INDEX OF BULLDOG SERVICE BULLETINS APPLICABLE TO ALL SERIES AND MODELS
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1 INDEX OF BULLDOG SERVICE BULLETINS APPLICABLE TO ALL SERIES AND MODELS SB No. Effectivity Issue/Revision Dated Description/Title Compliance/Comments BDG/100/00 ALL Rev. 5 01/12/2011 INDEX OF SERVICE BULLETINS AND SERVICE LETTERS Annex A ALL Rev. 5 01/12/2011 All Series and Models Annex B Annex C Annex D Annex E Annex F Series 100 Model 101 Series 100 Model 102 Series 100 Model 103 Series 120 Model 121 Series 120 Model 124 Rev. 2 31/03/2007 Series 100, Model 101 Only Rev. 2 31/03/2007 Series 100, Model 102 Only Rev. 2 31/03/2007 Series 100, Model 103 Only Rev. 3 01/12/2010 Series 120, Model 121 Only Rev. 2 31/03/2007 Series 120, Model 124 Only Annex G ALL Rev. 4 01/12/2011 SERVICE LETTERS All Series and Models BDG/100/1 ALL Iss. 1 17/04/1972 BDG/100/3 ALL Iss. 2 15/08/1972 BDG/100/4 ALL Iss. 1 18/01/1973 BDG/100/5 ALL Iss. 1 05/02/1973 ENGINE CONTROL CABLE BALL END JOINTS DAMAGE NOTIFICATION OF DUNLOP SERVICE BULLETINS , 73-6, AND 79-1 FLAP VALVE ATTACHMENT (AIR CONDITIONING SYSTEM) ENGINE CONTROL CABLE ASSEMBLIES - INSPECTION WITHDRAWN. Embodiment of Mod. No. BH.56 renders compliance unnecessary. Accomplish by 30th September
2 BDG/100/6 ALL Iss. 1 26/03/1973 ENGINE - INTRODUCTION OF CHANGES TO IMPROVE INTAKE VALVE AND SEAT LIFE WITHDRAWN. Superseded by Service Bulletin BDG/100/15 BDG/100/7 ALL Iss. 1 21/05/1973 ENGINE CONTROLCABLE BALL END JOINTS - LUBRICATION WITHDRAWN. Embodiment of Mod. No. BH.56 renders compliance unnecessary BDG/100/8 ALL Iss. 1 21/10/1973 BDG/100/9 ALL Iss. 1 07/09/1973 BDG/100/10 ALL Iss. 1 11/09/1973 METHOD OF SETTING MAX ENGINE RPM ON PROPELLER GOVERNOR & FINE PITCH STOP ENGINE - IDLING SPEED AND MIXTURE ADJUSTMENT ENGINE - SHROUD TUBE RETAINING COMPONENTS by AL.8 BDG/100/11 ALL Iss. 1 11/09/1973 ENGINE - FUEL INJECTOR NOZZLE CLEANING BDG/100/12 ALL Iss. 1 10/09/1973 ENGINE - FACILITIES FOR CYLINDER REPAIR BDG/100/13 ALL Iss. 1 10/09/1973 BDG/100/15 ALL Iss. 1 26/09/1973 BDG/100/16 ALL Iss. 1 26/09/1973 BDG/100/17 ALL Iss. 1 01/10/1973 BDG/100/18 ALL Iss. 1 28/09/1973 BDG/100/19 ALL Iss. 1 08/10/1973 ENGINE - MANUFACTURER'S POLICY FOR PRO- RATED ENGINE REPLACEMENT ENGINE - INTRODUCTION OF ROTATOR TYPE INTAKE VALVES ENGINE - PARTS CATALOGUE AMENDMENT - CONNECTING ROD BOLT FUEL SYSTEM - DISCHARGE OF FUEL VIA TANK VENT OUTLET ENGINE - INTRODUCTION OF HARDENED OIL PUMP DRIVE IMPELLER ENGINE - ALTERNATOR MOUNTING BRACKET ASSEMBLY 2 WITHDRAWN. Superseded by Service Bulletin No. BDG/100/65 WITHDRAWN. Incorporated in ASM by AL.8
