DGCA NO SUBJECT REFERENCE AD COMPLIANCE APPLICABILITY DGCA / P-68 / 01 LIMIT STOP PILOT'S SEATS RAI AD NO.72-72/P.68-1 AS IN AD AS IN AD DGCA / P-68 / 02 ENGINE LEVERS PEDESTAL RAI AD NO.73-87/P.68-2 AS IN AD AS IN AD DGCA / P-68 / 03 ALTERNATOR WARNING PROTECTION RAI AD NO.74-116/P.64,P66- AS IN AD AS IN AD 10,P.68-3 DGCA / P-68 / 04 AMENDMENT OF PLACARDS AND FLIGHT MANUAL RAI AD NO.75-195/P.68-8 AND AS IN AD AS IN AD RAI AD NO.75-196/P.68-9 DGCA / P-68 / 05 RIGHT SYSTEM FUEL FILTER RAI AD NO.75-156/P.68-5 AS IN AD AS IN AD DGCA / P-68 / 06 STABILATOR RAI AD NO.75-171/P.68-6 AS IN AD AS IN AD DGCA / P-68 / 07 FUEL SELECTORS PLACARD RA AD NO.85-150/P68-7 RI AS IN AD AS IN AD DGCA / P-68 / 08 ENGINE MOUNTS RAI AD NO.75-252/P.68-10 AS IN AD AS IN AD DGCA / P-68 / 09 FUEL TANKS RAI AD NO.76-129/P.68-11 AS IN AD AS IN AD DGCA / P-68 / 10 FUEL BOWL FILTER MANUFACTURED BY THE FIRM "SECONDO MONA" RAI AD NO.76-209/P.64, P.66- AS IN AD AS IN AD P/N 7760A 11, P.68-12 DGCA / P-68 / 11 ELECTRICAL SYSTEM P.68 RAI AD NO.77-157/P.68-13 R1 AS IN AD AS IN AD DGCA / P-68 / 12 RUDDER TRIM CONTROL ROD P/N 68-5.6053 RAI AD NO. 77-161/P.68-14 AS IN AD AS IN AD DGCA / P-68 / 13 FLAP ACTUATOR SWITCH P/N NOR-7.345-1/M RAI AD NO. 83-26/P.68-15 R3 AS IN AD AS IN AD DGCA / P-68 / 14 STABILATOR BALANCE WEIGHT ATTACHMENT CHANNEL P/N 68- RAI AD NO.78-107/P.68-16 AS IN ADS AS IN ADS 3.3017-3 AND FAA AD 80-01-01 DGCA / P-68 / 15 ELEVATOR MASS BALANCE ATTACHMENT P/N 68-3:3017-3 RAI AD NO.78-201/P.68-16 R2 AS IN AD AS IN AD DGCA / P-68 / 16 FUSELAGE FRAME 3 AND MOUNTING BRACKETS FOR RUDDER RAI AD NO. 78-184/P.68-17 AS IN AD AS IN AD CONTROL CABLE PULLEYS DGCA / P-68 / 17 PROPELLER PITCH CONTROL JOINT END RAI AD NO.78-187/P.68-18 AS IN ADS AS IN ADS AND FAA AD 81-07-03 DGCA / P-68 / 18 FRAME NO.3 AND RUDDER REDAL INTERCONNECTING BELL CRANK RAI AD NO.80-88/P.68-17 R2 AS IN ADS AS IN ADS BRACKETS AND FAA AD 80-15-02 DGCA / P-68 / 19 LONGITUDINAL TRIM SYSTEM RAI AD NO.80-7/P.68-19 R3 AS IN ADS AS IN ADS AND FAA AD 81-07-08 DGCA NO SUBJECT REFERENCE AD COMPLIANCE APPLICABILITY DGCA / P-68 / 20 AUXILIARY FUEL PUMP DRAINAGE RAI AD NO.79-148/P.68-20 AS IN AD AS IN AD DGCA / P-68 / 21 OIL COOLER