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 ABXA20231018204Unknown · unknownAFTER ENGINE START, CAPT'S AIRSPEED AND ALTITUDE INDICATIONS WERE BLANK. CAPT'S & F/O'S FD'S WERE ALSO BLANK. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. NO EICAS OR STATUS MESSAGES DISCREPANCY STARTED AFTER GPU POWER TRANSFER. GPU HAS AN ELECTRICAL SDR ABXA20230918187Unknown · unknownMN CARGO DOOR LIGHT ILLUMINATED WHILE CLIMBING THRU 5000 FT RAN QRH RETURNED TO KLAX THE LIGHT DISTINGUISHED AFTER 10 MINS AT 7000 LEVEL FLIGHT GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED DOOR INDICATION IAW MEL-52-71-1-2 AIRCRAFT RETURNED TO SERVICE.SDR ABXA20230816176Module · faultedFWD EQUIPMENT SUPPLY VALVES DO NOT AGREE, EICAS MSG FWD EQUIPMENT VALVE. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED AIR SUPPLY MODULE ASSY. IAW B767 AMM 36-23-01. OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.SDR ABXA20230724146Unknown · unknownEMERGENCY LIGHTS FLICKERING OFF AND ON WITH LIGHTS ARMED DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED EMERGENCY LIGHTING IAW MEL 33-51-1C. PLACARD INSTALLED. AIRCRAFT RETURNED TO SERVICE.SDR ABXA20230717145Unknown · unknownON TAXI OUT R HYD. LEVEL WAS INDICATING 0.74 RF. RETURNED TO GATE. AIRCRAFT GROUNDED BY MAINTENANCE. MAINTENANCE SERVICED R HYD SYSTEM TO 1.10 IAW B767 AMM 12-12-01. NO LEAKS NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.SDR ABXA20230627138Unknown · unknownC HYD PRIM 1 EICAS MESSAGE DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED A VISUAL AND FUNCTIONAL CHECK OF THE C1 PUMP SHOWED ALL NORMAL. LOAD TEST AND INDICATIONS NORMAL. NO ISSUES NOTED WITH OPERATION. ALL WORK REF B76SDR ABXA2023041151Unknown · unknownAFTER ENGINE START AUTO SPEED BRAKE APPEARED ON EICAS AND AUTO SPD BRK LIGHT ILLUMINATED ON OVERHEAD PANEL. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED THE AUTO SPEEDBRAKE SYSTEM IAW MEL 27-62-1A. MAINTENANCE PROCEDURES COMPLIED WISDR ABXA2023030631None · noneON PUSH BACK MAIN CARGO DOOR WARNING LIGHT CAME ON. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE CYCLED DOOR SWITCH AND LIGHT EXTINGUISHED. DOOR VERIFIED LOCKED IAW B767 AMM 52-32-22. AIRCRAFT RETURNED TO SERVICE.SDR ABXA20221230159Pump · low pressureL HYD ACMP HAS LOW PRESSURE DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED L ACMP PER AMM 29-11-01 LEAK CHK OK. AIRCRAFT RETURNED TO SERVICESDR ABXA20221101123Aoa · fault messageLH AOA PROBE ON TAXI OUT, AIRCRAFT TO BLOCK AND GROUNDED BY MAINTRNANCE. MAINTENANCE RESET AOA CIRCUIT BREAKER OPS CHECK NORMAL IAW B767 AMM 30-32-00. AIRCRAFT RETURNED TO SERVICESDR ABXA2022092196Control Valve · faultedLH PACK OVERHEAT AND INCREASING TEMP PERFORMED QRH NO HELP. AICRAFT ATB TO CVG AND WAS GROUNDED BY MAINTENANCE. INSPECTED MEL PROCEDURES FOR DI 34798 PROPER MEL PROCEDURES WERE IN PLACE. INSPECTED HEAT EXCHANGERS AND ALL DUCTS FOR BLOCKAGE OR LEAKS NO DEFECTS.SDR ABXA2023050879Skin Panel · corrodedDURING AIRCRAFT CHECK AT AIRBORNE (TAMPA), MAINTENANCE REPORTED CORROSION ON THE RIGHT WING TOP SKIN PANEL NO. 2 (112T3302-4) UPPER SURFACE AT THE FWD SPAR FASTENER LINE AT WS 225. CORROSION WAS REMOVED BY BLENDING AND MINIMUM REMAINING THICKNESS DOCUMENTED ISDR ABXA2023050878Unknown · corrodedDURING AIRCRAFT CHECK AT AIRBORNE (TAMPA), CORROSION WAS FOUND ON THE FORWARD CARGO DOOR LOWER SILL UPPER OUTER CHORD(143T8204-1). THE 2 AREAS OF CORROSION ARE LOCATED AT STA 566 AND STA 610. AREA 1 AT STA 566- ORIGINAL MATERIAL .200 INCH, MATERIAL LOSS OF .0SDR ABXA2023050880Skin Panel · corrodedDURING AIRCRAFT CURRENT CHECK AT AIRBORNE (TAMPA), MAINTENANCE REPORTED CORROSION ON THE RIGHT WING TOP SKIN PANEL NO. 2 (112T3302-4) UPPER SURFACE AT THE FWD SPAR FASTENER LINE. FOUR LOCATIONS OF CORROSION REPORTED OUT OF LIMITS PER 767-300 SRM 57-20-01. LOCASDR ABXA2023050881Beam · crackedAMES NR 0496 - CABIN, STA 903.5 RBL89, RH INNER CHORD(STUB BEAM) TRANSITION RADIUS CRACKED(END MARKED). STUB BEAM REPAIRED PER ABX-EA-5300-0052-101 (REPAIR - INNER CHORD, STA 903.5, RBL89, B767). VENDOR DID NOT REPORT REPAIR TO ABX AIR. THIS WAS DICOVERED BY ASDR ABXA2022071984None · noneWARNING ELEX STATUS MSG ON TAXI OUT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE R&R STALL WARNING CARD IAW B767 AMM 27-32-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICESDR ABXA2022061166None · noneAUTOTHROTTLES DID NOT ADVANCE TO N1 POWERSETTING FOR TAKE-OFF. ABORTED TAKE OFF AT 40 KTS AND RETURNED TO BLOCK. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE RESET THE AUTO-THROTTLE COMPUTER CIRCUIT BREAKERS. PERFORMED MCDP AUTO-THROTTLE TESTS REF B767 AMSDR ABXA2022060362None · noneCENTER FUEL QTY BLANK WITH TOTALIZER DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED CENTER TANK FUEL QUANTITY INDICATION IAW MEL 28-41-1-2. PLACARD INSTALLED. AIRCRAFT RETURNED TO SERVICESDR ABXA2022040439Unknown · crackedAFTER TAKEOFF DURING GEAR/FLAP RETRACTION LOSS OF ALL CENTER HYD FLUID AND PRESSURE. USED ALT FLAP AND GEAR EXTENSION AND RETURNED TO CVG FOR A HEAVY WEIGHT (362,000 #) LANDING. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE FOUND TAIL SKID CONTROL MODULE DSDR ABXA2022012817Valve · faultedDURING TAXI LEFT ENG BLEED EICAS MESSAGE, AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED & REPLACED LH ENG PRSOV IAW B767 AMM 36-11-09. AIRCRAFT RETURNED TO SERVICE.SDR ABXA20211231136Valve · inoperativePARKING BRAKE EICAS MESSAGE WHEN PARKING BRAKE LEVER RELEASED. AIRCRAFT RETURNED TO BLOCK AND WAS GROUNDEDD BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE PARKING BRAKE VALVE 32-44-04 OPS NORMAL. PART EFFECTIVITY VERIFIED. AIRCRAFT RETURNED TO SERVICE.SDR ABXA20211127125Spring · brokenDURING TAKE-OFF ROLL, CAPT’S SEAT ROLLED BACK. ABORTED TAKE-OFF. AS A SIDE NOTE , BRAKE TEMPS WENT TO 7 AND 8’S DUE TO THE ABORTED TAKE-OFF.AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REPLACED BROKEN SPRING ON HORIZONTAL ADJUSTMENT LEVER. OSDR ABXA20211122122None · noneAUTOTHROTTLE DISC LIGHT CAME ON DURING PUSHBACK RETURNED TO GATE AND WAS GROUNDED BY MAINTENANCE. MAINTENANCE CONDUCTED TEST 02 AND 10, NO FAULTS FOUND. REF AMM 22-00-02. A/C