Beech 400A

Service difficulty reports · 1,397

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '400A'
  ORDER BY difficulty_date DESC"

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SDR DJFA2007007Unknown · odorTRIP NR 1129042 CREW NOTED A SMOKE ODOR IN THE CABIN DURING PRE-LANDING ENVIRONMENTAL SYSTEM CHECK. ODOR WENT AWAY AFTER HEAT WAS TURNED DOWN. MAINTENANCE PERFORMED SEVERAL GROUND RUNS AND WAS UNABLE TO DUPLICATE THE DISCREPANCY. AIRCRAFT WAS RELEASED AND HJan 13, 2007 · N465LX · Beech 400A · Air Distribution SystemSDR DXTA200701854Engine · power lossNR 1 ENGINE WOULD NOT MAKE TAKEOFF THRUST AT FIREWALL.Jan 12, 2007 · N153QS · Beech 400A · Engine (Turbine/Turboprop)SDR DXTA200701843Brake Assy · malfunctionedRT BRAKE ON LT SEAT PILOT INOPERATIVE. THE BRAKE WORKS INTERMITTENTLY. BRAKE ON RT PANEL GOES TO THE FLOOR THEN WILL START TO WORK AGAIN FOR A SHORT TIME. RT SEAT HAD GOOD BRAKES AT ALL TIMES. RETURNED TO DEPARTURE. PERFORM "POWER BRAKE BLEEDING" OF THE BRAJan 9, 2007 · N149QS · Beech 400A · Landing Gear Brake SystemSDR DXTA200701842Squat Switch · disconnectedAUTOPILOT WILL NOT FOLLOW HEADING BUG COMMAND. FOUND BOTH SQUAT SWITCHES DISCONNECTED. RECONNECTED BOTH SQUAT SWITCHES IAW MM 32-60. PERFORMED OPERATIONAL CHECK OF AUTOPILOT. OP CHECKS GOOD.Jan 8, 2007 · N139QS · Beech 400A · Autopilot SystemSDR DXTA200701836Transducer · inoperativeHYDRAULIC PRESSURE GAUGE INDICATED 0 PSI IN FLIGHT. VARIED BETWEEN 0 AND 1000 PSI THEN WENT TO 0 PSI FOR THE REMAINDER OF THE FLIGHT. REMOVED AND REPLACED HYDRAULIC PRESSURE TRANSDUCER. AND CONNECTOR PLUG FOR PRESSURE TRANSDUCER (P339) IAW MM 29-30-00. OPS CHJan 4, 2007 · N153QS · Beech 400A · Hydraulic Indicating SystemSDR DXTA200701834Unknown · unknownBRAKE PEDALS FEEL SPONGY ON LT AND RT SIDE. BRAKES DO STOP AIRCRAFT BUT TAKE EXCESSIVE AMOUNT OF TRAVEL. BLEED BRAKES REF MM 32-40-00. NO DEFECT NOTED. TAXIED AIRCRAFT AND TESTED BRAKING SYSTEM. NO DEFECT NOTED. PEDALS FUNCTION NORMALLY AT THIS TIME.Jan 3, 2007 · N153QS · Beech 400A · Landing Gear Brake SystemSDR DJFA2007001Inlet · crackedDURING A SCHEDULED MAINTENANCE INSPECTION, MAINTENANCE FOUND THE INLET CRACKED. THE CRACK WAS LOCATED AT THE INNER SECTION WHERE THE INLET MOUNTS TO THE ENGINE AND WAS ABOUT .25 INCH LONG FROM THE FASTENER HOLE TO THE INLET EDGE. THE INLET WAS REPAIRED IAW Jan 3, 2007 · N478LX · Beech 400A · Turbine Engine Air Inlet SectionSDR DJFA2007004Coalescer Bag · odorTRIP NR 1124081 CREW REPORTED UNCONTROLLABLE COCKPIT HEAT AND THE ODOR OF SOMETHING BURNING. AIRCRAFT RETURNED TO FIELD. