N42836, cancelled Jun 26, 2019
Service difficulty reports · 146
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 = 'N42836' AND deregistration_id = 'N42836-2019-06-26' 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 = 'N42836' AND deregistration_id = 'N42836-2019-06-26' 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 HYIA20180222001Hub · damagedDURING ROUTINE BLADE CHANGE DISCOVERED DAMAGE AT BLADE ROOT AND PROPELLER HUB, REMOVED PROPELLER ASSEMBLY FOR FURTHER INVESTIGATION. ADDITIONAL RESULTS TO BE SUPPLIED AS AVAILABLE.SDR HYIA20160624001Bulb · failedON CLIMBOUT, CREW SMELLED BURNING ODOR, APPEARED TO BE COMING FROM WEMAC VENTS. MAINTENANCE INSPECTED THE ACFT LIGHTING SYSTEM AND FOUND THE LIGHT SOCKET ON ROW 5-AB LATERAL LIGHT BULB PINS TO BE ARCED TO SOCKET. MAINTENANCE R & R THE SOCKET AND LAMP IAW SPMSDR HYIA20160108002Fitting · failedPILOT REPORTED WHEN THE GEAR WAS RETRACTED ON DEPARTURE THERE WAS AN UNUSUAL NOISE, GEAR WAS EXTENDED, THE WHOLE PLANE SHOOK & A LOUD NOISE CAME FROM THE RT SIDE. THE RT GEAR TOOK EXTREMELY LONG TO EXTEND. INSPECTED & FOUND THE EXTEND & RETRACT ACTUATOR TO FSDR HYIA20160108001Fan · defectivePILOT REPORTED ON APPROACH TO LAND, RECIRCULATION FAN NR 2 FAULTED, BEFORE FAULT THERE WAS A UNIQUE SMELL. REMOVED & INSTALLED NR 2 RECIRCULATION FAN IAW 42 AMM JIC 21-22-21 RAI 10000. OPERATIONALLY TESTED GOOD IAW 21-22-21-OPT-00100. NO DISTINCTIVE SMELL NSDR HYIA20141217003Spar · corrodedTEMPORARY REPAIR PERFORMED TO RT WING FWD SPAR LOWER CHORD IAW ENGINEERING STRUCTURAL REPAIR INSTRUCTION DT S-6990 14-23433 DATED NOV 18, 2014. ACFT WILL BE FERRIED WHERE IT WILL UNDERGO HEAVY CHECK & THE PERMANENT REPAIR WILL BE ACCOMPLISHED. SEE ATTACHED DSDR HYIA20141114001Controller · dirtyEXCESS CABIN ALTITUDE, REPORTED THEY EXPERIENCED A CABIN DEPRESSURIZATION APPROXIMATELY 45 MILES AWAY FROM DESTINATION ON INITIAL DESCENT. THE CREW THEN DONNED O2 MASKS & FOLLOWED THE QRH & DECLARED AN EMER. LANDING WAS UNEVENTFUL. THE TOWER REPORTED THE CSDR HYIA20141006001Battery · malfunctionedPILOT REPORTED MAIN BATTERY OFF LIGHT ILLUMINATED IN FLIGHT & NOTICED A BURNING SMELL IN COCKPIT. INSPECTED ALL ELEC POWER SYS. REMOVED & INSTALLED MAIN BATTERY, BATTERY CHARGE CONTACTOR, BATTERY PROTECTION UNIT & MAIN BATTERY CHARGE PUSH BUTTON SWITCH IAW ASDR HYIA20141002001Symbol Generator · faultedFIRST OFFICER`S SIDE EFIS & SGU FAIL FOLLOWED BY INTERMITTENT AHRS FAILURE. AHRS FAIL INCLUDED RADIO ATT GOING TO ZERO WITH GEAR NOT DOWN WARNING. BURNING SMELL BRIEFLY ACCOMPANIED ABNORMALITY. SMELL WAS BRIEF, 30 SEC & APPROX HALFWAY THROUGH ABNORMALITY. SDR HYIA20140725001Battery · defectiveMAIN BATTERY CHARGE OFF LIGHT ILLUMINATED. MX PANEL MAIN BATTERY VOLTS SHOWED 18 