| AD Number: | AD Subject: | SB Reference: |
| 1-068 |
INDICATING AND RECORDING -STALL WARNING -INSTALLATION OF DATA CONCENTRATOR UNITS WITH SOFTWARE VERSION 3.4 |
SAAB 2000-31-001 |
| 1-069 |
FUEL SYSTEM -FUELING PANEL -REMOVAL OF LAMP BOARD IN FUELING PANEL |
SAAB 2000-28-003 |
| 1-071 |
ENGINE CONTROLS -CONTROL QUADRANT REPLACEMENT -NUT ON POWER LEVERS APPLIED WITH LOCTITE |
SAAB 2000-76-003 |
| 1-073 |
FIRE PROTECTION -FIRE DETECTION -INSTALLATION OF MODIFIED CONTROL UNITS |
SAAB 2000-26-002 |
| 1-076 |
HYDRAULIC POWER -INTEGRATED HYDRAULIC PACKAGE -IMPROVED AC -ELECTRICAL MOTOR |
SAAB 2000-29-004 |
| 1-077R2 |
FUSELAGE -WING REAR ACCESS DOOR -INSPECTION OF CHAFING ON HYDRAULIC TUBES AND ELECTRICAL HARNESSES |
SAAB 2000-53-010R1 |
| 1-080 |
FIRE PROTECTION -FIRE EXTINGUSHING -ENGINE -INSPECTION OF THE FIRE HANDLE SWITCHES |
SAAB 2000-26-006, |
| 1-082 |
APU -IGNITION EXCITER -DELETION OF MOD NO. 5365 AND IMPLEMENTATION OF MOD NO. 5692 |
SAAB 2000-49-005 |
| 1-084 |
ICE AND RAIN PROTECTION -AIRFOIL DE-ICING SYSTEM -DRAIN HOLE STABILIZER |
SAAB 2000-30-006 |
| 1-085R1 |
LANDING GEAR -ANTI-SKID SYSTEM -IMPROVED HUBCAP DRIVE COUPLING |
SAAB 2000-32-019 |
| 1-087 |
EQUIPMENT/FURNISHING -REPLACEMENT OF THERMAL INSULATION |
SAAB 2000-25-016 |
| 1-088R1 |
STABILIZERS -RUDDER -INSPECTION OF LOWER RIB |
SAAB 2000-55-005 |
| 1-090 |
NACELLES -NACELLE FIREZONE SEALING |
SAAB 2000-54-008 |
| 1-091 |
OXYGEN SYSTEM -PASSENGER OXYGEN -DROPOUT BOXES INSPECTION |
SAAB 2000-35-001 |
| 1-092 |
WINGS -ACCESS COVERS INSPECTION/REWORK OF FUEL TANK ACCESS DOORS |
SAAB 2000-57-009 |
| 1-093R6 | AIRWORTHINESS DIRECTIVES FOR ENGINES, PROPELLERS AND OTHER VENDOR EQUIPMENT | NO BULLETIN |
| 1-095 |
FLIGHT CONTROL -RUDDER DISCONNECT SYSTEM -INSPECTION OF THE DISCONNECT UNIT |
SAAB 2000-A27-020 |
| 1-096R1 |
FLIGHT CONTROL -RUDDER DISCONNECT SYSTEM -REPLACEMENT OF THE DISCONNECT UNIT |
SAAB 2000-27-021R1 |
| 1-098 |
LIGHTS -CEILING/WINDOW AND LAVATORY LIGHTS -INSPECTION, REWORK AND REPLACEMENT OF THE FLUORECENT LIGHT LAMP HOLDERS |
SAAB 2000-33-009 |
| 1-099 |
FIRE PROTECTION -FIRE EXTINGUSHING -INSPECTION OF TWO-WAY CHECK VALVE |
SAAB 2000-26-010 |
| 1-101 |
