N364CM
Service difficulty reports · 112
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 = 'N364CM' 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 = 'N364CM' 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 ABXA20260917427Battery · defectiveDURING INSP/MTC, 2 EACH EMERGENCY LIGHTS INOP, SUPERNUMERY AREA. REPLACED BATTERY PACK AT POSITION M736 PER B767 AMM 33-51-07. SYSTEM CHECKS NORMAL. A/C RETURNED TO SERVICE.SDR ABXA20260916412Smoke Goggles · deterioratedDURING INSP/MTC, FOUND FO SMOKE GOGGLES DETERIORATED. REMOVED F.O. SMOKE GOGGLES. REPLACED WITH SERV. GOGGLES IAW AMM 25-64-00. NO DEFECTS NOTED. ACFT RETURNED TO SERVICE.SDR ABXA20260901377Resistor · faultedDURING TAXI EMERGENCY DOORS LIGHT ILLUMINATED. CREW RETURNED TO THE BLOCKS (BTB). REMOVED AND INSTALLED RESISTOR 59032 IAW B767-WDM 52-71-12, PERFORMED PSEU BITE TEST IAW B767 FIM 32-09 FAULT TREE803, BITE TEST GOOD. A/C REMAINS NO ETOPS AND RETURNED TO SERVISDR ABXA20260901392Skin · dentedDURING C-CHECK, INSPECTION AT FUSELAGE SKIN, LOWER SKIN PANEL, AT BS 1373, BETWEEN STR 27R AND ABOVE STR 29R WAS FOUND DENTED OUT OF SRM LIMITS 53-00-01, FIG 101, DETAIL 3 AND WHILE PERFORMING SRM 53-00-01, REPAIR 14, FOUND DOUBLER TO STOP ON AN INTERNAL DOUSDR ABXA20260901391Skin · corrodedDURING C-CHECK, CORROSION WAS OBSERVED ON THE RT WING UPPER SURFACE SKIN PANEL NR 1 AT WS 434 OVER UPPER RIB FLANGE PIN 113T1545-6, THE DAMAGE WAS REMOVED BY BLENDING AFFECTED AREA IAW SRM 51-10-02 WITH MEASURED MATERIAL REMAINING OF0.112 INCHES FROM INITIAL TSDR ABXA20260901390Skin · damagedDURING AN INSPECTION, LEFT WING LOWER SKIN EXISTING BLEND REPAIRS AT WS 110, STRINGER 10 WAS FOUND. THE AFFECTED FASTENERS WERE REMOVED, AND HFEC ROTO AND SURFACE INSPECTIONS WERE ACCOMPLISHED WITH NO ADDITIONAL DAMAGE. THE BLEND AFFECTS SKIN PANEL AND SKIN PASDR ABXA20260901389Skin · corrodedDURING C-CHECK AT AMES (TPA), DURING STRUCTURAL INSPECTION OF THE RIGHT-WING TOP SKIN PANEL NO.1 UPPER SURFACE, CORROSION WAS FOUND AT WS 350 UNDER WING FIXED TRAILING EDGE PANEL 113T1609-2. CORROSION WAS REMOVED BY BLENDING AND FOUND TO BE OUT OF LIMITS PER SSDR ABXA20260901388Skin · corrodedDURING C-CHECK, DURING STRUCTURAL INSPECTION THE LT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION BETWEEN RS 300.105 AND RS 323.281, UPPER REAR SPAR AREA STRG-1. CORROSION WAS BLENDED IAW SRM. DAMAGE REPAIRED IAW FVCI EO 26099-5, & ABX-REA-5513-SDR ABXA20260901387Skin · corrodedDURING C-CHECK, DURING STRUCTURAL INSPECTION THE LT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION BETWEEN RS STA 300.105 AND RS STA 323.281, UPPER REAR SPAR AREA STRG-1. CORROSION WAS BLENDED PER SRM. ENGINEERING CONTACTED FOR FURTHER EVALUATION ANSDR ABXA20260901386Skin · corrodedDURING C-CHECK, LT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX" 3" LONG AT 