Bombardier DHC-8-202
Service difficulty reports · 8,233
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 = 'DHC8202' 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 aircraft_model_key = 'DHC8202' 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 BIGA20260824001Air Duct · detachedAIRCRAFT WAS ENROUTE TO RESPOND TO A FIRE MISSION. WHILE ENROUTE THE SMOKE-JUMPER CREW SAW WHAT APPEARED TO BE SMOKE COMING FROM RIGHT AFT CABIN FLOORBOARDS. THE AIRCRAFT MADE AN UN-SCHEDULED LANDING AT GPI WITH NO INCIDENT. ONCE ON THE GROUND THE AIRCRAFT SDR 2023FA0000702Engine · power loss10/5/2023 AT AROUND 4:25 PM CST, D8-200 N805MR WAS DEPARTING MIAMI EXECUTIVE AIRPORT. AIRCRAFT WAS SET UP FOR CRUISE CLIMB WITH AUTOPILOT ENGAGED. PROP RPM 1064 AND 1058. TORQUES AT 95.5 AND 95.5%. BETWEEN 3000-4000 FEET, #2 ENGINE SPIKED TO 112.75 AND # 1 WESDR 2022FA0000214None · noneUNDETECTED, STANDING FUEL IN A WING DRY BAY WITH A BLEED AIR TUBE HAS PROMPTED THIS REPORT. THE AIRCRAFT HAS BEEN MODIFIED WITH STC ST03382NY, WHICH CONVERTS A DRY BAY IN EACH WING TO AN EXTENDED RANGE AUXILIARY FUEL TANK. AT HEAVY CHECK, ON OPENING THE ACCESSSDR HKGA20220314004Spacer · crackedBLEED SYSTEM PRSOV SPACE MOUNTING EARS FOUND CRACKED. REMOVED SPACER, REPLACED CRACKED ANGLES P/N 85531139-101 & 85531139-105. RE-INSTALLED REPAIRED SPACER.SDR HKGA20220314003Spacer · crackedBLEED SYSTEM PRSOV SPACE MOUNTING EARS FOUND CRACKED. REMOVED SPACER, REPLACED CRACKED ANGLES P/N 85531139-101 & 85531139-105. RE-INSTALLED REPAIRED SPACER.SDR HKGA20220314002Spacer · crackedBLEED SYSTEM PRSOV SPACE MOUNTING EARS FOUND CRACKED. REMOVED SPACER, REPLACED CRACKED ANGLES P/N 85531139-101 & 85531139-105. RE-INSTALLED REPAIRED SPACER.SDR HKGA20190821742Trim Tab · crackedRH ELEVATOR SPRING TAB CRACKED @ TRAILING EDGE. REMOVED AND REPLACED RH ELEVATOR SPRING TAB IAW DHC-8 MM 27-34-11.SDR HKGA201908217041Trim Tab · damagedDURING INSPECTION IT WAS FOUND THAT THE LH ELEVATOR SPRING TAB HAS A BULLET HOLE @ TRAILING EDGE. REMOVED AND REPLACED LH ELEVATOR SPRING TAB IAW DHC-8 MM 27-34-11.SDR CA190628008Switch · broken(CAN) WE HAD AN ENGINE IFSD ON MSN 522 DUE TO THE RH ENGINE SURGE BETWEEN 80% AND 120% ON FRIDAY 21/JUNE/19. PRECAUTION ENGINE SHUT DOWN WAS PERFORMED AND THE AIRCRAFT WAS SAFELY LANDED WITHOUT ANY INCIDENT: PILOT REPORT: THE ENGINE STARTED SURGING IMMEDIATELYSDR CA190605008Elevator System · malfunctioned(CAN) WHEN THE CREW ROTATED THE AIRCRAFT, THERE WERE NO RESPONSE TO PITCH CONTROL INPUT AND THE CREW ELECTED TO EXECUTE A REJECTED TAKEOFF. THE AIRCRAFT IS CONFIGURED IN A Y29 COMBI VERSION (HUNTING CARGO/COMBI 8/2822) WITH 28 ADULT AND ON CHILD + 412 KGS BAGSSDR CA190507007Tab · dented(CAN) DURING TAXI, WHILE PREFORMING THE BEFORE TAKEOFF CHECKS PRIOR TO