N662UA
Service difficulty reports · 337
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 = 'N662UA' 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 = 'N662UA' 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 CALA2026101220299Skin · damagedDURING THERMOGRAPHY INSPECTION OF OUTBOARD AILERON LH WAS FOUND WATER INGRESS INDICATION. PICTURES ATTACHED. AFTER THERMOGRAPHY INSPECTION WAS FOUND WATER INGRESSION ON LOWER SKIN. DAMAGED AREA WAS REMOVED & REPAIRED FOLLOWING SRM .DONE NEW INSPECTION ON REPASDR CALA2026083119076Skin · puncturedPUNCTURE BETWEEN AFT CARGO DOOR AND R3 ENTRY DOOR ON THE RIGHT SIDE OF ACFT. DAMAGE LOCATED BTWN BS 1439 & 1461 IAW SRM 53-00-00-0G-0. FOUND DAMAGE TO BE 5.4 INCH LONG BY 2.6 INCH WIDE, ON BS 1439 - 1461, STR 21-22R. DAMAGE IS OUT OF LIMITS IAW SRM 53-00-SDR CALA2025082208058Windshield · no discrepancyBIRD STRIKE ON F/O WINDSHIELD AFTER TAKEOFF CREW REPORTED NO ENGINE INDICATION ISSUES. FOUND NO EVIDENCE OF A BIRD STRIKE ON F/O WINDSHIELD NOR ON CROWN AREA REF PICS OF A/C WHEN BLOCKED INTO GATE AND PIC TAKEN OF CROWN AREA. PERFORMED BIRDSTRIKE INSPECTION IASDR CALA2025073107181Unknown · odorAFTER ENG START, SELECTED PACKS ON HAD STRONG FUME ODORS IN BACK OF CABIN, REPORTED BY THE AFT CABIN AREA FLIGHT ATTENDANTS THAT WAS A FUEL ODOR AFTER ENG START FOR ABOUT 5 MINS UNTIL IT CLEAR OUT OF CABIN. REPORTED ONLY HAVING THIS ISSUE OUT OF LHR. VERIFISDR CALA2025073007077Slide · looseDOOR 2L SLIDE PACK IS SUSPECTED TO HAVE BECOME LOOSE THUS MOVING THE BUSTLE COVER LOWER DOOR 2L SLIDE BUSTLE LOWER FWD LATCH BECAME DISENGAGED, BUSTLE REMOVED SLIDE PACK CHECKED IAW AMM 25-66-98-206-001, NO DEFECTS NOTED. SLIDE BUSTLE RE-FITTED, ARM/DISARM LEVSDR CALA2025072806973Lamp · inoperativeRH AFT EXTERIOR EMERGENCY LIGHT NOT LIGHT DURING TEST. RH AFT SLIDE ESCAPE LIGHT LAMP REPLACED IAW AMM 33-51-06-902-082.SDR CALA2025061205492None · noneDOOR BUSTLE INSPECTION POST INSTALL REF LOG 5137002 DOOR 1L BUSTLE INSTALLED AS PER AMM 25-66-01-424-070 RII INSPECTION REQUIRED RII OF PASSENGER SERVICE DOOR BUSTLE C/O REF AMM: 26-66-01-404-072. VERIFIED INSTALLED CORRECTLY, NO OTHER SYSTEMS DISTURBED. RENDESDR CALA2025060905386Wire · damagedDOOR 1R ENTRY DOOR POWER OPENING ASSIST HAS A INTERMITTENT FAULT ACTIVATING EMER LIGHTS WHEN DOWN MODE SWITCH PRESSEDCORRECTION DOOR 1L NOT DOOR 1R UPDATE - DOOR 1L ELECTRICAL CLOSING SWITCH ON FA PANEL AND EXTERNAL DOOR TOGGLE SWITCH WHEN SELECTED DOWN (CLOSESDR CALA2025060905383Lamp · inoperativeEMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - EXTERIOR D2L EMERGENCY LIGHT INOP D2L SLIDE EMERGENCY LIGHT LAMP REPLACED AS PER AMM 33-51-06-902-082. NOW OK.SDR