DGCA NO SUBJECT REFERENCE AD COMPLIANCE

DGCA NO SUBJECT REFERENCE AD COMPLIANCE APPLICABILITY

DGCA / NEW-MISC / 01 MAGNETIC PARTICLE INSPECTION OF UNDERCARRIAGE BOLTS OF AGRICULTURAL AIRCRAFT.

DGCA LETTER NO. 77-5/69-AI(I) DT. 24/5/1969.

EVERY C OF A OVERHAUL/ MAJOR INSPECTION OR 12 MONTHS WHICHEVER IS EARLIER.

DGCA / NEW-MISC / 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

1) 50 HRS INSPECTION 2) 100 HRS INSPECTION

AS IN THE LETTER

DGCA / NEW-MISC / 03R1 TO PREVENT POSSIBLE FIRES THAT COULD RESULT FROM SMOKING MATERIALS BEING DROPPED INTO LAVATORY PAPER OR LINEN WASTE RECEPTACLES

FAA AD 74-08-09R3 AS IN AD ALL TRANSPORT AIRCRAFT INCLUDING BUT NOT LIMITED TO B707,B737,B747,HS 748, DC 3,DC 4.

DGCA / NEW-MISC / 04 INSTALLATION OF 'G'-METER DURING CLOUD SEEDING OPERATION.

DGCA LETTER NO. 4/26/73-AI(I) DT. 20/6/74

AS IN THE LETTER AS IN THE LETTER

DGCA / NEW-MISC / 05 PAINTING OF HELICOPTERS ENGAGED IN AGRO OPERATION WITH "DAY GLOW" PAINT.

DGCA LETTER NO.78/111/75-AI(I) DT. 23/3/77

WITH IMMEDIATE EFFECT AS IN DGCA LETTER

DGCA / NEW-MISC / 06 FREQUENCY TOLERANCE LIMIT FOR TRANSMITTERS REV.1

DGCA LETTER NO. 4-18/79 AI(1) DT.February 1992 DATED 27TH FEB., 1992

FORTHWITH FORTHWITH

DGCA / NEW-MISC / 07 IMPROVED LUBRICATION AND INSTALLATION OF MODIFIED DISTRIBUTOR BLOCK IN BENDIX SCINTILLA 'S' TYPE MAGNETOS.

BENDIX SB NO. 551A & 566 APPLICABLE TO MAGNETOS OVERHAULED AFTER 30/9/76

APPLICABLE TO BENDIX SCINTILLA 'S' 20, 'S' 200, 'S' 1200 SERIES MAGNETOES

DGCA / NEW-MISC / 08 IDENTIFICATION OF AIRCRAFT PIPELINES.

ISI SPECIFICATION NO. IS 6753-1972

WITHIN MAY 1980 APPLICABLE TO AIRCRAFTS WITH AUW OF 15000 KGS & ABOVE & TYPE CERTIFICATED


AFTER 1/5/76

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

DGCA / NEW-MISC / 10 "FASTEN SEAT BELT WHILE SEATED", SIGN OR PLACARD ON EACH FORWARD BULKHEAD AND ON EACH PASSENGER SEAT BACK.

FAR PART 121.317(b) FORTHWITH PASSENGER AIRCRAFT

DGCA / NEW-MISC / 11 INSPECTION/ REPLACEMENT OF GEAR DISTRIBUTOR OF BLOCK OF BENDIX S-1200 SERIES MAGNETOS.

FAA AD 82-13-01 & BENDIX SB NO. 613

AS IN AD AS IN AD

DGCA / NEW-MISC / 12 EXAMINATION OF ENGINE INVOLVED IN PROPELLER STRIKE INCIDENTS.

DGCA LETTER NO. 9-414/81-AI(II) DT. 14/9/82

IMMEDIATE ALL TYPES OF PISTON ENGINE AIRCRAFT.

DGCA / NEW-MISC / 13 REPLACEMENT OF PAPER INDUCTION AIR FILTERS.

FAA AD 84-26-02 AS IN AD AS IN AD

DGCA / NEW-MISC / 14 LIGHTING FOR INTERIOR EMERGENCY EXIT MARKINGS

FAR 121.310(c) FORTHWITH 1) LARGE TRANSPORT A/C HAVING SEATING CAPACITY OF MORE THAN 30 PASSESGERS AND TYPE CERTIFIED AFTER 1 ST JAN. '1958 2) B707, CARAVELLE, F27AND HS748 A/C ARE EXEMPTED.

DGCA / NEW-MISC / 15 SERVICING OF AIRCRAFT TYRES WITH NITROGEN GAS

FAA AD 87-08-09 AS IN AD APPLICABLE TO AIRBUS A300, A310, BOEING 707, 737 & 747.

DGCA / NEW-MISC / 16 INSPECTION OF IPECO CREW SEATS. FAA AD 90-09-08 AS IN AD APPLICABLE TO BOEING B737 & B747 AIRCRAFT.

DGCA / NEW-MISC / 17 PRECAUTIONARY CHECK FOR CORRECT LOCATION OF BRIDGE PIECES INSIDE THE MAIN

CAA AD 001-02-93 AND SB 25-46

AS IN AD AND SB AS IN AD AND SB


BUOYANCY TUBES.

DGCA / NEW-MISC / 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 & SB AS IN AD & SB

DGCA / NEW-MISC / 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 AND SIL

AS IN AD AND SIL

DGCA / NEW-MISC / 20 TO PREVENT DISRUPTION OF THE FUEL FLOW TO THE ENGINE RESULTING IN FAILURE ATTAIN RELATED POWER

BLA AD 1998-007-AB& FAA AD 98-01-06

AS IN AD AND SB. APPLICABLE TO PRECISION AIRMOTIVE ( FACET PRODUCTS AND MARVEL SCHEBLER) MA-3A, MA-3PA, MA-3SPA AND MA-4SPA CARBURETORS

DGCA / NEW-MISC / 21 INSPECTION/REPLACEMENT- AFFECTED MAGNETO CAPACITORS

FAA PRIORITY LETTER 94-06-09 AND TCM CRITICAL SB 641 DT. FEB. 1 '1994

AS IN PRIORITY LETTER AND CSB.

AS IN PRIORITY LETTER AND CSB.

DGCA / NEW-MISC / 22 SICMA AERO SEAT-PASSENGER SEATS- AFT TRACK FITTINGS

DGAC AD 1994-085 (AB) R2 AS IN AD. AS IN AD.

DGCA / NEW-MISC / 23 UP LIMIT POSITION SECURITY. BVAD 94-116(B). AS IN AD. AS IN AD.

DGCA / NEW-MISC / 24 NAVIGATION - VHF/NAV RECEIVER MODIFICATION.

BLA AD 1995-053(AB). AS IN AD. AS IN AD.