3 BDG/100/20 ALL Iss. 1 15/10/1973 BDG/100/21 ALL Iss. 2 30/01/1975 BDG/100/22 ALL Iss. 1 15/10/1973 BDG/100/23 ALL Iss. 1 15/10/1973 BDG/100/24 ALL Iss. 1 30/10/1973 ENGINE - INSPECTION AND REPAIR OF CRANKSHAFT AND GEAR ASSEMBLY ENGINE - REPLACEMENT OF MAGNETO DRIVE SHAFT BUSHING ENGINE - LYCOMING SERVICE INSTRUCTION No. 1124B - OIL CONSUMPTION LIMITS ENGINE - LYCOMING SERVICE LETTER No. L157B - FULL FLOW OIL FILTER MAIN LANDING GEAR SHOCK ABSORBER - CRACK TESTING OF SPHERICAL BEARINGS WITHDRAWN. Applicable on engine overhaul only. WITHDRAWN. See engine operator's handbook for max oil consumption limits WITHDRAWN. Not practical on Bulldog Aircraft BDG/100/25 Up to Con. No. 120/247 Iss. 1 26/03/1974 MAINPLANE ATTACHMENTS TO STUB ROOT WINGS - ATTACHMENT BOLTS LOOSE BDG/100/26 BDG/100/27 All except Models 101 & 121 MODELS 101 AND 104 Iss. 1 26/02/1974 Iss. 1 28/02/1974 BDG/100/28 ALL Iss. 3 08/01/1976 BDG/100/29 ALL Iss. 1 27/02/1974 BDG/100/30 ALL Iss. 1 21/03/1974 BDG/100/31 ALL Iss. 1 19/03/1974 BDG/100/32 ALL Iss. 1 02/04/1974 PILOT'S & CO-PILOT'S SEAT - LOCATING PLUNGERS NOT ENGAGING SIMULTANEOUSLY PILOT'S & CO-PILOT'S SEAT - BACK LOCATING PLUNGERS NOT ENGAGING SATISFACTORILY CANOPY JETTISON CABLE ASSEMBLY - FRACTURING AT FORWARD SWAGED END OPERATION OF ALTERNATOR FIELD SWITCH - PREVENTION OF DAMAGE TO ALTERNATOR AND VOLTAGE REGULATOR HARTZELL PROPELLER HUBS - EXCESSIVE GREASE LEAKAGE CONTROL COLUMN AND TORQUE TUBES - LOOSE ATTACHMENT BOLTS ENGINE AND PROPELLER CONTROL CABLES - INSPECTION AND LUBRICATION OF SWIVEL BALL ASSEMBLIES 3. Embodiment of Mod. No. BH.101 renders compliance unnecessary. Embodiment of Mod. No. BH.72 renders compliance unnecessary. Embodiment of Mod. No. BH.76 renders compliance unnecessary WITHDRAWN. Information incorporated in Maintenance Schedule by AL.1
4 BDG/100/33 ALL Iss. 1 05/04/1974 BDG/100/34 BDG/100/35 BDG/100/36 All up to Con. No BH120/420 ALL EXCEPT MODEL 101 All from Con. No. BH120/248 Iss. 3 25/11/1975 Iss. 1 26/03/1974 Iss. 1 09/04/1974 PORT CONTROL COLUMN TORQUE TUBE - FOULING OF FUEL PIPE RUDDER TORQUE TUBE SPLIT BEARINGS - SECURING BOLTS TORQUE LOADING STALL WARNING HORN DIAPHRAGM - LOSS OF ADJUSTMENT MAINPLANE ATTACHMENTS TO STUB ROOT WINGS - ATTACHMENT BOLTS - INSPECTION BDG/100/37 ALL Iss. 1 03/05/1974 FLAP ACTUATOR JACK SCREW - LUBRICATION. Embodiment of Mod. No. BH.145 renders compliance unnecessary BDG/100/38 