N656UA
Service difficulty reports · 336
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 = 'N656UA' 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 = 'N656UA' 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 UALA2013031101439Amplifier · faultyREPLACED PA AMP AND AUDIO ACCY UNIT. PUT BACK OLD AUDIO ACCY UNIT. PA AMP MR23316 - 1 REPLACED WITH MR23316 - 30. REF LOG 8, PANASONIC DID SO WORK EARLIER TODAY, PLEASE HAVE THEM REPLACE THE PARTS OR RELOAD SOFTWARE FOR TROUBLESHOOTING PURPOSES. REPLACED AUSDR UALA2013022601168Igniter · faultyREPLACE IGNITER PLUGS (NR 1 ENGINE). REPLACED IGNITORS NR 1 ENGINE.SDR UALA2013022501106Skin · corrodedFUSELAGE SKIN SURFACE LOWER AREA, CORROSION BELOW FASTENER HOLE AT 1 IN ABOVE LOWER EDGE BS 962. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION ON SKIN LOWER AREA AND INSTALLED DISC FILLER IAW ECRA 5340-01497.SDR UALA2013022501107Web · corrodedLEFT MAIN WHEEL WELL, REAR SPAR WEB CORRODED AT BS 955, LBL 78. REPAIRED THE BS 955 LT SIDE CTR WING SECTION REAR SPAR BULKHEAD WEB & MODIFICATION OF FAILSAFE STRAP IAW REO-G15835, AND ECRA 5340-01497.SDR UALA2013022401089Skin · damagedLEFT HORIZONTAL STAB INBOARD, L/E AREA LOWER SKIN DAMAGED. REPAIRED LEFT HORIZONTAL STAB INBOARD LOWER PANEL SKIN FWD TORQUE BOX IAW REO-G15880 AND EC-RA 5510-02276.SDR UALA2013022401102Skin · damagedLEFT FUSELAGE SKIN DAMAGED AT BS 1725.5 S24-27L. INSTALLED INTERIM REPAIR.SDR UALA2013021800914Housing · crackedRIGHT OVERWING SLIDE COMPARTMENT, DISCONNECT HOUSING FOUND BROKEN-CRACKED, DURING SQUIB DATE CHECK. REMOVED RIGHT DISCONNECT CAM ASSEMBLY, REMOVED AND REPLACED RIGHT DISCONNECT HOUSING AND REINSTALLED CAM ASSEMBLY PER MM.SDR UALA2013021800906Shear Tie · corrodedAFT CARGO BILGE, SHEAR TIE IS CORRODED, ON AFT SIDE OF BS 1307 WEB BETWEEN S-38L TO S-39L. REMOVED AND REPLACED SHEAR TIE PER DWG 146T1211, REV F AND SRM 51-40-2. MAJOR REPAIR.SDR UALA2013021800913Shear Tie · corrodedAFT CARGO COMPARTMENT LOWER BILGE, 2 EACH SHEAR TIES CORRODED ON AFT SIDE ALONG FASTENERS AT BS 1330, S-35L TO S-37L. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED SHEAR TIES FROM BS 1330, STR-35L TO S-37L PER BAC DWG 146T1212, REV E AND SRM 53-06-07 ON NOSDR UALA2013021800912Shear Tie · corrodedAFT CARGO COMPARTMENT BILGE, SHEAR TIES CORRODED ON AFT (FASTENER) SIDE OF FRAME BENEATH PRESSURE WEB AT BS 1330, S-37L TO S-39L. MAJOR REPAIR ACCOMPLISHED. REMOVED & REPLACED SHEAR TIES AT BS 1330, S-39L TO S-37L BAC DWG 146T1212, REV E AND SRM 51-40-2.SDR UALA2013021800908Shear Tie · corrodedAFT CARGO COMPARTMENT BILGE, SHEAR TIE CORRODED, ON AFT SIDE OF BS 1307 WEB, BETWEEN STR 38L-STR 37L. MAJOR REPAIR ACCOMPLISHED. REMOVED SHEAR TIE AND FABRICATED A NEW SHEAR TIE AND