165" FROM FUSELAGE BODY. (AROUND FASTERNERS) FOUND WITH CORROSION BETWEEN RS STA 160 AND RS STA 180, UPPER REAR SPAR AREA STRG-1. CORROSION WAS BLENDED PER SRSDR ABXA20260901385Skin · corrodedDURING C-CHECK, LT HORIZONTAL STAB, UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX" 3" LONG AT 8" FROM FUSELAGE BODY. (AROUND FASTERNERS) LT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION BETWEEN RS STA 13.986 AND RS STA 30.605, UPPER REASDR ABXA20260901384Skin · corrodedDURING C-CHECK, RT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX 2" LONG AT 70"" O/B SIDE. (AROUND FASTERNERS) RT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION AT RS 275.605, UPPER REAR SPAR AREA STRG-1. CORROSION WAS BLSDR ABXA20260901383Skin · corrodedDURING C-CHECK, RT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX" 2" LONG AT 47" FROM OTBD SIDE. (AROUND FASTERNERS) RT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION BETWEEN RS 290 & RS 310, UPPER REAR SPAR AREA STRG-1) COSDR ABXA20260901382Skin · corrodedDURING C-CHECK, RT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APPROX 3" LONG AT 22" FROM OTBD SIDE & 2.5" FWD OF REAR SPAR. (AROUND FASTERNERS). CORROSION BLENDED IAW SRM. DAMAGE REPAIRED IAW FVCI EO 26099-10 AND ABX-REA-5513-66201SDR ABXA20260901381Skin · corrodedDURING C-CHECK, RT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX 4" LONG AT 161" FROM FUSELAGE BODY. (AROUND FASTERNERS) CORROSION WAS BLENDED IAW SRM. DAMAGE REPAIRED IAW FVCI EO 26099-7, & ABX-REA-5513-66193-00.SDR ABXA20260901380Skin · corrodedDURING C-CHECK, R/H HORIZONTAL STAB UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX 5" LONG AT 95" FROM FUSELAGE BODY. (AROUND FASTERNERS) FOUND CORROSION BTWN RS STA 104.105, UPPER REAR SPAR AREA AND STRG 1. CORROSION WAS BLENDED IAW SRM. ENGINEERING SDR ABXA20260901379Skin · dentedDURING C-CHECK & INSPECTION, FUSELAGE SKIN, LOWER SKIN PANEL AT BS 1373, BTWN STR 27R & ABOVE STR 29R WAS FOUND WITH A DENT OUT OF SRM LIMITS 53-00-01, FIG 101, DETAIL 3, & WHILE PERFORMING SRM 53-00-01, REPAIR 14, FOUND DOUBLER TO STOP ON AN INTERNAL DOUBLERSDR ABXA20260514202Lamp · inoperativeEQUIPMENT COOLING SMOKE DISCRETE LIGHT WON'T ILLUMINATE DURING TEST ON GROUND BY MTC. RELAMPED EQUIPMENT COOLING SMOKE DETECTOR LAMP PER B767 AMM 21-58-19. OPS CHECK SATISFACTORY. A/C REMAINS NO ETOPS. A/C RETURNED TO SERVICE.SDR ABXA20260409159Skin · crackedDURING A-9 CHECK, WO 16376144 EXTERNAL DVI OF FUSELAGE SKIN, FORWARD SERVICE DOOR (R1) FOUND 1INCH CRACK ON AFT LWR CORNER AFTER REMOVING AFT SCUFF PLATE. , FOUND CRACK TOTAL LENGTH 3.5 INCHES,FOUND TO BE OUT OF LIMITS. CALLING . MAINTENANCE REPAIRED CRACKESDR ABXA20260404146Control Handle · bindingGEAR HANDLE LEVER GETS JAMMED DURING ACTUATION. HAD TO CYCLE IT TO LOCK IN POSITION MTX GROUNDED A/C MTX