ALL Iss. 1 17/05/1974 HARTZELL PROPELLER - PERMISSIBLE BLADE TIP PLAY BDG/100/39 ALL Iss. 1 27/05/1974 FUEL TANKS - INTERNAL INSPECTION BDG/100/40 ALL Iss. 3 23/02/1977 BDG/100/41 ALL Iss. 1 01/10/1974 BDG/100/42 ALL Iss. 1 24/10/1974 BDG/100/43 ALL Iss. 1 24/10/1974 BDG/100/44 ALL Iss. 1 24/10/1974 BRAKE MASTER CYLINDERS - TRAP VALVE SEAL MALFORMED FUEL TANK VENT PIPES - CHAFED DUE TO DISPLACEMENT OF GROMMETS BULLETIN No. 373 BULLETIN No. 367F - INSPECTION OF ENGINE PISTON PINS INSTRUCTION No. 1098B - PROPELLER FLANGE BUSHING LOCATIONS WITHDRAWN. Superseded by Issue 2 of Service Bulletin No. BDG/100/21 4
5 BDG/100/45 ALL Iss. 1 25/10/1974 BDG/100/46 ALL Iss. 1 31/10/1974 BDG/100/47 ALL Iss. 1 31/10/1974 BDG/100/48 ALL Iss. 1 04/11/1974 BDG/100/49 ALL Iss. 1 08/11/1974 INSTRUCTION No IDENTIFICATION OF PRIMER & FUEL INJECTOR LINES BULLETIN No ENGINE INSPECTION AFTER OVERSPEED BULLETIN No ENGINE FUEL PUMP INSPECTION ENGINE MOUNTING - INSPECTION FOR CHAFING BY C.S.U. CONTROL CABLE INSPECTION OF C.S.U. CONTROL CABLE SUPPORT BRACKET WITHDRAWN. Superseded by Service Bulletin No. BDG/100/72, Issue 2.. Embodiment of Mod. No. BH.69 renders further compliance unnecessary.. Embodiment of Mod. No. BH.121 renders further compliance unnecessary. BDG/100/50 SERIES 120 AIRCRAFT ONLY Iss. 1 21/11/1974 ELEVATOR TRIM TAB CONTROL CABLE ASSEMBLY - FOULING STRUCTURE BDG/100/51 ALL Iss. 1 20/11/1974 BDG/100/52 ALL Iss. 1 02/12/1974 BDG/100/53 ALL Iss. 1 10/12/1974 BDG/100/54 ALL Iss. 1 31/01/1975 BDG/100/55 ALL Iss. 1 05/02/1975 ENGINE MIXTURE CONTROL QUADRANT - MARKING FOR BEST POWER MIXTURE SETTING NOTIFICATION OF GOODYEAR LEAFLET No. E/BULLDOG/1 - INTERCHANGEABILITY OF NOSEWHEEL BEARING RUDDER TORQUE TUBE SPLIT BEARINGS - NON-CONFORMANCE WITH SPECIFICATION ENGINE STARTER MOTOR TERMINAL POST CONNECTION - CRACKING OF FIELD LINK ENGINE STARTER MOTOR PINION HOUSING - FAILURE OF ATTACHMENT LUG by AL.8 by AL.8 5
6 BDG/100/56 ALL Iss. 1 11/02/1975 BDG/100/57 ALL Iss. 1 01/03/1977 BDG/100/58 BDG/100/59 Up to Con. No. BH120/393 MODELS 102, 103 AND 123 Iss. 1 14/03/1975 Iss. 1 23/04/1975 BDG/100/60 ALL Iss. 1 08/04/1975 BDG/100/61 ALL Iss. 1 19/03/1975 BDG/100/62 ALL Iss. 2 24/10/1975 ENGINE STARTER RING GEAR - INCORRECT POSITIONING LIST OF ACTIVE SERVICE BULLETINS FOR BULLDOG SERIES 100 & 120 AIRCRAFT FUEL TANK CONTENTS TRANSMITTERS - PUNCTURED FLOATS FUEL COCK CONTROL - CHAFING BY RUDDER CONTROL CABLE DETERIORATION OF OIL SEPERATOR TO ENGINE SUMP HOSE NOSE UNDERCARRIAGE SHOCK ABSORBER - SCORING OF BORE BY PISTON LOCKING PIN CHAFING OF HYDRAULIC PIPE FROM STARBOARD BRAKE MASTER CYLINDER WITHDRAWN. Superseded by this Service Bulletin Index. Embodiment of Mod. No. BH.148 renders further compliance unnecessary.. Embodiment of Mod. No. BH.104 renders further compliance unnecessary.. WITHDRAWN AFTER 400 FLYING HOURS WITHDRAWN. Superseded by Service Bulletin No. BDG/100/085 BDG/100/63 ALL Iss. 1 24/04/1975 BDG/100/64 ALL Iss. 1 05/05/1975 BDG/100/65 ALL Iss. 1 07/05/1975 BDG/100/66 ALL Iss. 1 30/06/1975 BDG/100/67 ALL Iss. 1 14/11/1975 BDG/100/68 Up to Con. No. BH120/391 MAGNETO SWITCH CABLE - BREAKING AT MAGNETO TERMINATION BULLETIN No. 382 AND BENDIX SERVICE BULLETIN No. RS43 BULLETIN No OIL PUMP IMPELLER AND DRIVE REPLACEMENT BENDIX FUEL INJECTOR - POSSIBLE INADVERTENT INTERCHANGE OF WASHERS AT MIXTURE AND IDLE VALVES EXCESSIVE RELATIVE MOVEMENT BETWEEN CONTROL COLUMNS Iss. 1 13/11/1975 CHAFING OF FRONT CENTRE ENGINE BAFFLE. Embodiment of Mod. No. BH.109 renders further compliance unnecessary... Embodiment of Mod. No. BH.130 renders further compliance unnecessary. 6
7 BDG/100/69 BDG/100/70 BDG/100/71 ALL EXCEPT MODEL 101 ALL WITH VARLEY BATTERY 24.19/25C Con.Nos. up to & incl. BH.120/420 Iss. 1 17/11/1975 Iss. 2 20/08/1976 Iss. 1 11/12/1975 BDG/100/72 ALL Iss. 2 04/11/1976 BATTERY TRAY STRUCTURE - RIVETS MISSING VARLEY BATTERY - CRACKING OF VENT STOPPERS ELEVATOR CONTROL CABLE, LOWER AFT - CHAFING PROCEDURES TO BE CARRIED OUT FOLLOWING REPORTED ENGINE OVERSPEED. Embodiment of Mod. No. BH.132 renders further compliance unnecessary. BDG/100/74 ALL Iss. 1 15/03/1976 INSTRUCTION No BENDIX MAGNETOS - REPLACEMENT OF SLICK IGNITION LEADS BDG/100/75 BDG/100/76 BDG/100/77 BDG/100/78 BDG/100/79 BDG/100/80 MODELS 124 & 126 ONLY SERIES 100 ONLY Con.Nos. up to & incl. BH.120/391 Con.Nos. up to & incl. BH.120/391 Con.Nos. up to & incl. BH.120/391 MODELS 124, 125 & 126 ONLY Iss. 1 24/05/1976 BENDIX RADIO TRANSCEIVER TYPE RT.241B Iss. 1 25/06/1976 REPLACEMENT OF THROTTLE CABLES Iss. 1 29/12/1976 ELEVATOR TRIM TAB HINGE PIN MISSING Iss. 1 29/12/1976 PITOT STATIC PIPES CHAFING Iss. 1 29/12/1976 Iss. 1 03/02/1977 FUEL PIPE - FUEL COMPARTMENT TO FRONT BULKHEAD - CHAFING BULLETIN No AEROBATIC ENGINE LUBRICATION REQUIREMENTS. Embodiment of Mod. No. BH.141 renders further compliance unnecessary. BDG/100/81 ALL Iss. 1 23/02/1977 PROPELLER - INTRODUCTION OF REVISED FINE PITCH STOP WITH INCREASED DIAMETER 7. Embodiment of Mod. No. BH.140 renders further compliance unnecessary.
