N664UA
Service difficulty reports · 398
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 = 'N664UA' 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 = 'N664UA' 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 CALA2026092119563Flashlight Assy · dischargedGALLEY 6 FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT INOP. FLASHLIGHT AT G6 FLIGHT ATTENDANT SEAT REMOVED & REPLACED PER TASK 25-60-00-210-801-C1. OP CHECK OKAY.PARTS USED: 78-2500-3-0845, QTY :1SDR CALA2026091119369Pca · faultedREPEAT WRITEUP. LT WING INBD AILERON NOT FULLY STOWED INFLIGHT. MULTIPLE FLT CONTROL ISSUES ON FINAL DUE TO WINGS HAVING MISMATCHED AILERON POSITIONS & RT WING HAVING TO CORRECT FOR LT WINGS POSITION. LT INBD AILERON SITTING HIGH IN FLT, ACRT ON RT AUTOPILSDR CALA2026060416828Drain · crackedNR 2 NACELLE STRUT FORWARD UPPER SPAR DRAIN HOLE WITH A CRACK. NR 2 NACELLE STRUT FORWARD UPPER SPAR DRAIN HOLE, THE INTERIM REPAIR WAS PERFORMED SATISFACTORILY IAW ECRA 5450-03126 REV A PART 1 STEP 1, AND MDE JIC B76-54-0001 R01.SDR CALA2026060316762Longeron · crackedRIGHT SIDE UNDERWING LONGERON REQUIRES REPLACEMENT OPS 550032484 AND EA 5710-02896 OPS 008. RT SIDE UNDERWING LONGERON REPLACEMENT OP 008 OVERVIEW WAS ACCOMMPLISHED SATISFACTORILY IAW EA 5710-028 96 REV B OP 008SDR CALA2026043015854Battery Pack · faultedRH OVERWING EMERGENCY BATTERY PACK AT SEAT 21A NEEDS TO BE CHANGED. R & R RH OVERWING EMERGENCY BATTERY PACK REF AMM 33-51-07.SDR CALA2026022614082Light · failedEMERGENCY FLOOR LIGHTS FROM 30FED TO 35FED ALL DIM WITH A BURNING ODOR IN SURROUNDING AREA. 31F - FLOOR PROXIMITY EMERGENCY LIGHT FOUND TO BE DAMAGED AND BURNED OUT AND EXPLAINS BURNING ODOR IN SURROUNDING AREA. LIGHT ASSY REPLACED IAW CMM 25-23-52. OPS TEST CSDR CALA2026012613249Unknown · odorAFT GALLEY FLT ATTENDANTS REPORTED AN ODOR DURING FLIGHT. DE-BRIEFED FLT CREW AFTER INBD FLT ZRH-ORD. PILOTS STATED AT NO POINT DURING THE FLT DID THEY EXPERIENCE ANY SMOKE/ODOR, NO ABNORMAL INDICATIONS IN FLT DECK. 3 FLT ATTEDANTS REPORTED TO FEEL LIGHT HEASDR CALA2026012613244Unknown · smokeNEED TO PERFORM SMOKE ODOR, CONDITIONAL INSPECTION CREW DEBRIEFING REFERENCE: TASK 05-51-56-940-801-C1 PERFORMED VISUAL INSPECTION OF OVENS AND COFFEE MAKERS FOR BURNING AND ARCING INSIDE AND BEHIND. NO EVIDENCE NOTED IN AFT GALLEY. ALSO OPS CHKD EACH OVEN BYSDR CALA2025122312319Girt Bar · fodL2 DOOR WHEN ARMING, THE YELLOW FLAP THAT IS SUPPOSE TO COME OUT AND BLOCK HANDLE, STICKS FOUND DEBRIS IN GIRT BAR FLOOR BRACKETS. PERFORMED CLEANING AND LUBRICATION OF DOOR L2 GIRT BAR FLOOR LINKAGE. OPS TEST GOOD. YELLOW FLAG IS ENGAGING WITHOUT INTERFERENSDR CALA2025120811899Duct · crackedBELOW 50 PERCENT THRUST LT ENG ANTI ICE VALVE CAME ON A FEW TIMES THEN RESOLVED PERFORMED L ENG IDLE