PERFORMED OPERATION OF LANDING GEAR RETRACT & EXTEND HANDLE SEVERAL TIMES IAW B767 AMM 32-31-00. NO DEFECTS NOTED OPS CHECK GOOD.RETURNED A/C TO SERVICE..SDR ABXA20260127028Stringer · corrodedCORROSION,FOUND UPPER AND LOWER SKIN PANEL, AND S-36R STRINGER, STA 1241 TO 1263 . THIS AIRCRAFT WAS RECEIVING A HARD LANDING INSPECTION IN CVG AND BULGED SKIN WAS FOUND AT STA 1253 ALONG S-36R. FURTHER INVESTIGATION REVEALED CORROSION BEYOND THE SRM LIMITS OSDR ABXA20251106289Sensor · defectiveDURING TAXI, RIGHT ENGINE N1 STARTED ON 2 STARTS AND NO N1 INDICATION ON SEI SHOWS 0. AIRCRAFT RETURNED TO BLOCKS (BTB). REMOVED AND REPLACED N1 SPEED SENSOR IAW B767 AMM 77-12-01. OPS CHECK GOOD. A/C REMAINS ETOPS 180. STANDBY INDICATOR REINSTALLED IAW BSDR ABXA20251019275Smoke Goggles · crackedDURING INSPECTION, MAINTENANCE FOUND SMOKE GOGGLE CRACKED AT SUPERNUMERARY MID SEAT. REMOVED AND REPLACED SMOKE GOGGLE AT SUPERNUMERARY MID SEAT PER REF. AMM 25-64-00. AIRCRAFT RETURNED TO SERVICE.SDR ABXA20250924238Cdu · odorON CLIMBOUT, THERE WAS A STRONG ODOR OF ELECTRIC WIRE BURNING. EMERGENCY DECLARED. AIR TURN BACK (ATB) TO CVG. REF LP 39228-63/3 & 39228-65/2 FOR TROUBLESHOOTING & WORK PERFORMED. NO DEFECTS NOTED. LP 39228-63/3 PERFORMED INSPECTION OF ALL C/BS & PACK BAYSSDR ABXA20250911222Fmc · intermittentON TAXI OUT, RIGHT FMC MOMENTARILY BLANKED. A/C RETURNED TO BLOCKS. (BTB). DEFERRED IAW MEL C ABX-34-61-1-1A. REMOVED AND REPLACED R FMC IAW B767 AMM 34-61-01. OPS CHECK GOOD. A/C RETURNED TO SERVICE.SDR ABXA20250715160Warning Message · false activationON TAXI, RUDDER RATIO ON EICAS MSG., ALL HYDRAULIC PRESSURES NORMAL. AIRCRAFT RETURNED TO BLOCKS. (BTB) ACCOMPLISHED OPERATIONAL TEST OF RUDDER AND RUDER TRIM CONT IAW AMM 27-21-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR ABXA2025621133Start Valve · defectiveDURING PUSHBACK, #2 ENGINE RIGHT ENGINE STARTER VALVE INOP. AIRCRAFT RETURNED TO BLOCKS. (BTB) . DEFERRED IAW MEL C ABX-80-00-2-1. REPLACED RH ENGINE START VALVE IAW AMM 80-11-02 / 401. DI 63480 REMAINS OPEN DUE OPS CHECK PENDING. RH ENG START VALVE OPS SDR ABXA20250430087Engine · power lossABORTED TAKEOFF (ATO) SLIGHTLY UNDER 80 KTS. RT ENGINE MADE TO POWER, HOWEVER, LT ENGINE ONLY MADE IT TO 88% N1. AIRCRAFT RETURNED TO BLOCKS. (BTB). RAN ENGINES AT TAKEOFF POWER WITH EEC'S OFF, ENGINES MADE TAKEOFF POWER IAW 71-00-00, ITEM TRANSFERRED TO DSDR ABXA20250123021Heater · malfunctionedAFTER PUSHBACK CAPT PITOT DISCREET LIGHT ILLUMINATED W/ EICAS MSG A/C RETURNED TO GATE(BTB) AND MTX GROUNDED AC MTX PERF FIM 30-31 FT 805 WITH PITOT HT BREAKER PULLED (CAPT) AND TEST SWITCH HELD WARMING LIGHT NEVER ILLUMINATES, VERIFIED NO POWER TO K241 CURRESDR ABXA20250117019Fmc · odorDURING MAINTENANCE PRE FLIGHT THE F/O FMC CDU BURN SMELL AND C/B P11 E29 POP OUT. MTX GROUNDED AC DEFERRED PER MEL 