N173YV, cancelled Dec 22, 2011
Service difficulty reports · 43
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 = 'N173YV' AND deregistration_id = 'N173YV-2011-12-22' 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 = 'N173YV' AND deregistration_id = 'N173YV-2011-12-22' 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 GLBA20110218GBulb · burned outPILOT REPORTED THAT THE INSTRUMENT EMERGENCY LIGHTS ON LT SIDE WOULD NOT ILLUMINATE. MX REPLACED THE EMERGENCY LIGHT BULB PN: 1864 IAW BMM 33-10-04, OPS CK GOOD.SDR GLBA20110121FStructure · damagedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND THE LT STABILON T/E DAMAGED 1.25", 19.375" FROM FUSELAGE AND 26.75" FROM OTBD EDGE. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-55-001. MATERIALS SDR GLBA20110120GSkin · debondedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND THE AIRSTAIR DOOR LOWER INTERIOR SKIN DEBONDED 17" ALONG THE LOWER EDGE RADIATING UPWARD FROM LOWER EDGE 3.25". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. ESDR GLBA20110120FAttach Fitting · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND THE LT AILERON WEIGHT CLIP CRACKED, R & R LT AILERON TC 1900-2710.00. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 09-1900-27-002. MATERIALS UTILIZED ARE INCLUDED ISDR GLBA20100902FHandle · loosePILOT REPORTED THAT AFTER CLOSING THE AIR STAIR DOOR THE OUTSIDE HANDLE CAME OFF. MAINTENANCE REPLACED THE CABIN DOOR HANDLE SNAP RING PN MS16624-1075, REF MM 52-10-05 STEPS (A,B).SDR GLBA20100824GSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A DENT, TOP OF LEFT AILERON, 1.75" BY .75", 38.125" FROM OB EDGE AND .875" FROM TE. AND A .5" CRACK WAS FOUND RUNNING FWD TO AFT ON LOWER SKIN 37.125" FROM OB EDGE. MAINTENANCE REPAIRED THSDR GLBA20100729FFan · failedSIG EVENT - PILOT REPORTED THAT DURING FLIGHT BLOWERS AIRFLOW BECAME VERY WEAK AND A SLIGHT BURNING SMELL WAS THEN NOTICED. MX REPORTED THAT THEY REPLACED THE VENT BLOWER IAW AMM 21-20-01, PN 114-380078-11 SN OFF 558A, SN ON 57A.SDR GLBA20100617FConnector · not seatedSIG EVENT - PILOT REPORTED THAT WHEN ATTEMPTING TO EXTEND THE LANDING GEAR, GEAR DID NOT EXTEND, IN TRANSIT GEAR HANDLE LIGHT CAME ON INTERMITTANTLY, THEN EXTINGUISHED, WITH HANDLE DOWN, DID NOT RECEIVE 3 GREENS, UPON PERFORMING MANUAL EXTENDED AND RECEIVED 3 SDR GLBA200911141Wire · chafedAIR RETURN - THE PILOTS REPORTED THAT LANDING GEAR CIRCUIT BREAKER POPPED IN CRUISE AND WHICH RESULTED IN A RETURN TO "DEN". MX REPAIRED 4 CHAFED WIRES THAT WERE FOUND AT THE LT UPLOCK SWITCH HARNESS IAW AC 43-13-1B CHAPTER 11 SECTION 13. GROUND POWER WAS APSDR GLBA2009100101Line · leakingPILOTS REPORTED THE GEAR INSTRANSIT LIGHT DID NOT EXTINGUISH, LANDING GEAR RELAY CIRCUIT BREAKER POPPED AND