INSTALLED PER BAC DWG 140T2102, REV C AND SRM 51-40-2.SDR UALA2013020500697Skin · dentedCARGO DOOR, LOWER FWD CORNER HAS NUMEROUS DENTS. EVALUATED FOUR DENTS AND FOUND TO BE OUT OF SRM 52-30-01 LIMITS. CUT OUT DAMAGED DOOR SKIN, FABRICATED AND INSTALLED A DOUBLER AND FILLER. CATAGORY 'B' REPAIR.SDR UALA2013020500695Skin · dentedBULKPIT DOOR HAS 2 EA SKIN DENTS 2 IN FROM AFT EDGE, JUST ABOVE SCAB PATCH. AT C15 VISIT, RE-EVALUATED DENTS AND FOUND 3 TOTAL DENTS ABOVE EXISTING DOUBLER. ALL 3 DENTS ARE NOT WITHIN SRM 52-30-01 LIMITS, AND A OVER Y RATIOS ARE 17.14, 21.73 & 25. REMOVED EXSDR UALA2012120407039Trim Switch · faultyCREW REPORTS BURNING ELECTRIC ODOR FROM CAPT CONTROL WHEEL NEAR AILERON TRIM STICKER. DOES NOT FEEL WARM TO THE TOUCH. NO SMOKE OR HEAT EVER OBSERVED. REPORTED FROM PREVIOUS SHIFT SMELL SEEMED TO BE COMING FROM CAPT STAB TRIM SWITCH. OHM CHECKED FROM CONNESDR UALA2012120406933Yoke · odorCREW REPORTS BURNING ELECTRIC ODOR FROM CAPT CONTROL WHEEL NEAR AILERON TRIM STICKER. MAINTENANCE CONFIRMS THAT ELECTRICAL ODOR IS COMING FROM PILOT YOKE. DOES NOT FEEL WARM TO THE TOUCH. SAMC TEXT: NO SMOKE OR HEAT EVER OBSERVED.SDR UALA2012110206300Cdu · faultyL FMC MCDU IS BLANK, FLT DIVERTED. NO EICAS MSG DISPLAYED. SWITCHED TO RT FMC, NO HELP. TWO CDUS REQUIRED TO ENTER MNPS AIRSPACE. FOUND LEFT CDU AT FAULT. REPLACED CDU PER MM.SDR UALA2012082304718Pressure Switch · faultyLEFT ELEC HYD PUMP DOES NOT OPERATE IN AUTO. DEFERRED DUE TIME ON FUNCTION OPERATES NORMAL. REPLACED S26 PRESS SWITCH AND D54 CONNECTOR. OP CHECKS OKAY.SDR UALA2012081604553Display · failedUPPER EICAS SCREEN FLICKERS OR GOES BLANK WITH ENGINES SUPPLYING ELECTRICAL POWER. REPLACED UPPER EICAS DISPLAY AND CB C4081. OPS CHECKED NORMAL.SDR UALA2012081504530Display · failedLOWER EICAS BLANKED OUT AFTER SECOND ENGINE START. REPLACED EICAS DISPLAY SELECT PANEL. INSTALLED LOWER CRT IN UPPER POSITION AND INSTALLED NEW CRT IN LOWER POSITION. OPS CHECKED GOOD.SDR UALA2012071603835Indicator · faultySTANDBY ENGINE INDICATOR BLANK WHEN SELECTED ON. REPLACED STANDBY ENGINE INDICATOR PER MM, OPS NORMAL.SDR UALA2012071103728Structure · damagedLT ENGINE INNER INLET COWL HAS A HOLE APPROX 5-16THS BY 1-4 IN. LOCATION IS APPROX 10 O`CLOCK POSITION 7.5 IN FWD OF AFT END OF INLET COWL. REPAIRED PER SRM.SDR UALA2012042702523Unknown · faultedPREDICTIVE WINDSHEAR SYSTEM DOES NOT TEST CORRECTLY. REPLACED WEATHER TRANSCEIVER PER MM AND ACCOMPLISHED TEST, TEST PASSED. NEWLY INSTALLED RT UNIT FAILED, REINSTALLED ORIGINAL UNIT AND TESTS OKAY.SDR UALA2012042302429Amu · faultyACARS NO COM MULTIPLE OCCASSIONS DURING FLIGHT. REPLACED ACARS MANAGEMENT UNIT AS PER MM, OPS CHECKED NORMAL.SDR UALA2012040202044Control Valve · illuminatedT/E