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 = '1900D' 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 = '1900D' 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 CA070912007Flex Drive · seized(CAN) ABOUT 2 MINUTES INTO A FLIGHT THE CREW DETECTED AN ELECTRICAL ODOR. THE PILOTS TURNED OFF THE VENT BLOWER SYS WHICH HELPED FOR A BIT BUT NOT LONG. NO SMOKE WAS NOTICED, JUST THE ODOR. ALL OTHER NON-ESSENTIAL ELECTRICS WERE TURNED OFF. THE SMELL STAYED SSDR GUUA09080701Bolt · brokenDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT MLG UPPER ATTACH BOLT BROKEN. REPLACED LT MAIN LANDING GEAR UPPER DRAG LEG ATTACH BOLT, AIRFRAME FITTING AND DRAG BRACE ASSEMBLY.SDR S2YA07007Angle · crackedDURING STRUCTURAL INSPECTION OF THE AIRCRAFT, A CRACK WAS FOUND IN THE RIGHT HAND FUSELAGE TO WING ANGLE P/N 114-43002-180 AND THE DOUBLER INSTALLED IN AUGUST OF 2000. THE ANGLE HAD BEEN PREVIOUSLY REPAIRED, RECORDED AND SUBMITTED ON A 337 DATED 08/15/00. THSDR S2YA07006Angle · crackedDURING STRUCTURAL INSPECTION OF THE AIRCRAFT, A CRACK WAS FOUND IN THE LT FUSELAGE TO WING ANGLE. THE ANGLE IS LOCATED NEAR FS 288 IN THE AREA OF STRINGER 10L AND 10R. THE ANGLE WAS CRACKED IN THE RADIUS AT THE FORWARD END: THE CRACK WAS NO GREATER THEN 1.80 SDR S2YA07005Seat Track · crackedDURING STRUCTURAL INSPECTION OF THE AIRCRAFT, A CRACK WAS FOUND IN A SEAT TRACK EXTRUSION. THE SEAT TRACK IS LOCATED AT FS 290.85 EXTENDING APPROXIMATELY 5 INCHES. THE DAMAGE CONSISTED OF A HALF-INCH CRACK IN THE LOWER VERTICAL FLANGE WHERE THE UPPER PORTION OSDR GUUA09050701Uplock Switch · out of adjustFLIGHT: 9243 NAS/FLL, DURING FLIGHT LANDING GEAR RED UNSAFE LIGHT FLICKERED SEVERAL TIMES. ADJUSTED LEFT LANDING GEAR UPLOCK SWITCH. OPERATIONAL CHECK NORMAL.SDR CA070906007Gearbox · worn(CAN) FLAPS WOULD NOT RETRACT AFTER LANDING. GEARBOX FOUND EXCESSIVELY WORN. (TC NR 20070906007)SDR CR33955Bearing · brokenPROPELLER BLADE MAIN BEARING BROKEN IN HUB SOCKET. BEARING RETURNED TO BIG SKY AIRLINES FOR REVIEW.SDR GLBA20060992Angle · crackedRT HEAVY ANGLE CRACKED APPROXIMATELY 1.5 INCHES AT FS 288.0. MAINTENANCE INSTALLED DOUBLER ON RT HEAVY ANGLE IAW. SRM 53-90-23. REPAIR APPROXIMATELY 13.8 INCHES IN LENGTH FROM NEW HEAVY ANGLE.SDR GLBA20060991Frame · crackedFRAME CRACKED AT FS 177.35 APPROXIMATELY 1 INCH AT CUTOUT FOR STRINGER 9R. MAINTENANCE REPAIRED CRACK AT STRINGER RELIEF HOLE 9R AT F.S. 177.35 IAW SRM 51-70. REPAIR APPROXIMATELY 5.5 INCH BY 2.5 INCH. 2024 T3, .080. RII COMPLIED WITH IAW TASKCARD 8.2.1.SDR CA071003024Oil System · fluctuates(CAN) ON APPROACH, ENGINE OIL PRESSURE WAS SEEN TO FLUCTUATE AND THE ENGINE WAS SHUTDOWN IN FLIGHT. MFG WILL MONITOR INVESTIGATION OF THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20071003024)SDR