DGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY DGCA/BOEING 767/01 EMERGENCY EVACUATION SLIDES FAA AD AS IN THE AD AS IN THE AD
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1 DGCA/BOEING 767/01 EMERGENCY EVACUATION SLIDES FAA AD DGCA/BOEING 767/02 PNEUMATIC SYSTEM CHECK VALVE INSPECTION FAA AD DGCA/BOEING 767/03 FLAPS CARRIAGE SPINDLES FAA AD DGCA/BOEING 767/04 OIL FILTER PRESSURE SWITCH FAA AD DGCA/BOEING 767/05 LEADING EDGE SLATS FAA AD DGCA/BOEING 767/06 ENTRY/SERVICE DOOR FAA AD DGCA/BOEING 767/07 POWER FEEDER CONNECTORS FAA AD DGCA/BOEING 767/08 TRAILING EDGE WEDGES OF THE LEADING EDGE SLATS FAA AD DGCA/BOEING 767/09 SLAT CONTROL AND RIGGING FAA AD DGCA/BOEING 767/10 MAIN LANDING GEAR FAA AD DGCA/BOEING 767/11 CROSSOVER PNEUMATIC DUCT FAA AD DGCA/BOEING 767/110 TO PREVENT AN UNDETECTED FAILURE OF THE PRIMARY LOAD PATH FOR THE BALLSCREW IN THE DRIVE MECHANISM OF THE HORIZONTAL STABLIZER AND SUBSEQUENT WEAR AND FAILURE OF THE SECONDARY LOAD PATH FAA AD DGCA/BOEING 767/12 FUEL BOOST PUMP ASSEMBLIES FAA AD DGCA/BOEING 767/13 THRUST REVERSER SYSTEM (P & W 4000 SERIES ENGINES) FAA AD DGCA/BOEING 767/14 THRUST REVERSER SYSTEM ( P & W JT9D-7R4 OR GE CF6-80A ENGINES) FAA AD DGCA/BOEING 767/15 MAIN LANDING GEAR BRAKES FAA AD DGCA/BOEING 767/16 THRUST REVERSER SYSTEM (ROLLS ROYCE RB ENGINE) FAA AD DGCA/BOEING 767/17 MAIN LANDING GEAR AFT TRUNNION FAA AD DGCA/BOEING 767/18 MAIN LANDING GEAR AFT TRUNNION FAA AD DGCA/BOEING 767/19 RAM AIR TURBINE (RAT) FAA AD DGCA/BOEING 767/20 LEADING EDGE SLATS OR FIXED LEADING EDGE OF THE WING FAA AD DGCA/BOEING 767/21 AUXILIARY POWER UNIT BATTERY GROUNDS FAA AD DGCA/BOEING 767/22 ELECTRICAL WIRING BUNDLES FAA AD DGCA/BOEING 767/23 FORWARD TRUNNION ASSEMBLY FAA AD
2 DGCA/BOEING 767/24 FORWARD TRUNNION JOINT OF THE MAIN LANDING GEAR FAA AD DGCA/BOEING 767/25 MAIN LANDING GEAR BEAM FAA AD DGCA/BOEING 767/26 WING REAR SPAR FAA AD DGCA/BOEING 767/27 THRUST CONTROL CABLE FAA AD DGCA/BOEING 767/28 FORWARD ENGINE MOUNT THRUST LINKAGE FAA AD DGCA/BOEING 767/29 DIAGONAL BRACE OF THE NACELLE STRUT FAA AD DGCA/BOEING 767/30 THRUST REVERSER SYSTEM (CF6-80C2 ENGINE) FAA AD DGCA/BOEING 767/31 TENSION BOLTS ON STRUT FAA AD DGCA/BOEING 767/32 FUEL TANK BOOST PUMPS FAA AD DGCA/BOEING 767/33 DOOR LATCHES FAA AD R1 DGCA/BOEING 767/34 AUXILIARY TRACK ASSEMBLY FAA AD DGCA/BOEING 767/35 WING FRONT SPAR FAA AD DGCA/BOEING 767/36 CABLE ASSEMBLY FAA AD DGCA/BOEING 767/37 BELLCRANK ASSEMBLIES FAA AD DGCA/BOEING 767/38 THRUST REVERSERS FAA AD DGCA/BOEING 767/39 PRIMARY STRUT STRUCTURE (POWERED BY ROLLS ROYCE RB 211) FAA AD DGCA/BOEING 767/40 ENVIRONMENTAL CONTROL SYSTEM (ECS) FAA AD DGCA/BOEING 767/41 NACELLE STRUT AND WING STRUCTURE FAA AD DGCA/BOEING 767/42 ELEVATOR POWER CONTROL SYSTEM FAA AD DGCA/BOEING 767/43 PRIMARY STRUT STRUCTURE (POWERED BY GE ENGINES) FAA AD DGCA/BOEING 767/44 PRIMARY STRUT STRUCTURE FAA AD DGCA/BOEING 767/45 PASSENGER OXYGEN SYSTEM FAA AD DGCA/BOEING 767/46 HYDRAULIC SHUTOFF VALVES FAA AD DGCA/BOEING 767/47 WARNING ELECTRONIC UNIT OR MODULAR AVIONIC WARNING ELECTRONIC ASSEMBLY FAA AD DGCA/BOEING 767/48 DRAIN TUBE ASSEMBLIES OF THE SLAT TRACK HOUSING OF THE FAA AD