8 BDG/100/83 ALL Iss. 1 14/03/1977 BDG/100/84 ALL Iss. 1 14/03/1977 BDG/100/85 ALL Iss. 1 14/03/1977 BDG/100/86 ALL Iss. 1 30/03/1977 BDG/100/87 BDG/100/88 ALL BUT MODELS 124/125/126 Con.Nos. up to & incl. BH.120/391 Iss. 1 17/03/1977 Iss. 1 10/05/1977 BDG/100/89 ALL Iss. 2 20/02/1978 BDG/100/90 ALL Iss. 1 25/10/1977 BDG/100/91 Con.Nos. up to & incl. BH.120/405 Iss. 1 05/05/1978 BDG/100/92 ALL Rev. 1 26/02/2002 BDG/100/93 ALL Iss. 1 02/11/1978 RIGID BRAKE PIPES ON RADIUS ARMS - CHAFING IN P-CLIPS C.S.U. CONTROL CABLE - CHAFING ON FAIRLEAD PIPELINE FROM STBD BRAKE MASTER CYLINDER - CHAFING BY AIR AND FUEL HOSES NOSE LEG STEERING RETAINING PLATE - CRACKING OIL SEPARATOR TANK ASSEMBLY - INTERCHANGEABILITY OF SPARE PARTS - REVISION FIREWALL REINFORCING CHANNELS - CRACKING NOTIFICATION OF HARTZELL SERVICE BULLETIN Nos. 118A AND 118B PROPELLER GOVERNOR - NOTIFICATION OF WOODWARD SERVICE BULLETINS Nos B AND CABIN LOWER FORWARD TRIM PANELS - DISTORTION FUSELAGE/MAINPLANE, LOWER JOINT PLATE ASSEMBLIES - CRACKING BENDIX MAGNETOS - INSPECTION OF IMPULSE COUPLINGS AND STOP PINS. Embodiment of Mod. No. BH.146 renders further compliance unnecessary.. Embodiment of Mod. No. BH.146 renders further compliance unnecessary. OPTIONAL. Embodiment of Mod. No. BH.120 renders compliance unnecessary. BDG/100/94 ALL Iss. 1 16/11/1978 AIR CONDITIONING DUCT - REINFORCEMENT BDG/100/95 ALL Iss. 1 17/1178 BRAKE MASTER CYLINDER MOUNTING BRACKET ON FIREWALL - CRACKING 8
9 BDG/100/96 ALL Iss. 2 14/06/1979 BDG/100/97 ALL Iss. 1 19/08/1981 BDG/100/98 ALL Iss. 1 19/08/1981 BDG/100/99 ALL Iss. 1 19/08/1981 BDG/100/100 ALL Iss. 1 08/02/1980 BDG/100/102 ALL Iss. 1 11/08/1980 BDG/100/103 ALL Rev 1 10/12/1982 BDG/100/104 ALL Rev. 0 19/08/1981 BDG/100/105 BDG/100/106 ALL EXCEPT MODEL 101 MODEL 1210 ONLY Rev. 0 17/11/1980 Rev. 0 11/08/1980 BDG/100/109 ALL Rev. 0 28/09/1981 BDG/100/110 ALL Rev. 0 18/03/1982 BDG/100/111 ALL Rev. 1 01/03/1983 BULLETIN No BENDIX FUEL INJECTOR INSTRUCTION No.1012E LETTER No.L192A - SPARK PLUG FOULING NOTIFICATION OF BENDIX SERVICE INSTRUCTION No OVERHAUL PERIODS NOTIFICATION OF HARTZELL SERVICE LETTER No. 61F - OVERHAUL PERIODS LETTER No.L147B - USE