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THE COALESCER SOCK EXTREMELY DIRTY. SUBSEQUENT OPERATIONAL CHECKS PROVED SATISFACTORY.Jan 1, 2007 · N462LX · Beech 400A · Humidity Control SystemSDR DJFA2006366Support Bracket · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE LEFT INBOARD HORIZONTAL STABILIZER ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN BEECHJET COMMUNIQUE' NUMBER Dec 21, 2006 · N718TA · Beech 400A · Horizontal Stabilizer StructureSDR DJFA2006365Tire · failedTRIP NR 1120054; CREW REPORTED THE RT MAIN TIRE WENT FLAT AND CAME APART ON LANDING. MX REMOVED THE AIRCRAFT FROM THE ACTIVE TAXIWAY AND IS ASSESSING ANY ADDITIONAL DAMAGE. SDR WILL BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION.Dec 20, 2006 · N750TA · Beech 400A · TireSDR DJFA2006362Link · brokenKTEB-KHPN TRIP# 1118794 ON LANDING THE CREW OBSERVED THAT THE LEFT THRUST REVERSER WAS DIFFICULT TO DEPLOY. MAINTENANCE FOUND THE LEFT LOWER OUTBOARD IDLER ARM CRACKED AND BROKEN AT THE TR DOOR END BUSHING. THE FAILIED ARM CAUSED ADDITIONAL DAMAGE TO THE TR Dec 17, 2006 · N715TA · Beech 400A · Engine Thrust ReverserSDR 2007FA0000160Bracket · crackedDURING INSPECTION OF HORIZONTAL STABILIZER ROLLER BRACKETS AND STRUCTURE IAW COMMUNIQUÉ NR 70, FOUND LT HORIZONTAL STABILIZER FWD ROLLER BRACKET, PN 45A21085-003, AND LT AFT ROLLER BRACKET, PN 45A21086-003, BOTH CRACKED. MFG AC TECH SUPPORT BELIEVES IMPROPER Dec 16, 2006 · N93XP · Beech 400A · Horizontal Stabilizer Miscellaneous StructureSDR DJFA2006361Skin · crackedDURING A SCHEDULED MAINTENANCE EVENT, MAINTENANCE DISCOVERED CRACKS ON THE TOP SKIN OF THE PYLON. THE CRACKS WERE LOCATED NEAR THE INBOARD TRAILING EDGE; THE FORWARD CRACK WAS .9" LONG 17.25" FROM THE TRAILING EDGE. THE SECOND CRACK WAS .2" LONG 16.125" FROM TDec 16, 2006 · N751TA · Beech 400A · Nacelle/Pylon, Plate/SkinSDR DJFA2006359Fuel Cap · wornTRIP NR 1116583 WHILE IN CRUISE AT FL350, CREW NOTICED FUEL LEAKING FROM LT OVERWING FUEL CAP. CREW DECLARED AN EMERGENCY AND DIVERTED.. MAINTENANCE FOUND EXCESSIVE PLAY ON THE CAP WHILE LOCKED. ON FURTHER INSPECTION THE CAP SEALS WERE FOUND WORN EXCESSIVELY. Dec 15, 2006 · N479LX · Beech 400A · Fuel StorageSDR DJFA2006358Door · crackedDURING ROUTINE MAINTENANCE WALKAROUND FOUND RT IB LANDING GEAR DOOR BRACKET HINGE CRACKED. THE CRACK IS APPROXIMATELY 3 INCHES LONG AND SHEETMETAL DAMAGE ON THE EDGE IS ABOUT 12 INCHES LONG. MAINTENANCE REPLACED THE GEAR DOORDec 15, 2006 · N493CW · Beech 400A · Landing Gear DoorsSDR DJFA2006357Support Bracket · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE LEFT INBOARD HORIZONTAL STABILIZER ROLLER BRACKET AND RIB STRUCTURE WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN BEECHJET CDec 12, 2006 · N405CW · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2006353Support Bracket · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE LEFT INBOARD HORIZONTAL STABILIZER ROLLER BRACKET STRUCTURE WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN BEECHJET COMMUNIQUDec 6, 2006 · N775TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2006354Drain · openTRIP NR: 1114218 CREW REPORTED FUEL LEAKING FROM BOTH WING TIPS NEAR THE TRIM TABS. AIRCRAFT RETURNED TO DEPARTURE. MAINTENANCE FOUND LT AND RT OB SUMP DRAINS OPEN. MAINTENANCE CLOSED THE SUMP DRAINS AND NO FURTHER LEAKING WAS OBSERVED.Dec 6, 2006 · N750TA · Beech 400A · Fuel StorageSDR DJFA2006352Hydraulic System · low pressureON LANDING, CREW REPORTED LOSS OF HYDRAULIC PRESSURE AND NORMAL BRAKES. EMERGENCY BRAKING WAS USED. MAINTENANCE FOUND THE LOW PRESSURE LINE RUPTURED AND LEAKING HYDRAULIC FLUID ON THE LEFT THRUST REVERSER . THE RUPTURE OCCURED APPROXIMATELY 6" FROM THE 90 DDec 5, 2006 · N410CW · Beech 400A · Hydraulic System, MainSDR DXTA200601779Line · leakingWHILE TAXING TO THE RAMP, EXPERIENCED A LOSS OF HYDRAULIC FLUID WHICH REQUIRED HAVING TO USE EMERGENCY BRAKING TO STOP THE AIRCRAFT. DISCOVERED A LARGE AMOUNT OF HYDRAULIC FLUID ON GROUND UNDER NR 1 ENGINE. FOUND NR 1 ENG PRESSURE HYD LINE LEAKING. REMOVED ADec 4, 2006 · N122QS · Beech 400A · Hydraulic System, MainSDR DXTA200601761Control Cable · out of adjustLOUD BUZZ HEARD AND VIBRATION FELT THROUGH OUT AIRPLANE APPROX. 10 MINUTES AFTER TAKEOFF. BUZZ AND VIBRATION INTENSIFIED AS AIRSPEED INCREASED WENT AWAY WHEN FLAPS EXTENDED FOR LANDING. ON POSTFLIGHT. FOUND FLAPS NOT FULLY RETRACTED WITH FLAP INDICATOR SHOWINNov 29, 2006 · N132QS · Beech 400A · Trailing Edge Flap Control SystemSDR DXTA200601758Cable · out of adjustAIRCRAFT ROLLS LT AND RT 2 TO 3 DEGREES OF BANK EACH WAY WITH THE AUTOPILOT ENGAGED (WHEN AUTOPILOT IS DISCONNECTED THE AIRCRAFT HAS RT ROLL TRIM AND DOES EACH TIME. SPOILER BRIDLE CABLE TENSION TO WITHIN LIMITS. OPS CHECK GOOD ON GROUND, IAW MM 27-60-00.Nov 27, 2006 · N101QS · Beech 400A · Autopilot SystemSDR DXTA200601750Display · burned outMFD WENT BLACK IN FLIGHT- DETECTED POSSIBLE SMOKE. REMOVED AND REPLACED MFD WITH OVERHAULED UNIT RECEIVED. ALL WORK PERFORMED IAW SRM NR 523-0775807. OPS CHECK GOOD. NO SMOKE ODOR NOTED AT THIS TIME.Nov 22, 2006 · N102QS · Beech 400A · Indicating/Recording SystemSDR DXTA200601749Computer · inoperativeDURING FLIGHT AT FL 210 WHILE CLIMBING AUTOPILOT AND YAW DAMPER DISENGAGED. COPILOTS PFD WENT BLANK THE FLASHED ON AND OFF SEVERAL TIMES OVER NEXT COUPLE OF MINUTES. WAS UNABLE TO RESET A/P FOR SEVERAL MINUTES. TRANSFERRED A/P TO LT SIDE AND CONTINUED TO LANDNov 22, 2006 · N125QS · Beech 400A · Autopilot SystemSDR 2006FA0001205Rib · crackedDURING AN A, B, AND C INSPECTION, FOUND THE