GUUA08240701Unknown · unknownFLIGHT: 9136 FLL/EYW AFTER TAKEOFF, THE LANDING GEAR HANDLE LIGHT REMAINED ILLUMINATED WITH THE LANDING GEAR RETRACTED. RETURNED TO FLL. LANDED WITHOUT INCIDENT. PERFORMED LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECKS NORMAL.SDR GLBA20060990Skin · corrodedUPON ROUTINE INSPECTION MAINTENANCE FOUND CORROSION ON RT SIDE OF BELLY AT FS 228.25 FROM BUTTLINE 2.25 RT TO BUTTLINE 5.0 RT APPROXIMATELY 1 INCH WIDE. MAINTENANCE REMOVED APPROXIMATELY 6 INCH BY 12 INCH AREA OF SKIN AT FS 228.25 TO REMOVE CORROSION AND INSTSDR GLBA20060988Spar · crackedMAJOR REPAIR - UPON ROUTINE INSPECTION THE HORIZONTAL STABILIZER SPAR WEB WAS FOUND TO HAVE TWO CRACKS RADIATING FROM DEICE TUBE HOLE APPROXIMATELY 1/4 INCH & 1/2 INCH. MAINTENANCE REPAIRED MAIN SPAR CENTER WEB ON HORIZONTAL STAB I.A.W. BEECH 1900D SRM 55-91. SDR GUUA08220702Bracket · corrodedAT SCHEDULED INSPECTION DISCOVERED LOWER RUDDER ATTACH BRACKET EXFOLIATED. REPLACED LOWER RUDDER BRACKET.SDR GUUA08220701Bracket · corrodedAT SCHEDULED INSPECTION DISCOVERED UPPER RUDDER ATTACH BRACKET EXFOLIATED. REPLACED UPPER RUDDER BRACKET.SDR AMWA25033GFrame · chafedFUSELAGE FRAME HAD FRICTION CHAFING. REPAIRED IAW ENGINEERING REPORT 6829-1SDR AMWA25033FFrame · chafedFUSELAGE FRAME HAD FRICTION CHAFING. REPAIRED IAW ENGINEERING REPORT 6829-1.SDR AMWA25033EFrame · chafedFUSELAGE FRAME HAD FRICTION CHAFING. REPAIRED IAW ENGINEERING REPORT 6829-1.SDR AMWA25033DFrame · chafedFUSELAGE FRAME HAD FRICTION CHAFING. REPAIRED IAW ENGINEERING REPORT 6829-1.SDR AMWA25033CFrame · chafedFUSELAGE FRAME HAD FRICTION CHAFING. REPAIRED IAW ENGINEERING REPORT 6829-1.SDR AMWA25033BFrame · chafedFUSELAGE FRAME HAS FRICTION CHAFING. REPAIRED IAW ENGINEERING REPORT 6829-1.SDR AMWA25033AFrame · chafedFUSELAGE FRAME HAD FRICTION CHAFING. REPAIRED IAW ENGINEERING REPORT 6829-1.SDR AMWA25033IFrame · chafedFUSELAGE FRAME DAMAGED BY CHAFING. REPAIRED IAW ENGINEERING REPORT 6829-2, REV 1R DATED AUG 1, 2007.SDR AMWA25033HFrame · chafedFUSELAGE FRAME HAD FRICTION CHAFING. REPAIRED IAW ENGINEERING REPORT 6829-2.SDR AMWA25032Spar · damagedRT MAIN SPAR FASTENERS NEAR BL 114.250 AND WS 124.588 HAD (2) OVERSIZED FASTENERS. REPAIRED IAW REPAIR DRAWING 1900UE 159-1 REV 1R, DATED AUGUST 14, 2007.SDR GUUA08210701Unknown · unknownFLIGHT: 9142 MIA/EYW DURING APPROACH, LANDING GEAR CIRCUIT BREAKER POPPED WHEN GEAR HANDLE MOVED TO THE DOWN POSITION. CONTINUED TO EYW LANDED WITHOUT INCIDENT. PERFORMED LANDING GEAR OPERATIONAL CHECK SEVERAL TIMES UNABLE TO DUPLICATE.SDR GLBA20060981Angle · crackedMAJOR REPAIR - LT HEAVY ANGLE CRACKED AT F.S. 288. APPROXIMATELY 2 INCHES IN LENGTH. MAINTENANCE REPAIRED THE LT HEAVY ANGLE AT F.S. 288.0 I.A.W. BEECH 1900D SRM 53-90. REPAIR