N394UP
Service difficulty reports · 74
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 = 'N394UP' 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 = 'N394UP' 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 IPXA2023091401301Door · corroded*SUPPLEMENTAL SDR* FAULT: CREW ENTRY DOOR FRAME UPPER HAS CORRODED FASTENERS. DOT 140-44 CLEANED PER SOPM 20-30-03 STEP 9. CREW ENTRY DOOR, NO DAMAGE WAS FOUND, NO MATERIAL LOST, ONLY PAINT WAS REMOVED REVIEWEDSDR IPXA2023091401292Door · corrodedCREW ENTRY DOOR FRAM UPPER AT PLACARD HAS CORROSION. DOT 140-43 REMOVED CORROSION IN PLACERD IAW SRM 53-00-15-1A-1 NOMINAL THICKNESS 0.032" MATERIAL LOSS .003" REMAINING THICKNESS 0.029" FOUND TO BE IN LIMITS. T89336. TREATED AND PRIMED AREA IAW SRM 51-20-01-0SDR IPXA2023091401281Door · corroded*SUPPLEMENTAL SDR* FAULT: MCD FWD OPENING ROD INBD END CORRODED. DOT 140-42 AFTER FURTHER EVALUATION NO CORROSION NOTED. CLEANED MCD FWD OPENING ROD WITH SCOTCH BRITE AND ALCOHOL. IAW SOPM 20-30-03. TREATED AND PRIMED AFFECTED AREA ON OPENING ROD. IAW SRM 51-2SDR IPXA2023091401252Door · corrodedFWD LARGE CARGO DOOR FRAME UPPER FWD CORNER CORRODED AND AT BONDING LOCATION. DOT 140-40 REMOVED CORROSION FROM FWD LARGE CARGO DOOR FRAME NEXT TO BONDING LOCATION. USED ULTRA SONIC (T89336) AND IS WITHIN LIMITS. NOMINAL THICKNESS .071, REMAINING MATERIAL .06SDR IPXA20230911301Unknown · unknown*SDR FILED OPEN* FAULT: CREW ENTRY DOOR FRAME UPPER HAS CORRODED FASTENERS. DOT 140-44 VERIFIED AREA CLEANED AND NO DAMAGE FOUND. WORK COMPLETED.SDR IPXA20230911252Unknown · unknown*SDR FILED OPEN* FAULT: FWD LARGE CARGO DOOR FRAME UPPER FWD CORNER CORRODED AND AT BONDING LOCATION. DOT 140-40 VERIFIED C.I.C. APPLIED.<BR>WORK COMPLETED.SDR IPXA20230911292Unknown · unknown*SDR FILED OPEN* FAULT: CREW ENTRY DOOR FRAM UPPER AT PLACARD HAS CORROSION. DOT 140-43 VERIFIED APPLIED TOPCOAT WORK COMPLETED.SDR IPXA202309111281Unknown · unknown*SDR FILED OPEN* FAULT: MCD FWD OPENING ROD INBD END CORRODED. DOT 140-42 VERIFIED APPLIED TOP COAT. WORK COMPLETED.SDR IPXA2023090328518Unknown · unknownR ENG HPSOV ON EICAS AFTER STARTING THE RIGHT ENGINE AFTER PUSHBACK RESULTED IN A BTB ** OII 2 ** (LINKED TO T3F18E002BZ2A) DEFERRED IAW MEL 36-11-2-2SDR IPXA2023011289809Eec · faultedATB, EMERGENCY DECLARED, LEFT ENGINE FAILURE ON T/O. ENGINE RECOVERED. PERFORMED FIM TASK 71-01-00-810-994-H01 REV 138.00. DUE TO PIMU FAULT CODE 160-14. REPLACED EEC IAW AMM 73-21-15 PB 401 REV 138.01. FOUND OPS TEST SATIS.SDR IPXA2022072684570A/C Pack · abnormalINSPECTION TYPE:ETOP** ETOPS FILED OPEN**AFT CABIN TEMP MSG AND INOP LIGHT ILLUMINATED. DEFEND AFT CABIN TEMP CONT SYS PER MEL 21-61-1-2 DMP ACCOMPLISHED BY 0556511 AUTHORIZED BY 0557835 PLACARD INSTALLED. DI LOG UPDATED.SDR IPXA2022072584562Eicas · fault messageINSPECTION TYPE:ETOPWITH RIGHT SYSTEM SELECTED "WXR FAIL" DISPLAYED ON HSI (BOTH SIDES) WXR TEST NOT ATTEMPTED ALSO STATUS MSG "WXR SYS". LEFT SYSTEM OK.WEATHER RADAR SYS TEST C/O IAW AMM 34-43-00-735-033-002 