DGCA / NEW-MISC / 25 CESSNA ENGINE OIL FILTER ADAPTER ASSEMBLIES


DGCA / NEW-MISC / 26 TO PREVENT COMPRESSOR WHEEL RUPTURE WHICH COULD RESULT IN AN UNCONTAINED APU FAILURE AND DAMAGE TO THE AIRCRAFT


DGCA / NEW-MISC / 27 SICMA AERO SEAT(PAX SEAT) LEG COLLAR

BVAD 97-134(AB) AS IN AD AS IN AD


DGCA / NEW-MISC / 28 TO PREVENT THE TRANSMISSION OF MISLEADING ENCODING ALTIMETER INFORMATION BETWEEN AFFECTED AIRCRAFT


DGCA / NEW-MISC / 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 / NEW-MISC / 30 TO PREVENT SMOKE & A POSSIBLE FIRE IN THE COCKPIT CAUSED BY OVERHEATING OF THE ELECTRIC DOOR SEAL INFLATION SYSTEMS

FAA AD 98-21-21R1 AS IN AD AS IN AD

DGCA / NEW-MISC / 31 TO PREVENT FAILURE OF THE SEAT RESTRAINT SYSTEM

FAA AD 98-25-10R1 AS IN AD A SIN AD

DGCA / NEW-MISC / 32 TO PREVENT DEVIATION FROM AN INTENDED FLIGHT PATH DURING A NON PRECISION APPROACH


DGCA / NEW-MISC / 33 TO PREVENT REDUCED OXYGEN CONSUMPTION WHEN PASSENGERS ARE REQUIRED TO USE DEFECTIVE OXYGEN MASKS , WHICH COULD RESULT IN PASSENGER INJURY,


DGCA / NEW-MISC / 34 ALLIED SIGNAL-VHF COM RECEIVER BANDWIDTH REDUCTION

DGAC AD 1999-298(AB) AS IN AD AS IN AD

DGCA / NEW-MISC / 35R1 CANCELLED: NAVIGATION SYSTEMS --- MODE S AND C TANSPONDERS --- CHECK

EASA AD 2006-0265-CN AS IN AD AS IN AD

DGCA / NEW-MISC / 36 TO PREVENT VHF NAVIGATION RECEIVER INTERFERENCE FROM FM RADIO STATION BROADCAST FREQUENCIES



DGCA / NEW-MISC / 37 TO PREVENT FALSE TRAFFIC ALERT COLLISION AVOIDANCE SYSTEM (TCAS II)


DGCA / NEW-MISC / 38 TO ENSURE THE ILS RECEIVER PROVIDES THE FLIGHT CREW WITH ACCURATE GLIDE SLOPE PATH


DGCA / NEW-MISC / 39 REVISED OPERATING LIMITATIONS FOR THE AFFECTED STANDBY VACUUM SYSTEMS INTO THE AIRPLANE FLIGHT MANUAL


DGCA / NEW-MISC / 40 THIRD OCUPANT SEAT HEADREST LOCKING POINT


DGCA / NEW-MISC / 41 IFE ELECTRIC HARNESS PROTECTION IN CENTRAL FOLDABLE ARMREST


DGCA / NEW-MISC / 42 INSPECT THE AUTOPILOT SERVO ACTUATOR FOR A LOOSE FASTENER


DGCA / NEW-MISC / 43 TO PREVENT AN UNCONTAINED APU FAILURE & DAMAGE TO THE AIRPLANE


DGCA / NEW-MISC / 44 SICMA AERO SEAT - MODIFICATION OF SEAT BELT ATTACHMENT FITTING

DGAC AD 2002-471(AB)R1 AS IN AD AS IN AD

DGCA / NEW-MISC / 45 TO PREVENT LOSS OF THE MAIN SOURCES OF ATTITUDE DATA


DGCA / NEW-MISC / 46 TO PREVENT FAILURE OF THE MAGNETO IMPULSE COUPLING, RESULTING IN SEIZURE OF THE ENGINE


DGCA / NEW-MISC / 47 CARGO & BAGGAGE FAR 121.314 ON OR BEFORE 31-12-2002 1. Turboprop aeroplane having a


COMPARTMENT type certified Pax seating capacity of 10 or more excluding crew seat. 2. Turbojet aeroplane irrespective of seating capacity 3. Those a/c type certified in accordance with FAR Pt 25 and 4.Those a/c engaged in scheduled air transport services carrying passengers.

DGCA / NEW-MISC / 48 TO PREVENT UNDESIRABLE AUTOTRIM COMMAND


DGCA / NEW-MISC / 49 TO PREVENT INACCURATE NAVIGATION DUE TO INCORRECT BEARING INFORMATION

FAA EMERGENCY AD 2001-14-51

AS IN AD AS IN AD

DGCA / NEW-MISC / 50 TO MODIFY THE ALTITUDE ENCODER INPUTS OF THE CTL-92 TRANSPONDER CONTROL PANELS.


DGCA / NEW-MISC / 51 (R1)

TO PREVENT FAILURE OF THE FUEL REGULATOR SHUTOFF VALVE

FAA AD 2004-25-16 R1 (ORG FAA AD 2001-08-01,2001-17-13 , & 2004-25-16 IS SUPERSEEDED)

AS IN AD AS IN AD

DGCA / NEW-MISC / 52 TO PREVENT ENGINE FUEL PUMP FAILURE.

DGAC AD 2001-17-15 AS IN AD AS IN AD

DGCA / NEW-MISC / 53 TO PREVENT DAMAGE TO THE FIRE EXTINGUISHING SYSTEM COMPONENTS


DGCA / NEW-MISC / 54 MODIFICATION OF AIRCRAFT COCKPIT DOOR

SFAR 92-4, FAR 121.583, FAR 25.795 & FAR 121.313

Door Modification Requirement: 1.After 1st July 2002, the cockpit door of each applicable airplane must have

Applicable to airplane having a door between the passenger & pilot compartment and engaged in 1.Scheduled Air Transport


an internal locking device installed, operative, and in use. Such internal locking device has to be designed so that it can only be unlocked from inside the cockpit. 2.Not later than 9th April 2003, the cockpit doors of all applicable airplanes should be modified i.To resist forcible intrusion by unauthorized persons and be capable of withstanding impacts of 300 joules (221.3 foot -pounds) at the critical locations on the door, as well as a 250 pounds (1113 Newtons) constant tensile load on the knob or handle, and ii.Resist penetration by small arms fire and fragmentation devices to a level equivalent to level IIIa of the National Institute of Justice Standards (NIJ) 0101.04 of USA. (Refer FAR 121.313 (j) (1) & FAR 25.795) 3.Plan for compliance: Not later than 1st July 2002, all operators affected by this modification shall submit a report to DGCA their plans for modifying the cockpit doors as

services.(passenger) Or 2. All cargo operations where provision is also available to carry passengers (Refer FAR 121.583)


given in item 1 & 2 above and to restore compliance with all applicable Airworthiness requirements. 4.Operational Procedure: a)Key to the cockpit door shall be available to flight crew members only. However, any cabin crewmember may have the key provided internal cockpit door locking device is installed, operative & in use. b) A key for each door (having a lock) that separates a passenger compartment from an emergency exit must be identified to passengers in the briefing by cabin crew. The key required for access to the above emergency exit must be readily available for each cabin crewmember. c) A means for the crew in an emergency to unlock each door that leads to a compartment that is normally accessible to passengers & that can be locked by passengers. d) Each operator must establish methods to enable a cabin crew to enter the cockpit in the event that a


flight crew member becomes incapacitated . Any associated signals or confirmation systems must be operable by each flight crewmember from that flight crewmember’s duty station.

