N663UA
Service difficulty reports · 347
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 = 'N663UA' 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 = 'N663UA' 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 CALA2026052616525Light · faultedRED PATHWAY EMERGENCY LIGHT INOP FWD OF SEAT 20K . REQUESTING DEFERRAL LENS CRACKED BUT WORKING RED PATHWAY EMERGENCY LIGHT FWD OF SEAT 20K HAS A CRACK BUT WORKING. DEFERRED REF NEF 2520TP DEFERRED REMOVED AND REPLACED LIGHT ASSEMBLY. OPS TEST GOOD. REF AMM 33SDR CALA2026031314546Light · brokenGALLEY 2A EMERGENCY LIGHT FOUND BROKEN REPLACED EMERGENCY LIGHT ASSY AND OPS CHECK SATISFACTORY WRT SWPM 20-30-00. PARTS USED: 25-3351-3-0008, QTY :1SDR CALA2026012013107Light · inoperativeFOUND PATHWAY LIGHT ON SIDE OF SEAT 39D INOP. FOUND 39F LIGHT INOP AS WELL. REPLACED BOTH PATHWAY LIGHTS AT SEATS 39D AND 39F. STILL NOT WORKING. REFERENCE CMM 25-23-52. DISCONNECTED BOTH PATHWAY LIGHTS AT 39 D&F. MEASURED 6V AT BOTH CONNECTORS AND MEASURED GSDR CALA2025112411413Bottle · no discrepancySLIDE PRESSURE DOOR 2L NOT IN GREEN PERFORMED VISUAL INSPECTION OF DOOR 2L SLIDE PRESSURE GUAGE, FOUND WITHIN TOP OF GREEN BAND, WITHIN LIMITS, REF CYLINDER CHECKTASK 25-66-02-206-001, OK TO CONTINUE.SDR CALA2025100309574Lamp · inoperativeEMERGENCY LIGHTS, LT FWD ESCAPE SLIDE EMERGENCY LIGHT INOP, ESCAPE LIGHT LAMP RESEATED AND TESTED IAW AMM 33-51-06-902-082, LIGHT NOW OPERATES.SDR CALA2025082808210Bottle · no discrepancyPLEASE CHECK DOOR 2L PRESSURE GAUGE INSPECTED DOOR 2L PRESSURE GUAGE. FOUND NEEDLE ONE NEEDLE WIDTH OVER (TOWARDS HIGHER END OF BAND) IAW AMM 25-66-02 A/C OK TO CONT. NOTE: A/C CABIN WAS HOT PRIOR TO APU PACKS BEING TURNED ON.SDR CALA2025070206141None · no discrepancyDURING A/C REFUELING, PRIOR TO ENG OR APU START, 1 F/A REPORTED STRONG FUEL SMELL IN ACFT. NO OTHER CREW OR PASSENGERS WERE EFFECTED BY ODOR. CAPTAIN WALKED TO BACK OF ACFT ON 3 DIFFERENT OCCASIONS AND NEVER NOTICED ANY SMELL OR FUMES/ VISIBLE SMOKE. STONG SMSDR CALA2025063006080Compressor · no discrepancyLOUD BANG AND BRIGHT FLASH ON LEFT SIDE AFTER TAKE OFF POSSIBLE BIRD STRIKE CREW SAID THEY FELT KICKED TO THE LEFT WITH THE LOUD BANG AND THE WHITE FLASH FROM THE LEFT SIDE, ACCMP OVERWEIGHT LANDING INSPECTION AND BIRD STRIKE INSPECTION. REF AMM TASK 05-51-35-SDR CALA2025061605571Module · faultedOXYGEN MASKS DEPLOYED AT SEAT 11F RESTOWED PAX 02 MASKS ABOVE SEAT 11F REF AMM 35-21-15-532-150-001.SDR CALA2025052604946Unknown · vibrationAIR RETURN FOR VIBRATIONS IN FLIGHT CONTROLS CREW DEBRIEF STATED AT 10,000 FT FELT VIBRATION IN THE CAPTS AND FOS YOKE IN CLIMB TO CRUISE AT SPEEDS OF 250,280 TO 320 THE INTENSITY RAMPED UP AND STAYED THERE IN ALL PHASES OF FLIGHT. DURING TURNS, ASCENDING ANDSDR CALA2025031402816None · noneAFT LEFT DOOR PRESSURE GAUGE BELOW GREEN. VERIFIED GUAGE IS WITHIN SERVICABLE RANGE.SDR CALA2025022502470Sensor · faultedTEST FLIGHT DISCREPANCY . . LE EDGE SLAT ASSYMETRY I N CLIMB. POSSIBLE OVERSPAT 33000 FEET, AIR SPEED REACHED 300 KNOTS FOR A SHORT PERIOD TIME. 50 KNOTS ABOVE MAX SPEED OF 250KNOTS PLUS NOTICED L.E FLAPS INDICATIONS START TO MOVE ALSO. BELOW 250KNOTS EVERYTHISDR CALA2025021400349Access Panel · crackedDURING THE ACCOMPLISHEMENT OF EA 5300-01600-004, IT WAS FOUND A CRACK ON THE FORWARD OUTER CHORD INSIDE THE HORIZONTAL ACCESS PANEL. CHORD, RH PERMANENT REPAIR. THE PERMANENT REPAIR OF RH CHORD WAS ACCOMPLISHED AT TASK 76-0553-8-0153 AS PER EA5300-01600, OP 05SDR CALA2025021100334Skin · damagedDURING REMOVAL OF STATIC DISCHARGER BASE ON THE RUDDER WAS FOUND UNDER THE BASE FOUR HOLES OUT OF STANDARD ON LH SIDE AND ONE RH SIDE THE RUDDER UPPER PANEL SKIN STATIC DISCHARGER WAS REPAIRED AS PER EC/RA: 5540-01602. ITEM OK TO SERVICE. ALL APPLICABLE INSPESDR CALA2025021000324Spar · crackedRII INSPECTION REQUIRED DURING DVI OF STRUT #2 FIRE SEAL AND FIREWALL - TOP SURFACE INSPECTION WAS OBSERVED CRACK ON NACELLE STRUT FWD UPPER SURFACE. ACCOMPLISHED ALL EC/RA# 5451-01467 STEPS.SDR CALA2025020900315Floorbeam · corrodedTHERE ARE CORROSION POINTS ON THE BEAM LOCATED AT STA287 BETWEEN LBL 45.0 AND LBL 50.0 OF MAIN DECK FLOOR STRUCTURE. FOR REFERENCE SEE B767 SRM 53-10-51-0I-1 FIGURE 1 DETAIL I ITEM 20. (ORIGINATING DOCUMENT NR 2426011) AS COVERED IN NR 2426011 ALL STEPS OF EC/SDR CALA2025020500297Shear Tie · corrodedDURING REMOVAL OF SHEAR TIE WAS FOUND OLD EXTERNAL DOUBLER SKIN WITH CORROSION AT STA 1540 AND BETWEEN STGR 39 LH AND 39RH (ORIGINATING DOCUMENT NR 2422715). ERMANENT SOLUTION WITH INSPECTION REQUIREMENTS THAT MUST BE ACCO 0 ON OR BEFORE THE AIRCRAFT REACHES 2SDR CALA2025020200251Skin · crackedIT WAS FOUND A CRACK INDICATION AT FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER AFTER NDT INSPECION PART 6 51-00-16 REV 139. (ORIGINATING DOCUMENT NR2396712)SDR CALA2025012900234Skin · crackedFWD SERVICE DOOR AFTER CUTOUT - IT WAS FOUND A SKIN AND BEARSTRAP CRACK INDICATION IN THE MARKED HOLE AT 1 AND 7 ON''CLOCK POSITION. ( ORIGINATING DOCUMENT NR 2395993)SDR CALA2024093000711Unknown · odorSMELL OF ELECTRICAL SMOKE SMELLED IN ROW 42 PER CREW LIGHT IN THAT AREA FLICKERED FOR A MOMENT DURING EVENT OF SMELL REF L/P 9364747. DURING AND AFTER HIGH POWER ENGINE RUNS NO ELECTRIC SMELL OR FLICKERING LIGHTS NOTICED.CONDITIONAL INSPECTION REQUIRED BY TOMCSDR CALA2024072502099Escape Hatch · obstructedDURING REMOVAL OF LH OVERWING ESCAPE HATCH REF LOGPAGE 8707327, ESCAPE HATCH DOOR HITS LH CABIN CLASS DIVIDER FRAME PREVENTING CORRECT OPERATION OF EMERGENCY EXIT DOOR. CABIN CLASS DIVIDER ADJUSTED