N419MC
Service difficulty reports · 287
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 = 'N419MC' 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 = 'N419MC' 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 UIEA2011072500369Skin · crackedCRACK DAMAGE IN LOWER SKIN ASSY AT BS 983, S38R IN THE DRAG SPLICE FITTING AREA. THE CRACK DAMAGE WAS DETECTED DURING C02 PLUS A3 CHECK AND WHILE COMPLYING WITH SB 747-53A2444, REV 2. NRC 50352 WAS USED TO DOCUMENT THE FINDING OF THE CRACK DAMAGE. (THE ACTIONSDR UIEA2011072300386Frame Splice · crackedA CRACKED HOLE WAS DETECTED ON THE RT BULKHEAD FRAME SPLICE FITTING. THE CRACK (APPROX. 0.03 INCH LONG) IS REMOVED BY OVERSIZING THE HOLE THROUGH THE STACKS TO 0.341 INCH. THE HOLE ON THE SPLICE FITTING ONLY IS OVERSIZED TO 0.505 INCH TO PROVIDE AN INSURANCE SDR UIEA2011071900370Bulkhead Web · crackedAPU COMPARTMENT FWD BULKHEAD WEB, A CRACK WAS FOUND AROUND OTBD FASTENER HOLE AS SHOWN IN FIG 1.SDR UIEA2011071500392Tension Tie · crackedRIGHT BS 720, STR 12 TENSION TIE AREA FOUND 1 EA FASTENER HOLE CRACKED AT FWD CHANNEL C/W 50593(FX RT BS 720 STR 12 TENSION TIE FWD CHANNEL REPAIRED IAW SRM 53-20-30, REPAIR 1, FIG 201.)SDR UIEA2011071500390Tension Tie · crackedFX LT BS 840, STR 10 TENSION TIE FOUND 1 EA FASTENER HOLE CRACKED AT FWD CHANNEL C/W 50513 (FX LH BS 840 STR 10 TENSION TIE FWD CHANNEL REPAIRED IAW SRM 53-20-30, REPAIR 1, FIG 201.)SDR UIEA2011071300393Structure · deformedLEFT BLG INBD W/W DOOR FWD OTBD EDGE WEB DEFORMED. LT BLG INBD W/W DOOR FWD EDGE REPAIRED IAW EO 4452A077.SDR UIEA2011071100389Skin · dentedSECTION 48, LT FX SKIN BS 2420 - BS 2440 BETWEEN STR 25 L 80 STA 26L DENTS / WRINKLING DAMAGE REPAIR. SKIN BS 2412 - 2436 BETWEEN STR 241 - 26L REPAIRED IAW SRM 53-00-01 REPAIR 1, FIG 201.SDR UIEA2011061500316Retainer · crackedDURING WALKAROUND INSPECTION, MX FOUND THE LT BODY GEAR DOOR, SEAL RETAINER LOOSE AND DOOR HINGE WITH CRACK DAMAGE. (REF FIGURES 1 & AMP; 2). (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, SCHEDULE REPEAT INSSDR UIEA2011061200294Pdu · defectiveCARGO PDU PRODUCED ACRID FUMES (REMOVED DEFECTIVE PDU FROM ACFT AND INSTALLED A BLANKING PLATE).SDR UIEA2011052300264Skin · dentedDURING REPLACEMENT OF THE RT LOGO LIGHT, HIGH-LIFT CONTACTED HORIZONTAL STABILIZER LEADING EDGE SKIN - STAB STA 260; CAUSING CREASE/DENT DAMAGE TO THE EXTERNAL SKIN (REF. FIGURE 1), MEASURING 5.0 IN. X 2.0 IN. X 0.156 IN. DAMAGE IS BEYOND THE SRM LIMITS IAW THSDR UIEA2011040700240Seat Track · crackedDURING LOADING, THE BS 1860, RBL 98 MAIN DECK SEAT TRACK WAS FOUND CRACKED. THE DAMAGE MEASURES 14 INCHES IN LENGTH. (FUSELAGE - REPAIR - FWD LOWER LOBE SEAT TRACK AT BS 1860, RBL 98; EO 4453A548 - PART 1 OF THIS EO ACCOMPLISHES A TEMPORARY REPAIR OF THE DAMASDR UIEA2011013100039Skin · damagedDURING PRE-FLIGHT INSP PERFORMED; CREW REPORTED DAMAGE TO THE FUSELAGE SKIN AT BS 2420 - BS 2440 - BETWEEN STR-25L & AMP; STR-25L CONSISTING IN DENTS/WRINKLING (REF FIGURE 1) DIMENSIONS: L:10.0 IN, W:8.0 IN, D:0.140/ L:12.0 IN. W:7.5 IN. D:0.140 THE DAMAGE ISDR UIEA2010122500198Skin · delaminatedDURING WALKAROUND INSP, MX REPORTED