APPROXIMATELY 13 INCHES.SDR GLBA2006980Angle · crackedMAJOR REPAIR - RT HEAVY ANGLE CRACKED AT F.S. 288. MAINTENANCE REPAIRED R/H HEAVY ANGLE AT F.S. 288. IAW BEECH 1900 SRM 53-90. REPAIR LENGTH APPROX 13 1/2 INCHES. RII C/W IAW TASKCARD 8.2.1.SDR GLBA20060979Frame · crackedMAJOR REPAIR - FUSELAGE FRAME CRACKED AT F.S. 177.35 RT STRINGER 9 AT RELIEF HOLE. MAINTENANCE STOP DRILLED AND PATCHED AFFECTED AREAS I.A.W. BEECH SRM 51-70. PATCH DIMENSIONS 3 INCH BY 2.4 INCH. .080 2024 T3 . RII COMPLIED WITH PER TASKCARD 8.2.1.SDR GUUA08200701Uplock Switch · out of adjustFLIGHT:9197 TPA/FLL - DURING FLIGHT, LANDING GEAR HANDLE LIGHT FLICKERS ON AND OFF. ADJUSTED LEFT MAIN LANDING GEAR UPLOCK SWITCH OPERATIONAL CHECK NORMAL.SDR GUUA08190701Unknown · unknownDURING APPROACH LANDING, GEAR WOULD NOT EXTEND WHEN GEAR HANDLE SELECTED DOWN, DIVERTED. MANUALLY EXTENDED LANDING GEAR. LANDED WITHOUT INCIDENT. TROUBLESHOT SYSTEM COULD NOT DUPLICATE OPERATIONAL CHECK NORMAL.SDR ERAA200700003Unknown · odorSTRONG BURNING SMELL AT FL190 AND LIGHT SMOKE OBSERVED BY CREW & PAX. RETURNED TO ANC. VISUALLY INSPECTED WIRING & CONNECTIONS AT WINDSHIELD PANELS, CB PANELS, OVERHEAD SWITCH PANELS. NO DEFECTS NOTED. UNABLE TO DUPLICATE DISCREPANCY AT EXTENSIVE GROUND RUSDR AMWA86756BCBattery · false activationBATTERY CHARGE ANNUNCIATOR ILLUMINATED WHEN GEAR WAS EXTENDED AND THEN EXTINGUISHED. AC LANDED WITH NO FURTHER INCIDENT. THIS BATTERY CHARGE ANNUNCIATOR WRITEUP IS A NUISANCE WRITEUP AND DISTRACTION TO THE CREW. COULD NOT DUPLICATE ON GROUND, OPS CHECKS NORSDR AMWA86724BCBattery · false indicationDURING A FERRY FLIGHT, THE BATTERY CHARGE ANNUNCIATOR ILLUM IN FLT. ACFT LANDED WITH NO FURTHER INCIDENT. THIS IS A NUISANCE WRITEUP AND DISTRACTION TO THE AIR CREW. RAN ACFT, SYSTEM OPS CHECKED NORMAL, COULD NOT DUPLICATE.SDR GLBA20060986Spar · crackedMAJOR REPAIR - HORIZONTAL STAB SPAR WEB CRACKED AROUND DE-ICE TUBE HOLE. MAINTENANCE REPAIRED HORZONTAL STAB SPAR WEB I.A.W. BEECH 1900D SRM 55-91. REPAIR APPROXIMATELY 5 3/4 INCHE BY 4 3/4 INCH. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.SDR NSVA20070213Unknown · malfunctionedAUTOFEATHER SYSTEM WILL NOT ARM. FOUND CIRCUIT BREAKER POPPED, CLEANED SOLENOID AND LUBRICATED. RAN A/C IAW BEECH MM 61-21-00. OPS CHECK GOOD, NO FAULTS NOTED.
SDR NSVA20070214Actuator · malfunctionedAIRCRAFT IS PITCHING UP AND DOWN UNCOMMANDED. REQUIRES EXCESSIVE FORCE ON CONTROL WHEEL TO MAINTAIN DESIRED PITCH, EVEN WITH ELECTRIC TRIM DISCONNECTED. REMOVED AND REPLACED ELECTRIC ELEVATOR TRIM TAB ACTUATOR IAW REPS AIRLINER 1900D M/M 27-30-07-201. PERFOSDR GLBA20060984Skin · canningEVIDENCE OF OIL CANNING PRESENT AT FS 202.25 2 INCHES FROM CENTER OF REPAIR TO STRINGER 15 R APPROXIMATELY 2 INCHES SQUARE. MAINTENANCE