N409MC

Service difficulty reports · 236

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 = 'N409MC' 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.

SDR UIEA2011060400273Structure · damagedDURING LOADING OPERATIONS, ENGINE PALLET CAUSED DAMAGE TO FLOORBOARD PANELS BS1500 - BS1625, LBL 85.65 GOUGES/PUNCTURE DAMAGE (REF FIG 1). THE HOLE IS APPROX 30 INCHES LONG BY 2.5 IN. WIDE.Jun 4, 2011 · N409MC · Boeing 74747UF · Fuselage Structure (General)SDR UIEA2011060100270Cdu · inoperativeRIGHT CDU INOP, FROZEN ON POSITION REPORT (REPLACED RT CDU IAW MM 34-61-02, ALL OPERATES NORMAL ).Jun 1, 2011 · N409MC · Boeing 74747UF · Flight Environment DataSDR UIEA2011030200138Skin · damagedEGAT FOUND DAMAGE ON EXISTING REPAIR OF AFT CARGO DOOR (P/N 65B04250-17, S/N 001244) OUTER SKIN AT FOWARD LOWER SIDE AND SEAL RETAINERS (P/N 65B04712-5) IN FEBRUARY 2011.(A PERMANENT REPAIR WAS ACCOMPLISHED PER NRC 346 AND EGAT EL NO. T2011A52B-332. BOEING APPMar 2, 2011 · N409MC · Boeing 74747UF · Cargo/Baggage DoorsSDR UIEA2011022800134Skin · damagedDURING D2-CHECK, A DENT AND A GOUGE WERE FOUND ON RT FUSELAGE SKIN AT BS 2586, S-50R TO S-51R.THE DENT AND GOUGE WERE LOCATED CLOSE TO AN EXISTING EXTERNAL SKIN REPAIR AND THE DENT AND GOUGE WERE BEYOND THE ALLOWABLE LIMIT PER SRM 53-00-01 FIG.101. REPLACED THFeb 28, 2011 · N409MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA2011022300132Skin · dentedDENT DAMAGE IN 65B23701-5 SKIN WAS DETECTED AT BS 529 BETWEEN S23L TO S24L. DEPTH OF DENT WAS .046 INCHES, WIDTH WAS 1.1 INCHES, & LENGTH WAS 1.9 INCHES AS RECORDED PER EGAT NRC 035. TO RESTORE THE TRIMMED OUT AREAS OF 65B23701-5 SKIN TO ITS ORIGINAL STRENGTH Feb 23, 2011 · N409MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA2011021800090Skin · delaminatedMAJOR REPAIR. DURING WALK-AROUND INSP. MX FOUND THE NR 4 RT THRUST REVERSER TRANSLATING COWL WITH DELAMINATION DAMAGE TO THE OUTER SKIN, LOCATED APPROX AT THE 3 O'CLOCK POSITION (REF FIG 1 AND 2). (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESFeb 18, 2011 · N409MC · Boeing 74747UF · Engine Thrust ReverserSDR UIEA2011021600140Bolt · wrong partFWD NR 1, NR 8 BOLT TOO SHORT REF EGAT EI NR T2011A27B-349, REV 00. REPLACED NEW BOLT.Feb 16, 2011 · N409MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2011021400139Access Door · wornWORN ON NR 1 PYLON RT ACCESS DOOR ASSY. REPAIRED DAMAGE AREA IAW T2011A54B-34, REV 00.Feb 14, 2011 · N409MC · Boeing 74747UF · Nacelle/Pylon, Main FrameSDR UIEA2011021100050Control Cable · frayedFWD LT WING SPOILER CTRL CABLE WS1A-3 BROKEN STAND. REPAIRED IAW AMM 27-61-00, REV 70 ADJUSTMENT / TEST.Feb 11, 2011 · N409MC · Boeing 74747UF · Drag Control SystemSDR UIEA2011021100049Control Cable · wornFWD LT AILERON CONTROL CABLE AS-3 WORN OUT. REPAIRED IAW AMM 27-11-00 REV 70. ADJUSTMENT TEST.Feb 11, 2011 · N409MC · Boeing 74747UF · Aileron Control SystemSDR UIEA2011021100048Control Cable · wornFWD LT AILERON CONTROL CABLE AB-9 WORN OUT. (IAW AMM 27-11-00. ADJUSTMENT TEST.)Feb 11, 2011 · N409MC · Boeing 74747UF · Aileron Control SystemSDR UIEA2011021100047Control Cable · frayedFWD RT WING SPOILER CONTROL CABLE WSIA-6: BROKEN STRAND (IAW AMM 20-11-03. REV 70. ADJUSTMENT/TEST).Feb 11, 2011 · N409MC · Boeing 74747UF · Drag Control SystemSDR UIEA2011020900136Skin · damagedDURING D-CHECK INSP OF DATUM ACFT, A SCRATCH AND DENT WERE REPORTED ON THE BULK CARGO DOOR (PN 65B01857-22, SN TLS11203) OUTER SKIN AT THE