DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/B 300/1(R1) INSPECTION OF NOSE LANDING GEAR FORK ASSEMBLY TO FAA AD 2004-23-02, ORG FAA AD AS IN AD AS IN DETECT CRACKS. 87-22-01(R1)IS SUPERSEEDED. AD,02/12/04 DGCA/B 300/2 INSPECTION/ MODIFICATION OF WING SKINS. FAA AD 89-19-04 R1 & AS IN AD AS IN AD BEECHCRAFT MANDATORY SB 2040 R3 DGCA/B 300/3 INSPECTION/ ADJUSTMENT OF UPPER AFT COWLING ACCESS FAA AD 93-01-20 & BEECH SB AS IN AD AS IN AD DOOR LATCHES. 2329 DGCA/B 300/4 DETERMINATION OF SCOTCH FOAM IN EITHER AILERON AT FAA AD 89-22-14 & BEECH SB AS IN AD AS IN AD MANUFACTURE AND ìITS REMOVAL. 2256 DGCA/B 300/5 FUSELAGE - INSPECTION OF AFT FUSELAGE MOISTURED FAA AD 90-08-17 AND BEECH SB AS IN AD AS IN AD DRAINAGE SYSTEM. 2312. DGCA/B 300/6 INSPECTION AND REPLACEMENT OF CAST ACRYLIC COCKPIT FAA AD 91-12-11 AS IN AD. AS IN AD. "D" SIDE ìWINDOW. DGCA/B 300/7 ESTABLISHMENT OF RESTRICTIVE LIFE LIMITS FOR THE LOWER FAA AD 91-12-10 AS IN AD. AS IN AD. FORWARD ìWING ATTACH FITTINGS. DGCA/B 300/8 INCORPORATION OF REVISED TAKEOFF AND CLIMB FAA AD 91-20-14R1 AS IN AD. AS IN AD. PERFORMANCE CHARTS ìINTO THE POH/AFM. DGCA/B 300/9 ONE TIME VISUAL INSPECTION OF ALL ENGINE TRUSS-TO- FAA AD 92-15-01 AS IN AD. AS IN AD. FIREWALL BOLTS. DGCA/B 300/10 WINGS ATTACH FITTINGS WITH INCONEL BOLTS AND NUTS. BVAD 93-115(B) AS IN AD. AS IN AD. DGCA/B 300/11 INSPECTION OF CABIN SEAT FRAMES FOR CRACKS AND FAA AD 94-01-01 AND BEECH SB AS IN AD. AS IN AD MODIFICATION AND ìREPAIR TO THE CABIN SEATS. 2443 OR TOSINGTON SB 001. AND SB. DGCA/B 300/12(R1) REPETITIVE INSPECTION TO FUSELAGE STRINGERS 5 THROUGH FAA AD 2005-01-18, ORIGINAL AS IN AD. AS IN AD 11 FOR ìCRACKS AND REPAIR OF CRACKED STRINGERS. FAA AD 93-25-07 IS AND SB. SUPERSEEDED. DGCA/B 300/13 PREVENT CRACKING & FAILURE OF OUTFLOW /SAFETY VALVES FAA AD 96-17-10 AS IN AD. AS IN AD. WHICH COULD RESULT IN RAPID DECOMPRESSION OF AIRPLANE DGCA/B 300/14 TO PREVENT NOSEDOWN PITCH & A DESCENT ROLE FAA AD 97-25-03 AS IN AD. AS IN AD. DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/B 300/15 TO PREVENT OUTFLOW/ SAFETY VALVE CRACKING FAA AD 97-25-01 AS IN AD. AS IN AD. DGCA/B 300/16 REVISION ON AIRPLANE FLIGHT MANUAL SAFETY PROCEDURE FAA AD 98-04-24 AS IN AD. AS IN AD. DGCA/B 300/17(R1) TO PREVENT FUEL FLOW INTERRUPTION FAA AD 2005-01-04, ORG FAA AD AS IN AD. AS IN AD. 98-15-13 IS SUPERSEEDED DGCA/B 300/18 TO PREVENT FAILURE OF THE ACTUATOR CLEVIS ASSEMBLY IN FAA AD 98-21-35 AS IN AD. AS IN AD. MAIN L/G CAUSED BY FATIGUECRACKING DGCA/B 300/19 MODIFYING THE ELEVATOR TRIM TAB ACTUATORS FAA AD 99-02-15 AS IN AD. AS IN AD. DGCA/B 300/20 TO DETECT ANY IMPROPERLY MACHINEDL/G EMERGENCY FAA AD 99-18-15 AS IN AD. AS IN AD. HAND PUMPS DGCA/B 300/21 TO PREVENT THE BALANCE WEIGHT ATTACHMENT SCREWS FAA AD 2002-23-11 'AS IN AD' 'AS IN AD' FROM BECOMING LOOSE DGCA/B 300/22 TO ASSURE THAT CLEAR & COMPLETE OPERATING FAA AD 2003-02-03 'AS IN AD' 'AS IN AD' INSTRUCTION ARE VISIBLE FOR OPENING THE AIR STAIR DOOR & EMERGENCY EXITS DGCA/B 300/23 TO DETECT & CORRECT LOOSE BOLTS NOT SECURING THE FAA AD 2004-17-02 AS IN AD AS IN AD PEDESTAL CROSS SHAFT DGCA/B 300/24 TO PREVENT A LOSS OF VACUUM TO DEPRESSURIZE THE FAA AD 97-23-17 AS IN AD AS IN AD AIRPLANE CABIN. DGCA/B 300/25 TO PREVENT THE PASSENGER SEATS FROM FAILING DURING FAA AD 2006-19-09 AS IN AD AS IN AD EMERGENCY LANDING CONDITIONS WHEN HIGH INERTIAL LOADINGS OCCUR DGCA/B 300/26 TO DETECT AND CORRECT IMPROPERLY ASSEMBLED OR FAA AD 2007-12-06 SUPERCEDED AS IN AD AS IN AD DAMAGED FLIGHT CONTROLS FAA AD 2006-23-02 DGCA/B 300/27R1 TO PREVENT COLLAPSED PNEUMATIC SUPPLY TUBES WHICH FAA AD 2010 - 26 -03 AS IN AD AS IN AD COULD RESULT IN FAILURE OF THE TAIL DEICE BOOTS TO OPERATE DGCA/B 300/28 TO DETECT & CORRECT THE INSTALLATION OF AN INCORRECT FAA AD 2010-05-10 AS IN AD AS IN AD BUS BAR,WHICH COULD RESULT IN FAILURE OF THE PITOT HEAT ANNUNCIATORS TO ILLUMINATE DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/B 300/29 ATA 91 - CHARTS FAA AD 2011-15-05 AS IN AD AS IN AD