N477MC
Service difficulty reports · 265
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 = 'N477MC' 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 = 'N477MC' 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 UIEA2026050100287Flap Track · corrodedLHW #4 FLAP TRACK FOUND SURFACE CORROSION AT BEARING PLATE CONTACT AREA(<P>CORROSION REMOVED AND REPAIRED AS PER RI-57-22-18196 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050100288Flap Track · corrodedRHW #5 FLAP TRACK UPPER SURFACE CORROSION AT BEARING PLATE CONTACK AREA(<P>CORROSION REMOVED AND REPAIRED AS PER RI-57-22-18221 REV B. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050400289Liner · tornBULK CARGO STA 2160 LINER FOUND TORN AT SEVERAL LOCATION(<P>CARRY OUT REPAIR AS PER RI-25-54-18224 REV C. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050400290Panel · damagedM/D STA 1720 TO 1780 LH DADO PANEL FOUND DAMAGED(<P>DADO PANEL REPAIRED AS PER RI-25-21-18164 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050400291Panel · damagedM/D STA 1620 TO 1720 LH DADO PANEL FOUND DAMAGED(<P>DADO PANEL REPAIRED AS PER RI-25-21-18163 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050400292Beam · crackedRHW L/E D-BEAM LOWER CHORD AT ILES 690 FOUND CRACK(<P>LOWER CHORD FABRICATED AS PER BOEING DWG 65B12246 AND PL, AND NEW LOWER CHORD REPLACED AS PER SRM 51-10-02, AND NEW LOWER CHORD HOLE TRANSFERRED AS PER SRM 51-40-05, AND NEW LOWER CHORD INSTALLED AS PER SRMSDR UIEA2026050400293Beam · crackedRHW L/E D-BEAM ILES 691 WEB FOUND CRACKED(<P>WEB REPAIRED AS PER RI-57-41-18266 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050500296Stop Fitting · missingRHW L/E TO FRONT SPAR CAVITY ILES 756-766.45 UP STOP FITTING MISSING(<P>STOP FITTING FABRICATED AS PER RI-57-21-18259 REV A, AND NEW FITTING HOLES TRANSFERRED AS PER SRM 51-40-05, AND NEW FITTING INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050600304Panel · damagedM/D LHS BS 1920 - 2020 DADO PANEL FOUND DAMAGED(<P>DADO PANEL FWD CUTOUT GOUGE AND AFT CUTOUT DEFORM AREA REPAIRED AS PER RI-25-21-18165 REV B. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050800306Skin · not enteredAFT CARGO DOOR LOWER FWD CORNER FOUND UNIDENTIFIED EXISTING REPAIR(<P>SKIN REPAIRED AS PER SRM 52-30-01-2R-2 REPAIR 2 FIG 201 DETAIL III. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051000308Beam · crackedRHW L/E D-BEAM LOWER CHORD AT ILES 690 FOUND CRACK(<P>LOWER CHORD FABRICATED AS PER BOEING DWG 65B12246 AND PL, AND NEW LOWER CHORD REPLACED AS PER SRM 51-10-02, AND NEW LOWER CHORD HOLE TRANSFERRED AS PER SRM 51-40-05, AND NEW LOWER CHORD INSTALLED AS PER SRMSDR UIEA2026051700323Fairing · delaminatedLHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700324Fairing · delaminatedLHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.D. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700325Fairing · delaminatedLHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.D. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700326Fairing · delaminatedLHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700327Fairing · delaminatedLHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700328Fairing · delaminatedLHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700329Skin · delaminatedLHW O/B FORE FLAP UPPER T/E FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700330Fairing · delaminatedLHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.C. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700331Fairing · delaminatedLHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700332Skin · delaminatedLHW I/B FORE FLAP UPPER T/E FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700333Skin · delaminatedLHW I/B FORE FLAP UPPER T/E FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700334Fairing · delaminatedLHW I/B FORE FLAP UPPER T/E FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700335Fairing · delaminatedRHW O/B MID FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700336Fairing · delaminatedRHW O/B MID FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700337Fairing · delaminatedRHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700338Fairing · delaminatedRHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700339Skin · crackedLHW I/B FORE FLAP O/B UPPER PNL INNER FOUND CRACK(<P>PERFORMED REPAIR AT CRACK AREA AS PER SRM 51-70-10 REPAIR 4 FIG 202. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026051700340Fairing · cracked#1 PYLON RH T/E FAIRING DOOR FWD INNER SKIN FOUND CRACK(<P>PERFORMED REPAIR AT CRACK AREA AS PER HX RI-54-56-18253 REV.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026052000342Fairing · cracked#1 PYLON LH T/E FAIRING DOOR FWD INNER SKIN FOUND CRACK(<P>PERFORMED REPAIR AT CRACK AREA AS PER HX RI-54-56-18252 REV.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026052000343Fairing · cracked#4 PYLON RH T/E FAIRING DOOR FWD INNER SKIN FOUND CRACK(<P>PERFORMED REPAIR AT CRACK AREA AS PER HX RI-54-56-18250 REV.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026052000344Fairing · cracked#4 PYLON LH T/E FAIRING DOOR FWD INNER SKIN FOUND CRACK(<P>PERFORMED REPAIR AT CRACK AREA AS PER HX RI-54-56-18251 REV.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026012800018Torque Box · crackedAFT CARGO BS 1680 RT TORQUE BOX PANEL FOUND CRACKED. AFT CARGO BS 1660-1680, RBL 30" TO RBL 45.5" TORQUE BOX UPPER SKIN WEB REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-2. NO FURTHER DEFECTS NOTED.SDR UIEA2025112201321Start Valve · warning messageSTARTER CUTOUT MSG. R & R ENG NR 1 ENG START VALVE IAW AMM 80-11-01. OPS CHECKED GOOD, NO FAULTS NOTED. ENG 1 START VALVE STATUS MSG CLEARED.SDR UIEA2025060300718Rivet · looseAPU COMP-WL 310RH STA 2669-2690 FRAME RIVET FOUND LOOSE.(<P>APU COMP-WL290-WL330, STA 2658 - STA2701.5 RH, FUSELAGE EXTERNAL BONDED SKIN ASSY MULTIPLE FASTENER HOLE ELONGATED AREA REPAIRED IAW RI-53-80-17668 REV. A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060500729Fitting · looseRIGHT WING FIXED T/E GROUND SPOILER I/B SUPPORT RIB AT WBL 255.692 UPR FWD SUPPORT FTG LOOSE. RT WING FIXED T/E GROUND SPOILER I/B SUPPORT RIB AT WBL 255.692 UPR FWD SUPPORT FTG 69B11632-14 ASSY REPLACED AND INSTALLED IAW RI-57-51-17673 REV A. NO FURTHER DEFESDR UIEA2024052800455Channel · crackedFOUND M/D R/H TENSION TIE AFT CHANNEL CRACK AT STA 800.(<P>1. REPAIR DAMAGE AREA IAW WORKSHEET 40389 (SRM 53-20-30-2R-1 REV 100) 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024052800456Channel · crackedFOUND M/D L/H TENSION TIE AFT CHANNEL CRACK AT STA 760.