N299SK, cancelled Apr 3, 2020
Service difficulty reports · 26
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 = 'N299SK' AND deregistration_id = 'N299SK-2020-04-03' 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 = 'N299SK' AND deregistration_id = 'N299SK-2020-04-03' 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 CHQA20140403102Fire Loop · faultyCREW REPORTED THAT AFTER TAKEOFF, THEY RECEIVED AN ENG 1 FIRE DETECTION FAIL MSG. THE CREW DIVERTED THE ACFT & LANDED WITHOUT FURTHER INCIDENT. REPLACED THE ENG 1 PYLON FIRE LOOP. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20130728197Engine · odorDURING FLIGHT THERE WAS AN OIL BURNING ODOR IN THE COCKPIT WHILE USING BLEED SYSTEM 1 AND BOTH PACK SYSTEMS TURNED ON. THE ODOR WAS ONLY PRESENT IN THE COCKPIT AND CLEARED ON THE GROUND WHILE USING THE APU AS A BLEED SOURCE. LANDED WITHOUT INCIDENT. MX REPSDR CHQA20130727193Unknown · odorDURING ALL PHASES OF FLIGHT, A SLIGHT OIL BURNING ODOR WAS PRESENT. MX RAN BOTH ENGINES WITH THE ENGINE BLEED AND PACK SYS TURNED ON. NO ODORS OR DEFECTS WERE NOTED AND ACFT RETURNED TO SERVICE.SDR CHQA20130625136Bulb · inoperativeDURING INSPECTION, THE OVERHEAD COCKPIT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE COCKPIT EMERGENCY LIGHT BULB. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20130504153Skin · damagedDURING INSPECTION, A TOOLING MARK ON THE INTERIOR BELLY SKIN WAS FOUND ADJACENT TO STRINGER 21L AND BETWEEN FRAMES 10 AND 11. THE SKIN WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-008436.SDR CHQA20130502162Frame · damagedDURING INSPECTION, AN ELONGATED RIVET HOLE WAS FOUND ON FRAME 12 BETWEEN STRINGERS 21R AND 20R. THE FRAME WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-008257.SDR CHQA20130502161Support · damagedDURING INSPECTION, A MISDRILLED RIVET HOLE ON THE RIGHT CONTROL CABLE QUADRANT SUPPORT. THE SUPPORT BRACKETS AND QUADRANT SUPPORT WERE REPLACED IN ACCORDANCE WITH SRM 51-40-02 AND 51-20-03.SDR CHQA20130501159Stringer · corrodedDURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21L BETWEEN FRAMES 13 AND 9. THE STRINGER WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130501158Support · corrodedDURING INSPECTION, CORROSION WAS FOUND IN THE LEFT AILERON QUADRANT SUPPORT WEB AT FRAMES 12-13 AND STRINGERS 20L-21L. THE QUADRANT SUPPORT WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130501157Support · corrodedDURING INSPECTION, CORROSION WAS FOUND IN THE RIGHT AILERON QUADRANT SUPPORT WEB AT FRAME 12 AND 13 AND STRINGERS 20R AND 21R. THE RIGHT QUADRANT SUPPORT WAS REPAIRED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130501156Stringer · corrodedDURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21R BETWEEN FRAMES 13 AND 9. THE STRINGER WAS REPLACED IAW SRM 51-40-02.SDR CHQA20130501151Floor Support · corrodedDURING INSPECTION, CORROSION AND CRACKS WERE FOUND ON THE FLOORBOARD SUPPORT FLANGE OF THE LEFT OMEGA BEAM BETWEEN FRAME 24 AND FRAME 25. THE OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10.SDR CHQA20130430160Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SHEAR CLIP AT FRAME 13 BETWEEN STRINGERS 21L AND 20L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130426155Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 65 BETWEEN STRINGERS 7L AND 9L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02 AND 53-31-04.SDR CHQA20130426154Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 73 BETWEEN STRINGER 8R AND 9R. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130426152Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP ON FRAME 66 BETWEEN STRINGERS 6L AND 7L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130426150Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND AT THE SCREW HOLE ON THE CENTER OMEGA LEFT SIDE BETWEEN FRAMES 24 AND 25. THE CENTER OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-008055.SDR CHQA20130426149Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA AT THE CARBON CROSS MEMBER FRAME 27. THE OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10.SDR CHQA20130426148Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 73 BETWEEN STRINGER 8L AND 9L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130426147Bracket · crackedDURING INSPECTION, A CRACK WAS FOUND IN THE BRACKET BETWEEN FRAME 64 AND FRAME 65 AT STRINGER 5L. THE BRACKET WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02, 51-30-01, AND 53-31-02.SDR CHQA20130426146Doubler · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE REPAIR DOUBLER LEFT OMEGA FRAME 20. THE DOUBLER WAS REPLACED IN ACCORDANCE WITH SRM 53-00-10.SDR CHQA20120428134Selector Switch · faultyCREW REPORTED, RECEIVED A BLEED 2 VALVE CLOSED MESSAGE IN FLIGHT. THE CREW FOLLOWED THE QUICK-REFERENCE HANDBOOK BUT THE VALVE WOULD NOT INDICATE OPEN. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BLEED 2 PUSHBUTTON SSDR CHQA200900164Engine · making metalFLIGHT 5356, JAX TO STL. ON DESCENT INTO STL, THE CREW HEARD A THUMP FROM THE REAR OF THE AIRCRAFT AS THRUST WAS DECREASED TO FLIGHT IDLE. A SHARP SPIKE IN E2 EGT WAS FOLLOWED BY AN E2 OUT MESSAGE ON EICAS. THE E2 OUT CHECKLIST WAS FOLLOWED ALONG WITH THE PSDR CHQA200900135Smoke Detector · faultyDURING CLIMB OUT, THE CREW RECEIVED A LAV SMOKE WARNING MESSAGE ON THE EICAS DISPLAY. THIS WAS ACCOMPANIED BY A HAZE OR SMOKE WITH CONDENSATION COMING FROM THE LAVATORY AREA AND THE PACKS BY A DEAD HEADING CREW MEMBER. THE CREW RETURNED TO DEPARTURE AND DECLSDR CHQA200900265Line · looseDURING CRUISE, THE FLIGHT CREW NOTICED AN OIL BURN RATE OF (2) QUARTS PER HOUR AND THE OIL QUANTITY OF E2 HAD DROPPED BELOW 6 QTS. THE FLIGHT DIVERTED IN ORDER TO HAVE ENOUGH OIL TO CONTINUE TO OPERATE THE ENGINE UNTIL LANDING. THE AIRCRAFT LANDED WITHOUT INSDR CHQA200500113Warning Light · activatedDURING CLIMB AT FL210, RECEIVED "AILERON SYS 1 FAIL" EICAS MESSAGE. LEVELED OFF AT FL230 AND TOLD ATC TO STAND BY. FOLLOWED QRH AND TURNED OFF AILERON SYSTEM 1 AND SLOWED TO 250 KIAS. EMERGENCY DECLARED WITH ATC AND F/A PREPARED CABIN FOR EMERGENCY LANDING.
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