO#$D PREVENT CONTN#EDSAFE F$G"T OR SAFE $ANDNG.

F AA AD2010-13-10

AS N AD AS N AD VDE DGCA $ETTERNO. A-31/ 655

. 09-08-10

DGCA/NM/126 COMM#NCATON- VER( "G" FRE)#ENC(+V"F/AM TRANSCEVER- MODFCATON

EASA AD2010-0186

AS N AD AS N AD VDE DGCA $ETTER NO A-31/280 DT 15-10-10

DGCA/NM/127 R% 127+R1



17/36

DGCA/NM/115R1NAVGATON-MODE S TRANSPONDER-MODFCATON/ REP$ACEMENT.

EASA AD2009-0173R1

AS N AD AS N AD $ '.- A31/930

't* 10*11*10



18/36


ADCo%&'ian

c"A&&'icai'it

y#"%ar(s

DGCA/NM/128 F$G"T CONTRO$-T#RNB#C*$E- NSPECTON EASA AD2010-0233

AS N AD AS N AD VDE DGCA $ETTER NO.M-4/118-19 . 30-12-

DGCA/NM/129 AR TRANSPORT ASSOCATON +ATA OF AMERCA CODE35 O(GEN. FAA AD 2011-01-09 AS N AD AS N AD VDE DGCA $ETTER NO.M-4/43 . 29-03-11

DGCA/NM/130R1 REVISIED TO DGCA/ NEW-MISC/ 130R2 VIDE DGCA LETTER NO. M-4/ 164 DT. 25.08.2015

DGCA/NM/131 ATA 34 >NAVGATON S(STEMS >MODE S TRANSPONDERCONTRO$ PANE$S -MODFCATON

EASA AD 2011-0043

AS N AD AS N AD VDE DGCA $ETTER NO.M-4/60. . 04-05-11

DGCA/NM/132 REVSED TO 132+R1

DGCA/NM/133 ATA 25 > E)#PMENT AND F#RNS"NG-$FE =AC*ET

VAC##M BAG-MODFCATON

EASA AD 2011-

0094

AS N AD AS N AD VDE DGCA $ETTER NO.

M-4/169 . 30-06-11DGCA/NM/134 ATA 25- E)#PMENT/ F#RNS"NG-E$T ANTENNA-

MODFCATON/REP$ACEMENT.EASA AD 2011-

0103 AS N AD AS N AD VDE DGCA $ETTER NO.

M-4/175 . 30-06-11

DGCA/NM/127R1 ATA 34 NAVGATON S(STEMS -MODE S TRANSPONDER-MODFCATON/ REP$ACEMENT.

EASA AD 2010-0204

+CORRECTON07-06-2011

AS N AD AS N AD VI'E '"$A LETTER NO.!*4+170 dt. 12*07*11

DGCA/NM/135 ATA 25 > E)#PMENT AND F#RNS"NG-PASSENGERSEAT REP$ACEMENT

EASA AD 2011-0098


DGCA/NM/136 =ONT ARCRAFT SSTEM/COMPONENT+=ASC CODE2622FRE BOTT$E,PORTAB$E.

FAA AD 2011-11-04


DGCA/NM/132R1 ATA 35 O(GEN MAS* REG#$ATOR NF$ATAB$E"ARNESS-DENTFCATON/REP$ACEMENT EASA AD 2011-0090 R1 AS N AD AS N AD VDE DGCA $ETTER NO.M-4/230 DT. 14/09/11

DGCA/NM/137 ATA 35 O(GEN. FAA AD 2011-14-08

AS N AD AS N AD VI'E '"$A LETTER NO.!*4+239 'T. 14+09+11

DGCA/NM/56+R1 ATA 25-E)#PMENT/F#RNS"NGS FAA AD 2011-21-08

AS N AD AS N AD VI'E '"$A LETTER NO.!*4+342 'T. 23+11+11



19/36


ADCo%&'ian

c"A&&'icai'it

#"%ar(s

DGCA/NM/138 REVI#E' VI'E LETTER NO. !*4*92 'T. 26.06.12

DGCA/NM/139 ATA 34- NAVGATON RADO A$TMETER NDCATORMODFCATON

EASA AD 2011-0239

AS N AD AS N AD VI'E '"$A LETTER NO.!*4+398 'T. 15*01*12

DGCA/NM/140 TO NSTA$$ P$ACARDS TO AD N $OCATNG ANDDEP$O(NG $FE RAFTS TO PREVENT F#RT"ERN=#R( OR $OSS OF $FE N T"E EVENT OF A"E$COPTER $ANDNG N T"E !ATER.

