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.

SDR 2024FA0000009Brake Caliper · leakingLOOSE BRAKE DURING TAXI.HYDRAULIC LEAK FOUND ON LEFT INBOARD BRAKE PACKINGS.Jan 8, 2024 · N861VL · Bnorm BN2A26 · Hydraulic System, MainSDR 2024FA0000008Brake Caliper · leakingLOOSE BRAKE DURING TAXI.HYDRAULIC LEAK FOUND ON LEFT INBOARD BRAKE PACKINGS.Jan 8, 2024 · N861VL · Bnorm BN2A26 · Hydraulic System, MainSDR 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 AREAMay 18, 2023 · N902VL · Bnorm BN2A26 · Wing, Plate/SkinSDR 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.Jan 28, 2023 · N907GD · Bnorm BN2A26 · Engine (Reciprocating)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.Apr 28, 2021 · N404WB · Bnorm BN2A26 · Magneto/DistributorSDR UOIA2017080300001Caliper · brokenRIGHT BRAKE FAILED TO OPERATED, THE AIRCRAFT GO OUT OF RUNWAY.Aug 3, 2017 · N906GD · Bnorm BN2A26 · Landing Gear Brake SystemSDR UOIA20170803Rudder · inoperativeDURING FLIGHT RUDDERS STOPPED RESPONDING.Mar 8, 2017 · N906GD · Bnorm BN2A26 · Rudder Control SystemSDR UOIA201510071114Stud · brokenLEFT ENG CYLINDER NR 3 CRANKCASE STUDS BROKEN.Oct 6, 2015 · N906GD · Bnorm BN2A26 · Reciprocating Engine Power SectionSDR RI9A20150809001Starter · bindingBENDIX ON STARTER OF RT ENGINE FAILED TO DISENGAGE AFTER STARTUP. R & R STARTER WITH NEW. NO FURTHER DISCREPANCIES NOTED.Aug 3, 2015 · N5891V · Bnorm BN2A26 · Engine StarterSDR LU4R2015020618118Blade · crackedPROPELLER BLADE FOUND CRACKED AT SHANK.Feb 3, 2015 · N908GD · Bnorm BN2A26 · Propeller Blade SectionSDR 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 CDec 22, 2014 · N5891V · Bnorm BN2A26 · Reciprocating Engine Power SectionSDR UOI2014F00000Indicator · overheatedSMOKE IN THE COCKPIT. LT ENG CLUSTER OIL TEMP INSTRUMENT OVERHEAT.Feb 13, 2014 · N906GD · Bnorm BN2A26 · Engine Oil TemperatureSDR UOI2013F00001Cylinder · brokenDURING FLIGHT, ENG SHUTDOWN. ENG CYLINDER BROKEN.Oct 1, 2013 · N901GD · Bnorm BN2A26 · Reciprocating Engine Cylinder SectionSDR UOI2013F00000Caliper · leakingBRAKE CALIPER LT SIDE, LEAKING.Jun 24, 2013 · N907GD · Bnorm BN2A26 · Landing Gear Brake SystemSDR 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. AFTERAug 5, 2012 · N5891V · Bnorm BN2A26 · Reciprocating Engine Power SectionSDR 2012FA0000558Caliper · leakingLEFT MAIN LANDING GEAR INBD BRAKE CALIPER, LEAKING.Jul 17, 2012 · N906GD · Bnorm BN2A26 · Landing Gear Brake SystemSDR 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 SMOKJun 6, 2012 · N5891V · Bnorm BN2A26 · DC RegulatorSDR 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 ANFeb 20, 2012 · N2233Z · Bnorm BN2A26 · Reciprocating Engine Power SectionSDR 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 CYFeb 18, 2011 · N779KS · Bnorm BN2A26 · Reciprocating Engine Cylinder SectionSDR UOI2011F00000Drive Assy · worn(ENGINE INTERNAL) PROPELLER GOVERNOR DRIVE DAMAGE.Dec 31, 2010 · N908GD · Bnorm BN2A26 · Propeller GovernorSDR 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 THJul 23, 2010 · Bnorm BN2A26 · Magneto/DistributorSDR 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)Jul 7, 2009 · N903VL · Bnorm BN2A26 · Rudder Control SystemSDR 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.Jan 18, 2009 · Bnorm BN2A26 · Engine Air Intake SystemSDR 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 OVERHJun 3, 2008 · Bnorm BN2A26 · Trailing Edge Flap ActuatorSDR 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)Jan 30, 2007 · Bnorm BN2A26 · Steering UnitSDR 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 CLEAVLJun 13, 2006 · Bnorm BN2A26 · Wheel/Ski/FloatSDR 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.Apr 