VOLTS THEN READ 29. HOWEVER, LIGHT REMAINED ILLUMINATED UNTIL DESCENT 10000 FEET. STRONG BURNING SMELL IN FLIGHT DECK. MX REPLACED MAIN BATTERY. OPERATIONS TEST MAIN BATTERY PSDR HYIA20130928001Power Supply · dischargedEMERGENCY EXIT LIGHTS DO NOT ALL ILLUMINATE DURING TEST. REPLACED POWER SUPPLY UNITS 3WL, 10WL, 15WL, 18WL, 29WL.SDR HYIA201307290001Wire · brokenLANDING GEAR WOULD NOT EXTEND NORMALLY. THREE RED UNLOCKED INDICATORS REMAINED ILLUMINATED AFTER SELECTING GEAR DOWN. PERFORMED EMERGENCY LANDING GEAR EXTENSION. GEAR CAME DOWN NORMALLY AND 3 GREEN DOWN AND LOCKED INDICATION WITH NO RED UNLOCK LIGHTS ILLUMISDR HYIA201305280001Vent Line · cloggedON TAXI TO GATE, COCKPIT STARTED TO FILL WITH SMOKE. SELECTED BOTH BLEEDS AND BOTH PACKS TO OFF. INSPECTED NR 1 ENGINE NR 5 BEARING VENT TUBE. CLEANED CLOGGED VENT TUBE. PERFORMED ENGINE RUNUP AND FOUND TO OPERATE NORMALLY.SDR HYIA20121205002Access Door · departedPILOT REPORTED THAT WHILE CONDUCTING A POST FLIGHT REVIEW OF THE ACFT, THEY NOTED THAT THE HYD BAY ACCESS DOOR 195CL HAD DEPARTED THE ACFT IN FLIGHT. UPON MX INSPECTION, THE DOOR WAS REPLACED.SDR HYIA20111031001Spar Cap · corrodedDURING HEAVY CHECK CORROSION ZL-532-GVI-10000, 572220-DVI-10000, SPOTS WERE FOUND ON LT WING AT AFT SPAR UPPER CAP VERTICAL FLANGE BETWEEN RIBS 24-26. CORROSION WAS REMOVED AND DAMAGES BLENDED IAW PREVIOUS SRI. REVIEWED REPAIRS AND ISSUED STRUCTURAL REPAIR ASDR HYIA836HC201121Floorbeam · damagedDURING HEAVY CHECK FLOORBEAM FR13 WAS BEING REPLACED. DURING THE INSTALLATION THE OEM DESIGNED CONTROL CABLE GUIDE THROUGH-HLOES WERE ACCIDENTALLY DRILLED ON THE WRONG (OPPOSITE) SIDE OF THE BL0. REPAIRED IAW STS EA 09-2011-227. REPAIR PERFORMED BY TECH SERSDR HYIA836HC201120Beam · crackedDURING HEAVY CHECK OVERSIZED HOLES FOUND IN NR1 ENGINE LOWER COWL BEAM AT OIL LINE SUPPORT BRACKET ATTACH POINT. IN ADDITION TO OVERSIZED AND ELONGATED HOLES, THE MATERAL BETWEEN HOLES WAS FOUND TO BE CRACKED, WITH CRACKS TERMINATING AT EACH HOLE. REPAIRED ISDR HYIA836HC201113AFrame · crackedDURING HEAVY CHECK A CRACK WAS FOUND ON THE LT SIDE OF UPPER FRAME 28. REPAIRED IAW EA 12-2011-010. REPAIR PERFORMED BY TECH SERVICES (MRO) UNDER W/O 17010. DTA EVALUATION TO BE ACCOMPLISHED WITHIN 12 MONTHS IAW AC120-93.SDR HYIA20111027004Skin · corrodedCORROSION WAS FOUND ON LOWER SKIN AT FRAME 31. CORROSION WAS REMOVED IAW SRM 51-21-58 AND FOUND TO BE OUT OF LIMITS. REPAIRED IAW EA 12-2011-018. REPAIR PERFORMED BY TECH SERVICES UNDER W/O 17010. DTA EVALUATION TO BE ACCOMPLISHED WITH IN 12 MONTHS IAW AC 12SDR HYIA836HC201119Frame · damagedDURING HEAVY CHECK, RT SPONSON FRAME WAS DAMAGED. SPONSON FRAME WAS REPAIRED IAW EA 09/2011-184. REPAIR PERFORMED BY TECH SERVICE (MRO) UNDER