NAVIGATION -FLIGHT MANAGEMENT SYSTEM (FMS) -INSTALLATION OF A NEW FLIGHT MANAGEMENT COMPUTER (FMC-4100) |
SAAB 2000-34-027 |
| 1-102R1 |
WINGS -INSTALLATION OF STAKED BUSHINGS IN THE AILERON ACTUATION FITTINGS |
SAAB 2000-57-014R1 |
| 1-104 |
FLIGHT CONTROL SYSTEM -ELEVATOR CONTROL SYSTEM- POWERED ELEVATOR CONTROL UNIT LIGHTING PROTECTION INSPECTION |
SAAB 2000-27-030R1 |
| 1-105 |
REAR FUSELAGE -SEALING OF FIRE SHIELD IN THE APU AREA |
SAAB 2000-53-024 |
| 1-108 |
WINGS -REPLACEMENT OF THE MAIN LANDING GEAR TRUNNION FITTINGS |
SAAB 2000-57-010 |
| 1-109 |
COMMUNICATION -RADIO TUNING UNIT -INSTALLATION OF NEW IMPROVED RADIO TUNING UNITS |
SAAB 2000-23-017 |
| 1-111R1 |
FLIGHT CONTROLS -AILERON -INSPECTION OF AILERON WING CONTROL CABLES |
SAAB 2000-27-33 |
| 1-112R2 |
HYDRAULIC POWER -RH NACELLE -INSPECTION FOR CHAFING ON THE MLG EMERGENCY UPLOCK RELEASE HYDRAULIC PIPE |
SAAB 2000-29-007R2 |
| 1-114R1 |
CEILING AND LAVATORY LIGHTS -INSPECTION OF THE FLUORECENT LAMP INSTALLATION AND THE FLUORENT LAMP HOLDERS |
SAAB 2000-33-014 |
| 1-120 | ICE & RAIN PROTECTION-AIRFOIL DE-ICING -INTRODUCTION OF NEW IMPROVED CHECK VALVE | SAAB 2000-30-012 |
| 1-121 |
ICE & RAIN PROTECTION-PROP-DEICE HARNESS-INSPECTION ON CHAFING ON ELECTRICAL HARNESS AND HYDRAULIC PIPE |
SAAB 2000-30-014R01 |
| 1-122 |
FUSELAGE - REAR PRESSURE BULKHEAD - REINFORCEMENT ANGLE |
SAAB 2000-53-026 |
| 1-123 |
MAIN LANDING GEAR-SHOCK STRUT-INSTALLATION OF A NEW STRONGER OUTBOARD TRUNNION PIN |
SAAB 2000-32-042 |
| 1-124 |
EQUIPMENT FURNISHING-FLOOR HEATER-DISCONNECTION OF FLIGHT ATTENDANT FLOOR HEATER |
SAAB 2000-A25-080 |
| 1-126 |
HYDRAULIC POWER-EXPANSION CHAMBER ATTENUATOR-NEW END-PIECE FOR IHC AFT ECA |
SAAB 2000-29-016 |
| 1-129R1 |
ENGINE-PROPELLER GEARBOX-INSPECTION OF BORESCOPE PLUG ATTACHMENT NUT |
SAAB 2000-A72-001R1 |
| 1-131 |
ENGINE AND FUEL CONTROL-FADEC-DEFECTIVE EEPROM CHIPS |
AE2100A-73-25 |
| 1-132 |
AILERONS-INSTALLATION OF STAKED BUSHINGS IN THE AILERON TRIM TAB ACTUATOR FITTINGS |
SAAB 2000-57-011 |
| 1-140 |
LIGHTS-EMERGENCY LIGHTING-INSPECTION OF THE AFT EXTERIOR LIGHT |
SAAB 2000-33-016 |
| 1-142R1 |
WINGS-FWD AND REAR SPAR MODIFICATION TO IMPROVE FATIGUE LIFE |
SAAB 2000-57-029 |