CALA2025060905382Lamp · inoperativeEMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - EXTERIOR RIGHT EMERGENCY LIGHT (FWD OF AFT CARGO) INOP MID RIGHT SLIDE LIGHT LAMP REPLACED AS PER AMM 33-51-06-902-082. NOW OK.SDR CALA2025060905363Light · inoperativeEMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - ESCAPE PATH AISLE LIGHTING ON SEATS 38F, 39F AND 40F NOT ILLUMINATING ESCAPE PATH LIGHTS REPLACED AS PER CMM 25-23-52. PARTS USED: 29-3326-3-0013, QTY :1 ESCAPE PATH LIGHT FIXTURES INSPECTED AND CONFIRMED CSDR CALA2025060405267Idg · faultedAT CRUISE ALT, LEFT GEN DRIVE LIGHT FIRST THEN GEN OFF. 1X GEN OFF RESET FAILED REF FM 2.60.35 ON ARRIVAL LEFT IDG DELTA P POPPED OUT. IDG FILTER REMOVED AND FOUND CONTAMINATION. IDG REMOVAL/ INSTALLATION CARRIED OUT I.A.W AMM 24-11-01-004-002-006/ 24-11-01-40SDR CALA2025051404672Warning Message · false activationIN FLT GOT MASTER CAUT AND LE SLAT ASYM EICAS MSG. COMPLIED W/ Q RH. CREW DEBRIEF: LE SLAT ASYM MSG ON SELECTION OF FLAPS 5, QRH COMPLETED TE FLAPS SELECTED TO 20 WITH NO ISSUE. NO REPORTED FLIGHT CONTROL HANDLING ISSUES FELT. RETRACTED LEADING EDGE SLATS ON ASDR CALA2025041804019Light · inoperativeEXTERNAL EMERGENCY LIGHT, RIGHT SIDE (L391) INOP PERFORMED EMERGENCY LIGHT TEST IAW AMM TASK 33-51-00-705-029-001. FOUND L391 LIGHT FUNCTIONAL. OK TO CONTINUE.SDR CALA2025041703925Light · malfunctionedIN REFERENCE WITH LOGPAGE#4512799 PERFORMED SYSTEM TEST OF THE EMERGENCY LIGHTS IRW AMM 33-51-00-705-029-001. EMERGENCY LIGHTS FAILED TO STAY ON DURING THE 1 MINUTE PERIOD REQUIREMENT. LEFT SIDE OF THE AC EMERGENCY LIGHTS TURNED OFF WITHIN 10-20 SECONDS WITH ESDR CALA2025031302795Slide · faultedFOUND R/H OVERWING SLIDE HOSE CLAMP DETACH REMOVED AND REPLACED RH OFF WING SLIDE ASSY PER AMM 25-65-01/401 CONFIG 1 UPTO AND INCLUDING STEP 3 G(8). NEED TO CONTINUE INSTALLATION FROM STEP H. C/W RII REQUIREMENTS FOR R/H OVERWING SLIDE ASSY INSTALLATION REF SDR CALA2025030300471Fseu · faultedLE SLAT ASYM EICAS B LE SLAT ASYMMETRY CREW DEBRIEF: ON APPROACH WHEN FLAPS/SLATS WERE EXTENDED, GOT A SECOND REPORT. LE SLAT ASSYMETRY EICAS. NO ABNORMAL ROLL EXPERIENCED. FLAPS REMAIN EXTENDED AND HANDLE IS AT 20. PER FIM 27-81 FAULT TREE 809 SYSTEM IS OK.SDR CALA2025010601790Fseu · faultedLE SLAT DISAGREE EICAS CREW REPORTS THEY ACCOMPLISHED PROCEDURE AND LE SLAT DISAGREE MSG CLEARED. PERFORMED BITE CK OF FSEU PER REF FIM 27-51 FAULT TREE 809. FOUND MESSAGE NUMBER 27-51333. REMOVED AND REPLACED FSEU REF AMM 27-51-01. OPS CK GOOD. NO STATUS MESSSDR CALA2024102102699Skin · corrodedIT WAS FOUND CORROSION ON THE SKIN (P/N 146T3241-12) AT THE DRAIN HOLE AREA LOCATED BETWEEN STA 1540 AND 1562 & STR 39LH AND 