N676MC, cancelled Dec 6, 2018
Service difficulty reports · 47
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 = 'N676MC' AND deregistration_id = 'N676MC-2018-12-06' 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 = 'N676MC' AND deregistration_id = 'N676MC-2018-12-06' 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 DALA12000030881Light · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT 6D TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND THE LIGHT RETURNED TO AN OPERATIONAL CONDITION.SDR DALA1219179881Sign · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERWING EMERGENCY EXIT SIGN ON THE LEFT SIDE OF THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EXIT SIGN AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF THE SYSTEM.SDR DALA1154689881Battery · dischargedMAINTENANCE FOUND FIRST CLASS EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERIES PER AMM. AIRCRAFT OK FOR SERVICE.SDR DALA1147039881Fan Blade · brokenDURING TAKEOFF ROLL JUST ABOVE 80 KNOTS A LOUD BANG WAS HEARD FOLLOWED BY AIRCRAFT SHIMMY. FLIGHT CREW ABORTED TAKEOFF AND NOTICED ENGINE NR 2 VIBRATION. ENGINE NR 2 WAS SHUTDOWN. MAINTENANCE FOUND FAN BLADES DAMAGED AND 1 BLADE BROKEN OFF AT THE BLADE ROOTSDR DALA1139919881Fuel Line · disconnectedAIRCRAFT RETURNED TO ATL DUE TO UNCOMMANDED FUEL VENTING FROM LEFT WING TIP IN FLIGHT. FUEL VENTING STOPPED ONLY AFTER CENTER TANK WENT DRY. MAINTENANCE FOUND FUEL LINE AFT OF RIGHT AFT FUEL BOOST PUMP FITTING DISCONNECTED. RE-INSTALLED LINE AND SECURED FITSDR DALA1112849881Skin · crackedMONITOR BLIND FASTENERS-AD-FAR FUSELAGE EXTERIOR FORWARD SERVICE DOOR JAMB AFT LOWER CORNER HAS NDT VERIFIED CRACK AT FASTENER. REPAIR PER 5330-01134-02D. CUT OUT DAMAGED AREA 2.35 INCH BY 1.2 INCH. NDT VERIFIED DAMAGE REMOVED IAW NDT SPM 06-10-01. FABRICASDR DALA1112829881Skin · crackedDURING LCK IN DHN, AN 0.125 INCH LONG CRACK WAS FOUND IN THE FUSELAGE SKIN AT THE FWD CARGO DOOR JAMB CUTOUT, UPPER FORWARD CORNER. WORK PER ER/A 475544-14AD AS FOLLOWS: SECTION I - DURING LCKAT DHN - FEB 2011. SECTION II - WITHIN EVERY 3,000 CYCLES AFTER SECSDR DALA1112809881Skin · crackedDURING LCK AT DHN, A 0.25 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN AT FORWARD SERVICE DOOR JAMB CUTOUT, AFT LOWER CORNER. DFRD STA ATL 22FEB11 ATA 5331. WORK PER ER/A 489370-14AD AS FOLLOWS: SECTION I. DURING LCK AT DHN -FEB 2011, SECTION I - ON OR BEFORE SDR DALA1112619881Angle · crackedMONITOR BLIND FASTENER-LEFT ENGINE PYLON STA 1151 UPPER PYLON TO FUSELAGE ANGLE CRACKED APPROX 1 INCH CUT OUT DAMAGED AREA 2.5 INCH BY 1 INCH. NDT VERIFIED DAMAGE REMOVED IAW NDT SPM 06-10-01. FABBED AND INSTALLED 1 FILLER AND SPLICES. HEAT TREATED TO STA SDR DALA1112389881Channel · crackedNOSE LANDING GEAR STA 106 LEFT LONG 28 CHANNEL CRACKED ON OTBD END APPROX 1/2 INCH. REMOVED ANGLE IAW DC-9 SRM 51-30-2 AND 51-30-5. LOCATED, DRILLED AND INSTALLED NEW ANGLE IAW DC-9 SRM 51-10-4, 51-30-2 AND 51-30-5. BLIND