FLIGHT, THE CREW REPORTED THE PITCH CONTROL WAS JAMMED AND THE FLIGHT WAS CANCELLED. AFTER INSPECTION OF THE FLIGHT CONTROL SURFACES, DENT DAMAGE WAS FOUND ON THE L/H ELEVATOR SPRING TAB SDR CA190503014Check Valve · cracked(CAN) DIVERSION CARRIED OUT DUE TO #2 HYDRAULIC FLUID LOSS. MAINTENANCE REPLACED BROKEN HYDRAULIC CHECK VALVE P/N: 3-1582-2-3 LOCATED IN THE TAIL SECTION AND RETURNED THE AIRCRAFT TO SERVICE. (TC# 20190503014)SDR CA190415014Starter Gen · malfunctioned(CAN) UNIT SLOW TO START. LH STARTER GENERATOR VENT HAD INDICATIONS OF SMOKE OR OIL ON COWL. FOUND DRIVE SHAFT LOOSE AND UNIT WAS MAKING SMOKE. TEAR DOWN REPORT SHOWS: ENCLOSURE BROKEN/US. D.E. BEARING FAILURE. MISSING SECTIONS OF END BELL SCREEN. C.E. BEARINGSDR CA190411016Bolt · loose(CAN) DURING PILOT PRE TAKE OFF FLIGHT CONTROL CHECK, WITH CONTROL LOCK DISENGAGED, ELEVATOR MOVEMENT RESTRICTED, UNABLE TO MOVE AFT OF NEUTRAL POSITION. AIRCRAFT RETURNED TO BAY FOR MAINTENANCE ACTION. MAINTENANCE TROUBLESHOOTING CARRIED OUT. FARING ON RH ELSDR A8ZR20181113003Firewall · crackedACCOMPLISHED DOUBLER INSTALLATION FOR CRACK ON UPPER FIREWALL WEB PN 85410554 OF #1 NACELLE RH IB SIDE AT XN 127.00 REF BOMBARDIER DEHAVILLAND RD 8-54-1565 ISSUE 3 DTD 18 FEB 04SDR A8ZR20181113002Structure · crackedACCOMPLISHED REPLACEMENT OF CRACKED CLOSING MEMBER PN 85410449 OF NR 1 NACELLE RT IB SIDE FIREWALL REF RD 8-54-611 ISSUE 4 DTD 12 APR, 2001.SDR A8ZR20181113001Firewall · crackedACCOMPLISHED DOUBLER INSTALLATION FOR CRACK ON UPPER FIREWALL WEB PN 85410554 OF NO 1 NACELLE RT IB SIDE REF RD 8-54-3940 ISSUE 1 DTD 24 MAY, 2017.SDR A8ZR20181106001Firewall · crackedACCOMPLISHED DOUBLER INSTALLATION FOR CRACK ON UPPER FIREWALL WEB PN 85410554 OF NR 2 NACELLE RT OB SIDE REF RD 8-54-3940 ISSUE 1 DTD 24 MAY, 2017.SDR A8ZR20181106002Structure · crackedACCOMPLISHED REPLACEMENT OF CRACKED CLOSING MEMBER PN 85410449 OF NR 2 NACELLE RT OB SIDE FIREWALL REF RD 8-54-611 ISSUE 4 DTD 12 APR, 2001.SDR 2018FA0000393Hydraulic Line · leakingDURING CLIMB IN VVI-SRE LEG, THE AIRCRAFT SUFFERED TOTAL LOOS OF SYSTEM NR.2 HYDRAULIC FLUID, QRF TO DEPARTURE STATION. CORRECTIVE ACTION: HYDRAULIC FLUID LOOS WAS CAUSED BY A DEFECTIVE FLEXIBLE LINE LOCATED IN NLG BAY. THE DEFECTIVE HYDRAULIC FLEXIBLE LINE WASDR 2019F00058Signal Cond Unit · failedPROPELLER OVERSPEED INDICATION ENG#1. AIRCRAFT TURN BACK TO AIRPORT AFTER SHUTTING DOWN AFFECTED ENGINE ACCORDING TO PROCEDURE. CORRECTIVE ACTION: SIGNAL CONDITIONER UNITS SWAPPED BETWEEN ENG#1 AND ENG #2. CLEANED OVERSPEED GOVERNOR SOLENOID VALVE CONNECTOR. ESDR A8ZR20180817001Skin · dentedDENT FOUND AT BS331, STRINGER 31L. REFORMED THE DENT AND CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 42-2018-061, REV. A.SDR A8ZR20180921001Light · defectiveRT