FAA AD 2011-25-01

AS N AD AS N AD VI'E '"$A LETTER NO.!*4+395 'T. 15*01*12

DGCA/NM/141 TO PREVENT TCAS #NT FROM DROPPNGTRAC*S,!"C" CO#$D COMPROMSE SEPERATONOF AR TRAFFC AND $EAD TO S#BSE)#ENT MD ARCO$$SON.

FAA AD 2012-02-08

AS N AD AS N AD VI'E '"$A LETTER NO.!*4+9 'T. 13.03.12

DGCA/NM/03R1 . "NO SMOKING" PLACARD TO BE INSTALLED ON LAVATORY

DOOR TO PREVENT FIRES FROM SMOKING MATERIALS

BEING DROPPED INTO LAVATORY PAPER OR LINEN

WASTE RECEPTACLES

FAA AD 74-08-09R3


DGCA/NM/142 ATA 25- E)#PMENT AND F#RNS"NG-PASSENGER SEATBAC*REST $N*-NSPECTON/REP$ACEMENT.

EASA AD 2012-0038


DGCA/NM/143 ATA 26-FRE PROTECTON-"AND OPERATED FREETNG#S"E-MODFCATON

EASA AD 2012-0037

AS N AD AS N AD VI'E '"$A LETTER NO.!*4+51 'T 25.04.12

DGCA/NM/138R1 TO DETECT AND CORRECT CRAC*NG OF T"E CENTRA$ AND $ATERA$ SPREADERS ,!"C" CO#$D $EAD TO

F#RT"ER CRAC*NG OF T"ESEATSPREADRES,CA#SNG N=#R( TOPASSENGERS OR CRE! MEMBERS D#RNG "EAV(T#RB#$ANCE N F$G"T OR N T"E EVENT OF ANEMERGENC( $ANDNG.

FAA AD 2012-08-07




20/36


ADCo%&'ian

c"A&&'icai'it

y#"%ar(s

DGCA/NM/144

TO PREVENT LOSS OF PRESSURE IN THEESCAPE SLIDES/RAFTS AFTER AN

EMERGENCY EVACUATION .WHICH COULDRESULT IN INADE(UATE %UOYANCY TO

SUPPORT THE RAFTS PASSENGERCAPACITY DURING DITCHING AND

INCREASE THE CHANCE FOR INURY TORAFT PASSENGERS)

FAA AD 2012-0$-2#

AS N AD AS N AD

DGCA/NM/14#

TO PREVENT TOR%O$AR"ER %EARIN"

#EI,URE -FAILE' TUR%O$AR"ER

$O!PONENT#-AN' 'A!A"E TO TE AIRPLANE

FA AD 2012-10-#2 AS N AD AS N AD

DGCA/NM/14$

TO PREVENT MISLEADING INFORMATIONDURING LOCALIER PERFORMANCE&LP'

LOCALIER PERFORMANCE WITH VERTICALGUIDANCE&LPV' OR S%AS LATERALNAVIGATION/VERTICAL NAVIGATION&LNAV/VNAV' APPROACHES DUE TO

SOFTWARE PRO%LEM IN HONEYWELLWIDE AREA AUGMENTATION SYSTEM

&WAAS' GLO%AL NAVIGATION SATELLITESENSOR UNITS&GNSSU'

FAA AD 2012-14-1#

AS N AD AS N AD



21/36


ADCo%&'ian

c"A&&'icai'it

y#"%ar(s

DGCA/NM/14*

TO PREVENT FAILURE OF THE MAIN LANDINGGEAR TIRES DURING TAEOFF ORLANDING.WHICH COULD CAUSE DAMAGE TO THE AIRPLANESTRUCTURE.FLAPS.ENGINE.AND WHEEL WELLAND RESULT IN REDUCED CONTROLLA%ILITYOF THE AIRPLANE)

FAA AD 2012-1*-01

AS N AD AS N AD

VIDE DGCA LETTER

NO) A-31/*82 DT

08)10)12

DGCA/NM/148

PREVENT SEPARATION OF REAR GASGENERATOR CASE AND RELEASE OF HIGHENERGY DE%RIS.WHICH COULD RELEASEIN INURY AND DAMAGE T AIRPLANE)