FLAP DISAGREE FAULT WHEN FLAPS GO BETWEEN 1 & 5. REPLACED T/E FLAP CONTROL VALVE MODULE & BYPASS VALVE. REPLACED FLAP BYPASS VALVE. TESTED OK IAW MM.SDR UALA2012033001997Indicator · faultedFLAP NEEDLE SPLIT WHEN FLAPS DROPPED FROM 5 THRU 25, NEEDLES ALIGNED AT 25, SPLIT AT 30. CYCLED FLAPS AND DUPLICATED SPLIT AGAIN WHEN FLAPS DROPPED THRU EACH POSITION. FLAPS DRIVE SMOOTH HYDRAULICALLY, SUSPECT FLAP POSITION INDICATOR SYSTEM. REPLACED MODULESDR UALA2012033001998O-Ring · leakingHYD LEAK IN NOSE WHEEL WELL AREA. FOUND WITH GEAR HANDLE IN UP POSITION LEAK IS BETWEEN THE LEFT SWIVEL FITTING & THE GEAR ACTUATOR. REPLACED O-RING ON THE UP FITTING UNION, NO LEAKS.SDR UALA2012032601929Static Inverter · malfunctionedSTATIC INVERTER MALFUNCTIONED. REPLACED STATIC INVERTER, OP CHECKED GOOD AND PILOTS TESTED. ALL CHECKED GOOD.SDR UALA2012020800755Actuator · leakingLT OUTBOARD ELEVATOR PCA HAS RUNNING LEAK FROM SHAFT SEAL. SHOULD READ LEAKING FROM LT CENTER ELEVATOR PCA. PCA REMOVED. COMPLETED INSTALLATION OF LT CTR ELEV PCA.SDR UALA2011101905671Pump · failedNR 1 ENG EDP WILL NOT DESELECT PRESSURE. REPLACED NR 1 ENGINE EDP, OPS CHECKED GOOD.SDR UALA2011091304957Actuator · faultyRUDDER TRIM ACTUATOR CHG. DUE TO RECENT HISTORY IF RUDDER TRIM PROBLEMS ACCOMPLISH THE FOLLOWING. REPLACE THE RUDDER TRIM ACTUATOR PER MM. THE PCN FOR THE RUDDER TRIM ACTUATOR IS 563-9038. PLEASE CHECK ONLINE IPC FOR CORRECT EFFECTIVITY. REPLACED RUDDER TSDR UALA2011091304956Coupler · defectiveR HF INOPERATIVE. CARRIED OUT HF TEST. TONE OK. TRANSMISSION OKAY. TRANSCEIVER PREVIOUSLY REPLACED. WILL REQUIRE HF COUPLER, NO TIME (PCN 530-9045). REPLACED HF COUPLER, OP CHECKS GOOD.SDR UALA2011091304955Connector · faultyNO RUDDER TRIM INDICATION OR MOVEMENT WITH RUDDER TRIM KNOB ELECTR. CONNECTOR REMOVED & RECONNECTED RUDDER TRIM ACTUATOR TEST PERFORMED PER AMM. SYS OPS NORMAL.SDR UALA2011080304050Autothrottle Sys · malfunctionedAUTOTHROTTLE FAIL AT STATUS ON ADI IS BLANK. TMC APPEARS OK. LEG FAULT A-T DISC TMC 01310800 AND TEST FAILURE OF MCDP-TMC. REPLACED TMC. AUTOLAND TEST 02, 30, 40 PASSED.SDR UALA2011062703163Pump · leakingLEFT HYD QTY LIGHT DURING ROLL OUT. SYSTEM QTY WHEN TO ZERO VERY RAPIDLY FOLLOWED BY L HYD PRIM SAMC TEXT: PUMP EICAS DURING TAXI IN. COMPLETED CHECK LIST AND SHUT DOWN PUMPS. ACC MAINT REPORT ENGINE DRIVEN HYD PUMP LEAK AT PUMP DEPRESSURIZATION SOLENOID. SDR UALA2011061002866Controller · malfunctionedRIGHT ENG BLEED LGT & R ENG HPSOV EICAS MSG DURING DESCENT WITH ENG BLEED SW ON & ENG RUNNING. REPLACED HPC CONTROLLER PER MM. ACP HIGH POWER ENGINE RUN, ALL INDICATIONS AND OPS NORMAL.SDR UALA2011052502551Cable · burnedAFT GALLEY NEW TECH CART CABLES P52, P61 & P62 HAVE BURNT PINS. REPLACED CABLE