GEAR HAD TO BE MANUALLY EXTENDED. UPON FURTHER INSPECTION AFTER LANDING THE PILOTS NOTED HYDRAULIC FLUID IN THE LEFT HAND WHEELWELL. MAINTENANCE REMOVESDR GLBA20090724GFrame · crackedDURING ROUTINE SCHEDULED MAINTENANCE A FRAME FLANGE AROUND TWO RIVETS WERE FOUND CRACKED AT FS 544.0 BETWEEN STRINGERS 12L AND 13L. CRACKS RADIATE APPROXIMATELY .250" FROM RIVET CENTER. MAINTENANCE REPAIRED THE FRAME AT FS 544.0 BETWEEN STRINGERS 12L AND 13LSDR GLBA090722001Frame · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MX, A FRAME FLANGE AROUND 2 RIVETS WERE FOUND CRACKED AT FS 544.0 BETWEEN STRINGERS 12L AND 13L. CRACKS RADIATE APPROX .250 INCH FROM RIVET CENTER.SDR GLBA20090524092Sensor · dirtyPILOTS REPORTED A STALL HEAT CAUTION ANNUNCIATOR WOULD NOT TURN OFF WITH THE SWITCH IN THE ON POSITION. MAINTENANCE CLEANED CONNECTIONS ON A1 & A2 STALL WARNING CURRENT SENSORS. FUNCTIONAL CHECKS WERE GOOD.SDR GLBA200905241Annunciator · inoperativeSTALL HEAT CAUTION ANNUNCIATOR WILL NOT TURN OFF WITH THE SWITCH IN THE ON POSITION.SDR GLBA20090430CSwitch · out of adjustCABIN DOOR ANNC CAME ON IN FLIGHT. DIVERTED TO NEAREST SUITABLE AIRPORT. MAINTENANCE TROUBLESHOT THE SYSTEM AND ADJUSTED THE FORWARD AND AFT LATCH SWITCHES.SDR GLBA200812011Autofeather Sys · malfunctionedSIGNIFICANT EVENT - FLIGHT 5128 EN ROUTE FROM PIR TO DEN DURING APPROACH INTO DENVER ON FINAL AT ABOUT 6000FT & 160KTS. THE NR 2 ENGINE AUTOFEATHERED 3 TIMES WITH TORQUE AT 1200, GEAR DOWN AND PROPS 1700 RPM. MAINTENANCE PERFORMED AN OPERATIONAL RUNUP OF THESDR GLBA200810171Rivet · missingMAJOR REPAIR - DURING ROUTING SCHEDULED MAINTENANCE A CONFORMITY INSPECTION WAS PERFORMED AND FOUR RIVETS WERE FOUND MISSING ON THE HORIZONTAL STABILIZER SPAR CENTER WEB. MAINTENANCE INSTALLED FOUR MS20470AD5 RIVETS IDENTIFIED AS "A" IN STEP 23 OF THE BEECH SSDR BSAASDR0728Tube · defectiveRIGHT BLEED FAIL ILLUMINATED IN FLIGHT. ITEM INITIALLY DEFERRED. REMOVED AND REPLACED EVA TUBING, RAN AIRCRAFT OPERATIONAL CHECK GOOD.SDR BSAASDR0727Pressure Switch · dirtyRIGHT BLEED AIR FAIL LIGHT ILLUMINATD. THE RIGHT BLEED AIR PRESSURE SWITCH WAS CLEANED AND EVA TUBING INSPECTED FOR LEAKS. AIRCRAFT RAN ON GROUND AT HIGH POWER SETTINGS. NO OTHER DEFECTS WERE NOTED.SDR BSAASDR0707Wire · chafedWHEN GEAR HANDLE WAS SELECTED DOWN, THE LANDING GEAR INDICATION CD TRIPPED. CREW ABORTED LANDING AND FOLLOWED EMERGENCY PROCEDURES. CREW VERIFIED GEAR WAS DOWN AND LOCKED. A CHAFED WIRE WAS FOUND UNDER THE FLOOR BY THE PCB RACKS, WIRE NR D14B22. WIRE WAS RSDR BSAASDR0620Spar Cap · corrodedPITTING CORROSION WAS FOUND IN LT WING JUST AFT OF WING DRAIN ON THE FWD FACE OF THE MAIN SPAR CAP FROM WS125 TO 128, AND ON THE RIB JUST IB OF THE WING DRAIN. PITTING CORROSION WAS ALSO FOUND IN THE