39RH. MANENT SOLUTION WITH INSPECTION REQUIREMENTS THAT MUST BE ACCOMP ON OR BEFORE THE AIRCRAFT REACHES 37,500 TOTAL FLIGHT CYCLES. ACSDR CALA2024102102697Stringer · damagedBULK CARGO COMPARTMENT WAS FOUND TOOL MARK AT STGR 38LH BETWEEN STA 1562/1582. (NR 2236807)SDR CALA2024102102700Stringer · corrodedBULK CARGO COMPARTMENT WAS FOUND CORROSION AT STGR 39LH BETWEEN STA 1540/1562. (NR 2231086) UPGRADE OF ATTRIBUTES PERFORMED REPAIR AT STRINGER 39LH AS PER SRM 53-00-03-2R-2 TYPE III AND TABLE III DETAIL IV .SDR CALA2024102102689Floorbeam · corrodedINSPECTING BODY BELLOW AFT CARGO FLOOR WAS FOUND CORROSION SIGNS ON FRAME SURFACE, STA 1197, STRINGER 36L.SDR CALA2024102102688Skin · damagedTHERE ARE OLD SCRIBE MARKS ON EXTERNAL SKIN OF FUSELAGE, LOCATED BETWEEN STA 654 PLUS 110/STA 785.9 AND BETWEEN STR20LH/36LH. FOR REFERENCE SEE SRM 53-30-01-0I-1 FIG 1, SHEET 2(ITEM 3) AND SHEET 4(ITEM 6). IS A PERMANENT SOLUTION WITH INSPECTION REQUIREMENTS TSDR CALA2024101802677Floor Support · corrodedINSPECTING THE BODY BELLOW THE AFT CARGO FLOOR WAS FOUND SIGNS OF CORROSION ON THE FRAME SURFACE, STA 1197/110 , STRINGER 34L.SDR CALA2024101402635Pressure Blkhd · dentedDURING CLEAN PROCESS WAS FOUND STA 1582.0 PRESSURE BULKHEAD WITH DAMAGE LOCATED IN DOME WEB. REPAIR IS A PERMANENT SOLUTION WITH INSPECTION REQUIREMENTS. REVISION OF EC/RA 5380-01408 ON OR BEFORE THE AIRCRAFT REACHES ACCOMPLISH INSPECTION REQUIREMENTS PER PARTSDR CALA2024101102632Skin · crackedDURING HFEC INSPECTION OF THE FASTENER OPEN HOLE, WAS FOUND A CRACK LENGTH 0.040" AT THE FWD SERVICE DOOR CUTOUT AFTER LOWER CORNER.SDR CALA2024060301667Panel · missingPDA 2 ON ETOPS WALKROUND FOUND PANEL 446BR MISSING. PYLON PANEL 446BR FITTED, AMM REF 54-53-01-404-007 FOR INSTALLATION. PARTS USED: 76-5453-3-0063,QTY :1SDR CALA2024042601243Control Module · defectiveSTAB TRIM LIGHT CAME ON AFTER T/O WITH FLAPS OUT. WITH FLAPS UP EICAS WENT OUT LEFT AND RIGHT EICAS COMPUTERS. PERFORMED FIM TASK 27-48FT809, FOUND COL TRIM SW FAULT BALL PERFORMED FIM TASK 27-48FT809, COMPLETED TEST 30 MCPD TEST, TEST PRESENT ON RT SAM, NO FASDR CALA2024020500327Relay · inoperativeLAV SYS 2 FLUSH CB R-35 POPED ONLY 3 LAVS WORKING R&R LAV FLUSH CONTROL RELAY (K2311) IAW WDM 38-32-11. PERFORM OPS CHECK OF LAV SYSTEM IAW 38-32-00/201, OPS CHECK GOOD. BREAKER NOT POPPING OUT. PARTS USED: 99-2332-3-0034,QTY :1. RNWY TURN OFF CD POPPED N-6 PESDR CALA2024011900156Wire Harness · chafedL ENG FIRE LP 2 EICAS. THE LEFT ENGINE FIRE LOOP 2 HAS A FIRE OR THERE IS A FAILURE OUT PUT. INTERMITTENT STATUS MESSAGE NO EICAS MESSAGE ON ARRIVAL. L ENG LP 2 INTERMITANT DURING CRUISE. TALKED TO CREW, WRITE UP IS IN REFERENCE