| 1-147 |
NACELLE-PYLONS-ATTACH FITTINGS-INSPECTION OF THE BACKUP STRUTS IN THE LH AND RH NACELLE |
SAAB 2000-A54-022 |
| 1-157R1 |
WINGS-REAR SPAR MODIFICATION TO IMPROVE FATIGUE LIFE |
SAAB 2000-57-037 |
| 1-158 |
OIL-ACOC SELF-SEAL COUPLINGS-INSPECTION FOR CORRECT INSTALLATION AND ADDITION OF NEW CLAMP |
SAAB 2000-79-005 |
| 1-159 |
STABILIZERS-ELEVATORS-INSPECTION OF FASTENERS AND AREAS ADJACENT TO EMERGENCY PITCH TRIM ACTUATOR FITTING |
SAAB 2000-A55-009 |
| 1-162 |
FLIGHT CONTROLS-ELEVATOR CONTROL SYSTEM-INSPECTION OF THE EMERGENCY PITCH TRIM SYSTEM (EPTS) |
SAAB 2000-27-046 |
| 1-163 |
MAIN LANDING GEAR-EXTENSION AND RETRACTION-INSPECTION AND/OR REPLACEMENT OF THE RETRACT ACTUATOR RAMROD |
SAAB 2000-32-059 |
| 1-164 |
HYDRAULIC SYSTEM-NUMBER 2 SYSTEM-CHANGE OF DUAL SHUTTLE VALVE |
SAAB 2000-29-020 |
| 1-165 |
NACELLE/PYLONS-ATTACH FITTINGS-INSPECTION OF THE BACKUP STRUTS IN THE LH AND RH NACELLE |
SAAB 2000-54-024 and SAAB 2000-54-025 |
| 1-166 |
NAVIGATION-PITOT TUBE SYSTEM-CHANGE OF MAIN PITOT STATIC TUBES |
SAAB 2000-34-060 |
| 1-168 |
FUEL-INSPECTION FOR CHAFING IN THE LH AND RH WING TANK |
SAAB 2000-28-012 |
| 1-171 Cancelled |
PROPELLER-PITCH CONTROL UNIT-NEW SERVO VALVE |
DOWTY SB S2000-61-84 |
| 1-174 |
NACELLE-FRONT SPAR-INSPECTION OF SHEAR ANGLES |
SAAB 2000-54-026 |
| 1-175 |
NACELLE-FRONT SPAR-INSPECTION OF DRAG ANGLES |
SAAB 2000-54-028 |
| 1-177 |
FLIGHT CONTROLS-AILERON AND ELEVATOR CONTROL SYSTEM-INSPECTION OF ROLL AND PITCH DISCONNECT HANDLES |
SAAB 2000-27-047 |
| 1-178 |
WINDOWS-INSPECTION OF WINDSHIELD WIPER SPOILER |
SAAB 2000-56-003 |
| 1-180 |
NACELLES/PYLONS-FRONT SPAR-INSTALLATION OF PRESSURE PADS ON SHEAR ANGELS |
SAAB 2000-54-027 |
| 1-181 |
NACELLES/PYLONS-WING/NACELLE INTERFACE-REPAIR OF DRAG ANGELS AND INSTALLATION OF PRESSURE PADS |
SAAB 2000-54-029 |
| 1-182 |
WING-COLD EXPANSION OF FRONT AND REAR SPAR BETWEEN WS20 AND WS83 |
SAAB 2000-57-0038 |
| 1-183 |
POWER PLANT-ENGINE MOUNTING STRUCTURE-TORQUE INSPECTION AND RE-TORQUING SEQUENCE OF THE INTERMEDIATE STRUT REAR ATTACHMENT |
SAAB 2000-71-014 |
| 1-190 |
ELECTRICAL POWER-AC GENERATION-INSPECTION OF TERMINALS ON THE GENERATOR RELAY (7XA AND 8XA) |
SAAB 2000-24-017 |