FAA AD 2012-18-14

AS N AD AS N AD

VIDE DGCA LETTER

NO) A-31/8#3 DT0$)11)12

DGCA/NM/14+R1

OXYGEN - FLIGHT CREW OXYGEN MASREGULATOR - IDENTIFICATION /OPERATIONAL PROCEDURE /REPLACEMENT

EASA AD2012- 02#4 R1

AS N AD AS N AD

VIDE DGCA LETTER

NO) A-31/40

D) 1#)01)13



22/36


ADCo%&'ian

c"A&&'icai'it

y#"%ar(s

DGCA/NM/1#0 REVISED TO DGCA / NEW MISC/1#0 R1

DGCA/NM/1#1 REVISED TO DGCA/NEW MISC/151 R1 VIDE DGCA LETTER NO . M-4/ 209 DT. 16.12.14

DGCA/NM/1#2R1

REVISED VIDE DGCA LETTER NO A-31/#0$ DT) 24)0*)13



23/36


ADCo%&'ian

c"A&&'icai'it

y#"%ar(s

DGCA/NM/1#3R2

REVI#E' TO '"$A+NE !I#$+153 R3 VI'E '"$A LETTER NO. A*31+791 'T. 12.12.13

DGCA/NM/3#R1

CANCELLED- NAVIGATION SYSTEMSMODE S AND C

TRANSPONDERSCHEC

EASA AD200$-02$#-

CN

AS N AD AS N AD VIDE DGCA

LETTER

NO A-

31/30+

DGCA/NM/1#4

E(UIPMENT/FURNISHINGS-VARNISHON VENEEREDPANELS)INSPECTION/REFURNISHING)

EASA AD2013-010$


LETTER

NO A-

31/341

DGCA/NM/1##

UNSAFE CONDITION AS THE SEARCHLIGHT /GIM%ALDISCONNECTINGFROM THE

HELICOPTER AND

FAA AD 2013-10-01)


LETTER

NO A-

31/3*8



24/36


ADCo%&'ian

c"A&&'icai'ity #"%ar(s

DGCA/NM/1#$

TO PREVENT THE %RUSHES IN THEA/C MOTOR FROM WEARINGDOWN. WHICH COULD RESULT IN

THE RIVET IN THE %RUSHCONTACTING THE COMMUTATORCAUSING SPARS CONSE(UENTFIRE AND /OR SMOE IN THE TAILCONE WITH NO MEANS TODETECT OR EXTINGUISH THE FIRE

FAA AD 2013-0+-11

AS IN AD AS IN AD

VIDE DGCA

LETTER

NO A-

31/40$

DT)

10)0$)13

DGCA/NM/1#*

TO PREVENT THE FAILURE OF

URETHANE SEALS TO MAINTAINSUFFICIENT HALONCONCENTRATION IN THE CARGOCOMPARTMENTS TO EXTINGUISHOR CONTAIN FIRE OR SMOE

FAA AD 2013-11-04

AS IN AD AS IN AD

VIDE DGCA

LETTER

NO A-

31/444

DT)

DGCA/NM/1#8

UNSAFE CONDITION AS FAILURE OF THE OVERLOAD CLUTCHRESULTING I IN FLIGHT FAILUREOF THE HOIST. WHICH COULDRESULT IN INURY TO PERSONS

%EING LIFTED

FAA AD 2013-0$-#1

AS IN AD AS IN AD

VIDE DGCA

LETTER

NO A-

31/4*3

DGCA/NM/1#2R2

REVISED TO DGCA/NEW MISC/152 R3 VIDE DGCA LETTER NO. A-31/235 DT. 15.04.14



25/36

DGCA NO S#$%e&t

#"$ranc" ADCo%&'ian


DGCA/NM/1#+

REVISED TO DGCA/NEW MISC/159R1 VIDE DGCA LETTER NO. A-31/611 DT. 15.09.14

DGCA/NM/1#0 R1

TO PREVENT TUR%OCHARGER TUR%INE WHEELFAILURE.REDUCTION ORCOMPLETE LOSS OF ENGINEPOWER.LOSS OF ENGINE OIL

FAA AD 2013-21-02

AS IN AD AS IN AD

VIDE DGCA

LETTER

NO A-

31/*#*

DGCA/NM/1#3R3


DGCA/NM/1$0




26/36

DGCA NO S#$%e&t

#"$ranc" ADCo%&'ian


DGCA/NM/1$1

TO CORRECT POSSI%LEMISALIGNMENT ISSUES WITH THE

TRANSPONDERS THAT COULDRESULT IN INCREASED PILOT ANDAIR TRAFFIC CONTROLLERWORLOAD AS WELL ASREDUCED SEPARATION OFAIRPLANES