OF ANDEROL 471 MAIN SPAR CENTRE SECTION - MAIN LANDING GEAR ATTACHMENT LUGS - INSPECTION NOTIFICATION OF BENDIX SERVICE INSTRUCTION No MAGNETOS - INSPECTION OF CAM RETAINING SCREWS REDUCTION IN COMMUNICATION NOISE - NEW HEADSET AVAILABILITY OUTBOARD FUEL TANKS - WATER/SEDIMENT CHECKS - FREQUENCY NOTIFICATION OF BENDIX SERVICE BULLETIN No.458 INSTRUCTION No BENDIX RSA FUEL INJECTORS INSTRUCTION No ENGINE OVERHAUL PERIODS 9 WITHDRAWN. Superseded by SB BDG/100/119.
10 BDG/100/112 ALL Rev. 0 18/03/1982 BDG/100/115 ALL Rev. 0 27/04/1982 BDG/100/116 ALL Rev. 0 27/04/1982 BDG/100/117 ALL Rev. 0 28/06/1982 BDG/100/119 ALL Rev. 0 10/08/1982 BDG/100/120 ALL Rev. 0 10/08/1982 INSTRUCTION No.1274B - FUEL & OIL HOSES - REPLACEMENT INSTRUCTION No.1060D - PUSH ROD IDENTIFICATION INSTRUCTION No COMBUSTION CHAMBER CLEANING PROCEDURE BULLETIN No.240K - REPLACEMENT OF ENGINE PARTS NOTIFICATION OF BENDIX SERVICE BULLETIN No MAGNETOS - LOOSE DISTRIBUTOR BLOCK BUSHING INSTRUCTION No.1037J - OVERHAULS BDG/100/121A ALL Rev. 0 13/10/1982 BDG/100/122 ALL Rev. 0 01/03/1983 NOTIFICATION OF BENDIX SERVICE BULLETIN No.623 AND FAA AD No INSTRUCTION No OIL COOLER BYPASS VALVES BDG/100/123 ALL Rev. 0 13/06/1983 ENGINE MOUNT CRACKING BDG/100/124 ALL Rev. 0 05/10/1983 BDG/100/125 ALL Rev. 0 05/10/1983 BDG/100/126 ALL Rev. 0 05/10/1983 BDG/100/127 ALL Rev. 0 29/03/1984 NOTIFICATION OF HARTZELL SERVICE LETTER No. 5 - TACHOMETER READING ERRORS INSTRUCTION No FUEL PUMP DRIVE SPLINES LETTER No. L161C - OVERHAUL MANUAL REVISION POLICY FUSELAGE - CRACKING OF ANGLE AND DIAPHRAGM AT TAILPLANE SPAR ATTACHMENTS. 10
11 BDG/100/128 ALL Rev. 0 23/01/1984 BDG/100/129 ALL Rev. 0 23/01/1984 BDG/100/131 ALL Rev. 0 08/06/1987 BDG/100/141 ALL Rev. 0 05/12/1984 BDG/100/143 ALL Iss. 2 02/05/2007 BDG/100/144 ALL Rev. 0 12/09/1985 BDG/100/145 ALL Rev. 0 19/12/1992 BDG/100/153 ALL Rev. 0 23/04/1987 BDG/100/156 ALL Rev. 3 10/12/1996 BDG/100/157 ALL Rev. 2 22/01/1993 BDG/100/158 ALL Rev. 0 22/01/1991 BDG/100/159 ALL Rev. 0 20/05/1991 BDG/100/160 ALL Rev. 0 30/07/1991 INSTRUCTION No VALVE STICKING INSTRUCTION No ENGINE TEST AFTER OVERHAUL FUSELAGE - CRACKS, BUCKLING AND LOOSE BOLTS IN FRAME 82 