LEFT ELBOW FITTING RAI AD NO.79-186/P.68-21 AS IN ADS AS IN ADS AND FAA AD 83-05-07 DGCA / P-68 / 22 CONTROL WHEEL SHAFT UNIVERSAL JOINT P/N NOR 7315-03 RAI AD 80-1/P68-22 AND FAA AS IN ADS AS IN ADS AD 82-18-11 DGCA / P-68 / 23 MAGNETO' GROUND WIRE RAI AD NO.81-100/P.68-23 AS IN AD AS IN AD DGCA / P-68 / 24 ALTERNATOR OUTPUT CABLE RAI AD 91-151/P68-25 AS IN AD AS IN AD DGCA / P-68 / 25 FIN AREA RAI AD 81-151/P68-25 AND AS IN ADS AS IN ADS FAA AD 83-14-03 DGCA / P-68 / 26 PUEL PIPES SECTIONS BEHIND ENGINE COMPARTMENT FIREWALL RAI AD 82-197/P68-26 AS IN AD AS IN AD DGCA / P-68 / 28 STABILATOR TORQUE TUBE BRACKET ATTACHMENT BOLTS RAI AD 83-54/P68-28 AND AS IN ADS AS IN ADS FAA AD 83-15-04 DGCA / P-68 / 29 AILERON CONTROL CABLES RAI AD 84-130/P68-29 R1 AS IN AD AS IN AD DGCA / P-68 / 30 FUEL SYSTEM RAI AD 91-124/P68-30 R3 AS IN AD AS IN AD DGCA / P-68 / 31 STABILATOR TRAVEL STOP RAI AD NO.84-129/P68-31 AS IN AD AS IN AD DGCA / P-68 / 32 AILERON CONTROL CHAIN RAI AD NO.84-146/P-68-32 AS IN ADS AS IN ADS AND FAA AD 85-08-06 DGCA / P-68 / 33 R1 TO DETECT & CORRECT CRACKS IN THE FRONT & REAR WING FAA AD 2009 - 24 -03 AS IN ADS AS IN ADS SPARS,WHICH COULD RESULT IN THE WING SEPERATING FROM THE AIRPLANE DGCA / P-68 / 34 FIBERGLASS WING LEADING EDGES RAI AD 87-36/P68-34 R1 AND AS IN ADS AS IN ADS FAA AD 87-10-12 DGCA / P-68 / 35 MANUFACTURER-TYPE - BRAKE OIL RAI AD 86-22/P68-35 AS IN AD AS IN AD DGCA / P-68 / 36 ENGINE MOUNT-WING ATTACHMENT RAI AD 91-453/P68-36 R4 AND AS IN ADS AS IN ADS FAA AD 88-13-08 DGCA / P-68 / 37 OVERHEAD PANEL ON THE LEFT HAND PILOT SEAT RAI AD 87-27/P68-1 AS IN AD AS IN AD DGCA / P-68 / 38 STABILATOR TRIM TAB RAI AD 88-167/P68-37 AND AS IN ADS AS IN ADS FAA AD 88-21-04 DGCA NO SUBJECT REFERENCE AD COMPLIANCE APPLICABILITY DGCA / P-68 / 39 FLIGHT CONTROL CABLES INSPECTION RAI AD NO.92-089 AS IN AD AS IN AD DGCA / P-68 / 40 ENGINE MOUNT INSTALLATION INSPECTION RAI AD NO.89-71/P68-39 AND AS IN ADS AS IN ADS FAA AD 89-03-03 DGCA / P-68 / 41 ENGINE AND PROPELLER CONTROL CABLES RAI AD 90-262/P68-40 AS IN AD AS IN AD DGCA / P-68 / 42 INSPECTION OF ENGINE MOUNTS RAI AD 91-83/P68/41 AS IN AD AS IN AD DGCA / P-68 / 43 MAFFLER ASSEMBLY LH AND RH P/H