FAA AD NO)2014-0#-2*

AS IN AD

VT-IIT

N/A AS MODE S TRANSPONDER

MODEL

VIDE DGCA

LETTER

NO)

A*31+ 243 'T. 15.04.14

VT-ETL

N/A AS MODE S TRANSPONDER NOT

INSTALLED

VT-HNS


INSTALLED

VT-GDGN/A AS MODE S

TRANSPONDER NOTINSTALLED

VT-GII


INSTALLED



27/36

DGCA NO S#$%e&t

#"$ranc" ADCo%&'ian

c"A&&'icai'ity

#"%ar(s DGCA NO

DGCA/NM/1#2 R3


DGCA/NM/

1$2

COMMUNICATIONS COCPIT VOICE

RECORDER - REPLACEMENT

EASA AD

2014-0088

AS IN AD

VT-IITN/A AS CVR NOT

INSTALLED

VIDE DGCA

LETTER

NO) A-

31/30*DT)

08)0#)14

VT-ETLN/A AS CVR NOT

INSTALLED

VT-HNSN/A AS CVR NOT

INSTALLED

VT-GDGN/A AS CVR NOT

INSTALLED

VT-GII

N/A AS CVR NOTINSTALLED



28/36

DGCA NO S#$%e&t

Re'r(n&e AD Co)*li(n&eA**li(-

$ilit+Re)(r, DGCA NO

'"$A+N!+160R1 REVISED TO DGCA/NEW MISC/160 R2

'"$A+N!+160R2 E/UIP!ENT+FURNI#IN"**** $RA#

PO#ITION IN'I$ATOR****!O'IFI$ATION AIR$RAFT FLI"T

!ANUAL***A!EN'!ENT

EA#A A'

2014*0095 R1

A# IN A' VT*IIT N+A a $a Pont Ind)ato

#te not ntaed. )IDEDGCALETTE#NO* A-+,/.+DT*,.*.*,

VT*ETL N+A a $a Pont Ind)ato

#te not ntaed.

VT*N# N+A a $a Pont Ind)ato

#te not ntaed.

VT*"'" N+A a $a Pont Ind)ato

#te not ntaed.

VT*"II N+A a $a Pont Ind)ato

#te not ntaed.

'"$A+N!+163 E/UIP!ENT+FURNI#IN"**** $RA#

PO#ITION IN'I$ATOR #TE!

***REPLA$E!ENT- AIR$RAFT FLI"T!ANUAL***A!EN'!ENT

EA#A A'

2014*0125

A# IN A' VT*IIT N+A a $a Pont Ind)ato

#te not ntaed. )IDE

DGCALETTE#NO* A-+,/,,DT*,.*.*,

VT*ETL N+A a $a Pont Ind)ato#te not ntaed.

VT*N# N+A a $a Pont Ind)ato

#te not ntaed.

VT*"'" N+A a $a Pont Ind)ato

#te not ntaed.

VT*"II N+A a $a Pont Ind)ato

#te not ntaed.

'"$A+N!+164 OXYGEN- OXYGEN MASK

REGULATOR INFLATABLE

HARNESS/ INFLATION HOSE-

IDENTIFICATION/REPLACEMENT

EASA AD

2014-

0142R1

A# IN A' VT*IIT N+A a o(en a

e(ato not ntaed. )IDEDGCALETTE#

NO* A-+,/+DT*+.*.*,

VT*ETL N+A a o(en a

e(ato not ntaed.

VT*N# N+A a o(en ae(ato not ntaed.

VT*"'" N+A a o(en a

e(ato not ntaed.

VT*"II N+A a o(en a

e(ato not ntaed.