ASSEMBLY LETTERNo.L205 - STUCK EXHAUST VALVES FLYING CONTROLS - PILOT'S RUDDER TORQUE TUBES - FAILURE AT LEVER HUB WELD NOTIFICATION OF GATES VARLEY SERVICE BULLETIN No. 2/85 - BATTERY CHECKS ENGINE CONTROLS - INSPECTION & REWORK OF CONTROL CABLES FLYING CONTROLS - CONTROL ROD END FITTINGS - SECURITY OF ATTACHMENT FLYING CONTROLS - INSPECTION OF HANDGRIP FITTINGS ON CONTROL COLUMN HARTZELL PROPELLERS - CRACKING OF FRONT HALF OF PROPELER HUB ASSEMBLY FUSELAGE - INSPECTION OF THE REAR FUSELAGE ASSEMBLY FOR BATTERY ACID SPILLAGE AND RESULTANT CORROSION NOTIFICATION OF TEXTRON LYCOMING SB No. 369H - ENGINE INSPECTION AFTER OVERSPEED OR OVER BOOST NOTIFICATION OF TEXTRON LYCOMING SB No POWERPLANT - FRACTURE OF GOVERNOR OIL CONTROL PIPE ALERT HIGHLY 11
12 BDG/100/161 ALL Rev. 0 30/07/1991 BDG/100/162 ALL Rev. 1 10/12/1996 NOTIFICATION OF TEXTRON LYCOMING SB No. 475A - REVISED INSTRUCTIONS FOR OVERHAUL OF CRANKSHAFT GEAR FLYING CONTROLS - CORROSION OF ELEVATOR TORQUE TUBES BDG/100/164 ALL Rev. 1 16/11/1993 BDG/100/165 ALL Rev. 2 20/12/1996 BDG/100/166 ALL except Con No BH120/201 Rev. 1 01/12/2010 BDG/100/167 ALL Rev. 0 26/10/1995 BDG/100/168 ALL Rev. 0 06/11/1996 BDG/100/169 ALL Rev. 0 21/11/1996 BDG/100/170 ALL Rev. 0 20/12/1996 BDG/100/171 ALL Rev. 0 31/01/2006 BDG/100/172 ALL Rev. 0 25/07/2007 FUEL SYSTEM - TO PREVENT POSSIBLE DISRUPTION OF FUEL SUPPLY MAINPLANES - NOTIFICATION OF LIFE LIMITATION FOR MAIN SPAR JOINT WINGS - INTRODUCTION OF STRENGTHENING TO THE CENTRE SECTION OF THE MAIN SPAR LANDING GEAR - BRAKE SYSTEM - INSPECTION OF BRAKE TORQUE TUBE ASSEMBLIES POWERPLANT - TO INSPECT THE HIGH PRESSURE FUEL PUMP FOR POSSIBLE MANUFACTURING DEFECT POWERPLANT - TO INSPECT THE ENGINE FOR DEFECTIVE PISTON PINS NOTIFICATION OF FATIGUE LIFE LIMITATION OF AIRCRAFT INTRODUCTION OF CLEVELAND BRAKE SYSTEM - NOTIFICATION OF BULLDOG MODIFICATION No. BH/196 MAIN LANDING GEAR RADIUS ARM NDT INSPECTION i.a.w. FAA AD superseded by SB BDG/100/170 i.a.w. FAA AD BDG/100/173 ALL Rev. 0 31/08/2007 RUDDER CONTROLS INCORRECT ASSEMBLY BDG/100/174 ALL Rev. 0 01/09/2010 MAIN LANDING GEAR RADIUS ARMS - CORROSION 12
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