6, 2005 · N29884 · Bnorm BN2A26 · Fuselage, Landing Gear Attach FittingsSDR CA050427006Rod · brokenDURING TAXI NOTICED RUDDER PEDALS SLOPPY, UPON INSP DISCOVERED RUDDER BAR DRIVE ROD BROKEN.Apr 3, 2005 · Bnorm BN2A26 · Rudder Control SystemSDR 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 IJan 23, 2005 · Bnorm BN2A26 · Reciprocating Engine Cylinder SectionSDR AUS20040502Washer · missing(AUS) THROTTLE QUADRANT FRICTION ADJUSTER WASHER MISSING. FOUND DURING INSPECTION IAW AD/BN2/69 AND SB 272.Jun 1, 2004 · Bnorm BN2A26 · Power LeverSDR AUS20040320Shaft · sheared(AUS) RT ENGINE PROPELLER GOVERNOR DRIVESHAFT SHEARED IN AREA LEVEL WITH THE MOUNTING FACE.Apr 27, 2004 · Bnorm BN2A26 · Propeller GovernorSDR AUS20030786Rib · cracked(AUS) ELEVATOR END RIB CRACKED. FOUND DURING INSPECTION IAW SB-190.Jul 28, 2003 · Bnorm BN2A26 · Elevator, Spar/RibSDR AUS20021181Bracket · worn(AUS) ELEVATOR OUTBOARD HINGE BRACKET WORN AND RIVETS LOOSE. FOUNDDURING INSPECTION IAW AD/BN2/70 AND BN2/SB259.Oct 11, 2002 · Bnorm BN2A26 · Elevator Tab, Attach FittingsSDR AUS20020123Brush Block · shorted(AUS) ALTERNATOR BRUSHES SHORTING BETWEEN THE SLIP RINGS AND ALTERNATOR SLIP RING END BEARING.Feb 11, 2002 · Bnorm BN2A26 · DC Generator-AlternatorSDR AUS20011400Clamp · mismanufactured(AUS) GASCOLATOR FILTER BOWL UNSECURELY CLAMPED. INVESTIGATION FOUND INADEQUATE DEPTH OF HOLE PREVENTED FULL ENGAGEMENT OF ONE LEG OFTHE SADDLE CLAMP.Aug 4, 2001 · Bnorm BN2A26 · Aircraft Fuel Filter/StrainerSDR AU010044Control Cable · seized(AUS) RT PROPELLER CSU CONTROL CABLE OUTER CONDUIT WORN THROUGH WITHTHE INNER CABLE CATCHING ON THE WORN AREA. CONTROL SEIZED.Jan 10, 2001 · Bnorm BN2A26 · Propeller Controlling SystemSDR AU010043Cable · misinstalled(AUS) ENGINE MIXTURE CONTROL INNER CABLE ONLY ENGAGED IN THE ENGINE CONTROL END BY APPROXIMATELY 1.5 TURNS.Jan 5, 2001 · Bnorm BN2A26 · Mixture ControlSDR AU010042Cable · loose(AUS) ENGINE THROTTLE CABLE OUTER CONDUIT DISCONNECTED AT FIREWALL. THE NUT SECURING THE CONDUIT HAD NO LOCKWIRE.Jan 4, 2001 · Bnorm BN2A26 · Power LeverSDR 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 INTERNALNov 6, 2000 · N903VL · Bnorm BN2A26 · Propeller GovernorSDR 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)Sep 28, 2000 · N904VL · Bnorm BN2A26 · Accessory GearboxesSDR 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 RMay 25, 2000 · Bnorm BN2A26 · Rudder, Spar/RibSDR 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)May 1, 2000 · N678TA · Bnorm BN2A26 · Reciprocating Engine Cylinder SectionSDR 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 MEApr 25, 2000 · N999SA · Bnorm BN2A26 · Magneto/DistributorSDR 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)Apr 14, 2000 · N678TA · Bnorm BN2A26 · Reciprocating Engine Rear SectionSDR 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.Mar 5, 2000 · Bnorm BN2A26 · Heating SystemSDR 20000407SH014Beam · crackedCRACK AT FLANGE CAUSED BY NORMAL WEAR AND STRESS ON AIRCRAFT. (X)Feb 24, 2000 · N29884 · Bnorm BN2A26 · Rudder Control SystemSDR 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.Aug 26, 1999 · Bnorm BN2A26 · Elevator Control SystemSDR 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.Jul 12, 1999 · N999SA · Bnorm BN2A26 · Magneto/DistributorSDR 99ZZZX3020Bellcrank · damagedHOLES ELONGATED IN LEVER (BELLCRANK) BOTH SIDES ALLOWING EXCESSIVE PLAY IN RUDDER.Jul 1, 1999 · N29884 · Bnorm BN2A26 · Rudder Control SystemSDR 99ZZZX3004Bellcrank · damagedHOLES ELONGATED IN LEVER (BELLCRANK) BOTH SIDES ALLOWING EXCESSIVE PLAY IN RUDDER.Jul 1, 1999 · N29884 · Bnorm BN2A26 · Rudder Control System
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