FWD EMERGENCY EXIT DOOR, LT & RT UNDER WING EMERGENCY EXIT DOOR BETA LIGHTS P/N 1971001 FAILED BRIGHTNESS CHECK REF TASK CARD 3350/02 AND REPLACED REF AMM 33-51-00 REV 38.SDR A8ZR201809121005Skin · gougedACCOMPLISHED RE-SKIN ON AFT BAGGAGE DOOR UPPER SECTION THAT MEASURES 5.7" X 49.70" FOR GOUGES IN SKIN REF RD 8-52-029 ISSUE 2 DATED 2014-06-05.SDR A8ZR20180924003Light · defectiveRT FWD EMERGENCY EXIT DOOR, LT & RT UNDER WING EMERGENCY EXIT DOOR BETA LIGHTS P/N 1971001 FAILED BRIGHTNESS CHECK REF TASK CARD 3350/02 AND REPLACED REF AMM 33-51-00 REV 38.SDR A8ZR20180924002Light · defectiveRT FWD EMERGENCY EXIT DOOR, LT & RT UNDER WING EMERGENCY EXIT DOOR BETA LIGHTS P/N DSC543-1 FAILED BRIGHTNESS CHECK REF TASK CARD 3350/02 AND REPLACED REF AMM 33-51-00 REV 38.SDR A8ZR20180921003Light · defectiveRT FWD EMERGENCY EXIT DOOR, LT & RT UNDER WING EMERGENCY EXIT DOOR BETA LIGHTS P/N 1971001 FAILED BRIGHTNESS CHECK REF TASK CARD 3350/02 AND REPLACED REF AMM 33-51-00 REV 38.SDR A8ZR20180921002Light · defectiveRT FWD EMERGENCY EXIT DOOR, LT & RT UNDER WING EMERGENCY EXIT DOOR BETA LIGHTS P/N 1971001 FAILED BRIGHTNESS CHECK REF TASK CARD 3350/02 AND REPLACED REF AMM 33-51-00 REV 38.SDR A8ZR20180920001Light · defectiveRT FWD EMERGENCY EXIT DOOR, LT & RT UNDER WING EMERGENCY EXIT DOOR BETA LIGHTS P/N 1971001 FAILED BRIGHTNESS CHECK REF TASK CARD 3350/02 AND REPLACED REF AMM 33-51-00 REV 38.SDR A8ZR20180831001Light · defectiveAFT RT EMERGENCY BETA LAMP FAILED BRIGHTNESS TEST. BETA LAMP ASSY REMOVED AND REPLACED REF AMM 33-51-00 REV 38 DATED MAY 15/17.SDR A8ZR20180911002Structure · dentedACCOMPLISHED DOUBLER REPAIR AT STA 315.80 & BETWEEN S30S AND S31S FOR DENT WITH CREASE REF EA 45-2018-080 REV ORIGINAL ISSUE DATED 06/20/2018.SDR A8ZR20180823007Striker · out of limitsACCOMPLISHED RE-CONTOUR OF NR 2 ENGINE I/B COWL DOOR NACELLE STRIP-STRIKER FOR THE UPPER EDGE OF THE DOOR IAW EA 43-2018-083, REV A.SDR A8ZR20180911004Structure · dentedACCOMPLISHED DOUBLER REPAIR AT STA 213.8 & BETWEEN S16S AND S17S FOR DENT REF EA 48-2018-042 REV ORIGINAL ISSUE DATED 06/20/2018.SDR A8ZR20180830004Structure · crackedACCOMPLISHED REPLACEMENT ON MAIN AIRSTAIR DOOR AFT EDGE MEMBER UPPER SECTION FOR CRACKS, REF STS EA 32-2018-078 REV IR DATED 06/15/2018.SDR A8ZR20180830003Skin · dentedACCOMPLISHED REPLACEMENT OF DOUBLER TO UPPER SKIN ON AIRSTAIR DOOR FOR DENT, REF BOMBARDIER RD 8-52-040 ISSUE 4 DATED 2014-06-05.SDR A8ZR20180924001Light · defectiveRT FWD EMERGENCY EXIT DOOR, LT & RT UNDER WING EMERGENCY EXIT DOOR BETA LIGHTS P/N DSC543-1 FAILED BRIGHTNESS CHECK REF TASK CARD 3350/02 AND REPLACED REF AMM 33-51-00 REV 38.SDR A8ZR20180829007Skin · dentedLEFT LOWER SURFACE OF THE HORIZONTAL STABILIZER 15.5 INCHES INBD FROM OTBD EDGE AND 6.5 INCHES FWD OF