HORIZONTAL STABILIZER MOUNTING FACES NOT PARALLEL WITH THE VERTICAL STABILIZER, HORIZONTAL STABILIZER ROLLER CLEARANCE CHECKS IAW MM 27-40-00 OUT OF SERVICE LIMITS. INSPECTED STABILIZER IAW MFG COMMUNIQUÉ NR 70 AND Nov 20, 2006 · N311HS · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2006345Unknown · odorBURNING SMELL IN COCKPIT ON APPROACH. PAX ON BOARD. GENERAL WALK AROUND INSPECTION BEFORE TAXI SHOWED NO OBVIOUS DAMAGE. TAXIED A/C WHILE OPERATING SYSTEMS, NO BURN SMELL. RAN A/C TO FULL POWER, OPERATED BLEED AIR AND ELECTRICAL SYSTEMS-COULD NOT DUPLICATE.Nov 20, 2006 · N746TA · Beech 400A · Air Distribution SystemSDR 2006FA0001204Release Cable · frayedDURING SCHEDULE (A) AND (B) INSPECTION FOUND LT MLG EMERGENCY UPLOCK RELEASE CABLE ASSY. SEVERLY FRAYED AND CABLE FUNCTION COMPROMISED AT UPLOCK ATTACH CLEVIS END. THIS SB 32-3200. SB 32-3200 IS A RECOMMENDED SB ONLY, COMPLIANCE RECOMMENDED WHEN CABLE ASSY Nov 18, 2006 · N95GK · Beech 400A · Landing Gear Retraction/Extension SystemSDR DJFA2006347Rib · crackedHORIZONTAL STAB ROLLER SUPPORT RIBS ON LEFT AND RIGHT SIDES WERE FOUND CRACKED DURING C-CHECK INSPECTION WHILE PERFORMING THE INSPECTION RECOMMENDED IN RAYTHEON COMMUNIQUE 70. MAINTENANCE REPLACED THE LEFT AND RIGHT RIBS.Nov 18, 2006 · N768TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2006348Control Panel · miswiredDURING POWER ON, PRIOR TO FLIGHT, INSTRUMENT FLOOD LIGHT CIRCUIT BREAKER POPPED AND CREW NOTICED A BURNING ODOR. MAINTENANCE FIRST THOUGHT THAT IT WAS A BAD PANEL BUT LATER DISCOVERED THE THE COPILOT UTILITY LIGHT PANEL MOUNTING SCREW HAD 28 VOLTS ON IT AND WNov 18, 2006 · N793TA · Beech 400A · Light System WiringSDR DJFA2006344Gpu · smokeCREW REPORTS THAT THE GPU- (GROUND POWER UNIT) CAUSED ELECTRICAL SMOKE INSIDE TAIL CONE. ONCE GPU WAS DISCONNECTED SMOKE DISSIPATED. NO EVIDENCE OF FIRE HAS BEEN DISCOVERED.Nov 18, 2006 · N466CW · Beech 400A · Electrical Power SystemSDR DJFA2006340Unknown · odorDIVERTED FOR STRONG ELECTRICAL SMELL IN REAR OF AIRCRAFT. INSP. WIRING AND COMPONENTS IN LAV. GROUND RAN AT ALL SETTING WITH ELECTRICAL LOAD, PACKS AND A/C ON. NO DEFECTS NOTED AT THIS TIME.Nov 8, 2006 · N493CW · Beech 400A · Air Distribution SystemSDR DJFA2006338Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE RT IB HORIZONTAL STABILIZER NOSE RIB STRUCTURE WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70.Nov 1, 2006 · N794TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR 2006FA0001100Fuel Tank · debondedINVESTIGATED REPORTS OF IN-FLIGHT POPPING NOISES FROM UNDER FLOOR AREA ADJACENT TO CABIN DOOR. FOUND FORWARD LT AUXILLARY TANK STRUCTURE UNDERSIDE HONEYCOMB PANELS DISBONDED FROM TANK STRUCTURE SHEETMETAL. NO