RELEASED PENDING TEST 30/40 TO CAT I PLACARD ROTATED.CONDUCTED TEST 30/40 PER AMM 22-SDR ABXA20200803201Module · faultedABORTED T/O FOR RED FLAPS EICAS MESSAGE WITH FLAPS IN THE "5" POSITION, ALSO GOT A "NO LAND 3" FLAG. AIRCRAFT BACK TO GATE, GROUNDED BY MAINTENANCE. BITE CHECK OF PSEU, FSEU AND FSPM'S, SHOW CENTER FSPM WITH MODULE FAULT. REMOVED AND REPLACED CENTER FSPM, ISDR ABXA20200803187Module · intermittentSTAB TRIM EICAS MESSAGE DURING CLIMB OUT OF PTY. FLIGHT WAS SCHEDULED TO SJU, FLIGHT CREW ELECTED TO DIVERT TO MIA. AIRCRAFT WAS GROUNDED IN MIA. MAINTENANCE COMPLIED WITH FIM 27-09 F/T 811 SAM BIT PROCEDURE, PASSED. COMPLIED WITH FIM 27-48 F/T 809, NO STCSDR ABXA2020081703165Module · faultedUNSCHEDULED STAB TRIM EICAS MEESAGE AND AURAL WARNING DURING TAKE-OFF ROLL, ABORTED TAKEOFF AT 85 KNOTS.AIRCRAFT WAS GROUNDED. TROUBLESHOT USING FIM 27-09 FT 813, FOUND STCM FAULT BALL ON THE LEFT SAM, FAULT BALL CLEARED AND SYSTEM TEST NORMAL REMOVED AND REPSDR ABXA20200724152Warning Message · illuminatedUNSCHEDULED STAB TRIM EICAS AND MASTER WARNING ILLUMINATED ON TAKEOFF, ABORTED TAKEOFF AT 60 KNOTS. AIRCRAFT WAS GROUNDED.SDR ABXA20200722150Floor Panel · crackedCRACK AT MAIN CABIN FLOOR BETWEEN STUB FITTING AND FLOOR BEAM. AIRCRAFT WAS GROUNDED.SDR ABXA20200722149Beam · corrodedGOUGE ON LH WING INBD FLAP OUTBD FLAP TRACK AFT FITTING INBD SIDE. AIRCRAFT WAS GROUNDED.SDR ABXA20200722148Skin · crackedCRACK L1 DOOR AT AFT LOWER INNER RADIUS. AIRCRAFT WAS GROUNDED.SDR ABXA20200722147Stiffener · corrodedLH WING SLAT NR 2 INBD PANEL MOUNT FLANGE HAD CORROSION AT OTBD UPPER CORNER; REPLACED. AIRCRAFT WAS GROUNDED.SDR ABXA20200521063Controller · malfunctionedAFT CABIN TEMPERATURE EICAS MESSAGE. AIRCRAFT WAS GROUNDED.SDR ABXA202003063046Control Unit · faultyL HYD QTY EICAS + LHYD SYS PRESS EICAS + RUDDER RATIO EICAS + RT YAW DAMPER EICAS MESSAGES DISPLAYED. HYDRAULIC CONTROL UNIT WAS REPLACED. AIRCRAFT WAS GROUNDED. MAINTENANCE SUSPECTS FAULTY VALVE FOR EICAS MESSAGES.SDR ABXA202001140001Wire · damagedTHE AFT LOWER CARGO DOOR WOULD NOT CLOSE ELECTRICALLY. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE AFT LOWER CARGO DOOR ELECTRICAL SYSTEM'S WIRING WAS INSPECTED. IN THE FORWARD LOWER CARGO COMPARTMENT, DAMAGED WIRES WERE FOUND BEHIND A WALL PANELSDR ABXA2019112202174Guard · out of positionTHE EMERGENCY LIGHT SWITCH DISARMS WHEN THE GUARD IS CLOSED. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE EMERGENCY LIGHTS CAPTURE MECHANISM IN THE SWITCH GUARD WAS REPOSITIONED.SDR ABXA20190618117Panel · missingRIGHT ENGINE PYLON AFT OUTBOARD SIDE PANEL ASSEMBLY IS MISSING PANEL NUMBER 446AL. THE PANEL POSSIBLY DEPARTED DURING OPERATION OF THE AIRCRAFT. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND A SERVICEABLE PANEL 446AL WAS INSTALLED. THE CAUSE OF THE MISSSDR ABXA2019060314110Manifold · separatedTHE LEFT ENGINE 14TH STAGE MANIFOLD ASSEMBLY SEPARATED OUTBOARD OF THE COUPLING AT ONE OF THE ENGINE'S THREE HIGH PRESSURE BLEED PORTS. THIS CAUSED A LEFT ENGINE FIRE INDICATION WITH THE OVERHEAT LIGHT ILLUMINATED IN THE FLIGHT DECK DURING CLIMB AFTER TAKEOFF.SDR ABXA20190220005Blower · faulty"FWD CARGO FIRE" EICAS MESSAGE REPORTED BY THE FLIGHT CREW TO DISPLAY DURING FLIGHT. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE FORWARD LOWER CARGO COMPARTMENT WAS INSPECTED. THERE WAS NO SIGNS OF FIRE. THE FORWARD CARGO SMOKE DETECTOR AIR FLOW BSDR ABXA20190108002Drive Shaft · disconnectedAFTER TAKEOFF, THE “TE FLAP ASYM” EICAS MESSAGE ILLUMINATED. THE LEFT FLAP INDICATOR SHOWED APPROXIMATELY 4 DEGREES OF FLAPS, AND THE RIGHT FLAP INDICATOR SHOWED 5 DEGREES. MOVING THE FLAP LEVER HAD NO EFFECT ON THE FLAPS. THE CREW PERFORMED AN AIR TURN BACK ASDR ABXA2018082017093Skin · damagedEXTERNAL SKIN HAD TWO FASTENER HOLES, AT THE EDGE OF SKIN AT BS 654+22 WAS DAMAGED AT STRINGER 16L. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA2018082017092Beam · corrodedCORROSION ON THE RIGHT WING REAR SPAR TO TRAILING EDGE UPPER PANEL ATTACH BEAM AT WING STATION 280. THE UPPER PART OF THE ATTACH BEAM WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA2018082017091Beam · gougedGOUGES ON THE INBOARD FLAP INBOARD TRAILING EDGE BEAM AT WING STATION 344.3. THE BEAM WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA2018082017090Beam · corrodedCORROSION ON THE LEFT WING REAR SPAR TO TRAILING EDGE, UPPER PANEL ATTACH BEAM AT LWS 285. THE ATTACH BEAM AND UPPER PANEL WERE REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA2018082017088Skin · gougedGOUGE FOUND ON THE SKIN, AT THE AFT EDGE OF THE FORWARD LOWER CARGO DOOR AT BS 618. THE AIRPLANE WAS GROUNDED. THE SKIN WAS REPAIRED.SDR ABXA2018082017087Skin · corrodedCORROSION FOUND ON THE RIGHT WING LOWER SKIN PANEL NR 1, RWS 918. THE AIRPLANE WAS GROUNDED. THE SKIN WAS REPAIRED.SDR ABXA2018082017086Skin · corrodedCORROSION FOUND ON THE RIGHT WING, LOWER SKIN, RWS 924.16. THE AIRPLANE WAS GROUNDED. THE SKIN WAS REPAIRED.SDR ABXA20161209175Unknown · malfunctionedAFTER LANDING, THE LEFT THRUST LEVER WOULD NOT MOVE FROM IDLE FOR ONE MINUTE. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE ADJUSTMENT TEST PROCEDURE WAS PERFORMED IN ACCORDANCE WITH AMM 78-31-00. NO FAULTS WERE FOUND. THE CAUSE OF THE FAULT WITH THSDR IXXA20160818057Angle · corrodedCORROSION INTERIOR OF THE AFT 437BR ACCESS AFT UPPER CORNER, NEAR THE AFT HINGE OF THE LEFT ENGINE NAC STRUT AFT FAIRING. CORROSION WAS BLENDED OUT OF LIMITS, REPLACED THE UPPER ANGLE IN THE HYDRAULIC BAY IN ACCORDANCE WITH SRM 51-40-02 SECTION 7. AIRCRAFT GRSDR IXXA20160821056Splice Plate · corrodedLEFT WING LEADING EDGE LOWER CHORD SPLIT ON EDGE WHERE NUMBER 5 SLAT INBOARD DRIVE ROD DOOR CONTACTS. REMOVED DAMAGE SPLICE PLATE AT LEFT WING STATION 330.475. INSTALLED NEW SECTION OF SPLICE PLATE IN ACCORDANCE WITH 472222REA01 AND SRM 51-40-02. AIRCRAFT GROSDR IXXA20160818053Attach Angle · crackedACFT GROUNDED FOR HEAVY MAINTENANCE. INBD THRUST REVERSER ATTACH ANGLES FORWARD OF CASCADE VANES CRACKED AT 1:00 POSITIONS AS SEEN WITH SLEEVE DEPLOYED. R & R INBD ATTACH ANGLES IAW SRM 51-41-01.
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