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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DXTR20121217003Angle · crackedLEFT ENG THRUST REVERSER, LOWER DOOR, INBD & OTBD STIFFENERS CRACKED. R & R INBD STIFFENER ON THE LT ENG THRUST REVERSER LOWER DOOR, PN OFF 202-0001-29 AND PN ON 202-0001-29 IAW SRM 51-42-00. R & R OTBD STIFFENER ON THE LT ENG THRUST REVERSER LOWER DOOR, PN ODec 13, 2012 · N132QS · Beech 400A · Engine Thrust ReverserSDR DXTR20121217001Skin · crackedLT PYLON AFT UNDERSIDE SKIN IS CRACKED AT TOW RIVET LOCATIONS. COMPLIED WITH THE REMOVAL AND REPLACEMENT OF THE LT PYLON SKIN, PN 45A34420-049. PN OF THE RIVETS USED FOR THE R & R IS CR3242-4-02 BLIND RIVETS. WORK WAS PERFORMED IAW THE MODEL 400XP, SRM CHAPDec 12, 2012 · N102QS · Beech 400A · Nacelle/Pylon, Plate/SkinSDR DXTR20121217002Angle · crackedLT T/R, OTBD STANG FAIRING, UPPER ATTACH BRACKET IS CRACKED. R & R LEFT THRUST REVERSER OTBD UPPER STANG ANGLE. WORK WAS PERFORMED IN REF TO SRM 51-40-01.Dec 9, 2012 · N102QS · Beech 400A · Engine Thrust ReverserSDR L7OA201212070001Pitch Control · malfunctionedPITCH TRIM FAILED ON TAKEOFF. REVERTED TO EMERGENCY TRIM THEN BACK TO NORMAL. AUTO PILOT PITCH TRIM OK. PERFORMED A FULL FUNCTIONAL CHECK OF THE PITCH TRIM SYSTEM IAW AMM 27-40-00-201. COULD NOT DUPLICATE PROBLEM.Dec 7, 2012 · N999YB · Beech 400A · Stabilizer Control SystemSDR DXTA2012112905197Control Unit · malfunctionedAFTER LANDING, THE BRAKES APPEARED TO WORK NORMALLY. PILOT APPLIED THE BRAKES BUT THE PEDALS WERE STIFF. IT FELT LIKE THE ANTI-SKID CHECK DURING TAXI OUT. A SECOND ATTEMPT WAS MADE AND THE BRAKES WERE STILL STIFF AND THE AIRPLANE WAS NOT SLOWING DOWN. COPNov 28, 2012 · N116QS · Beech 400A · Brake Anti-Skid SectionSDR 2015FA0000402Starter Gen · inoperativeSTARTER GENERATOR SENT TO AND RECEIVED BACK AS O/H. INSTALLED ON ACFT IN 09/2010 AND UNIT DID NOT OPERATE PROPERLY.Nov 26, 2012 · N213BK · Beech 400A · Starter-GeneratorSDR DJFA20121124001Warning Light · false activationCREW REPORTED DURING TAKEOFF ROLL "ANTI-SKID FAIL" LIGHT ILLUMINATED AND DEACTIVATED SYS. MX INSPECTED ANTI-SKID TRANSDUCERS AND PERFORMED OPS CHECKS ON THE BRAKE/ANTI-SKID SYS, ALL CHECKS FOUND BRAKE/ANTI-SKID SYS TO BE OPERATING CORRECTLY. A MX VERFICATIONNov 24, 2012 · N444FL · Beech 400A · Brake Anti-Skid SectionSDR DXTA2012112605190Door · out of adjustRED LIGHT IN GEAR HANDLE WOULD NOT EXTINGUISH AFTER GEAR RETRACTION, TOWER NOTICED AND SAID IT APPEARS TO BE THE RT SIDE. GEAR WAS EXTENDED NORMALLY WITH A GEAR SAFE INDICATION, LANDED NORMALLY. JACKED ACFT AND SWUNG LANDING GEAR. CONFORMED INTRANSIT GEAR FANov 23, 2012 · N120QS · Beech 400A · Landing Gear Door Retract SectionSDR L7OA2012F00256Pitch Control · failedAUTOPILOT PITCH TRIM FAIL. FLIGHT CREW SQUAWKED THAT IN LEVEL FLIGHT WITH THE AUTOPILOT ENGAGED, WAS GETTING A RUNAWAY STAB IN THE NOSE DOWN POSITION. ACFT SYSTEMS PRESENTLY BEING TROUBLESHOT FOR PROBLEM.Nov 21, 2012 · N870BB · Beech 400A · Autopilot SystemSDR DXTA2012112105188Control Valve · failedAFTER LANDING, BRAKES APPLIED AND WORKED FINE. ACFT WAS TAXIING TO PARKING, PILOT APPLIED BRAKES AND NO RESULT. PEDALS WERE STIFF. SECOND ATTEMPT