DELAMINATION DAMAGE FOUND ON THE RT OTBD MID FLAP - WBL565 L/E PANEL. THE DAMAGE IS LOCATED INBD OF FLAP TRACK, NR 7 MEASURING 24 IN X 16 IN (REF FIG 1). THE DAMAGED AREA EXCEEDS THE SRM 57-53-01, FIG 101, ALLOWABLE DAMAGE SDR UIEA2010121500192Bearing · damagedDURING A-CHECK, WEAR WAS FOUND IN THE NOSE CARGO DOOR - 2L INTERCOSTAL LATCH FITTING BEARING (REF FIG 1). BEARING (PN KPW19-1P) HAS A DENT (SMALL CHIP BROKEN OUT FROM BEARING) MEASURING: 0.224 INCH WIDTH AND 0.10 INCH DEPTH. THE DENT EXCEEDS THE AMM 52-31-06SDR UIEA2010121300190Structure · damagedDURING ROUTINE A-CHECK OF ACFT , THE NR 2 AND NR 4 LT THRUST REVERSER CORE COWL L/E WERE FOUND WITH LOOSE FASTENERS AND BROKEN BONDING MATERIAL. THE NR2 AND NR4 RT T/R CORE COWL L/E'S WERE FOUND WITH BROKEN BONDING MATERIAL. (DISPOSITION IS TO REPAIR ALL THESDR UIEA2010120900188Skin · damagedDURING WALKAROUND INSP AT MST, MX FOUND DAMAGE TO RT OTBD FORE, MID & AFT FLAPS:1. RT OTBD FORE FLAP (PN 65B01901-30) - DAMAGE DETAILS (REF FIG 1): L/E HONEYCOMB DAMAGED /CRACKED/DELAMINATED OVER A LENGTH OF 150 INCH. RT OTBD MID FLAP (PN 65B01925-288) - DAMASDR UIEA2010110900175Skin · damagedTHE PURPOSE OF THIS EO IS TO DOCUMENT A MAJOR REPAIR. DURING REPLACEMENT OF THE HMU ON THE NR3 ENGINE, MX FOUND THE NR3 RT T/R CORE COWL WITH DAMAGE TO THE INSULATION AND THE INNER SKIN OF THE CORE COWL.SDR UIEA2010092900172Thrust Reverser · damagedTHE PURPOSE OF THIS EO IS TO DOCUMENT A MAJOR REPAIR. DURING ROUTINE INSPECTION A-CHECK, MX FOUND THE NR 3 RT THRUST REVERSER CORE COWL WITH A 4.0 INCH CRACK LOCATED APPROX AT THE 1 O'CLOCK POSITION (REF FIG1). OBTAIN ACCESS TO THE NR 3 RT THRUST REVERSER CSDR UIEA201000197Line · leakingENGINE 4, OIL QUANTITY DROPPED TO ZERO BEFORE OIL PRESSURE, REQUIRED ENGINE SHUTDOWN. FOUND OIL D-SUMP LINE AT 4 O'CLOCK POSITION CRACKED. R & R OIL LINE IAW MM 72-53-04 AND 79-21-02. PERFORMED HIGH POWER ENGINE RUN UP. (NR4) IAW MM 71-00-00 AND ALL INDICATIONSDR UIEA2010083100149Rod · brokenDURING WALKAROUND INSP AT STN, DAMAGE WAS DISCOVERED AT RT WBL238.30. FIXED T/E UPPER RIB INSTALLATION CONSISTING IN BROKEN TIE ROD AND CLEVIS. (THE BROKEN ROD WAS REMOVED AND A DETAIL VISUAL INSP WAS PERFORMED TO ASSURE DAMAGE-FREE CONDITION TO THE SURROUNDSDR UIEA2010081700143Skin · delaminatedDURING WALK AROUND INSP AT MX, REPORTED RT NR 14 L/E KRUEGER FLAP EXTERNAL SKIN (EDGEBAND) - DELAMINATION MEASURING 0.4 INCH WIDTH AND 10 PERCENT OF EDGEBAND LENGTH (REF FIG 1). DISPOSITION WAS MADE TO PERFORM TIME LIMITED REPAIR IAW SRM 51-70-02-1A FIG 101 SSDR UIEA2010070900097Skin · dentedDURING SPECIAL CHECK INSP BEING PERFORMED; DAMAGE WAS FOUND TO THE RT WING - INBD & OTBD T/E MID & AFT FLAPS WITH DENT/DELAMINATION AREAS AS DESCRIBED BELOW: RT WING INBD T/E MID FLAP INBD L/E FAIRING DENT (REF N/CR 50072 AND FIG 1). RT WING OTBD T/E AFT FLAP SDR UIEA201000187Floorboard · damagedMX FOUND DAMAGE/DELAMINATION TO THE MAIN DECK - FLOORBOARDS BS 385 LBL 3.75 & BS 410 LBL 4.0 (REFERENCE FIG 1). "DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, INITIATE REPETITIVE DVIS AT EVERY 25 FC AND PERMANESDR UIEA201000139Lens · crackedDMI 16202 