RUN FOUND LT ENG ANTI-ICE VALVE LIGHT INTERMITTENTLY ILLUMINATED, C/W AMM 36-11-00-715-149, ASPCU OPERATIONAL TEST. FOUND ASPCU SHOWING LT HPSOV FAULT. FOUSDR CALA2025120411777Transducer · faultedANTI-SKID EICAS MESSAGE, BITE SHOWED BOX 4-8 & XDCR-4 AFTER RESET XDCR-4 PERSISTENT.SWAPPED POSN 4 WITH POSN 3 XDCR & FAULT MOVED ALONG INDICATING XDCR-3. REPLACED NR 4 TRANSDUCER & FAULT REMAINED UNABLE TO CLEAR. REPLACED & RESET AACU M102 FAULT 4-8 ISOLATSDR CALA2025100909845Oven · contaminatedCREW REPORTED, ON APPROACH THE SMELL OF BURNING RUBBER FOR ABOUT 5 MINS. SMELL WENT AWAY AFTER LANDING. RAN BOTH ENGINES IAW AMM 71-00-00 AND SUPPLIED PACKS WITH ENGINE BLEED, NO SMELL NOTED. RAN PACKS FOR HOURS WITH APU BLEED AND NO SMELL NOTED, ACCOMPLISSDR CALA2025092909368Contactor · missingAPU CRANK CONTACTOR U/S ON FIT. APU CRANK CONTACTOR FOUND TO BE MISSING END STOP CAUSING CONTACTS TO BE MADE, NOTICED AFTER UNCOMMANDED APU START ON APU BATTERY CONNECTION. DEFECTIVE ON FIT APU CONTACTOR REPLACED AS PER AMM TASK 49-41-05-404-005. APU CRANK CSDR CALA2025091508948Unknown · fumesFLT ATTNDS SAID THEY ALL HAD THESE SYMPTONS. DIZZY HEADACHE SINUS PAIN AND SHAKES. DVRT TO DUB FLIGHT DECK CREW DEBRIEFED AND THEY ADVISED NO ILL EFFECTS ON THEIR SIDE, NO SMELL OR ABNORMALITY NOTICED IN FLIGHT DECK. NO PRESSURIZATION ISSUES OR AIR CONDITIONISDR CALA2025072106758Elec Connector · arcedCONNECTOR D256A FOUND WITH EVIDENCE OF ARCING AT PINS C15, D15 & D13. REQUIRES FURTHER INVESTIGATION. CONNECTOR D256 FRAME REPLACED ALONG WITH D256A PLUG INSERT. REFITTED ORIGINAL D256B AND D256C PLUG INSERT INTO NEW FRAME. IAW SWPM 20-71-14 PAGE 165/166. D256SDR CALA2025063006077Door · crackedDURING E1 INSPECTION FOUND UPPER BLOCKER DOOR ON INBOARD T/R CRACKED ALONG WITH METAL LINER DIRECTLY FWD OF IT. ACCOMPLISHED STEPS 1-3 INTERIM REPAIR PER ECRA 7831-03622. PERFORMED PART 1 INTERIM REPAIR STEP 4 OF ECRA 7831-03622. MEL 7831C ACCOMPLISHED.SDR CALA2025062705991Access Panel · missingRIGHT WING LEADING EDGE PANEL 621DB IDENTIFIED AS AN OUTBOARD LE SLAT MECHANISM LUBRICATION ACCESS DOOR/PANEL. DISCREPANCY PLACED ON CDL 57F LOG 5326724SDR CALA2025062005742Flashlight · no testON WALK FOUND L1 DOOR EMERGENCY FLASHLIGHT NOT TESTING. REPLACED BATTERY ON L1 DOOR FLASHLIGHT AND RESEALED AS REQUIRED. OPS CK AND TEST NORMAL.SDR CALA2025061805667Warning Light · false activationR AFT ENT DOOR EICAS AND ENTRY DOOR OVERHEAD LIGHT ON DURING TA XI IN. AFTER R ENG SHUTDOWN. FAULT NOT CONFIRMED. INTERNAL AND EXTERNAL DOOR OPERATIONAL CHECK REF B767-300 AMM 52-11-00-715-128 PERF. SATISF. OK FOR SERVICE.SDR CALA2025060905396Housing · excess playR WING SLIDE EICAS LT ILLUMINATED IN FLIGHT.DEBRIEF WITH CREW: CREW REPORTED STEADY INDICATION IN CRUISE , BUT IN CLIMBING AND DESCENDING