PROVIDED SAME RESULT. BRAKE PEDALS RELEASED AND BRAKES RETURNED TO NORMAL. R & R POWER BRAKE CONTROL VALVE IANov 20, 2012 · N116QS · Beech 400A · Landing Gear Brake SystemSDR DXTA2012111605183Brake Sys · contaminatedPEDALS WERE STIFF WITH NO RESISTANCE AND PLANE WAS NOT SLOWING. UPON EMERGENCY BRAKE APPLICATION, THE BRAKE PEDALS REENGAGED. FOUND AIR IN BRAKE SYSTEM. PERFORMED BRAKE BLEED AND EMERGENCY SYSTEM PURGE IAW MM 32-40-00-201. SERVICED EMERGENCY BRAKE NITROGEN INov 15, 2012 · N116QS · Beech 400A · Landing Gear Brake SystemSDR DXTA2012111205179Switch · out of adjustRED GEAR HANDLE LIGHTS FAILED TO EXTINGUISH AFTER GEAR RETRACTION (GEAR DOOR UNSAFE NOT UP AND LOCKED INDICATION). RETURNED TO AIRPORT, LANDING GEAR EXTENTION WAS NORMAL. NOSE GEAR UPLOCK SWITCH CLEANED AND ADJUSTED IAW AMM 32-30-00. GEAR OPERATION AND ANNUNNov 9, 2012 · N120QS · Beech 400A · Landing Gear Retraction/Extension SystemSDR CVGA201211009001Generator · failedLEFT GENERATOR FAILED INFLIGHT AND WOULD NOT RESET. PRIOR TO FAILURE, THERE WAS A BURNING ODOR COMING FROM THE VENTS IN THE COCKPIT, SMELL DISSIPATED AFTER GENERATOR WAS OFF-LINE.Nov 8, 2012 · N309AK · Beech 400A · AC Generator-AlternatorSDR CVGA20121108002Unknown · malfunctionedFLAPS WILL NOT REMAIN RETRACTED. FLAPS DROOP (HANG) DOWN AT FL220 & .65 MACH OR 320 KTS INDICATED. FLAP BUZZ IS LOUD AND VIBRATES FUSELAGE UNTIL AIRPLANE IS BELOW 200 KTS INDICATED & 10 DEGREES OF FLAPS SELECTED.Nov 8, 2012 · N642AC · Beech 400A · Trailing Edge Flap Control SystemSDR CVGA201211008001Unknown · malfunctionedLANDING GEAR WILL NOT RETRACT ON FIRST CYCLE. LANDING GEAR RETRACTED AFTER TAKEOFF AND INDICATED NOSE WHEEL DOWN, ALL GEAR DOORS CLOSED. 2ND CYCLE, GEAR RETRACTED AND GEAR HANDLE REMAINED ILLUMINATED "RED". 3RD CYCLE, LANDING GEAR RETRACTED SLOWLY. AIRPLANNov 8, 2012 · N642AC · Beech 400A · Landing Gear Retraction/Extension SystemSDR DXTA2012110805176Anti-Skid Sys · malfunctionedBRAKES ARE HARD & UNRESPONSIVE WITH THE ANTI-SKID SYS ON. NORMAL BRAKING WITH THE ANTI-SKI SYS OFF. COMPLIED WITH ENGINE RUNS AND TAXI CHECK AT AIRCRAFT BRAKING. NO DIFFERENCES. PERFORM ANTISKID ON AND ANTISKID OFF. COMPLIED WITH FAILURE DETECTION CIRCUIT CHENov 7, 2012 · N108QS · Beech 400A · Brake Anti-Skid SectionSDR DXTA2012110705174Unknown · odorWHEN PERFORMING OCF: RAN ACFT ON GROUND FOR 10 MINS AT VARIOUS HIGH AND LOW POWER SETTINGS (BLEEDS ON) NO ABNORMAL ODORS PRESENT. ON TAKEOFF JUST AFTER BECOMING AIRBORNE, A STRONG ENVIORMENTAL BURNING ODOR WAS PRESENT. NO VISABLE SMOKE BUT FUMES WERE VERY STRNov 6, 2012 · N132QS · Beech 400A · Air Distribution SystemSDR DXTA2012110205164Unknown · odorA STRONG ODOR OF HOT (NOT QUITE BURNING) PLASTIC OR RUBBER COMING FROM THE COCKPIT WEMAC VENTS DURING TAKEOFF, A FEW SECONDS AFTER APPLYING FULL TAKEOFF POWER. THE ODOR DISSIPATES SUBSTANTIALLY A FEW MINUTES AFTER TAKEOFF. PERFORMED TAKEOFF POWER SEVERAL TINov 1, 2012 · N132QS · Beech 400A · Air Distribution SystemSDR 2013FA0000001Bearing · failedAFTER LANDING, CREW NOTICED A DRAG AND A PULL TO THE LEFT AS THE PLANE SLOWED DOWN. NOTICED IT WAS TAKING MORE POWER THAN NORMAL TO MAKE THE ACFT MOVE FORWARD. STOPPED ACFT TO INVESTIGATE