N309UP
Service difficulty reports · 172
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 = 'N309UP' AND registry_match = 'registration' 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 = 'N309UP' AND registry_match = 'registration' 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 IPXA09655124Circuit Card · damagedINSPECTION TYPE:ETOP ATB - WHILE CLIMBING OUT, CREW RECEIVED RIGHT BLEED DUCT EICAS MESSAGE. NO EMERGENCY WAS DECLARED. ACFT OOS T/S IN PROGRESS. REMOVED AND REPLACED DETECTOR CARD PER AMM 26-10-01-4. T/S RT BLEED DUCT LEAK CAUTION EICAS MESSAGE. FOUND ELSDR IPXA09655039Skin · damagedINSPECTION TYPE:N/A FUSELAGE SKIN DAMAGED AT STA 654+58 STR 32R. REMOVED DAMAGE AND REPAIRED IAW EO B767-5330-32729-A.SDR IPXA09655038Skin · damagedINSPECTION TYPE:N/A FUSELAGE SKIN DAMAGE DUE TO LIGHTNING STRIKE AT STA 654 AND STRINGER 32R. REMOVED DAMAGE AND REPAIRED IAW EO B757-5330-32682-B.SDR IPXA09655922Floor Panel · dentedMCD CENTER FLOOR PANEL HAS LONG DENT IN PANELS. ACCOMPLISHED PERMANENT REPAIR PER EO B767-5320-9693-F. PERMANENT REPAIR ACCOMPLISHED AT NEXT C CHECK.SDR IPXA09654817Circuit Card · not seatedINSPECTION TYPE:ETOP ATB - RIGHT BLEED SYSTEM DUCT LEAK. A/C IS CURRENTLY OOS. CHECK CARRIED OUT PER TASK PER FIM 26-18-00 AND FOLLOWED WDM 26-18-21. NOTICED CARD M691 NOT SEATED PROPERLY. SAME RESEATED C/W TASK 26-18-00 TEST PASSED. PERFORMED ENGINE RUN SDR UPS09654817Duct · leakingINSPECTION TYPE:ETOP ATB - RIGHT BLEED SYSTEM DUCT LEAK. A/C IS CURRENTLY OOS.SDR UPS07650507A/C Pack · inoperativeINSPECTION TYPE:ETOP RIGHT SYSTEM DUCT PSI LOW, IN FLIGHT AT FL 290 RIGHT DUCT PSI WAS 10 LEFT PACK OFF AIRCRAFT WAS NOT MAINTAINING CABIN ALTITUDE. RECONNECTED HPC ELECTRICAL CONNECTOR. REF MM 36-11-00-5. REPLACED PRSOV PER MM 36-11-09-2. OPS CHECKED SYSTEM,SDR UPS07650456Anti-Ice Valve · malfunctionedINSPECTION TYPE:ETOP EICAS MESSAGE RIGHT ENGINE ANTI-ICE DISPLAYED AND VALVE LIGHT REMAINED ILLUMINATED WITH SWITCH ON. EXTINGUISHED WHEN POWER INCREASED AFTER SEVERAL ATTEMPTS. REMOVED AND REPLACED RIGHT ANTI-ICE VALVE, OPS CHECK GOOD PER 30-21-03-0.SDR UPS07650197Fitting · misinstalledINSPECTION TYPE:SIP LEFT PYLON AFT PITCH LOAD FITTING HAS SHORT EDGE MARGIN. FABBED RADIUS FILLER FROM 7075-T7351. LOCATED, DRILLED & REAMED TO FINAL SIZE. VERIFIED RADIUS FILLER LIES FLAT AS BACKUP FITTING. ALODINED & PRIMED RADIUS FILLER PER ER 07-2696. SDR UPS07650196Skin · gougedINSPECTION TYPE:2C LEFT ENGINE PYLON SKIN GOUGED. BLENDED BOTH GOUGES. BOTH BLENDS OUT OF LIMIT. HFEC INSPECTION BLENDED AREAS, NO CRACKS FOUND. DRILLED DOUBLER PER SRM 54-52-01-2. ALODINED & PRIMED DOUBLER & BLENDED AREAS. INSTALLED DOUBLER. INSTALLED SDR UPS07648824Controller · malfunctionedUNABLE TO PRESSURIZE AIRCRAFT. FOUND NO POWER ON BOTH CONTROLLERS. RE-ESTABLISH AIRFLOW IN E/E CABIN PRESS CONTROLLERS. FOUND "AC POWER LOSS" AND "NO AIR FLOW" BITE FAULTS ON BOTH CONTROLLERS. C/O VERIFICATION AGAIN AND FOUND BOTH NO FAULTS. RESET BOTH COSDR UPS06648780Seal · broken4TH DESCENT DEVICE FROM FWD TO AFT SEAL BROKEN AT CABLE. REMOVED 4TH DESCENT DEVICE. INSTALLED PER MM 25-61-03-2.SDR UPS06648781Seal · brokenINSPECTION TYPE:N/A 2ND DESCENT DEVICE FROM FWD TO AFT SEAL AT CABLE IS BROKEN. REMOVED AND REPLACED 2ND DESCENT DEVICE PER MM 25-61-03-2.SDR UPS06647723Engine · shutdownETOP IN-FLIGHT SHUTDOWN, RT ENGINE SHUTDOWN DUE TO HIGH OIL TEMP. (OPEN)SDR UPS06647695Battery Pack · inoperativeEMERGENCY EXIT LTS INOP DURING CHECK. REPLACED EMERGENCY LT BATTERY PACK ASSY IAW MM 33-51-07. OPS CK GOOD.SDR UPS05645819Hmu · malfunctionedATB - CRUISING AT FL340 MACH .82 LEFT ENG ROLLED BACK TO APPROX 65 PERCENT N1 FF 3.0 SAT WAS -57 OVER THE NEXT 20 MINUTES EXPERIENCED SIX MORE ROLL BACKS WITH REDUCTIONS OF N1 FROM 5% TO 60% ALL OTHER INSTRUMENTS INDICATED ROLL BACKS. REMOVED AND REPLACED HMUSDR UPS04643387Smoke Goggles · damaged3 SMOKE GOGGLES NOT USABLE DUE TO STRETCHED STRAPS. REPLACED THREE SMOKE GOGGLES ON SEAT, THIS CLEARED DEFERRAL M289838.SDR UPS01636986O-Ring · leakingRT ENG OIL QTY DROPPING IN FLIGHT. CHIP DETECTOR "O" RING BAD R/R SAME. NR 2 ENG NR 6 BEARING CARBON SEAL REPLACED IAW MAINTENANCE MANUAL 72-53-03 C AOL FOR GROUND RUN. REPLACE CARBON SEAL P/N537L685003 GRN ILLEG. REPLACE STATIC SEAL P/N 1664M10P22 GRN1541SDR UPS99628329Module · malfunctionedINSPECTION, A/C WOULD NOT OBTAIN DESIRED SPEED ABOVE 250 KTS ADI INDICATIONS FLAP LIMIT SPD CRZ 310 TAT-26. CLIMBOUT WAS THE SAME, NO EICAS MSG FOR FLAP/SLAT DISAGREE / ASY ASYMMETRY ALT FLAP SELECTOR NORM /OP. COULD NOT DUPLICATE PROBLEM. REMOVED AND REPLASDR UPS98627515Spar · delaminatedINSPECTION TYPE-N/A, RUDDER FRONT SPAR AT RUDDER STATION FRONT SPAR STATION 189 HAS 2 X 6 AREA OF DELAMINATION. REMOVED RUDDER ASSEMBLY, INSTALLED SERVICEABLE RUDDER ASSEMBLY IAW MM 27-21-01.SDR UPS98627514Spar Web · punctureINSPECTION TYPE-N/A, RUDDER FRONT SPAR WEB IS PUNCTURED AT RUDDER STATION 189, THREE INCHES LEFT OF CENTER LINE. REMOVED AND REPLACED RUDDER ASSEMBLY ON CARD NR 745375.SDR UPS98627513Rib · damagedINSPECTION TYPE-E, TOP DAMAGE CAUSED TO BULLNOSE RIB WEB AT RUDDER STA 181.034. RUDDER ASSEMBLY WAS REMOVED AND REPLACED ON CARD NR 745375.
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