W/O 17077.SDR HYIA836HC201118Structure · debondedDURING HEAVY CHECK THE TRANSVERSE LAVATORY WALL WAS FOUND WITH A LARGE AREA OF DISBOND. WALL REPAIRED IAW EA 14-2011-003. REPAIRS PERFORMED BY TECH SERVICE (MRO) COMPOSITE SHOP UNDER W/O 17010.SDR HYIA836HC201117Panel · debondedDURING HEAVY CHECK THE LONGITUDINAL LAVATORY WALL WAS FOUND WITH A LARGE AREA OF DISBOND. WALL REPAIRED IAW STS ENGINEERING SOLUTIONS EA 14-2011-003. REPAIRS PERFORMED BY TECH SERVICE (MRO)COMPOSITE SHOP UNDER W/O 17010.SDR HYIA836HC201116Cowling · crackedDURING HEAVY CHECK A CRACK WAS FOUND ON A BEAM IN THE LT LOWER ENGINE COWLING. THE DAMAGE CONSISTS OF A SINGLE CRACK 1.8" LONG THAT RUNS BETWEEN 2 LIGHTNING HOLES IN THE BEAM. THE CRACK WAS REPAIRED IAW STS ENGINEERING SOLUTIONS EA 12-2011-013. REPAIR PERFORSDR HYIA836HC201115Sink · crackedDURING HEAVY CHECK LAVATORY WASH BASIN WAS FOUND TO BE CRACKED. THE DAMAGE CONSISTS OF 4 CRACKS. DAMAGE REPAIRED IAW STS ENGINEERING SOLUTIONS EA 12-2011-022. REPAIR PERFORMED BY TECH SERVICE (MRO) UNDER W/O 17010.SDR HYIA836HC201114Skin · corrodedDURING HEAVY CHECK CORROSION WAS FOUND ON LOWER SKIN AT FRAME 31. CORROSION WAS REMOVED IAW SRM 51-21-58 AND FOUND TO BE OUT OF LIMITS. REPAIRED IAW STS ENGINEERING SOLUTIONS EA 12-2011-018. REPAIR PERFORMED BY TECH SERVICE (MRO) UNDER W/O 17010.SDR HYIA836HC201113Frame · crackedDURING HEAVY CHECK A CRACK WAS FOUND ON THE LT SIDE OF THE UPPER FRAME 28. THE DAMAGE CONSISTS OF A SINGLE CRACK THAT STARTS MIDWAY DOWN THE WEB RUNNING 1.6" THROUGH A .098" HOLE AND INTO THE AFT FACING FLANGE 0.6". REPAIRED IAW STS ENGINEERING SOLUTIONS EA 1SDR HYIA836HC201112Panel · delaminatedDURING HEAVY CHECK NR1 OTBD LATERAL PANEL WAS FOUND TO HAVE A LARGE DELAMINATION OVER THE CORE. PANEL REPAIRED IAW STS ENGINEERING SOLUTIONS EA 12-2011-023. REPAIR PERFORMED BY COMPOSITE SHOP UNDER W/O 17010.SDR HYIA836HC201111Panel · crackedDURING HEAVY CHECK, TOILET COMPARTMENT PANEL NR261EW FOUND CRACKED IN 3 PLACES. PANEL REPAIRED IAW STS EA 12-2011-020. REPAIR PERFORMED BY COMPOSITE SHOP UNDER W/O 17010.SDR HYIA836HC201110Panel · crackedDURING HEAVY CHECK SEVERAL CRACKS FOUND ON THE FACE OF INTERIOR PANEL NR261DW. PANEL WAS REPAIRED IAW STS EA 12-2011-019. REPAIR PERFORMED BY ACFT TECH SERVICES (MRO) COMPOSITE SHOP UNDER W/O 17010.SDR HYIA836HC201109Tube · chafedDURING HEAVY CHECK, NR1 ENGINE NR7 MOUNT TUBE FOUND CHAFED. BLENDED IAW ATR 42-320, SRM 54-21-00. ORIGNAL THICKNESS OF TUBE IS .0632", THICKNESS AFTER BLENDING IS .0551" AND WITH IN LIMITS. WORK PERFORMED BY ACFT TECH SERVICE UNDER W/O 17010.SDR HYIA836HC201108Skin · corrodedDURING HEAVY CHECK CORROSION FOUND ON EXTERIOR SURFACE OF FORWARD KEEL SKIN AT RT ECS CUTOUT. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM. REPAIR PREFORMED IAW STS ENGINEERING SOULTIONS EA 12-2011-43. REPAIR PERFORMED BY TECH SERVICES UNDER W/O 17SDR HYIA836HC201107Skin · corrodedDURING HEAVY CHECK CORROSION FOUND ON EXTERIOR SURFACE OF LT FWD KEEL SKIN AT THE LT ECS CUT OUT. REMOVED CORROSION IAW SRM 51-21-58 AND FOUND TO BE OUT OF LIMITS. REPAIRED IAW STS ENGINEERING SOLUTIONS EA 12-2011-041. REPAIR PERFORMED UNDER W/O 17010.SDR HYIA20111026005Skin · corrodedDURING HEAVY CHECK, CORROSION WAS FOUND ON LOWER SKIN AT FRAME 45. REPAIRED IAW STS EA 12-2011-017, REV A. REPAIR PERFORMED BY TECH SERVICES UNDER W/O 17010. DTA TO BE ACCOMPLISHED WITHIN 12 MONTHS IAW AC 120-93.SDR HYIA20111026003Skin · corrodedDURING HEAVY CHECK COROSION WAS FOUND ON THE LOWER SKIN AT VHF2 ANTENNA LOCATION. THE CORROSION WAS REMOVED IAW SRM 51-21-58 AND FOUND TO BE OUT OF LIMITS. REPAIR DOUBLER FABRICATED AND INSP IAW STS ENGINEERING SOLUTIONS EA 12-2011-012. REPAIRS PERFORMED BYSDR HYIA836HC201106Skin · corrodedDURING HEAVY CHECK, CORROSION WAS FOUND ON LOWER SKIN AT FRAME 45 BETWEEN STRINGERS 20R AND 20L. CORROSION WAS REMOVED IAW SRM 51-21-58 AND FOUND TO BE OUT OF LIMITS. DOUBLER FABRICATED AND INSTALLED IAW STS ENGINEERING SOLUTIONS EA 12-2011-017. REPAIR PERFORSDR HYIA836HC201105Skin · corrodedDURING HEAVY CHECK CORROSION WAS FOUND ON THE LOWER SKIN AT VHF2 ANTENNA LOCATION. THE CORROSION WAS REMOVED IAW SRM 51-21-58 AND FOUND TO BE OUT OF LIMITS. REPAIR DOUBLER FABRICATED AND INSTALLED IAW STS ENGINEERING SOLUTIONS EA 12-2011-012. REPAIR PERFORMSDR HYIA20111025001Skin · damagedDURING HEAVY CHECK INSP, LT AND RT FUSELAGE SKIN WAS DAMAGED BY DRILL MARKS BETWEEN FRAMES 39 TO 42 BELOW STRINGER 14. DAMAGE EXCEED LIMITATIONS. SUBMITTED INFORMATION WHICH ISSUED S.R.I. DO/TS-5488/11-16116 FOR REPAIR SPECIFICATIONS. DAMAGED SKIN WAS CUT OUSDR HYIA20111024001Frame · corrodedDURING HEAVY CHECK INSPECTION, CORROSION WAS FOUND ON MLG FAIRING RT WEB SEGMENT AT FRAME 29. CORROSION WAS OUT OF LIMITS PER THE SRM 51-21-58. CORRODED FRAME WAS CUT OUT AND NEW PORTION SPLICED IN.SDR HYIA201110200002Spar · corrodedLT WING-AFT SPAR LOWER CAP HORIZ FLANGE CORROSION BETWEEN RIBS 18-19. DAMAGE BEYOND THE LIMITS IAW THE SRM. DAMAGED SPAR CAP REPLACED IAW REPAIR.SDR HYIA20111020001Floor Panel · puncturedDURING HEAVY CHECK, FLOOR PANEL 222CZ REMOVED FOR MX. FOUND IMPACT DAMAGE AND 2 PUNCTURES IN THE FLOOR PANEL. 1 WAS 0.5 " IN LENGTH AND SECOND 1.0" IN LENGTH. REPAIRED IAW EA 12-2011-021.SDR HYIA2011101900001Skin · crackedDURING MX, PASSENGER DOOR INTERIOR SKIN WAS FOUND CRACKED, APPROX 2.25" IN LENGTH RUNNING IN THE UP/DOWN DIRECTION. CRACK THRU INNER SKIN