FORWARD ON SERATED PLATE AND CONFIRMATION OF ECAPE HATCH DOOR SDR CALA2024052201559None · nonePAX AT SEAT 5A DROPPED 13IN MACBOOK AIR INTO SIDEWALL. UNABLE TO RETREIVE OPENED LWR DECK LH SIDE WALL PANEL AT DRIVE BAY D. RETRIEVED 13 INCH MAC BOOK AS DESCRIBED AND GIVEN TO PILOT. INSPECTED AREA BEHIND DRIVE BAY ''D'' LH SIDE WALL PANEL - NO DAMAGE OR IRRSDR CALA2024040200925Socket · inoperativeIDT INSPECTION REQUIRED. EMERGENCY PATH LIGHT ASSY REPLACEMENT. EMERGENCY PATH LIGHT REPLACED SEE LOGPAGE: 7475861. IDT INSP REQUIRED. EMERGENCY LIGHT AT 228FR RT SIDE OF FRONT GALLEY INSPECTED REF AMM 33-51-10-962-173 AND SWPM SECTION 20-83. ALL FOUND SATISFASDR CALA2024032900916Light · no testEMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - GALLEY 2A COMPARTMANT 228F/R EEL LIGHT INOP. RELAMPED THE EEL NIL HELP. EEL ASSY. SUSPECTED. PARTS ORDERED. EEL ASSEMBLY REPLACED IAW AMM: 33-51-10-962-173 AND SWPM: SECTION 20-83. LIGHT TESTED AND CONFIRMESDR CALA2024032100814Hose · leakingRIGHT MAIN LANDING GEAR DID NOT RETRACT AFTER TAKEOFF UPON ARRIVAL FIND OUT A MAJOR HYDRAULIC LEACK ON RIGHT MLG SUSPECTED TWO RIGID LINES SEE PICTURES FOUND RETRACT SYS HYDRAULIC HOSE LEAKING ABOVE R MLG, UNDER THE RETRACT ACTUATOR. REF IPC 32-32-54-05 ITEM SDR CALA2024020500326Skin · damagedLIGHTNING STRIKE ON EXTERIOR SKIN LOCASTED APPROX. STA 654+121 STR 34R. 53-00-01-2R-29 REPAIR 29. REPAIRED LIGHTNING STRIKE ON EXTERIOR SKIN AT STA 654+121 STR 34R PER B767-300 SRM RII INSPECTION FOR MJR-RII-SDR EXTERNAL FUSELAGE SKIN DOUBLER REPAIR ACCOMPLISSDR CALA2024020200299Angle · cracked#1 ENGINE PYLON I/B AND O/B SIDE HAS 2 EA. PANEL ATTACH STRAPS CRACKED ON AFT PYLON FRAME STA 410.SDR CALA2024013000256Support Angle · crackedFIXED LE BRACE SUPPORT AT WS 530 CRACKED. REPLACED FIXED LE BRACE SUPPORT AT WS 530 IAW B767-300 SRM 51-40 -02.SDR CALA2024010500033Display · intermittentFO CDU BLANK. CDU FUNC NORMAL UNTIL CRUISE THEN FLICKERED AND BL ANKED REF LOGPAGE 6732059 FOR LOGPAGE SIGNOFF.**CHRONIC LVL-0**DUE TO RECENT HISTORY OF FIRST OFFICERS CDU NOT RESPONDING OR FLICKERING ACCOMPISH THE FOLLOWING: 1) FIM 34-61 TREE 843, REPAIR AND SDR CALA2023071202222Shutoff Valve · failedR ENG HPSOV EICAS ON T/O ROLL WITH ASSOC BLEED LIGHT. BLEED LIGHT DID NOT EXTINGUISH. V347 FAILED INTERNAL ELECTRICAL CHECK PER WDM 36-11-62, NEEDS NEW VALVE, REF AHM LP 5113215. REF AMM#36-11-18 REMOVED AND REPLACED HPSOV. LEAK AND OPS CHECKS GOOD WITH NO FUSDR CALA2023010900056Circuit Breaker · trippedTAT PROBE EICAS MSG AFTER LIFT OFF. RAN QRH AND RETURED TO EWR. FLIGHT CREW STATES L TAT PROBE C/B TRIPPED WITH ASSOCIATED EICAS MSG. RESET C/B AND PERFORMED TAT PROBE HEAT SYSTEM OPERATIONAL TEST REF AMM 30-33-00-715-710. TEST PASSED SEVERAL TIMES WITH NO FAUSDR CALA2022120503288Battery Pack · no testSEVERAL EMERGENCY LIGHT INOP THROUGH OUT THE CABIN AREA. (REF AAR NR 9669188) REMOVED AND REPLACED BATTERY PACK POS M732 AS PER B737 AMM 33-51-02. PERFORMED OPS CHECK AND FOUND NORMAL ASSOCIATED EMERGENCY LIGHTS.SDR CALA2022120503287Battery Pack · no testEMERGENCY ESCAPE SYS R FAILED TEST ON P 61.