THE INDICATION WAS INTERMITTENT PREFORMED CONTINUITY CHECK OF WIRING OF SENSOR S219 AND CHECKED FOR SHORTS AT PSEU BOX MSDR CALA2025060905370Pin · faultedREFERENCE 5076268, AND 5076026 PSEU BITE TEST ACC B767-300 AMM 32-09-04-704-013 ACTIONED AND FOUND CODE MESSAGE 219 (RELATED TO RH WING SLIDE SENSOR CLOSED). NEED CHECK AND ADJUST DOOR CLOSED SENSOR (S219 RIGHT SIDE) FOR THE SLIDE COMPARTMENT DOOR AS REQUIRED SDR CALA2025042104051Stringer · corrodedDURING INSPECTION OF LH AND RH STABILIZER TORSION BOX COMPARTMENTS (INTERNAL), IT WAS FOUND SIGNS OF CORROSION AT STRINGER S-36L BETWEEN STA 1809.50 AND 1843.00. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR PER GMM 09-25-05 AS PER GMM 09-25-05 THE REPAIR IS CLASSSDR CALA2025042104050Stringer · corroded(ZONES 313, 314) DURING INSPECTION OF LH AND RH STABILIZER TORSION BOX COMPARTMENTS (INTERNAL), IT WAS FOUND SIGNS OF CORROSION AT STRINGER S-36R BETWEEN STA 1809.50 AND 1843.00. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR PER GMM 09-25-05 AS PER GMM 09-25-05 THSDR CALA2025032503161Flag · stuckDOOR 2L ARM FLAG STUCK ARMING FLAG RELEASED AND ARMING LEVER CYCLED. OPERATIONAL CHECK NOW SATISFACTORYSDR CALA2025010601815Unknown · odorAFTER ENG START AFTER PACKS ON 4 AFT FLT ATTDS REPORTED FUMES AN D ODOR C/O INSPECTIONS SATIS ON AFT CABIN LAV'S/OVENS/COFFEMAKERS/CHILL ERS/CB'S/LIGHTS ACC. AMM. 05-51-56-940-801-C1 REV. 143. C/O PACK 1 AND 2 OPS WITH APU ONLY. NO SMELLS NOTICED. C/O EGR WITHSDR CALA2025010601812Unknown · odorDUE TO ODOR IN CABIN AFTER ENGINE START, INSPECTIONS SATIS ON AFT CABIN LAV'S/OVENS/COFFEMAKERS/CHILL ERS/CB'S/LIGHTS ACC. AMM. 05-51-56-940-801-C1 REV. 143. C/O PACK 1 AND 2 OPS WITH APU ONLY. NO SMELLS NOTICED. C/O EGR WITH BOTH ENGINES RUNNING AND BOTH PACSDR CALA2024111301123O-Ring · leakingFUEL LEAK LEFT WING OBSRVED IN FLIGHT DIVERT LHR PHOTOS ATTACHED OF FUEL LEAK FROM LEFT WING VIEWED FROM INSIDE CABIN. PHOTO UPDATE FROM OUTSIDE AT WING LEVEL ON ARRIVAL. SDR UPDATE L/H WING OVERWING FILL PORT HOUSING AND CAP INSPECTED. FILLER CAP AND PACKINGSDR CALA2024061001754Connector · corrodedAFTER MAINTENANCE EFFORT ANTI SKID CAUTION & NORM ANTI SKID STATUS MSGS INTERMITTENTLY POST MEL PROCEDURE B SUGGESTED BY PULLING CB LDG GR ANTI SKID 3-7 MEL COMPLIED WITH. PROCEDURE B APPLIED . VALVE NR 3 CONNECTOR FOUND CORRODED. NR 3 BRAKE TEMP SENSOR CHSDR CALA2023090502715Isolation Valve · unknownREJECTED TAKEOFF AROUND 60 KNOTS DUE TO R ISLN VALVE DISPLAYING UNABLE TO DUPLICATE THE CONDITION, HIGH POWER ENGINE RUN WAS PERFORMED BY U101442 NO DEFECTS NOTED DURING THE RUN NO EICAS OR LIGHTS ON ISLN VALVES , AIRCRAFT GOOD FOR SERVICESDR CALA2023060701785Panel · missing#2 ENGINE LH INBD ROUND PANEL FOUND MISSING ON ETOPS CHK IPC 54-53-01-17 ITEM400 