29/36

DGCA NO S#$%e&t


$ilit+Re)(r, DGCA NO

'"$A+N!+152R4 REVISED TO DGCA/NEW MISC/152R5 VIDE DGCA LETTER NO. A-31/746 DT. 07.10.14

'"$A+N!+159R1

TO DETECT AND CORRECTDISCREPANCIES OF THE %ATTERYWIRING INSTALLATION INSIDE

THE TU . WHICH COULD RESULTIN AN ELECTRICAL SHORT ANDPOSSI%LE IGNITION SOURCE

FAA AD NO)2014-1*-02

AS IN AD

VT-IIT

N/A AS APPLICA%LE TO

TRANSPORT CATEGORYAIRPLANES

)IDEDGCA

LETTE#NO* A-+,/,,

DT*,0*.1*,

VT-ETL

N/A AS APPLICA%LE TO TRANSPORT CATEGORY

AIRPLANES

VT-HNS


AIRPLANES

VT-GDG


AIRPLANES

VT-GII

N/A AS APPLICA%LE TO

TRANSPORT CATEGORYAIRPLANES

'"$A+N!+165

E(UIPMENT AND FURNISHINGS SAFETY %ELT ATTACHMENT %OLTS INSPECTION / REPLACEMENT

EASA ADNO) 2014-

018*AS IN AD

VT-IITN/A %Y SEAT

MANUFACTURER

)IDEDGCA

LETTE#NO* A-+,/+0

DT*,0*.1*,

VT-ETLN/A %Y SEAT

MANUFACTURER

VT-HNS

N/A %Y SEATMANUFACTURER

VT-GDG

N/A %Y SEAT

MANUFACTURER

VT-GII

N/A %Y SEATMANUFACTURER

DGCA NO S#$%e&t Re'r(n&e AD Co)*li(n&e A**li(- Re)(r, Letter No



30/36

$ilit+

'"$A+N!+166 REVISED TO DGCA/NEW MISC/166R1 VIDE DGCA LETTER NO . M-4/ 206 DT. 08.12.14

'"$A+N!+167 REVISED TO DGCA/NEW MISC/167R1 VIDE DGCA LETTER NO . M-/ 2.+ DT* .3*,2*,

'"$A+N!+168

TO DETECT AND CORRECT MODES TRANSPONDERS THAT DO NOTRESPOND CORRECTLY TO MODES ONLY ALL-CALLINTERROGATIONS. WHICH COULDRESULT IN INCREASED PILOT ANDAIR TRAFFIC CONTROLLERWORLOAD AS WELL ASREDUCED SEPARATION OFAIRPLANES)

EASA AD2014-18-01

AS IN AD

VT-IIT

N/A %Y MODEL NO) AS A/C

IS FITTED WITH GTX-33 MODE S TRANSPONDER )IDE

DGCALETTE#NO* A-+,/4.

DT*.4*,.*,

VT-ETLN/A AS MODE S


VT-HNSN/A AS MODE S


VT-GDGN/A AS MODE S


VT-GII N/A AS MODE S NOT INST

DGCA/NM/1#3R4 REVISED TO DGCA/NEW MISC/153R5 VIDE DGCA LETTER NO . M-4/ 212 DT. 16.12.14

DGCA/NM/1#2R#

E(UIPMENT FURNISHINGS SAFETY %ELTS/ TORSORESTRAINT SYSTEMS-INSPECTION/ REPLACEMENT

EASAAD2013-0020 R4

AS IN AD

VT-IIT

N/A AS AMSAFE %ELTSINSTALLED AT CESSNACO) ON 28 AUG 2012 )IDE

DGCALETTE#NO* A-+,/4

DT*

.4*,.*,

VT-ETLN/A AS AMSAFE %ELTS

NOT INSTALLED

VT-HNSN/A AS AMSAFE %ELTS

NOT INSTALLED

VT-GDGN/A AS AMSAFE %ELTS

NOT INSTALLED

VT-GII

N/A AS AMSAFE %ELTSNOT INSTALLED

DGCA NO S#$%e&t


$ilit+Re)(r, Letter No.



31/36

DGCA/NM/122R1

NAVIGATION – MODE S

TRANSPONDER AIRCRAFT

TYPE MODE STRAPPING – CHECK /

MODIFICATION.

EASA AD

2010-

0003R2

A# IN A'

VT-IITN/A %Y MODE S’

TRANSP) MODEL NO) )IDEDGCA

LETTE#NO* S-/ ,3.