DGCA / NEW-MISC / 55 HYDROLOK PIN ORIENTATION CAA AD 002-11-2001 AS IN AD AS IN AD

DGCA / NEW-MISC / 56R1 AIR TRANSPORT ASSOCIATION (ATA|) OF AMERICA CODE 25 EQUIPMENT / FURNISHINGS


DGCA / NEW-MISC / 57 GNS 430 UNITS TO PREVNT INACCURATE COURSE DEVIATION DISPLAYS


DGCA / NEW-MISC / 58 TO PREVENT IMPELLER FAILURE FROM CRACKS IN THE IMPELLER BACK FACE AREA


DGCA / NEW-MISC / 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 / NEW-MISC / 60 TO PREVENT UNWARRANTED DISPLAY OF THE ADC FLAG


DGCA / NEW-MISC / 61 TO REPLACE AFFECTED COMPRESSOR WHEELS


DGCA / NEW-MISC / 62 INSTALLATION OF CVR DGCA LETTER NO. 9-414/2002-AI(2)

31/10/2002 TO ALL TWIN TURBINE ENGINE AIRCRAFT WHERE STC IS AVAILABLE OR THE MANUFACTURER HAS INSTALLED THIS EQUIPMENT AS


A PART OF THE TYPE CERTIFICATE OF AIRCRAFT

DGCA / NEW-MISC / 63 INSTALLATION OF FDR DGCA LETTER NO. 9-414/2002-AI(2) DATED 30.09.2002

31/10/2002 TO ALL TURBINE ENGINE AIRCRAFT WHERE STC IS AVAILABLE OR THE MANUFACTUREE HAS INSTALLED THIS EQUIPMENT AS A PART OF THE TYPE CERTIFICATE OF AIRCRAFT

DGCA / NEW-MISC / 64 PASSENGER SEATS- CENTRAL SPREADERS MODIFICATION

DGAC AD 2002-504(AB) AS IN THE AD & SUBSEQUENT REVISIONS TO THE SB

AS IN THE AD & SUBSEQUENT REVISIONS TO THE SB

DGCA / NEW-MISC / 65 TO PREVENT DISPLAY OF ERRONEOUS PRIMARY FLIGHT AND ENGINE PARAMETER INFORMATION


DGCA / NEW-MISC / 66 TO PREVENT THE FMC FROM RETAINING INCORRECT INFORMATION


DGCA / NEW-MISC / 67 TO PREVENT FAILURE OF HOSE WHEN EXPOSED TO FIRE

FAA AD 2002-22-12(Corrected)

AS IN AD AS IN AD

DGCA / NEW-MISC / 68 TO PREVENT FAILURE OF THE EMERGENCY EMERGENCY EVACUATION SLIDE RAFT


DGCA / NEW-MISC / 69 EQUIPMENT: BABIES BASSINETS DGAC AD 2001-351(B) AS IN AD AS IN AD

DGCA / NEW-MISC / 70 TO PREVENT MOOUNTING BRACKET FAILURE AND SEPARATION OF THE RESCUE HOIST FROM THE HELICOPTER



TO ENSURE THAT THE FLIGHTCREW HAS ACCURATE LOCALIZER & GLIDESLOPE DEVIATION

FAA AD 2010-07-02 (FAA AD SUPERSEDES FAA AD 2006-22-05

AS IN AD AS IN AD


INDICATIONS

DGCA / NEW-MISC / 72 KIDDLE AEROSPACE HAND HELD HALON FIRE EXTIGENISHES-

DGCA letter No. 9-414/2003-AI(2) dated 22.05.2003

Within 6 months of issue of DGCA letter

As in DGCA Letter

DGCA / NEW-MISC / 73 TO DETECT UNSAFE CONDITIONS THAT COULD RESULT IN SEPARATION OF A PROPELLER BLADE


DGCA / NEW-MISC / 74 AIR CARGO PALLETS AND AIR CARGO NETS

LBA AD 2002-303 AS IN AD AS IN AD

DGCA / NEW-MISC / 75 TO PREVENT APU COMPARTMENT FIRES AND FUEL VAPOUR EXPLOSION


DGCA / NEW-MISC / 76 TO DETECT AND CORRECT DEFECTIVE SAFETY BELTS AND RESTRAINT SYSTEMS.

FAA AD 2003-26-06 AND DGAC AD 2002-104(AB)R2 & 2002-105(AB)R2

AS IN AD AS IN AD

DGCA / NEW-MISC / 77 TA / RA VSI-TCAS INDICATOR THALES AVIONICS

DGAC AD F-2004-053 AS IN AD AS IN AD

DGCA / NEW-MISC / 78 TO PREVENT THE LOADING OF THE BAROSET POTENTIOMETER, WHICH COULD RESULT IN AN UN ACCEPTABLE ALLTITUDE ERROR



TO PREVENT INTERROGATING AIRCRAFT FROM POSSIBLY RECEIVING INACURRATE REPLIES

FAA AD 2005-01-19 (ORIGINAL FAA AD 2004-10-15 IS REPLACED)

AS IN AD AS IN AD

DGCA / NEW-MISC / 80 TO PREVENT THE GPS NAVIGATION UNIT UNDER CERTAIN CONDITION, FROM PROVIDING ERRONEOUS CROSS DEVIATION INFORMATION.


DGCA / NEW-MISC / 81 OPERATIONAL ORDER ON DGAC AD F-2004-083 AS IN AD AS IN AD


INSTRUCTION FOR CONTINUED AIRWORTHINESS FOR LARGE AIRPLANES CERTIFICATED UNDER JAR 25

DGCA / NEW-MISC / 82 EQUIPMENT/ FURNISHINGS- LERMER GmbH WATER BOILERS

DGAC AD F-2004-132 AS IN AD AS IN AD

DGCA / NEW-MISC / 83 TO PREVENT SHIFTING OR UNRESTRAINED CARGO IN THE CARGO COMPARTMENT, WHICH COULD CAUSE AN UNEXPECTED CHANGE IN THE AIRPLANE'S CENTER OF GRAVITY


DGCA / NEW-MISC / 84 TO PREVENT FAILURE OF THE MAGNETO IMPULSE COUPLING ASSEMBLY AND POSSIBLE ENGINE FAILURE


DGCA / NEW-MISC / 85 TO CORRECT PROBLEMS WITH THE STANDBY VACUUM SYSTEMS (SVS) BEFORE FAILURE OR MALFUNCTION DURING INSTRUMENT FLIGHT RULES (IFR)


DGCA / NEW-MISC / 86 EQUIPMENT/FURNISHINGS- INSPECTION AND REPLACEMENT OF THE READING LIGHTS ELECTRICAL POWER SUPPLIES OF SOME SICMA AERO SEATS

DGAC AD F 2005-135 AS IN AD AS IN AD

DGCA / NEW-MISC / 87 TO PREVENT CERTAIN AIR DATA COMPUTERS (ADC) FROM DISPLAYING INCORRECT ALTITUDE INFORMATION (SHADIN ADC 2000)