P/N 6.1033-3/4 RAI AD NO.91-125/P68-42 AS IN AD AS IN AD DGCA / P-68 / 44 STABILATOR RAI AD NO.91-272/P68-44 AS IN ADS AS IN ADS AND FAA AD 91-22-06 DGCA / P-68 / 45 FUEL AND DEICE SYSTEMS RAI AD NO.91-351/P68-2 AS IN AD AS IN AD DGCA / P-68 / 46 STABILATOR TURQUE TUBE RAI AD NO.92-155 AS IN AD AS IN AD DGCA / P-68 / 47 FUEL SYSTEM RAI AD NO.93-070 AS IN AD AS IN AD DGCA / P-68 / 48 FUEL SELECTOR CONTROL RAI AD NO.94-014 AS IN AD AS IN AD DGCA / P-68 / 49 CORROSION ON STABILATOR TORQUE TUBE ATTACHMENT SHELVES RAI AD NO.94-026 AS IN AD AS IN AD DGCA / P-68 / 50 ENGINE OIL COOLER SYSTEM HOSES RAI AD NO.94-027 AS IN AD AS IN AD DGCA / P-68 / 51 ENGINE ALTERNATE SYSTEM RAI AD NO.94-028 AS IN AD AS IN AD DGCA / P-68 / 52 INSTALLATION OF STOP TUBE KIT AND ADJUSTMENT OF THE FUEL FAA AD 83-07-17 AS IN AD AS IN AD SELECTOR CONTROL DGCA / P-68 / 53 INSPECTION OF THE AILERON CONTROL CABLE TO THE RIGHT SIDE OF FAA AD 87-04-20 AS IN AD AS IN AD THE PHOTOGRAMMETRIC HATCH DGCA / P-68 / 54 TO PREVENT FUEL LEAKAGE INTO THE A/P CABIN FAA AD 91-11-14 AS IN AD AS IN AD DGCA / P-68 / 55 IMPROVEMENT OF FUEL TANK VENT SYSTEM TAAL/MOD/1 ISSUE DT.9.6.95 AS IN AD AS IN AD DGCA / P-68 / 56 TO PREVENT FAILURE OF THE NLG UPPER STRUT FAA AD 2000-24-05 AS IN AD & AS IN AD & SB SB DGCA / P-68 / 57R1 STRUCTURES --- WING SAFE LIFE FATIGUE LIMITS / WINGS & EASA AD 2010-0051 AS IN AD & AS IN AD & SB STABILIZERS STRUCTURES ---IMPLEMENTATION/INSPECTION SUPERSEDED EASA AD 2007- SB 0027 DGCA NO SUBJECT REFERENCE AD COMPLIANCE APPLICABILITY DGCA / P-68 / 58 THE BACKREST RECLINE OF PILOT & CO-PILOT REQUIRES THE REMOVAL IT-2004-522 AS IN AD & AS IN AD & SB OF QUICK RELEASE PIN SB DGCA / P-68 / 59R1 ENGINE INDICATING SYSTEM --- MUTIFUNCTION ENGINE GAUGE --- EASA AD 2014-0133 AS IN AD & AS IN AD & SB INSPECTION/REPLACEMENT SUPERSEDED EASA AD 2014- SB 0020 DGCA / P-68 / 60 TO DETECT AND CORRECT CRACKING AND CORROSION OF THE WING FAA AD 2014-10-01 AS IN AD & AS IN AD & SB SPARS, WHICH, IF NOT CORRECTED, COULD RESULT IN STRUCTURAL SB FAILURE OF THE WING DGCA / P-68 / 61 ATA- AIRCRAFT FLIGHT MANUAL – ALL ENGINE OPERATIVE RATE OF EASA AD 2015-0145 AS IN AD & AS IN AD & SB CLIMB PERFORMANCE – REVISION SB .