LT TAIL NAV LIGHT CRACKED. INSP LT TAIL NAV LIGHT IAW EO4433 A023 FOUND SATIS, NO FURTHER DAMAGE. DMI REMAINS OPEN. AFTER RECEIVING PART, LENS REPLACED & FIC SATUS IAW MM 33-43-01 REV 67 DMI 16202. (CLOSED)SDR UIEA201000166Door · damagedDURING INSPECTION, BODY LANDING GEAR DOORS 8014 TALLY 116 FOUND DAMAGE AND CRACKS ON RT AND LT BODY GEAR WHEEL WELL INBD DOOR. REPAIR IN CONJUNCTION WITH ATTACHED ENGINEERING ADVISE/EMAIL. "STOP DRILLED CRACKS IAW SRM 52-80-02. FIG 101"SDR UIEA201000115Wedge · damagedLT WING INBD AFT FLAP LWR SURFACE T/E WEDGE FOUND HOLE AS MARKED. LTW AND INBD ALT FLAP LOWER SURFACE T/E WEIGHT REPAIRED IAW SRM 51-70-02. FIG 5 AND REF TO PROCESS CARD. CONTROL SEQ NO CHW 505020-1.SDR UIEA201000111Seat Track · damagedM/D BS 1780 - 1820 RBL 75 SEAT TRACK LIP FOUND CHIPPED AND WORN AT SEVERAL LOCATIONS. PERMANENT REPAIR WAS ACCOMPLISHED IAW 747-400 F SRM 53-00-52 FIGURE 201, REPAIR 8.SDR UIEA201000114Skin · damagedFX STA 1920 - S40R BODY SKIN FOUND SCRATCH MARK. FX STA 1920 S, 40R SCRATCH OVERLAPPING SKIN TRIMMED OFF. REPAIRED IAW SRM 53-00-01-2R-10, FIG 201, REPAIR 10 WITHOUT ZERO TIME.SDR UIEA201000113Attach Angle · crackedRT WING - T/E CAVITY FIXED PANEL (OTBD OF NR 12 SPOILER) OTBD ATTACH ANGLE CRACK AT AFT SECTION. RT WING T/E CAVITY UPER FIXED PANEL OTBD OF NR 12 SPOILER OTBD UPPER ATTACH CRACKED ANGLE REPAIRED IAW SRM 51-70-12, FIG 201 REPAIR 1.SDR UIEA201000112Web · crackedM/D STA 1220 TO 1220 BL R117 TO R117 WEB CRACKED. BS 1220 RBL 117 BELOW FLOOR. INTERCOSTAL CRACKED WEB REPARIED IAW SRM 51-70-13. FIG 201, REPAIR 1.SDR UIEA201000110Doubler · crackedLT DOOR UPPER HINGE DOUBLER FOUND CRACK. LT NR 1 DOOR UPPER HINGE AREA CRACKED SKIN AND DOUBLER REPAIRED IAW MSG 2HKA-TLS-09-0009-01C.SDR UIEA201000169Support Angle · crackedDURING OFF LOADING DAMAGE TO THE MDSCD BS 1920 SUPPORT ANGLE FOUND TO BE CRACKED (REF. FIGURE 1). "DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, SCHEDULE REPEAT INSPECTIONS AT EVERY 10FC AND PERMANENT REPAIR ATSDR UIEA201000170Floor Support · corrodedCORROSION AT UPPER DECK GALLEY FLOOR FWD. OTBD SUPPORT FITTING WITH CORROSOIN DAMAGE. DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCIBED IN PART 1 WORK INSTRUCTIONS. SCHEDULE REPEAT INSPECTIONS AT EVERY A-CHECK AND PERMANENT REPAIR AT THE NEXT CSDR UIEA201000167Fairing · damagedDURING WALKAROUND INSPECTION DAMAGE WAS FOUND TO THE LT WING TO BODY FAIRING 191AHL MEASURING APPROX 12.0 IN X 12.0 IN. THE DAMAGE PENETRATED THROUGH THE HONEYCOMB MATERIAL. "DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 OF EO 44SDR UIEA201000168Panel · damagedDURING DAILY CHECK INSPECTION, A 6.0" X 6.0" PORTION OF PANEL 65B15964-267 WAS FOUND MISSING. THE -267 PANEL IS PART OF THE LT WING GEAR WBL 235 LG BEAM TO REAR SPAR LWR IST - IN ADDITION, THE PANEL SUPPORT STRUCTION SHIFTED (BENT) OB 1.0 INN. NDT HFEC INSP ACSDR UIE2008F00013Skin · crackedFOUND FIBERGLASS SKIN PANEL 293CL CRACKED. REPAIRED IAW SRM 53-00-70 AND SRM 51-70-07. (K)SDR UIE2008F00012Skin · crackedFOUND FIBERGLASS SKIN PANEL 294CR CRACKED. REPAIRED IAW SRM. (K)
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