REPAIRED AFFECTED AREA IAW SRM 51-70. INSERTION PATCH DIMENSION APPROXIMATELY 2 INCH X 2 INCH WITH REPAIR APPROXIMATELY 4.5 SDR GUUA08140701Attach Bracket · corrodedAT SCHEDULED INSPECTION DISCOVERED TOP RUDDER ATTACH BRACKET EXFOLIATED. REPLACED TOP RUDDER BRACKET.SDR GLBA20060985Hinge · crackedMAINTENANCE DISCOVERED BOTH CARGO DOOR HINGES CRACKED. MAINTENANCE REMOVED AND REPLACED CARGO DOOR HINGES IAW EO 05-02 . DOOR HINGE PN 129-440049-1. FUSELAGE PN 129-440049-3.SDR GLBA20060983Stringer · cracked(2) CRACKS FOUND ON STRINGER 10R AT F.S. 451.0. FORWARD CRACK .5625 INCH LONG AFT CRACK .2500 INCH LONG. MAINTENANCE REPAIRED CRACKS ON STRINGER 10R AT F.S. 451.0 IAW SRM 51-70. REPAIR APPROXIMATELY 9 INCHES LONG. RII INSPECTION COMPLIED IAW TASKCARD 8.2.1.SDR GLBA20060982Angle · crackedRT HEAVY ANGLE CRACKED AT RADIUS AT FS 288. CRACK IS APPROXIMATELY 2.2500 INCH LONG. MAINTENANCE REPAIRED THE RT HEAVY ANGLE IAW SRM 53-90. REPAIR APPOXIMATELY 13.5 INCHES. RII INSPECTION COMPLIED WITH IAW TASKCARD 8.2.1.SDR GLBA20060987Stringer · crackedFRAME CRACKED AT STRINGER 9R RELIEF HOLE ON FRAME AT F.S. 163.975. MAINTENANCE REPAIRED THE AFFECTED AREA AT FS 163.975 IAW SRM 51-70. REPAIR APPROXIMATELY 5 INCH BY 2INCH. RII INSPECTION COMPLIED WITH IAW TASKCARD 8.2.1.SDR GUUA08120701Unknown · odorFLIGHT:9249 DURING FLIGHT MILD CHEMICAL ODOR LIKE HYDRAULIC FLUID COMING THRU THE ENVIRONMENTAL SYSTEM. PERFORMED OPERATIONAL CHECK OF THE ENVIRONMENTAL SYSTEM COULD NOT DUPLICATE. OPERATIONAL CHECK GOOD.SDR GLBA20060975Shim · crackedBELLY SHIM CRACKED AT RT FS 298 TO FS 300 APPROXIMATELY 8.5 INCHES AFT OF WING SPAR. CRACK LENGTH APPROXIMATELY 1.7500 INCHES. MAINTENANCE INSTALLED PRESSURIZED COVER PATCH AT AFFECTED AREA IAW SRM 51-70. RII INSPECTION COMPLIED WITH IAW TASKCARD 8.2.1.SDR GUUA08080701Squat Switch · looseFLIGHT: 9223 AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. ADJUSTED RT MAIN LANDING GEAR SQUAT SWITCH. LANDING GEAR OPERATIONAL CHECK NORMAL.SDR AMWA86534Brake · weakWHEN AIRCRAFT LANDED CREW CALLED MAINT CONTROL AND WROTE BRAKES UP AS BEING SPONGY. MAINTENANCE BLED BRAKES, OPS NORMAL.SDR CA070808003Windscreen · cracked(CAN) ON CLIMBOUT, PILOTS WINDSCREEN SHATTERED/CRACKED. DEVIATED TO ANOTHER AND DEPLANED PASSENGERS. THE PILOTS INSPECTED THE WINDSCREENS AND DECIDED, BASED ON INFORMATION PROVIDED BY MAINTENANCE, OUT OF MM CHAPTER 5, THAT IT WOULD BE ACCEPTABLE TO FERRY FORSDR AMWA86499Rod · brokenON APPROACH TO GRI, CAPT PEDALS LOST RUDDER CONTROL. CAPT TRANSFERRED CONTROL OF THE ACFT TO THE FO. FO PEDALS HAD RUDDER CONTROL. FO LANDED WITH NO FURTHER INCIDENT. OCCURENCE REPORT FILED. REMOVED AND REPLACED RUDDER INTERCONNECT ROD (ROD END), RIGGED R
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