34-61-1-1A MX PROCED C/W PLACARD INSTALLED A/C RELIESED NO ETOPS .VERIFIED WARN ELEX STATIS MSG.NOT IN VIEW SEE LOG 39126-13/1 FOR ABX REA-3060-6SDR ABXA20250106502Warning Light · illuminatedDURING CLIMB MAIN CARGO DOOR LIGHT ON AT 30.0' AND EXSTINGUISHED AT 20.0' AC RETURND TO FIELD (ATB) AND LANED MTX GROUNDED AC.MTX DEFERRED MAIN CARGO INDICATION FOR DEPARTURE IAW MEL-ABX-52-71-1-2 . AND RETURNED AC TO SERVICE.SDR ABXA20241215258Control Unit · malfunctionedDURING TAXI OUT C HYD PRIMARY 1 EICAS MESSAGE APPEARED , AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC . TROUBLESHOT, AND REMOVED AND REPLACED ELECTRICAL LOAD CONTROL UNIT IAW B767 AMM 29-11-14 OPS CHECK OK AT THIS TIME . AND RETURNED AC TO SERVICE .SDR ABXA20241210249Warning Message · false activationABORTED TAKE-OFF AT ~75KTS DUE TO WARNING HORNING, RED FLAPS EICAS MESSAGE. AC ABORTED T/O DURING ABORT AFTER EXPENDING, SPOILERS, NOTED REF SPOILER EICAS MESSAGE AFTER ABORT WHILE TAXING NOTED FLAP/SLAT ELEC STATUS MTX GROUNDED AC . UPON INSPECTION FOUND NO ASDR ABXA20241114225Pneumatic System · faultedDURING TAXI THERE WERE NO APU PNEUMATICS. ACFT RETURNED TO GATE (BTB) AND MTX GROUNDED AC . MTX DEFERRED APU. PNEUMATICS FOR DEPARTURE IAW MEL ABX-49-11-1-1 AND RETURNED AC TO SERVICE .SDR ABXA20241023202Pin · no discrepancyON PUSH OUT TOW BAR LOCK SNAPED DUE TO BYPASS PIN NOT INSTALLED AC RETURNED TO GATE AND MTX GROUNDED AC AND COMPLIED WITH INSPECTION OF THE NLG IAW B767 AMM 05-51-29 AND NO DAMAGE NOTED .MTX RETURNED AC TO SERVICESDR ABXA20240916175Oil System · lowRH ENGINE LOW OIL UPON ENGINE START AND PUSH.BACK LH 19 ON START DROPPED TO 18 THEN TO 13 AND STABLE AT 14. RH 21 THEN 17 ON IDLE, NO ISSUES. AC RETURNED TO GATE AND MTX GROUNDED AC MTX CHECKED OIL @ SIGHT GLASS, FULL. EICAS READING 19 LH + 21 RH. SERVICED LHSDR ABXA20240913173Fmc · failedON ROLL OUT TO TAKEOFF LEFT FMC FAIL EICAS MESSAGE DISPLAYED , AC ABORTED TAKE OFF AND TAXIED OFF RUNWAY , THEY PERFORMED QHR AND PERFORMED A FLIGHT CREW DEFFERRAL IAW MEL ABX-34-61-1-1A. AND AC DEPARTED .SDR ABXA20240829166Skin · corrodedDURING MAINTENANCE CHECK DURING INSPECTION CORROSION BEYOND ALLOWABLE LIMITS PER THE BOEING SRM (57-20- 01) AT RH UPPER WING SKIN AT WING STRINGER U-2 TO U-4 AND RUNS UNDER THE RIB CHORD TO SKIN EDGE AT BL 97.95. CORROSION BETWEEN THE SKIN IN THE FASTENER HOLESDR ABXA20240829165Skin · corroded"DURING MAINTENANCE CHECK AT PEMCO (TPA) AND DURING INSPECTION CORROSION BEYOND ALLOWABLE LIMITS PER THE BOEING SRM (57-20-01) AT RH UPPER WING SKIN AT WINGS STRINGER S-15 AND RUNS UNDER THE PLUS CHORD TO SKIN EDGE AT BL 97.95. CORROSION BETWEEN THE SKIN IN THSDR ABXA20240619118Apu · auto shutdownAPU SHUT DOWN AFTER AC LEFT THE BLOCK AC RETUREN TO BLOCKS AND MAINTENANCE GROUNDED AC AND DEFERRED THE APU IAW 49-11-1B AND RETURNED TO