N416MC
Service difficulty reports · 173
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 = 'N416MC' 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 = 'N416MC' 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 UIEA2022052400532Flap · chafedLHW O/B AFT FLAP T/E FOUND CHAFING (95" TO O/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94, FEB20/2022</P>)SDR UIEA2022052400533Flap · delaminatedLHW O/B MID FLAP L/E FOUND DELAMINATION (140" TO I/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94 ,FEB20/2022</P>)SDR UIEA2022052400534Flap · delaminatedLHW O/B MID FLAP L/E FOUND DELAMINATION (107" TO I/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94 ,FEB20/2022</P>)SDR UIEA2022052400535Flap · delaminatedLHW O/B MID FLAP L/E FOUND DELAMINATION (55" TO I/B). PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94 ,FEB20/2022</P>)SDR UIEA2022052400536Skin · delaminatedLHW I/B FORE FLAP AFTER WEDGE UPPER SURFACE O/B AREA FOUND DELAMINATION (26" TO O/B)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94, FEB20/2022</P>)SDR UIEA2022052400537Skin · delaminatedRHW O/B T/E MID FLAP UPR SURFACE AT AFT AREA 135" FROM O/B EDGE FOUND DELAMINATED. PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A REV94, FEB20/2022SDR UIEA2022052500540Attach Bolt · elongatedAFT CARGO STA 1820-1840 RBL 30" MOST R/H HORIZONTAL TORQUE TUBE L/H SUPPORT BEARING ATT BEAM FOUND BOLT HOLE ELONGATED. LOCAL FABRICATE INTERCOSTAL AS PER BOEING DWG 65B06201 & PART LIST AND DOUBLER AS PER BOEING DWG 69B02959 PL AND NEW PARTS INSTALLED AS PERSDR UIEA2022052500541Frame · chafedAPU COMPARTMENT STA 2685 L/H FRAME MID SECTION FOUND CHAFING. FRAME CHAFING AREA REPAIRED AS PER SRM 53-80-07-2R-1 REPAIR 1 REV 94, DATE: 20 FEB 2022</P>)SDR UIEA2022052500542Frame · chafedAPU COMPARTMENT STA 2690 L/H FRAME MID SECTION FOUND CHAFING, FRAME REPAIRED AS PER SRM 53-80-07-2R-1 REPAIR 1 REV 94 DATE 20 FEB 2022</P>)SDR UIEA2022052500543Spoiler · dentedRHW #12 SPOILER FOUND 1EA DENT MARK AS MARKED. PERFORMED METAL HOTBOND REPAIR AS PER SRM 51-70-10 REPAIR 2 AND FIGURE - 203 REV 94 ,FEB 20/2022</P>)SDR UIEA2022052500544Spoiler · dentedLHW #4 SPOILER FOUND 1EA DENT MARK AS MARKED. PERFORMED METAL HOTBOND REPAIR AS PER SRM 51-70-10 REPAIR 4 AND FIGURE - 201 REV94 ,FEB20/2022SDR UIEA2022052600546Bushing · elongated#3 PYLON TORQUE BOX INNER AREA NAC STA 298.93 BLEED AIR DUCT R/H SUPPORT ROD LWR DUCT SIDE ATTACHED BOLT HOLE FOUND ELONGATION LINE REAM 2EA AFFECTED BUSHING HOLES AND FABRICATE 2 EACH BUSHING AS PER HX RI-36-11-15646 REV A</P>)SDR UIEA2022052600547Shear Tie · cracked1EA THROUGH THICKNESS CRACK WAS FOUND ON THE LBL 57.5 SHEAR TIE AS MARKED APPROX 13/4" IN LENGTH AT I/B SIDE & 1 1/4" IN LENGTH AT O/B SIDE. CRACK SHEAR TIE REPLACEMENT AS PER ATLAS AIR EO: 4453C024 REV 1 PART5</P>)SDR