FWD LOWER CORNER. (THE DAMAGED AREA WAS REPAIRED IAW EGAT NRC 352 AND EGAT EI T2011A52B-363 BY TRIMMING OUT THE DAMAGE AFeb 9, 2011 · N409MC · Boeing 74747UF · Cargo/Baggage DoorsSDR UIEA2011020800086Rib · crackedCRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORIZONTAL STAB STA 441. REPAIRED DAMAGE AREA IAW EI T2011A55B-289 REV 00 AND REV 01.Feb 8, 2011 · N409MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA2011020800085Rib · crackedCRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORIZONTAL STAB STA 450. REPAIRED DAMAGE AREA IAW EI T2011A55B-290 REV 00 AND REV 01.Feb 8, 2011 · N409MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA2011020800084Rib · crackedCRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORIZONTAL STAB STA 467. REPAIRED DAMAGE AREA IAW EI T2011A55B-292 REV 00 AND REV 01.Feb 8, 2011 · N409MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA2011020800083Rib · crackedCRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORIZONTAL STAB STA 493. REPAIRED DAMAGE AREA IAW EI T2011A55B-294 REV 00 AND REV 01.Feb 8, 2011 · N409MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA2011020800082Rib · crackedCRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORIZONTAL STAB STA 527. REPAIRED DAMAGE AREA IAW EI T2011A55B-298 REV 00 AND REV 01.Feb 8, 2011 · N409MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA2011020800081Rib · crackedCRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORZ STAB STA 518. REPAIRED DAMAGE AREA IAW EI T2011A55B-297 REV 00 AND REV 01.Feb 8, 2011 · N409MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA2011020800080Rib · crackedCRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORIZONTAL STAB STA 510. REPAIRED DAMAGE AREA IAW EI T2011A55B-296 REV 00 AND REV 01.Feb 8, 2011 · N409MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA2011020800079Rib · crackedCRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORIZONTAL STAB STA 501. REPAIR DAMAGE AREA IAW EI NO T2011A55B-295 REV 00 AND REV 01.Feb 8, 2011 · N409MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA2011020800078Rib · crackedCRACKED RIB AND LOWER CLIP IN THE FIXED L/E NOSE CAVITY RT HORIZONTAL STAB STA 484. REPAIRED DAMAGE AREA IAW EI T2011A55B-293 REV 00 AND REV 01.Feb 8, 2011 · N409MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA2011020800077Rib · crackedCRACKED RIB AND LOWER CLIP IN THE FIXED L/E NOSE CAVITY RT HORIZONAL STAB STA 458. REPAIRED DAMAGE AREA IAW EI T2011A55B-291 REV 00 AND REV 01.Feb 8, 2011 · N409MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA2011020800076Rib · crackedCRACKED RIB IN THE FIXED L/E NOSE CAVITY, LT HORIZONTAL STAB STA 518. REPAIRED DAMAGE AREA IAW EI T2011A55B-291 REV 00 AND REV 01.Feb 8, 2011 · N409MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA2011020800075Rib · crackedCRACKED RIB IN THE FIXED L/E NOSE CAVITY, LT HORIZONTAL STAB STA 510. REPAIRED DAMAGE AREA IAW EI T2011A55B-287 REV.00 AND REV 01.Feb 8, 2011 · N409MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA2011020800074Rib · crackedCRACKED RIB IN THE FIXED L/E NOSE CAVITY, LT HORIZONTAL STAB STA 501. REPAIRED DAMAGE AREA IAW EI T2011A55B-286 REV 00 AND REV 01.Feb 8, 2011 · N409MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA2011020800073Rib · crackedCRACKED LOWER RIB AND CLIP IN THE FIXED L/E NOSE CAVITY HORIZONAL STAB 458. REPAIRED DAMAGE AREA IAW EI T2011A55B-285 REV 00 AND REV 01.Feb 8, 2011 · N409MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA2011020800072Rib · crackedCRACK - RIB AND LOWER CLIP HORIZONTAL STAB STA 450. FIXED L/E NOSE CAVITY. REPAIR DAMAGE AREA IAW EI T2011A55B-284 REV 00 AND REV 01.Feb 8, 2011 · N409MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA2011020800071Rib · crackedCRACKED RIB AND LOWER CLIP HORIZONTAL STAB STA 441: FIXED L/E NOSE CAVITY. REPAIR DAMAGE AREA IAW EI NO T2011A55B-283 REV 00 AND REV 01.Feb 8, 2011 · N409MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA2011020800070Rib · crackedCRACKED RIB AND LOWER CLIP HORIZONTAL STAB STA 407: FIXED L/E NOSE CAVITY. REPAIRED DAMAGE AREA IAW EI NO T2011A55B-303 REV 00 AND REV 01.Feb 8, 2011 · N409MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA2011020800069Rib · crackedCRACKED RIB AND LOWER CLIP STAB STA 399: LT HORIZONTAL STAB FIXED L/E NOSE CAVITY. REPAIR DAMAGE AREA IAW EI NO T2011A55B-302 REV 00 AND REV 01.Feb 8, 2011 · N409MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA2011020800068Rib · crackedCRACKED RIB AND UPPER CLIP L/E STA 159: LT HORIZONTAL STAB FIXED L/E NOSE CAVITY. REPAIR DAMAGE AREA IAW EI NO T2011A55B-301 REV 00 AND REV 01.Feb 8, 2011 · N409MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA2011020800067Rib · crackedCRACK - RIB AND UPPER CLIP L/E STA 151: LT HORIZONTAL STAB FIXED L/E NOSE CAVITY. REPAIRED DAMAGE AREA IAW EI T2011A55B-300 REV 00 AND REV 01.Feb 8, 2011 · N409MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA2011020800066Rib · crackedCRACK - RIB AND UPPER CLIP L/E STA 145 LT HOR STAB FIXED L/E NOSE CAVITY. REPAIRED DAMAGE AREA IAW EI T2011A55B-299 REV 00 AND REV 01.Feb 8, 2011 · N409MC · Boeing 74747UF · Horizontal Stabilizer, Spar/RibSDR UIEA2011020700057Skin · wornFOUND WEAR ON FUSELAGE SKIN AND VERTICAL FIN SEAL INTERFACE FROM BS 2517 THROUGH 2628 LT SIDE. REMOVED DAMAGED AREA AND CHECKED REWORKED AREA IS WITHIN ALLOWABLE LIMITS IAW SRM 53-00-01. FIGURE 101 DETAIL V. REV 58.Feb 7, 2011 · N409MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA2011020700056Skin · wornFWD WEAR ON THE FUSELAGE SKIN AND VERTICAL FIN SEAL INTERFACE FROM BS 2280 THROUGH 2416 RT SIDE. REMOVED DAMAGED AREA AND CHECK REWORKED AREA IS WITHIN ALLOWABLE LIMITS IAW SRM 53-00-01. FIGURE 101 DETAIL V. REV 58.Feb 7, 2011 · N409MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA2011020700055Skin · wornWEAR FOUND ON THE FUSELAGE SKIN AND VERTICAL FIN SEAL INTERFACE FORM BS 2280 THROUGH 2416 LT SIDE. REMOVED DAMAGED AREA AND CHECK REWORKED AREA IS WITHIN ALLOWABLE LIMITS IAW SRM 53-00-01. FIGURE 101 DETAIL V. REV 58.Feb 7, 2011 · N409MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA2011020700054Skin · wornFOUND WEAR ON THE FUSELAGE SKIN AND VERTICAL F/N SEAL INTERFACE FROM BS 2517 THRU 2628 RT SIDE. REMOVED DAMAGED AREA AND CHECK REWORKED AREA CORD IS WITHIN ALLOWABLE LIMITS IAW SRM 53-00-01. FIGURE 101 DETAIL V. REV 58.Feb 7, 2011 · N409MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA2011013100053Support · crackedTHE SUPPORT AND SKIN PANEL OF LT: LWR FUSELAGE LONGERON BOX FAIRING SUPPORT STRUCTURE CRACKED, S35L. STA 1372. REPAIRED IAW SRM 51-70-07, REV 58 REPAIR DAMAGE AREA.Jan 31, 2011 · N409MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2011013100052Support · crackedTHE SUPPORT AND SKIN PANEL OF RT LWR FUSELAGE LONGERON BOX FAIRING SUPPORT STRUCTURE CRACKED S35R, STA 1372 IAW SRM 51-70-07, REV 58 REPAIR DAMAGE AREA.Jan 