( EMERGENCY BATT. PACKS M962 (DISCHARGED) (REF AAR NR 9669192) REMOVED, REPLACED AND TESTED NORMAL M962 BATTERY FOR EMERGENCY ESCAPE RIGHT SIDE, PUSH TO TEST TESTED NORMAL REF B767 AMM 25-65-17-004-001-001, 25-65-17-4SDR CALA2022120503286Battery Pack · no testEMERGENCY ESCAPE SYS L FAILED TEST ON P 61.( EMERGENCY BATT. PACKS M 961 (DISCHARGED) (REF AAR NR 9669191) REMOVED, REPLACED AND TESTED NORMAL M961 BATTERY FOR LEFT EMERGENCY ESCAPE, PUSH TO TEST TESTED NORMAL REF B767 AMM 25-65-17-004-001-001, 25-65-17-404-00SDR CALA2022082202135Battery · inoperativeROWS 21-23 AISLE EMERGENCY FLOOR LEVEL LIGHTING AND L+R OVERWING EXIT SIGNS AND RIGHT AISLE OVERHEAD EXIT SIGNS REMAIN ILLUMINATED WHEN AIRCRAFT IS DOWN POWERED WITH P5 EMERGENCY LIGHT SWITCH IN THE "OFF" POSITION. AIRCRAFT COMPLETELY DOWN POWERED WITH EXTERNASDR CALA2022060801464Duct · failedPER CREW AT 7000'' RIGHT DUCT LEAK LIGHT CAME ON WITH RIGHT BLEED DUCT LEAK EICAS MESSAGE. AT 14,000'' DUMPED 10,000 LBS FUEL. RAN CHECKLIST NO FIX. LANDED ROUGHLY 20,000 LBS OVERWEIGHT. ON P11 OPENED BUT REAPPEARS WHEN CLOSED. RAN FIM 26-18 FAULT TREE 804 BLOSDR CALA2022022400494Engine · failed2 LOUD BANGS FOLLOWED BY RIGHT ENG POWER LOSS - PWR CAME BACK W/IN 10 SECS AT 10000 FEET. R ENG SURGE DET MESSAGE SEE PICTURES FOR INFO. RT ENG PIMU BITE REVEALED NO RELATED OR ASSOCIATED MESSAGES AS T CONTINUING WITH FIM-71-05/803 BLOCK 2 THRU BLOCK 6, VISSDR CALA2022011400151Plate · dentedRIGHT INBOARD TRAILING EDGE FLAT HAS NUMEROUS DENTS DUE TO HAIL SHOULD READ TRAILING EDGE FLAP. REF SRM 57-53-01-1A-1 LOCKED FOR FERRY FLIGHT - ESC EVALUATED ALLOWABLE DAMAGED. UNLOCKED TO CLEAR LOGPAGE REFER FORM44-0008 ITEM1-32 ACCOMPLISHED. WORK ACCOMPLISHESDR CALA2022011200118Beam · corrodedB767-53-3-7154 AFT CARGO COMPT - FLOOR SUPPORT BEAM BOTTOM SIDE 5EA ANCHOR NUT AREA CORROSION FOUND STA1153 BTN RBL9" TO LBL36" AS MARKED. TRANSFER REF. NON - ROUTINE ZHF510485 AND ORIGINATED BY EMP V896820 AFT CARGO COMPT STA1153 FLOOR BEAM UPPER CHORD REPLACSDR CALA2022011000084None · corrodedB767-53-3-7154 AFT CARGO COMPT - FLOOR BEAM BOTTOM SIDE SEVERAL ANCHOR NUT AREA CORROSION FOUND AT STA1329 BTN RBL16"-RBL29" AS MARKED. TRANSFER REF. NON - ROUTINE ZHF513877 AND ORIGINATED BY EMP V896820 AFT CARGO COMPT STA1329 BETWEEN LBL43 AND RBL43 FLOOR BESDR CALA2022011000083None · corrodedB767-53-3-7025 FWD CARGO COMPT - FLOOR BEAM UPPER SURFACE CORROSION CRACK AT STA632 BTN LBL30"-LBL32" AS