TO LOGPAGE 6821086. MESSAGE WASSDR CALA2023121103623Light · missingEMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - 2X FWD GALLEY 227F/R & 228F/R EPL MISSING CLEAR LENSES. PLEASE REPLACE. BOTH EPL LENSES REPLACED IAW CMM 25-07-22.SDR CALA2023110303272Electronic Unit · faultyCONT. LE FLAP ASSYM AGAIN AT FL300 DOING 320 KTS.RTB AFTER SLOWING NORM IND ACFT LANDED @ 318000LBS, OVERWEIGHT LANDING NOT REQD. FLT CREW DEBRIEF: LE ASYM EICAS MSG WITH ASSOCIATED LE EDGE ANNUNCIATOR LT DURING CLIMB FOR 1MIN, THEN AGAIN AT 33000FT @ 320KTS FSDR CALA2023110203256Connector · unknownTHRUST MANAGEMENT SYSTEM A/T DISC LIGHT ILLUMINATED WITH AUTOTHR OTTLE ENGAGED IN (STATE MODE) MODE. THRUST REFERENCE MODE DISPLA Y ON EICAS & F/S POINTER DISPLAY ON EADI NORMAL IN VNAV PATH MODE ARRIVAL CREW INFORMATION: A/T DISCONNECTED IN CRUISE, RESET SDR CALA2023102503171Engine · faultedVIBRATION & STEADY HUM SOUND IN ACFT SINCE REACHING CRUISE ALT. ENTIRE FLT. LOUD HUMMING NOISE NOTABLE INCREASE IN EGT, FUEL FLOW. FLUCTUATING N2 AND VIB INDS. NOISE CHANGED WITH THROTTLE. ON ARRIVAL FOUND RT ENG INTAKE BLOW OUT PANEL UNLATCHED. WITH A SSOSDR CALA2023101603089Sensor · intermittentLE SLAT ASYM CAME ON RETRACTING FLAPS 1 TO ZERO AND INDCATOR DISPLAY OUT OF UP ACCOMPLISHED FIM 27-81-00/301 LEADING EDGE (LE) SLAT SENSOR INDUCTANCE/RESISTENCE TEST AND IT WAS FOUND SENSOR S279 WITH INDUCTANCE 6.52 (OVER LIMIT). PERFORMED ADJUST REF. AMM SUSDR CALA2023100902997Cylinder · activatedDURING THE ACTIVATION OF THE "OFF WING ESCAPE SYSTEM", ACCIDENTALLY THE SPOILER OVERRIDE ACTUATORS AND AND DOORS LATCH OPENING/SNUBBING ACTUATOR WERE FIRED. REMOVED AND REPLACED CYLINDER,ASSY, OFFWING EVACUATION REPLACED SPOILER OVERRIDE ACTUATOR SQUIB LH PN OSDR CALA2023071702270Extinguisher · unknownRAISING SDR FOR INCORRECT FITMENT OF COMPONENT PER TASK CARD 63-2620-1-2827. SDR RAISED FOR DISCOVERY OF INCORRECT FITMENT OF COMPONENT DURING TASK CARD 63-2620-1-2827 ON 15-JUL-23. TSAP RAISED.SDR CALA2022070401634Controller · failedMID CABIN TEMP EICAS C THE MID CABIN SUPPLY DUCT TEMPERATURE IS MORE THAN 190 DEGREES F (88 DEGREES C); OR THE ZONE TEMPERATURE MID CABIN CHANNEL HAS A FAILURE OR THE SYSTEM IS OFF.REMOVED AND REPLACED THE MAIN CABIN ZONE TEMP CONTROLLER. ALL TEMPS NORMAL.CREWSDR CALA2022030700603None · noneAIRCRAFT REPORTED TO BE TRANSMITTING ON GUARD FREQ (NO VOICE) GROUND MONITORING STATION REPORTS THAT NORMAL ATC COMS FROM AIRCRAFT BEING HEARD ON GUARD FREQ. REPLACED NO.1 TRANSCEIVER PER AMM 23-12-01-424-004 & REPLACED NO.2 (FO SIDE) AUDIO SELECTOR PANEL PER SDR CALA2021111702123Skin · corrodedREFER NRC L/P 9131558 FUSELAGE STA 1205 STR 36L STRINGER SECTION