DGCA / NEW-MISC / 88 TO PREVENT VACUUM PUMP FAILURE OR MALFUNCTION DURING INSTRUMENT FLIGHT RULES (IFR) FLIGHT


DGCA / NEW-MISC / 89 TO IDENTIFY AND PROVIDE CORRECTIVE ACTION FOR A POTENTIALLY INOPERATIVE SMOKE DETECTOR


DGCA / NEW-MISC / 90 TO PREVENT LOSS OF PRESSURE IN THE ESCAPE SLIDES/RAFTS AFTER AN EMERGENCY EVACUATION


DGCA / NEW-MISC / 91 TO PREVENT A BEARING ERROR, WHICH COULD LEAD TO AN AIRPLANE DEPARTING FROM ITS SCHEDULED FLIGHT PATH


DGCA / NEW-MISC / 92 COMMUNICATION --- COMM UNITS & TRANSPONDERS --- MODIFICATION / REPLACEMENT

FAA 2006 -19 - 04 / EASA AD 2007-0156

AS IN AD AS IN AD

DGCA / NEW-MISC / 93 EQUIPMENT & FURNISHING - PASSENGER SEATS REAR FITTING ASSEMBLY ATTACHMENT - REPLACEMENT

EASA AD 2006-0264 AS IN AD AS IN AD

DGCA / NEW-MISC / 94 TO PREVENT TREAD SEPERATION FROM A NOSEWHEEL TIRE DURING TAKEOFF OR LANDING


DGCA / NEW-MISC / 95 LANDING GEAR - MAIN LANDING GEAR WHEEL ASSEMBLY - INSPECTION / REPAIR


DGCA / NEW-MISC / 96 EQUIPMENT & FURNISHINGS - PASSENGER SEAT BACKREST -

EASA AD 2008 -0135 AS IN AD AS IN AD


REPLACEMENT

DGCA / NEW-MISC / 97 TO PREVENT DETACHMENT OF PASSENGER SEATS ASSEMBLIES DURING EMERGENCY CONDITIONS

FAA AS 2007-04-15 AS IN AD AS IN AD


TO PREVENT CYLINDER SEPRATION FAA AD 2007-04-19(R1) AS IN AD AS IN AD

DGCA / NEW-MISC / 99 OXYGEN---OXYGEN RESERVE CYLINDERS----REMOVAL/EMPTYING

EASA AD 2006-0286R1 AS IN AD AS IN AD

DGCA / NEW-MISC /100 TO PREVENT SHIFT IN FMS COMPUTED POSITION WHICH COULD RESULT IN UNCOMMANDED DEVIATIONS FROM THE INTENDED FLIGHT PATH OF THE AIRPLANE


DGCA / NEW-MISC /101 AIR TRANSPORT ASSOCIATION OF AMERICA (ATA) CODE 34:NAVIGATION

FAA AD 2007- 14 -06 AS IN AD AS IN AD

DGCA / NEW-MISC /102 EQUIPMENT & FURNISHING --- SEAT RESTRAINT SYSTEM PLASTIC ROTARY BUCKLE HANDLE --- INSPECTION /REPLACEMENT


DGCA / NEW-MISC /103 CVR- THE BULK ERASE FACILITY SHOULD BE DEACTIVATED BY REMOVING THE RELEVANT CARD FROM THE CVR UNIT.

DGCA LETTER NO. 9-414/96-AI(2) DT. 24TH SEPT 1996.

AS IN THE LETTER. AS IN THE LETTER.

DGCA / NEW-MISC /104 RISK OF HIGH PRESSURE OXYGEN CYLINDER TEARING


DGCA / NEW-MISC /105 TO PREVENT FAILURE OF AN EVACUATION SYSTEM


DGCA / NEW-MISC /106 NAVIGATION SYSTEMS --- MODE -- S EASA AD 2008 - 0159 AS IN AD AS IN AD


TRANSPONDER --- MODIFICATION/REPLACEMENT

DGCA / NEW-MISC /107 AIRCONDITIONING --- ZONAL DRYING SYSTEM DEACTIVATION

EASA AD 2006 - 0140R4 AS IN AD AS IN AD

DGCA / NEW-MISC /108 TO PREVENT THE POTENTIAL OF IGNITION SOURCES INSIDE FUEL TANKS WHICH IN COMBINATION WITH FLAMMABLE FUEL VAPOURS COULD RESULT IN FUEL TANKEXPLOSION & CONSEQUENT LOSS OF THE AIRPLANE

FAA AD 2008 - 22 -01 AS IN AD AS IN AD

DGCA / NEW-MISC /109 TO PREVENT APU COMPARTMENT FIRES & FUEL VAPOUR EXPLOSION


DGCA / NEW-MISC /110 TO PREVENT CERTAIN CONDITIONS FROM EXISTING WHEN PFD'S DISPLAY INCORRECT ATTITUDE,ALTITUDE,& AIRSPEED INFORMATION


DGCA / NEW-MISC /111 COMMUNICATIONS --- THALES COMMUNICATIONS VHF DATA RADIO --- MODIFICATION

EASA AD 2006 - 0334R1 AS IN AD AS IN AD

DGCA / NEW-MISC /112R1 NAVIGATION --- MODE S TRANSPONDER --- CHECK / MODIFICATION

EASA AD 2010 - 0067 AS IN AD AS IN AD

DGCA / NEW-MISC /113 IMPLEMENTATION OF FEDERAL AVIATION ADMINISTRATION (FAA) RULES REGARDING CRASHWORTHINESS STANDARDS FOR PASSEENGER OPERATIONS

FAR PART 121.311 Held in abeyance until further intimation

Reference (FAR 121.311)

DGCA / NEW-MISC /114R1 TO PREVENT FAILURE OF A HOOK FAA AD 2010-03-02 AS IN AD AS IN AD


DURING RESCUE HOIST OPERATIONS,LOSS OF THE RESCUED PASSENGER AND SUBSEQUENT SERIOUS INJURY OR FATALITY

DGCA / NEW-MISC /115R1 NAVIGATION --- MODE S TRANSPONDER --- MODIFICATION/REPLACEMENT

EASA AD 2009 -0173R1 AS IN AD AS IN AD

DGCA / NEW-MISC /116 NAVIGATION --- MODE A / C TRANSPONDER --- CHECK / MODIFICATION


DGCA / NEW-MISC /117R1 AIR TRANSPORT ASSOCIATION (ATA) OF AMERICA CODE 26: FIRE PROTECTION


DGCA / NEW-MISC /118R1 TO PREVENT AN OXYGEN CYLINDER FROM RUPTURING,WHICH,DEPENDING ON THE LOCATION,COULD RESULT IN STRUCTURAL DAMAGE & RAPID DECOMPRESSION OF THE AIRPLANE