CORROSION NOTED, HONEYCOMB MATERIAL APPEARS TO HAOct 25, 2006 · N45RK · Beech 400A · Fuel StorageSDR DJFA2006336Line · chafedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A (C) LEVEL INSPECTION A BRAKE RETURN LINE WAS FOUND TO BE CHAFING FROM A SCREW THAT SECURES THE CENTER COCKPIT TO CABIN FLOORBOARD. INSPECTION AND REPAIR OF THIS AREA IS OUTLINED IN SB 53-3511. THE CHAFEOct 20, 2006 · N783TA · Beech 400A · Hydraulic System, MainSDR DJFA2006334Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE RT IB HORIZONTAL STABILIZER ROLLER RIB STRUCTURE WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUÉ' NR 70. THE FORWAOct 19, 2006 · N783TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2006332Coalescer Bag · blockedKCMH - THE CREW REPORTED A STRONG BURNING SMELL WAS COMING FROM THE CABIN AREA DURING FLIGHT. BOTH CABIN AND CREW TEMPERATURE CONTROLS WERE SET AT FULL COLD. MAINTENANCE REMOVED AND REPLACED THE COALESCER SOCK. WHEN GROUND ENGINE RUNS WERE PERFORMED THROUGH Oct 16, 2006 · N472LX · Beech 400A · Humidity Control SystemSDR DXTA200601661Brake Assy · malfunctionedBRAKES GRAB AND TIRES SKID WITH ANTI-SKID ON. BRAKES OPERATE NORMAL WITH ANTI-SKID OFF. DEFERRED IAW NJA HAWKER 400XP. PERFORMED VISUAL INSPECTION AND OPERATIONAL CHECK OF BRAKES. NO DEFECTS NOTED. SYSTEM GROUND CHECKED GOOD IAW BE-400A MM 32-40-00-201.Oct 16, 2006 · N161QS · Beech 400A · Landing Gear Brake SystemSDR DJFA2006331Window · crackedTHE CREW REPORTED THAT THE COPILOTS WINDOW WAS CRACKED AND DELAMINATED.Oct 14, 2006 · N768TA · Beech 400A · Flight Compartment WindowsSDR DXTA200601650Master Cylinder · bypassingCO-PILOTS RT BRAKE PEDAL WENT ALL THE WAY TO THE FLOOR. PRESSURE CAME BACK AFTER SEVERAL PUMPS, NOTICED DURING TAXI. T/S: REMOVED AND REPLACED COPILOTS RT BRAKE MASTER CYLINDER, BLEED AND SERVICED. OPS CHECKS GOOD REF H400 XP MM 32-40-00.Oct 12, 2006 · N101QS · Beech 400A · Landing Gear Brake SystemSDR DJFA2006328Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE RT IB HORIZONTAL STABILIZER NOSE RIB STRUCTURE WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70.Oct 9, 2006 · N448CW · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2006327Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING AN INSPECTION OF THE HORIZONTAL STABILIZER RIBS AND ROLLERS, THE LEFT INBOARD HORIZONTAL STABILIZER NOSE RIB STRUCTURE WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN BEECOct 8, 2006 · N708TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR 2006FA0001040Sensor · damagedIN NORMAL FLIGHT, THE EFC OFF(ELECTRONIC FUEL CONTROL) ANNUNCIATOR LIGHT ILLUMINATED. THE PILOTS ATTEMPTED TO RESET THE EFC SEVERAL TIMES, FAILING AT EVERY ATTEMPT. TROUBLESHOOTING REVEALED