(<P>1. REPAIR DAMAGE AREA IAW WORKSHEET 40388 (SRM 53-20-30-2R-1 REV 100) 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024052800457Rib · crackedCRACK- LWR CHORD, UPPER CHORD AND WEB, R/H H.S.T TIP CLOSURE RIB, STAB BL 421.5.(<P>1. ACCOMPLISHED WORKSHEET #40372, SRM 55-10-09-2R-132 REV 100 AND EI T2024A55M-1231, REV 1 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024052800458Cargo Track · corrodedIND M/D CGO FLOOR STRUCTURE SEAT TRACK CORROSION AT STA 1980 RBL 11.33.(<P>1. REMOVE DAMAGE PART IAW SRM 51-40-02-0G-0 REV 100 2. REPAIRED DAMAGED AREA IAW W/S #40379 AND SRM 53-00-52-2R-12 REV 100 3. INSTALLED FASTENERS IAW SRM 51-40-02-4G-0 REV 100 AND DWG #SDR UIEA2024052800459Control Panel · abnormalFOUND ELT REMOTE PANEL FUNCTION ABNORMAL WHEN PFM OPERATIONAL TEST.(<P>IAW AMM 23-24-01/401 REV 110, REPLACED ELT CONTROL PANEL AND PERFORMED ELT CONTROL PANEL INSTALLATION TEST. THE RESULT WAS SATISFACTORY.</P>)SDR UIEA2024052800460Actuator · faultedFND L/H BLG ALTERNATE EXTENSION ELECTRICAL MOTOR CAN'T STOP WHEN PFM OPERATION TEST.(<P>1. IAW AMM 32-35-01-004-001, REV 110 AND AMM 32-35-01-404-007, REV 110 RDL L/H BLG ALTERNATE EXTENSION ELECTRICAL MOTOR. 2. IAW AMM 32-35-00-715-059 REV 110 PFM L/H BLG ALTSDR UIEA2023031200244Fan · unknownSTRONG SMELL OF ELECTRICAL SMOKE IN THE FLIGHT DECK WHILE PARKED AT GATE(<P>REMOVED & REPLACED FWD EQUIP CLNG FAN IAW 21-58-01. OPS CHECK GOOD.</P>)SDR UIEA2023030300199None · noneEQUIPMENT COOLING EICAS MESSAGE ILLUMINATED IN FLIGHT. WOULD NOT EXTINGUISH.(<P>TRANSFER TO MDDR 181366 PER MEL 21-58-04 CAT C, DUE DATE 13MAR2023</P>)SDR UIEA2022050300429Switch · fault messageBLEED 2 EICAS MESSAGE(<P>CMC # 36227 PER FIM TASK # 36-11/940. REMOVED AND REPLACED #2 ENG BLEED AIR OVERPRESSURE SWITCH PER AMM 36-21-03/401. THEN OPERATIONAL TEST WITH ENG RAN, OK PER AMM 71-00-00/501. NO MSG FOUND. A/C OK FOR SVC.<SPAN STYLE="WHITE-SPACE: PSDR UIEA2022042800400Cap · noneFOUND FLOOR BEAM CAP CORROSION AT STATION 2360, RBL 11.33, LBL 39(<P>1) REMOVED DAMAGE PART IAW SRM 51-40-02 REV 94. 2) FABRICATED PART IAW EI # T2022 P53M-1034 REV 0. 3) INSTALLED FABRICATE PART IAW SRM 51-40-02 REV 94 AND BNG NO 65B02634 SH22 REV, U SH 60 RESDR UIEA2022042800401Angle · noneCORROSION- INTERCOSTAL FWD LOWER WING TO BODY FAIRING INTERNAL SUPPORT STRUCTURE, STA 960 / STA 985.73, LBL 3.42 ACCESS PANEL NO 191 DDL(<P>1) REMOVE DAMAGE PARTS IAW SRM 51-40-02, REV 94 2) INSTALL NEW PARTS IAW SRM 51-40-02, REV 94 AND DWG NO 65B06976 SH2 RESDR UIEA2022042800402None · noneCORROSION- LOWER FRAMES. AFT CGO DOOR LOWER LOBE STRUCTURE BETWEEN STA 1810/ STA 1920(<P>1) BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02 REV 94 2) PFM NDT INSP REFER TO JOB CARD ATTACHING SHEET NO 0225742 3) MEASURED REWORK AREA DEPTH = 0-01'', LENGTH = 1.2'' SDR UIEA2022042800403Shear Tie · noneCRACK- FOUND SHEAR TIE CRACK AT STA 1000 RBL 57.5 WL 195(<P>1) REPLACE WITH NEW PART IAW EO 4453C024 PART 9 REV 1 AND EI NO T2022A53M-1112 REV 3 2) THE EI ATTACH TO T/C 6924033 (686) 3) JOB COMPLETED</P>)SDR UIEA2022042800404Shear Tie · noneCRACK- FOUND SHEAR TIE CRACK AT STA 1000 LBL 33.9(<P>1) REPLACE WITH NEW PART IAW EO 4453C024 PART 4 REV 1 AND EI NO T2022A53M-1112 REV 3 2) EI ATTACK TO T/C 6924033(686) 3) JOB COMPLETED </P>)
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