FAA 2009 - 21 -10R1 AS IN AD AS IN AD

DGCA / NEW-MISC /119R1 FIRE PROTECTION --- HALON 1211 FIRE EXTINGUISHERS --- IDENTIFICATION / REPLACEMENT


DGCA / NEW-MISC /120 FIRE PROTECTION --- PORTABLE HALON 1211 FIRE EXTINGUISHERS --- IDENTIFICATION / REPLACEMENT


DGCA / NEW-MISC /121 EMEGENCY LOCATOR TRANSMITTER --- POTENTIAL FAILURE TO TRANSMIT THE REQUIRED 406 MHz CODED SIGNAL

TC AD CF -2009-44 AS IN AD AS IN AD

DGCA / NEW-MISC /122R1 NAVIGATION ---MODE S EASA AD 2010 - 0003R2 AS IN AD AS IN AD


TRANSPONDER AIRCRAFT TYPE MODE STRAPPING --- CHECK / MODIFICATION

REVISION

DGCA / NEW-MISC /123 TO PREVENT SEPERATION OR SEIZURE OF THE TURBOCHARGER TURBINE WHICH COULD RESULT IN FULL OR PARTIAL ENGINE POWER LOSS,LOSS OF ENGINE OIL AND SMOKE IN THE AIRPLANE CABIN

FAA AD 2010 -07-08 AS IN AD AS IN AD

DGCA/ NEW-MISC /124 OXYGEN CYLINDER –INSPECTION / REPLACEMENT -- TO PREVENT OXYGEN CYLINDER FROM RUPTURING


DGCA/ NEW-MISC /125 TO PREVENT LOSS OF PROPELLER PITCH CONTROL,DAMAGE TO THE PROPELLER GOVERNOR,AND INTERNAL DAMAGE TO THE ENGINE WHICH COULD PREVENT CONTINUED SAFE FLIGHT OR SAFE LANDING


DGCA/ NEW-MISC /126 COMMUNICATION --- VERY HIGH FREQUENCY (VHF/AM) TRANSCEIVER --- MODIFICATION


DGCA/ NEW-MISC /127 (R1)

ATA 34-NAVIGATION SYSTEMS --- MODE - S TRANSPONDER --- MODIFICATION / REPLACEMENT

EASA AD 2010 -0204 (CORRECTION:07 JUNE 2011)

AS IN AD AS IN AD

DGCA/ NEW-MISC /128 FLIGHT CONTROLS --- TURNBUCKLES --- INSPECTION


DGCA/ NEW-MISC /129 AIR TRANSPORT ASSOCIATION (ATA) OF AMERICA CODE



35:OXYGEN

DGCA/ NEW-MISC /130R3 JOINT AIRCRAFT SYSTEM COMPONENT/ATA OF AMERICA CODE 35,OXYGEN


DGCA/ NEW-MISC /131 NAVIGATION SYSTEMS --- MODE --- S TRANSPONDER CONTROL PANELS --- MODIFICATION


DGCA/ NEW-MISC /132(R1) ATA 35-OXYGEN -- OXYGEN MASK REGULATOR INFLATABLE HARNESS -- IDENTIFICATION / REPLACEMENT

EASA AD 2011 - 0090(R1) REVISES EASA AD 2011 - 0090 CORRECTION : 24 MAY 2011

AS IN AD AS IN AD

DGCA/ NEW-MISC /133 LIFE JACKETS FOR INFANT --- SMALL CHILD


DGCA/ NEW-MISC /134 EQUIPMENT / FURNISHINGS -- EMERGENCY LOCATOR TRANSMITTER (ELT) ANTENNA -- MODIFICATION/REPLACEMENT


DGCA/ NEW-MISC /135 ATA 25- EQUIPMENT & FURNISHINGS - PASSENGER SEAT - REPLACEMENT


DGCA/ NEW-MISC /136 TO PREVENT USING CONTAMINATED GAS THAT MAY REDUCE FIRE SUPRESSION AND RELEASE TOXIC FUMES THAT WOULD ENDANGER THE SAFETY OF THE HELICOPTER AND ITS OCCUPANTS


DGCA/ NEW-MISC /137 ATA 35 - OXYGEN FAA AD 2011-14-08 AS IN AD AS IN AD

DGCA/ NEW-MISC /138R1 AIR TRANSPORT ASSOCIATION (ATA) OF AMERICA CODE



25:EQUIPMENT/FURNISHINGS

DGCA/ NEW-MISC /139 ATA 34 ----- NAVIGATION --- RADIO ALTIMETER INDICATOR ---- MODIFICATION


DGCA/ NEW-MISC /140 TO INSTALL PLACARDS TO AID IN LOCATING & DEPLOYING LIFERAFTS TO PREVENT FURTHER INJURY OR LOSS OF LIFE IN THE EVENT OF A HELICOPTER LANDING IN THE WATER


DGCA/ NEW-MISC /141 TO PREVENT TCAS UNITS FROM DROPPING TRACKS,WHICH COULD COMPROMISE SEPERATION OF AIR TRAFFIC & LEAD TO SUBSEQUENT MID AIR COLISIONS


DGCA/ NEW-MISC /142 ATA 25 - EQUIPMENT & FURNISHINGS - PASSENGER SEAT BACKREST LINK - INSPECTION/REPLACEMENT


DGCA/ NEW-MISC /143 ATA 26 - FIRE PROTECTION - HAND OPERATED FIRE EXTINGUISHER - MODIFICATION


DGCA/ NEW-MISC /144 TO PREVENT LOSS OF PRESSURE IN THE ESCAPE SLIDES /RAFTS AFTER AN EMERGENCY EVACUATION ,WHICH COULD RESULT IN INADEQUATE BUOYANCY TO SUPPORT THE RAFTS PASSENGER CAPACITY DURING DITCHING AND INCREASE THE CHANCE FOR INJURY



TO RAFT PASSENGERS

DGCA/ NEW-MISC /145 TO PREVENT TURBOCHARGER,BEARING SEIZURE,FAILED TURBOCHARGER COMPONENTS,AND DAMAGE TO THE AIRPLANE


DGCA/ NEW-MISC /146 TO PREVENT MISLEADING INFORMATION DURING LOCALIZER PERFORMANCE (LP),LOCALIZER PERFORMANCE WITH VERTICAL GUIDANCE (LPV),OR SBAS LATERAL NAVIGATION / VERTICAL NAVIGATION (LNAV/VNAV) APPROACHES DUE TO SOFTWARE PROBLEM IN HONEYWELL WIDE AREA AUGMENTATION SYSTEM (WAAS) GLOBAL NAVIGATION SATELLITE SENSOR UNITS (GNSSU)


DGCA/ NEW-MISC /147 TO PREVENT FAILURE OF THE MAIN LANDING GEAR TIRES DURING TAKE OFF OR LANDING WHICH COULD CAUSE DAMAGE TO THE AIRPLANE STRUCTURE,FLAPS,ENGINE,AND WHEEL WELL & RESULT IN REDUCED CONTROLLABILITY OF THE AIRPLANE


DGCA/ NEW-MISC /148 TO PREVENT SEPERATION OF THE REAR GAS GENERATOR CASE AND RELEASE OF HIGH ENERGY DEBRIS ,WHICH COULD RESULT IN INJURY AND DAMAGE TO THE AIRPLANE



