N1376G, cancelled May 29, 2020
Service difficulty reports · 21
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N1376G' AND deregistration_id = 'N1376G-2020-05-29' 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 n_number = 'N1376G' AND deregistration_id = 'N1376G-2020-05-29' 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 HYIA20191114001Fitting · corrodedDURING MAINTENANCE AN AREA OF CORROSION WAS VISUALLY IDENTIFIED ON THE TOP FACE OF THE LOWER LEG OF THE FORWARD LEFT HAND LOWER AFT WING FITTING (P/N: 0822550-43) THIS CORROSION MEASURES APPROXIMATELY .600 INCHES LONG, AND .473 INCHES WIDE WITH A MAX DEPTH OF SDR HYIA20191106002Spar Cap · corrodedDURING MAINTENANCE AN AREA OF CORROSION WAS IDENTIFIED ON THE RIGHT HAND LOWER AFT OUTBOARD SPAR CAP P/N: 5122041-24. THIS CORROSION IS LOCATED BETWEEN RIGHT WING STATIONS 223.21 AND 228.71, AND MEASURES 5.5 INCHES LONG BY .75 INCHES WIDE, AND HAS A MAX DEPTH SDR HYIA20190925003Rib · crackedDURING MAINTENANCE TWO CRACKS WERE DISCOVERED ON THE RIGHT HAND CLOSEOUT RIB (P/N: 5122115-56) AT RWS 106.79. THESE CRACKS ORIGINATE FROM A COMMON HOLE IN THE FORWARD ROW OF FASTENERS COMMON TO THE AFT MAIN LANDING GEAR TRUNNION SUPPORT PLATE. THE FIRST BEGINSSDR HYIA20190925002Rib · crackedDURING MAINTENANCE A CRACK WAS DISCOVERED ON THE LEFT HAND CLOSEOUT RIB (P/N: 5122115-55) AT LWS 106.79. THIS CRACK ORIGINATES FROM A HOLE IN THE FORWARD ROW OF FASTENERS COMMON TO THE AFT MAIN LANDING GEAR TRUNNION SUPPORT PLATE AND TRAVELS FORWARD AN APPROXISDR HYIA20171201001Socket · deterioratedDURING DESCENT FOR LANDING AT SCHEDULED DESTINATION, THE LWR PANEL LIGHT RHEOSTAT WAS ACTUATED. AFTER 2-3 SECONDS A STRONG ELECTRICAL ODOR WAS NOTED. THE PANEL LIGHTS WERE EXTINGUISHED AND THE ODOR RECEEDED. NO EMERGENCY WAS DECLARED AND THE LANDING WAS UNSDR HYIA20170828007Fitting · crackedDURING A ROUTINE INSPECTION, THREE CRACKS WERE FOUND ON THE RT OUTBOARD NACELLE FITTING. TWO OF THE CRACKS WERE FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. MEASURED .050 AND .090 IN LENGTH. THE THIRD CRACK WAS FOUND ON THE OUTBOASDR HYIA20161109196Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20161108182Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20160304001Unknown · odorPILOT REPORTED HEATER SMELL. RAN HEATER FOR 30 MINUTES, COULD NOT DUPLICATE SMELL. INSPECTED HEATER IAW MM CH 21.SDR HYIA20141001001Caliper · defectiveON PREFLIGHT PILOT REPORTED RT BRAKES INOPERATIVE, NO BRAKES ON THE RT SIDE. R & R THE RT BRAKE CALIPER & BRAKE PADS IAW MM 32-10-00. OPERATIONS CHECKED GOOD.SDR HYIA20130727001Light · faultyINSTRUMENT PANEL LIGHTS EXTINGUISHED AFTER TAKEOFF. F/O INSTRUMENT LIGHT CIRCUIT BREAKER TRIPPED FOLLOWED BY MOMENTARY PUFF OF SMOKE.SDR HYIA20130327001Skin · chafedDURING A SCHEDULED MX INSPECTION, HORIZONTAL STABILIZER WAS REMOVED WHICH REVEALED DAMAGE TO THE ACFT FUSELAGE SKIN. DAMAGE APPEARS TO HAVE BEEN CAUSED BY THE L/E OF THE HORIZONTAL STABILIZER CHAFING INTO THE FUSELAGE SKIN. DAMAGED AREA RANGED FROM FS 342.24 SDR HYIA20140415038Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, OEM PN 5142002-5, WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURESDR HYIA1376GLBEAMBeam · crackedDURING A ROUTINE SCHEDULED INSP, MX FOUND LT NACELLE INBD ENG CARRIER BEAM CRACKED. REPLACEMENT OF BEAM IN PROGRESS.SDR HYIA1376GCircuit Breaker · failedON PREFLIGHT INSPECTION, CREW REPORTED AVIONIC MASTER SWITCH INOP. CONTRACT MAINTENANCE REMOVED AND REPLACED SWITCH, SYSTEM CHECKED OK. THIS CIRCUIT BREAKER IS THE LATEST OF 36 TO BE CHANGED IN THE LAST TWO YEARS FOR PREMATURE FAILURE. ALL HAVE HAD THE SAMESDR 13505361376GCircuit Breaker · defectiveCREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH.SDR HYI2003F00006Master Switch · burnedUPON CLIMBOUT, PILOT SMELLED SMOKE, FOUND SMOKE COMING FROM AVIONICS MASTER SWITCH. PILOT NOTIFIED TOWER BEFORE SHUTTING DOWN AVIONICS SWITCH, LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED SWITCH AND RETURNED AIRCRAFT TO SERVICE.SDR 99ZZZX3741Bracket · brokenON RT ENGINE START, PILOT NOTICED SMOKE FROM RT COWL, SHUT DOWN ENGINE PER NORMAL PROCEDURE AND EVACUATED PASSENGERS. MAINTENANCE FOUND ALTERNATOR POWER CABLE CHAFED BY BROKEN ENGINE BAFFLE BRACKET. REPAIRED BRACKET, REPAIRED MINOR COWL DAMAGE, AND ALTERNATOSDR 99ZZZX1745Circuit Breaker · failedAFTER LANDING IN ACK, CREW SHUT OFF ALL EXTERNAL LIGHTS EXCEPT BELLY STROBE AND NAV LIGHTS. NOTICED SMOKE COMING FROM NAV LIGHT SWITCH/BREAKER. SHUT OFF SWITCH, TAXIED TO GATE, AND NOTIFIED MAINTENANCE. FOUND RT WING NAV LIGHT POWER WIRE SHORTED TO GROUND, SDR 97ZZZX1227Diode · burntPILOT REPORTED ARCING AND SMOKE FROM ELECTRIC HEATED WINDSHIELD. ELECTRICAL CONNECTION OR LEFT SIDE OF HEATED WINDSHIELD HAS DIODE THAT MELTED AND ARCED.SDR 97ZZZX1046Mount Beam · crackedESTIMATED CYCLES = 28,000. ESTIMATED ENGINE CHANGES = 70. LEFT ENGINE OUTBOARD BEAM FOUND CRACKED AT FORWARD MOUNT LOCATION BETWEEN NUTPLATE HOLES.
Back to N1376G, cancelled May 29, 2020