AFT EDGE WAS DENTED. ACCOMPLISHED DOUBLER REPAIR IAW EA 45-2018-074, REV IR.SDR A8ZR20180828002Skin · dentedTHE FUSELAGE SKIN AT BS 240.5 BETWEEN STRINGERS 29P & 30P WAS DENTED. REPAIRED IAW EA 42-2018-040, REV A-P2.SDR A8ZR20180911001Tail Cone · delaminatedACCOMPLISHED COMPOSITE REPAIR ON LWR TAILCONE FWD AT TAIL BUMPER FOR DELAMINATION STA X806 & Z130.43 REF SRM 53-70-28 REV 6 DATED SEP 17, 2017.SDR A8ZR20180829004Skin · dentedBS 293 TO 321.85, STRINGER 24S WAS DENTED. ACCOMPLISHED A DOUBLER AND TRIPLER REPAIR IAW EA 42-2018-041, REV B.SDR 2018FA0000170Generator · failedNR 1 GENERATOR FAILURE, CYCLING ON AND OFF. CAUSED MULTIPLE SYSTEM FAILURES, TO INCLUDE AUTO PRESSURIZATION SYSTEM FAILURE. THE NR 1 DC GENERATOR LIGHT ILLUMINATED WITH AUX INVERTER LIGHT. LEFT STALL WARNING LIGHT ILLUMINATED INTERMITTENTLY. AUTOPILOT DISCONSDR A8ZR20180829006Skin · dentedSKIN DENTED AT BS 321.6, STRINGER 24S-3.5, SUCCESSFULLY REFORMED BACK TO ORIGINAL CONTOUR WITH NO INDICATIONS FOR CRACKS AND CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 42-2018-041, REV B.SDR A8ZR20180829005Skin · dentedSKIN DENTED AT BS 307.5, STRINGER 26S+1.60/ SUCCESSFULLY REFORMED BACK TO ORIGINAL CONTOUR WITH NO INDICATIONS FOR CRACKS AND CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 42-2018-041, REV B.SDR A8ZR20180829009Skin · dentedSKIN PANEL DENTED ON THE RT AILERON TRIM TAB. REPAIRED IAW SRM 51-42-45.SDR A8ZR20180829008Skin · dentedACCOMPLISHED A SKIN REPLACEMENT AND SPLICE 10.8 INCH X 1.70 INCH ON THE RT ELEVATOR SPRING TAB UPPER SURFACE, 2.5 INCHES INBD OF HINGE NR 2, 2.8 INCHES FWD OF THE T/E IAW RD 8-55-037, ISSUE 6.SDR A8ZR20180827002Skin · dentedTHREE DENTS ON THE FUSELAGE AT BS 111.5 & 121.8 AND STRINGERS 21P & 22P. REFORMED TO ORIGINAL CONTOUR, CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 43-2018-066, REV IR.SDR JJBA2018061910007Wire · out of positionLEFT EMERGENCY EXIT FORWARD EMERGENCY LIGHT WAS UNSERVICEABLE. TROUBLESHOT AND FOUND WIRES IN CONNECTORS J12 ON SIDEWALL PANEL SWAPPED. SWAPPED WIRES BACK. OPS CHECKED SATISFACTORY.SDR A8ZR201808290010Skin · dentedFUSELAGE SKIN AT BS 295, STRINGER 31S+2.8 INCHES DENTED. REPAIRED IAW EA 45-2018-067, REV ORIGINAL.SDR A8ZR20180830002Skin · dentedACCOMPLISHED DOUBLER REPAIR ON L/H AILERON UPPER SURFACE AT YW 474 & 4.7" FWD OF TRIM TAB AND YW 476 & 1" TO 6" FWD OF TRIM TAB FOR MULTIPLE DENTS REF DEHAVILLAND SRM 57-60-21 REV 6 DATED SEPTEMBER 15, 2017SDR A8ZR20180821002Skin · dentedDENT ON FUSELAGE AT STA 328.5 & S13P+6" THAT MEASURES .50"L X .9"W X .006"D SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR WITH NO OFFSETS TO MATERIAL THICKNESS. CONSIDRERED ACCEPTABLE REF STS EA 42-2018-055 REV B DATED 04/19/2018.
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