Aircraft model · Fixed wing single engine · Airplane · registry code 056234W

Manufacturer (registry)
MORTON ROBERT
Model
BC12-D
Registry code
056234W
Registered
1 aircraft
Type
Fixed wing single engine
Engines
1 · 4 cycle
Seats
2
Weight class
Up to 12,499 lb
Certification
Not type certificated

Model codes come from the FAA registry’s reference file. ADs are matched to them by model name and maker.

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Airworthiness directives that may apply · 0

ADs whose products match this airframe model. Each AD’s applicability may narrow it by serial number, part number or configuration.

No ADs matched this model

Registered aircraft · 1

Query with SQL
duckdb -csv -c "SELECT n_number, serial_number, year_manufactured, status, registrant_name, registrant_city, registrant_state
  FROM 'https://openairdocs.org/data/latest/faa_aircraft_registration.parquet'
  WHERE aircraft_model_code IN ('056234W')
  ORDER BY n_number"

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.

NTSB investigations

No NTSB investigations matched to aircraft with this modelMatched through the registry by N-number, so foreign aircraft and some older cases aren’t counted.

FAA incident reports

No reports matched to aircraft of this modelMatched through the registry by N-number, so foreign aircraft and some older reports aren’t counted.

Service difficulty reports · 9

SDR 2021FA0000262Ring Assembly · wornLOSS OF COMPRESSION AND OIL ON #2 CYLINDER DUE TO WORN PISTON RINGS WITH 35 HOURS SINCE OVERHAULED CYLINDER WITH NEW RINGS GAPPED TO .014. *NOT FOUND IN AIRCRAFT INQUIRYSep 20, 2021 · N5075 · Tcraft BC12D · Engine (Reciprocating)SDR 2011FA0000496Spar · crackedFOUND SAFETY ISSUES WITH ALL FOUR WING SPARS ON THIS AIRCRAFT. THE WOODEN SPARS HAD SEVERAL CRACKS AND VARIOUS OTHER DEFECTS. I HAVE ALSO E-MAILED PICTURES OF SOME OF THE MORE NOTICEABLE AREAS. THIS AIRCRAFT WAS RECENTLY RESTORED AND NEW FABRIC WAS INSTALLED OAug 2, 2011 · N95885 · Tcraft BC12D · Wing SparSDR 2011FA0000299Strut · mismanufacturedMECHANIC REPORTED TO FSDO THAT THEY HAD PURCHASED AIRFRAME SEALED FRONT LIFT STRUTS, STC NR SA02300AK, PN AF-MA-A815 REPLACEMENT STRUTS THAT SATISFY AD 2007-16-14, ACTION 4, REPLACEMENT AND AD 2008-04-09 BY USING AN FAA APPROVED EQUIVALENT SEALED STRUT. AFTEMay 10, 2011 · N43036 · Tcraft BC12D · Wing Main, Frame StructureSDR CA071204011Attach Fitting · broken(CAN) WHILE INSTALLING NEW STRUTS IAW APPLICABLE STC, THE LT REAR ATTACH FITTING SEPERATED (BROKE IN HALF) AS VERY SLIGHT DOWNWARD PRESSURE WAS APPLIED TO THE LIFT STRUT. INSPECTION OF THE FAILED PART SHOWED A PRE EXISTING CRACK UNDER THE LOCKNUT. (TC NR 2007Nov 23, 2007 · Tcraft BC12D · Fuselage, Landing Gear Attach FittingsSDR 2007FA0000324Plate · looseWHEN BRAKES WERE APPLIED AFTER LANDING. IT APPEARS THAT THE PINS HOLD THE BACK PLATE ALLOW IT TO SHIFT ENOUGH TO HAVE POSSIBLY MADE CONTACT WITH THE BRAKE ACCUATOR ARM AND NOT ALLOW IT TO RELEASE. (K)Mar 17, 2007 · N43336 · Tcraft BC12D · Landing Gear Brake SystemSDR 2006FA0000658Nozzle · crackedDURING MAINTENANCE THE MECHANIC WAS REPLACING THE FUEL INJECTION NOZZLES DUE TO THE REQUEST OF THE OWNER. THE OWNER WANTED TO INSTALL A NEW KIT THE POSITION-TUNED FUEL INJECTION NOZZLES IAW THE ID SID05-7. DURING THE INSTALLATION OF THESE NOZZLES 1 CRACKED PJul 10, 2006 · N716B · Tcraft BC12D · Fuel Injector NozzleSDR 2004FA0000910Screw · brokenWHILE REMOVING THE JURY STRUTS BEFORE REMOVING THE WINGS FOR RECOVER, WHEN THE BOLT HOLDING THE JURY STRUT TO THE ADJUSTING SCREW AT THE FRONT SPAR WAS REMOVED THE ADJUSTING SCREW WAS IN TWO PIECES. THE EAR THAT IS WELDED TO THE SCREW BROKE JUST ABOVE THE WELNov 7, 2004 · N5031M · Tcraft BC12D · Wing Miscellaneous StructureSDR 95195Control Cable · brokenLEFT BRAKE PEDAL CABLE BROKE APPROXIMATELY 10 INCHES AFT OF BRAKE PEDAL.Oct 17, 2003 · N95195 · Tcraft BC12D · Landing Gear Brake SystemSDR 95ZZZX5040Fairlead · excess wearSLOT WORN IN BOTH LEFT AND RIGHT REAR CABLE GUIDES WITH SOME STRAND WEAR ON CABLES. RUDDER CABLES ARE BOTH ROUTED THROUGH 3 FAIRLEADS IN AFT PORTION OF FUSELAGE WITH PROMINENT DEFLECTION AT AFT LEAD. TOTAL TIME, 1,800 HOURS. SUBMITTER SUGGESTS CHECKING WEARAug 28, 1995 · N96539 · Tcraft BC12D · Rudder Control System
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 = 'BC12D'
  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.

The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

Query with SQL
duckdb -csv -c "SELECT m.code, m.manufacturer, m.model, count(g.n_number) AS aircraft
  FROM 'https://openairdocs.org/data/latest/faa_aircraft_model.parquet' m LEFT JOIN 'https://openairdocs.org/data/latest/faa_aircraft_registration.parquet' g ON g.aircraft_model_code = m.code
  WHERE m.match_key = 'BC12D' AND m.code NOT IN ('056234W')
  GROUP BY ALL
  ORDER BY aircraft DESC
  LIMIT 12"

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.