B-N Group BN-2A-26
Service difficulty reports · 82
Newest first. General aviation reporting is voluntary.
Query with SQL
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 = 'BN2A26' 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.
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 = 'BN2A26' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 2024FA0000009Brake Caliper · leakingLOOSE BRAKE DURING TAXI.HYDRAULIC LEAK FOUND ON LEFT INBOARD BRAKE PACKINGS.SDR 2024FA0000008Brake Caliper · leakingLOOSE BRAKE DURING TAXI.HYDRAULIC LEAK FOUND ON LEFT INBOARD BRAKE PACKINGS.SDR 2023F00146Wing · corrodedCORROSION WAS FOUND ON RIGHT WING STA 22 TO W STA 49 LOWER SHEET METAL LAMINATE ON FWD SIDE UNDER SPAR AREA AND AFT SIDE UNDER SPAR AREASDR UOIA2023012800005Crankshaft · brokenAFTER LANDING IN CULEBRA, RIGHT ENGINE QUIT ON TAXI TO THE RAMP. ENGINE WAS INSPECTED AND THE ENGINE CRANKSHAFT IDLE GEAR FOUND BROKEN. ENGINE WAS REMOVED AND REPLACED.SDR 2021F00092Gear · brokenPILOT PERFORMED PRE FLIGHT MAGNETO CHECK. THE LH MAG WAS INOPERATIVE. FURTHER INSPECTION BY MX PERSONNEL DISCOVERED THE LH MAGNETO DRIVE GEAR WAS MISSING 3 TEETH; MAKING THE MAGNETO NOT FUNCTIONAL.SDR UOIA2017080300001Caliper · brokenRIGHT BRAKE FAILED TO OPERATED, THE AIRCRAFT GO OUT OF RUNWAY.SDR UOIA20170803Rudder · inoperativeDURING FLIGHT RUDDERS STOPPED RESPONDING.SDR UOIA201510071114Stud · brokenLEFT ENG CYLINDER NR 3 CRANKCASE STUDS BROKEN.SDR RI9A20150809001Starter · bindingBENDIX ON STARTER OF RT ENGINE FAILED TO DISENGAGE AFTER STARTUP. R & R STARTER WITH NEW. NO FURTHER DISCREPANCIES NOTED.SDR LU4R2015020618118Blade · crackedPROPELLER BLADE FOUND CRACKED AT SHANK.SDR WS9R2015FA0000008Crankshaft · brokenENGINE RECEIVED FOR O/H DUE TO HIGH METAL. DURING DISASSEMBLY, IT WAS DISCOVERED THAT A PIECE OF THE CHEEK ON THE CRANKSHAFT HAD BROKEN OFF ALLOWING THE COUNTERWEIGHT TO IMPACT CONNECTING RODS AND THE CRANKSHAFT. THE COUNTERWEIGHT PINS WERE UNDAMAGED. THE CSDR UOI2014F00000Indicator · overheatedSMOKE IN THE COCKPIT. LT ENG CLUSTER OIL TEMP INSTRUMENT OVERHEAT.SDR UOI2013F00001Cylinder · brokenDURING FLIGHT, ENG SHUTDOWN. ENG CYLINDER BROKEN.SDR UOI2013F00000Caliper · leakingBRAKE CALIPER LT SIDE, LEAKING.SDR RI9A20120807557Crankcase · crackedPILOT HEARD RIGHT ENGINE RUNNING ROUGH AND SAW THE OIL PRESSURE DROP. SHUT THE ENGINE DOWN AND MADE A SAFE LANDING AT OUZINKIE AIR STRIP. UPON INSPECTION FOUND A CRACK IN THE CRANKCASE BETWEEN THE NR 3 AND NR 5 CYLINDERS. A NEW ENGINE WAS INSTALLED. AFTERSDR 2012FA0000558Caliper · leakingLEFT MAIN LANDING GEAR INBD BRAKE CALIPER, LEAKING.SDR RI9A20120617001Regulator · malfunctionedPILOT SMELLED ODOR AND SAW SMOKE FROM INSTRUMENT PANEL. PILOT RETURNED TO KODIAK AIRPORT WITHOUT INCIDENT AND MADE A NORMAL LANDING. ON INVESTIGATION, IT WAS FOUND THE RIGHT ENGINE ALTERNATOR VOLTAGE REGULATOR HAD CAUSED AN OVERVOLTAGE SITUATION AND THE SMOKSDR RI9A2012FA0000125Case · damagedPILOT EXPERIENCED AN ROUGH RUNNING LT ENGINE 20 MINUTES INTO THE FLIGHT. THE PILOT REPORTED THAT ALL LT ENGINE INSTRUMENT INDICATIONS WERE NORMAL AT THAT TIME. OIL PRESSURE DROPPED TO ZERO, TURNED BACK TO AIRPORT. DECLARED AN EMERGENCY AND LANDED WITHOUT ANSDR