ONLY. REPAIRED IAW STS EA 10-2011-088.SDR HYIA20111019001Skin · corrodedDURING HEAVY CHECK, CORROSION WAS FOUND ON THE EMERGENCY HATCH INNER SKIN AFT OF FRAME 9 AT STA 5136, INBD OF STRINGER 2R. CORROSION REMOVED IAW SRM 51-21-58 AND EXCEEDED THE LIMITS OF THE SRM. THE DAMAGE CONSISTS OF A .50" DIA HOLE IN THE INNER SKIN. REPAIRSDR HYIA20111013007Panel · crackedDURING HEAVY CHECK INSP, LT BASEBOARD DADO PANELS 241DW WERE FOUND TO HAVE SMALL CRACKS ALONG THE BOTTOM AND MISSING MATERIAL THAT WERE BEYOND SRM LIMITS. REPAIRS WERE MADE TO THE PANELS UNDER EA 09-2011-257.SDR HYIA20111013006Panel · crackedDURING HEAVY CHECK INSP, RT BASEBOARD DADO PANELS 252CW, 252AW, AND 242EW WERE FOUND TO HAVE SMALL CRACK ALONG THE BOTTOM THAT WERE BEYOND SRM LIMITS. REPAIRS WERE MADE TO THE PANELS UNDER EA 09-2011-260.SDR HYIA20111013005Panel · crackedDURING HEAVY CHECK INSP, LT BASEBOARD DADO PANELS 231FW, AND 2231JW WERE FOUND TO HAVE SMALL CRACKS ALONG THE BOTTOM AND UPPER ANGLE THAT WERE BEYOND SRM LIMITS. REPAIRS WERE MADE TO THE PANELS UNDER EA 09-2011-259.SDR HYIA20111013004Panel · crackedDURING HEAVY CHECK INSP, RT BASEBOARD DADO PANELS 232FW,232JW, AND 242AW WERE FOUND TO HAVE SMALL CRACK ALONG THE BOTTOM THAT WERE BEYOND SRM LIMITS. REPAIRS WERE MADE TO THE PANELS UNDER EA 09-2011-258.SDR HYIA20111013003Panel · crackedDURING HEAVY CHECK INSP, LT BASEBOARD DADO PANELS 251AW, 251CW, AND 251EW WERE FOUND TO HAVE SMALL CRACK ALONG THE BOTTOM AND MISSING THAT WERE BEYOND SRM LIMITS. REQUEST FOR REPAIRS WERE SUBMITTED TO STS ENGINEERING SOLUTIONS. REPAIRS WERE MADE TO THE PANELSSDR HYIA20111013002Panel · crackedDURING HEAVY CHECK INSP, RT BASEBOARD DADO PANELS 242DW AND 242AW WERE FOUND TO HAVE SMALL CRACK ALONG THE BOTTOM THAT WERE BEYOND SRM LIMITS. REQUEST FOR REPAIRS WERE SUBMITTED TO STS ENGINEERING SOLUTIONS. REPAIRS WERE MADE TO THE PANELS UNDER EA 09-2011-2SDR HYIA20110927002Spar Cap · corrodedDURING HEAVY CHECK INSP RT WING AFT SPAR UPPER CAP WAS CORRODED REF:ZL-632-GVI-10000/572220-DVI-10000 BEYOND LIMITS IAW THE SRM 57-22-00. DAMAGE WAS SUBMITTED THEN ISSUED S.R.I. DO/TS-3027/11-15459. REPAIR WAS PERFORMED BY TECH SERVICES UNDER W/O 17010, TASKSDR HYIA20110923001Skin · corrodedDURING HEAVY CHECK INSP, CORROSION WAS FOUND ON LT WING LOWER SKIN AT AFT SPAR NEAR RIBS 6-7. CORROSION WAS REMOVED AND BLENDED IAW SRI REF: DP/TS-3-3/11-15470 BY TECH SERVICES UNDER W/O 17010. APPROVED UNDER STRUCTURAL REPAIR APPROVAL SHEET (SRAS) DO/TS-303SDR HYIA20110922001Skin · corrodedDURING HEAVY CHECK INSPECTION, CORROSION WAS FOUND ON LT WING LOWER SKIN AT AFT SPAR NEAR RIBS 4 AND 7. CORROSION WAS REMOVED AND BLENDED IAW SRI REF: DP/TS-3-3/11-15470 BY TECH SERVICES UNDER W/O 17010. APPROVED UNDER STRUCTURAL REPAIR APPROVAL SHEET (SRAS)
Back to N42836, cancelled Jun 26, 2019