DGCA/ NEW-MISC /149R1 OXYGEN --- FLIGHT CREW OXYGEN MASK REGULATOR --- IDENTIFICATION / OPERATIONAL PROCEDURE / REPLACEMENT


DGCA/ NEW-MISC /150R1 TO PREVENT TURBOCHARGER TURBINE WHEEL FAILURE,REDUCTION OR COMPLETE LOSS OF ENGINE POWER,LOSS OF ENGINE OIL,OIL FIRE,AND DAMAGE TO THE AIRPLANE


DGCA/ NEW-MISC /151R1 AIR TRANSPORT ASSOCIATION (ATA) OF AMERICA CODE 34, NAVIGATION

FAA AD 2012-26-15R1 AMENDMNNT

AS IN AD AS IN AD

DGCA/ NEW-MISC /152R5 ATA 25: EQUIPMENT & FURNISHINGS --- SAFETY BELTS / TORSO RESTRAINT SYSTEMS --- INSPECTION / REPLACEMENT

EASA AD 2013-0020R4 Correction dated 05th september 2014

AS IN AD AS IN AD

DGCA/ NEW-MISC /153R10 ATA 25, EQUIPMENT / FURNISHINGS – HOIST – TEST / REPLACEMENT

EASA AD 2015-0226R3 REVISED EASA AD 2015-0226R1 REV EASA AD 2015-0226 SUPERSEDED(EASA AD2015-0160 SUPERSEDURE EASA AD 2015 -0069 SUPERSEDURE EASA AD 2014-0254 SUPER EASA AD2014-0201) supersedure EASA AD 2013 - 275R1

AS IN AD AS IN AD

DGCA/ NEW-MISC /154 EQUIPMENT / FURNISHINGS --- VARNISH ON VENEERED PANELS --- INSPECTION / RE - FURBISHING



DGCA/ NEW-MISC /155 UNSAFE CONDITION OWING TO SEARCHLIGHT / GIMBAL DISCONNECTING FROM THE HELICOPTER AND REMAINING ATTACHED SOLELY BY THE INTERNAL CABLE HARNESS,OR SEPERATING TOTALLY


DGCA/ NEW-MISC /156 TO PREVENT THE BRUSHES IN THE A/C MOTOR FROM WEARING DOWN ,WHICH COULD RESULT IN THE RIVET IN THE BRUSH CONTACTING THE COMMUTATOR CAUSING SPARKS AND CONSEQUENT FIRE AND/OR SMOKE IN THE TAILCONE WITH NO MEANS TO DETECT OR EXTINGUISH THE FIRE AND / OR SMOKE


DGCA/ NEW-MISC /157 TO PREVENT THE FAILURE OF URETHANE SEALS TO MAINTAIN SUFFICIENT HALON CONCENTRATIONS IN THE CARGO COMPARTMENTS TO EXTINGUISH OR CONTAIN FIRE OR SMOKE AND TO PREVENT PENETRATION OF FIRE OR SMOKE IN AREAS OF THE AIRPLANE THAT ARE DIFFICULT TO ACCESS FOR FIRE


DGCA/ NEW-MISC /158 UNSAFE CONDITION AS FAILURE OF THE OVERLOAD CLUTCH RESULTING IN IN FLIGHT FAILURE OF THE HOIST WHICH COULD RESULT IN INJURY



TO PERSONS BEING LIFTED

DGCA/ NEW-MISC /159R1 TO DETECT & CORRECT DISCREPANCIES OF THE BATTERY WIRING INSTALLATION INSIDE THE TU,WHICH COULD RESULT IN AN ELECTRICAL SHORT AND POSSIBLE IGNITION SOURCE

FAA AD 2014-17-02 AMENDMENT FAA AD 2013-18-09

AS IN AD AS IN AD

DGCA/ NEW-MISC /160R2 EQUIPMENT / FURNISHINGS --- CRASH POSITION INDICATOR --- MODIFICATION AIRCRAFT FLIGHT MANUAL --- AMENDMENT

EASA AD 2014-0095R1 REVISION EASA AD 2014-0095 SUPERSEDURE EASA AD 2014-0019

AS IN AD AS IN AD

DGCA/ NEW-MISC /161 TO CORRECT POSSIBLE MISALIGNMENT ISSUES WITH THE TRANSPONDERS THAT COULD RESULT IN INCREASED PILOT AND AIR TRAFFIC CONTROLLER WORKLOAD AS WELL AS REDUCED SEPARATION OF AIRPLANES


DGCA/NEW-MISC /162 ATA 23 ,COMMUNICATIONS – COCKPIT VOICE RECORDER – REPLACEMENT


DGCA/NEW-MISC /163 EQUIPMENT / FURNISHINGS – CRASH POSITION INDICATOR SYSTEM –REPLACEMENT, AIRCRAFT FLIGHT MANUAL – AMENDMENT


DGCA/NEW-MISC /164 ATA 35, OXYGEN – OXYGEN MASK REGULATOR INFLATABLE HARNESS / INFLATION HOSE – IDENTIFICATION / REPLACEMENT


DGCA/NEW-MISC /165 ATA 25, EQUIPMENT & EASA AD 2014-0187 AS IN AD AS IN AD


FURNISHINGS – SAFETY BELT ATTACHMENT BOLTS –INSPECTION / REPLACEMENT

DGCA/NEW-MISC /166R3 ATA 25, EQUIPMENT & FURNISHINGS – EMERGENCY FLOTATION SYSTEM – ROTORCRAFT FLIGHT MANUAL (SUPPLEMENT)


DGCA/NEW-MISC /167R1 ATA 25, EQUIPMENT & FURNISHINGS – EMERGENCY FLOTATION SYSTEM – ROTORCRAFT FLIGHT MANUAL (SUPPLEMENT)

EASA AD 2014-0244 SUPERSEDURE EASA AD 2014-0189

AS IN AD AS IN AD

DGCA/NEW-MISC /168 TO DETECT AND CORRECT MODE S TRANSPONDERS THAT DO NOT RESPOND CORRECTLY TO MODE S ONLY ALL-CALL INTERROGATIONS, WHICH COULD RESULT IN INCREASED PILOT AND AIR TRAFFIC CONTROLLER WORKLOAD AS WELL AS REDUCED SEPARATION OF AIRPLANES


DGCA/NEW-MISC /169R1 TO DETECT AND CORRECT CRACKS IN THE BACKREST LINKS, WHICH COULD AFFECT THE STRUCTURAL INTEGRITY OF SEAT BACKRESTS. FAILURE OF THE BACKREST LINKS COULD RESULT IN INJURY TO AN OCCUPANT DURING EMERGENCY LANDING CONDITIONS

FAA AD 2015-10-02 amendment FAA AD 2014-20-11

AS IN AD AS IN AD

DGCA/NEW-MISC /170 ATA 25, EQUIPMENT / FURNISHING – RESTRAINT SYSTEM ROTARY



BUCKLE SUBASSEMBLY– IDENTIFICATION / REPLACEMENT

DGCA/NEW-MISC /171 ATA 34- NAVIGATION,TO PREVENT SUCH INCORRECT DISPLAY OF LATERAL DEVIATIONS, WHICH COULD RESULT IN THE PILOT MAKING FLIGHT DECISIONS THAT PUT THE AIRCRAFT IN UNSAFE FLIGHT CONDITIONS, FLYING INTO AIRSPACE THAT WAS, BY THE GPS APPROACH DESIGN, TO BE AVOIDED (TERRAIN, OBSTACLE, TRAFFIC, RESTRICTED)