DT*,,*,,*,

VT-ETLN/A AS MODE S’ TRANSP)

NOT INSTALLED

VT-HNSN/A AS MODE S’ TRANSP)

NOT INSTALLED

VT-GDG

N/A AS MODE S’ TRANSP)

NOT INSTALLED

VT-GII

N/A AS MODE S’ TRANSP)NOT INSTALLED

DGCA/NM/1$+ REVISED TO DGCA/NEW MISC/169R1 VIDE DGCA LETTER NO . 9-414/06 AI(2) dt. 10.06.15 (New Delhi)

DGCA/NM/1$*R1

EQUIPMENT & FURNISHINGS –

EMERGENCY FLOTATION SYSTEM –

ROTORCRAFT FLIGHT MANUAL

(SUPPLEMENT)

EASA AD

2014-0244A# IN A'

VT-IITN/A AS APPLICA%LE TO

HELICOPTERS )IDEDGCA

LETTE#NO* M-/ 2.+

DT*

.3*,2*,

VT-ETLN/A AS APPLICA%LE TO

HELICOPTERS

VT-HNSN/A AS APPLICA%LE TO

HELICOPTERS

VT-GDGN/A AS APPLICA%LE TO

HELICOPTERS

VT-GIIN/A AS APPLICA%LE TO

HELICOPTERS

DGCA NO S#$%e&t


$ilit+Re)(r, Letter No.



32/36

DGCA/NM/1$$R1 REVISED TO DGCA/NEW MISC/166R2 VIDE DGCA LETTER NO . S-4/32 DT. 23.04.15

DGCA/NM/1#1R1 ATA 34, NAVIGATION.

FAA AD

2012-26-

15R1

A# IN A'

VT-IITN/A %Y AIRCRAFT MODEL

NO))IDEDGCA

LETTE#NO* M-/ 2.1

DT*,*,2*,

VT-ETLN/A %Y AIRCRAFT MODEL

NO

VT-HNSN/A %Y AIRCRAFT MODEL

NO

VT-GDGN/A %Y AIRCRAFT MODEL

NO

VT-GIIN/A %Y AIRCRAFT MODEL

NO

DGCA/NM/1#3R# REVISED TO DGCA/NEW MISC/153R6 VIDE DGCA LETTER NO . S-4/57 DT. 19.05.15



33/36


34/36

DGCA/NM/1#3R$ATA 25- E/UIP!ENT# +

FURNI#IN"#* OI#T*TE#T+

REPLA$E!ENT

EA#A A'

2015*0069A# IN A'

VT-IITN/A AS APPLICA%LE TO

HELICOPTERS )IDEDGCA

LETTE#NO* S-/ 04

DT*,1*.0*,

0

VT-ETLN/A AS APPLICA%LE TO

HELICOPTERS

VT-HNSN/A AS APPLICA%LE TO

HELICOPTERS

VT-GDG N/A AS APPLICA%LE TOHELICOPTERS

VT-GIIN/A AS APPLICA%LE TO

HELICOPTERS

DGCA/NM/1*1

ATA*34 ; Na


35/36

backrest links, which could

affect the structural integrity of

seat backrest. Failure of the

backrest links could result in

injury to an occupant during

emergency landing conditions.

2015*10*02

DGCALETTERNO) +-414/0$AI&2' 7)10)0$)1

#

VT-ETLN/A 5 67!5, S5 "6

!"5997

VT-HNSN/A 5 67!5, S5 "6

!"5997

VT-GDGN/A 5 67!5, S5 "6

!"5997

VT-GII N/A 5 67!5, S5 "6!"5997

DGCA/NM/1*3

ATA – 34, Navigation – Attitude

Heading Reference System –

Modification / replacement

EA#A A'

2015*0093A# IN A'

VT-IITN/A 5 AHRS "6

!"5997 VIDEDGCA

LETTERNO) +-414/0$AI&2' 7)10)0$)1

#

VT-ETLN/A 5 AHRS "6

!"5997

VT-HNSN/A 5 AHRS "6

!"5997

VT-GDGN/A 5 AHRS "6

!"5997

VT-GIIN/A 5 AHRS "6

!"5997

DGCA/NM/130R3

ATA-35, oxygen, to eliminate a

hazard that could jeopardize flight

safety, and to ensure that all

lavatories have a supplemental

oxygen supply.

FAA A'

2012*11*09R1A# IN A'

VT-IITN/A 5 5::9!,5;9 6

T


36/36

DGCALETTER

NO)M/42/

1$+ 7)

02)0+)1#

VT*ETL N+A a app)a?e to

e)opte on.

VT*N# N+A a app)a?e to

e)opte on.

VT*"'" N+A a app)a?e to

e)opte on.

VT*"II N+A a app)a?e toe)opte on.

'"$A+N!+174

To pe

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