THE PROBLEM. FOUND A FLAT TIRE AND WHEN MX ARRIVED AT THE ACFT THEY FOct 30, 2012 · N827SB · Beech 400A · Main Landing Gear Strut/Axle/TruckSDR DXTA2012102205159Brake Assy · contaminatedAFTER BLOCK-IN, LEFT BRAKE SMOKING. DURING INSPECTION, LEFT TIRE AND WHEEL ASSY WAS EXTREMELY HOT AND A DISTINCT ODOR OF HOT BRAKES. LANDING WAS NORMAL WITH VERY MINIMAL USE OF THE BRAKES. INSPECTED LEFT BRAKE ASSEMBLY, APPEARS TO BE NEW AND NO EVIDENCE OF OOct 20, 2012 · N120QS · Beech 400A · Landing Gear Brake SystemSDR 2012FA0000729Tube · gougedWHILE CARRYING OUT A B-CHECK INSPECTION ON THE LT FLAP, IT WAS NOTED THE LT FLAP TUBE ASSEMBLY HAD A LARGE GOUGE IN IT.Oct 18, 2012 · N473FL · Beech 400A · Trailing Edge FlapsSDR DXTA2012101105142Actuator · failedAFTER TAKEOFF. SELECTED GEAR UP. GREEN LIGHTS WENT OUT, RED GEAR HANDLE LIGHT STAYED ON. ON LANDING, SELECTING GEAR DOWN, 3 GREEN LIGHTS ON AND RED LIGHT WENT OUT. ATTEMPTED NLG OPS CHECK IAW MM 32-20-00-201, NLG WOULD STOP MOVING PRIOR TO UPLOCK ENGAGEMENOct 10, 2012 · N120QS · Beech 400A · Landing Gear ActuatorSDR DXTA2012101205140Bulb · inoperativeRT MAIN GEAR INDICATOR LIGHTS DID NOT ILLUMINATE GREEN ON GEAR EXTENSION. LIGHTS TEST WOULD NOT ILLUMINATE RMG LIGHT. FOLLOWED CHECKLIST AND ALL INFORMATION LED TO A NORMAL LANDING AS GEAR APPEARED TO BE DOWN AND LOCKED. REMOVED AND REPLACED ALL FOUR LIGHT BUOct 9, 2012 · N140QS · Beech 400A · Landing Gear Position and WarningSDR DXTA2012100805139Filter · dirtyVIBRATION FELT IN BRAKE PEDALS UPON LANDING ROLLOUT. BRAKE EFFECTIVENESS IS DIMINSHED UNTIL STRONG PRESSURE IS APPLIED TO PEDALS. GAINED ACCESS TO THE POWER BRAKE ANTI-SKID CONTROL VALVE FILTERS. CLEANED AND VISUALLY INSPECTED ANTI-SKID CONTROL FILTERS AND COct 7, 2012 · N108QS · Beech 400A · Landing Gear Brake SystemSDR DJFA20120929001Brake Sys · pressure lossCREW REPORTED LEFT SIDE, RIGHT BRAKE PEDAL INTERMITTENTLY COLLAPSES TO TRAVEL LIMIT WITH LITTLE OR GRABBY BRAKING ACTION. AFTER PUMPING PEDAL NORMAL BRAKE OPS RETURN, THOUGH PEDAL STILL FEELS SOFT AND DOESN’T MATCH LT PEDAL. THE RT SIDE BRAKES OPERATES NORMALSep 29, 2012 · N438LX · Beech 400A · Landing Gear Brake SystemSDR CVGA20120925001Warning System · activatedTAKEOFF WARNING HORNS SOUND ON TAKEOFF WITH PITCH TRIM IN THE GREEN BAND.Sep 21, 2012 · N315SL · Beech 400A · Central WarningSDR DJFA20120918001Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZ STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED (ALONG WITH 7 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT RT HORIZ CANTED STA 62.20, BETWEEN THSep 18, 2012 · N448LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120918002Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZ STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED ON THE LOWER FLANGE AT LT HORIZ CANTED STA 62.20, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. THE RIBS WERE REPSep 18, 2012 · N448LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120918003Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED ON THE LOWER FLANGE AT RT HORIZ CANTED STA 46.06, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. THE RIBS WERSep 18, 2012 · N448LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120918004Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED ON THE LOWER FLANGE AT LT HORIZ CANTED STATION 46.06, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. THE RIBSSep 18, 2012 · N448LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120918005Rib · crackedDURING INSP FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED (ALONG WITH 7 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT RT HORIZ CANTED STA 29.92, BETWEEN THESep 18, 2012 · N448LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120918006Rib · crackedDURING INSP FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED (ALONG WITH 7 OTHER RIBS; EA RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT LT HORIZ CANTED STA 29.92, BETWEEN THE FSep 18, 2012 · N448LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120918007Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZ STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED (ALONG WITH 7 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT RT HORIZ CANTED STA 13.78, BETWEEN THSep 18, 2012 · N448LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120918008Rib · crackedDURING INSPECTION, RIB WAS FOUND CRACKED ON THE LOWER FLANGE AT LT HORIZONTAL CANTED BS 13.78, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. RIB REPLACED.Sep 18, 2012 · N448LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120913001Motor · overheatedWHILE ON THE GROUND, CREW REPORTED CABIN STARTED FILLING UP WITH SMOKE STARTING FROM LAVATORY AREA. SMOKE WAS ALSO NOTED TO BE COMING OUT OF THE EXTERIOR EXHAUST AND INLET PANELS FOR THE AIR CONDITIONING UNIT. MAINTENANCE FOUND THE FREON AC COMPRESSOR MOTOR SSep 13, 2012 · N480LX · Beech 400A · Cabin Cooling SystemSDR DXTA2012090405119Spring · failedAFTER TAKEOFF WHEN GEAR HANDLE WAS RAISED, NOTICED RED IN TRANSIT LIGHT REMAINED ILLUMINATED AND ALL GREEN LANDING GEAR LIGHTS WERE OUT. TOWER REPORTED NOSE AND MAIN GEAR APPEARED TO BE RETRACTED BUT BOTH MAIN GEAR DOORS WERE EXTENDED. COMPLIED WITH CHECKLISep 9, 2012 · N120QS · Beech 400A · Landing Gear Position and WarningSDR DXTA2012091005119Landing Gear · malfunctionedAFTER TAKEOFF, WHEN GEAR HANDLE WAS RAISED, NOTICED RED IN TRANSIT LIGHT REMAINED ILLUMINATED AND ALL GREEN LANDING GEAR LIGHTS WERE OUT. TOWER REPORTED NOSE AND MAIN GEAR APPEARED TO BE RETRACTED BUT BOTH MAIN GEAR DOORS WERE EXTENDED. COMPLIED WITH CHECKLISSep 9, 2012 · N120QS · Beech 400A · Landing Gear Retraction/Extension SystemSDR DJFA20120827001Mount · crackedDURING INSPECTION OF NR 1 ENGINE FORWARD MOUNT AFT BRACKET AS CALLED OUT BY AD 2002-01-23, THE MOUNT WAS FOUND CRACKED. MX R & R BRACKET WITH KIT 128-4035, REV B.Aug 27, 2012 · N443LX · Beech 400A · Engine Mount SectionSDR DJFA20120815006Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STAB ASSY, RIB FOUND CRACKED ON THE LOWER FLANGE AT RT HORIZTONAL CANTED STATION 46.06, BETWEEN THE FWD AND AFT SPARS. CRACK EMANATE FROM THE FASTENER HOLE. RIBS REPLACED.Aug 15, 2012 · N438LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120815005Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STAB ASSY, RIB FOUND CRACKED ON THE LOWER FLANGE AT