ASSEMBLIES, OPS CHECK NORMAL.SDR UALA2011052502550Battery Pack · inoperativeLH AFT MED EMERGENCY EXIT IDENTIFIER AND FLOOR STRIP NEXT TO LAV INOPERATIVE. REPLACED BATTERY PACK PER MM, OP CHECKS NORMAL.SDR UALA2011052302515Lens · missingSEAT 36ABC EMERGENCY LIGHT LENS MISSING. REPLACED BROKEN LENS.SDR UALA2011052302514Lens · brokenSEAT 27ABC EMERGENCY LIGHT LENS BROKEN. REPLACED BROKEN LENS, OP CHECKS GOOD.SDR UALA2011033001535Cable · damagedFWD RT LIGHT BAR IS INOP. REPAIRED EEL CABLE USING CRIMPER TM13-0800C PER MM. OPS CHECK GOOD ON NON ROUTINE.SDR UALA2011033001534Light · inoperativeSEAT 26AB EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT AND OPS CHECK GOOD ON NON ROUTINE 23401.SDR UALA2011032501413Hinge Fitting · crackedLEFT WING INBOARD MAIN FLAP, TRAILING EDGE, AFT FLAP HINGE FITTING, INBOARD FLANGE CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE AND FABRICATED A REPAIR ANGLE AND FILLERS AND INSTALLED PER SRM.SDR UALA2011030301038Heat Exchanger · crackedLH PACK PRIMARY HEAT EXCHANGER WITH A 5" LONG HEAVILY BLOWING AIR WITH PACK ON. UPDATE HEAVY NOISE FOUND AFTER TOWING AND ARRIVAL TO THE GATE. REPLACED PRIMARY HEAT EXCHANGER AND PLENUM ASSY PER MM.SDR UALA2011022800977Wire · chafedLEFT WING SLIDE EICAS INTERMITTENT. REPEAT GRIPE. PSEU BITE SHOWS SAME FAULTS AS PREVIOUS. ADJUSTED S218 TARGET PER MM. REPAIRED CHAFED WIRE NR 216R-20 IN ADP BAY. SEU BITE AND SENSOR TESTS OK.SDR UALA2011021700816Sensor · faultyLT WING SLIDE EICAS, FLIGHT DIVERTED. REPLACED S218 SENSOR IAW AMM, GROUND CHECKS NORMALSDR UALA2011011200162Slide · unsecureDOOR 1L SLIDE DOOR NOT SECURE. FOUND ESCAPE SLIDE PARTIALLY DETACHED FROM DOOR. DOOR 1L EMERGENCY ESCAPE SLIDE REMOVED. DOOR 1L PROPERLY CLOSED. REMOVED SLIDE NUMBER IS MR25708-225. REPLACED ENTRY DOOR ESCAPE SLIDE PACK AT DOOR 1L PER MM.SDR UALA2010123004766Switch · faultedLT ENG FIRE LOOP 2 STATUS MSG DISPLAYED. REPLACED FIRE-OVERHEAT TEST SWITCH ON P8 STAND FIRE-OVERHEAT TEST PANEL. OP CHECK SEVERAL TIMES AND CHECKED OKAY.SDR UALA2010121504587Microphone · faulty2ND OBSERVERS OXYGEN MASK MIC WILL NOT TRANSMIT. REPLACED MASK ASSY, NO LEAKS NOTED. MIC STILL DOSEN'T TRANSMIT ON PA OR TO VHF.SDR UALA2010121004512Connector · dirtyEICAS MESSAGE REVERSER ISOLATION VALVE DISPLAYED AND REVERSER ISOLATION LIGHT ILLUMINATED DURING REVERSE THRUST. REACTIVATED REVERSER. CLEANED CONNECTOR AT REVERSER ISOLATION VALVE. CHECKED OPERATION SEVERAL TIMES. REVERSER OPERATION NORMAL, NO FURTHER MESSAGSDR UALA2010120904497Circuit Card · faultyLT ENGINE FIRE LOOP 2 DISPLAYED ON STATUS. FIRE TEST NO HELP. WON'T ERASE. REPLACED CARDS M684 AND M10274, LOOP RESISTANCE FROM CARD 684 PIN 19-20 1450 OHMS.
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