REPLACED MISSING PANEL REQUESTING PANEL PLACED ON EXT FOR PAINTSDR CALA2023051501492Shutoff Valve · leakingC HYD QTY ILLUMINATED 7 HOURS INTO FLT HYD SYSTEM LEAK CHECK ACCOMPLISHED IAW AMM TASK ACCOMPLISHED IAW AMM TASK 27-51-48-022-001 & TASK 12-12-01-613-059. PARTS USED: 00-0606-3-0024,QTY :1 29-00-97-306-003. FLAP SLAT SHUT OFF MODULE OBSERVED TO BE 27-51-48-42SDR CALA2023051201471Shutoff Valve · failedRIGHT ENG BLEED SHIFT FAILED TEST AT FL 350. HIGH STAGE VLV OPEN ED AT 0.89 EPR REPLACED HPSOV IAW B767 AMM 36-11-07-002-002 OPS /LEAK CHECK GOO D. SEE PARTIAL WORK COMPLETED AND PARTIAL SHEETS (1) PG 5 1 & 2. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1779046SDR CALA2023050501367Skin · corrodedAFT LOWER CORNER FASTENER HOLE HAS CORROSION IN IT AT THE L1 DOOR CUTOUT. REPAIRED L1 DOOR SKIN AT AFT LOWER CORNER IAW B767 SRM 53-10-01 REPAIR 1 FIG 201 DETAIL III, AND ECRA 5310-08135.SDR CALA2023050501354Skin · unknownOPEN AMES WORK PACK N664UA-1 FOR C-4 MAINTAINENCE CHECK.SDR CALA2023042801265Floor Support · corrodedCORROSION ON TOP SIDE OF FLOOR PANEL SUPPORT IN UPPER CABIN JUST INSIDE L1 DOOR STA. 303 TO 325 LBL 54. REMOVED AND REPLACED FLOOR SUPPORT AT STA 303-325 LBL 54 IAW SRM 51-40-2 PARA 7, 47550 FAB01 AND ECRA 5312-01158. WORK PERFORMED ON AMES ILN NON-ROUTINE 157SDR CALA2023032200838Keelbeam · corrodedMULTIPLE SPOTS OF CORROSION ALONG KEEL BEAM AREA BS 738.5-1081 RH AND LH SIDES MARKED. REMOVED CORROSION FROM 48EA AREAS ON KEEL BEAM LOWER INBOARD CHORD FROM STA 785.5-1152 LH AND RH. FOUND 0.070" LOSS FROM 0.375" WITH TOOL TAG 16822 TO BE THE GREATEST LOSS ASDR CALA2022092302444None · noneRUDDER RATIO EICAS RUDDER RATIO EICAS FIM FOLLOWED. 27-21 FAULT TREE 804. RH RUDDER ACCOMPLISHED. ALL OPERATIONS NOW NORMAL. RATION CHANGE MODULE REPLACED IAW AMM TASK 27-09-00-022-003 & ROTABLE PARTS CHANGE WAS INDICATED - TT # 1418946 SN OFF 9065 27-09-00-SDR CALA2022091902399None · noneDURING 2SVC LHRMM FOUND EMERGENCY PATHWAY LIGHTS DAMAGED AT 37F, 34F, 38D, 34D. REMOVED AND REPLACED EMERGENCY SEAT MOUNTED AISLE LIGHTS AT 37F, 34F, 38D, 34D IAW AMM 33-51-10-962-104.SDR CALA2022083102222None · noneAUTOTHROTTLE DISC ON T/O SUSPECT TMC COMPUTER NIL STK LHR TMC PLACED ON MEL 3 C/BS PULLED AND COLLARED TMC AC, TMC DC AND PLACARDS INSTALLED. MEL 2230A COMPLIED WITH. 22-02-00-815-801. TMC SERVO ON THE P11.AIRCRAFT DOWNGRADED TO AUTOLAND LIMIT 2, DISPATCH DESKSDR CALA2022032800797Control Module · faultedRTO AT 95KTS DUE TO UNSCHED STAB TRIM MSG REMOVED AND REPLACED LEFT STAB TRIM CONTROL MODULE I.A.W FIM 27-09 FAULT TREE 813. OPS CHECK NORMAL AS PER AMM 27-09-00-422-008. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1785251 SN OFF 1997 IPC REFERENCE # 27-09-00 SDR CALA2021112502173Fmc · failedR FMC FAIL ITEM LOCKED BY TOMC ON OTHER FMC INPUT BUS. TMC FINDS NO DATA ON FMC DATA BUS, MCDP P-11, FAULT CLEARED AND UNABLE TO DUPLICATE AGAIN. ....WITH RIGHT FMC. AND REPLACED LEFT FMC WITH NEW PART. S/N NO INFC L-R FMC DATA. CROSS CHANNEL ACTIVITY MONITOR SDR CALA2021030800274Skin · crackedCRACK FOUND APPROX 1.125" LONG AT STR13AL BETWEEN BS1654-1674 WHILE ACCOMPLISHING EA 5380-01178 OPS 001 SKIN INSPECTION. FUSELAGE SKIN CRACK REPAIRED BETWEEN STA1654-1674 STR 13AL IAW SRM 53-80-01 REPAIR 7 FIG 201 DETAIL VII CAT B REPAIR. REF TABLE 202 FOR IQ SDR CALA2021030800273Stringer Splice · crackedB767-53-3-7154 AFT CGO STA 1300-1307 S-38R SPLICE FOUND CORRODED AND CRACKED REF NR LP 9131244 AFT CARGO STA 1300 TO STA 1307 S38R STRINGER SPLICE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 AND ATTACH FORM 44.0008 ITEM 1-6 ACCOMPLISHED.SDR CALA2021030500259Floorbeam · corrodedB767-53-3-7062 CABIN STA 325 LBL 53 FLOOR BEAM FOUND CORRODED AS MARKED REF NR LP 9131170 CABIN STA 325 LBL 30" TO LBL 60" FLOOR BEAM REPLACED AS PER SRM 53-00-51 REPAIR 1 FIG 201 AND ATTACH FORM 44.0008 MAINTENANCE WORKSHEET ITEM 1-30.SDR CALA2019110301882Switch · out of positionAFTER DEPARTURE VMO NEVER EXCEEDED 260 KTS CAUSING RETURN TO E WR. FOUND S591 ALTERNATE VMO/MMO SWITCH IN THE "ALTN" POSITION. POSITIONED SWITCH TO "NORM" AND LOCKWIRED. AIR SPEED NOW CHECK GOOD UP TO 420 KNOTS ,ALSO PERFORMED LOW LEVEL LEAK CHECKS ALL GOOD SDR CALA2019090901508Battery · dischargedSUPPORT TASK - GALLEY NR 6 LWR CLG EMERG LIGHT FOUND DIM - REF NR LP 9131314. EMER LT BATTERY EQ NR M734 REPLACED AND LAMP TEST RESULT NORMAL AS PER AMM 33-51-07.SDR CALA2019090901509Battery · dischargedSUPPORT TASK - EMER LIGHT L391 AND L644 FOUND DIM - REF NR LP 9130467. EMER LIGHT BATTERY PACK M733 AND CHARGER REPLACED AND LAMP TEST RESULT NORMAL AS PER AMM 33-51-07.SDR CALA2019041200569Fairing · missingLEFT ENGINE INTERMEDIATE CASE STRUT FAIRING MISSING, 9 O''CLOCK STRUT UPPER SIDE. INTERMEDIATE CASE FAIRING MISSING FROM L/H ENG 9 O CLOCK POSITION NEEDS TO BE REPLACED BEFORE 51 HOURS OF OPERATION. PER TABLE 601 AMM 72-34-05-206-005. NO OTHER DAMAGE OR LOOSE SDR CALA2019041200566Fairing · missingINTERMEDIATE CASE STRUT FAIRING MISSING FROM LT ENG S/N 724379 AT THE 9 O CLOCK POSITION LOOKING FWD FROM THE AFT OF ENGINE. REF GMM 02-30-95 PDA PROGRAM CAT 2 APPROX SIZE OF PANEL 14" X 6" IAW AMM 72-34-05 MISSING FAIRING IS TO BE REPLACED BEFORE THE 51ST HOUSDR CALA2018072301683Actuator · fracturedRT MAIN LANDING GEAR LT DID NOT ILLUMINATE GREEN UPON LANDING, GEAR UNSAFE LIGHT DID ILLUMINATE. LANDING GEAR REPAIRED AS PER REF ECRA 3210-02463. ALL OPS CHECKS COMPLIED WITH, WITH NO DEFECTS NOTED AT THIS TIME. PERFORMED REQUIRED INSPECTIONS OF WORK ACCOMPLI
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