FASTENERS INSTALLED IN ANGLE TO BE SDR DALA1112249881Channel · crackedLT MLG W/W DOOR INTERIOR SIDE FWD ZEE CHANNEL IS CRACKED AT INBOARD END. REMOVED CHANNEL IAW DC-9 SRM 51-30-2,51-30-5 AND 51-30-6. LOCATED DRILLED AND INSTALLED NEW CHANNEL IAW DC9 SRM 51-10-4, 51-30-2, 51-30-5 AND 51-30-6, P-205 Q-948 490448. REQUIRED INSPSDR DALA1111889881Shear Tie · crackedSTA 1190 L14R SHEAR TIE CLIP CRACKED. REMOVED CRACKED SHEAR TIE CLIP IAW DC9 SRM 51-30-5. RECEIVED MATERIAL FOR NEW CLIP. FABRICATED NEW CLIP IAW DC9 SRM 51-10-2, 51-10-4 DWG 9958239. INSTALLED CLIP IAW DC9 SRM 51-30-5. REQUIRED INSPECTION COMPLETED BY QSDR DALA1111779881Shear Tie · crackedAFT ACCESSORY COMPARTMENT-UPON REMOVAL OF CRACKED CLIP UNDERNEATH FOUND SHEAR TIE CRACKED AT LONG 14R FRAME STA 1190. REMOVED CRACKED/DAMAGED SHEAR TIE IAW DC9 SRM 51-30-2,51-30-5. RECEIVED NEW SHEAR TIE LOCATED AND DRILLED NEW SHEAR TIE IAW DC9 SRM 51-10-4.SDR DALA1113119881Frame · crackedFUSELAGE EXTERIOR AT CANTED FRAME STA 1292 BETWEEN L14L AND L15L SKIN CRACKED. REMOVED EXISTING DOUBLER IAW SRM 51-30-2. REMOVED CRACKED SKIN BY EXTENDING EXISTING CUT OUT IAW SRM 53-04 FIG 12B. HFEC INSPECTION IAW NDTSPM 06-10-01. NO CRACK INDICATIONS. SDR DALA1112789881Skin · crackedFORWARD CARGO DOORJAMB, FORWARD UPPER CORNER HAS APPROX 1/8 INCH CRACK AT FASTENER. CUTOUT DAMAGED SECTION OF SKIN IAW DRAWING SR09530117. HFEC INSPECTED CUTOUT IAW DC9 NDTSPM 06-10-01.001, NO FURTHER CRACKING NOTED. FABRICATED DRILLED, AND INSTALLED REPAIRSDR DALA1112609881Angle · crackedLEFT ENGINE PYLON STA 1116 UPPER PYLON TO FUSELAGE ANGLE CRACKED APPROX 2 INCHES. REMOVED CRACKED ANGLE AND EXISTING SPLICES IAW DC-9 SRM 51-30-2 AND 51-30-5. FABRICATED NEW ANGLE IAW DC-9 SRM 54-10-0 FIG 1 HEAT TREATED ON PEMCO TRAVELER 2478N00306. INSTALLSDR DALA1015779881Battery Pack · dischargedDURING LINE CHECK MAINTENANCE FOUND FIRST CLASS EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED BATTERY PACK AT R1 EMERGENCY EXIT SIGN. OPERATIONAL CHECK OF LIGHTS NOW CHECK GOOD PER AMM 33-53-00.SDR DALA1015769881Power Supply · inoperativeDURING LINE CHECK MAINTENANCE FOUND L1 & R1 EMERGENCY DOOR LIGHTS INOP. MAINTENANCE REPLACED POWER SUPPLY AT L1 DOOR. OPERATIONAL CHECK OF LIGHTS NOW CHECK GOOD.SDR DALA1012119881Battery Pack · inoperativeDURING LINE CHECK, MX FOUND EMERGENCY LIGHTS INOP IN ROW 5-8, 19-22, AND 23-26 INOP. MX REPLACED BATTERY PACKS FOR ROWS 19-22 AND USED SPARE BATTERIES FOR ROWS 5-8 AND 23-26. OPS CHECK OF LIGHTS NOW ALL CHECK GOOD.SDR NWAA094499881Stud · failedDURING PREFLIGHT CHECK, THE PILOT FOUND THAT THE EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE FAILED STUD AND HARDWARE IN THE EXTERIOR EMERGENCY FLOOD LIGHT ASSEMBLY AND FUNCTIONALLY CHECKED IT IAW AMM 33-44-00.SDR NWAA092349881Rib · crackedDURING "M" CHECK FOUND CRACK IN RT WING LEADING EDGE RIB FASTENER HOLE AT STA XCW 124. REPAIRED PER EA 98-215902.SDR NWAA084769881Battery Pack · dischargedDURING LINE