3 WINGS DGCA/BOEING 767/49 AIRPLANE FLIGHT MANUALS--CENTER TANK FU FAA AD DGCA/BOEING 767/50 THRUST REVERSER CONTROL SYSTEM FAA AD DGCA/BOEING 767/51 WIRE BUNDLES BETWEEN THE P50 PANEL AND THE NOSE WHEEL WELL STRUCTURE FAA AD DGCA/BOEING 767/52 AFT TRUNNION OF OUTER CYLINDER OF MAIN LANDING GEAR FAA AD DGCA/BOEING 767/53 TRIPOD STRUT ASSEMBLY FAA AD DGCA/BOEING 767/54 RIGHT MAIN LANDING GEAR AND AUTO-SPEEDBRAKE CONTROL SYSTEM FAA AD DGCA/BOEING 767/55 RIVETS IN SIDE PANELS OF THE NOSE WHEEL WELL FAA AD DGCA/BOEING 767/56 MIDSPAR FUSE PINS FAA AD DGCA/BOEING 767/57 BOLTS OF SUPPORT BEAM OF HINGE FITTING ASSEMBLIES FAA AD DGCA/BOEING 767/58 BARREL NUTS THAT ATTACH VERTICAL FIN TO BODY SECTION 48 FAA AD DGCA/BOEING 767/59 INBOARD AND OUTBOARD SUPPORT OF THE INBOARD MAIN FLAP FAA AD DGCA/BOEING 767/60 INBOARD AFT FLAP FAA AD DGCA/BOEING 767/61 AFT PRESSURE BULKHEAD-TO-FLOOR INSULATION BLANKETS FAA AD DGCA/BOEING 767/62 INBOARD TRAILING EDGE FLAPS FAA AD DGCA/BOEING 767/63 DRAINAGE SYSTEM OF CANTED PRESSURE DECK LOCATED IN WHEEL WELLS OF MAIN LANDING GEAR (MLG) OF LEFT AND RIGHT WINGS DGCA/BOEING 767/64(R1) FAA AD SHOULDER RESTRAINT HARNESS FAA AD DGCA/BOEING 767/65 AFT PRESSURE BULKHEAD WEB FAA AD DGCA/BOEING 767/66 OUTER CYLINDER OF MAIN LANDING GEAR (MLG) FAA AD DGCA/BOEING 767/67 AIR DATA COMPUTER (ADC) SYSTEM FAA AD DGCA/BOEING 767/68 AFT PRESSURE BULKHEAD - OIL CAN FAA AD DGCA/BOEING 767/69 OFF-WING ESCAPE SLIDES FAA AD
4 DGCA/BOEING 767/70 HANGER ARM OF THE HYDRAULIC PUMP OF THE RAT FAA AD DGCA/BOEING 767/71 NACELLE STRUT AND WING STRUCTURE FAA AD DGCA/BOEING 767/72 REAR SPAR BULKHEAD FAA AD R1 DGCA/BOEING 767/73 WIRE BUNDLES FAA AD DGCA/BOEING 767/74 WASTE TANK CRADLE FAA AD DGCA/BOEING 767/75 DIAGONAL BRACE FUSE PINS OF WINGS FAA AD DGCA/BOEING 767/76 AUXILIARY POWER UNIT (APU) FAA AD DGCA/BOEING 767/77 LEFT AND RIGHT BUTT LINE (BL) 25 VERTICAL CHORDS FOR CRACKS FAA AD DGCA/BOEING 767/78 AFT TRUNNION AREA FAA AD DGCA/BOEING 767/79 AFT PRESSURE BULKHEAD FAA AD DGCA/BOEING 767/80 INBOARD FAIRING SEAL FAA AD DGCA/BOEING 767/81 IN FLIGHT ENTERTAINMENT COOLING CARD FAA AD DGCA/BOEING 767/82 HORIZONTAL STABILIZER PIVOT BULKHEAD FAA AD DGCA/BOEING 767/83 FORWARD CARGO COMPARTMENT FAA AD DGCA/BOEING 767/84 DOOR-MOUNTED ESCAPE SLIDE/RAFTS FAA AD DGCA/BOEING 767/85 FUEL SPAR SHUTOFF VALVE FAA AD DGCA/BOEING 767/86 DRIP SHIELDS FAA AD DGCA/BOEING 767/87 HORIZONTAL TANGS OF THE MIDSPAR FITTING OF THE STRUT FAA AD DGCA/BOEING 767/88 CENTER OVERHEAD STOWAGE BIN MODULES FAA AD DGCA/BOEING 767/89 OUTBOARD OVERHEAD STOWAGE BINS FAA AD DGCA/BOEING 767/90 FREQUENCY CONVERTERS FAA AD DGCA/BOEING 767/91 OFF-WING EMERGENCY ESCAPE SLIDE FAA AD DGCA/BOEING 767/92 AILERON CONTROL OVERRIDE QUADRANT FAA AD DGCA/BOEING 767/93 MAIN LANDING GEAR (MLG) BOGIE BEAM PIVOT PINS FAA AD DGCA/BOEING 767/94 ENGINE FUEL FEED TUBE FITTING AND THE FRONT SPAR FAA AD DGCA/BOEING 767/95 BULKHEAD OUTER CHORD AT STATION (STA) FAA AD