31, 2011 · N409MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA201000239Engine · shutdownSHORTLY AFTER TAKEOFF NR1 ENGINE OIL FILTER ILLUMINATED. SHUTDOWN ENGINE. ON ARRIVAL FOUND EICAS SHOWN OIL QTY READING 1 FOR NR1 ENGINE. ON INSP FOUND OIL IN THE TAIL PIPE. CHECKED MAIN CHIP DETECTOR AND "B" SUMP FOUND HEAVY METAL DEPOSIT ON CHIP DETECTORS. Nov 2, 2010 · N409MC · Boeing 74747UF · Engine (Turbine/Turboprop)SDR UIEA2010092300164Cdu · malfunctionedDURING TAKEOFF ROLL CAPT CDU BLANKED , THUS THE CAPTAIN LOSSING T/O SPEEDS(MX SWAPPED LT CDU TO CTR POSITION, LT IRU TO CTR AND SWAPPED LT FMC TO RT AND DEFERRED THE CTR CDU, CTR IRU AND THE RT FMC. ALL SYS OPS NORMAL.Sep 23, 2010 · N409MC · Boeing 74747UF · Attitude Gyro and Indicating SystemSDR UIEA201000198Start Valve · faultyREJECTED TAKEOFF. LOW SPEED EICAS MESSAGE "STARTER CUTOUT 3". START VALVE FOUND FAULTY, ITEM DEFERRED IAW DDG IAW 80-11-01.Sep 15, 2010 · N409MC · Boeing 74747UF · Engine Start Valves/ControlsSDR UIEA2010082300145Seat Track · damagedTHE PURPOSE OF THIS EO IS TO DOCUMENT A MAJOR REPAIR. DURING WALK AROUND INSP, DAMAGE TO THE MAIN DECK BS1820, LBL 98.58. SEAT TRACK DAMAGE WAS FOUND, CRACK MEASURING 14.0 INCH LONG (REF, FIG 1). DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRAug 23, 2010 · N409MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2010060800029Panel · brokenDURING A2-CHECK INSP, MX FOUND THE RT WBL 515 - OTBD MID FLAP L/E & AMP; RT WING FIXED T/E WITH CRACK/DAMAGE. WBL 515 - L/E OF RT OTBD MID FLAP BROKEN . THE DIMENSION IS 0.787 & .787 ) WBL 515 RT WING FIXED T/E FAIRING PANEL BROKEN AT WBL 515.. (1)PERMANENT RJun 8, 2010 · N409MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2010052600007Rib · damagedDURING WALKAROUND, DAMAGE WAS FOUND TO THE TO THE LT WING T/E INBD MID FLAP OTBD T/E COVE RIB. THE REPAIR PER PART 1 OF THIS EO IS CATEGORY C AND REQUIRES REPETITIVE INSPECTION IAW PART 2 OF THIS EO AT 5 CYCLE INTERVALS AND REPLACEMENT AT THE NEXT A-CHECK AFTEMay 26, 2010 · N409MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000191Nozzle · dentedDURING MX WALKAROUND, FOUND A DENT ON THE EXHAUST NOZZLE OUTER SLEEVE AT APPROX THE 6:00 POSITION ON THE NR1 ENGINE. THE DENT IS APPROX 2" LONG AND 0.05 INCHES WIDE AND IS APPROX 42 INCHES FROM THE T/E OF THE NOZZLE. IAW SRM 54-41-30 THE DENT IS OUT OF LIMITS.Mar 23, 2010 · N409MC · Boeing 74747UF · Engine Collector/Tailpipe/NozzleSDR UIEA201000190Fastener · missingA RIVET WAS MISSING AND WAS NOTED ON THE LT WING L/E RIB, OTBD LOF LANDING LIGHT. PERFORMED A TIME LIMITED REPAIR BY INSTALLING A BLIND FASTENER IN LIEU OF A SOLID RIVET. SCHEDULE REPEAT INSPECTIONS AT EVERY 25 FC AFTER PART 1 AND PERMANENT REPAIR PRIOR TO ORMar 16, 2010 · N409MC · Boeing 74747UF · Wing, Rib/BulkheadSDR UIEA201000088Skin · delaminatedLT WING UPPER SURFACE OTBD, ALL OTBD AREA FOUND DELAMINATED. RT WING OTBD AIL UPPER SURFACE DELAMINATED AT SEVERAL LOCATION AS MARKED. LT WING UPPER SURFACE OTBD AILERON REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU 507013-1. Jan 6, 2010 · N409MC · Boeing 74747UF · AileronsSDR UIEA201000090Skin · delaminatedRT WING OTBD AFT FLAP L/E MID AREA FOUND DELAMINATED. RT WING - OTBD AFT FLAP REPAIRED IAW SRM 51-70-07 FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU506866-1. EO 4457A224RA, 4457A225RA.Jan 5, 2010 · N409MC · Boeing 74747UF · Trailing Edge Flaps
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