UIEA2022052600548Shear Tie · cracked1EA THROUGH THICKNESS CRACK WAS FOUND ON THE LBL 75.92 SHEAR TIE AS MARKED APPROX 1 3/4" IN LENGTH AT I/B SIDE & 1 1/4" IN LENGTH TO O/B SIDE(<P>CRACK SHEAR TIE REPLACEMENT AS PER ATLAS AIR EO: 4453C024 REV. 1 PART 6</P>)SDR UIEA2022052600549Skin Panel · installedFUSELAGE - SECTION 46 - BS 1640 TO 1740 LEFT SIDE AT STRINGER 34 - SKIN PANEL INSPECTION -SB 747-53A2487 R4- AD 2002-23-15. SKIN PANEL MODIFICATION AS PER EO NO.4453A036 FIG 3 AND RI NO. RI-53-60-15609 REV.A</P>)SDR UIEA2022052600550Fitting · damagedFUSELAGE - LONGERON EXTENSION FITTING - BODY STATION 1480 TO BODY STATION 1540 - STRINGERS S-32 TO S-33 (EO4453A818 5& 6). L/R STA 1480 - STA 1540 LONGERON EXTENSION FITTINGS REPLACEMENT AS PER ATLAS AIR EO4453A818 PART 3 4 AND RI NO. RI-53-00-15644 REV.ASDR UIEA2022052700551Fastener · crackedEO 4453A821-1 4 FUSELAGE SKIN NOSE WHEEL WELL FORWARD CORNER DOUBLER INSPECTION AND MODIFICATE (SB 747-53A2851) (L/H FASTENERS & WASHERS DEVIATIONS; DOUBLER S.E.M AND R/H FASTENERS & WASHERS DEVIATIONS FASTENER HOLE CRACK (1EA), L/R DOUBLER INSTALLED AS PER BOSDR UIEA2022052900555Housing · crackedRHW I/B FORE FLAP TO MID FLAP MOST O/B LEVER HOUSING FOUND CRACK. LEVER HOUSING REPLACED AS PER SRM 51-10-01 AND NEW HOUSING INSTALLED AS PER SRM 51-40-02SDR UIEA2022052900556Web · crackedRHW I/B FORE FLAP MOST O/B WBL 410.25 O/B RIB ASSY UPPER CHORD & WEB FOUND CRACKED(<P>LOCAL FABRICATE WEB AS PER RI NO.RI-57-00-15623 REV.A AND REPLACED UPPER CHORD AS PER SRM 51-10-02 AND NEW WEB AND UPPER CHORD INSTALLED AS PER SRM 51-40-02</P>)SDR UIEA2022052900557Structure · crackedREFER WO.790016 RI-57-00-15623 REV A HFEC OPEN HOLE INSPECTION FOUND R/H I/B FORE FLAP O/B RIB ASSY AT WBL 410.25 AT I/B WEB, I/B LOWER CHORD & O/B LOWER CHORD CRACKED. LOCAL FABRICATE I/B LOWER CHORD AND O/B LOWER CHORD AS PER BOEING DWG: 65B39038 AND PART SDR UIEA2020082001833Spar · crackedCRACK ON ONE FASTENER HOLE OF LT WING FRONT SPAR WEB COMMON TO LOWER CHORD AT FSSU 676. ACCOMPLISHED EI NO T2020A57M-1947 REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR UIEA2020082001832Seat Track · corrodedCORROSION DAMAGE ON SEAT TRACK AT STA 2195 RBL 11.33. REPAIR SEAT TRACK, IAW SRM 53-00-52 REPAIR 12 REV 89 AND EI NO T2020A53M-1845 REV 1 DWG 65B38253
SH 54 REV. JOB COMPLETED.SDR UIEA2020082001825Structure · crackedCRACK FOUND WEB CRACK AT RT HST TIP HSBL 421.5. REPAIRED DAMAGED AREA, IAW EI NO T2020A55M-1851 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR UIEA2020082001823Floorbeam · corrodedCORROSION ON LOWER SURFACE OF FLOOR BEAM UPPER CHORD AT STA 1920 NEAR RBL 102.58. ACCOMPLISHED THE JOB IAW EI NO T2020A53M-1985. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR UIEA2020082001824Doubler · corrodedCORROSION ON DOUBLER SPLICE OF MAIN DECK CARGO COMPARTMENT STRUCTURE, BETWEEN STA 1940-1960, RBL 75.92. REMOVED THE CORROSION DOUBLER SPLICE IAW SRM 51-40-02 REV 88. FABRICATE THE DOUBLER SPLICE IAW EI NO T2020A53-1887 REV. 0. INSTALL THE FABRICATED PART IAW SSDR UIEA2020082001826Skin · dentedAIRCRAFT DAMAGE LOG PERFORM CONTROL ITEM NUMBER 2707 LEFT AILERON I/B HAS DENT ON LOWER SIDE. CUT OUT THE DAMAGED MATERIAL AND CLEAN, MEASURE THE DAMAGED AREA (L=2", W=2, D=1.5" FROM INBD EDGE 21" FROM AFT EDGE AT INBD 460 OF LH AILERON SIDE. BOND 4 REPAIR PLISDR UIEA2020082001827Rib · crackedCRACK DAMAGE ON LWR CHORD OF RH HST RIB AT HSBL 421.5. ACCOMPLISHED EI NO T2020A55M-1851 REV 1 THAT ATTACHED TO WD NO. 4824624. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR UIEA2020082001828Web · canningOIL CANNING DAMAGE ON WEB AT AFT CGO COMPARTMENT NEAR STA 1680, RBL 45.50. REPAIR DAMAGED AREA IAW EI NO T2020A53M-1984 REV 2. JOB COMPLETED AND CONDITION CHECK SATISFIED.SDR UIEA2020082001829Floorbeam · corrodedCORROSION ON FLOOR BEAM UPPER CAP AT STA 2240 BETWEEN LBL 50.00 AND LBL 67.01. ACCOMPLISHED JOB IAW EI NO T2020A53M-1983 REV 1 AND SRM 53-00-51-2R-2, REPAIR 3, REV 89. JOB COMPLETED AND CONDITION CHK NORMAL.SDR UIEA2020082001830Floorbeam · corrodedCORROSION ON FLOOR BEAM UPPER CAP AT STA 800 OUTBD OF LBL 98.58. REPAIR FLOOR BEAM IAW EI NO T2020A53M-2046 REV 1. CONDITION CHECK NORMAL AND JOB COMPELTED.SDR UIEA2020082001831Fastener · looseFOUND FASTENERS LOOSENED ON SKIN OF FUSELAGE FROM STA 2658 TO STA 2701.ACCOMPLISH IAW EI NO T2020A53M-1991 REV 2. JOB COMPLETED AND CONDITION CHK SATISFIED.SDR UIEA2020082001834Access Door · dented4 EA DENT ON SKIN P/N 65B02771-1901 OF APU LH ACCESS DOOR. REPAIRED DAMAGED AREA IAW EI NO T2020A52M-1997 REV 1. APPLY YELLOW DOT NO 32597 FOR DENT AREA #1 AND #2, CONDITION "AS IS". JOB COMPLETED AND CONDITION CHECK NORMAL.SDR UIEA2020082001835Seat Track · crackedCRACK DAMAGE ON M/D SUBSTITUTE SEAT TRACK AT STA 1485 LBL 75.92 REPAIRED DAMAGED AREA IAW SRM 53-00-52-2R-13 REPAIR 13 REV 89 AND DWG NO 144420802 SHEET 3 REV B AND DWG NO 65B38251 SHEET 32 REV -. JOB COMPLETED AND CONDITION CHK NORMAL.SDR UIEA2020082001836Structure · crackedFOUND FLOOR STRUCTURE SUBSTITUTE TRACK CRACK AT STA 1480 RBL 75.92. ACCOMPLISHED IAW SRM 53-00-52-2R-13 REPAIR 13 REV 89 AND DWG NO 65B38251 SH 32 REV - AND DWG NO 144U0802 SH 3 REV B. JOB COMPLETED AND CONDITION CHK SATISFIED.SDR UIEA2020040600708Sensor · faultyN416MC REQUESTED TO RETURN TO AMS TO TROUBLESHOOT DEFERRED APU BECAUSE OF SCHEDULE AND GROUND SUPPORT EQUIPMENT AVAILABLE AT RIX, OAI. FLIGHT OPERATION REQUEST.(<P>TROUBLESHOOTING CARRIED OUT PER FIM FOR CMC FAULT 49091. CHECKED INLET PLENUM FOR OBSTRUCTIONS FSDR UIEA2019121076018Fmc · malfunctionedDUAL FMC FAIL IMMEDIATELY AFTER TAKEOFF, FAILED 8-10 TIMES ENROUTE.