MARKED. TRANSFER REF. NON - ROUTINE ZHF516482 AND ORIGINATED BY EMP V896820 FWD CARGO COMPT STA 632 BETWEEN LBL 43 AND RBL 43 FLOOR BEAM UPPER CHORD REPLACSDR CALA2022011000105None · corrodedB767-53-3-7154 AFT CARGO COMPT - FLOOR SUPPORT BEAM BOTTOM SIDE 5EA ANCHOR NUT AREA CORROSION FOUND STA1153 BTN RBL9" TO LBL36" AS MARKED. TRANSFER REF. NON - ROUTINE ZHF510485 AND ORIGINATED BY EMP V896820 AFT CARGO COMPT STA1153 FLOOR BEAM UPPER CHORD REPLACSDR CALA2022011000103Skin · noneSUPPORT TASK - BULK CARGO DOOR OUTER SKIN AFT EDGE PREVIOUS REPAIR DOUBLER HAS DENT. TRANSFER REF. NON - ROUTINE ZHF517134 AND ORIGINATED BY EMP V896888 RII INSPECTED BY HX169509 ADD EMP:V898550 BULK CARGO DOOR OUTER SKIN INTERIM REPAIRED AS PER ECRA 5236-0102SDR CALA2022010700067Shear Tie · corrodedB767-53-3-7056 BULK CARGO COMPT - BELOW FLOOR SHEAR TIE CORROSION FOUND AT STA1540 S37R-S38R AS MARKED TRANSFER REF. NON - ROUTINE ZHF512861 AND ORIGINATED BY EMP V896820 BULK CARGO COMPT STA1540 BETWEEN STR37R AND 38R SHEAR TIE REPLACED AS PER SRM51-10-02 ATTSDR CALA2022010700051Floorbeam · corrodedB767-53-3-7025 FWD CARGO COMPT - FLOOR BEAM UPPER SURFACE CORROSION CRACK AT STA632 BTN LBL30"-LBL32" AS MARKED. FWD CARGO COMPT STA 632 BETWEEN LBL 43 AND RBL 43 FLOOR BEAM UPPER CHORD REPLACED AS PER SRM 51-10-02.SDR CALA2022010700050Floorbeam · corrodedB767-53-3-7154 AFT CARGO COMPT - FLOOR BEAM BOTTOM SIDE SEVERAL ANCHOR NUT AREA CORROSION FOUND AT STA1329 BTN RBL16"-RBL29" AS MARKED. TRANSFER REF. NON - ROUTINE ZHF513877 AND AFT CARGO COMPT STA1329 BETWEEN LBL43 AND RBL43 FLOOR BEAM UPPER CHORD REPLACED ASSDR CALA2022010300008Bracket · corrodedB767-53-3-7077 CABIN - LH STA999 S-16L TO S-17L SHEAR TIE FOUND CORRODED. TRANSFER REF. NON - ROUTINE LP9130759 AND ORIGINATED BY EMP V926653 CABIN BS999 BETWEEN STR16L AND STR17L SHEAR TIE REPLACED AS PER SRM51-10-02 AND INSTALLED AS PER SRM51-40-02, ATTACH FSDR CALA2022010300007Bracket · corrodedB767-53-3-7077 CABIN - S16L - S17L JOINT BRACKET FOUND CORRODED. TRANSFER REF. NON - ROUTINE LP9130782 AND ORIGINATED BY EMP V923418 CABIN BS977 BETWEEN STR16L AND STR17L SHEAR TIE REPLACED AS PER SRM51-10-02 AND INSTALLED AS PER SRM51-40-02, ATTACH FORM 44-00SDR CALA2021122902478Bracket · corrodedB767-53-3-7077 CABIN - S16L - S17L JOINT BRACKET FOUND CORRODED. TRANSFER REF. NON - ROUTINE LP9130782 AND ORIGINATED BY EMP V923418 CABIN BS977 BETWEEN STR16L AND STR17L SHEAR TIE REPLACED AS PER SRM51-10-02 AND INSTALLED AS PER SRM51-40-02, ATTACH FORM 44-00SDR CALA2021122702442Shear Tie · corrodedB767-53-3-7056 BULK CARGO COMPT - BELOW FLOOR SHEAR TIE CORROSION FOUND AT STA1540 S37R-S38R AS MARKED TRANSFER REF. NON - ROUTINE ZHF512861 AND ORIGINATED BY EMP V896820
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