CHECK MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WAS INOPERATIVE OR TOO DIM TO BE FUNCTIONAL. MX CHARGED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OP CONDITION.SDR NWAA085029881O-Ring · leakingSHORTLY AFTER TAKEOFF FLIGHT ATTENDANT REPORTED STRONG FUEL ODOR IN CABIN. A SLIGHT FUEL ODOR WAS NOTICED IN THE COCKPIT. FLIGHT CREW LANDED AT DESTINATION. MX NOTICED APU INTAKE PLENUM WET WITH FUEL AND ALSO A FUEL LEAK AT THE APU FUEL HEATER. THE APU ANDSDR NWAA082669881Attach Angle · crackedDURING LINE CHECK FOUND CRACK IN THE RT DORSAL FIN ATTACH ANGLE AT BS 1266. REPAIRED PER EA 98-213301. (A)SDR NWAA082659881Skin · crackedDURING LINE CHECK FOUND CRACK IN FUSELAGE SKIN AT BS 1266 LT BELOW VERTICAL STABILIZER ATTACH ANGLE. REPAIRED PER EA 98-213119. (A)SDR NWAA080529881Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT LIGHTS FOR THE TAIL COMPARTMENT WERE INOPERATIVE. BOTH LEFT AND RIGHT LAMPS WERE CHANGED BUT DID NOT CORRECT THE FAULT. MAINTENANCE THEN REPLACED THE BATTERIES AND THE SYSTEM OPERATIONALLY CHECKED SDR 0600979881Line · leakingWHILE EN ROUTE TO DESTINATION, THE CREW RECEIVED INDICATIONS THAT ALL OF THE HYDRAULIC FLUID IN THE RIGHT HAND SYSTEM HAD BEEN LOST. COM PROCEDURES WERE COMPLIED WITH AND THE FLIGHT CONTINUED TO AN UNEVENTFUL LANDING AT GRR. THE AIRCRAFT CAME TO A FULL STOP SDR 0600149881Rod End · failedWHEN THE LEADING EDGE SLATS WERE SELECTED FOR EXTENSION DURING APPROACH, THE AIRCRAFT ROLLED TO THE RIGHT. CREW NOTED THAT THE BLUE -SLAT EXTEND- LIGHT DID NOT ILLUMINATE AND THE AMBER -SLAT DISAGREEMENT- LIGHT WAS ILLUMINATED. AFTER APPROXIMATELY 90 SECONDSSDR 0600099881Duct · looseWHEN THE LEADING EDGE SLATS WERE SELECTED FOR EXTENSION DURING APPROACH, THE AIRCRAFT ABRUPTLY ROLLED TO THE RIGHT AND THE -SLAT DISAGREE- LIGHT MOMENTARILY ILLUMINATED. MAINTENANCE FOUND THE SLATS ON THE RIGHT HAND WING TO BE BINDING AND OPERATING SLOWER THASDR 0500989881Packing · leakingWHILE INBOUND FOR LANDING AT MYR, THE LEFT HYDRAULIC SYSTEM FLUID QUANTITY WENT TO ZERO AND THE PRESSURE DROPPED. COM PROCEDURES WERE COMPLIED WITH AND THE RIGHT HYDRAULIC SYSTEM FUNCTIONED NORMALLY. NO EMERGENCY DECLARED AND THE AIRCRAFT LANDED WITHOUT INCISDR 0500739881O-Ring · wornDURING APPROACH FOR LANDING AT DTW, THE CREW NOTICED THAT THE LEFT HYDRAULIC SYSTEM FLUID DROPPED TO ZERO QUANTITY INDICATION. COMPLIED WITH COM PROCEDURES AND THE AIRCRAFT LANDED WITHOUT INCIDENT. DTW MAINTENANCE FOUND THE LEFT HYDRAULIC SYSTEM WAS COMPLETESDR 0204149881Engine · malfunctionedCLIMBING THROUGH 8000 FEET, MASTER CAUTION ILLUMINATED. ENGINE NR 1 OIL QUANTITY WAS ZERO AND OIL PRESSURE LIGHT WAS ILLUMINATED. ENGINE NR 1 WAS SHUTDOWN. FLIGHT CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT PERFORMING AN UNEVENTFUL LANDING. MAINTENANCE REPLSDR 0203659981Stabilizer · crackedDuting Hck in ATL, a .25" crack was found in the upper plate of the horizontal stabilizer center section. Repaired per EA 98-190787.SDR 