DAMAGE TO THE N1 SENSOR PROBE CAUSED BY THE N1 PICK-UP, AT 24 EQUALLOct 5, 2006 · N827SB · Beech 400A · Fuel Controlling SystemSDR DJFA2006326Wire · damagedCYVV - WHEN THE LANDING GEAR WAS EXTENDED THE CREW DID NOT RECEIVE A DOWN AND LOCKED INDICATION FOR THE LEFT MAIN GEAR. THE GEAR INDICATION BULB TESTED GOOD. AN EMERGENCY WAS DECLARED AND AN ALTERNATE GEAR EXTENSION WAS PERFORMED. THE AIRCRAFT LANDED IN KALOct 5, 2006 · N408CW · Beech 400A · Landing Gear System WiringSDR DXTA200601630Evaporator · odorSTRONG MILDEW ODOR NOTED WHEN BLOWER AND OR A/C ARE ON. INSPECTED AND FOUND FWD EVAPORATOR TO HAVE A STRONG MILDEW ODOR. CLEANED FWD EVAP AND OPERATED BLOWER. NO MILDEW SMELL PRESENT REF HAWKER 400XP M/M 20-00-00 AND 21-51-00.Oct 4, 2006 · N142QS · Beech 400A · Air Distribution SystemSDR DXTA200601629Connector · defectiveFOUND STRONG BURNING ODOR ON CLIMB-OUT. SUSPECTED FREON AIR AS PROBLEM. TURNED OFF FREON AIR AND ODOR WENT AWAY. REPLACED DEFECTIVE GALLEY CONNECTOR IAW HAWKER 400XP DWG 07-233001 REV IR.Oct 3, 2006 · N149QS · Beech 400A · Equipment/Furnishings WiringSDR DJFA2006324Switch · overheatedTHE FLIGHT CREW REPORTED A ODOR OF SMOLDERING INSULATION APPEARS WHEN THE AVIONICS MASTER SWITCHES WERE ON. AFTER SHUTTING THE AVIONICS OFF THE ODOR DISSIPATED. MAINTENANCE TRACED THE SMOKEY ODOR TO THE FUEL VALVE ANNUNCIATOR SOCKET AFTER DISCOVERING THAT THSep 30, 2006 · N798TA · Beech 400A · Fuel Selector/Shut-Off ValveSDR DJFA2006323Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING AN INSPECTION OF THE HORIZONTAL STABILIZER, THREE RIBS WERE FOUND CRACKED ON THE LEFT HORIZONTAL STABILIZER. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN BEECHJET COMMUNIQUE' NUMBER 70. TSep 28, 2006 · N437CW · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DXTA200601617Mixing Valve · faultyON TAXI OUT, CO-PILOTS BRAKE FAILED. INITIALLY HARD BRAKES WITH NO BRAKING. RIGHT PEDAL WENT TO FLOOR, THEN WITH 3 PUMPS, HAD BRAKES, BUT A/C SHUTTERED TO A STOP WITH SEVERE RUMBLE NOTICED. GAINED ACCESS TO BRAKE MIXING VALVES. REMOVED FAULTY RT MIXING VALSep 26, 2006 · N123QS · Beech 400A · Brake Anti-Skid SectionSDR DJFA2006322Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STAB ROLLER INSPECTION THE LT AND RT IB HORIZONTAL STAB NOSE RIB STRUCTURES WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70.Sep 25, 2006 · N471CW · Beech 400A · Horizontal Stabilizer, Spar/RibSDR 2006FA0000932Rib · crackedTHE RIBS LOCATED UNDER THE HORIZONTAL STABILIZER BRACKETS WERE CRACKED, BOTH THE LT AND RT SIDES. THIS IS COVERED UNDER COMMUNIQUE NUMBER 70.Sep 20, 2006 · N27XP · Beech 400A · Horizontal Stabilizer, Spar/Rib
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