RT WING IN THE SAME LOCATION ON THE FWD FACE OF THE MAIN SPSDR BSAASDR0619Latch · malfunctionedDURING CRUISE, A PASSENGER REPORTED TO THE CREW THAT THE RT FWD COWLING HAD COME LOOSE. WHEN THE CREW LANDED, THEY NOTED A YAW UPON TOUCHDOWN. THE IB FWD COWL LATCH HAD COME LOOSE FIRST, ALLOWING THE COWLING TO CONTACT THE SPINNER SCREWS. THE IB AFT COWL LATCHSDR BSAASDR0602Windscreen · crackedTHE LEFT COCKPIT WINDSHIELD INNER PANE CRACKED DURING CRUISE AS FL230, OAT WAS -40, WINDSHIELD HEAT WAS ON AT THE TIME, AIRCRAFT WAS NOT IN ICING CONDITIONS AT THE TIME, FLIGHT CONDITIONS WERE VFR. CREW LANDED WITH NO FURTHER INCIDENT. THE WINDSHIELD WAS CHASDR BSAASDR0601Switch · malfunctionedDURING CLIMB-OUT, CARGO DOOR OPEN ANNUNCIATOR WARNING LIGHT CAME ON AS CREW ASCENDED THROUGH 12,000 FT. CREW RETURNED TO STATION. THE CARGO DOOR OPEN LIGHT WAS INITIALLY DEFERRED IAW THE MEL, AND ACFT WAS RETURNED TO SERVICE. DEFERRAL WAS CLEARED BY ADJUSTISDR 1050617008AMWPanel · failedLEFT WING UPPER BIN EVIDENCE OF DEFORMATION AT TURTLE BACK MOUNT FLANGE AREA. REPAIRED IAW SR-CO-00024. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE.SDR 1050617009Frame · crackedCENTER CANTED FRAME AT FS 588. LEFT FLANGE CRACKED AT NUT PLATE AND RIVET, STRINGER 7L AND 8L. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE.SDR 1050617008Flange · wornLT UPPER TURTLEBACK FLANGE WORN. CRACKED ON IB EDGE. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE.SDR 10506017007Frame · corrodedCORROSION FOUND ON INSPECTION FOR ABC STRUCTURAL FS 213.25. MORE INFORMATION TO BE ADDED AT A LATER DATE.SDR 62683Valve · malfunctionedLANDING GEAR FAILED TO EXTEND ON FIRST ATTEMPT. GEAR FINALLY EXTENDED ON THE SECOND ATTEMPT. REMOVED AND REPLACED HYD SERVICE VALVE. OPS CK GOOD.SDR 62587Control Handle · malfunctionedON APPROACH TO LANDING. THE FIRST AND SECOND ATTEMPTS TO EXTEND LANDING GEAR FAILED. CREW WIGGLED HANDLE AND GOT GEAR TO EXTEND WITH ALL GEAR INDICATING DOWN LOCK. LANDED SAFELY WITH NO FURTHER INCIDENT. REMOVED AND REPLACED LANDING GEAR HANDLE. OPS CK GOOD.SDR 62453Handle · unsecureCREW NOTICED EMERGENGY EXIT HANDLE STICK OUT WAY FROM FUSELAGE MX RESEATED EXIT. REMOVED AND INSP LT EXIT DOOR REINSTALLED AND SECURED.SDR 62001Fire Loop · faultyRT FIRE LOOP ANNUNCIATOR ILLUMINATED IN FLIGHT AND REMAINED ON. FLIGHT CREW LANDED AND TAXIED TO THE GATE WITH NO FURTHER INCIDENT. NO EMERGENCY DECLARED. NO EQUIPMENT INVOLVED OR REQUIRED. T/S RT ENG FIRELOOP. REMOVED AND REPLACED FIRELOOP.SDR 60135Pressure Switch · malfunctionedUPON GETTING READY TO LAND IN PKB. CREW EXTENDED LANDING GEAR WITH CAUSE LANDING GEAR C/B TO POP AND NOT RESET. CREW CALLED AND DID A FLY BY TO VERIFY GEAR WAS DOWN. TOWER CALLED OUT EQUIPMENT AND THEY LANDED SAFELY WITH