ISCA2011022201Retaining Nut · failedIN CRUISE FLT, AT 2500 FT AGL & APPROX 15 MILES FROM DESTINATION, PILOT NOTED A SLIGHT VIBRATION ON STARBOARD (RT) ENG FOLLOWED BY A LOUD BANG. IN RESPONSE, PILOT SHUT THE ENG DOWN, AND FEATHERED PROP. AFTER LANDING, THE POST-FLIGHT INSP REVEALED THE NR 3 CYSDR UOI2011F00000Drive Assy · worn(ENGINE INTERNAL) PROPELLER GOVERNOR DRIVE DAMAGE.SDR CA100723007Impulse Coupling · brokenMAG WAS RECEIVED DUE TO SEIZED CONDITION. UNKNOWN WHEN IT OCCURRED DURING ENG OPERATION. 1 IMPULSE FLYWEIGHT WAS FOUND BROKEN AWAY FROM IMPULSE ASSY AND WEDGED BETWEEN THE OTHER FLYWEIGHT AND THE MAG HOUSING. THE IMPULSE COUPLING WAS REMOVED AND THE RIVET THSDR 2009FA0000759Beam · crackedWHILE PERFORMING FLUORESCENT DYE PENETRANT INSP IAW AD 2002-25-03 OF CAPTAINS RUDDER PEDAL BEAMS FOUND CRACKED ON (LT) INNER SIDE FWD BEAM. (K)SDR CA090119013Sleeve · looseON GROUND RUN IT WAS DISCOVERED THAT CYLINDER NR 5 ON THE RIGHT ENGINE, EGT WAS NOTICABLY HIGHER THAN OTHER CYLINDERS. INDUCTION TUBE WAS REMOVED FROM THE CYLINDER, THE INDUCTION TUBE SLEEVE IN THE OIL SUMP WAS FOUND TO BE LOOSE.SDR CA080608003Nut · stripped(CAN) DURING A TRAINING FLIGHT, ON OVERSHOOT FROM A ABORTED LANDING, FLAPS RETRACTED UN-COMMANDED. PILOT REDUCED POWER AND WAS ABLE TO LAND STRAIGHT AHEAD ON REMAINING RUNWAY. INSPECTION FOUND THE FLAP ACTUATOR STRIPED. ACTUATOR WAS REMOVED AND SENT FOR OVERHSDR CA070202008Collar · broken(CAN) NOSE LANDING GEAR STEERING COLLAR, BROKE IN TWO PIECES DURING GROUND HANDLING. COLLAR CRACKED AFT GREASE FITTING HOLE ANF FWD RT RELEASE DOG SLOT. (TC NR 20070202008)SDR CA060702001Wheel · cracked(CAN) ON TAXI AFTER LDG, A VIBRATION WAS NOTED ORIGINATION ON THE LH LDG GEAR. IT WAS ORIGINALLY THOUGHT TO BE A WHEEL OUT OF BALANCE. ON INSPECTION, A CRACK WAS OBSERVED ON THE INNER WHEEL 1/2 OUTBOARD ASSEMBLY. THE CRACKED RIM WAS REPLACED WITH NEW CLEAVLSDR 2005F00072Attach Bracket · brokenGEAR LEFT HAND OLEO ATTACHMENT BRACKET FAILED DURING LANDING. A/C NOSED INTO THE MUD CAUSING MAJOR DAMAGE. PN NB-40-0075 IS COVERED UNDER AD2002-02-11 AND HAD 217 LANDINGS AND 101 HOURS SINCE LAST INSPECTION PER PAR (D)(1) OF AD.SDR CA050427006Rod · brokenDURING TAXI NOTICED RUDDER PEDALS SLOPPY, UPON INSP DISCOVERED RUDDER BAR DRIVE ROD BROKEN.SDR CA050311002Engine · failed(CAN) ENG FOUND TO HAVE DROP IN OIL PRESS. INSP, PUNCTURE HOLE WAS FOUND IN TOP OF RT CRANKCASE HALF. METAL WAS FOUND IN OIL SCREEN. CYL 2, 4, AND 6 WERE REMOVED FOR INSP. 4 OF 12 LIFTER BODY CONTACT FACES WERE BROKEN. BROKEN MATERIAL FROM LIFTER BODIES ISDR AUS20040502Washer · missing(AUS) THROTTLE QUADRANT FRICTION ADJUSTER WASHER MISSING. FOUND DURING INSPECTION IAW AD/BN2/69 AND SB 272.SDR AUS20040320Shaft · sheared(AUS) RT ENGINE PROPELLER GOVERNOR DRIVESHAFT SHEARED IN AREA LEVEL WITH THE MOUNTING FACE.SDR AUS20030786Rib · cracked(AUS) ELEVATOR END RIB CRACKED. FOUND DURING INSPECTION IAW SB-190.SDR AUS20021181Bracket · worn(AUS) ELEVATOR OUTBOARD HINGE BRACKET WORN AND RIVETS LOOSE. FOUNDDURING INSPECTION IAW AD/BN2/70 AND BN2/SB259.SDR AUS20020123Brush Block · shorted(AUS) ALTERNATOR BRUSHES SHORTING BETWEEN THE SLIP RINGS AND ALTERNATOR SLIP RING END BEARING.SDR AUS20011400Clamp · mismanufactured(AUS) GASCOLATOR FILTER BOWL UNSECURELY CLAMPED. INVESTIGATION FOUND INADEQUATE DEPTH OF HOLE PREVENTED FULL ENGAGEMENT OF ONE LEG OFTHE SADDLE CLAMP.SDR AU010044Control Cable · seized(AUS) RT PROPELLER CSU CONTROL CABLE OUTER CONDUIT WORN THROUGH WITHTHE INNER CABLE CATCHING ON THE WORN AREA. CONTROL SEIZED.SDR AU010043Cable · misinstalled(AUS) ENGINE MIXTURE CONTROL INNER CABLE ONLY ENGAGED IN THE ENGINE CONTROL END BY APPROXIMATELY 1.5 TURNS.SDR AU010042Cable · loose(AUS) ENGINE THROTTLE CABLE OUTER CONDUIT DISCONNECTED AT FIREWALL. THE NUT SECURING THE CONDUIT HAD NO LOCKWIRE.SDR VLI2003F00000Shaft · brokenDURING CRUISE RT ENGINE PROPELLER FEATHERING WITHOUT NOTICE. ENGINE SHUT DOWN AND LANDING WITHOUT PROBLEMS. DURING INVESTIGATION, FOUND PROPELLER GOVERNOR SPLINE SHAFT BROKEN IN TWO PIECES. REPLACED GOVERNOR, RUN UP SATISFACTORY. POSSIBLE GOVERNOR INTERNALSDR 20001129SH027Bearing · brokenDURING ROUTINE INSPECTION, REMOVED OIL FILTER AND FOUND EXCESSIVE PARTICLES ON OIL SCREEN. REMOVED ENGINE FOR SENDING TO OVERHAUL. PRELIMINARY VIEW FOUND LEFT MAGNETO CASE BEARING DISINTEGRATED AND CASE GEAR WEAR. (X)SDR CA000719018Beam · cracked(CAN) FLUORESCENT LP EXAMINATION WAS CONDUCTED ON THE AIRCRAFT PILOT, COPILOT LT, RT RUDDER PEDAL TORQUE ARM RADIUS. RESULTS: COPILOT RUDDER SET REVEALED REJECTABLE CRACK INDICATIONS AS MARKED. IN SERVICE BULLETIN (PRECAUTIONARY EXAMINATION) THERE WERE NO RSDR 20000523SH029Cylinder · separatedSJU/FDO - ON CRUISE FLIGHT, LEFT ENGINE STARTED TO VIBRATE. ENGINE SHUT DOWN WAS ACCOMPLISHED AND LANDED IN FAJADO. INSPECTION REVEALED NR 4 CYLINDER FOUND SEPARATED FROM ENGINE. ENGINE REPLACED. (X)SDR 20000517SH017Bushing · wornPILOT REPORTED LEFT ENGINE WAS HARD TO START. REMOVED LEFT MAGNETO INSPECTION AND NOTED ''POINT'' MARKS USED FOR FACTORY SEALING STILL IN PLACE INDICATING MAGNETO INTERNAL INSPECTION REVEALED OILITE BUSHING IN DISTRIBUTOR BLOCK EXCESSIVELY WORN PRODUCING A MESDR 20000508SH019Gear · brokenON CRUISE FLIGHT, LEFT ENGINE QUIT. PILOT LANDED, INVESTIGATION REVEALED BROKEN CRANKSHAFT GEAR. ENGINE RETIRED FROM SERVICE AND AND OVERHAULED ENGINE INSTALLED ON AIRCRAFT. (X)SDR CA000427011Pump · leaking(CAN) ON APPROACH, THE CREW SMELLED A FUEL SMELL AND SHUT DOWN THE HEATER AS A PRECAUTION. AFTER LANDING, MAINTENANCE PERSONNEL FOUND THE HEATER FUEL PUMP LEAKING. THE PUMP HAD LESS THAN 100 HOURS SINCE NEW.SDR 20000407SH014Beam · crackedCRACK AT FLANGE CAUSED BY NORMAL WEAR AND STRESS ON AIRCRAFT. (X)SDR AU990956Control Rod · worn(AUS) ELEVATOR CONTROL ROD WORN PAST LIMITS IN THE AREA OF THE GUIDE ROLLERS. ROD HAD BEEN ILLEGALLY REPAIRED USING METAL FILLER OR SIMILAR MATERIAL.SDR 99ZZZX2926Impulse Coupling · looseDURING INSPECTION OF MAGNETO AND IMPULSE COUPLING, FOUND ONE OF THE PAWL PINS WAS WORKING LOOSE FROM IMPULSE BODY. ALL OTHER WEAR APPEARED NORMAL. IMPULSE HAD BEEN INSPECTED 190 HOURS PRIOR AND HAD BEEN FOUND TO BE NORMAL.SDR 99ZZZX3020Bellcrank · damagedHOLES ELONGATED IN LEVER (BELLCRANK) BOTH SIDES ALLOWING EXCESSIVE PLAY IN RUDDER.SDR 99ZZZX3004Bellcrank · damagedHOLES ELONGATED IN LEVER (BELLCRANK) BOTH SIDES ALLOWING EXCESSIVE PLAY IN RUDDER.
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