REV 136.02. WXR SYS OK.SDR IPXA2022052782562Wing Root · crackedINSPECTION TYPE:C16CRACK ON R/H OVERWING EMERGENCY EXIT DOOR LOWER MAIN SILL INNER CHORD AT STA 883.5REPAIR I.A.W BOEING SR:4-5501411401 AND UPS EO B767-5310-83826-ASDR IPXA2022052782561Wing Root · crackedINSPECTION TYPE:C16CRACK ON L/H OVERWING EMERGENCY EXIT DOOR ;OWER MAIN SILL INNER CHORD AT STA 883.5REPAIR I.A.W BOEING SR:4-5500527955 AND UPS EO B767-5310-83822-ASDR IPXA2022052582486Support Beam · corrodedINSPECTION TYPE:C16CORROSION ON RH WING INBD SPOILER SUPPORT BEAM UPPER CHORD BETWEEN WBL 168 AND 2BL 238REPAIR I.A.W 767-300BCF SRM 57-51-02, ALLOWABLE DAMAGE 1, REV. 43.00.SDR IPXA2022052382369Skin Panel · debondedINSPECTION TYPE:C16DISBOND DAMAGE WAS FOUND ON LOWER SURFACE OF SKIN PANEL ON R/H WING INBD AFT FLAP NEAR WBL 122REPAIR I.A.W B767-300BCF SRM 57-53-01-2R-1, SRM 51-70-10-2R REPAIR GENERAL, AND SRM 51-70-10-2R-4 REV 43.00.SDR IPXA2022052382368Skin Panel · debondedINSPECTION TYPE:C16DURING C16 CHECK OF DATUM AIRPLANE, DISBOND DAMAGE WAS FOUND ON LOWER SURFACE OF SKIN PANEL ON R/H WING INBD AFT FLAP NEAR WBL 205.REPAIR I.A.W B767-300BCF SRM 57-53-01-2R-1, SRM 51-70-10-2R REPAIR GENERAL, AND SRM 51-70-10-2R-4 REV 43.00.SDR IPXA2021111776091None · noneINSPECTION TYPE:ETOP** ETOPS FILED OPEN**L PACK TEMP EICAS MESSAGE AFTER START. NO OTHER FAULT INDICATION. DEFERRED PER MEL 21-51-1-1. L PACK INOP. DMP C/W. DI LOG UPDATED, PLACARD REMOVEDSDR IPXA2021031967001Anti-Ice Valve · malfunctionedINSPECTION TYPE:NA**ATB - NO EMERG DECLARED - NO EMERG EQUIP USED. ** L ENG BLEED OFF THEN L ENG ANTI ICE THEN L PACK TEMPPACK 1 NOTED INOP/BLANK W/APU BLEED AVAIL.AIR SUPPLY BITE MODULE TESTED . PCK CONTROLLERS TESTED IAW . ALL W/OUT FAULTS. A/C ELEC PWR DWN SDR IPXA2020121363320Light · inoperativeINSPECTION TYPE: N/A FOUND ON PS1 EMERGENCY LIGHT INOPERABLE. REPLACEMENT OF EMERGENCY LIGHT PERFORMED, IAW AMM 33-51-03 PB 201 REV 131.02.SDR IPXA2020112162616Sensor · inoperativeINSPECTION TYPE: N/A SUPPLEMENTAL SDR, ATB, NO EMERGENCY DECLARED AND NO EQUIPMENT USED. LEADING EDGE FLAP ASSYMETRY. QRH COMPLIED WITH DESTINATION WEATHER AT CAT II MINS AIR TURN BACK. FLAP ALE EXTENDED FL200 SPEED CLIMB 280, 240 KIAS. R & R SLAT NR 9 INBSDR IPXA2020070357281Skin Panel · corrodedINSPECTION TYPE:C15 CORROSION ON THE LT WING LOWER SKIN PANEL AROUND THE FUEL SUMP DRAIN VALVE. PERFORM REPAIR IAW SRID 3-4752002896 AND EO B767-5730-77048-A.SDR IPXA2020070357280Skin Panel · corrodedINSPECTION TYPE:C15 CORROSION ON THE RT WING LOWER SKIN PANEL AROUND THE FUEL SUMP DRAIN VALVE. PERFORM REPAIR IAW SRID 3-4751949658 AND EO N B767-5730-77047-A.SDR IPXA2020052255641Slat System · malfunctionedINSPECTION TYPE:NA**DIVERSION** LE SLAT ASYMMETRY DURING FLAP RETRACTION. SPEED LIMITED TO LESS THAN 245 KTS. MAINTAINED 20,000 FT. HAD TO USE ALERTERNATE FLAP EXXTENSION IN CGN. LANDING NORMAL WITH 20 DEGREES OF FLAPS. NO EMERGENCY DECLARED.IAW FAULT CODE
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