SERVICE AND AC DEPARTED .SDR ABXA20240619117Control Panel · faultedCREW DISCREPANCY: CAPT FD NOT SHOWING SELECTED ALTITUDE, ALSO NOT SHOWING TO AND FD AT TOP OF PFD. WENT BACK TO BLOCK. REMOVED AND REPALCED MCP PER AMM 22-11-02. OPS CK GOOD PER AMM 22-00-02, MCDP TEST NO. 4 A/C REMAINS CAT I PENDING MCDP TEST 30/40 SEE LP 386SDR ABXA20240618116Apu · auto shutdownAPU SHUT DOWN DURING PUSH, AC RETURUNED TO GATE AND MANTENANCE GROUNDED AC AND DEFERRED APU FOR FLIGHT IAW MEL ABX-49-11-1A AND RETURNED AC TO SERVICE AC DEPARTEDSDR ABXA20240618115Indicator · faultedLOST FLIGHT DIRECTOR DURING PUSHBACK AC RETURNED TO THE GATE AND MAINTENANCE GROUNDED ACFT AND TRANSFERED POWER FD CAME BACK C/W MCDP GROUND TEST 30 IAW AMM 22-00-01. ALL INDICATIONS NORMAL A/C REMAINS CAT 3B OPERATIONAL RETURNED AC TO SERVICESDR ABXA2024041078Door · unsecureMCD WARNING ANNUCIATORS INDICATOR ILLUMINATED DURING PUSH-BACK , AC RETURED TO THE GATE AND MAINTENANCE CLOSED AND LATCHED MAIN CARGO DOOR IAW B767 AMM 52-32-00 DOOR OPS CHECK GOOD .AC TAXIED OUT AND DEPARTED IN SERVICABE CONDITION ,.SDR ABXA2024031558Apu · shutdownAPU SHUTDOWN ON PUSHBACK AC RETURNED TO THE GATE AND MAINTENANCE GROUNDED AC . AND DEFERRRED THE APU FOR DEPARTURE IAW MEL ABX-49-11-1A AND RETURNED AC TO SERVICE. AC DEPARTEDSDR ABXA20240304151Fseu · faultedDURING ILS 31R AT KJFK, WHEN FLAPS SELECTED TO 25, FLAPS STAYED AT 20. EXECUTED MISSED APPROACH. HELD AT CHANT. DECLARED AN EMERGENCY. REBRIEFED AND COMPLETED VISUAL APPROACH TO 31L. LANDED SAFELY.C/W FSEU BYTE CHECK I/A/W FIM27-51 FT 809. NO FAULTS. INSPECTEDSDR ABXA20231230231Unknown · unknownCAPT FD INOP AND ALT IND ON A/S INOP .A/C RETURNED TO GATE MAINTENANCE GROUNDED A/C .C/W TURNING OFF FLIGHT DIRECTOR AND COMPLETE IRU REALIGNMENT PER AMM 34-24-01 OPS CHECK GOOD ON CAPT'S AND FO'S FLIGHT DIRECTOR A/C REMAINS CAT IIIB STATUS.MAINTENANCE RETUSDR ABXA202312263228Pitot Tube · malfunctionedL AUX PITOT EICAS AND OVERHEAD DISCREATE LT ILLUMINATED AFTER ENGINE STARTED AC RETURNED TO BLOCK AND MAINTENACE GROUNDED AC .T/S FIM PER 30-31 FT. 804, FOUND PITOT FAULTY, REPLACED L AUX PITOT PROBE IAW AMM 34-11-01, PART EFFECTIVITY VERIFIEDPERFORMED L AUX PSDR ABXA2023113210Unknown · unknownRIGHT CENTER FUEL PUMP INOP, CENTER RT PUMP DID NO OPERATE AFTER START OF RIGHT A/C RETURNED TO BLOCK AND MAINTENANCE GROUNDED A/C.DEFERRED SYSTEM IAW MEL 28-22-2A. FOR DISPATCH . AC FLOWN TO LIM . PERFORMED GROUND FAULT INTERRUPTOR OPS TEST. FOUND RELAY K1SDR ABXA20231025206Module · leakingAFTER TAKEOFF EICAS MSG 1) CHYD QTY 2)C HYD 2 OVHT CENTER HYD SYSTEM REAAD 0.16 AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT GROUNDED BY MAINTENANCE. TROUBLE SHOT AND FOUND OUTBOARD SLAT PDU CONTROL VALVE MODULE LEAKING .REMOVED AND REPLACED LEFT OUTB
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