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.

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 AUMar 8, 2013 · N656UA · Boeing 767322 · Interphone/Passenger Announcement (PA) SystemSDR UALA2013022601168Igniter · faultyREPLACE IGNITER PLUGS (NR 1 ENGINE). REPLACED IGNITORS NR 1 ENGINE.Feb 25, 2013 · N656UA · Boeing 767322 · Spark Plug/IgniterSDR 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.Feb 24, 2013 · N656UA · Boeing 767322 · Fuselage Main, Plate/SkinSDR 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.Feb 24, 2013 · N656UA · Boeing 767322 · Wing, Center BoxSDR 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.Feb 23, 2013 · N656UA · Boeing 767322 · Horizontal Stabilizer, Plate/SkinSDR UALA2013022401102Skin · damagedLEFT FUSELAGE SKIN DAMAGED AT BS 1725.5 S24-27L. INSTALLED INTERIM REPAIR.Feb 23, 2013 · N656UA · Boeing 767322 · Fuselage Main, Plate/SkinSDR 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.Feb 17, 2013 · N656UA · Boeing 767322 · Emergency EquipmentSDR 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.Feb 16, 2013 · N656UA · Boeing 767322 · Fuselage Internal Mounting StructureSDR 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 NOFeb 16, 2013 · N656UA · Boeing 767322 · Fuselage Internal Mounting StructureSDR 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.Feb 16, 2013 · N656UA · Boeing 767322 · Fuselage Internal Mounting StructureSDR 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.Feb 16, 2013 · N656UA · Boeing 767322 · Fuselage Internal Mounting StructureSDR 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.Feb 4, 2013 · N656UA · Boeing 767322 · Cargo/Baggage DoorsSDR 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 EXFeb 4, 2013 · N656UA · Boeing 767322 · Cargo/Baggage DoorsSDR 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 CONNEDec 4, 2012 · N656UA · Boeing 767322 · Stabilizer Control SystemSDR 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.Dec 4, 2012 · N656UA · Boeing 767322 · Control Column SectionSDR 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.Oct 31, 2012 · N656UA · Boeing 767322 · Central DisplaySDR 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.Aug 21, 2012 · N656UA · Boeing 767322 · Hydraulic Pressure Relief Valve, MainSDR UALA2012081604553Display · failedUPPER EICAS SCREEN FLICKERS OR GOES BLANK WITH ENGINES SUPPLYING ELECTRICAL POWER. REPLACED UPPER EICAS DISPLAY AND CB C4081. OPS CHECKED NORMAL.Aug 15, 2012 · N656UA · Boeing 767322 · Central ComputersSDR 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.Aug 15, 2012 · N656UA · Boeing 767322 · Central ComputersSDR UALA2012071603835Indicator · faultySTANDBY ENGINE INDICATOR BLANK WHEN SELECTED ON. REPLACED STANDBY ENGINE INDICATOR PER MM, OPS NORMAL.Jul 14, 2012 · N656UA · Boeing 767322 · Engine Integrated Instrument SystemSDR 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.Jul 8, 2012 · N656UA · Boeing 767322 · Nacelle/Pylon, Main FrameSDR 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.Apr 26, 2012 · N656UA · Boeing 767322 · Wind Shear Detection SystemSDR UALA2012042302429Amu · faultyACARS NO COM MULTIPLE OCCASSIONS DURING FLIGHT. REPLACED ACARS MANAGEMENT UNIT AS PER MM, OPS CHECKED NORMAL.Apr 21, 2012 · N656UA · Boeing 767322 · Data Transmission Auto CallSDR 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.Mar 31, 2012 · N656UA · Boeing 767322 · Trailing Edge Flap Control SystemSDR 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 MODULEMar 30, 2012 · N656UA · Boeing 767322 · Trailing Flap Position Indicating SystemSDR 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.Mar 28, 2012 · N656UA · Boeing 767322 · Hydraulic System, MainSDR UALA2012032601929Static Inverter · malfunctionedSTATIC INVERTER MALFUNCTIONED. REPLACED STATIC INVERTER, OP CHECKED GOOD AND PILOTS TESTED. ALL CHECKED GOOD.Mar 26, 2012 · N656UA · Boeing 767322 · Pitot/Static SystemSDR 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.Feb 8, 2012 · N656UA · Boeing 767322 · Elevator Control SystemSDR UALA2011101905671Pump · failedNR 1 ENG EDP WILL NOT DESELECT PRESSURE. REPLACED NR 1 ENGINE EDP, OPS CHECKED GOOD.Oct 18, 2011 · N656UA · Boeing 767322 · Hydraulic Pump (Electric/Engine), MainSDR 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 TSep 13, 2011 · N656UA · Boeing 767322 · Rudder Tab Control SystemSDR 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.Sep 13, 2011 · N656UA · Boeing 767322 · HF Communications SystemSDR 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.Sep 12, 2011 · N656UA · Boeing 767322 · Flight Control System WiringSDR 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.Aug 2, 2011 · N656UA · Boeing 767322 · Auto Throttle SystemSDR 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. Jun 25, 2011 · N656UA · Boeing 767322 · Hydraulic Pump (Electric/Engine), MainSDR 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.Jun 8, 2011 · N656UA · Boeing 767322 · Pneumatic Distribution SystemSDR UALA2011052502551Cable · burnedAFT GALLEY NEW TECH CART CABLES P52, P61 & P62 HAVE BURNT PINS. REPLACED CABLE ASSEMBLIES, OPS CHECK NORMAL.May 24, 2011 · N656UA · Boeing 767322 · Equipment/Furnishings WiringSDR UALA2011052502550Battery Pack · inoperativeLH AFT MED EMERGENCY EXIT IDENTIFIER AND FLOOR STRIP NEXT TO LAV INOPERATIVE. REPLACED BATTERY PACK PER MM, OP CHECKS NORMAL.May 24, 2011 · N656UA · Boeing 767322 · Emergency LightingSDR UALA2011052302515Lens · missingSEAT 36ABC EMERGENCY LIGHT LENS MISSING. REPLACED BROKEN LENS.May 22, 2011 · N656UA · Boeing 767322 · Emergency LightingSDR UALA2011052302514Lens · brokenSEAT 27ABC EMERGENCY LIGHT LENS BROKEN. REPLACED BROKEN LENS, OP CHECKS GOOD.May 22, 2011 · N656UA · Boeing 767322 · Emergency LightingSDR UALA2011033001535Cable · damagedFWD RT LIGHT BAR IS INOP. REPAIRED EEL CABLE USING CRIMPER TM13-0800C PER MM. OPS CHECK GOOD ON NON ROUTINE.Mar 30, 2011 · N656UA · Boeing 767322 · Light System WiringSDR UALA2011033001534Light · inoperativeSEAT 26AB EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT AND OPS CHECK GOOD ON NON ROUTINE 23401.Mar 30, 2011 · N656UA · Boeing 767322 · Emergency LightingSDR 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.Mar 24, 2011 · N656UA · Boeing 767322 · Trailing Edge FlapsSDR 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.Mar 2, 2011 · N656UA · Boeing 767322 · Cabin Cooling SystemSDR 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.Feb 27, 2011 · N656UA · Boeing 767322 · Equipment/Furnishings WiringSDR UALA2011021700816Sensor · faultyLT WING SLIDE EICAS, FLIGHT DIVERTED. REPLACED S218 SENSOR IAW AMM, GROUND CHECKS NORMALFeb 16, 2011 · N656UA · Boeing 767322 · Escape SlideSDR 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.Jan 10, 2011 · N656UA · Boeing 767322 · Escape SlideSDR 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.Dec 29, 2010 · N656UA · Boeing 767322 · Overheat DetectionSDR 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.Dec 15, 2010 · N656UA · Boeing 767322 · Communications SystemSDR 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 MESSAGDec 10, 2010 · N656UA · Boeing 767322 · Engine Thrust ReverserSDR 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.Dec 9, 2010 · N656UA · Boeing 767322 · Fire Detection
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