CUTOFF FOUND ATTACH SKIN CORROSION. TRANSFER REF NR LP 9131765 AND ORIGINATED BY V896890. AFTER REF NDT PART 6, 53-00-06 REPAIR INSP REQUIREMENTS ARE AS FOLLOWS PER SRM 53-00-01-2R-31 RPR 31 TABLSDR CALA2021111702115Stringer · crackedAFT CARGO COMPT STA 1205 S-36L AREA FOUND CORROSION CRACK. TRANSFER REF NR LP 9131558 AND ORIGINATED BY V897013. AFT CARGO COMPT STRINGER 36L BETWEEN STA 1197+120VAND STA 1219 REPAIRED AS PER SRM 53-00-03 REPAIR 2 FIG 201. WORK ACCOMPLISHED BY MECHANIC V897532SDR CALA2021111502105None · corrodedAFT CGO COMPT STA 1285 LBL 24" FLOOR BEAM UPPER CHORD FOUND CORROSION CRACK. TRANSFER REF. HX NON-ROUTINE LP 9131773 AND ORIGINATED BY EMP NO. V896921 AFT CARGO COMPT STA 1285 LBL 20.5 - LBL 25.5 WL 123 FRAME INNER CHORD J SECTION REPAIRED AS PER EC/RA 5360-01SDR CALA2021110502041Beam · elongatedB767-53-3-7141 CABIN STA 544 LBL 55-68 FLOOR SUPPORT HOLE FOUND ELONGATE. TRANSFER REF. NON-ROUTINE LP 9131173 AND ORIGINATED BY EMP V927004. CABIN BS 544 FLOOR BEAM UPPER CHORD BETWEEN LBL 55 AND LBL 88 REPAIRED AS PER EC/RA 5315-01163 REV-. ADD EMP:V896920 SDR CALA2021110302031None · noneB767-53-3-7141 CABIN STA 544 LBL 55-68 FLOOR SUPPORT HOLE FOUND ELONGATE. TRANSFER REF. NON-ROUTINE LP 9131173 AND ORIGINATED BY EMP V927004. CABIN BS 544 FLOOR BEAM UPPER CHORD BETWEEN LBL 55 AND LBL 88 REPAIRED AS PER EC/RA 5315-01163 REV-. ADD EMP:V896920 SDR CALA2021110302021Beam · noneB767-53-3-0166 CABIN - BS1500 RBL10 FLOOR SUPPORT HOLE ELONGATED AS MARK. TRANSFER REF. NON-ROUTINE LP 9131246 AND ORIGINATED BY EMP V896926. CABIN BS 1500 FLOOR BEAM UPPER CHORD RBL 10 REPAIRED AS PER SRM 53-00-51 REPAIR 2 FIG 201. ATTACHED FORM 44-0008 ITEMSDR CALA2019032500463Bulkhead · crackedREF NR LP B767-06-3-7059 CABIN : STA 955 TO 975 RBL 30 CANTED PRESSURE DECK WEB FOUND CRACK CABIN STA 955 TO STA 975 RBL 30 CANTED PRESSURE DECK WEB INTERIM REPAIRED AS PER EC/RA 5358-01001 REV - PART 1.SDR CALA2019020100202Structure · cracked02MAR HKG CF -L :LH STA 1809 HORIZ INNER CHORD 1 EA FAST FN D CRK AT 8 O''CLK POS RUNNING TO EDGE.AREA REPAIRED PER EA 5312-0 1059 REV B OP9 STEP 1 AND SRM 53-80-08 REP 10 FIG 201 DET II.REP EAT INSPECTION AS PER SRM 53-80-08 REP 10 TBL 202, INSP THRESHOL D ISSDR CALA2018022300763Fuse · inoperativeEXTERIOR EMERGENCY LIGHT LEFT SIDE OF AIRCRAFT INOPERATIVE. REPLACED THE FUSES IN M738 CHARGER. OPS CHECKED NORMALSDR CALA2018022300765Lamp · inoperativeOVERHEAD EMERGENCY LIGHT AT SEAT ROW 19K INOPERATIVE. REPLACED THE LAMPS. OK FOR SERVICE.SDR CALA2018022300764Lamp · inoperativeOVERHEAD EMERGENCY LIGHT AT ROW 4K INOPERATIVE. REPLACED THE LAMPS, OK FOR SERVICE.
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