DGCA/NEW-MISC /172 TO DETECT AND CORRECT DEFECTIVE HARNESSES, WHICH COULD LEAD, IN CASE OF A SUDDEN DEPRESSURIZATION EVENT, TO A HARNESS RUPTURE, THEREBY PROVIDING INADEQUATE PROTECTION AGAINST HYPOXIA AND POSSIBLY RESULTING IN UNCONSCIOUSNESS OF THE AFFECTED FLIGHTCREW MEMBER AND CONSEQUENT REDUCED CONTROL OF THE AIRPLANE


DGCA/NEW-MISC /173 ATA -34, NAVIGATION – ATTITUDE HEADING REFERENCE SYSTEM – MODIFICATION / REPLACEMENT


DGCA/NEW-MISC /174 TO PREVENT FIRE EXTINGUISHERS FROM FAILING TO OPERATE IN THE EVENT OF A FIRE, WHICH COULD



JEOPARDIZE OCCUPANTS' SAFETY AND CONTINUATION OF SAFE FLIGHT AND LANDING

DGCA/NEW-MISC/175 TO DETECT AND CORRECT SOLDER DEPOSITED ON THE FRANGIBLE PLUG OF THE FIRE EXTINGUISHER, WHICH COULD RESULT IN FAILURE OF THE FIRE EXTINGUISHER TO DISCHARGE, AND CONSEQUENT INABILITY TO PUT OUT A FIRE IN AN ENGINE OR IN THE APU.


DGCA/NEW-MISC/176 TO DETECT AND CORRECT AFFECTED OXYGEN MASK REGULATORS, WHICH COULD LEAD, IN CASE OF MASK USAGE AT OR ABOVE 10,000 FEET AFTER A DEPRESSURIZATION EVENT, TO THE INHALATION OF AIR WITH IMPROPER CONTENT OF OXYGEN, DUE TO THE BAD DILUTION SETTINGS, THEREBY PROVIDING INADEQUATE PROTECTION TO THE AFFECTED FLIGTHCREW AGAINST HYPOXIA. HYPOXIA CAN START FROM A HEADACHE AND DROWSINESS AND LEAD EVENTUALLY TO UNCONSCIOUSNESS WITH SEVERE CONSEQUENCE IN TERMS OF AIRPLANE CONTROLLABILITY.


DGCA/NEW-MISC/177R1 B/E AEROSPACE PROTECTIVE FAA AD 2017-18-12 AS IN AD AS IN AD


BREATHING EQUIPMENT (PBE), PART NUMBER (P/N) 119003-11, THAT IS INSTALLED ON AIRPLANES.

SUPERSEDED FAA AD 2016-11-20

DGCA/NEW-MISC/178 APPLICABLE TO PMC11, PMC31 AND GMC11 SMOKE DETECTORS AND SUBJECT OF THE AD IS ATA 26-FIRE PROTECTION-OPTICAL AND AMBIENT SMOKE DETECTORS-IDENTIFICATION/REPLACEMENT, IF NOT CORRECTED, WILL GENERATE AN ABNORMAL AGEING OF THE SMOKE DETECTOR, LEADING TO A DECREASE OF THE LIGHT INTENSITY CAPABILITY, POSSIBLY RESULTING IN FAILURE TO DETECT SMOKE AND CONSEQUENT RISK OF AN ON BOARD UNCONTROLLED FIRE.,


DGCA/NEW-MISC/179 APPLICABLE TO 10-30/24, 12-61/24 AND 12-82/23 EMERGENCY PARACHUTES AND SUBJECT OF THE AD IS ATA 25-EQUIPMENT/FURNISHINGS-EMERGENCY PARACHUTE RUBBER BANDS-REPLACEMENT, IF NOT CORRECTED, COULD CAUSE A MALFUNCTION OF THE EMERGENCY PARACHUTE. FOR THE REASONS DESCRIBED ABOVE, THIS AD REQUIRES REPLACEMENT OF THE AFFECTED RUBBER BANDS WITH SERVICEABLE RUBBER BANDS.



DGCA/NEW-MISC/180 APPLICABLE TO KIDDE GRAVINER SINGLE HEAD AUTOMATIC FIRE EXTINGUISHERS AND SUBJECT OF THE AD IS ATA 26-FIRE PROTECTION-ENGINE AND AUXILIARY POWER UNIT AUTOMATIC FIRE EXTINGUISHERS-INSPECTION/OVERHAUL, IF NOT DETECTED AND CORRECTED, COULD RESULT IN THE FAILURE OF THE FIRE BOTTLE TO DISCHARGE, WHICH REDUCES THE ABILITY OF THE FIRE PROTECTION SYSTEM TO EXTINGUISH FIRES IN THE ENGINE OR AUXILIARY POWER UNIT (APU) FIRE ZONES, POSSIBLY RESULTING IN DAMAGE TO THE AEROPLANE AND INJURY TO THE OCCUPANTS. DUE TO SIMILARITY OF DESIGN, THIS CONDITION MAY ALSO AFFECT OTHER P/N FIRE EXTINGUISHERS.


DGCA/NEW-MISC/181 ATA 28 – FUEL – BURNER AND FUEL HOSES – IDENTIFICATION / REPLACEMENT, IF NOT DETECTED AND CORRECTED, COULD RESULT IN A FIRE, DAMAGING THE BALLOON AND ITS ENVELOPE, ULTIMATELY LEADING TO AN EMERGENCY LANDING, WITH CONSEQUENT INJURY TO BALLOON OCCUPANTS AND PERSONS ON THE GROUND.



DGCA/NEW-MISC/182R1 ATA 25 – EQUIPMENT / FURNISHINGS – REAR CABIN ATTENDANT SEAT – INSPECTION / REPAIR, IF NOT DETECTED AND CORRECTED, COULD LEAD TO FAILURE OF THE SEAT OCCUPIED BY THE CABIN ATTENDANT, POSSIBLY RESULTING IN INJURY TO THE SEAT OCCUPANT.

EASA AD 2016-0167R1

REVISED (CORRECTOION:

01 MARCH 2018) EASA AD

2016-0167

AS IN AD AS IN AD

DGCA/NEW-MISC/183 ATA 25 – EQUIPMENT / FURNISHINGS – SEAT ENERGY ABSORBER ASSEMBLY – REPLACEMENT, IF NOT DETECTED AND CORRECTED, COULD LEAD TO INJURY OF THE SEAT OCCUPANT.


DGCA/NEW-MISC/184 ATA 28 – FUEL – CROSS FEED FUEL PIPE – REPLACEMENT, IF NOT CORRECTED, COULD LEAD TO A FUEL LEAKAGE WHICH, IF NEAR AN IGNITION SOURCE FROM THE ELECTRICAL EQUIPMENT, COULD RESULT IN A FIRE OR A FUEL VAPOR EXPLOSION WITH CONSEQUENT LOSS OF THE AEROPLANE.