(<P>PERFORMED FMC L & R GROUND TEST IAW AMM 34-61-00, NO DEFECTS NOTED. PERFORMED FMC L & R SERVO LOOP GROUND TEST, NO DEFECT NOTED.</P><P>LP 1077093 - M6: WHEN GROUND POWER WAS PULLED, PROBLESDR UIEA2019111985929Oil System · abnormal#4 ENGINE OIL QTY DECREASED TO 4 QTS, PRECAUTIONARY ENGINE SHUTDOWN. (<P>REMOVED AND REPLACED #4 ENGINE IAW AMM 71-00-02 AND MCS PACKAGE 59263. LEAK AND OPS CHECK GOOD PER AMM 71-00-00.</P>)SDR P5CA2019091500180Trim System · out of adjustSLOW SPEED (60 KTS) RTO DUE TO CONFIG STAB EICAS MESSAGE & HORN. NO EXCEEDANCES, ABOVE MIN FUEL. CONTINUED AFTER ADJUSTING STAB TRIM. NOTED BY MAINTENANCE. NO MX ACTION REQUIRED, MCC NOTIFIED.SDR P5CA2018112980364Actuator · malfunctionedAIR RETURN FOR #1 FUEL CROSSFEED EICAS MESSAGE AND CONSUMPTION NOTED FROM CENTER TANK(<P>REMOVED AND REPLACED ACTUATOR FOR #1 CROSSFEED VALVE PER AMM 28-22-02. ALL OPS CHECKS NORMAL<BR /></P>)SDR P5CA2018101000308Modulating Valve · faultySTATUS MESSAGE ZONE TEMP WITH ASSOCIATED HIGH FLIGHT DECK TEMPERATURE.(<P>REMOVED AND REPLACED UPPER DECK TRIM AIR MODULATING VALVE PER AMM 21-61-10/401 <BR /></P>)SDR P5CA2018080600178Channel · crackedBS 720, STRINGER 9R, TENSION TIE FWD CHANNEL RADIUS FOUND CRACKED, 0.25 INCH. THE TENSION TIE FWD CHANNEL WAS REPAIRED IAW SRM 53-20-30-2R, REPAIR 1.SDR P5CA2018080600179Fitting · crackedNR 4 ENGINE, LT THRUST REVERSER LOWER ACTUATOR HOUSING FITTING FOUND CRACKED. THE ACTUATOR HOUSING WAS REPAIRED IAW CMM 78-32-02, REPAIR 016.SDR P5CA2018021800041Shear Web · crackedRIGHT WING FIXED TRAILING EDGE GROUND SPOILER INBD SUPPORT RIB, WBL 255.69, SHEAR WEB CRACKED. REPAIRED SHEAR WEB IAW EO 4457A169, PART 2, AND SRM 51-70-13-2R-1, FIGURE 201.SDR P5CA2017101900362Compressor · stalledNR 1 ENGINE COMPRESSOR STALL ON DEPARTURE DURING CLIMB AT APPROXIMATEY 3000 MSL. OPENSDR P5CA2017071600222Oven · failedDURING THE MIDDLE OF CRUISE FLIGHT, CREW OBSERVED VOLUMINOUS SMOKE EMITTING FROM THE GRILL PLATE ABOVE THE OVEN, ACCOMPANIED BY A VERY STRONG ELECTRICAL BURNING ODOR. CREW SHUTDOWN ALL ELECTRICITY IN UPPER GALLEY BY PULLING CIRCUIT BREAKERS. SMOKE GENERATIONSDR P5CA2017040300084Warning Message · illuminatedELEC DRV 1 EICAS ON T/O ROLL AT 70KTS, BRAKE TEMPS MAX 3 AFTER RTO AUTOBRAKE. MX DISC NR 1 IDG PRIOR TO NR 1 ENGINE SHUTDOWN. CARRIED OUT HIGH ENERGY BRAKE INSPECTION, NO DEFECTS NOTED IAW AMM 05-51-10.SDR P5CA2016120300304Escape Rope · abnormalCOCKPIT DESCENT DEVICE EXTEND. REMOVED AND REPLACED IAW 25-61-01.SDR P5CA2016120300307Escape Rope · abnormalCOCKPIT DESCENT DEVICE NR 3 EXTENDED. REMOVED AND REPLACED IAW AMM 25-61-01.SDR P5CA2016120300310Escape Rope · abnormalCOCKPIT DESCENT DEVICE NR 4 EXTENDED. REMOVED AND REPLACED IAW AMM 25-61-01.SDR P5CA2016120300311Escape Rope · abnormalCOCKPIT DESCENT DEVICE NR 5 EXTENDED. REMOVED AND REPLACED IAW AMM 25-61-01.
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