RT HORIZTONAL CANTED STA 46.06, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. RIB REPLACED.Aug 15, 2012 · N438LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120815004Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STAB, RIB FOUND CRACKED ON THE LOWER FLANGE AT RT HORIZONTAL CANTED STATION 29.92, BETWEEN THE FWD AND AFT SPARS. CRACK EMANATES FROM THE FASTENER HOLES. RIB REPLACED.Aug 15, 2012 · N438LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120815003Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STAB, RIB FOUND CRACKED ON THE LOWER FLANGE AT RT HORIZONTAL CANTED STATION 13.78, BETWEEN THE FWD AND AFT SPARS. CRACK EMANATES FROM THE FASTENER HOLES. RIB REPLACED.Aug 15, 2012 · N438LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120815002Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STAB, RIB WAS FOUND CRACKED ON THE LOWER FLANGE AT LT HORIZONTAL CANTED STATION 46.06, BETWEEN THE FWD AND AFT SPARS. CRACK EMANATE FROM THE FASTENER HOLES. RIB REPLACED.Aug 15, 2012 · N438LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120815001Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER, THE RIB DESCRIBED BELOW WAS FOUND CRACKED (ALONG WITH 5 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT LT HORIZTONAL CANTED STATION 13.78, BAug 15, 2012 · N438LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120802001Master Cylinder · inoperativeDURING TAXI, CREW REPORTED LT BRAKE PEDAL ON BOTH SIDES TO BE INEFFECTIVE WITH ANTI-SKID ON AND OFF. MX FOUND THE LT MASTER CYLINDER FAILED. BOTH MAIN WHEEL BRAKES AND THE LT BRAKE MASTER CYLINDER WERE REPLACED.Aug 2, 2012 · N444FL · Beech 400A · Master Cylinder/Brake ValveSDR L7OA2012072400001Dump Valve · faultyON APPROACH, CYCLED LANDING GEAR HANDLE DOWN, 3 GREEN LIGHTS ILLUMINATED, RED UNSAFE LIGHT IN THE LANDING GEAR HANDLE REMAINED ILLUMINATED. CYCLED GEAR UP AND EXTEND IT AGAIN. ALL 3 GREEN LIGHTS FAILED TO ILLUMINATED AND NO RED UNSAFE INDICATION IN GEAR HAJul 23, 2012 · N333YJ · Beech 400A · Landing Gear Retraction/Extension SystemSDR CVGA20120715001Unknown · unbalancedAIRCRAFT WOULD NOT PRESSURIZE ON CLIMB-OUT.Jul 15, 2012 · N309AK · Beech 400A · Cabin Pressure Control SystemSDR DJFA20120711001Unknown · odorDURING FLIGHT, CREW REPORTED HEARING A POPPING SOUND, FOLLOWED BY A BURNING ODOR. THE ODOR DISSIPATED AFTER A SHORT TIME AND THE ACFT LANDED SAFELY AT DESTINATION. MX WAS UNABLE TO FIND ANY DISCREPANCIES. DISCREPANCY HAS NOT REPEATED.Jul 11, 2012 · N429LX · Beech 400A · Air Distribution SystemSDR 9JLA201207160886Altimeter · defectiveCREW REPORTS THE STAND-BY ALTIMETER STICKS INTERMITTENTLY. REMOVED THE DEFECTIVE STAND-BY ALTIMETER SN AG554. INSTALLED AN O/H STAND-BY ALT. PN 122-382142-13, SN AG922. FUNCTIONAL CHECKS SATISFACTORY.Jul 6, 2012 · N393GH · Beech 400A · Altimeter, Barometric/EncoderSDR DJFA20120706001Control Unit · malfunctionedON LANDING, CREW REPORTED LOSS OF BRAKING ACTION WITH THE ANTI-SKID SYSTEM ON. WITH ANTI-SKID SYSTEM TURNED OFF, THE BRAKES WORK NORMALLY. MX FOUND THE ANTI-SKID CONTROL UNIT FAILED.Jul 6, 2012 · N404FL · Beech 400A · Brake Anti-Skid Section
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