5 DGCA/BOEING 767/96 INBOARD AND OUTBOARD FLAPS OF THE TRAILING EDGE FAA AD DGCA/BOEING 767/97 STOWAGE BINS FAA AD DGCA/BOEING 767/98 TO PREVENT EXCESSIVE VIBRATION OF AIRFRAME IN FLIGHT RESULTING IN LOSS OF CONTROL OF AIRPLANE DGCA/BOEING 767/99 TO PREVENT FAILURE OF THE SAFETY FITTINGS FOR THE CARGO FIRE EXTINGUISHING BOTTLES DUE TO CORROSION DGCA/BOEING767/100 TO DETECT AND CORRECT CRACKING IN THE BULKHEAD STRUCTURE AT STA DGCA/BOEING767/101 TO PREVENT POSSIBLE MIGRATION OF FLAME FROM A MAIN TANK FUEL BOOST PUMP INLET TO THE VAPOUR SPACE OF THE FUEL TANK DGCA/BOEING767/102 TO DETECT AND CORRECT DAMAGE TO WIRES IN THE FORWARD AND AFT LOWER LOBE CARGO COMPARTMENT DGCA/BOEING767/103 TO PREVENT INSUFFICIENT ELECTRICAL BONDING WHICH COULD RESULT IN A POTENTIAL OF IGNITION SOURCES INSIDE THE FUEL TANKS DGCA/BOEING767/104 TO DETECT AND CORRECT CORROSION OF THE OUT TANK WIRE HARNESS DGCA/BOEING767/105 TO ENSURE THERE IS SUFFICIENT FIRE SUPPRESSANT TO CONTROL A CARGO FIRE DGCA/BOEING767/106 SS AD FAA AD FAA AD FAA FAA AD FAA AD FAA AD FAA AD FAA AD DGCA/BOEING767/107 TO PREVENT FAILURE OF AN EVACUATION SYSTEM FAA AD DGCA/BOEING767/108 TO PREVENT A POTENTIAL ELECTRICAL ARC FROM IGNITING THE BMS 8-39 POLYURETHANE FOAM INSULATION ON THE DUCT ASSEMBLIES OR THE ECS FAA AD DGCA/BOEING767/109 TO ENSURE THAT CERTAIN LIGHTED PUSHBUTTON SWITCHES I FAA AD THE FLIGHT COMPARTMENT DO NOT MALFUNCTION AND CAUSE THE FLIGHT CREW TO BE UNABLE TO CONTROL CRITICAL AIRPLANE SYSTEMS AND CONTINUE SAFE OPERATIONS DGCA/BOEING767/110 TO PREVENT THE DEPLETION OF THE MAIN BATTERY WHILE IN FAA AD
6 FLIGHT DGCA/BOEING767/111 TO PREVENT UNDETECTED FAILURE OF THE PRIMARY LOAD PATH FOR THE BALLSCREW IN THE DRIVE MECHANISM OF THE HORIZONTAL STABLIZER AND SUBSEQUENT WEAR AND FAILURE OF THE SECONDARY LOAD PATH DGCA/BOEING767/112 TO PREVENT A FIRE NEAR A COMPOSITE DRAIN MAST AND POSSIBLE DISRUPTION OF ELECTRICAL POWER SYSTEM CAUSED BY A LIGHTNING STRIKE ON A COMPOSITE DRAIN MAST DGCA/BOEING767/113 TO PREVENT THE POTENTIAL FOR IGNITION SOURCES INSIDE FUEL TANKS CAUSED BY LATENT FAILURES, ALTERATIONS, REPAIRS, OR MAINTENANCE ACTIONS DGCA/BOEING767/114 TO PREVENT THE IN LINE FLOW INDICATORS OF THE PASSENGER OXYGEN MASKS FROM FRACTURING & SEPARATING DGCA/BOEING767/115 TO DETECT AND CORRECT FATIGUE CRACKING OF THE HIDDEN FUSELAGE SKIN AND CRACKING DGCA/BOEING767/116 TO DETECT AND CORRECT CRACKING IN THE AFT PRESSURE BULKHEAD WEB DGCA/BOEING767/117 TO DETECT AND CORRECT CRACKS IN THE AFT PRESSURE BULKHEAD WEB. DGCA/BOEING767/118 AIR TRANSPORT ASSOCIATION CHAPTER 25: EQUIPMENT FURNISHINGS FAA AD FAA AD FAA AD FAA AD FAA AD FAA AD FAA AD FAA AD DGCA/BOEING767/119 AIR TRANSPORT ASSOCIATION CHAPTER 53: FUSELAGE FAA AD
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