NO FURTHER INCIDENT THERE. R/R JACK AC/SDR 56653Handle · stuckWHEN LANDING GEAR WAS PLACED IN DOWN POSITION LANDING GEAR FAILED TO EXTEND GEAR MANUALLY PUMPED DOWN IND THREE GREENS ACFT LANDED WITH NO FURTHER INCIDENT...CAUSE OF PROBLEM WAS CONTROL, LANDING GEAR HANDLE. WE HAVE RR LDG GEAR SELECTOR HANDLE. P/N 101384137SDR 56120Switch · dirtyDURING LANDING APPROACH MAIN LANDING GEARS FAILED TO EXTEND. THE CREW MANUALLY PUMPED DOWN THE GEARS. RECEIVED 3 GREEN INDICATIONS, LANDED WITH NO FURTHER INCIDENTS. CLEANED CONTACT ON SERVICE VALVE SWITCH.SDR 55265Landing Gear · failedUPON DECENT FOR LANDING IN MCO. GEAR WOULD NOT EXTEND. IT HAD TO BE EMERGENCY EXTENDED (PUMPED DOWN) CREW GOT THREE DOWN AND LOCKED IND AHD SAFETY WITH NO FURTHER INCIDENTS.SDR 55265AMWALanding Gear · malfunctionedUPON DECENT FOR LANDING IN MCO. GEAR WOULD NOT EXTEND IT HAD TO BE EMERGENCY EXTENDED (PUMPED DOWN). CREW GOT THREE DOWN AND LOCKED INDICATIONS AND LANDING SAFETY WITH NO FURTHER INCIDENTS. P/N 1143640681 S/N506D95 PCB TIME DELAY RELAY.SDR 51904Lead · looseON FLIGHT 5517, DURING THE FLIGHT THE RIGHT ENGINE ITT WENT TO 1000 DEGREES CELSIUS THEN WENT BACK TO NORMAL. SHORTLY THERE AFTER THE ITT AGAIN WENT TO 1000 DEGREES CELSIUS AND STAYED THERE. THE CREW REDUCED POWER ON THE RIGHT ENGINE AND RETURNED TO AIRPORT WISDR 045518Circuit Breaker · trippedUPON ARRIVAL, THE MAIN LANDING GEAR WOULD NOT EXTEND TO NORMAL OPERATION. AFTER NOTICING THAT THE CIRCUIT BREAKER HAD POPPED, THE CREW RESET IT THREE TIMES, AFTER THE THIRD RESETTING THE CIRCUIT BREAKER STAYED. IT SHOWED 3 GREENS WITH NO RED HANDLE. THE AIRCSDR MASA99111Fuel Pump · failedFLT 5906 - PIT-FKL - AFTER TAKEOFF, THE AIRCRAFT EXPERIENCED A FUEL PUMP FAILURE ON THE NR 1 ENGINE. THE CREW DECLARED AN EMERGENCY, AND RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION WAS DEFERRED PER MEL 28-5. THE AIRCRAFT WAS RETURNED SDR MASA98164Cam Locks · out of adjustDUJ/PIT - FLT 5954 - CREW REPORTED THE PASSENGER DOOR CAMLOCKS WOULD NOT LATCH COMPLETELY. MAINTENANCE RIGGED THE DOOR CAMLOCKS, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (X)SDR 97ZZZX3236Attach Bracket · excess wearFLEET CAMPAIGN, 'MAINTENANCE INSPECTED THE LT AND RT OTBD FLAP ATTACHMENT BRACKETS AND THE AFT ROLLER BEARING IAW RAYTHEON ACFT CO (RAC) SAFETY COMMUNIQUE NR 137 DATED MAY, 1997. FOUND ATTACHMENT BRACKETS WITH EXCESSIVE WEAR AND AFT ROLLER BEARINGS BINDING. SDR 97ZZZX3235Attach Bracket · excess wearFLEET CAMPAIGN, 'MAINTENANCE INSPECTED THE LT AND RT OTBD FLAP ATTACHMENT BRACKETS AND THE AFT ROLLER BEARING IAW RAYTHEON ACFT CO (RAC) SAFETY COMMUNIQUE NR 137 DATED MAY, 1997. FOUND ATTACHMENT BRACKETS WITH EXCESSIVE WEAR AND AFT ROLLER BEARINGS BINDING.
Back to N173YV, cancelled Dec 22, 2011