0202069881SwitchWHILE CRUISING AT ALTITUDE, CREW AND PASSENGERS NOTICED A VERY STRONG RUBBER SMELL IN THE CABIN AND COCKPIT. ALSO, THERE WAS EXCESSIVE HEAT COMING FROM OVERHEAD AREA. DISSIPATED DURING DESCENT AT ABOUT 11,000 FEET. FLIGHT DIVERTED TO GRR. MAINTENANCE PERFORMEDSDR 0003759881Battery Pack · inoperativeDURING LINE CHECK, FOUND EMERGENCY LIGHT IN AFT CEILING AND TAIL CONE RELEASE HANDLE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONAL CHECK NORMAL.SDR 0003189881Bulkhead · crackedTAIL INTERIOR- CRACKED LIGHTENING HOLE IN WEB OF LEFT PYLON BULKHEAD AT STA 1209 BETWEEN L11 AND L14. CUT OUT DAMAGED WEB, DRILLED REPLACEMENT WEB FABRICATED DOUBLER PER EA 98-177275 AND SRM 51-30-2.SDR 0000749881Warning Light · illuminatedTHE LEFT ENGINE REVERSER UNLOCK LIGHT INDICATION ILLUMINATED DURING TAKEOFF. TAKEOFF WAS ABORTED AT 101 KNOTS. AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE PLACED THE LEFT ENGINE REVERSER ON MEL 78-1 AND COMPLIED WITH DISPATCH DEVIATION GUIDESDR 9901059881Battery · dischargedDURING LINE CHECK, FOUND EMERGENCY LIGHTING IN FIRST CLASS SECTION INOPERATIVE. MAINTENANCE REPLACED BATTERIES IN EMERGENCY LIGHT POWER SUPPLY, OPERATIONAL CHECK NORMAL.SDR 9808279881Windshield · crackedDURING CLIMB THROUGH FL250, 280 KIAS, CAPTAIN'S WINDSHIELD OUTER PANE CRACKED. FLIGHT RETURNED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE WINDSHIELD.SDR 9721169881Battery · dischargedDURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS INOPERATIVE AT ROWS 2 AND 4. MAINTENANCE REPLACED BATTERIES IN BATTERY PACK B5-24, OPERATIONAL CHECK NORMAL.SDR 9718269881Power Supply · inoperativeDURING LINE CHECK, FOUND 3 EMERGENCY LIGHTS IN GALLEY INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD.SDR 9706469881Slide · low pressureDURING LINE MAINTENANCE INSPECTION, FOUND TAIL CONE SLIDE PRESSURE LOW. REPLACED SLIDE.SDR 9622399881Switch · malfunctionedTAKEOFF WARNING HORN SOUNDED AS TAKEOFF POWER WAS APPLIED. ABORTED TAKEOFF AT 5 KTS AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE RIGHT SLAT SWITCH, OPERATIONAL CHECK NORMAL.SDR 9611979881Battery Pack · dischargedDURING LINE CHECK, FOUND AFT ENTRY DOOR AND TAIL CONE EMERGENCY LIGHTS OUT. REPLACED BATTERIES AND PACKS, OPERATIONAL CHECK OK.SDR 9514439881Torque Links · failedDURING TAKEOFF ROLL, EXCESSIVE VIBRATION FROM NOSE GEAR AREA WAS EXPERIENCED. ABORTED TAKEOFF AT APPROXIMATELY 30 KNOTS AND RETURNED TO GATE. REPLACED THE UPPER AND LOWER NOSE GEAR TORQUE LINKS AND BUSHINGS. AIRCRAFT RETURNED TO SERVICE.SDR 9510069881Clips · out of adjustDURING LINE CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO PULL THE TAILCONE INTERIOR HANDLE FROM THE CLIPS. ADJUSTED THE CLIPS.SDR 9508719881Tires · out of roundABORTED TAKEOFF AT 60 KNOTS DUE TO EXCESSIVE VIBRATION FROM NOSE GEAR AREA. FOUND BOTH NOSE TIRES WITH OUT OF ROUND CONDITION. REPLACED BOTH TIRES. AIRCRAFT RETURNED TO SERVICE.
Back to N676MC, cancelled Dec 6, 2018