DGCA/NEW-MISC/185 ATA 25 – EQUIPMENT / FURNISHINGS – PILOT AND CO-PILOT SEATS – MODIFICATION, IF NOT CORRECTED, COULD LEAD TO FURTHER CASES OF UNWANTED FLIGHT CREW SEAT



MOVEMENT, POSSIBLY RESULTING IN REDUCED CONTROL OF THE AEROPLANE.

DGCA/NEW-MISC/186 AIR TRANSPORT ASSOCIATION (ATA) OF AMERICA CODE 57, WINGS, ISSUED TO DETECT AND CORRECT CORROSION AND CRACKING OF THE WING FIXED LEADING EDGE AND FRONT SPAR STRUCTURE, WHICH COULD RESULT IN REDUCED STRUCTURAL INTEGRITY OF THE AIRPLANE.


DGCA/NEW-MISC/187 AIR TRANSPORT ASSOCIATION (ATA) OF AMERICA CODE 32, LANDING GEAR, ISSUED TO PREVENT SUCH CRACKING, WHICH COULD RESULT IN DEPLETION OF THE COMBINED (LEFT) AND UTILITY HYDRAULIC SYSTEM FLUID AND THE NITROGEN EMERGENCY BLOW DOWN SYSTEM, FAILURE OF THE COMBINED (LEFT) HYDRAULIC SYSTEM (ALL PHRASES) TO PROVIDE ADEQUATE HYDRAULIC PRESSURE, AND FAILURE OF THE MLG TO EXTEND WHEN COMMANDED.


DGCA/NEW-MISC/188 AIR TRANSPORT ASSOCIATION (ATA) OF AMERICA CODE 27, FLIGHT CONTROLS, TO PREVENT



FAILURE OF THE ELEVATOR ASSEMBLY AND CONSEQUENT LOSS OF CONTROL OF THE AIRPLANE.

DGCA/NEW-MISC/189 AIR TRANSPORT ASSOCIATION (ATA) OF AMERICA CODE 32, LANDING GEAR; 53, FUSELAGE; 54, NACELLES/PYLONS; 55, STABILIZERS; AND 57, WINGS, TO ENSURE FATIGUE CRACKING OF PRINCIPAL STRUCTURAL ELEMENTS (PSES) IS DETECTED AND CORRECTED; SUCH FATIGUE CRACKING COULD RESULT IN REDUCED STRUCTURAL INTEGRITY OF THE PSES AND CRITICAL COMPONENTS.


DGCA/NEW-MISC/190 AIR TRANSPORT ASSOCIATION (ATA) OF AMERICA CODE 44, CABIN SYSTEMS, TO PREVENT DISPLAY OF MISLEADING ALTITUDE DATA, WHICH COULD RESULT IN INADVERTENT FLIGHT INTO TERRAIN


DGCA/NEW-MISC/191 AIR TRANSPORT ASSOCIATION (ATA) OF AMERICA CODE 2140; HEATING SYSTEM, TO DETECT AND CORRECT A HAZARDOUS CONDITION CAUSED BY DETERIORATION OF THE COMBUSTION HEATER, WHICH COULD LEAD TO IGNITION OF



COMPONENTS AND RESULT IN SMOKE AND FUMES IN THE CABIN.

DGCA/NEW-MISC/192 AIR TRANSPORT ASSOCIATION (ATA) OF AMERICA CODE 2520, PASSENGER COMPARTMENT EQUIPMENT, TO PREVENT SERIOUS INJURY TO THE OCCUPANT DURING FORWARD IMPACTS IN EMERGENCY LANDING CONDITIONS


DGCA/NEW-MISC/193 AIR TRANSPORT ASSOCIATION (ATA) OF AMERICA CODE 34, NAVIGATION, TO DEFINES THE UNSAFE CONDITION AS AN ADS-B UNIT INCORRECTLY BROADCASTING A SOURCE INTEGRITY LEVEL (SIL) OF 3 INSTEAD OF ITS AUTHORIZED SIL OF 0. THIS CONDITION COULD RESULT IN THE UNIT COMMUNICATING UNRELIABLE POSITION INFORMATION TO AIR TRAFFIC CONTROL AND NEARBY AIRCRAFT AND A SUBSEQUENT AIRCRAFT COLLISION.


DGCA/NEW-MISC/194 AIR TRANSPORT ASSOCIATION (ATA) OF AMERICA CODE 25 EQUIPMENT/FURNISHINGS. THIS AD DEFINES THE UNSAFE CONDITION AS A BROKEN BUCKLE KNOB. THIS CONDITION COULD RESULT IN A RESTRAINT SYSTEM STRAP FAILING TO RELEASE FROM



THE BUCKLE, PREVENTING OCCUPANTS FROM EXITING THE HELICOPTER DURING AN EMERGENCY

DGCA/NEW-MISC/195 ATA 25 – EQUIPMENT / FURNISHINGS – CABIN ATTENDANT SEAT – INSPECTION


DGCA/NEW-MISC/196 JOINT AIRCRAFT SYSTEM COMPONENT (JASC) CODE 2611, SMOKE DETECTION, TO PREVENT FAILURE OF THE SMOKE DETECTOR, ON-BOARD UNCONTROLLED FIRE, AND DAMAGE TO THE AIRPLANE.


DGCA/NEW-MISC/197 JOINT AIRCRAFT SYSTEM COMPONENT (JASC) CODE 2510, FLIGHT COMPARTMENT EQUIPMENT; TO PREVENT UNEXPECTED MOVEMENT OF PILOT AND CO-PILOT SEATS ON TAKEOFF AND LANDING. THE UNSAFE CONDITION, IF NOT CORRECTED, COULD RESULT IN REDUCED CONTROL OF THE AIRPLANE.


DGCA/NEW-MISC/198 ATA – 25, EQUIPMENT / FURNISHINGS – SEAT RESTRAINT SYSTEMS – AFM AMENDMENT / MODIFICATION.


DGCA/NEW-MISC/199 JOINT AIRCRAFT SYSTEM COMPONENT (JASC)/AIR TRANSPORT ASSOCIATION (ATA) OF



AMERICA CODE 7820, EXHAUST NOISE SUPPRESSOR

DGCA/NEW-MISC/200 JOINT AIRCRAFT SYSTEM COMPONENT (JASC)/AIR TRANSPORT ASSOCIATION (ATA) OF AMERICA CODE 3414, AIRSPEED/MACH INDICATOR- TO PREVENT INCORRECT AIRSPEED INDICATIONS DURING FLIGHT, WHICH COULD LEAD TO LOSS OF CONTROL. DUE TO DESIGN REDUNDANCY, THIS IS ONLY APPLICABLE IF MORE THAN ONE DEFICIENT PROBE IS INSTALLED.


DGCA NO SUBJECT REFERENCE AD COMPLIANCE

Documents

Transcript of DGCA NO SUBJECT REFERENCE AD COMPLIANCE